CURRENT PERIODICAL SERIES
PUBLICATION NO. : 14 5 3
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TItLE: U.,S. GOVERNMENT RESEARCH
REPORTS
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VOLUME:
DAItE January - June 196 1
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ISSUES:
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7
Cumulative
Index
Volume 35
January — June 1961
'h'oan Price $1
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OF MIC
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For sale by the Superintendent of Docum^ts, U. S. Government Printing Office, Washington 25, D. C.
U. S. GOVERNMENT
RESEARCH REPO
RTS
Volume 35
January - June 1961
U. S. Department of Commerce
Business and Defense Serviceis Administration
Office of Technical Service s
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4 - '^i'
CONTENTS
Number Index
Subject Index
Source Index
Page
• 1
■ 27
■ 81
t'tfct>nirji.;H
I !
♦ : H
,: .* .j,
?■> ^>■' "-
A I
ill
•
-^
■ , * .
NUMBER
INDEX
\
1
"^ m
'• ■ ■
Numter Pace
Number Pa|p
NuRiter
Par
Number
tsm.
AAL 7-7951 416
AAL Tll-57-36 21
AAL TR-57-77 3»7
AD-US 343
803
AD- 305 694
634
.« * , . " • 1 ■
AAL 7-7951, R-1 3»»
AO-130 462
473
AD- 205 707
610
•_* AAI. 7-7951. R-2 369
AAL TR-S7-29 54t
AD- 121 182
806
AD- 305 745
Ul
^ *■■»*.■
AAL 7-7951. R-3 •»•
AAL TR-57-31 1 '
AD- 121 716
763
AO-206 047
Ttt
■ , , r
AAL 7-7953. R-1 357
AAL TR-57-32 41 ,
AD-123 629
539
AD- 206 051
715
1 • '
( .' * ^ .
AAL 7-7954. R-1 SlO
AAL TR-57-33 tl
'AD-124 114
36
AO- 206 314
29
— "fc ■
I AAL 8-7951. R-7 3M
AAL TR-57-34 -^. I '
AD-124 406
205
AD- 206 691
189
.
1 AAL 8-7954. R-2 X6
AAL TR-57-35 <**■ 1 1
AD- 126 383
362
AD-207 217
721
-'-^
'
AAL 8-7958 270
AAL TR-57-36 311
AD- 1 28 532
618
AD- 207 400
7U
■i t-
AAL 21-01-024 313
AAL TR-57-37 • 91'
AO-129 167
•99
AD-207 4S6
464
■
AAL 22-0601-0002. R-1 394
AAL TR-57-S8 IB
AAL TR-S7-40 S4|l
., AO-129 932
731
AD-207 529
MS
AAL 22-1 201 -(XXXI, SR-1 363
AD- 130 967
769
AD-207 594
327
. ,
• , *• ■ '
AAL 22-1201-0001. R-1 366
AAL TR-57-43 171
AD- 131 259
153
AO-207 7S0
573
j
■ ' • ■ !
AAL 22-1301-0002 770
AAL TR-57-44 U
AD-133 862
49
AO- 207 809
47
J
AAL 22-l301-0nrt». R-1.
AAL TR-57-47 U.
AD- 133 863
130
AO-207 8S6
7W
•cries 2 393
AAL TR-57-48 0
AD- 133 949
548
AO- 297 896
7M
^
1 ' ' •
AAL 22-1301-0009, R-2 271
AAL TR-57-49 Ul
AD-135 202
635
AD- 208 235
M
, . . . "*'
1
AAL 23-1401-0004, RR-1 273
AAL TR-57-50 U»
AO-13S602
689
AD- 208 366
6M
4 ■ 1 *
AAL 22-1401-0005 271
AAL TR-57-51 / 14
AD- 136 254
93
AD- 208 292
739
■
AA1,-TN-S6-1 40S
AAL TR-57-52 l! I
AD- 136 863
716
AD- 208 579
41
»
' . 1 '
AAL-TN-S6-2 464
AAL TR-57-53 : 1
AD- 138 891
553
AD- 208 631
164
..""'*
AAL-TN-S6-3 464
AAL TR-57-54 \ 7
AD- 139 670
542
AD- 208 936
81
^
,
AAL-TN-56-4 46S
AAL TR-57-55 13
AD- 142 102
710
AO-208 937
91
.
AAL-TN-56-5 SW
AAL TR-57-61 1 0
AD- 143 050
601
AO-209 045
710
I
1
AAL-TN-S6-6 441
AAL TR-S8-16 * 3 7
AD- 144 368
335
AD- 209 338
4CI
'
I
, 1
AAL-TN-56-7 405
AAL TR-58-17 11
AD- 144 442
311
AD- 209 391
683
■> . ■ . .. •
AAL-TN-S6-8 411
AAL TR-5e-18 7
AO- 146 632
330
AD- 209 630
7«
•^T ^ , ■ i. . '
AAL-TN-S6-9 40S
AAL TR-58-21 5
AD- 146 789
284
AD- 209 700
617
AAL-TN-56-10 ' 464
AAL TR-58-22 1
AD- 147 496
190
AD-210 0a6
94»
AAL-TN-S6-11 4a>
AAL TR- 58 -23 4
AD-147 553
638
AO- 210 006
399
4i
AAL-TN-56-12 403
AAL TR-58-24 15
AD-147 811
740
AD- 210 113
738
*
* .
AAL-TN-S6-13 440
AAL TR-58-27 , J
AO- 148 554
577
AO-210 114
167
*
AAL-TN-S6-I4 47«
AAL TR-59-1 00
AD- 148 555
577
AO- 210 116
167
'
' ',
AAL-TN-S6-15 478
AAL TR-59-3 23
AD-148 606
430
AO-210 118
49B
1
AAL-TN-5616 403
AAL TR-59-6 18
AD-148 627
732
AD-210 145
41
1 -I
AAL-TN-S6-17 441
AAL TR-59-7 18
AD-I48 801
732
AD- 210 240
7M
,
AAL-TN-56-18 , S»7
» AAL TR-59-8 18
* AAL TR-59-10 IW
AD- 148 930
578
AD-210 287
7a
,• • " ■
AAL-TN-S6-19 403
AD- 148 987
155
AD-210 724
IM
* .' ^
AAL-TN-S6-20 400
AAL TR-59-23 |16
AO-149S04
591
AO-210 8P4
tm.
AAL-TN-56-21 400
AAL TR-59-24 J8
XAL TR-59-25 |M
AD- ISO 401
323
AO-210 805
960
»
AAL-TN-$6-22 400
AD-ilSO 870
A041S2 041
111
AO-210 847
m
• I .
AAL-TN-S6-23 400
AAL TR-60-14 M
494
AD-210 922
75
AAL-TN-S6-24 400
AAL,TR-«0-15 16
AO- 152 443
572
AD-210 938
281
»
AAL-TN-56-25 401
AAL TR-60-16 16
AD- 152 478
62
AD-210 940
221
■
* .
AAL-TN-S6-36 401
AALTR-75-16 19
AO- 152 546
415
AD- 211 059
169
•
' AAL-TN-S6-27 4D1
AliMA-DC-IN-4-S9 737
AD- 152 552
106
AD- 211 215
78
'■■,.,'
AXL-TN-S6-28 ' , 401
ABMADG-TN -59-59 787
AD-153 917
738
AO-211 367
6W
AAL-TN-S6-29 401
ABMA D6P-TR-5-59 797
AD- 155 313
4
AD- 211 296
60
,
AAL-TN-56-30 401
ABMAI RP-TR-2-60 755
AD-ISS 353
764
AD- 211 297
6rr
■ * . .- ,
AAL-TN-56-31 401
Aac TR-59. rev. 29
AO-155 879
37
XD-211 303
7*3
AAL-TN-S6-32 401
'
AD-1S6 360
109
AO-211 322
309
,
♦ ""
AAL-TN-S6-33 401
A£>-76tft 7^4
AD-1S6 541
779
AD- 211 397
337
AAL-TN-S6-34 441
AO-7994 Ip
AD- 157 442
314
AD- 211 414
994
: » -
AAL-TN-56-36 403
AO-10 037 B
AO- 158 023
744
AD- 211 435
' 724
' ' * - ^
AAL-TN-S6-37 399
AD- 10 920 689
AD- 158 218
66
AD- 211 480
191
1 - - ' . '
AAL-TN-S6-38 40S
AO-13 890 537
AD- 158 529
726
AD- 211 487
316
1 ■ ii" - ■ .
AAL-TN-S6-39 39«
AD-13911 587
AD- 158 775
452
AD- 211 496
4U
1 '' ,■ ' ■ "
AAL-TN-57-4 397
AD- 16 351 87
AO-159 318
962
AO-211 536
275
,
1
,•
AA1.-TN-57-5 440
AD- 16 811 6Q
AO- 159 800
9W
AD-211606
453
.
1 ' 1
AAL-TN-57-12 392
AD- 18 814 587
AO- 159 902
100
AD- 211 724
210
.
AAL-TN -57-36 403
AD- 22 410 . 617
AD- 160 OSS
967
AD- 211 733
780
AAL TN-59-18 13
AD- 24 418 »/-
AD- 160 057
967
AO-211 948
331
i.
AAL TN-59-19 12
AO-24 718 6M/
ADrl60a61
567
AD- 211 953
48
•
AAL TN-60-8 12
AD- 36 069 t i'f
AD:^60 869 sufieraeded
166
AD- 212 087
792
f ■ •• .
AAL TN-60-9 it
AD- 30 646 16
AD- 161 563
747
AD- 21 2 110
143
' * *>
AAL TN-60-11 18
AD- 35 462 76 i
AO- 162 022
162
AD- 21 2 194
4S0
AA1--TN-60-14 IS
AD- 35 493 14i
AD 162 607
775
AD- 212 440
101
*
AAL TN-60-19* 716
AD-46 2S1 MN
AD- 200 068
738
AD-212 617
196
*
AAL TN-60-ao 6M
AD-49 219 448
AD -200 649
731
AD-212 748
739
AAL-TN-60-21 785
AD-51 344 773
AO- 200 650
732
AD- 21 2 848
173
* ' ,
AAL TR-57-1 369
AD-S3a65 330
\D - 200 706
719
AD- 212 889
798
■ 1 * •
AAL TR-57-2 ZTi
AD- 54 347 - S9B
M)- 200 945
572
AO- 212 910
637
- 1
♦ AAL TR-57-3 339
AD-54 515 m
AD- 201 159
757
AO-213 228
319
'
>■"'
AAL-TR-57-4 141
AD-63 630 771
AD- 201 225
740
AD- 21 3 430
690
AAL TR-57-5 3»»
AD-71 333 45
AD- 201 450
612
AD- 213 537
349
'
,
AAL TR-57-6 402
AO-82 734 601
AD- 201 524
AD-X1672 f
764
AD- 213 643
494
AAL TR-57-7 « 408
AD-87 968 73
574
AD- 21 3 702
339
.
AAL TR-57-8 3W
AD-93 756 48
AD- 202 672
969
AD- 213 783
300
*
AAL TR-57-9 272
, AD-1G6 522 543
AD- 202 838 /
47
AD-213 899 s.
AO- 214 354 ^-
172
'
AAL TR-57-10 270
AD-10B394 589
AD- 203 696
742
798
1
.*^'
AAL TR-57-11 271
AD- 110 027 S44
AD- 204 097
lit
AO- 214 596
729
AAL TR-57-12 401
■ AD- 1 10 039 4*
AD- 204 225
974
AD- 21 4 597
193
•
AAL TR-57-14 «7t
AO-110050 «9
AD- 204 431
194
AD-214 729
350
- ' . - ^
AAL-TR-57-15 260
AD~110 090 55
AO-205 151
719
AO- 214 843
195
'
AAL TR-57-19 19
AD- 110 608 416
AD- 205 345
992
AO'215 221
787
'
'
AAL TR- 57 -20 2M
AD- 113 786 149
AO-SOS 464
964
AO-215 381
213
1
AAL TR-57-21 317
AD-114 467 294
AO-115 143 540
1
AO-208 517
194
AD- 215 434
808
* ■
AAL TR-5t-24 2M
AD- 205 586
601
AD- 215 454
766
NiBiber
AO-21S 482
AD- 215 625
AO-21S641
AD- 215 MS. r
AD-21S960
AD-21S9M
AD- 216 292
AD- 216 294
AD- 216 2>»5
AD-216 434
AD- 216 556
AO-216 657
AD-216 736
AD- 217 102
AD- 217 169
AD- 217 243
AD- 217 407
AD- 217 515
AX>-217 521
AD- 217 545
AD- 217 614
AD- 217 615
AD-217 6S2
AD-217 980
AD- 217 993
AD- 218 013
AD- 218 374
AD- 218 570
AD- 218 681
AD- 218 842
AD-218 852
AD-21B 886
AD-218 970
AD- 219 0»
AD- 219 061
AD- 219 090
AD- 219 319
AI>-219 334
AD- 219 361
AD-219 685
AD- 219 606
AD- 219 687
AD- 219 750
AD- 219 800
AD-219 846L
AD- 219 882
AO-219 954
AO-219 981
AD- 220 006
AD- 220 099
AD- 220 103
AD- 230 117
AD- 220 201
AD- 220 202
AD- 220 203
AD- 220 204
AD- 230 205
AD- 230 206
AD- 220 241
AD- 230 282
AD- 220 345
AD- 230 531
AD- 230 587
AD- 230 647
AD- 230 653
AD- 230 673
AD- 230 676
AO- 230 812
AD- 220 830
AD- 230 851
AD- 230 853
AD- 225 033
AD- 225 038
AD-22S0S5
AD- 235 104
AD- 225 106
AD- 225 115
AD- 225 130
AD- 235 303
AD- 235 216
AO-22S 275
AD- 225 306
AD- 225 440
AD- 225 462
AO-23S 50r7
AX>-23S548
AD- 235 722
AD-23S794
AD- 225 874
AD- 225 974
A£>-225 975
AD- 226 006
361
AD-236 0B3
307
AD- 236 la
177
AD- 236 245
596
AD- 236 328
173
AD- 235 513
310
AD- 236 520
63
AD- 236 522
580
AO- 236 571
560
AD- 226 573
721
AD- 226 691
t«
AO- 225 695
3
AO-226 834
331
AD- 236 983
329
AD- 227 100
161
AD- 227 147
434
AD- 227 279
783
AD- 227 317
66
AO-237 412
473
AD- 227 460
421
AO- 227 511
38
AD- 227 616
168
AO- 227 622
539
AD- 227 641
433
AD- 227 659
3«
AO- 227 703
410
Ao-ar 709
62»
AD- 227 737
746
AO- 227 830
557 -
AO- 227 821
113
AD- 227 863
601
AD- 227 912
749
AD- 227 919
421
AO- 227 930
798
AO- 227 938
m
AO- 227 943
223
AO- 228 093
411
AO- 228 063
343
AO-23iOM
611
AD- 228 lOB
3X>
AO-238 114
29t
AD- 228 117
337
AD- 228 120
56
AD- 228 13S
181
AD- 228 196
430
AD- 228 164
223
AD- 228 166
176
AO-228 177
339
AD- 228 181
189
AD- 238 212
336
AO-228 250
146
AO-228 367
163
AD- 228 309
7»5
AO- 230 396
766
AO- 228 399
7«6
AO-23S402
766
AO-228 483
766
AD- 228 558
766
AD- 228 594
*»
AO- 2ft 615
44«
AO-238 618
409
AO-228 63S
333
AO- 238 638
343
AO-228 707
343
AD- 229 021
278
AO- 229 040
3S2
AD- 229 041
630
AO- 229 046
m
AD- 229 109
731
AD- 229 112
575
AD- 229 180
339
AD- 229 196
593
AD- 229 236
619
AD- 229 280
336
AX>-229 312
331
AO- 229 361
451
AD- 239 364
134
AD-239S68
683
AD-229»9
61
AO- 229 372
68
AO- 229 379
166
AD- 229 380
682
AO-229 40q
Tn
AO- 229 403
444
AO- 229 434
777
AO- 229 435
192
AD- 229 493
213
AD- 229 494
1S8
AD- 229 511
2'
AO- 229 513
AO- 229 528
a»
AD- 229 532
7Z7
AD- 229 592
Nunter
151
AD- 229 603
793
97
AD- 239 624
9
49
AO- 229 644
19
131
AD- 229 646
78
16S
AD- 229 706
99
102
AD- 229 720
198
805
AD- 229 733 ,
57
297
AD- 229 735
153
408
AD- 229 737
93
111
AD- 229 738
304
142
AD- 229 740
95
351
AD- 229 833
20
343
AO- 229 922
122
341
AD- 229 923
131
376
AD- 229 924 i
121
406
AD- 229 935
121
105
AD- 229 939
191
163
AD- 229 941
63
764
AD- 229 943
113
778
AD- 229 944
213
54
AD- 229 950
107
Z>A
AD- 229 965
338
771 •
AD- 230 009
184
699
AD- 230 010
185
as8
AD- 230 025
48
«4
AD- 230 071
337
795
AO- 230 098
282
723 .
AD- 230 116
118
7a «
AD-230 117
145
lU
AD- 230 120
83
224
AD-230 162
462
191
AO- 230 170
153
191
AO- 230 172
101
SO
AO- 230 184
306
190
AD-230 194
26
70
AD-230 202
r
7SS
AO-230 242
282
311
AD-Z30 243
177
21
AD-230 244
6
76
AD-230 246
8
77
AO-230 248
24
230
AD-230 254
192
64
AD-230 258
36
270
AD-230 259
60
216
AD-230 318
76
55
AD-230 328.
"^i
34
AD-230 329
90^
731
AD-230 332
34
90
AD-230 351
79
5«
AD-230 352
24
101
AD-230 353
r
122
AO-230 385
457
297
AO-230 401
780
730
AO-230 412
721
432
AD-230 420
302
333
AD-230 421
122
721
AD-230 445
8
•Of
AD-230 474
210
62
AD-230 482
47
1^
AD-230 528
762
10
AD- 230 535
9
10
AD-230 536
9
733
AD-230 537
33
146
AD- 230 538
11
106
AD- 230 541
806
738
AD- 230 544
145
194
AD-230 545
6
•8
AO-230 552
43
118
AD-230 558
201
431
AD-230 562
280
111
AD-230 565
280
732
AD-230 596
206
102
AD- 230 598
94
21
AO-230 599
M
89
AD- 230 601
B
81
AD- 230 703
625
7
AD-230 716
767
29
AD-230 730
901
10
AD-230 765
575
17
AD-230 769
798
123
AD-230 794
557
609
AD-230 813
36
49
AD-230 814
541
7*9
AD-230 863
77
769
AO-230 866
64
117
AD-230 867
109
110
AD-230 925
148
29
AD-230 944
5S9
324
AD-230 946
332
77
AD-230 992
596
114
AD- 230 993
738
738
AD- 231 043
396
Number
AD- 231 067
AD- 231 071
AD- 231 098
AO-231 101
AO-231 102
AO-231 106
AO-231 113
AO-231 127
AD- 231 130
AD- 231 142
AD- 231 151,
AD- 231 15X
AD- 231 155
AD- 231 160
AD- 231 182
AD- 231 184
AO-231 213
AD- 231 229
AD- 231 234
AD- 231 241
AD- 231 247
AO-231 252
AO-231 299
AD- 231 313
AD- 231 332
AO-231 346
AD-231 358
AO-231 368
AO-231 372
AD-231 388
AD-231 406
AO-231 409
AO-231 411
AD-231 415
AO-231 422
AO-231 424
AO-231 430
AO-231 434
AO-231 450
.AD-231 464
AD-231 465
AO-231 468
AD-231 473
AD-231 475
AO-231 480
AO-231 493
AO-231 516
AD-231 545
AD-231 562
AD-231 620
AD-231 625
AD-231 641
AO-231 772
AD-231 804
AO-231 817
AO-231 842
AD-231 843
AO-231 844
AD-231 848
AO-231 855
AO-231 860
AO^l 875
AD-231 895
AD-231 897
AD-231, 907
AD-231 919
AD-231 936
AD-231 937
AD-231 951
AD-231 996
AD- 232 010
AO- 232 041
AD- 232 049
AD- 232 064
AD- 232 079
AD- 232 085
AD- 232 098
AD- 232 161
AD- 232 164
AO-232 175
AD- 232 180
• AD- 232 180.
AD- 232 181
AD- 232 188
AD- 232 225
AD- 232 268
■ AD- 232 286
AD- 232 288
AD- 232 289
AO-232 343
AO-232 381
AO-232 388
•<•»»•
9W
777
224
MM
34
730
304
372
9M
399
75
199
346
16
320
7
317
r
212
996
79
5M
337
765
551
579
12
755
496
44
341
59
26
90
330 ~
391
624
212
419
461
Vt
2U
76
606
467
14
549
176
19S
2M
W
711
996
941
109
919
Si
694
46
499
414
364
94
796
99
90
547
219
796
466
399
491
000
792
741
799
92
9
9n
796
279
20S
102
223
211
623
95
164
572
323
/
Number
AD- 232 403
.AO-232 403
AD- 232 410
AD- 232 419
AD- 232 445
AD- 232 446
AO-232 457
AD- 232 486
AD- 232 491
AD- 232 561
AD- 232 562
AD- 232 565
'AD- 232 635
AD-232 636
AD- 232 637
VCD-232 638
AD-232 641
AO-232 644
AD- 232 646
AO-232 656
AO-232 657
AO-232 662
AD- 232 663
AD- 232 679
AD- 232 696
AD- 232 698
AD 232 708
AO-232 716
AO-232 743
AD- 232 743
AD- 232 745
AD- 232 746
AD- 232 752
AD-232 771
AD- 232 815
AO-232 831
AD- 232 835
AD-232 865
AD- 232 880
AD- 232 897
AD 232 911
AO-232 918
AD- 232 922
AD- 232 924
AO- 252 927
AD- 232 931
AO-232 942
AD- 232 947
AD- 232 993
AD- 233 004
AD- 233 022
AO-233 053
AO- 233 061
AD- 233 091
AD- 233 093
AD- 233 098
AD-233 129
AO-233 132
AD-233 147
AO-233 164
AO-233 167
AO-233 168
AD-233 187
AD-233 188
AD-233 212
AD-233 218
AO-233 222
AD-233 243
AD-233 254
AD-233 280
233 291
233 292
233 293
233 340
233 352
1-233 353
233 380
233 406
233 424
233 433
23.'^ 434
1253 457 '
AO-233 477
AD-233 478
AD-M3 480
AD- 233 501
AO-233 50S
AO-233 506
AO-233 509
AO-233 515
AO-233 516
AO-233 575
AD- 233 608
£ME
NiMnfaer
104
AO-233 625
29
AD-233 680
277
AD- 233 687
400
AO-233 688
757
AO-233 706
797
AD-233 722
469
AO-233 723
7S9
AD-233 729
609
AD-233 781
349
AD-233 795
36
AD-233 797
123
AD-233 836
912
AO-233 862
312
AD- 233 889
313
AO-233 898
69
AO-233 902
24
AO-233 959
996
AO-233 969
992
AD- 234 018
442
AD- 234 030
479.
AD- 234 043
54t
AD- 234 049
4IIB
AD- 234 057
KB
AD- 234 060
AD- 234 081
634
AD- 234 066
5r
AD- 234 087
206
AD- 234 107
391
AD- 234 110
265
AD- 234 112
. 11
AO-234 130
496
AO-234 124
4B9
AD- 234 157
199
AO-234 160
]»
AO-234 179
9
AD- 234 184
994
AD- 234 191
2»
, AD- 234 194
33
AD- 234 229
472
AD-234 230
346
AO-234 250
196
1X0-234 268
942
-475
AD-234 295
294
AO-234 296
294
AO-234 359
694
ft AO-234 373
299
AD-234 380
619
AO-234 384
304
AO-234 385
99
AO-234 394
197
AD-234 399
496
AO-234 401
166
AO-234 445
544
AO-234 463
I9t
AD-234 464
639
AO-234 469
462
AO-234 478
2M
AD-234 479
96
AO-234 480
699
AD-234 481
22
AO-234 483
If
AO-234 486
wt
AO-234 487
IT
AD- 254 494
m-
AD-234 511
469
AD-234 515
479
AO-234 541
221
AD-234 544
188
AO-234 552
599
AO-234 553
999
AO-234 555
999
AO-234 560
96
AD-234 584
9
AD-234 599
199
AD-234 629
611
AD- 234 659
40S
AD-234 684
99
. .'AD-234 691
99
AO-234 693
4t4
AD-234 700
9
AO-234 701
47
AO-234 709"
906
AO-234 724
199
, AO-234 729
469
AO-234 732
<n
AO-234 743
199
AD-234 747
47
AO-234 751
546
AO-234 775
980
AO-234 784
335
AO-2S4794
468
AO-234 795
rsE
Nianfaer
£H!
Ntmber
567
AD-234 797
M6
AO-235 651
289
AD-234 798
191
AD-235 654
479
AD-234 814
933
AO-aS665
790
AD-234 831
968
AO-a5 684
333
AD-234 837
698
AD- as 699
418
AD-234 865
454
AD- as 755
148
AD-234 866
436
AO-235 769
83
AO-234 894
436
AO-235 774
693
AD-234 910
552
AO-235 778
775
AD-234 912
276
AD- 235 785
110
AD-234 915
213-
AD- as 788
342
AO-234 916
276
AO-aS 795
449
AD-234 918
187
AO-a5 804
618
AD-234 919
106
AO-aS806
407
AD-234 920
341
AO-aS 832
619
AD-234 921
213
AD-235 833
767
AD-234 927
966
AD-235 848
69
AD-234 938
451
AD- as 849
606
AD-234 945
185
AO-235 859
38
AD-234 946
194
AO- 235 860
34
AD-234 957
470
AO-aS 902
148
AD-234 972
35
AD- as 929
696
AD-234 974
5
AD- as 934
535
AD-234 998
306
AO-aS940
82
AD- 235 010
422
AD-235 942
395
AD- 235 018
326
AO-aS947
395
AD- 235 019
195
AO-a5 996
606
AD- 235 020
551
AO- 236 057
282
AD- 235 027
768
AO- 236 065
472
AD- 235 030
686.
AO- 236 095
203
AD- 235 033
993
AD- 236 163
343
AD- 235 037
309
AO-236 164
624
AO- 235 038
308
AO-236 193
25
AD- 235 042
718
AD- 236 201
433
AD- 235 043
768
AO-236 205
614
AD- 235 058
464
AD- 236 206
433
AD- 235 059
707
AD- 236 208
556
AD- 235 064
45t
AO-236 215
792
AD- 235 065
461
AO-236 219
43
AD- 235 066
453
AO-236 230
453
AD-235 061
187 jG
196 ''
AO-236 225
587
AD- 235 092
AO-236 255
192
AD- 235 093
AO- 136 262
80
AD- 235 094
333
AO-236 263
192
AD- 235 095
187
AO-236 3a
335
AD- 235 096
196
AO-236 337
31
AD- 235 140
147
AO-236 371
442
AD- 235 143
987
AD- 236 376
162
AD 235 144
698
AD- 236 377
161
AO-235 151
166
AD- 236 406
278
AD- 235 155
147
AD- 236 453
171
AD- 235 161
180
AO-236 454
278
AD- 235 186
333
AO-236 458
760
AD- 235 198
395
AO-236 460
477
AD- 235 210
419
AO-236 461
131
AD- 235 212
279
AO-236 466
222
AD- 235 213
196
AD- 236 467
193
AD- 235 21J
918
AO-236 500
155 ,
AO-235 2Bl>
197
AO-236 519
31
AD-235«L
594
AO-236 593
413
AD- 235 289
339
AD- 236 670
696
AD- 235 304
783
AO-236 709
625
AD-235 312
316
AD-236 727
625
AD 235 316
554
AO-236 728
571
AD- 235 319
^
AD- 236 729
188
AD- 235 340
551
AO-2S6 735
285
AD- 235 354
6r
AD- 236 737
733
AD- 235 374
165
AD- 236 738
30
AD- 235 377
187
AO-236 747
172
AD- 235 385
194
AO-236 749
184
AD- 235 391
459
AO-236 750
547
AO-235 398
299
AO-236 751
750
AO-235 436
196
AO-236 752
148
AD- 235 428
998
AD- 236 753
136
AD- 235 436
179
AO-236 754
303
AD-235 445
696
AO- 236 758
460
AD- 235 447
99t
AO-236 787
332
AD-235 450 Mk
AD- as 453 ft
308 .,
AD- 236 811
393
799 '
AD- 236 817
398
AO-235 466
554
AD- 236 847
179
AO-235 468
i'*
AO-236 861
145
AD-235 532
*214
AD- 236 862
86
AO-235 539
707
AD- 236 865
602
AO-aS 570
215
AD- 236 942
330
AD- as 571
1*1
AO-236 967
594
AD- 235 577
791,
AD- 236 960
332
AD-235 581
480
AO-236 973
162
AD-a5 6l2
341
AO-236 999
564
AD-235 627
215
AD-B7 04S
591
AD- as 629
211
AO-a7 049
636
AD-235 631
230
AO-a7 05l
276
AD- 235 637
54
AO-a7 052
408
AD- as 641
144
AD- 37 099
432
463
221
783
552
542
960,
466
569
200
196
6a
258
260
154
172
448
547
347
474
214
799
603
699
727
199
46
172
596-
61^
59^
«4
470
151
449
410
788
458
169
796
615
331
618
458
470
632
178
295
296
599
765
603
471
259
12
639
600
453
182
307
548
285
475
452
602
760
565
595
535
534
535
535
535
535
535
7a
599
413
333
33
189
138
561
140
949,
1*9
721
324
631
32
624
409
470
Number
AO-ZS7 07S
AD- 237 090
AO-237 KM
AD- 237 109
AD- 237 116
AD- 237 130
AD- 237 151
AO-Z37 244
AD- 237 414
AO-237 432
AD-B7 4B
AX>-237 4M
AD- 237 499
AD- 237 442
AO-237 445
AD- 237 4»4
AD- 237 455
AO-237 459
AD- 237 493
AXV237 494
AD-237S04
AD- 237 560
AD- 237 572
AD- 237 619
AO-2S7 63t
AO-ir 631
AD- 237 634
AD- 237 635
AD- 237 641
AD- 237 643
AD- 237 643
AD- 237 691
AO-237 711
AD- 237 728
AD-2S7 7S2
AD- 237 753
AD- 237 754
AD- 237 755
AD- 237 757
AD-B7M9
AO-237 115
AD- 237 S39
AD- 237 832
AD- 237 164
AD- 237 165
AO-2r •66
AO-237 a67
AD-237a6«
AD- 237 920
AO-237 925
AO- 237 957
AO-237 967
AD- 237 96S
AD- 237 970
AD- 236 000
AD- 236 034
AD- 238 035
AO- 236 036
AD- 236 040
AO- 236 049
AO- 236 066
AO-2SaaM
AO-236aM
AD-23S 109
AD- 236 114
AD- 236 IV
AX>238 153
AD- 230 1S6
AO-Z38 165
AD- 236 168
AD- 236 169
AD-2S« 177
AD- 238 205
AD- 238 226
AD- 238 248
AO-238 2S5
AD-2M2M
AO-2S8 2M
AD-238 2M
AD- 238 299
AD- 238 346
AD- 238 360
AO-238 376
AD- 238 433
AD- 238 436
AD- 238 443
AO- 338 472
AD- 238 479
AD- 238 481
AO-238 539
AO- 338 614
AD- 338 636
AD- 238 669
AD- 338 740
«M
AO-238 764
IM
AD- 238 MS
•07
AO- 238 709
804
AD- 238 786
32
AO-238 8Z3
585
AD- 238 923
697
AO-ZS8 923
630
AD- 238 961
463
AO-238 967
S«7
AD- 237 969
7«t
AD- 238 973
6*5
AD- 238 983
6U
AD- 238 991
338
AO-238 992
3M
AO-238 99S
•07
AD-238 997-
79i
AD- 239 004
•07
AD- 239 006
304
AD- 239 007
618
AD- 239 043
595
AD- 299 044
11*
AO-2W063
«3D
AO- 239 064
M7
AD- 239 106
594
AO- 239 108
737
AO- 239 138
621
AO-2S9M6
637
AO- 339 170
S«
AD- 239 177
s«
AD- 239 181
m
AO-239 227
136
AO- 239 242
•9
AO-239 362
444
AO-239 280
364
AO-239 332
666
AO-239 361
396
AD- 239 376
396
AD- 239 399
539
AD- 239 400
323
AD- 239 404
33
AD- 239 436
538
AD- 239 463
74^
AO-239 464
599
AO-239 476
79
AD- 239 486
123
AO-2S9SS7
234
, AD- 239 548
636
AD- 239 602
107
AO-239 645
759
AD- 239 651
52 '
AD- 239 652
609
AD- 239 653
394
AO-239 690
796
AD- 239 691
m
AO-239 696
708
AO-239 764
708
AD- 299 772
7W
AD- 299 771
HH
AD- 299 777
S70
AD- 239 778
771
AD- 299 826
149
AD- 239 830
621
AO- 339 832
734
AD- 299 869
IS
AO-239 875
723
AD- 239 876
683
AD- 239 896
324
AD- 239 919
578
AO-239 923
616
AD-239 92S
803
AD- 239 941
687
AO-239 942
n -'
AO-399 954
n'^
AO-2M963
387
AD- 299 964
703
AO- 299 979
S60
AO-239 97*
SOB
AO- 299 994
7U
AO-240 011
273
AO- 240 024
113
AO- 240 025
594
AO- 240 028
774
AO- 240 036
704
AO- 240 047
42
AO- 340 073
289
AD- 240 087
789
AD- 240 097
383
AO-240 128
70S
AO-240 134
764
AD- 240 144
109
AD- 240 159
788
AO-240 160
196
AD- 240 177
319
AD-240 17«
1
993
783
684
796
44
•7
3M
117
310
389
•83
639
986
602
768
695
tm
Til
761
947
702
171
160
791
S<3
983
90
795
703
95
635
691
786
447
Number
f^
N«Mnber
r
-
Nvmber
NinU»r
P>E
-J y
Nianber
Number
AD- 240 179
796
AO- 242 359
197
AD- 243 545
141
AO-244 7S6
ri
AO-245 504
874
AO-346 449
AD- 240 180
796
AD- 242 361
9«
AD- 243 547
460
AO-244 757
368
AO-245 509
30
AO-246 455
AD- 240 192
577
AO- 242 362
Uf
AD- 243 568
799
AO-244 767
390
AD-245 513
9S7
AD- 246 491
AO-240 194
94
AD- 242 408
7W
AD- 243 601
109
AO-244 771
299
AD- 245 523
•«
AO-246 496
AD- 240 361
303
AD- 242 414
' n
AO-243 614
986
AD- 244 779-
575
AD-245 524
941
AO-246 500
AO-240 283
786
AD- 242 415
SB
-
AD- 243 621
4ST
AD- 244 788
584
AD-245 540
470
AD- 246 506
AD- 240 285
297
AD- 242 437
$79
AD- 243 632
S»
AD- 244 789
584
AO-245 548
SM
AD- 246 506
AO-240 287
SS4
AO- 242 445
TOB .
AD- 243 658
. m
AD- 244 798
761
AD-245 549
991
AD- 246 507
AD- 240 299
388
AD-242 4S4
MB
AD- 243 718
M4
AD- 244 8I9L
325
AD-245 562
799
AD- 246 510
AD- 240 310
439
AO-242«57 * 151' 1
AD- 243 719^
>»9
AD- 244 833
324
AD-245 565
AD-245 572
te
AO-246 513
AO-240 322
81
AO- 242 468
TU.
• !
AD- 243 734
»
AD- 244 841
409
469
AO-246 515
AO-240 350
259
AD- 242 475
AD- 243 746
•97
AD- 244 842 ,
552
AD-245 575
381
AO-246 519
-AD- 240 379
745
AO-242 485
m
AD- 243 750
AD- 243 76r
«»
AO-244 855
362
AD-245 581
907
AO-246 523
AD- 240 389
684
AD- 242 505
107
78
AO-244 6S6
362
AD-245 607 »
258
AD- 246 530
AD- 240 400
719
AD- 242 504
107
AD- 243 792
749
AD- 244 858
336
AD-245 613
471
AD- 246 540
AD- 240 483
84
AO-242 506
107
AD- 243 793
749
AD- 244 881
347
AD-245 618
299
AD- 246 544
AO-240 503
43
AO-242 506
lot
AD-243 825
365
AD- 244 882
302
AD-245 619
399r
AD- 246 546
AO-2W5I4
722
AO-242 517
917
A0^243 836
261
AD- 244 888
334
AD-245 623
949
AO-246 559
AD- 240 530
759
AO-242 524
' 10
AD-243 839
550
AD- 244 900
341
AD- 245 663
407
AO-246 589
AO-240 61S
41
AD- 242 S 28
78
^
AD-243 836
215
AD- 244 901
340
AD-245 668
.998
AD- 246 590
AD- 240 618
609
AD- 242 530
930
'
AD-243 854 ■
299
AD- 244 902
340
AD-245 671
'944
AD- 246 591
AD- 240 631
694
AD- 242 538
•07-
AD- 243 859
197
AD- 244 903 '
340
AD-245 672
997
AD- 246 593
AD- 240 638
179
AD- 242 540
794
\
AD-243 864
786
AD- 244 904
340
AD-245 673
919
AD- 246 601
AD- 240 656
771
AD- 242 555
43B
AD-243 871
496
AD- 244 906
318
AD- 245 689
90»
AO-246 621
AD- 240 666
487
AO-242 573
195
i
AO-243 872
379
AD-244 907
nis
AD- 245 690
347
AO-246 622
iO)- 246 623
AD- 240 687
307
AD- 242 576
997 ,
-1
AD-243 898
401
AD- 244 916
609
AD-245 703
39S
AO-240 694
464
AD- 242 653
1
',
"i
AD- 243 924
779
AD- 244 921
♦7
AD-245 723
299
AD- 246 636
AD- 240 697
214
AD- 242 655
IIS . .
AD-243 927
944
AD- 244 937
730
AD-245 724
949
AD- 246 627
AD- 240 709
720
AO- 242 656
IIS •
•
AD- 243 947
196
AD- 244 945
325
AD-245 726
379
AO-246 631
AD- 240 721
691
AD- 242 660
910
'■•'
• AD-243 967
496
AD- 244 957
414
AD-245 769
399
AO-246 632
AD- 240 734
595
AO-242 667
sr«" .
■i
AD-243 974
692
AD- 244 958
274
AD-245 788
913
AO-246 633
AO-240 766
295
AD- 242 669^
218
AD-243 979
471
AD- 245 017
334
AD-245 802
979
AD- 246 634
AO- 240 767
165
AD- 242 791
574
)
AD-243 989
271
AD- 245 021
755
AD-245 803
421 .
AD- 246 635
AD- 240 788
797
AD- 242 704
MS
AD-243 994
616
AD- 245 023
278
AD-245 804
763
AD- 246 636
AO-240 799
583
AD- 242 729
7t7
AD- 244 034
737
AD- 245 060
283
AD-245 809
479
AD- 246 643
AD- 240 807
4S5
AD- 242 738
IM
4
AD- 244 087
599
AD-245 061
384
AD-245 853
3
AO-246 651
AD- 240 814
396
AO-242 747
ST»
AD- 244 089
330
AD- 245 064
263
AD-245 656
AO-246 653
AD- 240 819
298
AO-242 750
» ■ • .
AD- 244 094
791
AD-245 072
313
AO-24S 887
7r
AO-246 678
AD- 340 860
784
AD- 242 797
lU
AD- 244 095
791
AD-245 078
280
AO- 345 909
4n
AD- 246 688
AO-240 887
48
AD- 242 802
-412
AD- 244 096
790
AO- 245 088
344
AD-24i936
493
AD- 246 691
AD- 240 889
84
AD- 242 859
- 25
AD- 244 097
Tie
AD-245 089
331
AD- 2^ 928
990
AO-246 716
AO-240 891
616
AD- 242 860
77
AD- 244 098
7S1
AD-245 090 .
AD-245 116
465
AD-2«936
699
AO-246 741
AD- 240 892
589
AD- 242 865
774
AD- 244 099
791
346
AD-245 968
«7
AO-246 763
AO-240 909
308
AD- 242 924
*I3
AD- 244 103
196
AD-245 117
318
AD^4S 991
951
AD- 246 766
AD- 240 959
304
AD- 242 962
740
AD- 244 204
692
AD-245 118
413
Aa«245 992
944
AD- 246 771,sifierMded
AD- 241 139
686
AO-242 963
741
AD- 244 207
949
AO-245 119
323
Aa- 245 996
903
AO-246 777
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AO-244 298
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AO-247 159
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AD- 246 364
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AD- 244 642
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AO-247 170
AD- 242 171
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AO-247 199
AD- 242 179
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AD- 244 694
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176
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AO-247 231
AO- 242 247
108
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AD- 244 708 -i
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572
AD- 246 424
636
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688
AD- 243 492
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AD- 244 736
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190
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AD-245 500
257
AD- 246 440
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AD- 247 239
AD- 242 302
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AO- 245 508
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800
AD- 243 530
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545
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AD- 247 242
AD- 247 243
AO-247 244
AO-247 241
AD- 247 rn
AD- 247 »1
AD- 247 2S4
AD- 247 285
AD- 247 287
AD- 247 290
AO-247 300
AX>-247 315
AD-M7 336
AO-247 336
AD- 347 337
AO-247 338
AD-M7 3S3
AO-M7 399
AD- 347 367
AO-M7S61
AD- 3*7 385
AD- 247 434
AD- 247 435
AD- 247 433
AD- 247 470
AD- 247 471
AD- 247 517
AD- 347 535
AD-3«7 539
AD- 247 550
AA-347S64
AD- 347 569
AD- 347 577
AD-M7 590
AD- 347 593
AD-347 6S8
AD- 347 667
AD- 347 685
AO- 347 686
AD- 347 702
AO-347 731
AO- 347 745
AO-347 758
AO-347 763
AO-347 838
AO-347 899
AO-347 893
AD-347 8fS
AO-247 898
AO-347 906
AX>-347 913
AD- 347 915
AO- 348 004
AO- 248 006
AD- 248 019
AO- 248 035
AO- 348 038
AO- 248 040
AD- 348 045
AO-a48 063
AD- 348 067
AD- 348 070
AD- 348 071
AO- 348 073
AO-248 112
AO-248 133
AO-248 140
AD- 248 141
AO-248 148
AO-348 151
AO-348 154
AO-348 192
AO-348 303
AO-248 306
AD- 348 310
AO-348 316
AO-348 327
AO-348 238
AO-348 232
AO-248 233
AD- 248 235
AO-348 358
AO-348 259
AO-348 363
AO-348 364
AO-34a 365
AO-348 368
AO-348 276
AO-248 280
AO-248 301
AO-248 306
AD- 248 307
AO-248 330
450
478
411
770
436
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558
427
555
438
533
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543
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763
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588
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364
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559
560
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606
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730
627
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780
780
779
711
590
560
604
600
637
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AO-348 356
AO-348 362
AO-248 363
AD- 248 364
AO-248 365
AD- 248 367
AD- 248 373
AO-248 385
AO-248 386
AO-248 393
AO-348 432
AD- 348 445
AO-34e 447
AO-348 449
AO-348 4S3
AO-348 484
AO-248 496
AO-248 508
AQ- 248 516
AO-348 517
AO-248 530
AD- 348 540
AO-348 542
AO-348 545
AO-24e 550
AO-248 554
AO-348 369
AO-348 572
AD- 348 573
AO-348 579
AO-348 587
AO-3«Jf8
AP'IBMO
'AO-348 593
AD- 348 596
AD- 248 616
AD- 248 622
AD- 248 631
AD- 248 634
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AD- 248 637
AO-248 647
AO-248 651
AO-248 652
AD- 248 653
AO-248 655
AD- 248 657
AO-248 65'»
AD-248 666
AD- 248 667
AD- 248 685
AD- 248 708
AD- 248 716
AO-248 723
AD- 348 732
AD- 248 744
AD- 248 780
AD- 248 801
AO-248 864
AO-348 887
AO-248 888
AD- 248 ••9
AO-248 912
»>248 927
AO-248 933
AO-248 947
AO-248 954
AD- 248 970
AO- 249 025
AO- 249 042
AO- 249 063
AO^ 249 067
AO- 249 068
AO- 249 079
AO- 249 080
AD- 249 100
AD- 249 103
AO-249 104
AO-249 107
AO-3«9 108
AO-349 109
iSD-349 116
AD- 249 167
AO-249 1(9
AO-249 192
AD- 249 195
AD- 249 196
AD- 249 224
AO-349 231
Jb- 349 235
AO-349 339
AO-349 369
AD- 349 331
\
711 AD- 349 378
S99 AO-349 432
610 AD- 349 423
ft» AD- 249 44^
«21 AD- 249 452
■m AD-249 4»
772 AD-249 5l#
aaa ao- 349 523
SS7 AD- 349 571
745 AD- 349 572
373 AD- 249 573
m AD-249588
422 AO-249 644
773 AO-249 659
S40 AO-249 715
U4 AO-349 719
S«» AD-349 770
604 AO-349 773
364 AD- 349 777
964 AO-349 786
606 AD- 349 788
719 AD- 249 800
SU > AD- 249 801
7M AO-349 802
■2 AO-349 817
92 AO-349 830
■m AD- 349 836
737 AO-249871
993 AO-349 921
581 AD- 349 937
623 AO- 250 065
967 AO-2S0 102
725 AD- 250 104
tn AO-2S0 104
604 AO-250 199
633 AO-2S0 203
6#5 AD- 250 257
609 AO-250 289
683 AO-250 379
787 AD- 250 501
573 AD- 250 530
753 AD- 250 661
761 AD- 290 665
762 AD- 250 672
761 AD- 350*75 »
996 AD- 350 732
996 AD- 250 782
596 AD-250799
607 AO- 350 896
607 AD- 350 918
633 AO- 350 924
709 AD- 350 937
711 AD- 250 938
570 AD- 250 958
627 AD- 250 959
701 AO-250 980
594 AEDC-TN-54-28
693 AEDC-TN-S8-9
793 AEDC-TN-59-134
790 AEOC-TN-59-145
790 AEDC-TN-60-136
bV AEDC-TN-60-173
622 AEDC-TN-60-176
619 AEDC TN-60-177
M7 AEDC TN-60-178
719 AEDC -TN -60- 180
•36 AEDC -TN -60- 182
«33 AEDC TN -60- 189
•37 AEDC-TN-60-191
999 AEDC -TN -60- 192
774 AEDC -TN -60- 194
767 AEDC -TN -60- 202
795 AEDC -TN -60- 21 4
736 AEDC -TN -60- 227
796 AEDC -TN -60- 230
681 AEDC-TW-58-21
986 AEDC-TR-60-5
•33 AEDC-TR-60-11
70B AEL-57033-F
706 AERDL 1569-Tm
70B AERGL-1626-TR
•91 AEROL-1643-TK
TOO AeraChem TM-21
7B7 AEWES TR-3-545, »-3
746 AEWES TR-3-554
719 AEWES TR-3-455, R-3
757 AF-TR-5125
701 AF-TR-5702
782 AF-TR-6199
•94 AF-TK-6682
BIT AI'-TSEAC4-4461-5-l
na APSM Exhibit 57-3.
793 at^eraeded
ram Wumber
709 AFBitl BxhiUt S8 10
•84 AF8MO-7-40S9
684 APaMD-8-2849
696 APa«D-9-4639
706 APa«IO-9- 10272
788 AnM>-60-862
797 AMMD-60-968-5
773 AFM4D-60-2288
753 AI»»«>-60-4867
7r APnO-60-5488, V. 1
795 AFa)ilO-60-6122. v. 1
697 AF»4D-60-6l22. v. 3
801 AF»<D-60-6186. v. 3
806 AFBMD-60-6187. v. 1
708 APBUD A60-5488
786 APflMD TN-59-6
754 AFIMD TW-60-18
796 AFBMD TR-59-U
802 API64D TR-59-18
803 AFmO) TR-60-55
682 APIMD TR-60-72(l)
786 AFBvID TR-60-72<2)
688 AP»»ID-TR-60-74. *.
785 AF8MD-TR -60-74, *.
706 APak4D TR-60-85. *.
774 AF»«D TR-60-85, ».
725 AP«4D-TR -60-85, »,
797 AF»ID TR-60- 179-1
804 AF»40 TR -60- 179-2
730 APIMD TR-60-180
799- APntO TR-60-183
712 AFBMD TR-60- 184
••6 APIMO TR-60-203
696 AFOCDD-TN -60-34
762 APCCDO-TN -60- 39
798 APCCUD-TN -60-58
778 AFCCOO TN -60-60
790 APCCDO-TN -60- 1013
789 AKXai>-TN*60-10l4
749 APOCDO TN-60-1020
792 APCCDO TN -60- 1021
801 APCCDO TR-60-27
735 APCCDO -TR -60- 40
804 APCCDD-TR-60-41
TOO APCRC-TN-57-58
764 ATCHC TN-58-191
770 APCRC-TN-58-201
IV APCRC-TN-58-409
697 APCRC TN-58-486
702 APCRC TN-58-S60,
709 svoefacded
726 APCRC-TN-59-180
736 APCRC-TN-59-243
739 APCRC -TN- 59 -270
767 APCRC TN-59-459
772 APCRC TN-59-470
193 APCRC-TN-59-481
454 APCRC-TN -59-624
338 APCRC-TN -59-625
36 AFCIU:-TN-59-663
157 APCRC-TN-59-785
96 APCRC-TN -59-953
173 APCRC-TN -60- 103
193 APCRC-TN -60- 107
193 APCRC-TN -60- 121
337 APCRC-TN -60 188
325 APCRC-TN-60-441
193 APCRC -TN -60- 1 000
306 APCRC-TN-6O-10O7
218 APCRC-TR-S6-305
325 APCRC-TR-58-233
348 APCRC-TR-58-366
737 APCRC -TR- 58 -277
769 APCRC-TR-59-217
737 APC*C-TR-59-222
195 APC»C-TR-59-255
193 AFCRC-TR-59 256
85 APCRC-TR-59-269
719 AFCRC-TR-59- 290
101 AFCRC-TR-59 293
447 APCRC-TR-59-353
460 APCRC -TR -59-368
310 APCRC -TR- 59 -370
67 AFCRC-TR-59 -37 2
40 AFCRC-TR-S9-373
40 AFCRC-TR-S9-374
612 AFCRC-TR-59-40S
103 AFCRC-TR-60-121
198 AFCRC-TR-60-144
689 AFCRL-103
417 APCItL-201
APCRL-220
980 AFCRL ES070
■ivpl.
580
494
216
MO
712
980
799
584
582
582
910
9«>
741
740
799
114
982
580
736
584
584
584
740
741
582
582
739
580
580
606
194
558
736
435
478
637
682
190
344
452
795
134
684
684
55
572
384
105
413
166
195
131
4
336
323
133
383
383
30
106
221
219
219
214
220
100
313
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548
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105
158
559
413
38
168
151
34
794
475
161
173
157
163
172
414
221
94
800
706
7«
119
Number
APCRL-TN-50-783
APCRL-TN-58-243
AFCRL-TN-59-557
>FCRL-TN-60-110
AFCRL -TN -60- 158
AFCRL -TN -60- 166
AFCRL TN -60- 167
' AFCRL-TN-60-168
AFCRL -TN -60- 183
AFCRL -TN -60-210
APCRL-TN -60-316
AFCRL -TN -60- 336
APCRL-TN -60- 327
APCRL-TN -60- 343
APCRL-TN -60- 251
AFCRL-TN-60-257
• AFCRL -TN -60- 358
APCRL-TN -60- 361
AFCRL-TN-60-363
APCRL-TN -60-357
AFCRL -TN-60- 368
APCRL-TN -60- 369
APCRL-TN -60- 270
APCRL-TN -60- 271
AFCRL -TN -60- 373
AFCRL-TN-60-275
APCRL-TN -60- 277
APCRL-TN -60- 278
APCRL-TN -60- 281
AFCRL TN-60-283
AFCRL- IN -60- 384
APCRL-TN -60- 296
AFCRL -1^1-60- 297
APCRL-TN -60- 357
APCRL-TN -60-360
APCRL-TN -60- 379
APCRL-TN -60-388
APCRL-TN -60- 400
APCRL-TN -60- 401
APCRL-TN -60-411
AFCRUTN -60-413
AP.CRL-TN -60-414
APCRL-TN -60-417
APCRL-TN -60-419
APCRL TN-60-434
APCRL-TN -60- 435
APCRL-TN -60- 436
AFCRL-TN -60-433
APCRL-TN -60-436
APCRL-TN -60- 437
APCRL-TN -60- 439
APCRL-TN -60-443
APCRL-TN -60- 455
APCRL-TN -60- 457
APCRL-TN -60-458
APCRL-TN -60- 459
APCRL-TN -60-461
APCRL-TN -60- 462
APCRL-TN -60- 464
APCRL-TN -60-464
APCRL-TN-60-467
APCRL-TN -60-470
APCRL-TN -60- 483
APCRL-TN -60- 486
APCRL-TN -60- 489
APCRL-TN -60- 497
APCRL-TN -60- 498
APCRL-TN -60-964
AFCRL-TN -60-565
APCRL-TN -60-57400
APCRL-TN-60-575
APCRL-TN -60-581
APCRL-TN -60-586
APCRL-TN -60-595
APCRL-TN -60- 597
APCRL-TN -60-601
AFCRL-TN-60-606. aufipi
APCRL-TN -60-6 10
AFCRL-TN -60-613
APCRL -^-60 -6 1 4(1)
AFCRL IN -60-6 14 (II)
AFCRL -1^-60-616
APCRL-TN -60-628
APCRL-TN -60-630
APCRL-TN -60-631
APCRL-TN -60-632
AFCRL-TN -60-634
APCRL-TN -60-637
APCRL-TN -60-638
APCRL-TN -60-639
APCRL-TN -60-642
AFCRL-TN -60-645
AFaU--TN -60-647
Number
^-
81
AFCRL-TN -60-649
62
AFCRL-TN -60-652
319
APCRL-TN -60-656
166
APCRL-TN -60-657
161
APCRL-TN -60-658
155
APCRL-TN -60-663
166
APCRL-TN -60-667
185
APCRL-TN -60-668
106
APCRL-TN -60-669
120
AFCRL-TN -60-670
279
APCRL-TN -60-674
30
APCRL-TN -60-675
31
AFCRL TN -60-683
131
APCRL-TN -60-684
154
APCRL-TN -60-685
558
APCRL-TN -60-691
537
AFCRL-TN -60-699
413
APCRL-TN -60-751
309
APCRL-TN -60-756
31
AFCRL-TN -60-758
4
APCRL-TN -60-759
4
APCRL-TN -60-762
4
APCRL-TN -60- 764
4
APCRL-TN -60-765
35
APCRL-TN -60-767
155
APCRL-TN -60-768
309
APCRL-TN -60-769
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APtJBR- TR-60- 128
694
APOSR -TR-60- 1 29
7*4
APOSR-TR -60- 130
•600
AFOSR-TR-60- 131
210
APOSR-TR -60- 134
626
AFOSR-TR-60- 135
457
AFOSR-TR-60- 136
604
APOSR -TR-60- 137
336
AFOSR -TR-60- 140
177
APOBR -TR-60- 149
410
APOSR-TR -60- 150
450
APOSR-TR 60-158
450
APOSR -TR-60- 160
478
APOSR TR 60-163
791
AFOSR-Tft-60-165
606
AFOSR TR-60- 169
550
APOSR -TR-60- 170
626
APOSR -TR-60- 171
434
APOSR -TR-60- 176
450
APOSR-TR -60- 177
784
APPTRC-TN 57-52
406
APSAM-55-25
550
APSAM-58-7*
SOI
APSAM-58-152
600
APS AM -60-3
686
APSAM-60-17
458
APS AM -60- 22
607
APSAM-60-29
439
APSAM-60-42
607
AFSAM-60-48
406
AFS AM -60-60
469 •
AFS AM -60-62
394
APS AM -60-65
539
APS AM -60-6*
411
APSAM-60-71
406
APS AM -60-72
472
APSAM-60-73
467
APS AM -60-75
702
APSAM-60-77
449
AFSAM-60-79 4,
693
APSAM-60-80
627
APSAM-60-81
790
APSAM-60 82
484.
AP8AM-60 84
447
APSAM-60- 85
631
APS AM -60-87
404
APS AM 60- U
449
770
549
59*
593
552
633
604
546
782
696
696
47S
208
3
146
45*
89
592
6*
457
326
79
27S
314
142
141
2S
140
201
209
112
192
443
25
471
65
141
96
90
552
274
346
407
341
394
344
468
268
326
457
144
160
581
581
626
446
695
540
449
610
549
553
701
262
68*
693
690
543
693
22
399
IS
140
404
20
141
m
694
134
20
*S7
141
267
265
140
544
139
3*9
. 400
343
Number
Niunter
M
APSAM-«1-U
«M
ARL-TN -60-17
772
AP$AM-61-12
6W
ARL-TN-60-109
580
APSAM-148, R-1
*M
ARL TN-60- 119
449
APSAM-290, R-1
943
ARL-TN -60- 121
800
APSAM-392. R-1
S42
AJIL -TN-60- 124
604
APSAM-410. R-1 i
APSAM AR-3-60
MO
ARL-TN-60-125
318
140
ARL-TN -60- 137
606
APSWC-TN-59-33
*30
ARL-TN -60-138
586
APSWC-TN-59-36
783
ARL-TN -*0- 140
606
APSWC- TN-60- 25
3S4
ARl.-TN -60-142
327
APSWC- TN-60- 29
302
ARL-TN -60- 144
333
APSWC -TR-59 -34
738
ARL-TN -60- 145
607
APSWC-TR-59-43
799
ARL -TN-60- 149
4S6
APSWC-TR-59-44
'. 101
ARL-TN -60- 150
542
AOC -0290-01.-2
747
ARL -TN-60- 158
554
AOC-1233
941
ARL-TR-60-274. pi. 1
347
AOC-1541
MO
ARL-TR-60-279
312
AOC-1541, aupp.
90
ARL-TR-60-281
309
AOC-1880
m
ARL-TR-60-282
561
AOC-TN-28
M
ARL-TR-60-290
419
AOC-TN-31
146
ARL-TR-60-292
184
AIL -3689-1
9H
ARI,-TR-60-29S
612
AIL-3905-1
U3
ARL -TR-60- 296
315
AIL -45 20-1
SM
ARL-TR-60-298
195
AIL-4589-M-1
7U
ARL-TR-60-300
174
AIL-4600-l
41
ARL -TR-60- 301
345
- AIL-4614-l
31*
ARL -TR -60-303
304
AIL -5341 -TN- 4
7M
ARL-TR -60-307
94
AU.-5791-4
708
ARL-TR -60-309
778
AlL-5934-1
9*S .
ARL-TR -60-313
435
AIL-73S*-1. 1.2
41
ARL -TR-60- 31 4
600
AIL-7601-H-1 '
41*
ARL-TR -60-315
533
AINA-2
ISO
ARL -TR-60- 3 16
471
AINA-S
707
ARL -TR-60- 319
435
AIR-33-59-PR-21B
6
ARL-TR -60-321
459
AIR-244-58-PR-I77
420
ARL -TR-60- 323
633
AIR-244-58-PR-182
1*2
ARL-TR -60-324
478
AlR-a6l-59-PR-202
*82
ARL-TR-60-330
630
AIR-290-60-PR-225
392
ARC- 2
699
A1R-314-60-IR-106
260
ARPA Order 5-58
720
AIR-314-60-IR-129
538
ARPA Order 6-58, Taak 8 i
747
Alreaearch AE-6378-MR.
ARPA Order 6-58. Taak 11
275
rev. 3
580
ARPA Order 24-59, Taak 2
213
AlrcMvch AE-7029-MR.
ARPA Order 24-59, Taak 3
549
rev. 2
580
ARPA Ordat^26-59
35
Alre»e«rch AE-7030-MR.
ARPA Order 26-59
708
rev. 2
580
ARPA Order 40-59. Taak 3
550
AlreMarch AE-7474-R.
ARPA Order 40-59. Taak 3
696
V. 1
580
ARPA Order 56-60
167
AlreMarch AE-7474-R.
ARPA Order 80-59
342
V. 2
SSO
ARPA Order 85-60
166
AlreMarch AE-7518-MR
sao
ARPA Order 106-60
349
Alreaearch SC-5175. rev.
2 580
ARPA SFS-7
416
AL-2606
740
ARPA SPS-8
422
AU C-61489
559
ARPA SPS-19
432
ALO6U-160-4
too
ART-TR -60-336
US
AMC-TR-60-7-257. ». 1
749
ARTEMIS -6
707
AMC-TR-60-7-257, ». 2
749
ASRDL-1481
233
AMC-TR -60-7-577
5*2
ASRDI -1983
1*2
AMC- TR-60- 7 -637
611
ASRni.-2041
421
AMC-TR -60-7-«*7a
445
ASROL-2043
421
AMC-TR -60-7-107
712
ASRDL-a047
411
AMR-IOOS
5*4
ASRni.-2049
444
AMRG PM-12
413
ASRCIL-2087
«7S
AMRG PM-24
380
ASROL-2092
m
AMRG FM-2S .
2W
ASROL-2099
421
AOHEL TM-12-60
58
ASRXX.-2112
4a
AOHEL TM-17-60
398
ASR0L-211II
411
AOHEL TM-18-60
392
ASRnL-2tlS
4U
APC/rAT/60-A-l. PR
57
ASRDI. -2121
S17
AyOC TN-59-25
1*2
ASRni.-2122
u
APOC-TR-59-33(I)
5*0
ASRDI -2123
m
AKXJ-TR-59-33. pi. 2
sao
ASRXX.-2125
104
AKX-TR -60-65
7W
ASRCIL-2129
2
APL/JHU BB-291
108
ASRIX.-2131
U
APL/JHU CM -958
699
ASRDI. -2132
41
APL/JHU CM-959
146
ASROL-2133
288
ARA-70e
57
ASRDI. -2134
4}
ARA-720
436
ASROL-2135
»
ARA-823
737
ASROL-2136
41
ARCRL-TR -60-412
411
ASRlX-2137
ao
ARP-1099-1S
341
ASIUX.-2138
190
ARP 1146-6
337
ASRaL-2141
431
AltP-1149-2
41
ASU)L-214S
317
ARP-1149-3
719
ASRDL-2149
752
ARP-1149-4
5**
ASROL-2151
566
ARP-2152-10
460
ASROL-2152
7*2
AJlP-2164-12
612
ASROL-2155
7«B
ARP-2172-6
92
ASRnt.-2158
708
ARP-3157-14
.**
ASROL-2159
705
ARP-3164-12
i'Mi
ASROL E-1198
1*3
ARP C-164
:s6i
ASROL M-1466
172
ARP D-165
'783
ASROL M-1870
IS
ARCMA TN-lHlN-7
800
ASRHl. M-1918
109
Ntmtier
Number
ASROL M-1924
5*7
BRL-TN-1304
43*
ASROL M-1936
5*7
BRL-TN-1313
58
ASROL M-1948
S*7
BRL-TN-1315
121
ASROL T-1459, aupp 1
352
BRL-TN-1337
307
ASRDL T-1473
352
BRL-TN-1354
422
ASROL T-1479
152
BRL-TN-13S6
*36
ASROL T-1480
»
BTL- 27424- K
941
ASRL-TR-86-1
BTL-27424-M
341
ATI 23 309
Ml
8TL-27424-N
342
ATI -29 321
Ml
BTL -27424-0
109
ATI -52 532
717
BTL- 27480-1
1*3
ATI-52 581
783
BTL-27480-IC
289
ATI-65 612
79
BTL-27480-L
289
ATI -86 039
*9*
BuMedMR 005.12-0005.4.
ATI -86 858
*«S
R-9
3*
ATI -90 054
IM
BuMed MR 005. 15-0002. 2
14
ATI-114680
407
MIrd MR 006. 15-0002. 2.
ATI- 148 927
419
R-6
14
ATI -152 755
417
BiMedMR 006.15-0002.7.
ATI-153 158
479
R-2
13
ATI -159 367
410
BuMedMR 005.15-0002.7.
ATI -162 940
MS
R-IO
M
ATI- 163 038
772
BuMed-MR 005.15-0003.7,
ATI- 173 115
*13
R-12
369
ATI -179 543
472
BiMed MR 005.15.0002.7.
ATI-199 919
946
R-13
**9
ATl-207 933
801
BuMed MR 005. 15-0002. U
ATI -210 349
474
R-1
269
Avco RAO-TM-6(f'*7
217
8uMad-MR 005.15-0002.11
Avco RAD-TR-60-r
620
R-2
210
Avco RAD-TR-60-29
*21
BuMed-MR 005.15-0005.6.
AvcoRN-132
114
R-6
748
Avco RR-37
»4.
._ B«4kled-MR 005. 15-0005.6.
Avco RR-42
494
R-7
710
Avco RR-44
210
B«i'era TB-60-3
994
Avco RR-80
214 -
Bitfera TB-60-4
194
Avco RR-85
346
t^ev TB-60-8
689 ^
Avco RR-88
117
Bufera TB-60-9
Avco RR-89
tt,
BuPera TB-60- 1 1
9M
AvcoRR-90
«4;
Bitf>era TB-60- 13
9»
Avco RR-91
194
Bt£hipa-371-V-19
90
Avco RR 93
558
Bk£hlpa 375-N-29
744
Avco RR-94
605
CAL AO-10S2-A-11
3J6
AWSM- 105-37
555
CAL AO-1118-A-7
217
AWSM- 105-39
279
CAL AP-1285-A-I
SOB
AWSM- 105-39, Jan S3.
CAL AP-12B5-A-2
770
auperaeded
279
CAL AI-1190-A-5
«•
AVySM-105-54
149
CAL JA-1256-S-9
710
BAC-775
601
CAL-VC-1196-G-6
81
ac-150
66
CAL VG-1196-G-7
80
IBN-«32
602
ai-19. V. 1
808
BaN-*90
119
CH Ref. 60-1. V. 1
SOB
BBN 721
331
Cn Ref-60-3
S*2 1
BBN-7r
•02
CBI TR-21
M3
aBN-780
422
m,-96
34 t
BeU- 7006 -3352-001, v. 1
769
CCL-97
Ul i
Bell -7006 -3352-001. v. 2
769
Cr4,-98
407 1
Bell-8007-981-011
64
CCL-99
BeU -9015- 19-002
606
ClC-101
171
aL-u
549
C1C-12S
Mi
8LC-59-*
223
aT-21-U
T14
BM-3734
738
or E-79-2
9M
BM RI-.Vt.SA
J694
CML-TR-P153-I2
SM
BN-178
320
Cmvalr MP-59-053
779
BN-181
86
Coavair TM-349-19
118
BN-196
330
Coun-27
417 ;
8N-197
408
Coun-29
ISl
BN-211
761
CROL SP-1-20
a«
BN-216
77
CRDL SP-l-21
906
BN-218
334
CROL SP-2-34
S91 i
BN 220
86
CRDl. SP-4-22
752
BN-221
788
CROLR-2380
97 J
BN-225
700
CROLR-.3000
84 i
BR-NYU-34
427
CRIX.R-3002
39 1
BRL-lOU
99
CRDLR-3006
39 ?
BRL-1093
422
CRiXR-3007
19 ;
BRL-109S
454
CRni.R-3009
57 t
BRL-1104
34
CRnLR-3010
»
BRL-1113
325
CRIXR-3013
13
BRL-1114
436
CROLR-3016
i*
BRL-1116
442
CROLR-3019
'3M
BRL MR-1237
436
CRDLR-.3O20
9»
BRL MR- 1241
306
CRDL R- 3024
171
BRL MR- 1242
436
CROLR-3026
Ml
BRL MR- 1245
454
CROLR-3033
Ml
BRL MR- 1278
58
CROLR-3034
3M
BRL MR 1279
58
CROLR-30S0
Ml
BRL MR-1280 '
176
CSl Con-60-1
M4
BRL MR 1283
42
CSl Con -60-2
M« i'
BRL MR- 1286
58
CU-1-60
M2
BRL MR 1292
173
OU-1-60
493 !;
BRL MR-1299
306
CU-1-60-ONR-366<08)
476
BRL MR 1300
466
CU-l-60-QNR-366<34)
476 1
BRL-TN-869
440
CU-3-60
78
CU-4-60
CU-J-60
CJJ-*-«0
CU-7-40
CU-«-<>0
CU-«-*0
CU-U-59
CU-U-*0
CU-12-59
CU-13-W
CU-14-58
CU-U-59
CU-U-W
CU-15-«0
CU-»6-*0
CU-16-M
CU-17-60
CU-l«-«0
CU-42-*0
CU-63-«0
auTXHLEy-4*
CTA AST/BOR- 13081
CWL fW-MI
CWL nil-32-4i
CWLR-2347
CWK-700-10
CWR T»-S»-iO
CX-49
CX-SO
DA 33-0»-ORD-l»«. RS
DAC AJ6O-CETM-A06. 0
DAC SM- 37637
DAC SM-37766
DACL-IM
DACL-8a55-2
OASA-140
DASA-3S2
DASA-MKDel)
OASA-J26
DASA-529
DASA IS31
DASA-730
DASA-799
DASA-10S2
DASA- 1157
DASA- 1176
DiASA-1177
0ASA-lir7
CMSA-1190
OCL E-452
DCL-R-232
DQ-llS
Da- 116
Dike QK-3-10O4
CMIC 116R
OMC-127
-136A
-197
UMC-13a
-139
-140
-141
-142
-143
-H
DMK-
DMIC-
DMiC-
□MIC-
DMIC-
OMC-
okiac-143
DMIC-146
dmk:i47
DMIC 14«
dmk:'149
DMIC 461
DMC M-63
DMIC-M-6S
DliieC M-66
CMC-M-«a
DMC-M-49
DMK; M-70
DMIC M-71
DMK: M-72
DfcBCM-73
DMK;-M-74
DI<iC-M-7S
omk;-m-7»
D*«C-M-77
DMC-M-7»
dmk:-m-79
dmk-m-w
DMIC-M-U
DMC M-U
omk:-m-s3
DMC-M-M
DMC-M-SS
DMK:-M-86
<y N»tor
187 DMIC-M-87
107 DfcOC-M-W
1«7 DOPL TR-6; 3
108 DOPL TR-T;7
292 DOPL TR-8<4
S69 DOPL TR-8< I
77 DOPL TR-80
230 oon.-n.-tn
H oon.-n-t<»
77 DOPLTIl-8!6
SM DOPL TR-8! 7
77 DOPL TR-8! 9
7« DOPLTR-«0
M* DOn. TR-« 1
760 DOPLT»-8(3
761 DOPL TR-8(7
S65 DOPL TR-8<«
595 DOPL TR-i:o
806 DOPL TR-8:4
164 DOPl. TR-«: 5
7W DOPL TR-8: 8
419 DOPL TR-r9
272 DOPL TR-e<il
339 DOPL TR-8(i3
V2 DOPL T»-8(i5
730 DOPL TR-8117
6» DOPL TR-8(I8
108 DOPL TR-8"1
631 DOPL TR-8' 5
285 DOPL TR-8'«
582 DOPL TR-91 12
788 DOMIIT-1-lil
802 DOMIT-l-l
443 DPCR-240. 1 1. 2
595 DPS/T15-l4<l/483
772 DP8/rW-60l ^5
4» 06R-743S-3
541 D6R-7484
334 (8R-7484
464 CBR-7692-3
464 C6R-5-7476
440 DSR-7-8120
SOT DTMB-S97. ti^eraeded
462 Drrk«-880
S« DrrMB-1015
58 DTMB-10S2
I7« OTMB-1160
218 orrMB-1170
465 Drn«-ir2
45 aTMB-1290
765 DTMB-1295
88 CmiB-13U
88 orrMB-1347
539 DrrMB-1353
199 DTMi-1360
614 OrnS- 1370
X>1 DrTMB-1404
92 cm*- 1410
330 DrrMB-1415
468 DrrMB-i43l
613 CrTMB-1454 .
4S9 Orn«-1478
437 DTM-1480
613 cmi«-1482
461 DTMB-1488
779 cmac-i7i
779 OTMBC-55i
77t DuBl«pTR-j52-60-l
776 DURl RR-417-71
rn DWC C7674 104
66 E-S753(tefe:ior
330 BCA-192.04
70 BOt.-M236
93 EB-401
92 EE-433
198 EE-461
198 BE-466
198 EEItL-6-32
317 EBllL-6-33
198 EEIU,-6-37
198 EEKL-6-38
313 EEIIL-6-39
339 EERL-ni
311 EERL-I12
474 BERL-113
4S8 BERL-114
444 EBS-OIOOS^M
610 EES-030 031
610 EES-O4OO40F
446 EES-620 32^
610 EES-8»a6t
610 BES-830 001
776 EES-1A660:4
571
635
SM
733
569
«I4
«M.
48
155
330
81
283
959
97
S7
7M
■D4
713
MB
67
in
910
IM
965
BBS-4E(E1)101717
EM-147
111-155
EM- 161
BM-162
ENCR-4S
BQ6-210-QL-4
B06-»0
BCe-400-2Q-l
EP-123
EF-133
Bf-137
Er-141
BIU.-91
EtL-97
ERL-9e
ERL-99
BRL-100
ERL-IOI
ERL-103
ERP RM-IO
ERP RM-14
ERP RM-15
ERP RM-16
ES-2<>(XE-3)
ESL-MIT-7591-t-2
ESL MIT -7976 -60- 5
ESL K«IT-e494-t-l
ETT-728
ETT-SOl
ETT N-600
F-TR-2364-1A-1
PA-M60-14-1
P4-R-15V
FA-R-1534
PA-S-5584
PA-T53-14-1
PA-T60-8-1
PAA Taak59-X».9
PAAT»«kD/E- 1-6089
PAA TMkD- 2-5213
PAMD-FT245-1
PAMD-R245-(010-01Z)
FAMD-R245 025
PAMD-R245.014
-R245.015
PAMD-R246A-002
PDRG-60-2
PORC-60-3
PDRC-60-4
PIP -Al 878
PI I-A3033-3
PI I-A3O49-10
n I-A3049-11
FPL 59-2
FPL 8iC-4
PPL Bu6-6
PPL BijS-7
FPL Bitf-8
PRIR. 113/9
FRI-R. 146/4
Prta-278. 1
PRL TN-2
PRL TN-3
PRL TN-9
FRL TN-12
FRL-TR-3
FRL-TR-5
PRL-TR-8
PRL-TR-ll
PRL-TH-12
PllL-TR-13
PRL-TR-15
PRL-Tll-17
PRL-TR-18
PIUl,-T11-19
PRL-TR-21
PllL-TR-22
PRL-TR-25
PRO- 200/10
PZK -9-140
aA-1168
GA-1683
CASL TR-148
OCC ER-aOOOO-56. »
book U' p(. A.
OCC ER -00000- 56.
book 2, |K. 8
OOC BR-OO0OO-S6,
kMk 3. pt. C
OOC ER-00000-S6. ».
pu. A-C
CE Acroptiyalcs OHM
615 GEMEIectnxUc)e-l31-P
221 GM-TM-162
320 (341-1812
476 GMI-1940
349 0841-2133
80 CMI-214S
788 GMI-2154
307 OIE-57-5
342 Grant AF APOSR-61-4,
465 TN-1
5 Grmnt AP APOSR-6l-2a,
103 TR-1
555 Grwit NSF C-642
230 Gruii NSP G 2668
47 Grani NSF G-5250
47 Gram ^SP C-8434
296 Grant NSP C-9503
295 Grant PHS G-M-743<C5)
296 GRD APSG-94
295 GRD AFSG-120
638 GRD AFSG-123
444 GRD AFSC-125
588 CRD AFSC-126
763 GRD GRP-48
352 GRD GRP-69
286 GRD RN-35
451 GRD RN-38
451 GRD-TR-60-296
64 GTEL TR-60-204.6
750 GTEL TR -60- 703. 9
750 CTEL TR -60- 704 -104-
407 204-306-208.2
584 GWU-T-111/60
780 OWU-T-113/60
613 HAC TM-591
362 Haael-9905
173 HE-150-178
781 HE-150-183
S61 HEI M-809
561 HEI M-828
430 HEPL-192
158 HEPL-199
158 HErL-203
158 HEPL-206
HH-60-15
158 HH-60-84
710 HH ARD-236
771 HH ARD-257
396 HLCITM-54.2
496 HMB-1187
301 HMX
bZ7 lf>S-14
587 HR-59-474
442 HR-60-412
182 HR-60-479 '
182 HSN-2
182 HSNP-32/1960
182 1«R RM 59/23-SM
182 HSR-RM-59/25-SM
201 HSR RM-59/36-SM
550 HSR RM-59/27-SM
83 WR-RR-60/1-SM
59 HSR-RR-60/4-SE
99 KR TN-99/7-SM
582 Hr-6
59 Kr-7
59 HimiRRO-67
59 HumRRO-RR-3
68 HuinRRO-RR-6
60 Hu(nRRO-TE-65
315 HuniRRO-TR-64
316 ICP-12S2. ak^eraeded
695 lBR-18-7
437 lER-20-133
438 1ER-Z7-20
§82 lER-27-21
438 1ER-60-2S
453 lER-60-27
438 IBR-60-28
73 IER-60-245
101 IER-60-258
799 IER-60-261 »
791 IER-60-a63
86 lER-60-a6S
>. 1. IBR-60-367
736 IBR-60-369
». 1. lER-60-271
736 lER-60-272
IBR-60-278
736 IBIl-«0-3aO
2. IER-60-284
726 IER-60-286
30 160 IBR:60-289
». I.
Pat
735
4S«
lis
«r
633
70S
TUB
310
593
701
595
621
604
638
5M
541
284
154
»
m
m
$m
467
704
278
108
408
br
S7I
79P
MS.
M''
S7S
MB
lis
SI
7B9.
61*
«l«
BIS
784
417
711
158
SB
BOB
ITS
983
sn
S4S
S43
7»l
775
753
121
121
121
121
477
334
131
944
973
6B3
136
897
361
361
422
471
•«
•m
7S1
IBS
s»
73«
.ao
47
47
SM
91*
907
971
9M
718
10
\
Numter
IBR-60-290
IER-60-293
lER-60-298
lER -60-303
lER -60-306 '
lER-60-315 ^
lER -60-316
IER-60-317
IBR-60-321
IBR-73-7
IER-78-2
lER-82-11
IER-82-12
IBR-82-14
IBR-108-4
IBR- 138-5
IBR-131-6
IBR-131-8
lER- 131-9
IER-lSO-3
IBR-lSO-2
ILU DCL-95
ILU DCL-96
ILU DCL-98
ILU DCL-lOO
IMM NYU 360
IMM-NYU-3b4
lMM-NYU-367
IMM-NYU-269
IMM-NYU-272
IQRE^iP-1
IR1.-138
IIIL-131
1IIL-13S
IIIL-137
lllL-139
110.-140
IRL-141
IRL-142
ISMS 223, i«v.
ISMS 23»
ISMS 229
ISMS-230
-331
-340
ISM5-243
ISMS 244
ISMS 245
ISMB 247
ISMS 249
kSMS 250
ISMS-254
ISMS 258
ISMS 260
ISMB-2bl
ISMS-368
lST-2900-218 R
1ST- 2900- 230- K
ITL-A2115
ITL-230a-C
ITT-3029
JPRC MR-22
IPC 1-58-1
M-4-29
M-4-43
M- 20- 194
PR-30-229
PR-]0-2a
PR-30-274
PR -30- 294
R-20-72
R 20-127
KAC-159A>'90-1
KS-6 camera
L4T-373
LPE-570-A1
UR TR-136
UR TR-137
UR TR-138
UR TR-144
UR TR-145
UR TR-146
UR TR-148
UR TR-149
UR TR-150
LL-3C-00O2
LL-21G-00O3
U.-21G-0003. r«». 3
1-L-21G-0005
LL-21G-0OO9
u.-3ic-aou
FL
FL
FL
FL
FL
FL
FL
FL
Pay
733
108
436
467
631
5W
734
724
760
213
776
609
89
774
470
US
S3
324
60S
313
471
77
570
788
774
334
1S6
761
761
192
234
479
559
31
384
155
119
398
398
283
415
596
186
323
1S7
1S7
222
186
763
187
761
762
Ml
996
996
5*7
596
596
802
707
742
143
352
300
747
437
427
307
448
447
447
438
448
311
711
223
804
81
428
337
298
111
572
638
470
470
470
415
190
767
174
174
455
Number
LL-21C-001S
LL-21C-0016
LL-21O-0019.
LL-21C-0024
LL-21C-0036
LL-21G-0027
LL-21G-0028
LX- 220-0021
LL-22C-0O35
IX-23G-0039
LL-23G-0042
LL- 230-0043
LL-23C-0046
LL-2aC-005l
LL- 230-0064
IX-3SC-0001
LL-35G-00O4
LL-25G-O0O5
LL-25G-a017
LL-25C-0O19
LL -250-0020
LL-25G-0021
LL-25C-0029
LL-30G-0009
LL- 300-0011
LL-33C-0014
LL-34G-0006
LL-36-44
LL-46-48
LL-47-37
LL-58-2
LL-46O-0003
LL-46C-0007
LL-46G-000e
LL-46G-0OO9
LL-47G-0O0S
LL-47G-0006
LL-47G-00O7
LL-47O-0010
IX-47O-0011 .
U.-5IO-0016 I
LL-51G-0017 \
U.-51G-a018 '
LL-53C-0013
LL-52C-0014
LL-53C-0O40
LL-53G-0042
LL-53G-a043
LL-53C-0045
LL-53G-0046
LL-53G-0O47
LL-S3G-005I
LL -54-19 ^
LL-54C-00r
LL-55O-0027
LL-55C-0028
LL-55G-0030
LL-58G0011
LL-58G-0O13
LL-58C-0014
LL-58O-0015
LL-81G-0023
LL-B2C-0021
LL-82C-0023
LL-82C-0O24
LL-S4C-0013
1X-85C-0008
LL-313C-0002
U,-TR-I02
LL-TR-139
LL-TR-164
LL-TR-165
LL-TR-172
U.-TR-179
LL-TR-183
LL-TR-184
LL-TR-I90
LL-TR-194
LL-TR-195
LL-TR-202
LL-TR-204
LL-TR-205
LL-TR-306
LL-TR-307
LL-TR-30e
LX-TR-209
LL-TR-310
LL-TR-212
LL-TR-217
LL-TR-219
4-L-TR-221
LL-TR-223
LL-TR-224
908
174
auperaeded 439
799
931
4)9
439
60
762
438
333
973
997
9M
931
9M
4B
Ml
49
900
190
BOl
973
SS7
Utt
999
9S1
4S
•»'
IS7
9
1B7
M
«19
»22
223
438
4a
42S
727
t«
i«
HI
471
629
B21
BIO
•>»
767
*
S2
78
ISO
763
82
9
m
•4
as
"S44
T95
428
944
727
49 '
ISO
111
944
48
49
ISO
49
349
399
78
S7
49
212
49
90
82
S3
78
SO
399
8S9
Number
LL-TR-236
LL-TR-227
LL-TR-234
LLU DCL-103
LMSD-2466
LMSD-2702
LMSO-4507
LMSO-48 360
U4BO-48 373
299
299
428
595
69
65
453
174
308
-48 408
LkfSO-49 73S
IJi60-49 771
U«D-5)06
LM5D- 288 003
LM5D-288 029
LliSO-388 07S
'^LMBD-338 140. v. 1
LMSD-2B8 140. v. 2
LM50-288 1^4
LlwED-28a 168
LM5D-288 169
LMSO-288 184
LMBO-388 190. ai^tpl. 2
Umbo- 288 254
LMSD-288 264
LMSD-311 695
LMSD-311 864
LMSD-480 391
Lli6D-480 485
LMSD-703 005
LMSD-703 006
LMSD-703 013
LMSD-703 021
LMSD-703 029
LMSD-703 036
LMSD-703 043
LMSD-703 045
LMSD-703 047
LMSD-703 049
LMSD-703 060
LM5IK703 ISO
Lock NR-60
Lock SB -60-1
Uxk SB-60-25
Lock SB -60- 29
Lock SB-60-30
LockSB-60-36
Lock SRB-60-3
MAC -7864
MarqMR-60-109
MEOeW-RS-1-59
M£Oew-RS-2-59
MEOEW-RS-3-59
MEOEW-RS-4-S9
MEDEW-RS-S-S9
MEOEW-RS-2-60
MEOEW-RS-4-60
MEDEW-RS- 5.-60
MEOEW-RS-6-60
MEOEW-RS-7-60
MEOEW-RS-8-60
Meteor-34
Meteor - 39
MEWD-1033
MH-2490e
MH Aero RED 28030
MH TD-42060
Microtech- 172
MIP engine
ML -695
ML-714
ML-732
ML-733
ML-74S
ML-747
ML-755
MLNYNS-S032-B-15. 40
MLNYNS-5047, pc. 123
MMUM)-2112
ML(UM)59 137
MMUM)69 160
MMUM)59 182
MMUM)S9 211
MUUM)S9 230
ML(UM)S9 242
MMUM)60 1
MUUM)60 020
MUUM)60 106
MOT RL-3828-2
MOT RLF -3828-4
U
6S
65
65
65
190
194
65
65
131
179
180
439
300
632
429
65
358
192
613
796
763
455
604
308
439
SO
444
417
61
71
552
333
SO
444
417
300
609
412
3B6
747
142
142
»I
403
403
545
543
543
404
545
545
89
87
436
583
52
583
748
65
301
574
430
301
301
473
4S8
7n
318
382
74
39
74
74
74
74
68
74
68
158
IBS
number
MPL-14
MRC TSR-63
MRl R-523. 38-59
MRl R-664-S8
MRI R-696-S8
MRl R-736-59
MRl R-778-59
MRL(CMRO)-78
MRMOMRO)-79
MRMOMRO)-S0
MRMOMRO)-81
MRUOMRO)-88
MRMOMRO)-89
MRMORO)-71
MR N-136
MR N-309
MR-N-rO
MSEE-S3-33
kfiEE-SS-02
MSEE-60-22
MSEE-60-2S
MSOP- 1851. auperaeded
MSRP DP-51
MSRP RR-16
kiCRP RR-66
MUP TR-161
MUP TR-162
MUP TR-167
MUP TR-168
182
- 185-a
-192
-193.
-193.
-194
-195
vol.
vol.
MUP TR
MUP TR
MUP TR
MUP TR
MUP TR
MUP TR
MUP TR
MUP TR-198
MUP TR-199
MUP TR-300
NAA-MD-S9-277
NAA-MD-60-98
NAA MD-60-S29
NAA-MDA-59-79
NADC-Al-5957
NADC-8L-L53192
NAOC-BlA-6020
NADC-MA-6025
NAOC-MA-6036
NADC-MA-6027
NADC-MA-6029
NADC-MA-6030
NADC-MA-6031
NADC-MA-6034
NADC-MA-L6018
NADC-MA-L6021
NAFI-MR-54
NAMC-ACEL-437
NAMC-ACEL-439
NAMC-ACEL-444
NAMC-AEL-UOe
NAMC-AEL-1675
NAMC-AML-AE-1096
NAMC-AML-AE-1102
NAMC-AML-AE-4195. pt. 2
NAMC-AML(M)-59S '
NAOTS TR-9-59. FR
NARF-S8-18T
NARF-58 19T
NARF-59-32T
NARF-60-23T
NATC-ET3 15-127
NATrS-ATL-47
NAVDOCKS TP-Te-6
NAVEXOS P-1034. app. A
NAVEX06 P-1466
NAVDRO-1222
NAVORO-1234
NAVORD-2031
NAVORD-3073
NAVDRD-3341
NAVORD-4366
NAVORD-576S
NAVQRO-5894
NAVORO-5904
NAVORO-5939
NAWORO-5957
NAVDRD-6076
NAVORO-6227
NAVORD-6244
NAVORD-6415
NAVORD-6495
NAVORD-6496
NAVORO-6496. pC. 2
574
324
345
167
167
990
98
IIS
US
112
112
624
344
453
100
100
7S4
S3
IB7
334
601
429
B3S
BOl
B07
215
7W
932
333
115
US
215
96
9S
US
US
213
633
4S7
357
736
B04
9M
708
161
IB
13
BB9
74S
210
369
3B9
710
14
14
738
S3B
406
752
35
735
330
778
329
94
792
100
100
101
7S4
Ml
41«
101
752
168
625
39
496
615
634
553
345
71
740
601
61
576
630
757
337
331
611
611
11
NtMnber j
r>E
Number
I!!!
NAVOItD-4611
NAVOIU>-«6;U
NAVORD-4663
NAVOR£>-«675
NAVOIlO-«6M
NAVORD-67a6
NAVOIU>-«727
MAVDiU>-«741
NAVORO-*74a
MAVOIlD-*921
NAVORD-7014
NAVORO-7157
NAVDIIO-7JK
NAVPERS- 10786
NAVSHIP5-250-346-3
N A VTRADEVCEN ■ 9- U - 1
NAVniAIjeVCEN- 166-1-41
NAVTllAOeVCEN-.9*-2
HAYnuicmycBti-ut-2
NAvnuavcm -513- 1
NAVTHAOBVCEN-SM- 1
NAVTHAOeVCEN- 1«8-
ao-4
NAVWEn-Sl*74
NAVWEfS-MOS
NAWEn-tOlft
NAVWEPS-6113
NAVWEPS-4IM
NAVWEJ8-6774
MAVWEPS-67M
NAVWEPS-6«4«
NAVWEPS-7016
NAVWEPS-7043
NAVWEPS-70M
NAVWEPS-7076
NAVWE»-70«6 ,
NAVWE«-7W4
NAVWEPS-7096
HAVWBPS-709*
NAVWEPS-7103
NAVWE«-7104
NAVWEPS-7152
NAVWBFS-7160
NAVWEP5-7161
NAVWQ^ 7254
NAVWEPS-7a64
NAVWEPS-7289
NAVWEPS-7290
MAVWEPS-7292
NAVWER 7302
MAVWW5 73l»
NAVWEPS 7563
l«AVWEPS-7564
NAVWEPS 7565
MAVWEPS-7566
NAVWEPS 7569
MAVWEPS 7612
MAVWEPS SSL-AC-OS
NAVWEPS SSL-AE-01
MAVWEPS SSL-AE-08
NAVWEPS SSL-AE-25
NAVWEPS SSLAF-21
NAVWEPS SSL -AG- 47
NAVWEPS SSL-AC-48
NAVWEPS SSL-AG-51
NAVWEPS SSL-Al-02
NAVWEPS SSL-AR-06
NAVWEPS SSL-AZ-09
NAVWEPS SSL-BC-01
NAVWEPS SSL-BC-02
NAVWEPS SSL-BC-Oa
MAVWEPS SSL-BC-04
NAVWEPS SSL-BC-06
MAVWEPS SSL-BE-Ol
NAVWEPS SSI, BE -02
NAVWEPS SSL BE 03
NAVWEPS SSL BE -08
NAVWEPS SSL BF-06
NAVWEPS SSL-BL-01
NAVWEPS SSL-BR-02
NAVWEPS SSL-BR-08
NAVWEPS SSL-BR-04
NAVWEPS SSL-CL-02
NAVWEPS SSL-CR-02
NAVWEPS SSL-OC-06
NAVWEPS SSL -HA -01
MAVWEPS SSL-HA-09
NAVWEPS SSL-HA-09
NAVWEPS SSL-HA-06
NAVWEPS SSL -HA -07
NAVWEPS SSL-HF-04
NAVWEPS SSL-HF-08
NAVWEPS SSL-HF-06
NAVWEPS SSL-HF-07
7»7
NAVWBK
ISL-HV-02
424
730
NAVWEPS feSL-HV-04
424 ■
639
NAVWBK BL-HV-05
292
736
NAVWEPS SL HV-06
424
634
NAVWEPS feL-NF-02
328
W9
NAVWEPS SSLNM-02
406
SOS
NAVWEPS fSL-N*4-03
336
■m
NAVWEPS SSL NP-02
465
7*5
NAVWEPS 6SL-NR-01
468
331
NK-6062 .
430
694
MS TN-2-2
IBS
806
NB TN-H 3
130
753
MB TN -11-4
IS)
97
NK TN-ll-S
uo
75
NS6 TN-l«j-7
390
360
NBE TN-li-l
SOS
171
NB TO-«
465
134
NK -IM-6^
82
41
NK TN-6:
112
137
MB -nt-n
23
10
tm TH-T.
130
NK TN-7:
36
399
NB TN-7'
103
430
MB TN-71
7*7
123
MB TN-r
S3
739
NK TN-71
IM
773
NK TN-7<
M6
771
NK TN-SI
US
757
NK TN-S:
419
768
NK TN-S:
303
739
NK TN-81
479
335
MB TN-81
US
443
MB TN-r
us
583
NK TN-81
MB
31
NK TN-ll 16
m
61
NCBL MH30
753
380
NCEL M-133
7IS
315
NHRI. M-135
743
308
NCEl. Mh36
714
191
NCRl. M-' 42
739
280
NCFl. M-S48
714
576
NCEL M-(53
736
792
NTRI, 14-174
743
730
NCEL M-180
713
321
NCEL M-iei
714
331
NCFJ. M-(«4
717
JOS
NCEL M-S90
790
303
nCEL Mh 196. re».
713
763
NCRl. M- Oi re».
717
321
NTRI. M-|04
714
321
NCRt. M-
06
714
443
NCEL M-
10. tuppl.
716
443
NCEL M-
13
713
739
NCEl. M-
22
716
418
NCEL M-
23
745
SS6
NCEL N-(
08
73S
S04
NCEL N-(
12
747
423
NCEL N-(
15
7S3
291
NCEL N-(
19
741
291
NCEL N-(
21
7U
389
NCEL N-(
29
730
423
NTKI. N-(
60
• 74S
423
NCEl. N-(
63
781
434
NCRl. N-l
70
742
422
NCEL N-(
71
729
290
NCEL N-(
75
7U
291
NCRl. N-l
81
717
422
NCEL N-
•5
747
289
MCEL N-l
•6
716
290
NCEL R-
194
313
290
NCEL R-
197
613
290
NCEL R-
03
SBS
290
NCEL N-
06
716
291
NCEL N-
09
746
291
NCEL N-
11
7SS
289
MTRI. N-
28
73»
289
NCEL N-
39
7U
292
NCEL N-
45
715
292
NCEL N-
49
717
291
NCEL N-
.57
743
5i
NCRI. N-
,58
730
NCEL N-
60
743
292
MCEL N-
68
751
292
NCFJ. N-
71
701
424
NCEL N-
,75
746
433
NCRl. N-
.76
^
423
NCEL N-
i95
423
NCEL N-
D2
715
423
NCEL N-
tl2
749
423
NCEL N-
il6
716
424
MCEL N-
02
715
424
NCEL N-
140
716
423
NCBL N-
141
716
414
NCEL N-
144
715
NCEL N-249
NCRl. N-255
NCEL N-367
NCEL N-276
NCEL N-277
NCEL N-281
NCEL N-292
NCEL N-297
NCEL N-299
NCEL N-300
NCEL N-302
NCEL N-319
NCBL N-333
NCEL N-337
NCEL N-354
NCEL N-3ai
NCEL N-389
NCEL N-392
NCEL R 002
NCEL R-003
NCBL R-a07
NCEL R-0e7
NCEL R-089
NCEL R-091
NCRl. R-109
NCKl. R-UO
NEL-258
NEL-478
NEPA-303-EMM-6
NEPA-354-EAM-S15
NEPA-3M EAM-S17. rev
NEPA-398-SCM-6 /
NEPA-406 EMM 1^
NM 11 02 12.4. S-9
NM 18 02 99. R-80
NM 001 058. 25. 02
Ml 001 no 500.37
NM 006 012.04.43 .
NM 006 012.04.44
NMC-TM -60-56
NMC-TM -60-63
M«-9404
NM. Ra(-60-|
NOL BRR-9
NOL BRR-18
NOL MCM-12
NOL MCM-13
NOL MM-U
NOI. MDM-15
NniX:-425
NOLC-4S7
NOU:-478
Nnix:-5i4
NOU:-528
Nai^-533
Nnix:-537
NOLC-S38
NOR -60- 16
NOi:S-279
NOTTS- 294
NCTS-701
NOTS-882
NOTS-2n3
NOTS s-re-3
NOTB TA-2
NOTS TA-7
NOTS TM-786
NOTS TM-1113
NOTS TP-2041
NOTS TP-2M8
NOTS T? r43
NOTS TP-2354
NOTS TP-2371
NOTS TP-2372
NOTS TP-2377
NOTS TP-2379
NOrre TP-2434
NOTS TP-2452
NOTS TP-2458
NOTS TP-24B6
NOTS TP-2497
NOTS TP-2513
NOTS TP-2517
NOTS TP-2519
HOTS TP 2521
NOTS TT-25r
NOTS TP 2528
NOTS TP-2531
NOTS TP 2532
NOTS VBXi
NOTS TP-2535
NOTS TP-2536
NOTS TP- 2541
7lS NOTS TP-2967 7K
TIS NOTS TP 2582 4Ba
714 NOTS TP-2610 BO*
715 NP-6364 •!•
744 NP-6712 77*
743 NRCC-5893 lit
746 NROC-5917 IK
743 NRCC-5918 IK
714 NROC-S919 IK ■
713 NRCC-5927 KB
729 NROC LR-186A KB
729 NROC LR-274 SK
7S1 NROC LR-278 IK
7S1 NRCC LR-284 IK
716 NROC LR-2SS IK
743 ,- NROC LR-288 B3I
789 NROC LR-289 MB
785 NROC LR-290 KB
717 NROC LR-291 711
717 . NROC MA-243 4n
739 5 NROC MB-225 481
714 -• NROC MB- 226 9H
181 NROC MD-45 7V
418 t' NRCC MD-46 73S
313 NROC MH-100 609
430 NRCC MI-822 377
717 NRCC MP- 17 SU
32 NROC MS- 103 KB
53 NROC MS- 103 Ml
784 NROC MT-41 2U
782 NRL-399e SM
782 NRL-4037 SOt
782 NRL-4129. si^ip. 3M
782 NRL 4164 K*
36 .NRL-4306 M
140 NRL-5386 7M
763 NRL-5413 4tU
368 NRL-5499 SS
692 NtL-5501 71
692 NRL-5506 M
544 NRL-5513 104
689 NRL-5S14 KB
96 Nia--5516 M
383 Nia.-5517 «
772 NRL-5520 •!
768 NRL-5521 MO
321 NRL-5523 IK
321 NRll-5530 MS
321 NRL-S532 4M
321 NRL-5534 iU
601 NRL-5538 3K
61 NRL-5545 441
430 NRL-S547 31*
122 NftL-5948 S3
576 NaL-5549 431
806 NRL-5550 991
792 NRL-5551 K4
730 NRL-5553 71
287 NRL-S5S4 144
625 NRL-5555 4K
39 NRL-5556 277
436 NRL-5557 MB
634 NRL-S560 3K
337 NRL-5563 3»
308 NRL-5S6S IM
m NRL-5366 14B
443 NRL-5578 363
313 NRL-5580 990
321 NRL-5581 9*1
71 NRL-5582 77*
730 NRL-5593 57*
439 NRL-5606 7U
767 NRL MR-1127 < 730
694 NRL RD 257 30B
309 NSP C-3661 1»4
341 NSP G-49S1 10
335 NSP G-5276 *M
443 NSP G-5754 ,IK
583 NSP G-5939 Mf
443 NSP G-5939 IM
31 MP G-7368 Kl
61 NSP G-9670 9M
3B0 NBF G-10375 1*4
315 N6F C-1071S 323
430 NSP G-Y/9.7/79 33
308 NSP G-Y/9. 14/139 33
191 NSP C-Y/32. 48/272 308
380 NBP Y/9.5/80 *]*
431 ML-437 337
443 NSL-441 119
44S ML-442 *34
73» NEL-443 49*
418 ML-454 «74
S» NSL-462 43*
12
NiMober
MROP -45
MROP ER-2.5082
NSROP ER-2.5082lf
NWL-1599
NWL-1715
NWL-1722
NWL-1724
NWL-1725
NWL-1736
NWPW-T-6-59
NWPW-T-7-59
NWPW-T-35-59
NYU TR-400-14
NYU TR-400-16
OMCC-9038-aR-3
ONR-7
OORR 60-2
OORR-770- . . .
OORR-821.6
OORR -839. 10-P
OORR -968. 30-M
OORR-968. 31-M
OOftR-ll«2: ...
OORR- 1253. 30
OORR-1469. 1
OORR -1510. 8 -P
OORR- 1538. 13-E
OORR -1543. 16 -P
OORR- 1574:5
OORR-1597- ...
OORR- 1597: 10-M
OORR- 1604:12-0
OORR-1716. 13-E
OORR- 1833. 2-M
OORR-1840.9-M
OORR- 1840. tS-M
OORR-18S7.4-M
OORR- 1863. 3-M
OORR- 1923. 5-C
OORR-2045.3-P
OORR - 2070. 1-M
OORR-212S.6-M
OORR-212S. 12-M
OORR-2307.S-E
OORR-2207.6-E
OORR-2211.1-P
OORR-221S. 14-M
OORR -22'|6. 2-M
OORR-22'16 4-M
OORR-2aM.3-E
, OORR- 2304. 1-C
OORR-2360
OORR-2360- ...
OORR-2360...
OORR- 2422. S-M
OORR -2560. 1-M
OORR 2S60. 2-M
ORD M7-230
ORD F-2O-30S
ORO P-30-311
ORD P-20-136
ORD P-20-137
ORD P-30-138
ORD P-20-139
06RD-6111
OSURF-398-P
06URF-«53. PR
06URP -691-1
OSURF-716-7
OSURP -716-8
06URP-716. Pinal
OSURF -778-1
06URF-79e-8
06URP-818
CBURP-823-1
OSURF-827-4
aSURF-8r-6
OSURF -854-1 J
06URF-882-53
OSURF -896-1
OSURF -896 -2
OSURF -896-6
a6URF-973-2
06URF-1073-1
OSURF -1073 -2
OSW ROPR-43
CSW ROPR 44
OSW RDPR 45
OSW RCPR-46
OTAC LL-55
OTAC LL-57
OTAC LL-59
OTAC n.-60
OTAC LL-61
Number
Page
Number
UB
OTAC LL-64
751
PB 147 530
441
OTAC LL-65
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593
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PB 147 533
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OTAC-RR-30
588
PB 147 559
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738
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169
PB 147 588
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CI-R-340. lurpl-
472
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199
PB 147 643
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PS 147 646
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623
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199
PB 147 743
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116
PB 147 746
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PB 147 748
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168
PB 147-756
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PB 147 757
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168
PB 147 765
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169
PB 147 767
763
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208
PB 147 768
490
OTS SB- 435
472
PB 147 775
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391
PB 147 776
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PB 147 778
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PB 147 780-
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PA TN-27
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70
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PA TR-36,58
738
PB 147 908
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PB 147 963
100
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PB 147 170
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PB 147 243
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PB 148 154
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PB 147 305
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PB 148 281
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PB 148 287
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PB 148 288
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PB 148 293
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169
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148 724
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re 150 086-6
304
re 150 0*6-7
299
re 150 086-*
348
re 150 086-9
343
re 150 0*8
M
re 150 0*9
m
re 150 096
1*1
re 150 097
20B
re 150 100
146
re 150 101
194
re 150 109
sn
re 150 133
30»
re 150 160
211
re 150 170
342
n 150 171
94
re 150 198
217
re 150 307
217
re 150 213
nr
re 150 214
151
re 150 215
30*
re 150 216
96
re 150 217
306
re 150 218
170
re 150 219
170
re 150 227
in
re 150 229
re 150 230
193
re 150 243
VU
re 150 2*0
341
re 150 2*2
2*9
re 150 317
341
re 150 318
342
re 150 319
337
re 150 320
39*
re 150 321
336
re 150 322
320
re 150 323
S30
re 150 327
40*
re 150 329
333
re 150 331
332
re 150 332
IM
re 150 334
8»
re 150 335
sn
re 150 336
Stt
re 150 338
s«
re 150 346
•91
re 150 347
S*
re 150 349
s>»
re 150 351
7«
re 150 361
79*
re 150 368
324
re 150 369
90
re 150 371
70*
re 150 372
771
re 150 374
609
re 150 378
719
re 150 388
730
re 150 390
53
re 150 391
31*
n ISO 392
60*
re 150 406
694
re 150 407
6*6
re 150 412
30*
re 150 413
799
re 150 414
59
re 150 415
134
re 150 416
316
re 130 417
781
re 150 418
315
re 150 430
700
re ISO 431
79*
79*
•m
•m
491
451
453
624
24
108
437
84
39
723
701
41
2*
7*4
7*7
30
16
1*
IS
11
156
13
15
*06
18
17
•03
94
73
399
49
431
9*6
174
533
471
606
5*
•9
66
39
2B
36
68*
•6
•7
100
99
I
••
9
• 97
7
10*
10*
151
71
179
171
99
23
•9
lot
709
109
83
34
131
30
39
Number
Number
14
re ISO
re 150
re 150
re ISO
re ISO
ra ISO
re ISO
re ISO
re ISO
re 150
re ISO
re ISO
re ISO
ra ISO
re ISO
re ISO
ra ISO
re ISO
re ISO
re ISO
re ISO
re ISO
re ISO
re ISO
ra ISO
424
429
430
431
432
433
436
437
438
439
440
441
442
443
444
445
446
447
ra 150
ra 150
ra 150
ra ISO
ra 150
n ISO
ra 150
ra 150
ra ISO
ra ISO
ra ISO
ra ISO
n ISO
ra ISO
re ISO
re ISO
re ISO
re 150
ra ISO
ra 150
ra ISO
ra ISO
ra ISO
ra ISO
ra ISO
ra ISO
ra ISO
re ISO
ra ISO
ra ISO
n ISO
ra ISO
ra ISO
ra ISO
ra ISO
ra ISO
n ISO
n ISO
ra ISO
ra ISO
ra ISO
ra ISO
ra ISO
n ISO
re ISO
ra ISO
ra 150
re ISO
re ISO
re ISO
re ISO
ra ISO
ra ISO
ra ISO
ra ISO
re ISO
re ISO
re ISO
re ISO
re ISO
ra ISO
ra ISO
re ISO
ra ISO
ra ISO
re ISO
re 150
re ISO
ra ISO
449
450
451
452
454
456
457
458
459
461
466
467
468
469
470
471
472
473
474
475
476
477
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
500
501
502
503
504
507
508
S09
510
»11
514
SIS
516
517
518
519
530
521
S22
523
524
525
536
577
528
529
531
532
534
535
536
537
109
re 150 538
107
ra 150 539
Wf
re 150 540
m
re 150 541
309
ra 150 542
«99
ra 150 543
•1
ra 150 544
91
re 150 545
49
ra 150 547
14
ra 150 548
14
ra 150 552
1*
ra 150 556
13
ra 150 557
113
re 150 558
32
ra 150 560
32
ra 150 S61
94
ra 150 562
119
ra 150 561.
PB 150 564
92
98
ra 150 565
.107
ra 150 566
2
re 150 567
34-
ra 150 568
99
re 150 569
61
re 150 570
57
re 150 571
39
re 150 572
63
ra 150 573
39
re 150 574
79
re 150 575
99
re 150 576
99
re 150 577
*39
ra ISO 578
90
ra 150 S92
17
ra 150 593
•
ra 150 594
99
ra 150 595
117
ra 150 596
.11
ra 150 597
80
ra 150 598
*0
ra 150 599
••
ra 150600
*9
ra 150'601
90
ra 150 602
79
ra 150 603
7*
ra 1S0604
6
ra 150605
•1
ra 150606
148
ra 150607
lU
ra 150608
33
ra 15Q609'
20
ra 150610
707
ra 150611
•
ra 150612
75
ra 150613-1
99
ra 150613-2
95
ra 150614
10*
ra 150615
12s
ra 150 616
•0
ra 150617
••
ra 150 618
7
ra 150619
139
ra 150 630
110
re 150 621
919
ra 150 624
9
ra 150626
9
ra 150 677
119
ra 150 628
•2
ra 150629
7*
re 150 631
609
re 150 633
47
ra 150 634
*0
ra ISO 636
34
ra 150 637
101
ra 150 638
2
ra ISO 639
97
ra ISO 641
34
ra 150 643
54*
ra 150 644
77
ra 150 645
79
ra 150 646
100
ra 150 647
S3
re 150648
114
re 150 649
109
re ISO 650
U
re 150 651
t*
re 150 652
34
re 150 654
*5
re 150 656
118
re 150 657
803
re 150 663
703
re 150 664
27
re 150 665
113
re 150 666
P«£e
Number
24
re 150 666
V
ra 150 669
•9
ra 150 671
III
re 150 673
9
ra 150 678
110
ra 150 679
110
ra 150 680
794
^ ra 150 681
110
re 150683
73
re 150 684
43
re 150 686
115
PB 150 687
US
ra 150 688
794
ra 150 689
19
ra 150 690
19
ra 150 691
22
ra 150 692
15
re 150 693
17
re 150 694
16
re 150 695
18
re 150 696
17
re 150 697
14
re 150 698
21
ra 150 699
17
ra 150 700
63 ■
ra 150 701
15
ra 150 702
2
re 150 703
20
re 150 704
22
re 150 705
18
re 150 706
16
ra 150 707
16
ra 150 70*
49
ra 150 709
49
ra 150 710-1
48
ra 150 710-2
49
re 150711
212
re 150 712
49
re 150 713
82
ra 150 714
82
ra 150715
78
re 150 716
50
re 150 717
190
re 150 718
HI
re 150 719
167
re 150 730
166
re 150 721^
87
re 150 722
544
re 150 723
48
re 150 724
49
re 150 725
130
re 150 736
67
re 150 730
67
re 150 733
65
re 150 734
65
re 150 735
1
re 150 736
1
re 150 737
1
re 150 738
31
re ISO 739
284
re 150 740
TH
re 150 741
89
re 150 742
85
re 150 747
774
re 150 748
61
re 150 749
3*
re 150 753
109
re 150 754
11*
ra 150 755
69
re 150 757
112
re 150 762
*4
re 150 764
606
re 150 765
99
n 150 766
10
re 15<J767
10
re ISO 768
77
ra 150 769
794
re 150 770
lOS
re 150 771
46
re 150 772
79
re 150 773
62
re 150 774
43
re 150 775
•I
re 150 776
119
re 150 777
114
re 150 778
79
re 150 780
692
re 150 781
408
re 150 783
*M
re 150 784
•»
'* re 150 788
57
re 150 790
SO
ra 150 792
111
re 150 793
Number
159
re 150 794
119
ra 150 795
.21
ra 150 796
m
ra 150 797
■m-
ra 150 798
m:
ra 150 799
•BO"
re 150 800
41
ra 150 801
SI
ra 150 802
99
•ra 150803
109
ra 150 804
101
ra 150*06
473
ra 150 806
429
ra 150 809
406
ra 150 810
413
. ra 150811
430
ra 150 812
463
re 150 813
464
re 150 814
466
re 150 815
619
re 150 816
419
re 150 817
435
re 150 818
433 ■
re 15(t819
463
re 150 830
623
re ISO 822
439
re 150 823
430
ra 150 825
421
ra 150 830
411
ra 150 831
444
ra 150 833
430
ra 150 834
463
ra 150 835
433
ra 150 836
434
ra 150 837
434
ra 150 83*
450
ra 150 839
433
ra 150 842
444
ra 150 843
450
ra 150 844
433
ra 150 845
433
ra 150 846
633
ra 150 847
479
ra 150 848
442
ra 150 849
431
re 150 850
414
re 150 851
992
ra 150 852
413
re 150 853
436
re 150 854
451
re 150 855
•06
ra 150 856
699
re 150 857
9*
re 150 858
117
re 150 859
130
re 150 860
51
re 150 861
8*
ra 150 862
118
ra 150 864
768
ra 150 866
41
ra 150 867
3
ra 150 868
419
ra 150 870
60
ra 150 871
108
re 150 872
114
re 150 873
39
re 150 874
45
ra 150 875
27
re 150 876
ill
re 150 877
11*
re 150 879
S3
re 150 880
31
ra 150 882
32
ra 150 883
83
n 150 8*6
74
re iso*S7
39
re 150*90
74
re 150 891
74
re 150 892
74
re 150 894
74
ra 150 895
74
ra- 150 896
74
re 150 897"
9*
re 150 89*
64
ra 150 899
103
ra 150 900
778
re 150 901
146
re 150 902
38
re 150 903
111
re 150 904
19
re 150 906
134
re 150 90*
724
re 150 909
1*7
're 150910
Est.
9
190
4*
174
174
60
21*
5
«7
165
43
4*
45
SI
51
US
fl3
43
44
43
122
123
107
107
56
59
60
60
306
63
6*
131
^21
121
121
90
53
757
75*
736
725
706
719
95
10
10
*•
14
95
19
204
25
10
303
65
29
7*6
770
31
63
2^
«9
103
39
120
92
69
94
119
105
65
77
*l
137
US
lis
108
973
953
960
374
374
391
734
718
727
739
539
739
783
764
722
IS
Number
Number
|i
I30 9U
ISO 912
ISO 913
ISO 914
ISO 913
ISO 916
ISO 917
ISO 920
ISO 921
ISO 922
ISO 923
ISO 925
150 926
ISO 927
n 150 92*
n 150 929
150 930
ISO 931
150 932
150 933
150 934
150 935
150 936
150 937
150 938
150 939
ISO 940
150 941
Pf 150 943
n 130 943
150 944
ISO 945
^946
150 949
150 991
150 952
150 954
150 953
150 957
150 9M
150 959
150 961
PI 150 962
150 963
150 964
150 966
150 967
150 9*9
n 150 970
n 150972
Pt 150 973
PB 150 974
PB 150 97S
S 150 962
150 965
Pt 150 968
ISO 969
150 991
150 992
150 993
1S0 994
150 996
150 999
151 072-R
131 064
131 CM
131 09S
PB 151 096
PB 151 097
151 096
151099
ISl 100
151 101
151 103
151 103
151 104
151 106
151 106
PB 151 107
PB ISl 106
PB 151 361-2
PB 151 377-3
PB 151 377-4
131 377-5
131 377-6
131 S77-7
131 377-8
131 933
152 000
PB 152 001
PB 152 002
PB 152 003
PB 152 004
PB 153 006
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
723
730
733
711
7BS
n
417
»
MB
4
4
4
4
9t
3
3
3
2
2
3
100
lOB
631
lOB
7«
90
68
117
58
43
58
317
73
44
63
140
700
115
59
65
83
333
9
456
36
117
61
116
10
■ 78
761
67
67
199
614
301
66
93
330
498
613
4S9
437
612
461
779
779
778
776
776
155
130
130
130
331
350
806
769
97
U
13
19
730
751
PB
PB
PB
PB
PB
152 Odb
152 0(7
132 O a
152 0(9
152 01 5
PB 1S2 0I6
PB 152 01 7
PB lS2a!2
PB 152 0 6
PB 152 or?
PB 152 018
PB 152 019
PB 152 010
PB 152 011
152 0)2
152 0^
152 0 14
152 015
152 016
152 a 19
152 010
1S2 0 tl
132 013
132 0 0
PB. 132 Q r
PB 152 0 19
PB 152 CM)
PB 152 0 SI
PB 152 CU
PB 152 CM
PB 152(55
PB IA2(iM
PB n2
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
(57
152(58-1
152(58-3
152 ( 59
152151
152 I 62
152163
152 ( 64
P» 152 I 66
PB 153 I 67
152 I 68
152 I 69
152 I m
152ir71
152 I r73
lS2ir74
152 1 176
152 177
152 P")
PB 152 185
PB 153 m
152
152 189
152 p91
152 092
1521)94
152 095
152096
152097
52 098
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
152
152
152
152
152
152
152
152
152
152
152
152
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB 152 099
n 152|l00
PB
PB
PB
PB 152|104
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB ^
PB 153 133
PB is: 134
PB is: 135
PB 15] 136
PB is: ir
PB i5i 138
r» is: 130
PB 15^131
PB iSl 132
PB is; 133
PB is: 134^
101
102
103
1(»
106
107
108
109
110
HI
112
113
152 114
152 115
152 117
153 118
153 121
is: 122
790
PB 152 135
751
PB 152 136
791
PB 152 137
791
PB 152 138
193
PB 152 139
233
PB 152 140
199
PB 152 142
738
PB 152 143
90
PB 152 144
71
PB 152 145
13
PB 152 146
12
PB 152 147
• 12
PB 152 148
i U
PB 152 149
11
PB 152 150
13
PB 152 151
316
PB 153 152
133
PB 152 153
110
PB 152 154
64
PB 152 155
43
PB 152 156
41
PB 152 157
Ml
PB 152 158
tl
PB 152 159
«
PB 152 160
71
PB 152 161
Si
PB 152 162
120
PB 152 163
76
PB 152 164
3
PB 152 165
63
PB 152 166
S4
PB 152 167
S
PB 152 168
«a
PB 152 169
9t
PB 152 170
119
PB 152 171
7a8
PB 152 173
61
PB 152 173
174
PB 153 174
171
PB 152 175
77
PB 152 176
77
PB 152 177
118
PB 152 178
193
PB 152 179
•31
PB 152 180
'M
PB 152 183
67
PB 152 185
201
PB 152 186
PB 152 187
106
PB 152 188
160
PB 152 189
185
PB 152 190
U
PB 152 191
B
PB 152 192
21
PB 152 193
181
PB 152 194
43
PB 152 195
210
PB 152 196
2»
PB 152 197
X
PB 152 199
31
Pt 152 200
8
Pt 152 301
M
Pt 152 302
77
Pt 152 304
■ 11
Pt 152 205
9S1
Pt 152 306
7
Pt 152 207
•
Pt 152 308
IM
Pt 153 309
77
Pt 193 310
•
Pt 152 211
7t
Pt 152 212
77
Pt 152 213
IS
Pt 152 214
11
Pt 152 215
139
Pt 153 316
116
Pt 193 218
•07
Pt 152 219
47
Pt 152 330
779
Pt 152 236
19
Pt 152 227
134^
Pt 152 228
97
Pt 152 239
7
Pt 152 230
lOB
Pt 152 331
224
Pt 153 232
r
PB 152 233
181
PB 152 241
972
PB 152 242
64
PB 152 344
46
PB 152 245
»
PB 152 347
M .
PB 152 249
1
04
PB 152 290
Hi
PB 152 251
f
PB 152 254
Ml
PB 152 255
M
PB 152 256
V
PB 152 257
41
PB 152 298
•
PB 152 259
m
PB 152 260
MO
PB 152 361
m 1
PB 152 262
PB 152 363
MP
PB 152 364
lip
PB 152 271
■E
PB 152 272
9k'
PB 152 273
' iW
PB 152 281
8
PB 152 282
fg
PB 152 283
m •
PB 152 284
1*
PB 152 289
m
PB 152 290
m
PB 152 291
i
PB 152 292
PB 152 294
m ■■
PB 152 295
8
PB 152 296
PB 152 297
1*2
PB 152 296
130
PB 152 299
130
PB 152 300
130
PB 152 301
110
PB 152 302
ISO
PB 1^2 303
301
PB 152 309
90
PB 153 310
259
PB 152 311
133
PB 152 312
86
«PB 152 313
331
PB 152 314
75
PB 152 315
76
PB 153 316
76
PB 153 319
7
PB 153 330
215
PB 152 321
799
PB 152 343
55
PB 152 344
113
PB 152 345
213
PB 152 348
45
PB 152 349
43
PB 152 350
34
PB 152 351
104
PB 152 352
41
PB 152 353
43
PB 152 354
29
PB 152 355
43
PB 152 356
30
PB 152 357
150
PB 152 358
66
PB 152 359
794
PB 152 360
97
PB 152 361
306
PB 152 364
189
PB 152 365
133
PB 152 366
188
PB 152 367
150
Ptf 152 368
150
PB 152 369
307
PB 152 370
133
PB 152 371
139
PB 152 372
133
PB 152 373
131
PB 152 374
189
PB 152 375
315
PB 152 376
134
PB 152 377
141
PB 152 378
149
PB 152 380
171
PB 152 381
796
PB 152 384
164
PB 152 385
151
PB 152 387
162
FB 152 388
165
PB 152 389
160
PB 152 390
166
, FB 152 391
> PB 152 393
230
97
PB 152 394
467
PB 152 396
219
PB 152 398
146
PB 152 399
196
PB 152 403
141
PB 152 406
136
PB 152 409
197
PB 152 411
164
393
134
176
180
219
174
193
301-
163
140
141
137
137
30 •
133
133
306
133
78
150
212
» 79
79
40
St
70
108
102
5
307
131
153
49
110
44
86
37
49
37
438
419
4S9
43S
1S7
181
101
172
143
38
10
90
22
70
40
00
07
100
100
«
S7
219
167
142
142
271
no
M»
U«
100
lOS
tot
319
319
200
200
179
175
IM
MO
193
192
137
137
132
144
M
MO
m
140
16
i^
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
Pt
Pt
Pt
Pt
PB
PB
PB
PB
PB
PB
PB
PB
, Pt
r Pt
Pt
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
Number
I 193 413
152 416
152 418
152 419
152 420
152 421
152 422
152 423
152 424
152 426
152 427
152 428
152 429
153 430
152 431
152 432
152 433
152 434
152 435
152 436
152 437
152 438
152 439
152 440
152 441
152 442
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152 444
152 445
152 446
152 447
152 448
152 450
152 451
152 452
152 453
152 454
153 455
152 456
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152 460
152 462
152 463
152 464
152 465
152 466
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152 468
152 469
152 470
152 471
152 473
152 473
152 474
152 476
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152 478
152 479
152 480
152 481
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152 484
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152 489
152 490
152 491
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152 493
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152 502.
152 503
152 504
152 513
152 517
152 519
152 520
152 521
152 522
152 523
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152 527
152 528
152 529
152 531
152 532
152 534
152 535
152 536
152 537
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PB 152 539
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Ft 152 540
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PB 152 541
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PB 152 542
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PB 152 543
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FB 152 548
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PB 152 557.
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PB 152 559
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PB 152 565
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PB 152 567
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PB 152 569
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PB 152 570
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PB 152 580
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PB 152 581
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PB 152 583
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152 603
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152 604
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152 605
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152 606
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152 607
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152 608
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152 609
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152 610
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152 612
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152 614
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152 616
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152 617
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152 618
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152 622
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152 623
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152 624
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152 625
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152 636
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152 628
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152 629
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152 630
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152 631
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SEL TR-104-5
900
STL^rR-60-00(X)-94316
800
PB 171 486
592
PB 171 600
6«8
PTC 2478 59R
592
RADC-TR-59-27
683
SEL TR- 157-1
4S3
STL/TR-60-(K)(«>-GR369
116
PB 171 487
614
PB 171 601
m
PPL-TR-60-2
312
RADC-TR-59-39
155
SEL TR-207-2
107
STL,mi -6O-()0nO-(»3O3
800
PB 171 488
614
PB 171 602
6*0
PPL-TR-60-3
.,ur
RADC-TR -59 -44
156
SEL TR-303-1
493
STL/TR -60-(l( KK)-CR3 10
636
PB 171 489
553
PB 171604
770
PPL-TR-60-6
'IM
RADC-TR-59-53
300
SEL TR-308-2
133
STL/TR -60-0000- N R356
797
PB 171 490
617
PB 171 60S
'•
PRB TRN-107
»2
RADC-TR-59.-62
725
SEL TR-315-1
493
STL/TR -«O-a000-GR4l3
800
PB 171 491
617
PB 171 606
MS
PRB TRN-108
312
RADC-TR -59-65
153
SEL TR-3I6-2
433
SUDAER-97
797
n 171 492
571
PB 171607
MB-
PRB TRN-109
9*9
RADC-TR -59-77
783
SEL TR-361-1
734
SUUi!M-I24
88
PB 171 493
619
PB 171608
Ml
PRP-1203
188
RADC-TR-59-110, *. 1
765
SEL TR-401-2
794
SUI-59-11
9
PB 171-^494
589
PB 171609
7M
PRMSTL)9-18
346
RADC-TR-59-110. ». 2
766
SEL TR- 404-1
95
SUI-59-22
2
PB 171 495
542
PB 171610
» r
Proj. 6X59-06-001
142
RADC-TR-59-110. ». 3
766
SEL TR-1502-1
lU
SUI-59-23
f7
PB 171 496
584
PB 171 611
ProJ. 9R38-01-015
709
RADC-TR-59-110, ». 4
766
SEL TR-1504-l
602
SWRG MWT-4
415
PB 171 497
551
PB 171612
7S3
PSl-3000:15-24-Q
109
RADC-TR-59-110. v. 5
766
SEL TR-1506-1
767
SWRJ EE-384
752
PB 171 498
568
PB 171613
791
PSI-3000:l5-25-Q
303
RADC-TR-59-110. v. 6
766
SEL TR-1507-1
S7S
TAM- 152
56
PB 171 499
586
PB 171614
TM
PSl-300O:21-2-Q
113
jRADC-TR-59-llOG
451
SEL TR-1551-3
432
TAM-153
60
PB 171 501
615
PB, 171 616
7n
PSl-.TOnO:21-3Q
113
RADC-TR -59- llOH
451
SEL TR-1553-1
S06
TAM- 158
453
PB 171 502
609
PB 171617
754
PSl-3000;21-4-Q
213
RADC-TR-59-124
<2E^
SEL TR-anOJ-l
783
TAM- 159
453
PB 171503
638
FB 171 618
IM
FME-ML-E-412-8. PR
758
RADC-TR -59- 128
*^
SEL TR-2051-l
S5
TAMC Ref-58-25P
413
PB 171 504
566
PB 171 619
: 3
IWB-ML-P-300-10
314
RADC-TR-59-142
764>
SEL TR-2101-1
55
TAMC Ref-59 24T
33
PB 171505
S61
PB 171 620
PU AEL-442
327
RADC-TR-59-144
733
SEL TR-2102-l
S6
TAMC Re(-60-8DU
151
fB 171306
561
PB 171684
7M
TV AEL-469
196
RADC-TR -59 -159
722
SEL TR-21(B-1
734
TAMC Ref-60-19T
707
.
PU AEL-477
913
RAOC-TR-59-160
722
SEL TR-59-104-2a5-704.3
94
TAR-TN-59-1
79
,
RAOC-TR-59-170 .
720
SEP-PSD59-4
304
TC-235-25 •
579
^
■
RAOC-TR-59-175
i.
731
23
. 1
Shells- 13649
t
72
TCC-EI20-59
i
316
Hmabn Page
TDl 900 151
TED ADC AE- 1412.1 U
TED ADC AE-1412.1 14
TED ADC AE-TOOOl 709
TED ADC EL-S49 1*1
TED ADC ES-7O45<5915-li0 13
TED ADC RS-704S(5915-A) 2M
TED ADC RS;7045<»15.M) 16
TED ATTS-11APP-J007. 1,
pt. 4 416
TED NAM-04614 35
TED NAM AE 1403. 1 14
TED NAM An- 1404. pi. 1 S36
TED NAM AE 4110. pi. 14 77*
TED NAM A£ 4*177, PR 330
TED NAM AE- 42222. pi. 3 752
TED NAM AE-51143 406
TED NAM-PP-375 35
TED-PTll-BL-9008, R-1 301
Til 8-40000-8 360
TOI-58-8 462
TPRC-U 479
TKBC-60-19 S61
'nBC-*o-a6 60S
XRK -60-39 15*
TREC -60-40 17«
TREC-60-43 711
TREC-60-S6 605
TREC -60-56 417
Tl(BC-60-S9 7U
TlBC-60-64 S64
TRBC -60-65 564
TRBC -60-67 711
TllEC-60-66 752
TREC-61-2 750
TREC-61-S 709
TREC-61-7 709
TRO-121-SR-2 336
TRG-127-SR-2 1»
TRC-131-SR-2 305
TSR-112 73
TX-2 dta^y »y«eni 190
UCLA De-59-34 712
UCLA De-5»-75 159
UCLA □e-60-15 163
UCLA DB-60-25 1»9
UCLA 06-60-35 7J0
UCLA DB-60-S7 7!9
UCLA DB-60-42 SM
UCLA De-60-46 425
UCLA De-60-47 466
tXXA 06-60-50 662
UCLA De-60-51 6 JO
UCLA 06-60-51 764
UCLA 06-60-94 626
UCLA-TE-60-1* 163
UMN CR-25 3M
IJM< CR-26 3M
UM4 CR-27 299
{Mm cn-» 393
UMN CR-32 534
\Mmi-9M7t-lP 552
UMH-0«7t-2-P 409
UMH-OaOOO 59«
UMa-03105 806
UMR1-03106-2-T
UMR1-03113-6-P
UMJU -03114
UMRI
UMKI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
UMRI
•<»S54-1-S
0SS97-1-T
03597 -2-T
Ja6S-l-P
2096
2406
2504
B97
a»i6-i7-p
2712
2750-9-T
2755
•2712-1-P
27»4-6-T
2794-7-T
■2M0-4-T
2iaO-5-F
2BS4-8-P
jr73-5-P
'2M6-1-T
•2900- 57 -T
2900-126-R
2900-129-R
M6
tab
96
ao6
M6
300
723
723
39
476
369
232
625
Number P—e
UMRI-29to-l34-T 413
UMRl-2S»-202-T 308
UMRI-2913-3-T 596
UBCEC !»-2l6 210
UBCEC-!i-217 l»7
UBCEC ! 6-218 lt2
UBCEC -: 1-101 13D
UBCEC-n-202 117
UBCEC-: 9-201 117
UBCEC-: 9-202 «4
U8CEC-1 3-201 607
UBCEC -I -73-201 327
UBNRIX.[aD-12«C) 277
U5NRDL|tR-62 274
U5NRDLiTR-102 f'S*
UBNROLm-111 fS4
U5NRDLfTR-127 ' JOB
UBNRDLrTR-152 335
UBNRDLrTR-277 335
UENROLfTR-289 335
U8NRDLtTR-36l 102
UBNRDLfTR-364 102
USNRDLfTR-369 785
UBNRDLrTR-3a0 303
USNRDL>TR-38S TU
UBNRDL>^TR-396 381
UBNRDLtTR-399 f»
U5NROLrTR-406 SB
UBNRDCfTR-40» 7«3
UBNRDLfTR-418 StS
USNRDLl-TR-419 319
U5NRDL»TR-421 373
USRL Rll-52 302
UTIA TT -22 194
UW ER- tl3-10 m
VAC R- 58 S64
VAC R- 97 964
VAC R- 04 %4
Vitro- 23 11-2-59 741
VRC-5 , 419
WADC-lN-5«-ir7 3M
WADC-lN-57-287 769
WAOC IN -58- 163 37
WADC-lN-58-256 785
WADC 1^-58-259.
102
si^jeraeded 195
WADC -IM -59- 1
WADC lN-59-42
WADC-lM-59-142
WADC-1 M-59-243.
-59-357
-52-2
-52-184.
Pi. 1.
WADC lN-59-326
WADC-1 M -59- 351
WADC-1 M-
WADC-TR-
WADC-1R-
WADC-TR-54-581
WADC TR-54-587
55-29. pt. J
55-29. pi. S
55-410
56-51. pt. 4
5651. pi. 5
56-585. pi. 2
-57-240. pC. 2.
led
57-374, pt. 5
WADC -fl- 57-622
tR-57-623
WADC tR-5«-95, pt. 3
WADC
:f5:3
WADC
WAOC
WAOC
WADC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WAOC
WADC
<76. », I
■1R-58-478. pi. 2
-1R-5a-S62. pi. 2
-1R-58-604
■1R-58-669
•1 11-58-673
■1R-59-29, pi. 2
■1R-59-36
-1R-59-63. pt. 2
•11-59-130
•TR-59-189<l)
m-59-237
-1 R-59-316
-1 11-59-337
-1 R-59-366
■1 R-59-379
■1 H-59-416.
-1 11-59-432.
■1R-59-448
-111-59 526
ft-
p(. 2
460
160
964
770
135
69
261
91
7r
748
570
469
434
157
592
93
179
991
339
Wi«nl»r
WADtf TR 59-547
WADC TR 59-570
WADC TR-59-619
WADC TR-59-736.
WADC-TR-59-742
WADC-TR-59-744,
WADC-TR-59-747
WADC TR-59-772
WADOTN-58-300,
W ADO- TN -59-344
WADD TN-60-1
W ADD- TN -60-36
W ADD- TN -60-66
WACO-TN -60-71
WADO TN-60-75
WADO TN -60-76
WADD TN -60-83
WADO TN -60-88
WADO TN -60-89
WADO TN-60-104
WADO TN -60- 108
WADO TN-60-1 15
WADO TN-60-123
WADO TN-60-136
WADO TN-60-137
WADO TN-60-140
WADD TN -60- 145
WADO TN-60-155
WAOO TN-60-161
WADO TN-60-165
WADO TN-60-183
WADD TN-60-197
WADO TN-60-aOO
WADO TN-6O-210
WADO TN-60-212
WAOO TN-60-213
WAOO TN -60-217
WADO TN-60-230
WADO TN-60-243
WAOO TN-60-244
WADO TN-60-260
WADO TN-60-261
WADO TN-60-28I
WAOO TR-59-326
WADO TR-59-469
WAOO TR-59-486.
WADO TR-59-708.
WADO TR-59-708.
WADO TR-59-728
WADD TR-59-743.
book 1
WADO TR-59-743,
book 2
WADO TR-59-743.
book 3
WADO TR-59-743.
pu. A-Cl
WADO TR:60-S6.
WADO TR -60-56,
WAOO TR -60-56.
WADD TR-60-*
WADO TR-60-7
WAOO TR-60-S1
WAOO TR-60-33
WAOO TR-60-41
WADO TR -60-42
WADO TR^O-43
WADO TR -60-46
WADO TR -60-53
WAOO TR-60-57
WADO TR-60-74,
WADD TR-60-74.
WADO TR -60-76
WADO TR-60-77
WADO TR -60-80
WADO TR-60-106
WADO TR-60-111
WADO TR-60-116
WADO TR -60-118
WADO TR-60-119
WACto TR-60-120
WAOO
WAOO
WADO
WADO
WAOO
WAOO
WADO
WADO
WAOD
WAOO
WAOD
WADO
TR -60-124
TR-60-132
TR -60-143
TR -60-150
TR-60-157
TR-60-161.
TR-60-162
TR-«0-174
TR-60-184
TR -60-188
TR-60-196
TR -60-198
P«ie Numfier P«ie
627 WADO TR -60- 199 M
345 WAOO TR-60 204 Mi
635 WADO TR-60 216 • IM
pt. 2 71 WAOO TR-60- 230 MV
726 WAOO TR-60- 233 • •
V. 4 445 WAOO TR-60- 234 419
330 WADO TR-60- 240 • W
335 WADO TR-60 244 4i
pt. 2 457 WADO TR 60-249 M
710 WAOO TR 60-252 M
608 WADD TK-60-r3 •
478 WADO TR-60-r5 4H
438 WADO TR-60- 260 1#
175 WAOO TR-60- 263 |B \
46 WAOO TR-60- 278 JM '
770 WADO TR-60 286 #
5 WADO TR-60- 293 , fli
39 WADO TR-60- 294 . I U
76 WADO TR-60- 295 Mil
147 WADO TR-60-303. pi. 1 474
197 WADO TR-60-304 , 754
25 WAOO TR 60 308 ' 83
425 WADD TR 60-309 M
265 WAOO TR 60-310 4W
362 WADO TR-60-312 8M
134 WAOO TR-60- 3 16 1*»
206 WADO TR-60- 329 195
341 WAOO TR-60- 333 375
30S WAOO TR-60- 138 44t
324 WAOO TR-60- 340 4M
287 WADO TR-60- 343 4tf i
329 WADO TR-60- 344 7»1
37 WADO TR-60- 352 73
137 WADO TR-60- 357 806
264 WADO TR-60- 360 SS
261 WADO TR-60-364 463
262 WADO TR-60-365 l»7
102 WADO TR-60- 372 418
575 WAOO TR-60-373 SPt
601 WAOO TR-60- 376 21
393 WADO TR-60- 377 446
393 WADO TR-60- 384 381
783 WAOO TR-60- 385 UO
102 WADO TR-60- 387 469
342 WAOO TR-60-388 19
p, 4 115 WADO TR-60-390 4*4
C' 1 293 WADO TR-60 393 418
nt 2 286 WAOO TR-60 395 143
5 WADO TR 60-412 173
, I WADO TR-60-415 408
726 WAOO TR-60-419 4il
, 1 WADO TR-60-425 4»
726 WADO TR-60-426 H
, 1 WADO TR-60- 427 754
726 WAOO TR-60-433 , 708
, 2 WADO TR-60-443 4iO
726 WADO TR-60-445 336
B, 1 801 WADO TR-60- 451 775
m' 2 802 WADO TR-60-461 315
«■ 3 J02 WADO TR-60-463. pi. 1 445
311 WADO TR-60- 468 197
161 WADO TR-60- 469 133
201 WAOD TR-60- 471 429
96 WAOO TR-60-473 70
147 WAOO TR-60-476 143
95 WADO TR-60- 484, pi. 1 454
S63 WADO TR-60- 489 610
159 WADO TR-60- 493 6
470 WADO TR-60-507 422
7S6 WADO TR-6O-510 448
- 1 94 WADO TR-60-5U. pt. 1 314
«■ 2 94 WADO TR-60-521 353
137 WADO TR-60-522a) 4«»
538 WADO TR-60-523 614
537 WAOO TR-60-534 796
36 WADO TR-60- 542 614
212 WADO TR-60-543 553
93 -WAOO TR-60- 544 277
258 WADO TR-60- 552 562
159 WADO TR-60- 553 586
92 WADO TR-60-558 436
WAOO TR-60-562 617
179 WADO TR-60-563 617
447 WADO TR-565 571
447 WAOO TR-60-568 619
73 WAOO TR-60- 584 589
69 WADO TR-60-590 711
pt. 1 711 WADO TR-60-596 688
397 WAOO TR -60-600 765
175 WADO TR-60-601 682
461 WADO TR-60-604 273
38 WADO TR-60-617 690
539 WADO TR -60-6 19 139
74 WADO TR-60-621 269
24
WAOD TR -60-633
688
WAOO TR -60-636
542
WADO TR -60-637
269
WADO TR -60-643. v. 1
584
WAOO TR -60-643. v. 2
585
WADO TR -60-660
688
WADO TR -60-661
318
WADO TR -60-662
691
WADO TR-60-668
551
WADO TR -60-669
561
WADD TR -60-673
363
WADO TR -60-674
718
WADO TR-60-678
601
WADO TR -60-687
589
WADO TR -60-691
568
WADO TR -60-701
575
WADO TR-60- 745
685
WAOO TR -60-748
682
WAL 112/83-17
221
WAL- 119/1
91
WAL 130.5/1
91
WAL 140.5/1
309
NuBbn-
%/
WAL 143/14-50
M
WAL -16 1.85/1
•t
WAL-311/45
wr
WAL-397/10
nf
WAL-401.54/1
"m
WAL-401/79-31
•M
WAL -648. 4/1
8K
WAL-711.2/1
Wf
WAL-732/114-1
■ 2#''
WAL-732/114-3
'i
WAL-732/114-5
. 1 tS
WAL-732/114-7
, '*
WAL -732/1 23
1 7a
WAL-80a/19-5
147
WAL 830. 5/1
IS
WAL-834.21/2 •
"1
WAL 893.3/3
. 81
wc-aiio U
712
WC D-122a»-(l-4)
712
WDL TR-1164
171 ••
WHOI Rrf. 59-54
34
WHO! Ref. 59-58
80
Number
WHO! Ref-59-59
90
WHOI Ref. 59-63
281
WHOI Re(-60-3
33
WHOI Ref. 60-10
414
WHOI Ref -60- »
413
WHOI Ref-60-40
414
WII-4/59
557
WIS -86: 2439
122
WR-473
43
WR-505
568
WR-53S^
569
WRL 403FO449-R7
172
WSU RR-1
940
WT(BU)33
194
WT(BU)34
605
WU Ref. 58-32
33
WU Ref. 59-*
383
WU Ref -59- 28
33
WVT RI-5904-
777
WVT RI -6001^1
749
WVT RK-6010
462
ZTB-131
8ttv
r*"'
-t'
■I-, ■
• i
-J
\^.
SUBJEa INDEX
f;
\-
1
V
&if.]ect
Pace
n Number
Subtect
_,
USt
PB Number
Subject
P-|«
n Number
*09A vehicle*
419
152 716
Adrenal cortical extract
AlrbUat
Abellan groupi
•
--Phyaiological effecta
14
'147 744
--Measurement
306
149 633
- -Theory
77
152 067
Adrenolytic drugs
--Shieldii^
58
150 454
318
152 606
--Physiological effecta
15
150 569
Air conditioning equipment
AbUiiOB
131
152 212
Aerial cameras
(Alibome)
194
148 720
--Applicationa
707
153 915
-Dealgn
735
171 257
AbUilon materlala
39
171 0S4
--Development
561
171 506
Air drop operadona
157
171 147
Aerial gunnery
. 't
--Equipment
68
150 631
HB
153 568
-Training devices
436
171 419
Air force equlpmeM
757
154 719
Aenal phoiographa
-^Schadulli«
162
153 067
Ablative coatlnga
422
171 416
-Alaaka
441
153 540
Air force reaearch
633
153 499
Abaorpclon
544
155 732
-Analyaia ,
683
150 916
Air intake fillers
^ -Thpoiy
4M
153 657
--Proceaalnf'
752
155 438
--Teat reaulta
744
154 674
Acceleration
Aerial photography
Air intelligence
-■Mathematical analyaia
710
153 695
--Antarctic regions
349
152 987
153
152 OlS
--Meaaurement
726
155 567
--Applicationa
707
153 915
Air reactiona
4SS
171 387
--Phyaiologlcal eflecta
14
150 440
--Military requirements
153
152 303
171 388
269
171 304
--Theoretical correctiona
478
171 385
Air traffic
171 343
Aerial reconnaiaaance
121
152 146
-Scheduling
39
171040
39«
171 367
-AUaka
411
153 371
Air traffic coiurol systems
- -Teatliv equipment
36
148 274
- - Effecti veneas
153
152 303
-Coding
39
m040
172
171 134
427
153 396
170
171 130
Acceleration tolerance
-Psychological (actora
263
153'387
"
171 131
- -Phyaiological effecta
399
147 778
-Visual factors
561
171 506
171 132
- -Phyaiological (actora
13
150 442
Aenal targeta
430
171 368
--Teatlng equipment
710
153 695
--Drag
709
153 861
- - Bqulptnent
41
171095
748
153 604
Aerial warfare
566
171509
Aeceleratora
--Bibliography
263
153 387
566
171504
--Performance
178
152
622
334
152 821
171 508
Accelerometera
Aerobee
35
150 873
--Human engineering
417
150 920
--Applicationa
SM
153
449
Aerobee Hi
52
150 931
561
171 510
-■Errora
4S7
152
917
169
148 717
--Test reaults
157
148 708
- -Senaitivity
5(2
154 424
Aerodynamic coefflcienta
454
171 407
Air traffic conirollera
Acecala
Aerodynamic data
--Performance
561
171 510
--DecompoaitkM '
700
153
911
- - Reduction
325
152 B43
Airbreathlng combuation
550
153 448
Aceutea
- -Tablea
326
152 479
Aircraft
- -Meuboliam
141
152
531
Aerodynamic heating
85
150 621
--Aerodynamic
400
153
526
194
148 701
character! atica
I9S
171 135
,
153
577
148 702
455
171 387
^•
153
528
^
327
152 557
171 388
' ■
153
529
m
454
149 676
--Control ayatema
160
152 230
153
530
558
153 569
--Detection
565
171509
•
401
153
531
634
153 103
r-
710
154 744
153
532
711
153 668
7S3
153 900
153
533
- -Countermeaaurea
157
171 147
- - Equipment
102
171 119
153
534
.
160
153 257
--Heat transfer
7<*
154 215-1
X
153
538
194
148 720
154 215-2
153
539
438
171 363
--Ice formation
279
152 977
403
153
363
474
153 105
286
153 630
«»
153
364
60S
153 568
--Inspection
100
152 399
153
525
773
153 693
--Laadiiv
708
161 914
Acetone
--Measurement
439
152 829
161 915
--CJiemical reacttona
410
153
157
--Phyaical effecta
454
171407
--Maintenance
an
153 547
j- -Determination
Acetyl bromide
694
154
210
-Theory
606
150 636
709
171 614
769
154 215-1
-Materlala
93
151096
--Microwave apectra
791
148
563
154 215-2
M7
171 328
Achievement teata
(
- -Thermal effecta
«0B
152 582
4SB
153 929
--Developme«
394
148 771
Aerodynamic ndae
86
148 689
161 229
- Reliability
13>
147 642
Aerodynamica
740
155 296
499
171 411
ACM-S2 mapper
4i
150 594
--Mathematical analyaia
800
155 323
610
161 231
AGOE
173
171 137
--Study and teaching
771
149 778
779
151 104
Acouatic impedance
--Theory
454
171 415
--Safety meaaurea '
38
148 870
-Mathematical analyaia
206
147 9M
Aeroelaatic interaction
285
171 192
—Sandwich construction
710
154 955
1
149^298
150^833
Aeroelaatic reaponae
454
171 407
--Simulation
418
171 404
J
A«Mloglcal sonde
281
152 541
-Stability
1«S
171 13S
•-Meaaurement
tt7
14»219
Aeroaols
IBS
171 192
Acouatic materlala
- - Absorption
ft20
153 450
-Stresses
708
155 090
--Development
178
150 392
--Scattering
39
150 663
Acouatic nenre
Aeroapace
272
171 029
characteriatica
285
171 192
--Surgery
139
152 766
Aerospace life auppon
441
171 418
-Take-ofl .
--Vlslb411ty ^
286
153 630
Atxuattc propertlea
Aerotheniiochemi at ry
550
153 448
752
153 900
--Teat methods
787
155 382
Afterglow temperature
622
153 807
Aircraft caMna
Agard 8
325
V52 556
-Coolli«
735
171 257
--Mathematical analyaia
192
149 627
Air
Aircraft equipment
Acouatlca
-Bibliography
744
tri-S SB-
->- Design
560
153 933
--AppUcatlona
336
149 682
448
--Effects of radiation
709 .
154 53S
AcryUcea
--Contaminatlan-
176
152 064
Aircraft finiahea
--Syntheala
695
15q730
-Cooling
736
154 626
--Bffectiveneaa
752
153 900
Acrylic reams
-Heating
195
149 672
Aircraft fires
--Applicationa
443
153
286
--Purlflcatioo
309
171 046
- -Countermeaaurea <
562
171552
--Solvent extraction
316
149
963
171 061
--Detection
38
171038
--Temperature factora
316
149
8S0
744
OTS SB-
Aircraft materlala
ACTH
]
448
-Patlfue
461
171 410
--Secretion
140
150
»66
- Radiation < >
117
150 955
Aircraft steels
92
171 077
Adaltne
806
150
227
454
149 676
Aircraft tlrea
^
Adapter unita
427
153
950
-Radioactivity
22
161 371-8
--Teat reaulta
158
152 494
Adaptive si'ltchlng circull
806
150
227
404
161 371-10
Airfolla
Addition compounda
472
153
310
692
161 371-11
- - Aertxlynamlc
Adhealvea
639
161 371-12
characteriatica
•05
153463
--Stre«aea
192
148
298
- -Spectrographic analyaia
117
150 955
27
!"' I
nNumber
AlrfoUa (COB. )
Alkyl halidea
-•U*
710
159 146
--Sound iranamlaalon
MMlwnMhril ■nilrtlr
773
153 692
Alkyl radlcala
--ModritMl rawiUa
335
152 556
-OMmlcal reactlona
daracienatica
336
153 479
Alkataa
-Ftiyaiologlcal effecta
--Theory
IS
150 630
Alloya
--TiaMonlc dMracterlwlcs
606
153 644
- -Corroalon
AlifnuiMa
--Cryaul atructure
■•Durtiaqmem
157
153 343
--Deformation
385
153 967
-•Difrualoa
--MaterUls
93
171 077
--PoTflnf
179
171 148
--Heat tranafer
199
151 072-H
-Meiallurglcal effecta ^
330
161 313
--Fliaae atudlaa
563
171539
--Scraaaea
779
153 753
^
710
153 750
'
153 751
--Tem^rature ttctora
- -Tera^ranire tect^
159
171 151
AiYplMW MgtM oUa
- -Teatlng equipment
Alrpteelaadliv*
593
154 969
--Thermodynamic
prcpertlea
--BquipmcM
38
153 350
--USSR
ISS
153 384
Alpka countera 1
--MMMcxslofflcal esctors
709
154 743
--DavalopmcM
■ -Sudatlcal ualrsls
416
171 370
Akarnatlng cuiiat
Alrpianc notae
--Detection
--AMlysia
140
153 363
AWmetera
- -Meaaureineni
37
171 076
--Applicatlooa
Airplane panela
••Dealgn
- -Sandwich cca«nict)aa
386
149 718
Altracor
.(
418
171408
Atamlnum
- -SuptiTKmic \
--AppUcatlona
daracteiiatlca
38*
171 199
-•BUai effecta
--Vibration
38
171090
--Cryatal atructure
711
171594
--Deformation
Alrplanea
- -Ooniroi ayatema
159
153 786
—Heat treatment
5*3
171591
--Intamal friction
- -Da- Icing ayatama
68
150 876
• -Shear atreaaea
- -Lai«laidliial atafeilliy
563
171 551
-•Sireaaea
Alrpon comrol ta«f«ra
-Daaiap
417
150 930
--Temperature tactore
Aliyona
--Llgkilnc ayatema
562
171 507
AUanlaun alloya
Alaakan Indian
366
153 338
--Caadnt
Alrrkola
.
--Oct Iral eOecta
276
152 746
--Corroaloa j
--Dafcydratloa
34
150 538
--Sartttca laiwlri
277
150 619
•-Creep '
AlfM
--Bxtruaion
--flqialcBlaftecta
554
153 735
Al«ri»a
76
148 063
, --Patlgue
595
153 664
--Fracture
--AppUcailona
313
153 447
--Mecharacal propertlee
r
574
153 663
-Thaory
186
153 441
--Metallurgy
317
153 675
--Sireaaea
318
153(07
--Temperature tmctmu
333
149 649
449
153 306
153 308
Alumlnuqi - ca rlion - i roi
4S0
153 458
aUoya :
596
153 678
--Mechanical propertlee
Aluminum caatloga
- -naac atudlea
410
147 045
- -Mechanical properUea
Alkali maul halkle cryatala
Alum inum - ch roml um -
- -Cryatal airuciun
313
153 427
titanium alloya
- -Laialanaranra
313
153 451
-•niaae atudlea
638
153 670
AhanlDum cryatal a
-nwocondualrlty
473
153 143
--Creep
• -PrOpSTtlAS
471
171 371
- - Deformatlao
--^^^■rt^
471
171 371
Alfcait aMHl halldea
Aluminum hjKlrldea
--Spactra
553
153 613
- -Bibllofraphy
Alkali mecala
Aluminum -Iron alloya
--Atomic atructura
316
148 733
--Development
- -Hbtiagrapiiy
33
OTS SB-4
11 Alumlaum-mafnealum
--Spectra
468
153 136
aUoya
Alkaline batterlea
--Deformation
--Oeaifc
45
153 187
--Fatigue
304
149 693
Aluminum - mot ybdenum -
45
153 187
titanium alloya
Alkaline cella
--Mechanical propertlea
- -Oealfn
55
150 449
Aluminum cnilde fllma
--Preparation
--«Ui««raphy
33
cirr5a-4
3 Aluminum osidaa
AlkaUaa earth halldee
- -Chemical effecta
--■ondliv
411
153 314
--Chemical reactlona
Aikallne earth metala
-•Magnetic propenlea
- -BIMlo(raphy
23
CrTSSi-4
2 --Mechanical propenlea
Alkalcada
Aluminum -titanium-
- -Symheata
30
153 096
vanadium alloya
--niaae atudlea
•' I
Subject
Page Ft Number
791 153 082
697 154 564
546
153 152
458 •
339
99
39
149
86
565
441
314
79S
614
739
795
613
91
90
768
47a
614
330
613
615
781
197
749
300
460
287
330
329
287
300
ar
778
777
Aluminum -titanium -
vanadium alloya (coo. )
- -Temperaiur»f8ctora
Aluma
■-Cryatal atructure
Amldea
-Hydrolyala
Page PB Number
461
IV 103
Aminea
312
190 596
- -Chemical reactlona
462
161 896
199
148 675
--Determination
776
161 336
-Mo^bcular atructure
801
154 868
- -OaldBiton
776
154 453
828
171 113
--Tcalc eflecu
301
153 169
461
151 103
Amino adda ,
463
161 896
-Biochemical effecta
vtn
171 348
Ammetera
-Calibrator
Ammlno coni^kuida
610
330
161 231
171 348
153 939
171 331
150 473
152 132
152 042
152 312
154 296
171 418
171 047
148 516
171 488
171 686
148 516
154 867
161 989
152 170
154 958
171 360
171 488
-W2 463
161 770
150 502
153 581
171 152
171 568-1
171 568-2
152 785
153 167
171 338
153 463
149 655
171 328
2 785
171 338
161 331
153 673
171 564
199 171 154
470
201
639
171 360
171 150
148 559
553
171 534
610
161 333
460
610
171 399
153 398
610
171546
434
171 364
173
408
795
70
149 670
171 373
154 063
171 074
--Appltcatlona
--Thermal propenlea
Ammoala
--Applicationa
--Spectra
Ammonium carbonate
- -Hydrolyala
Ammonium lona
- - Exchange reactlona
-SoluMlity
Ammonium perchlorate
--Combueiion
Amphibian planea
-Control ayatema
Amphlbtoua operationa
- - Equipment
Amphlbtoua vehidca
--Dealgn
Ampllftera
-Applicationa
- -Circulta
--Dealgn
Amplitude modulation
--Analyala
• -Mathematical analyala
--Maaauremeiu
AN/APD-4
AN/ASC-15-TI
AN/DPN-3I(XE-I)
AN/PPS-3
AN/CGA-2(XW-1)
AN/GPM-IS
ANA3PX-20
AN/C»C:27
AN/aSQ-l6(XW-l)
AN/MRC-71
AN/PPN-l3(XE-»
AN/PRM-IO
AN/PRM-14
ANAlRM-26
ANAJKM-2e«
ANAJIlM-37
Analyala of variance
Analytic functioiui
• -Determination
•-Thaory
199 171 194
610
111
409
697
144
276
149
275
14S
m
17
290
407
148
164
3
141
149
553
71
179
180
36
714
717
749
746
313
581
303
335
633
S3
727
764
436
572
577
732
300
434
732
577
732
451
452
7tS
766
421
350
575
424
296
434
424
739
318
596
760
633
184
186
323
449
576
594
S9o
161 331
150 541
luiOM I
153 451
154 157
149 065
152 746
148 976
153 085
152 47*
153 845
150 471
171 310
171 138
152 091
149 703
152 054
152 247
148 678
153 811
152 027
148 698
148 699
152 296
154 614
154 633
154 616
154 649
152 940
171 483
153 576
153 577
152 843
154 843
171 059
154 589
150 909
171 419
154 418
154 844
155 151
155 152
148 282
171 344
155 151
155 153
154 516
155 151
155 153
150 086-7
150 086-8
150 08t-9
150 086-1
150 086-3
150 086-3
150 086-4
' 150 086-5
150 086*
153 998
152 993
153 595
171 343
152 992
171 346
171 346
154 680
171 334
153 678
148 212
153 872
148 978
153 374
149 649
153 306
153 107
153 689
153 200
Analytic apacea
Anatomical modela
-Analyala
Anchora
- -Teat reeulla
Anecboic chambera
--Acouatic propenlea
Anemometera
- -Senaltivlty •
Aneaihetlca
- -Fhyalologlcal effecta
Anlmala
^ge n Number
322 149 *49
--Paraallea
Anlaol ropy
Aimthllation reactlona
--Analyala
--Theory
Anodea (Blectrdytlc call)
- -Coatlnga
Anonhoalte
Anoala
--Phyalological effecta
Antenna maata
--Development
Antenna radiation panema
--Analyala
--Determlaatlon
--Mathematical analyala
- Mea au rcment
-Polarization
-Siatlatlcal analyala
-Syntheala
--Theory
Anteniiaa
- -Bibliography
--Control ayatema
-Development
--Focuaing
•-Impedance
"MaierUla
--Mathematical analyala
-- Reflect ora
--Theory
- -Torque
Anthracene cryaula
--Lumlneeccnce
Anthropological data ,
AmlMotlca
--Bffectiveneaa
Antibodiea
--Adaorptlon
--Biochemical effecta
--Ptiyalological effecta
Anticorroalve palnia
- -Teet reauha
Anttferroelectriclty
Antlferromagnet I am
Antlflbnllailon
15
746
787
IM
IS
403
441
403
629
618
98
464
463
149
753
397
399
542
43
725
10*
49
299
306
431
162
168
288
429
166
41
166
219
298
72*^
43
56
122
80*
439
719
53
1*1
162
168
306
430
439
434
435
579
730
736
579
718
789
166
301
171
395
49
56
106
431
617
536
543
16
549
314
591
344
795
545
152 118
154 663
155 383
IM677
1^315
153 518
153 540
153 518
153 563
194 817
190 SSI
190 694
190 693
149 066
194 636
171 393
153 409
154 099
739 1S4 681
190 993
199 864
193 676
148 368
150 393
153 949
153 776
193 334
193 990
161 979
192 738
153 69*
148 739
190 740
148 397
153 343
153 841
194 595
194 596
150 648
152*14
152 039
154 071
152 719
193 994
146 395
149 069
148 709
161 979
192 201
199 713
1$3 7I9
193 239
193 342
193 243
153 3f<
199 719
193 864
193 097
190 901
154 078
148 729
152 833
152 219
152 861
148 368
152 614
152 077
150 319
171 490
153 489
403 193 192
148 931
190 441
193 640
192 862
190 899
192 932
194 062
193 370
Sublact
Anilfouling coatlnga
--Chemical analyala
--Teat reaulta
I
Antifriction bearinga
Antimony chlondea
--Cryatal atructure
Antiorgan aerum
-Biochemical effecta
Antlperaonnel weapona
--Bffectiveneaa
Antlprotona
--Nuclear reactlona
Antltrlgonometrlc functiona
Aperture fielda *
Applied mathetnatics
--Theory
Applied paychology
Approach lighta
--Vlalbillty
Appradmate computation
Page PB Number
--Appltcatlona /
--Biiore *
--Theory
Aptitude teata
--Applicationa
--Bffectiveneaa
--Sundarda
--Statiatlcal analyala
Aquatic anlmala
--Biochemiatry
-•Nutrition
Arctic regiona
- -Meteorology
--Phyalological effecta
Arctic aleda
--Dealgn
Area auction
--Teet reaulta
Argon
•-lonixatlon
--Biyalcal factora
--Spectrographlc analyala
Argon (Liquid)- -
Solvent propertlee
Armor plate
--Teat methoda
Airmored vehiclea
--Human engineering
--VIbrailor
Arreating hook
Artarlea
--Pathology
Artificial demuree
--Analyala
AnlflcUl kidney
--Applicationa
Aniflcial llghtnli^
waveform
Artificial Umbe
--Control ayatema
Artificial re^railon
- - Equipment
Aatla deecriptora
Aatronautlca
--Theory
Aatronomlcal cameraa
--Dealgn
39
74
199
473
691
271
98
463
464
449
43
46S
761
2*2
709
77
184
189
319
330
333
761
496
630
634
595
79
993
99w
134
135
361
363
363
137
686
703
383
413
367
313
88
606
410
408
338
39
309
398
307
709
19
690
403
804
683
19
807
190 769
190 768
190 770
190 771
190 773
190 773
190 774
190 779
171 191
193 310
148 419
193 999
150 351
150 693
150 694
153 754
190 6a
194 391
190 994
193 797
-194 743
150 641
148 707
153 373
153 373
153 375
149 730
152 894
193 279
147 904
193 104
193 490
153 103
193 415
152 292
153 806
148 006
152 798
148 293
152 626
153 572
152 756
152 272
148 006
148 079
152 907
150 723
153 352
152 942
150 368
152 895
153 35*
149 731
152 664
150 461
193 063
193 469
132 815
161'919
190Si63
19^363
193 193
194 2^3
149^
190 788
I7t9l9
X
Subject
Aatronomlcal data
• - Recording devicea
--Tablea
AacrtntMny
- -InatrumeiKation
Aatrophyaica
- -Blbllograpby
Aaymmetrlcal force Helda
Atmoaphere
--Abaorptlve propertlea
•-Analyala
--Arctic reglaaa
--Attenuation
--Bibliography
--Boundary layer
--Chemical analyala
--Chemical reactlona
- -Contamination
--Denalty
-- Elect romagttetic effecta
--Electromagnetic
propenlea
-Heat tranafer
-Light iranamlaalon
--Mathematical analyala
--Meteorology
--Motature conteat
Page PB Number
-Northern hfemlaphere
-Optical propenlea
•niyalologlcal effecu
-Preaaure
-Radiation
•RadtoactlTlty
-Reflective effecu
-Sampling
-Spectrographlc analyala
-StabUlty
-Temperature ,
-Temperature factora
-Turbulence
--Wave tranamlaaloo
Atmoaphere modela
Atmoepheric electricity
--Meaauremeitt
--Meteorological effecu
Atmoepheric refractiona
--Meaauretitent
--Meteorological factora
--Theoretical correctlona
Atmoepheric aounding
- -Inatnimenutlcn
933
3
3
131
465
473
196
960
280
413
599
999
412
707
708
406
306
384
349
119
479
806
35
380
708
38
198
793
196
30
191
194
384
196
413
706
90
194
558
688
996
413
998
999
960
464
194
635
464
419 V.
999
159
380
706
199
999
7t7
476
706
801
104
30
330
383
199
635
95
au
439 153 065
333
478
533
148 399
153 588
150 333
S9»
Atmoapherica SW
-Analyala 221
--Electromagnetic effecta 331
--Recording devicea 156
--Theory 107
Atomic bomb axploaiona 334
--Haxarda 941
- -nyalcal effecta 708
Atomic docka 789
Atomic power planta
--Arctic regioaa 783
Atomic apectra 806
--Analyala 467
623
•-DBtermlnatloa 998
--Theory 691
190 923
190 938
190 940
193 903
161 960
194 397
190 317
193 643
139 063
150 723
154 068
153 081
153 497
194 963
194 199
190 690
153 383
153 623
149 740
150 507
>I50 718
161 589
148 395
153 063
153 064
154 596
193 390
193 384
154 530
153 249
150 930
153 327
149 061
190 618
153 349
150 733
154 275
150 930
153 553
153 566
171 600
153 608
153 634
133 969
153 635
150 896
171 361
171 363
153 553
161 588
171 361
171 963
150 697
■ 153 745
148 710
153 064
154 279
193 931
194 068
193 906
153 835
154 275
154 273
153 190
150 939
149 060
153 951
148 710
171 544
150 753
153 060
153 399
147 533
153 279
153 174
193 174
149 069
190 820
193 Kt
194 402
199 p90
193 716
190 908
194 C71
193 193
190 701
192 664
147 748
ftf/t t% hfc—fcCT
ical aaalyiis
I— ctltw
-Scanarlnc
-Plqrstolaclcal tectors
693
IW
112
216
399
631
278
108
339
634
101
634
136
264
396
153 903
150 945
161 368
141722
149 699
150 946
149 6ft9
150 945
149 699
193 237
150945
150 088
153 237
193 197
152 888
153 136
153 Ul
787 155 382
•r%yiihoia0cal tectors
--Sociolnttol tactors
--Sutlatical uMlysia
--Teat methoda
attenuator*
--OtUbiaticn
10
197
363
2tS
996
536
683
8
10
137
539
686
10
6
8
994
994
579
423
150 899
153 371
153 371
153 782
153 8*1
153 604
148 774
152 101
150 851
148 292
154 866
171 545
149 901
154 459
150 852
152 142
150<B61
153 287
153 2r7
153 238
171 227
171 338
Subtact
Audlotnetera
Paae .P
8 Number
Sublect
Page 1
V Manber
ATlatloo peraoonel (con. )
--Teat methoda
998
153 778
- -CUaaaiflcatlon
194
152 798
Audit
748
148 787
261
153 631
--iMteaaurement
Auditory percepclcn
- -Paychological (actora
199
396
152 766
171 403
"OoiblBf
. 1
262
102
.fin
*206 .
133 572
171 119
171 153
171 143
- -SuHatlcal analyala
684
154 063
619
171 493
--Taat methoda
136
ia728
-Bqulpment
102
171 119
Auditory aignala
--Mlliury requiremente
6
171 075
•-DmiCtU»
466
153 170
--Performance
262
153 506
Auditory direaholda
393 '
153 852
--Meaaureinent
Aurorae
140
3
147 529
150 941
--Selectloa
537
538
361
153 855
153 854
153 631
190 942
393
153 852
150 517
•-Taat methoda
134
150 790
-RcAactlveenacta
--Snahem bemiaphera
, 156
2
148 386
150 941
150 942
-Training
261
688
260
153 631
171 600
171 332
-Sliectra
132
152 281
- -Training derlcea
5
171 CS3
152 282
Aviation lafety
38
1,48 870
561
171 506
AuateiUte
--Deformatkia
780
154 553
Avoidance behavior
397
153 468
Autafrettage
Autornata
742
154 207
AxUl now compreaaora
223
149 673
--Performance
468
152 874,
334
171 399
AJtuUy aymmetrlc nam
601
171 548
--Analyai*
194
148 701
)
806
150 726
--LamliMf boundary laye
r 606
153 118
152 135
-ktothematlcal analyaU
769
155 144
Automated maintenance
Automatic pUota
173
171 137
--TaUea
772
457
153 848
152 838
--Deaifn
Automation
160
152 230
Azldea
476
152 876
- -Oiemlcal reacilona
695
148 938
8CB
153 806
W7
147 841
18
150 214
--Syntheaia
695
148 937
ATlatka acddenta
Azimuth
171 067
--Analyais
562
171 062
--Determtnation
39
38
148 870
Azo compounda
561
171 506
--Symbeala
697
154 157
•t
710
154 744
Arlatioo medicine J
- -lUitlofraphy J^
266
272
171 333
171 029
*
Aviatloo peraaaaet
393
153 853
a
_ ■
- -Aialii iT"—"T
536
153 489
,
-Actitudea
137
262
365
152 271
153 271
152 782
ZP-
Subiact
F>ge PB Wurabar
8-47
286
153 630
8-70
711
171599
BackwaiKwave amplUiera
•-Oevelopmem
56
171 CM
165
152 562
295
152 994
426-^
153 400
571
153 938
Backward wave oaclllatori
--Slgnal-io-na«aa ratio
- 43
150 817
Bacteria
--Culture
'2
148 '169
--Detection
f 271
153 368
--Muutioiia
■> 270
52 477
- -Phjraiology
687
148 966
Bacterial aeroaota
■ -Temperature (ictora .
Bahamaa circle
270
153 343
279
153 905
Balancea
-•CaUbratloo
336
171 303
■^
408
171 236
--Dealgn
694
153 163
Rail beani«a
- -Lubrication
159
171 151
- -Maieriala
90
71 060
■all llghtnii«
621
153 916
Balllatlc cameraa
--Appllcatlona
. 436
150 070
B^UIaiic dau
--Momographa
306
52 732
--niotagraphlc analyaia
436
50 070
--RatXMtUng device*
580
54 968 .
BaUlabca
740
55 296
- -Teat (acllltiea
173
152 495
Balloona
--Applicationa
37
52 315
434
53 235
Banacfa ipacea
186
52 440
Band-paaa flltera
-Dealgn •
430
50^92
--Developmem
167
48 984
Band Mructure
212
50 596
Bang-bang aywem
425
53 438
466
53 099
Banking
--Theory
638
48 198
50 469
Bargaining
807
52 114
Barium carbonate^
--Chemical i laJBuna
Barium chromatear-
471
46 934
--Blactrlcal fatior*
59
49 960
BtrtanoKldea
- -Magnetic prop^lea
1
754
755
55 340
55 341
55 242
Barium ilianaie cryaiala
- - Dtelect rlc 'propentea
795
50 915
--Electrical propertiea
69
52406
Barium tltanaie*
--Application*
562
54 424
--Chemical reactlona
471
46 924
--Dielectric propertlea
150 899
Barometera
- -Callbratloa
465
71 237
Barrier grid tufa*
43
52 092
568
53 809
569
48 656
Bate
- -Ultraaonlc propf rtlea
428
53 697
Banenea
-Applicatioaa j
298
49 736
■ -Conulnara
730
54 639
-Daaign
45
52 314
722
71 582
--DavelopmeM
164
49 703
- -Elect rodea
45
52 914
Banery chaiiera
--DevelopraaM
293
49 703
Bayea nilea
596
53 840
Baacfaea
- -Qvlbbaan laUnda
554
53 735
--Broalon
413
47 311
•-Geology
704
49 216
- -Maaaachuaett*
278
49 638
413
47 311
- -Stabtltzation -
713
54 632
Beam-aplltter
400
53 308
Beama
- -BUUiography
83
52 143
-Creep
161
71 149
--Daformatloa
161
71 149
602
48 812
797
50 063
Su^act
Beama (con. )
--Shear atresaaa
--Sireaae*
-Vibration
Bearing*
- -Corro*ian prevention
-Material*
Bed-load tianapon dat*
Page PB Number
S^ibtect
fage raNumbar
603
753
584
173
609
,689
<>.
: derivative*
--Riyaical propertie*
•-Spectra
Benzene*
--Photolyaia
Benzoic acids
--Temperature factor*
- -Thermodynamic
propertlea
Benzyne
Beryllium
- -Bibliography
--Caatlag
--Determination
--Fracture
--Haadnok*
--Mechanical propeniea
'-Meltii^
--MeuUurgy
- -Prcx:eaaing
--Surface propeniea
Beryllium alloy*
--Mech*nic*l propertie*
Beryllium compound*
•Production
Beryllium hydride*
--Syniheai*
Beeael functlona
--Applicationa
Betatrona
--Dealgn
- -Development
Bibliography
--Adjuunt General'a
omcc
--Aerial reconnalaaance
--Aerial warfare
--Aerodynamic dau
--Air
--Air Force peraonnel
requirement*
--Air polluiloa
••Alkali metala
--Alkaline earth metal*
--Aluminum hydride*
--Antenna*
- -Arnted Service* Tech
nical InforTnation Agency.
Arlington. V*.
--Atmoaphere
--Aviation medicine
--Beam*
- -BerylUum
--Caatlag realn*
--Cathode ray cubea
-•Ontrlfugea
'-Oiemlcal information
aearching
•-China
• •Oonatruction
• -Coolanu
- -Oorroalon
--Cycloldal propellera
-David Taylor Model
Baain. Waahington. D. C.
--Diamond Ordnance Fuze
Laba , Waahii^on. D C
- -tlocumetsation
--Electric battariea
--Electrolytic cella
--Electromagnetic wavea
--Bxploaive forming
--Bzptaalvea
31
314
552
408
o9o
409
200
613
619
200
779
66
93
96
459
712
613
65
66
93
553
77
83
633
567
622
393
263
334
455
744
6
744
23
23
552
429
265
272
83
200
316
50
168
391
479
681
1
533
615
64
293
479
731
61
119
120
444
60
154 766
154 620
153 501
171 111
153 014
154 339
155 486
152 446
152 611
152 612
153 765
154 465
152 611
152 377
152 378 ,
171 521
154 417
152 377
151 106
152 197
171 088
171 083
171 411
155 086
171 521
150 613-2
152 197
171 088
460 171 389
171 081
171 489
152 066
150 524
153 934
153 822
153 820
153 440
153 387
152 821
171 387
171 388
arSSB-448
171 075
OTSSB-448
OTS SB-421
GTS SB-422
171 534
152 719
!fi m
171 333
171 029
152 143
152 377
152 378
171 034
171 127
OnrS SB-431
154 409
161 586
OTSSB-442
171 106
06TSB-449
171 501
152 130
257 153 726
153 496
161 586
CrrSSB-447
171 114
190 507
152 051
171 379
150 747
Bibliography (con. )
--Ferroelectric materlala
- - Perroelectriclty
- -Perromagnetiam
--Field emiasion
- - Fluorine compound*
(Organic)
- - Foreat Producta Lab. ,
Madiaon. Wia.
- Gallium
- -Group dynamic*
- -Heat alnka
--Haat reaiatant alloya
--High impact metal
forming
--High apeed camera*
- -High temperature
metallurgy *
- -High temperature
reaearch
- -Human erwlnaeiing
- -HydrcfoUa
-ice*
--Iconoacopea '
- - Intermetalllc compounda
- -International Geo-
phy*tcal Year
- - Ion emiaaion
--Jet propulaion
--Job analyaia
--Liquid meala
--Llquld-aolid cyclone
--Low t^emperature
arch
208
208
189
208
106
756
710
94
7
135
417
777
--Machine tranalatiooa
- -Magnetohydrodynamlc
wave*
- -Maintenance
-Material*
- -Metal platea
--Metallurgy
- -Metalorganlc compounda
--Microwave
apectrtiacopy
-Miaallea
--Molten aalta
- -National Bureau of
Standarda, Waahington.
D. C
- -Nltrxigen fluortdea
- -OfHce of Naval Re-
aearch. Waahington.
D C
--Operation* reaearch
■<tpclca
- -OaciUaior*
--OBOoe
--Permafroat
--Photoelectric abutter*
- -Fhyaiological
psychology
- - Piezoelectric materiala
--Plaama (Phyaica)
--Powder metallurgy
--Power auppliea
--Precipitation
- -Protective cooatnictitn
- -Paychoacouatic*
-Radiation
--Radiation couiKer*
- - Radiation damage
- - Radio wavea
-Ridlobiolagy
--Reaaoning
- - Refractory materiala
--Remote control ayatema
--Reaiatora
--Rocket propulaion
--Rocket*
--Rubber mouiKa
-Salta
- -Sandwich coaatructlop-'
--Scientific repona
580
777
804
266
392
609
281
341
591
34
106
64
6
264
91
391
753
803
160
222
116
533
417
752
453
777
23
634
479
27
465
756
137
477
341
189
412
281
341
137
341
465
199
681
31
1
621
560
99
56
206
635
143
264
591
143
168
177
436
310
27
710
131
257
393
OTSSB-434
OTS SB -434
152 213
OTSSl-434
161 576
171 252
154 955
152 151
150 498
,150 500
i71 372
CrrsS8-452
171 379
154 968
OTSSB-452
OTSS8-453
171 333
153 547
171 502
171 190
149 643
154 846
150 417
161 576
152 153
171 075
153 110
OTSSB-424
154 409
0TSSB^451
171 620
OTSSB-439
OTSSB-439
0T&SB-436
171 518
171 372
171 612
171 374
GrrSSB-452
arrssB-454
171 097
154 113
152 978
OTSSB-43S
161 560
171 252
116 303-S6
152 914
149 643
152 213
153 437
171 190
149 643
116 303-S6
149 643
161560
OrrsSB-423
171 6*9
150 617
171 106
147 766
150 896
171 124
149 713
149 714
161 581
152 349
153 110
154 846
153 069
OTSSB-429
171 184
153 182
153 793
0TSS8-425
154 965
148 703
153 726
153 440
Pl^» nttambUT
-ThsnnoelM^rtcliy
-Thermopiles
-Trailers
-Ti«liriB|
-Traaaducer*
- -Tr— iwors
--UBderMiier ■wtmmlif
--VIgUMKa
- -Voice cownwiretloo
contecture
cKm
Uteraioriea
t ymlmiNlty
■Magical vartere
Moloflcal wartare afenu
(ruroentatloi
Mrds
--Mifncdc pTopertlee
■taoHHh slloy*
--Thermel propertlce
■tamad) contpounde
- -Crystal airucture
■lanNdi oKldaa
- -Gonductlvtey
Hsmudi Milfidea
- -Conductivn y
Mnanloous costings
--OaiarioTaiioo
glackgian boards
■ackbody radUilon
--AkaorpUon
--Souroee
-Materials
■Uatefiects
- -CouMermessures
r (con. )
"gasattfic reports (cob. )
-Sclsarlflc reaesrdi
-aaiMiastitlon
iiaedlclae
-apace percaptlaa
aagUMerlog
-Tharailonlc emlsaion
-TkanBtacors
- -Steiulatloa
iUai tubes
■tlmlnesa
' -Ssfety devices
Mood
- -Ooagiiiackxi
--tOsctsof radtaUoe
-•riMfaalogy
-rotarograpiik: anslysis
Hood cfasmlstry
--GUmatlc (actors
: factors
els-
-PtetagrspMc analysis
m
7M
asi
Z72
2M
4M
477
IM
IM
168
16a
!«•
7S3
3M>
S3
2*3
391
169
620
136
122
S94
199
SM
411
14
13
2B3
742
744
1»9
7«8
683
279
701
627
til
111
7SI
113
559
4«S
4«a
433
440
S«
314
ISl
149 0g9
171 1*4
149 216
171 190
171 039
153 575
130 062
133 914
133 129
OTS
OTs St-
ars SB-
orsss-
cmai-
133 708
171 332
orssi'
153 496
153 505
OTS SB
171 577
152 157
152 172
153 199
133 6*9
171 154
133 267
153 371
130 440
152 033
152 907
II
9
4B0
4 12
4»
■ii3
743 154 6Z7
272
40*
691
271
543
143
400
16
999
999
199
366
367
999
S44
154 623
154 674
14S 390
171 25«
171 610
133 343
150 331
154 511
602 149 333
5*7 153 753
154 097
tS0 7»»
190 7M
15i^l
171 171
153 081
149 296
171 338
786 154 167
153 306
154 406
150 733
171 047
161 4
437 153 101
153 348
153 301
171601
153:
133 5K
171 Id
153 30!
150 571
153 3|t1
IS3 9(I
133 B»
153 34:
152 69(
193^3a
1S»40I
Subteci
Blood volume
--Decermlnaitan
BhiiM bodtes
Bodies of rcvolutloa
--Aerodynamic
characteristics
--Boundsry layer
-Heat tranafer
--HyJiuiynamlc
charscterl#ics
--Hypersonic
cliaracteristlcs
- -Preeeure dlstrOwtlan
-Reftocnve effects ,
--Transooic
characteiiatlcs.
--Velocity
Body
--Moboo
Body (SI*
- - Oeterralnatiod
Body temperanire
- -Climatic factors
-Coocroi
-Fhyslolaglcal (actors
Body weight
--nyslological factors
Boiling
-AMlysls
Bolts
--Corrosion prevemlor
--Stresses
Boltsmann equation
Bomb debris
Bombing
- -Training devlcee
Page FB Number
368
193
196
456
606
607
711
435
86
193
456
84
194
606
60
774
456
711
607
769
606
194
60
259
23
265
366
997
688
689
14
15
132 617
147 878
152 345
153 106
153 430
150 636
153 183
153 658
133 844
153 099
147 878
154 403
150 634
148 701
148 703
150 636
130 830
150 831
133 919
153 106
153 430
153 668
153 183
155 144
153 475
153 413
150 830
149 311
150 575
153 336
153 351
153 373
171606
155 397
ISO 568
150 319
150 572
22 150 575
633 154 967
301
712
(00
631
101
-Theory
Bone
--Radiographic snslysls
Bijolaan formulas
Boolean functiooa
Borel-Well ibeoram
Borldaa
- -Cryatal structure
Boroa
- -Bombardment
--□Iftualon
--Electrical factora
- -Properties
Bona carbides
— AppUcatlona
--Denalty
--Phase studies
Boron compounds
--Molecular structure
"Solvent properties
38
148
688
450
79
318
114
446
630
59
782
782
784
447
693
798
Boron compounda (Organlc)-
-Bandli« M
--Chemical reactions 34
145
406
--Polymerization
- -Syntheels
32
161 897
155 086
152 587
153 311
152 650
439 153 086
171 103
148 726
154 594
153 458
152 049
152 607
171 121
153 439
153 603
149 960
155 429
155 439
155 428
171 365
153 784
155 154
155 155
153 1
155
15?
34
145
279
W5
150 519
150 519
152 085
153 215
153 216
132 087
152 CBS
153 767
148 937
Subject
Boron halldes
--Chemical reactions
Boron hydrides
--Dscompoeltlon
"Spectre
--Toilc effects
Boron nitrides
- -Synthesis
Boron oildes
--OMOilcal reactions
- -fliBae aiudlea
Boron phoaphlrie
--Synihaala
Boundary layer
--Heat tranafer
--Mathematical analyals
--Meaaurement
--S«veraonic
charactenstica
- -Thickness
--Turbulence
Boundsry layer cootrol
- - Effectiveness
Boundsry layer control
ayatema
--Performance
Bouaalneaq's problem
Bragg-Grey
Brain
--Bflecta ol radiation
--Electrical properties
--Enzymes
--Physiology
Brake llnlnga
--Materials
Brass
•-Deformstion '
BrazlBg
-Materlala
Breakwaters
■-Dealgn
Breathing maaka
- - Effectiveness
Brem est rahlung
- -Deienninatlon
- -Intenalty
Brlckj
--Coitlngs
Brightness
- - DMerml nation
Broatfeand antennas
-Analysis
--Dssign
■ • Developn>ent
Bromine
--Photolysis
BrofBe
- -Catalytic propertiea
Brown Bear Cruise
Brueckner theory
Brune network
Bubble chamber
Bubblea
- -Photographic analyals
Budget coiKrol
Bulldozing reslsunce
Bumblebee
Bunny boots ■ _^
Bums
- -BKtchsmical effects
--Fatholoclcal effects
- -Pathology
--Production
--Therapy
Butadienes
--Mymerizatlon
Butanealone
--Luminescence
Butyl bromides
--Chsnilcsl reactions
Butyl rubber
--AppllcatKna
Page PB Number
275
700
552
273
39c
691
434
701
754
434
604
193
89
193
196
456
326
711
193
617
404
688
141
19
143
590
301
776
608
' 144
934
473
S90
543
57
429
434
53
288
699
472
33
616
294
616
616
444
751
103
464
543
271
142
403
404
545
271
545
690
332
703
697
47
153 767
154 709
153 612
171 309
153 174
153 843
171 364
154 959
152 980
171 364
196
152 739
327
i52 738
607
153 262
153 838
88
150 737
153 743
152 758
150 540
147 878
148 521
150 982
153 196
ia999
152 069
171 490
153 304
150 338
152 364
171 073
152 534
154 751
152 261
151 108
153 416
161 946 ,
153 444
153 438
171 107
161 834 I
150 457 .
153 696
153 555
. 153 619
153 73B ,
149 0B9 ,
153 147
148 367
153 033
149 696
149 017
149 087
150 713
152 009
150 873
153 516
153 406
153 406
152 368
am
153 192
153 194
153 191
152 599
153 641
151720
171 Oil
154 374
154 564
152 667
1
Subtea v
Page
PBNianber
Subject 1.
Pap
n Number
Centrlfugea (con. )
•^
PB Number
Cablea ' |
1
Cargo vehlclea
--Equi|>nent I
751
154 696
--Aralc reglona
313
152 940
710
153 69S
Cadmium crysula
'
152^2
- -Joints
748
153 694
- - Growth
110
152 036
--Cotwol systems
750
153 713
Ceramic capacltora
Catknium ninhate
"Design
313
152 940
--Development
724
153 723
--Dielectric properties
591
130 899
588
171 525
- -Temperature faaora
569
154 541
Ca<knlum sulfide crystals
750
152 006
Ceramic coatings
--Electrical properties
345
171 338
--Maneuverability
750
152 004
--Development
329
171 193
Caldte
-Materials
758
171 330
--Temperature factora
771
154 815
- -Bffeas of radtatlon
108
150 374
Carrier rocket
737
153 731
--Teat results
314
171 017
Caklian .
--Metallurgical effeas '
'
Cartridge caaea
--Ultrasanlc snalyala
69
171067
777
171 384
- -Materlala
59
150 825
Ceramic nuterlala
Calclian sulfate
. Caacode amplifier
421
150 704
--AppUcatlona
571
171 492
- -Resonance
25
152 068
Caat Iron
336
149 728
Calibration
--Corrosion
615
154 809
465
ISO 922
--Instrumentation
336
171 202
Oaat ateel
- -Dielectric propertiea
795
150 915
1 ,
424
171 233
--Mecfaanical propertiea
777
171 384
- -Electrical propertiea
69
152 805
• ■'' ! ■ ' ■ ■
171 234
Caatli«a
- -Magnetic propertiea
754
155 239
171 235
--Production
458
151 098
155 240
Camadape '
82
150 598
Catalyata
.ir ■
755
155 241
Calorimeters |
--AppUcatlona
165
I4y o9B
153 242
--Aiwlyals
948
132 966
735
154 725
"Marhsnical propertiea
70
171 074
Camera shutters
--Effectiveneas
27
152 126
446
171 998
--Design
223
148 299
-Surfacea
148
152 344
591
171 590
--Development
352
i:|u97
1^2 567
Catamarana
--Performance
590
154 751
Cameras
- -Model teat reaults
745
153 706
- -Temperature factors
446
171 406
333
Cstchmeni wster
742
154 642
447
171 965
352
152 565
Csthode rsy oacllloacopea
754
171 595
Cams
- -Teat reaults
601
153 485
--Themul properties
422
171 416
-Design
Qapadunce bridges V
738
153 866
Csthode rsy lube screens
Cerebral cortex
--Lumlnesoence
727
155 320
--Excitation
687
154 993
j- -AppUcatlona
389
171 219
--niotogrsphy
637
154 752
-niyalology
997
199 468
290
171 230
--VisibiUty
431
143 302
-Sllmulatlan
142
152 540
171 221
Cathode ray lubea
167
152 365
171 222
- -AppUcatlona
82
150 598
462
152 866
171 233
- -BibUography
SO
171 127 •
Caelum
Capacitors
168
OTS SB-431
- -Chemical reactloaB
65
150 861
-iCsllbrstlon
389
171 319
304
149 712
--Combuatlon
275
153 033
290
171 220
338
152 960
634
153 237
171 221
Calhodea
--Ionization
730
149 847
171 222
-•AppUcatlona
745
154 640
Cesium bromides
171 223
"Materlala
42
152 040
- -CondualvUy
110
ISO 544
428
150 709
Cathodea (Electron tubea)
Cesium cloud
414
150 721
622
153 820
- -Materlala
105
150 424
Cesium IwUdas
--loaujauan
203
148 979
♦
106
148 254
- -Color
470
147 174
171
153 380
208
152 538
Cealian lona
-•MatertaU
572
152 128
295
152 735
--Motion
790
154 460
Capillaries
296
152 610
Chalcopyrltes
471
ISO 323
- -Blood circuUUon
267
152 690
337
152 962
Chspmsn-Perraro problem
155
150 668
Cspiul structtre
479
153 148
467
153 683
Character recognltlcB
289
152 926
Carbides
622
153 823
Charge tranafer
548
154 748
- -Metallurgical effects
778
153 673
719
153 907
Charley
153
152 149
- - Phsse studies
214
152 454
723
154 450
Chebyahev InaquaUUea
185
152 161
Carbinols
- -Meullurglcal aiMlyals
54
149 707
Chemical elements
- -Chemical reaaiona
406
153 265
--Test results
304
152 670
--Determlnstion
274
153 571
--laomerlam
406
153 156
Csuchy problem
185
148 670
--Metallurjica] effects
794
148 781
Carbchydratea
187
148 672
Chemical equiUbriian
701
150^33
- -Metabolism
17
150 564
321
171 351
--Measurement
767
153 930
140
152 851
597
159 307
- -Tliaory
699
171 575
'
401
153 537
Cavitation
Chemical ieedar
712
194 615
153 538
- -Measurement
328
147 535
Chemical hnpurltlea
402
153 541
--Theory
774
154 871
--Chemical effecta
612
171045
153 548
Csvity resonatora
--Determination
144
161 946
Carbon
-Dealgn
298
153 095
Chemical mlUli«
749
171 112
--Chemical reactions
701
154 4»9
165
153 381
Chemical notation
123
171 123
--Oatermlnation
406
171 409
167
152 241
Chemical reactiona
"Nuclear resctlons
331
152 916
Cech manifolda
598
153 366
- -Analyala
25
ISO 334
vTanperature factors
Cairban dioxide
407
154 066
Cellometer computer
82
161 565
407
171 376
Celestial mechanics
258
171 196
408
171 373
--Abaarptlon
309
171046
309
171 337
700
154 709
--Analyals
399
153 335
Cells (Biology)
--Madiematlcal analyala
149
161 408 S-1
-•Riaae atudiea
708
154 155
--Biochemistry
12
148 269
- -Temperature (actora
rs
149 659
- -Phyaloioglcal effects
21
ISO 569
--Culture
19
152 003
701
154 959
--SpectTOgrsptalc analyals
791
148 935
--Electrical propertiea
687
148 219
--Theory r
38
152 152
Csrbonates
"'X^^*MagneUc propertiea
11
isosr
Chemical warfare ageata
- -Separation
565
154 746
--Pathology
691
148 415
272
149 634
Carbonic anhydraae
Celluloee
- -Countermeaaurea
272
149 635
--Physiological effecta
140
152 433
- -Chemical reactions
644
171 574
712
154 679
Carbnnlum ions
--Bffeas of rsdlstlon
589
154 754
713
154 875
--Exchange reactions
24 *
150 538
Oaneatlte strtictures
214
152 454
742
154 622
CarboxyUc sclda
fains IMS
--Detection ' «
339
149 641
•-Symfaeals
23
150 407
--AppUcatlona
40
171 OM
39
150 101
Cardiac muacle
Canuurus
936
147 93B
--ToKic effects
691
153 841
--Physiology
396
153 174
Centipede
301
153 937
153 843
Cargo
Centrifugal pomps
154 438
--HandUng
139
152 112
-Deeign
312
152 856-1
Cawmlcala
--Tranapcrtaticn
67
150 611
153 856-2
--Coding
123
171 129
150 612
313
152 856-3
ChemlaorpUoa
n
190 996
153
147 646
--Handbooka
747
154 635
Chamlatry
144
171001
442
153 145
--Performance
63
190 894
479
161 9B6
Cargo ships
Ceotrlfugea
638
171 503
- -Model teet results
310
152 734
-AppUcatlona
36
148 374
693
153 903
--BlbUogra|<iy
391
154 409
694
153 163
33
/
S»^i»a
--fkratoiocr
Chlorsl amides
--0»co— mipanm eftecta
CaUortdaloM
- -OKanalaadaa
--Solvwi propertlcs
Chtartas InTuMr
Chloriaa laotopea
--Spectra
Chlorc^orm
— BflKta of ndUtkB
ChlorafiqrUa
- -rhotocheinlcal reacdooa
Chlorapiaat
-ngratcal propertlca
CkronMofraptdc aMlyala
--AppttcaUaaa
Cbromlian allcya
--Davekjpnienc
Cairaailim-cotek - cungacen
aUora
--nqralcal propenlca
Cteoraium looa
--Chemical reactlcna
--Propeniea
Ovamium-iroa aUoya
-•Olfluataa
--Oiidatlcn
Chranium-lroa- nickel alk^a
--Paclfue
- -Tamperaturc tactora
propertiea
- -Bflactiveueaa
--Mactenlcal propeniea
--Tea« reaulta
--Ultraaonic factor*
CfaroaofraptM
--Oe«ipi
Clicular coils
-fanpeQance
CiTCulatory ayatem
--Clinailc tactora
--DIsiary tactora
--rMkoiOK^
--fkjrslcal tactora
--Ihjrsiolocr
ClmM clouds
•-Matsoroloflcal (actor a
a*l]Ua detcnae ay sterna
ClMMOcBUoB probiem
CJamiacmum mmamc
CMhrMs ancnrea
Clara
- -Crjrstal atructure
— Mactemcal properties
--TratricaliiUty
ClsaitfBf fliids
--Davelopnf*
CUmau
--Aiaata
--GrsciUaad
•-Japan
-Korea
CUaadc (aoora
Clossd loopcoocroi
Cksklaf
--AccapiaMUty
--I>ir«proa(liig
•-ttauiatlan
ram ftNiBdwr
Sublect
267
152 763
--Military requirementa
Ml
OTSSB-^
2
713
154 •75
Cloud ciiambera
- -Applicattcns
274
152 773
--Performance
S51
152 SS4
Cloud hetfiit indicator a
--Effectiveness
S46
152 Ml
Clouds
712
154 61S
--Abaorptlve [ropertles
- -Aaalysls
40*
150921
--Ice formation
--Meteorologlcsl taaors
SSI
171497
-Radar analysis
--Radiation
27»
149 65«
Clutter mapper
400
153 127
Coaada effect
27»
149 656
Coanda nozzle
757
lS0S44l'
Coaxal cablea
758
150S4!i
--Jolma
--Thermal insulation
71
161 921 \
Cobalt
ISI
171 033
--Diffusion
406
171 409
Colialt boridea
-Magnetic properties
613
153 593
Cobalt compouDda
--Molecular atructure
-Spectra
93
161 216
Cobalt-ircn alloys
- -Magnetic properties
703
146 076
CobaU isotopes(Radloactlv«
701
150 133
--AppUcationa
-- Radioactivity
614
153 743
Cobalt -molybdenum alloy a
91
161 6M
--Fhaae atudiea
200
149 066
Cobalt oKides
-t^se studies
96
171064
Cobb Sesmount
90
171 060
Cockpits
--Visual factors
795
154 062
Coda
144
152 393
--AppUcationa
94
150 »77
612
154 759
67
153 643
CoUmydn
445
153 333
Colliaton croaa aectiona
*
CoiMda
174
IS0 79«
--AppBcatloM
rnafiilatlnn
303
171353
--Optical eflecta
267
153 336
--Optical property s
397
153 369
6M
154 166
--Rescnsnce
272
153 348
-aublllzatlan
266
153 460
396
171 367
- -Temperature
ikctora
396
153 174
Color centers
IS
150 563
Color aim
- -AppUcatiOBS
280
152 700
Color ilKXagraphs
334
152 831
--Ideatiflcstloa
763
154 349
Colored flares
1S4
153 163
--Development
546
153 490
Colors
--SuiKlarda
470
147 173
751
153 006
67
153 073
Combat skilla
CcmUnatorial analysis
407
171 138
.■
31
190 765
Comtwstloa
411
iS3S14
412
153 334
--Analyaia
555
153 427
412
153 093
707
153 715
SSS
153 4r
SS5
153 427
--Heat transfer
279
153 345
--Mathematical analyaia
733
150 913
lOS
150 892
--nmographic analyaia
336
149 688
— nqratcal tactora
.lao
171 136
-aMUIitT
loa
150 748
-Thabry
3
P^
73
103
336
331
616
n Nunber
171063
171069
150 892
149 688
149 736
149 087
29 152 193
681
281
280
151
29
415
48
158
417
457
567
46
703
410
23
102
615
470
383
717
783
787
403
204
554
442
703
793
625
553
703
704
24
470
73
181
398
187
593
786
64
586
276
S4»
550
699
767
180
66
70
447
801
66
447
179
153 7rt
153 870
153 391
153 448
153 193
153 061
150 594
147 374
154 392
153 378
153 248
171 118
615 154 542
789 154 364
148 075
149 648
106 150 644
152 353
161 575
154 543
147 759
148 426
37 171094
154 700
154 863
154 864
153 192
171 163
153 667
lS3 44k
148 406
149 096
149 097
153 123
153 757
150 063
148 406
148 407
150 089
147 174
ISS 152 303
153 153 303
160 153 079
171 063
171089
171 153
153 469
148 696
153 646
148 974
152 155
154 104
153 090
171 538
153 448
153 619
171 155
1S3 930
148 699
148 364
153 351
153 299
154 458
150 835
154 410
154 411
153 503
Sub>ect
Page n NiMBber 4
Confauation chamber gaaea
--Analyaia 66
Combuation chamber a
--Deaign 66
178
Cometa
--Spactra
-•Thacry
Comnerce
-•ioriKo
--Caribbean Islands
--Economic aspects
- -Ceogrsphical fsctors
Commiaiicstlon systems
--Development
--Performance
- -Signal to noiae ratio
-Theory
CcmmiBilcation theory
Commutator s
Compaa charge toolzatlcn
Ccmpactificatlona
Complex componem
development
Complex compounds
- -Chemical reactions
--Decomposition
--Properties
--Stability ^
--Syntheaia -
Complex iona
--{dsorptlon
--Analysis
--Decomposition
--Hydrolysis
--Spacna , .
-,; Stability
Complex numbers
--Theory
Compltg vvMbt**
--AppUcatlona
--Theory
Composite material
Compressible fltw
--Boundary layer
-Tsblea
- -Thermodynamic
properties
Compression ahock
--Reduction
Computational chains
Computers
--Design
Concrete
-- Applications
-•Coatings
••Materials
- -Reflective effects
••Streaaes
••Teal reaulta
Confer encea
Confinement
Conforms I mapping
--Applications
••Theory
Conies 1 bodies
• - Aerodynamic
charaaeriatica
3
3
3
154
554
122
224
153
635
465
303
573
46
' 48
288
303
539
572
807
323
720
598
iZ!
144
695
794
694
702
703
704
28
274
703
472
38
276
409
410
703
S93
184
186
540
760
603
800
744
189
686
758
590
753
102
753
418
477
398
186
603
323
603
193
770
1SOS32
150 332
152 154
150 943
150 938
150 940
148 291
149 321
148 197
152 125
147 646
161 587
152 688
152 791
154 545
154 546
150 645
150 796
152 984
152 791
150 904
154 483
148 502
152 761
152 762
149 847
153 266
171 380
152 503
148 938
150 642
153 163
148 932
148 075
153 662
152 097
152 772
152 773
148 075
148(776
154 297
150 335
149 681
147 776
149 648
148 077
153 646
148 978
152 442
153 080
153 200
148 212
154 765
154 766
153 139
153 689
171 083
1S3 12S
153 477
li4 206
155 253
152 519
154 462
154 650
171 107 ■
154 636
161 575
154 630
153 178
152 927
153 469
152 374
1V4 766
153 436
154 76S
153 360
171 604
Subject
Page
n Number
Sdifea
I^IP
FBNtanber
SvbtKt
Coupling drculta
Pap
IV Nunuicr
Conical bodies (con. )
Copper (con.)
(
--Heat transfer
117
150 474
--Internal fklction
613
1S4 867
-Deaign
421
153 998
»6
171 195
--Phaae atudies
199
152 017
Cowell's method
309
171 337
--Hypersonic characterlailca 36
150 985
Copper slloys
%
Crab-Nebuls
534
147 323
772
154 583
--Resonance
198
152 106
Crack srrestors
585
171 576
--Preaaure dia^ribuion
36
150 965
Capper crystals
Crankahafts
--Reflective effecta
120
150 874
- -Defer mstlon
628
153 138
--Plating
67
153 643
350
153 C88
--Electricsl properties
628
153 138
Craterii^
58
150 999
•-Slreaaea
62
152 807
--Electron trsnsltions
112
148 830
Creep behavior
614
171 487
•-Stiructural analyaia
453
153357
Copper -gold alloys
Creeping colianna
161
171 149
CoaMCtora (Electric)
- -Phase studies
93
150 470
Cr«oso|e
--Deslp
567
153 24^
Copper-nickel alloys
1
--Cbe^cal analyaia
758
1S4 661
719
150 849
- -Magnetic properties
466
153 281
Crocco viriablca
456
153 104
CoBStruaion
Copper oxides
Croaa sHp mecfaaniam
470
171 360
--Bibliography
1
171 106
• •Crystal atructure
346
153 694
Crossed field amplifiers
300
153 995
715
154 669
Copper plating
Croaaed fietd devioea
733
154 501
154 673
- -Ultraaonic tactora
445
153 233
154 503
716
154 683
Copper wire
Cryocenlca
583
153 614-1
Contalnera
-•Fracture
96
150 637
153 614-2
--Corroaion
70
161 315
--Teat reaulta
199
152 147
*
610
161 231
--Oeai^
730
154 639
Corner array
162
148 709
739
154 289-3
•
749
171 368-1'
Corona (Electricity)
794
130 642
171 568-2
• -Analyaia
621
153 916
801
171 618
182
148 727
--Electromagnetic effeaa
789
154 078
•02
171 619
Continued fraaiona
Correction circuita
570
171 543
'
171630
--Theory
76
153 071
Correlation computer
81
150 649
-Handbooka
58
161 093-5
Cxmlnuoua media
768
154 130
Correlattan functions
49
150 597
767
153 905
Control surfsces
--AppUcationa
215
149 070
Crystal deteaora
--MstenalB
773
153 693
29S
1S2 861 '
--Equipment
430
1S3 227
Control systems
451
153 560
Cryatal fabric
153
152 148
--Analyaia
584
585
171 496
171 553
--Determination
189
147 643
148 608
Crystsl field theory
Crystal flltera
112
161 568
--AppUcationa
445
171 378
257
152 834
--Development
297
149 708
--Design
303
153 035
, .
323
148 609
.149 709
434
153 442
763
155 087
^149 710
i
581
171 480
--Theory
761
154 088
Cryaul hoUera
171 481
Correlation methoda
573
154 546
430
153 227
1
171 482
Corroalon
Cryatal oacillstors
171 483
--BibUography
615
171501
--Circuits
293
152 922
t60
I52J30
171^39
-Htndbooka
581
154 757
"Deaign j
163
149 719
324
--Tropical regtcna
96
161 749
289
149 722
601
171 548
Corroalon Inhibitor a
152 658
- -Equipment j
571
153758
- •Application*
781
154 612
Crystsl ovens
•
737
155 251
• •Development
201
161897
--Design
573
153 246
--Errors
52
149 849
584
171 HI
Crystal phosphors
- -Human aagliieerlng
392
535
153165
153 202
• •Teat reauks
Corroalon reaiatant alloys
781
154 611 ,.
- - niotocondual vity
Crysul reaifiers
553
150 895
153 755
--Test results
781
153 581
••Development
43
152 657
—Mathematical analyaia
163
147 «51
Coriaidum
48
150 805
149 136
--Surface propertiea
70
171 074
735
155 321
164
152 253
Corvua
583
153 487
Crystal atructut<!
• . " i .
295
152 741
Coaet leaders
78
150 509
-Analyaia
213
152 427
568
149 090
Coamlc radiaUxn
4
148 260
472
154 297
'
723
150 109
1
333
153 911
•-Deformation
95
150 468
--Performance
164
152 253
■ 1
615
150 696
--Magnetic effeaa
112
148 917
720
149 137
-Analyaia
782
154 704
148 918
-RellablUty
48
152 295
--Oetectioo
97
150 371 «
f
148 919
--SiabiUty
295
152 741
--Energy
259
153 968
--Mathematical analyaia
112
161 568
--SUbilizatlon
728
154 804
- •Geophyaical taaors
132
153 304
213
152 447
--Statiatical analyaia
734
149 236 ,
150 764 *
133
152 209
345
149 679
--Syntheaia
S3
152 210
K.
629
153 933
55
150 493
^1
152 211
788
154 103
36
150 823
149 736
--Theory
339
153 863
163
147 651
149 136
-•Intensity
3
5
152 0S7
148 2S8
--X-ray analyaia
Cryaul units
210
153 469
■
425
153 438
<
534
153 878
--Development 'V
170
149 715
466
153 099
- •Messuremem
5
150 801
307
152 673
574
153 663
258
148 494
Crysul video receivers
153 677
149 645
--Deaign
573
150 894
--Teat methnda
307
152 778
2S9
148 495
Cryauls
--Theory
302
153 034
^
392
148 496
- -Deformstion
114
150 651
Control valvea
••Nuclesr resctions
331
149 736
603
171 531
--Simulation
636
154 966
• •Fhotogrsphlc snslysis
463
153 171
--Elasticity,
114
150 651
Convection
••Physicsl efteas
98
150 937
--Excitation
465
150 922
-•Northern hemiaphere
803
154 449
331
152 916
- -Growth
798
155 154
Convex bodiea
••Polarization
332
149 737
«
155 ISS
--Theory
186
152 440
--Sourcea
3
152 067
155 156
321
149 663
97
150 518
155 157
599
148 200
- -Tables
392
148 496
--Mechanical propertiea
603
171 531
153 771
Coamlc rsdistion shcwers
1
--Optical propertiea
341
152 624
Convex aeta
185
152 161
--Measurement
616
148 215
--Reaonance
409
150 921
Conveyors
--Ststlstlcal analyaia
449
153 385
--Speara '
213
152 447
•-Equipment
751
154 658
Cosmic wind tunnels
l45
153 504
|- -Stresses •
--SirtM* propertiea
114
150 651
Cool electrons
721
154 523
Coueneflow
192
153 551
472
154 297
Coolants
327
149 677
--Thermodynamic
--Blbliogrsphy
533
OTSSB-449
153 857
properties
344
152 725
--Chemlcsl snslysis
406
154 408
328
153 858
--Vlbrsftoo
213
152 447
Coordinate converter
334
149 297
773
154 158
Cueing methods
260
153 460
Copoiymerizatlon
316
149 963
Coulomb potential
348
153 789
Culture
Coppjr
--Chemical reactlcna
Coulomb scatteiing
382
149 650
--Sociological tactora
10
190 851
25
150 334
Coupled antennas
Culture medU
704
153 663
- -Electromagnetic effeaa
43
150 553
- -Materiala
541
153 133
- -Deformation
201
152 261
,
Curb deteaora
4V
153 101
35
Ctaic fokatu
.Cwv«d-«Bnk conpuutloaa
Cur««d atTTara
•-Corraatai
cx-a
Pi* fBmnh»
««6
♦37
299
331
100
1)3 211
1S3 478
149 741
149 739
150 944
Cyaao radicals
Clwiiilnl reacUona
276 149 Ml
703 l4aa7S
-SfBctTOfrapiilc analysis
CytiaaUca
Cyclic compounds
--Cfamdcal reacOons
--Oscooipaalclaa
— Moiacvlar acrucnre
-iul»sM properties
4
191
392
47«
7«6
106
M7
147
275
339
790
406
339
275
190 936
152 9M
153 165
152*76
171 2H
130 227
154 157
171 156
149 664
171 342
153 655
153 156
171 342
149 664
Snbtecx
Cyciotdal propeller*
--MMtograpiiy
Cylcoaes
--Theory
Cycloocxatetraenc
-Spectr*
Cyclotron magneta
--DealgB
Cyttadsra
--Aerodynamic
daractarlsacs *■
--Btoctrofnafsedc effecta
- -E lectrcfnayietlc
properUe*
--Heat traaafer
--Hydroj^rnamlc
characteristics
-Materlala
- -MaitiemaUcal aoalyats
--RaOsctlve effecu
--Stresses
--Str«K(ural aaalyais
- -Staler sonic
ctarsctcrlaclcs
4 -Turbulent boundary layer
Psje n Nianber
64
556
107
616
606
770
219
33S
633
635
MH
M
775
337
33S
349
76*
453
195
772
152 IM
153 550
150 439
149 315
153 lis
171 604
ia296
152 777
171 4S5
171 4*4
14a 34«
150 366
149 210
152 923
152 777
152142
171 664
153 357
171 179
154 816
• SM>Hea
CyUadera (Stiffened)
- -Streaaea
CyUmk-lcal chaff
CyUndrtcal shells
--Creep
--Deformation
--Loaddlatrlbutlon
--Mathematical analyais
--Pressure dtstrlbuilon
--Stresses
Page n Number
-Theory
-Vlhrsttoa
Cytochemistry
Cytochrome c
--Purtflcatlan
62
150
197
S4
324
604
604
»4
87
604
324
453
604
192
87
90
336
691
152 Hf7
152 196
171 152
149 295
149 691
147 757
153 502
149 295
152 139
147 757
149 691
153 119
153 502
149 627
152 139
150 480
149 6*2
148 415
269 152 470
*< 'S^,.
.^
SiAJect
Pap
nN««iber
Su^ea
r^
FBNunber
Siiifea
Pap
FSNunber
Damping
Deepfreeze
715
154 669
Diesel engines (con. )
--Analysis
602
153 794
Defrultlng equipment
866
171 504
--Lubrication
180
153 354
- -BMectUeneas
589
711
17) 556
171 594
171908
- -Vlbrsuon
Diet
90
153^1
--Theory
608
153 416
--Biochemistry
400
153 164
"Alaaka
441
153 523
0MB9
565
147 546
- -Effects of radiation
693
155 176
--RiyBlologlcal effecta
14
147 744
Dmh*
170
171 130
De-icing maierlals
--Theory
17
150 471
171 131
- -Devclopmeac
68
150 876
nfference equatlona
187
150 793
171 132
Oe-idag ayatcms
197
152 492
Dark adaption
- -Test results
416
159 289
330
149 644
--Bqulpmeni
302
161968
De-ionlzation cross section 108
150 949 .
597
153 680
542
161 834
Delay elements
"■J
632
153 679
Data
--Development
59
148 662
Dlffareace flelda
317
152 675
-Codli^
187
130 793
437
152 654
Difference method
318
152 715-1
--Proceaaing
67
150 611
DeUy lines
152 715-2
150 612
- -Applications
170
152 547
Otfferentlal equations
215
149 070
122
150118
, .
299
152 639
476
148 525
1
191
148 733
V
432
171 4X
601
153 671
. 1 •
148 733
--Development
170
153 547
— AMiyals
454
171 419
148 734
432
171430
--AppUcstlons
83
171070
300
152 935
--Processing
167
150 604
89
150 871
452
153 361
Delay powders
jC
115
150 556
,
153 455
- -Combustion
59
148 663
150 557
479
153 770
Delta modulstors
421
153 004
118
152 068
561
171 910
Demlnertlizatlon
40
171031
295
152 741
601
154 422
Density sensitive Indicatora
602
153 739
711
171 609
-Deaign
557
154 763
632
153 679
765
150 086-1
Denul equipment
--Theory
77
150 641
•
153 376
--Deaign
544
152 865
78
150 646
766
150 086-2
Denul research
542
154 426
186
152 441
150 086-3
-AUska
18
150 239
152 442
150 086-4
Dental surgery
690
154 427
152 491
150 086-5
OescsUng
610
161 235
i
187
152 438
'i ■
150 086-6
Destructive iestln|
351
152 897
188
149 073
808
155 068
Destruaors-M2Al
306
152 596
330
149 644
--Punchad card methoda
224
148 723
Detection (RP)
322
153 382
808
155 068
--Analysia
622
154 843
344
152 725
Dau storsge systems
123
150 819
Deteaora
449
147 121
639
153 160
--Circulta
576
153 294
•
450
153 414
- -Circuits
296
.147 313
427
153 101
153 711
463
150 708
--MathematicaJ analyala
569
153 736
597
153 668
•-Coding
391
152 7r
--Reliability
565
171 509
153 «M
--Destip
300
152 9J5
Deteaora (PM) ^
-Deaign 40^
599
153 672
--Developmeni
82
150 598
53
150 764
633
153 432
233
148 385
Detergents "*
636
153 876
299
152 40»
-Effectlveneaa
407
171 128
763
154 961
•
440
132 609
- -Optical propertiea
'694
149 895
764
154 960
560
154 758
-Soli^lllty
24
150 089
Dlfferetcisl geuiieuy
600
153 413
637
147 756
Determinanta
597
153 680
7«S
150 066-1
--Analyala
450
150 711
--Theory
598
152 828
1 ^
766
150 086-2
150 086-3
--Theory
449
450
153 306
153 711
Differential iDequaUtlea
Differentiatli^ circuits
186
152 491
>♦
150 086-4
Detonation wavea
--Development
570
171 542
J
150 086-5
--Energy
553
154 813
Dlffracdon
150 086-6
--Mathematical analysis
739
154 578
--Mathematical analysis
221
148 295
807
147 787
--Physical effecta
118
150 532
350
153 088
--Equipment
81
149 593
--h-opagatlon
217
152 484
--Meaaurentent
336
152 730
451
150 086-7
150 086-8
550
801
153 448
154 458
--Theory
Diffraction gratings
349
152 842
452
150 086-9
--Theory
803
150 534
--Error a
109
150 638
- -Military requtremems
351
152 787
Deuterium
DIfluaion
--Theory
223
148 977
- -Bombardment
618
148 154
--Analyala
446
171 400
479
153 770
-Solubility
29
150 461
--Mathematical aoalyaia
148
148 676
Data tranamlsslon systems
Deuterona
211
149 063
--Circuits
297
152 998
--Nuclear reactiona
100
150 349
S44
152 663
--Codli«
222
148 686
--Scattering
332
149 732
--Meaauremeut
199
148 675
637
153 654
Dtabaae concrete pavement
418
153 178
212
152 291
733
149 235
Diabetea
•-Temperature faaora
91
161767
••OMt«i
300
152 721
-Therapy
546
153 152
113
152 185
573
153 803
Diachromoacope
153
152 303
--Theory
28
152 152
-Development
151
150 388
Diagrapha
301
152 833
614
153 742
--Equipment
48
150 594
Dickite
470
147 173
.
775
152 117
--Errors
190
152 465
Dielectric filma
Digestive aystem
233
148 686
--Preparation
171
153 380
--Biyeiology
17
150 567
1
351
152 933
Dielectric properdaa
399
153 511
637
153 654
Dlelectrlca T
345
152 544
Digital recording ayatema
807
148 502
--Applicationa
734
190 900
--Mathematical analyala
46
150 645
--Development
45
150 806
739
153 647
436
153 722
336
149 728
Dllatametera
--Teatti^ equlpmeflt
49
150 438
572
152 138
--Deaign
470
147 759
Dsy
--Blec^ical propertiea
425
153 417
Dlocotron
571
153 938
412
153 093
--Mathematical analyala
345
153 544
Diodes
Dead apace
6M
171 607
--niyalcal effecta
208
152 534
--AppUcstions
172
.152 348
Oacarbonation
565
154 746
--Propertiea
626
153 649
399
152 750
Osoaleratlon
--Refractive propertiea
343
149 628
433
147 244
--fhyalologlcal efleas
711
171599
--Temperature (actor a
5«»
154 541
S«9
153 736
Decompression
--SyiKheaia
434
171 364
718
155 258
-Pathological efleaa ,
542
154 426
Dlea
--Design
970
153 368
690
155 574
-Machinlag
445
171 378
--Development
113
150 813
Dacompreaalon chambers
20
150 207
- -Materiala
562
171 529
163
149 736
Oaconumlnatign equipment
- -Production
313
152 724
313
149 667
--Development
712
154 615
Diesel engines
--Electrical propertiea
635
153 873-2
743
154 677
--Cx>ollng
716
154 683
va
153 873-1
--Bffectlveaeaa
743
154 675
V
«
1><I|TT
DlodM(C(a.)
--Tb« r*auk«
Dipot*
flijg fp Huwipcr
c eflects
-KadUUcii
Olprapaixyl edm
--ToBic efteeu
DIrac'* DotatioBa
[XrecUan rinderi (RF)
- -Oevt]opamat
Direcaaa flndlm
OUka
"RadUtlaa
DIapiay •jratema
--Deaign
731
43
S7»
2*4
43
161
106
4a
143
S41
166
46
171
17J
297
4»
273
403
206
xa
153
172
190
299
SOS
57i
««2
171 566
192 657
1S3 276
1S2 623
1S0SS2
146 706
152 676
193 234
146 294
152 902
14S714
152 131
193 2S6
149 OSS
152 671
153 349
193 331
153 407
153 513
149 aN
152 394
171 573
152 015
146 706
152 466
192 409
152 536
153 756
154 303
DtapUy ■yatema (coa. )
- -Human engineerlag
--MlUcary requlremeou
Dlatributed ampUflera
--Ctrodta
--Development
Dtverairy reccpUon
--AppUcadona
DtverMty ayatema
--Oe*«kif»ne«
— BUiUapaplqr
"Codlnc
- -InatnanentaUoa
--Theory
DomalB criteria
Doploc
Doppter tracUng ayatema
- -AppUcaticna
--Developineat
--Performance ^.
Doufkta Or boarda
PBfle FBNinber
Subtect
Page
PS Number
Doubiaa flr lamlnatca
164
171 126
263
664
171 313
154 063
Draft Indicatora
- -Teat reaulta
745
154 664
535
154 064
153 755
Dth
--MadMinatlcal anaiyala
- -Meaauremeal
306
58
599
153 068
150 494
193 966
431
130 730
421
150 704
Drop*
- -Cflmtaiatian
177
179
^52 546
n2S02
164^
152 236
'M2
747
19^441
194 494
2n
123
479
152 964
150 819
152 978
"OadUadan
--Vekxrtty
456
84
193 162
190 100
639
171478
153 160
Druga
--nqralotoglcal eflecta
6
152 096
765
150 066-1
Dry batterlea
766
150 066-2
--Development
43
150 804
150 066-3
--Teat reaulta
94
171 102
150 066-4
Drycella
150 066-5
--Teal reaulta
54
171 102
150 066-6
Ducted bodlea
(07
171 519
--Preaaure dttacrlbutlca
769
155 144
'479
161566
Duaa
123
171 123
- -Aerodynamic
122
150 818
char^aerlatlca
85
150 531
223
148 977
Duopoly aituadoo
664
149 521
391
153 506
Durold
757
155 572
479
153 770
Dutdtdoor
393
153 323
627
171 543
Dyea
422
153 494
--Pbyalcal propertlea
314
152 446
436
150 724
- -Specif icaaona
73
171 069
Dynamic syatem ■ynthealzei
189
171 144
62
150 647
Dynamical ayatema
83
171 070
436
150 724
I^apraelum iaotopea
565
171509
--ReaoBance
212
152 450
422
150 066
163
171 169
171 173
.
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\
■ ' ir; rr
r r V ♦-• • «* ,
t
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1
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1
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i
-
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•
J
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1 ^9
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36
i
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Sutfct
Pap
nNimber
Sub^ea
Pffi
FB Number
Subteci
Page
FB Number
EA 1814
691
153 641
Electric diachargea
Electrical networka (cob. )
Ear
-Anaiyala
216
152 034
•-Syniheala(oaB.)
575
153 234
- -Acouatlc factora
397
171 392
- -Apptlcationa
117
150 988
724
153 704
--niyalcal (actora
399
147 778
195
149 672
153 708
--Fbyaiolocy
15
152 118
197
152 550
728
150 906
--Preaaure dlatrtfatsion
58
150 733
198
161 220
--Tlwory
576
153 107
Ear cuaMona
619
171493
--Energy
466
153 073
728
155 160
Bar protactora
- -Magnetic factora
788
154 060
E lectr ocardlograptay
139
171 140
-De6l9i
619
171 493
--niyalcal factora
47
152 667
266
152 460
Early warning radar ayatema
325
152 602
--Teat reaulta
267
152 763
-ReUaUUty
577
194 S44
Electric flelda
Electrochemiatry
24
150 515
Early warning radar ayatema
-Mathematical anaiyala 727
150 902
26
150 336
(Airborne)
- -Fhyalcal effecta
342
152 473
.,
150 870
--Porformaoce
299
149 741
--Phyalcal factora
106
150 526
28
152 097
Earth
631
147 748
147
171 141
--Preaaure
714
154 623
-Staaatical anaiyala
799
149 911
276
149 675
-- Radiation
202
152 639
Electric flltera
548
155 002
332
149 650
-Deaign
299
152 629
615
150 502
392
150 722
-Developmeat
292
152 254
699
171 155
412
153 634
-Syntheals
172
148 283
722
171582
Earth modela
Electric Inaulatora
731
OTS SB-447
- -AppUcatlooa
153
152 015
- -Electromagnecic
--Temperature factora
549
153 sr
Earthquakea
propertlea
, 568
153 776
Electrodea
--Simulation
411
153 422
-MaterUla
1 434
171 364
--Adaorptlve propertlea
28
152 097
EcMnococxua
403
153 S07
Electric motora
147
171 141
Ecology
- -Control ayatema
724
150 792
148
152 127
"AUaka
411
153 371
-MaterUla
106
150 644
--Chemical anaiyala
26
150 870
Ecmnmic conditlona
Electric motora (DC.)
--Development
548
155 002
--Anaiyala
224
148 196
--Coiarol ayatema
737
155 251
--Electrical propertlea
25
171 079
"Oiila
587
153 763
Electric potential
700
150 967
-Ham
282
152 693
--Meaaurement
29
492 132
--Polarization
298
149 726
-Howkraa
282
152*92
1 700
150 967
Electrodynamica
632
153 679
— MKbMnatical anaiyala
223
152 016
--Theory
m
150 864
E lectr oencepha lograpby
539
147 561
638
153 691
148 958
688
150 338
-atabiUty
807
147 842
Electric propulalon
731
arSSB-447
--Appiicatlona
687
154 593
147 643
- -Appiicatlona
64
150 777
--Equipment
544
150 607
--Sutiatlcal anaiyala
479
153 146
748
155 345-1
--Mathematical anaiyala
544
ISO 607
Edema
--Effectlveneaa
45
171 026
Electrolytea
- -Therapy
19
150 7SS
65
150 861
--Appiicatlona »
703
148 406
Education
150 882
--Phyaical effeaa
703
148 400
- ■'Soclolaglcal factora
135
148 293
311
171080 _
Electrolytic cella
Ejection aeata
Electric relaya
- -Bibliograptiy'
61
171 114 /
--Teat reaulta
418
153 404
--Development
309
149 704
- -Temper ature^actora
24
150 919
EkU boarda
183
171 172
- - Life expectancy
45
150 794/
276
149 679
Elaatlc platea
453
171 374
Electric aervomechanlama
1
Elearoroagneilc flelda
EUatlc ahella
--Development
720
199 147 \
--Mathematical anaiyala
106
152 077
- -Heat tranafer
801
ia3M
Electric wire
j
152 676
--Smdwlcii conatriKtian
192
148 298
- -Punguaproofing
728
194 4«7/
219
148 296
--auaata
324
148 406
--bwulation
730
194 656/
153 295
-Theory
- -Vibration
192
149 627
DlA^w*i«<*l ^«»^..^.*» ■ ■
-
220
338
152 474 '
152 868
?
S3
150 5;«
-- Meaaurement -
109
150 686
Elaatlclty
•
118
150 532
760
148 212
' --Mathematical anaiyala
114
150 691
Electrical double layer
26
150 870
800
155 323
192
148 725
--Meaaurement
147
171 141
- -Optical propertlea
476
152 781
152 069
--Theory
. 29
152 13^
--Theory
215
149 070
324
149 691
149 796
--Thermodynamic
700
150 967
Elearomagnetic theory
119
219
152 616
153 295
453
152 90*
propertlea
698
154 872
221
148 295
602
193 739
154 873
338
152 868
766
14SSt3
194 874
474
171 395
»
1716*4
Electrical energy
789
148 757
--Thaory
83
171 Otl
--AppUcatlooa
196
161 220
—Mathematical anaiyala
105
150 880
^
118
192 066
--Sourcea
197
171 138
336
152 869
324
152 609
Electrical equipment
632
153 679
453
171 374
--Arctic regiona
730
194 696
Electromagnetic wavea
1
.
602
153 794
--Calibration
292
171 201
--Abeorption
221
148 287
Elaatomera
171 206
i 148 288
,
--Development
757
171 578
--CooUng
533
(TTS SB- 449
- -BibUography
119
150 507
i
171 579
--Deaign -
721
195 577
\
120
152 061
• 1
--Molecular atruaure
316
153 172
■-Salvage
713
171479
--Detectlaa
576
153 294
I
--Streaaea
75
150 491
--DUtractloo
106
152 077
t
*
316
153 172
(Airborne) i
119
152 069
i
--Temperature factora
75
150 491
-Deaign
560
153 933
215
152 364
I
1
179
161969
Elearlcal networka
%
219
148 296
1
Electric acceleratora
197
171 138
--Anaiyala
721
155 577
221
148 295
Electric area
--Development
578
148 411
350
153 068
--Redualon
45
150 794
a 47
150 511
--Mathematical anaiyala
414
150 071
Electric bacterlea
55
152 183
--Meaaurement
792
171 254
- -Bibliography
731
OTSSB-447
•^
172
148 283
--niyalological effeaa
143
152 349
- -Development
311
171 OSO
294
149 637
--Propagation
116
150 629
»48
199 002 '
1 j
295
147 314
120
152 061
699
171 195
786
148 974
206
152 524
-,
--Effealveneaa
45
171 036
--IVrformance
304
152 986
220
149 060 .
Electric cablea
--Symhcaia
163
152 262
152 232 y
--Corroalon
729
154 624
167
148 980
192 474
Electric currenta
" ■*
190
149 652
221
192 174
--Applicailona
788
155 173
294
149 636
9<7
152 633
--Blectrical effecta
722
155 616
152 486
,
349
152 987
- -Meaaurcment
788
154 102
152 489
350
152 418
Electric detonaiora
295
147 314
152 929
--Effecta o< radiatloa
172
152 991
2%
152 860
152 963
.--Materlala
736
153X122
304
422
152 986
153 175
475
152 993
150 718
BlaaranMgMUc
- -Propafatlaa (
•Mdlattaa
-RaOectlan
P^« nnmabu
-Tnaanlraiaa
Btactrometers
--AppUcattcna
BlKtrta accaleraMrs
BtoctroB beams
- -Acowuc pro^KtlM
-AffUcaticma
— GaOguradca
--CeKrol
-Pocuilaf
•ttects
- Mwhwtinlcal aiMarMa
--Prodactka
--Propacsaan
Btactron bombanknent
--Apptlcattaaa
--Btocnical effect*
Btactran capture
-Mathematical analyali
eiiieut
47»
80*
117
3N
119
1X>
a*
i
i
230
330
349
351
221
S«8
575
197
633
734
300
723
116
433
631
301
338
574
399
4«7
55
436
571
107
433
723
430
631
789
42
213
4«7
613
618
619
211
204
618
100
304
Blectraa gaa
— Baarijr
llill • analyala
-•Properties
--Wave traBaalsston
Blectraa giB*
--AppUottoM
Blectraa mlcroecapes
- -Ap^cationa
Btectron mlcroecow
--AppUcationa
Electron optics
Blectraa tube heelers
--OMiffi
Blectnai tubes
•-Analysis
-•Coohng
-•Devetcpnient
--Bfleas at radlatlca
(--LUe expectancy
799
216
579
125
636
569
45
301
430
301
338
152 781
154 273
1S4 448
ISO 734
133 833
153 834
153 616
150 874
153 343
153 2S8
153 33S
149 735
152 431
152 842
152 981
148 287
148 288
ia295
171498
171557
149 547
171 138
153 934
148 998
153 99S
154J01
154 509
150 638
130 991
150 716
153 733
152 930
152 980
153 503
153 9«
132 931
130 492
153 400
153 937
130 822
150 715
148 333
153 504
153 488
150 414
152 040
148 671
rt3 397
171 521
148 154
171 523
152 918
147 543
147 543
150 523
150 857
15? 133
152181
148 72^
153 27<
152 ITS
153 464
153 831
152 304
152 931
153 50<
110 152 03(
152 26
152
304 149 71 I
623
721
54
166
432
. 577
733
56
206
54
319
150 71 '
154 521
150'
150 64
153:
153 2A
148 33 t
149 71^
149:
152 7^
1531
P^JBjrkmber
Blectraa tites (cea. )
--MaterUla
--MiUcary reqidremeiM
--RellaMUty
--StaMUty
--Temperature factor a
--Teei results
--Tliecry
Electrcoic camera
Blectronlc drculta
--Analyats
■ --Drfcloiineat
--Bqulpmeot
--Mathematical analyais
--Synthesis
Electrontc commutators
--Development
Electronic equipment
--AppUcatlooa
--Blast effects
"Cadb«
--CooHbc
• -GouMermeaaurea
-Development
-Effects of radiation
-Human engineerinc
-Maintenance
--hrts cstaloga
--ftrformance
--Production
- -Reliability
--Sahrage
--Suadorda
- -TeeUng equipment
Electronic equipment
(Airborne)
-Shock rest stance
Electronic relays
--Quality ccotrol
Electronic scanners
--AppUcstloos
--Cot«rol systems
Electronic switches
— Orcutts
--Theory
Electronic systems
- -Preaiervatloo
Electronics
--Theory
Elecxraas
--Deaalty
0
•^Blactncal effecta
--Energy
--Bxellttlan
— lateaelty
54
56
1«9
306
571
737
436
569
47
571
47
^Ti
576
298
431
433
293
422
723
733
149 707
149 713
153 560
149 714
153 431
171 492
135 330
154 484-1
154 484-2
154 4A)
171 117
171 492
171 117
152 931
152 588
153 294
152 672
150 730
147 244
149 703
150 066
154 213
149 235
Elactroaa (con. )
-•MapwUc moments
—Motion
••Noclaar reactiona
— Reeonaace
•-Scattering
-•Velodly
Btoctrofhlllc dtepUcemem
4» 150 707
427
432
722
306
533
162
54
55
166
427
165
295
724
206
168
300
13S
162
j,173
162
30*
18S
733
71#
165
162
430
161
153 101
153 206
150 910
150 911
171 345
OTSSB-449
153 067
1171 126
171 125
150 803
171 380
149 734
162 859 ,
148 098
153 3S8
153 007
152 935
152 166
148 384
171 137
153 067
1*1894-1
150 80S
155 151
ISO 153
171479
150 803
ia284
150 703
153 260
56 153 796
730
'734
733
48
425
294
578
733
308
31
34
117
383
415
431
589
623
799
349
628
216
333
622
215
349
150 912
150 900
150 913
150 806
153 579
153 273
154 190
154 198
154 199
148 700
148 256
150 452
150 988
152 697
153 484
153 498
147 533
153 834
153 584
154 272
152 523
153 741
152 481
171 335
153 807-
152 179
147 558
Psfe
467
618
579
611
il5
216
784
799
623
406
tf
Electrophareais
--Appllcatlcna
--laacrwnentatlaa
BlearofiMiagraphy
--AppUcatlooa i
Blear oahock
-Psychological effects
Blectroetstlc accelerstor*
--AppUcstton*
Electroetsttc display system
ElectroOTStic generation
- -Meaawemem
Bmlssivlty
Emotions
-Psychological effear
Encapeulatlpg techniques
Encke
Endflre smenns
Enddre array
Engioeering
Enzymes
--Dietary factors
-Effects of radlaiioa
Epinephrine
--Determination
-niyelolaglcal effecta
Epoxides
--niysiologicsl effects
--Thermal properties
Equsticns ct state
- -AppUcationa
--Determi nation
Equlvaleal nRvorka
Ergodlc theorem
Eroelon ,
- -Meaattt-emeiK
Errors
--Dstectloa
--Theory
Erythrocytes
--Abeorpilve propertle*
--Production
Eskimos
--AUska
- -Culture
-Nutrition
■ --niyslology
Eaters
--Properties
Estuaiiea
-Alaska
-Hytkrograpby
Etch pits
Etteaol
--Moleculsr structure
Ethsaolamines
--Chemlcsl reactions
Ethyl scetatc
- -So«Bid tranamisslon
Ethyl fluorides
--Mlcrowsve spectra
Ethyl nltrstes
--Propellent properties
Ethylene odde
- -Optical propertlea
Elhylsa* polymers
-•AppUcationa
--Effecta of radiation
--Optical properties
12
701
151
11
98
190
582
217
263
316
3
309 -
730
161
157
21
691
694
21
691
756
117
218
554
739
344
422
478
60
595
764
332
143
14
478
478
441
18
336
399
403
756
FB Number
153 291
154 817
153 276
147 306
153 291
152 179
152 481
150 171
152 180
150 717
153 215
153 216
148 269
154 669
ISO 388
152 101
150 406
152 468
153 627
161 222
153 325
171 034
150 938
ISO 940
171 337
153 719
148 706
171 004
150 671
171 608
154 264
ISO 569
149 336
154 721
147 908
152 443
153 114
153 730
152 725
153 175
153 360
148 225
153 415
150 909
152 736
171 160
150 854
153 367
153 530
153 521
153 523
150 239
153 338
1S3 941
153 347
153 515
623
704
206
467
438
406
47
617
624
155 082
33
150 497
32
152 645
608
149 891
26
152 089
91
150 917
150 701
153 662
152 t50
153 153
152 316
150 664
152 667
171 490
150 657
;
" Subjeg
Ethylenes
—Chemical reactions
Euclldesn space
Euier's sngles
--ApplicaUons
Euler'a conjecture
Europium
--Oiptical propertlea
Evacuatlan bag
Evaporation
--Meaaurement
Evaporators
--Deaign
"Development
--Scale
--Corroelon prevention
Exchange reactiona
--Velocity
Exhaust dlffusers
--Effectiveness
Exhsusi flame*
--Spectrogrsphic analysi*
Exhauat gaaea
--Heai tr*n*fer
--Riyelcal effect*
Exhauat nozzles
--Pressure dlstrl button
Exit taxlways
Exoephere
Expetlani beams
Experiment Luxembourg
Experimental dau
--Analysis
-•Scstistlcal analyais
Exploding wire
Exploelons
--Pressure
--Theory
Explosive chsrges
- -AppUcationa
--BUat
--Detonatian
Page PB Number
24
450
418
187
303
465
160
39
565
713
147
311
180
348
287
178
38
417
562
258
586
155
477
594
222
319
738
476
438
198
444
306
738
■■\:
. 1
X -
150 538
153 433
171 404
14f 687
15^41
153 51
1
510
277 153 606
171 145
171030
154 746
155 566
148 678
148 679
152 154
171 068
171 369
171 507
152 936
150 320
149 062
153 633
153 668
148 695
152 896
153 022
15t835
153 III
161 231
171 379
149 633
152 022
Subjeg
Page n Number
Exploeive decompression
--Psthofoglcal effeaa 20
Exploeive forming
Exploaivea '
- -Bibliography
--Blast
198
S83
to
1
«38
••Chromatographic analysis 694
— Crysul structure 61
-Detonation 739
-Ignition
-Senaltlvlty
S49
59
438
171 308
--Spectrographic analyais
--Test methods
582
438
152 257
152 966
153 629
"V. --Thermal properties
\ Exponentisl functions
^ --AppUcationa
7»^
572
Exposure
--Biochemical effects
574
400
401
-Coiauermessure*
-Pathological effea*
402
402
688
465
18
41
149 246
150 207
161 220
161 221
171 379
154 769
150 747
171 106
171 326
154 210
152 062
153 730
154 578
171 686
153 687
149 960
153 111
171 326
153 857
171 326
150 664
171 256
154 483
153 677
153 536
153 527
153 528
153 529
J53 5M
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 538
153 539
153 363
153 366
153 525
153 541
153 548
171 606
153 510
147 476
SutiXa
Wige PB Number
Exposure (con.)
- -Physiological effecu
14
150 568
15
150 572
16
147,745
150 213
150 577
150 578
17
147 743
150 230
150 564
21
150 569
139
152 850
141
152 531
265
153 336
' ,
153 351
,
267
152 695
153 338
153 352
2«rv
152 618
4
153 337
269
153 344
^
397
153 373
-
153 545
V
398
153 372
399
153 511
--Riy Biological factors
18
ISO 576
Exposure suits
--Fhysiologlcsl effea*
102
152 299
103
152 298
--Test results
464-
153 508
Exterior bslUstics
--Determination
455
171 3*7
171 388
Extraterrest^sl rsdio wavea
- -Refraaion \
156
152 471
- -Sources , X
535
147 322
147 336
147 338
ExtrsterrltotisI waters
479
153 121
Extrusion process
749
171 568-1
171568-2
Eye
-BlooddrculaUoa
400
153 303
--Modoo
14
152 138
37
171094
399
147 778
561
171 506
--Sensitivity
542
161834
--Shielding
13
153 001
P2 crldcal frequenciea
P3H-3N
Pacalolle cananmlcation
■yauma
--Bqulpmem
Pacatoille recardtnc tymemt
2S6
199
361
110
470
472
ISS
416
1S3M0
171 135
153 991
150 543
152 604
153 143
151 361-2
153 2S9
-AffltctiaoM
-thmcrf
ParadMc rmexiticMiaa
Paradty aMact
PaUfua (MeciOBlca)
--TMt mattioda
•-ykraMBic aaaJyits
P«l«B* (rkraManr)
164
734
570
77
in
537
541
«a6
134
13S
262
264
6«6
600
35
700
461
94*
Patty adda
•-Hoctemical affecxa
140
402
400
401
Paadteck ayacema
Perml aft cheory
Perml-Yaa( theory
Perritca
--AppUcationa
- <awialcai aaalyrta
•-CkHaical propemea
* "Blacii laimitf tic
propertlea
ning
c propeitlaa
- -Mlcroatructure
--Moldti«
--Propertlaa
--Spectra
--Temperature (actora
--Wave irana^iaatoB
Perrocene* /
--Chenucal rtactioni
Parroelcctnc :ryatala
-Aging
--Grwaih
- -Magnetic propertlea
--Temperature (actora
Perroelectrtc maiertala
--BlbliogriBhy
--Dtetectrtc propcrtlaa
402
402
S3
463
462
51
293
297
578
HI
630
337
390
444
106
214
230
345
795
796
636
313
301
112
345
220
69
no
591
344
69
795
122
20t
797
132 236
130 900
153 •!»
152 100
152 167
154 S36
146 610
154 459
150 790
152 166
153 506
148 004
148 006
153 132
150 421
150 967
149 909
171 410
171 099
139 133 113
152 851
153 363
153 364
153 526
153 527
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 539
153 525
133 541
153 548
150 764
147 9^
133,:
150 683
152 581
152 660
154 806
150 673
153 238
152 923
152 418
150 706
150 413
148 981
152 653
149 738
153 3t6
153 389
154 095
152 724
152 847
150 633
149 738
152 653
406 153 265
152 806
150 547
150 899
152 854
152 805
150 915
152 035
OTSSB-434
154 077
Perramagnetlc oryatala
--Analyais
Perramagnetic filma
--Mapiwic propertlea
--Optical propertiea
--P»iyatcal properties
--Propertiea
--Reaoaaace
Pai'iouiaytlc materials
--Analyais
--AppUcatloaa
--Development
--Dtffualoa
--Electromagnetic
properties
■-llajirtlc properties
- -Optical propertiea
--niyalcal propertiea
--Production
•-Reaooance
--Theory
Perromagnetiam
--Bibliography
--Mwtwiiiatlcal analyais
« "Theory
Perry aenrtce
Peyianan path integrala
Plbera
--Molecular atriKture
--Bryalcal properties
--X-ray analyais
Fibrin
- -P»iyaiologlcal efleaa
Field emiaalon
- -AppBcatiaBa
-BlbUagrapby
- -Inatrumentation
Field ion microacopy
FiMi wheel
Piling cafalneta
- -Demolition
Filler s
Pibn readers
--Design
Pln-ataUllzed rockets
--Deaign
Fira coitrol
--Madnniaticai analysis
Fire ccmrol computera
--Deaign
--Equipment
Fire control equipment
--Dealpi
Fire detector a
--Performance
Fira eatiagiiiahrrs
- -Corroaiaa prevention
Fire esingulahlng agents
- -Materials
Fire reaiatam coatlnga
--Effectlveneaa
Fire resistant paints
--Effectiveness
Plre4
- -Countermeaalirea
Fiaalm fragmenta
--Diffusion
--Radlaactlvlty
-Solubility
--Spectra
Fixed capacltora
--Teat results
Plake-giass
Flake laminate
Flame propagation
-Anatyaia
1
43
P*^ reSianber
Subject »
f^P
FB Number
FUme BurvellUnce datcacr
38
171 028
336
149 728
Flame velocitlea
26
132 095
796
171 569
552
153 769
471
153 284
700
150 031
629
153 563
- -nKXagrapblc analyais
217
152 484
601
150 073
Flames
621
153 700
-Diffusion
SSO
153 764
621
148 349
-bihibttion
562
171 552
789
148 757
- -Radiation
27
150-755
465
150 923
- -Spectrographlc analyala
27
150 755
47
146 750
Pleaa
81
149 593
--Alaaka
273
153 331
83
150 767
Fletcher's ice island
557
153 482
305
153 236
Flicker fuaion frequency
140
153 252
576
154 771
Flight anilude indicator a
105
150 644
-Equipment
418
171 404
30B
153 236
FUght decks
212
152 291
--Equlproent
FUghl paths
331
149 739
51
150 683
--Determination
435
152 320
68
150 412
152 321
337
153 277
-•Mathematical analysis
37
171 116
439
171025
562
171 OS*-
466
153 281
Plight almulatora
637
171 543
-A'ppUcationa
710
154 744
789
134 364
286
152 885
214
148 981
601
154 806
626
154 095
Flight vehicle materlala.
461
171 410
110
150 547
Floating crane
746
154 660
68
150412
Floating docka
110
152 310
- -Corroaion prevention
745
154 640
230
152 653
- -Equipment
745
154 664
338
152 868
Ploata
714
154 614
189
152 213
717
154 633
208
orrsa-434
--Equipment
745
154 616
788
154 103
746
154 649
337
149 654
154 660
435
152 320
--Launching
716
154 662
152 321
-Teat reauhs
714
. 154 672
633
153 282
Flonra
- -Aralc regions
717
154 700
593
153 389
--Maintenance
758
171 330
589
171 520
Fluid flow
593
153 389
-Analysis
89
194
152 356
148 702
690
154 427
--Heat tranafer
633
154 967
- -Magnetic (actors
773
153 692
107
150 450
- -Mathematical analysis
86
152 099
106
161 576
89
152 416
276
152 770
192
152 445
304
152 670
443
152 525
796
171 598
1
473
153 074
750
171 613
i i
«e«
153 749
fOf
153 837
306
152 596
m
IS4 582
757
171 579
773
774
154 862
148 394
764
150 909
154 871
-Stability
88
150 528
175
171 ISO
89
148 178
327
152 857
307
152 845
338
152 858
, ■ -
609
149 782
436
171 419
773
148 951
738
153 866
149 210
439
153 086
--Sireaaea
60(
153 749
173
153 014
--Surface tenalon
88
150 528
--Theory
620
149 089
38-
171 028
--Turbulence
89
150 331
^
326
149 686
781
154 611
771
148 317
,
773
152 117
562
171 552
■--Velocity
88
609
150 737
153 835
181
171 183
-Viacoalty
88
150 528
193
152 163
>•*
171 183
327
338
152 857
152 858
743
155 250
Fluid mechanlca
64
89
152 155
152 356
309
153 283
457
153 261
101
152 806
586
154 104
101
152 650
772
153 848
102
152 644
774
150 624
334
153 030
Flulda
775
152 117
433
171 239
--Conductivity
473
153 074
75
161 947
--Heat tranafer
348
150 036
69
171039
349
ISO 035
437
152 654
--Temperature factors
801
171 618
276
153 090
--Wave tranamission
475
147 400
Subject
Fluoreaceace
--Excitation
Fluoreaceni dyea
--AppUcationa
Fluorktea
--Heat of formation
Fluor Imetrlc method
Fluorine
--Chemical reactions
Fluorine (Uquld)
--Chemical reaalcns
Fluorine compounds (Organic)
- -Bibliography
--Chemical properties
--Chemical reactlona
- -Surface propertiea
- -Symheala
Fluorine Isoiopea
--Nuclear reaaions
F luorobenzenea
--Reaonance
F hior ocar bona
- -Syntheala
Fluoroethylene polymers
- -Heat crana(er
F luor oethy lenea
--Spectra
Fluoroacopes
--Applications .
Fluor oaiUcanea
- -Microwave apectra
PiKier
--Mathematical analyala
--Teat methoda
Flying platfcrma
--Deaign
--Development
--Teat reaulia
Flywheela
- -AppUcationa
Foams
- -Materlala
Food
--Container a
- -Effeaa of radiation
ftf PB Nianber
Subject
Page PB hhwber
Subjeq
Page PB Number
544
550
272
550
70
756
696
696
277
274
101
--HaaUi^
Pormaldeiqrde
--AppttcaQoaa
550
696
757
696
•
583
624
285
454
605
285
158
419
711
737
179
176
441
21
746
740
743
i?
150 943
153 401
153 445
149 634
153 764
152 297
171 252
155 45%
154 118
150 619
149 683
150 516
150 539
152 403
154 251
155 572
154 262
153 447
133 134
147 554
171 407
152 687
153 624
149 075
150 075
153 859
155 251
171 178
152 7»j'
171 418
150 671
155 414
155 566
171 606
154 633
--Decooumlnatlng effecta
--ToKic effects
Fourier aeriea
--AppUcationa
.Fourier crana(crma
Free jet Impingement
Free radicals
--Chemical reactiona
--Detection
--Bnecta of radiation
--Electron tranaltlons
--Hyperflne structure
--Production
--Spectra
--Spectrographlc analyala
--Stabilization ^
Frequency
- -Control
Frequency meters
-CaUbration
743
742
184
188
282
320
417
711
23
177
277
781
549
107
149
547
149
408
547
M13
276
592
292
423
424
43
154 657
154 642
148 707
149 073
152 799
152 431
153 083
153 642
150 407
171 184
171 310
171 596
152 961
150 430
152 488
153 814
148 976
152 685
153 814
150 443
152 770
150 072
789 153 716
171 216
171 231
171 240
171 229
171 230
171 232
Frequency modulation
- -Appllcaiiona
730
154 81
Frequency motkilation
receivers
--Test methods
426
153 24
Frequency multipliers
-Design
50
152 036
574
150 898
- -Teat reaulta
51
150 683
Frequency shift keyera
- -Mathetnatlcal analyala
288
152 985
Friction
--Temperature factors
469
171 474
- -Testing equipment
192
148 674
-Theory
90
150 952
Frtaloo brak(>*
- -Materials {
590
154 751
Froga
--Hiyaiology
140
152 399
From enda
735
150 847
Frontier aettlemeia
122
152 110
Froatblte
- -Therapy
18
147 746
132 032
366
153 353
Fuel cella
311
171060
699
171 155
731
arSSB-447
Fuel flkera
--Poroaity
180
161966
--Teat methoda
756
155 296
Fuel Injection
- -Phyalcal (actora
756
155 256
Fuel tanks
--Teat reaulta
564
153 879-1
133 S79-2
Puela
--Effects of radiation
209
153 258
-Stability
180
161 966
--Toxic efiecta
74 .
171 068
273
171 309-
396
153 174
691
153 845
--Tranaporution
447
153 078
Functional analyala
601
153 671
Functions
760
154 098
--Analyais
322
152 737
450
• 153 711
--AppUcationa
186
148 691
762
152 957
-Coding
597
153 092
- -Determination
79
152 292
593
153 806
-TaMea
763
154 961
764
154 960
--Theory
79
152 049
<
184
148 707
185
152 372
152 444
. >
188
152 430
317
152 674
319
152 375
338
152 777
449
153 754
596-*
153 135
597
152 956
762
154 452
400
193 303
Fungi
--Culture
541
153 122
Fungua eater
686
154 462
Fuaed aahs
27
OTSSB-429
Fuaion power generation
216
152 517
Puzea
—Teat methoda
583
133 447
J\
J*
» . _ 1
,
»
I
\
i
/
•■
•l
-
*
m
■
t
ti
>
• .
Subject
--apactragraphlc aitfiyala
n hhanber
535 147 327
Caleta cokamotoijr
CntH cbaory
-ApfiUcattoiw
94
94
7«
75
76
121
J 595
«01
319
575
* 6»
7«2
7S5
788
ABKXIOM
raatera
--Ctenlcal aOMU
-Dwcilco
idKamlnatloB
Garaeca
--Appttcationa
--Cryaal acructure
617
102
785
147
332
99
99
333
617
335
102
202
785
110
795
796
212
214
Gaa t—rlma
- 'Parfonnancc
--SMtallliy
--Theory
Gaa diraniata(ra|tiy
Gaa cjpcle cooling
GaadtfluatOB
:lGal aaalyata
--Temperature (kctora
Gaa (Uachargea
--Aaaijraia
--Appllcatlaaa
--BlKtrical propenlea
--Taaiperature
Gaa aotoUam
- -Cotter meaaurea
Gaa fknr
--Anatrala
-AppUcadoM
-Denalty
-Etactroniapietlc (actora
-Heat cranaieT
I ailaar boundary layer
: factors
[leal analyela
1
--Tabiea
--Temperature.
- -TMrbulaoce
--Velocity
--Vlacoalty
Caaf ararlt ayatema
Gaal
175
SC7
442
S«7
111
438
210
146
699
338
429
209
622
•9
194
196
3»
114
773
800
87
118
87
192
28
276
327
606
773
466
178
36
454
•6
17
118
87
196
584
114
US
333
152 151
152 151
150 951
152 175
152 177
150 839
147 547
171 555
148 500
171 549
154 812
155 324
155 257
154 103
763 171 687
154 428
154 439
154 430
153 644
153 908
171 156
171 041
171 124
152 677
153 790
171 491
171 341
161 575
161 584
155^
152 310
155 386
155 385
152 450
148 961
Sm ISS 336
171 157
148 011
153 128
155 001
171 033
171 363-
152 549
150 781
154 538
153 089
153 245
152 487
153 807
149 246
152 356
1«694
152 480
152 738
152 678*
154 158
155 323
150 347
150 762
150 347
152 551
150 170
153 091
149 677
153 13S
153 692
153 874
153 154
161 574
153 477
190 346
130 802
190 763
153 3S7
148 673
153 944
153 678
130 533
171 33S
Subject
Gaa lonlzaiiaii (coa. ) '
--Analyata
•-AppUcatlooa
--Blectrlcal eflecta
--Elaikrlcal (actora
--Majiwlc (actora
--Mathematical analysia
--Meaaurement
--Temperature (actora
--Theory
Gaa leaka
--Oeiectiaa
Gaa maaka
--Effectlveneaa
Gaa lurbtiiea
Page PB Number
-Foal coMumptlon
Gaailj— wiica
Gaaeoua eiectronica
Geeaoua rocket propel'aaa
--CombuatloB
Gaaea
--Abecrptlve prof»rtiea
--Acouatic ^ropertiea
--Adaorptlon
--Chemical reactlona
- -Chramatagraphic
anaiyais
--CombuatloB
- -Condenaatloo
--Denalty
--Detonation
--Electron tranaltiona
--Heat trana<er
--Haadaf
--Molecular acructure
--Ffayalcal tactorb
--Sefaration
--Soaad tranamiaaton
—Specific heet
194
799
63
419
lOS
631
348
310
574
799
304
216
348
786
606
218
576
13
66
178
93
443
607
314
--SpectTOfraptilc analyata
- -Temperature
--Thermal propertiea
--Thermodynamic
propertlee
Gaakaca «
--Materiala f
Gears -s
--Lutirlcatl^ii
Gelfer co«HitU-a
- -Statlaticai aaalyala
Geodare ayatfm
Geaadca
--AUaka
Gcodeelca
--AppUcationa
Ceodedc data
--AaaVata
--CeUecttac metboda
Gaofraphy
--Borneo
- -Caribbean lalanda
-Haiti
--Hoaduraa
GeotoBr
415
804
25
787
623
196
694
276
742
26
194
217
550
553
739
801
548
634
195
607
703
TOO
92
791
454
800
468
803
634
118
634
2U
314
554
634
152 426
153 584
152 065
152 319
150 526
147 748
152 789
1S2 549
150 898
149 911
152 4»
152 034
152 137
149 540
153 125
152 443
171 358
152 002
150 332
152 527
161 216
152 525
153 428
152 561
747 155 149
71
72
594
323
114
3*9
736
29
557
154
554
2*3
282
278
153 283
147 840
150 458
ISO 198
153 768
152 480
154 210
153 090
155 250
161 574
152 426
152 484
153 448
154 813
153 730
154 458
154 748
154 432
149 672
153 438
150 535
154 509
161 764
153 082
153 477
154 208
153 136
153 657
154 7»
154 722
150 486
154 4)2
152 443 ^
149 665
153 114
154 755
753 171 I
171065
152 755
148 419
152 722
153 678
153 347
171 348
171067
154 810
148 391
149 331
153 893
153 892
149 638
Subjea
Geomagnetic
micropulaatioaa
Geometric genua
Geometrical optica
Geophyalcal aurveying
- - Inatrumentacion
Gcoptiyatca
Germanium
- -CoulHCtivity
--Dielectric propertiea
--bnpurltlea
--Mapietic efleaa
- -n»toconductivity
Germaalum cryatala
--Conductivity
Genera
Glaclera
-Alaaka
- -Geoptiyaical eflepa
- -Graaalanrt
Glare
GUaa
--Adaorptiv^ propertiea
--Bondli«
--Development
--Dielectric propo-tiea
- -Effecta at radiatton
Glaaa textiles
--AppUcationa
--Coatinga
--Propertiea
Page PB Number
avii
- -Temperature (actora
Glovea
fTeet methoda
Glu
Glyda
--niy^otoglcal eOecta
Glycogen
--Sjradieata
Glycolyaia
- -Temperature factora
Gogglea
- -Arctic reglona
Gotter
Gold
--Bombardment
--Cryatal structure
--Deformation
Gold wire
--AppUcationa
Gondolas (Aeronautica)
--AppUcationa
Goalometers
--AppUcationa
Goufaau Une
Graft copolymera
Grains (Metallurgy)
--Deformation
--Streaaes
Graphite i
--AppUcationa I
--Cryatal structure
--Impregnation
--Thermal propertiea
Graphite electrodes
Gravimetric snalyals
--Applications
- -InstrumentaUon
Gravitating gaa
Gravity
--Determination
- -Biyalcal effeaa
Gravity anomaUea
Green function
Green Glca>
Grenadea
--Dealp
-M6
207
476
S75
206
475
343
110
344
636
344
211
54
ISO
278
152
716
550
159
590
472
446
171
171
69
75
, w
206
12
16
17
14
17
266
545
14
397
464
403
619
628
628
738
710
46
575
316
781
470
144
694
117
282
557
174
474
282
319
338
151
306
306
152 158
152 159
152 206
152 828
152 781
153 595
171 003
171 377
149 628
150 501
151973
171 511
152 973
152 918
149 707
152 290
149 638
152 387
154 647
171 512
153 259
171 526
154 297
153 439
152 219
153 319
171 061
171 096
171 061
149 674
152 028
150 213
147 743
147 744
150 564
153 353
153 370
147 744
153 545
153 509
153 51S
147 553
153 772
153 772
153 022
153 695
152 131
171 557
149 963
150 006
171 360
773
153 693
91
150 917
753
153 914
445
171 390
160
171 129
152 393
153 163
147 908
152 799
152 880
154 810
148 697
171 3»5
152 799
152 800
152 369
153 777
152 569
152 597
152 597
Subject
Pa|e
Pii Number
Subject
Page 1
685
<'^°" )686
>B Number
Siri>)eo
Croup (Maihemati
--TTieory (con. )
Crenadlnea
Grlgnard reagents
554
149 321
--Paychological (actors
14^902
149 904
c8><con
» 595
153 664
--Chemical reactlona
551
153 812
--Sociological factora
10
190 851
598
193 267
Grinders
10
150 852
193679
--Development
444
150 706
^,
139
148 293
193 076
Groasjean's method
783
153 891
-
685
147 903
600
193 177
Ground effea phenomena
419
150 073
--Slailatica] analyaia
539
171 545
Grmaky InequaUtlea
594
153 139
Ground Impact
711
171 599
--Teat methoda
7
152 103
Gtrn barrela
Group dynamics
8
ISO 361
11
150 475
- -ProceaaIng
742
194 307
/
122
137
150 495
US 292
--Theory
9
540
150 542
147 768
741
199 099
199 061
'
687
149 324
686
147 530
199 063
--BIbUograpby
7
150 498
Groupa (Mathematica)
323
152 436
742
199 068
135
150 500
594
153 860
199 060
--Paychological effeaa
539
153 760
600
153 413
Gun^aights
540
154 835
601
153 671
--CaUbratlon
57
152 361
•-Paychologlcal faaora
10
148 268
--Theory
76
148 063
Gyro atablUzera
1 .
10
ISO 859
78
150 509
--Performaaoe
737
155 252
'
364
152 913
150 951
Gyroacopea
265
152 889
'
188
148 685
-•Dealgn
179
171 157
540
147 767
. 1
318
152 607
--Development
419
194 298
-
540
153 080
323
152 747
Gyrotron
419
194 298
3
/
49
Sttjuct
F»g» W Number
(toU
•-Growth
--Mauorolofical factor*
aw
30
J50
2S0
- -Radar aoatysU 5S5
-Valociiy SM)
HallaOect 309
I campounrta (Organic)
reacuona 407
467
HaloBM compi
--OMmical
-ioalsatloii pcxendal
Haad ganeracora
--Oaalgii
Hartnri
--Loulalana
Hard ccp
- -Maaaurenien
Hardware Icema
Hannoalc analyaia
-- Applies ckwa
- - Brrori
Harmonic functiona
--ApT>licaiions
--oiBCerminailoa
Hanwailc oacUlaiara
- -Start artral aoalyala
Hartree-Pock
Harvard teal
Haip
7X
1S3
714
Tao
aoi
am
lOB
in
IIS
322
77
Its
319
112
339
344
9M
-Human enfloeerlBg
Haartaf
-niystolaKT
Heart
--tatbolof;
•njwical factora
-niyaiolaBf
Heart beat
--Meaaurement
Heat equetloB
Heat odMotBra
-OBatga
Heat cf aubamatloa
--Oatermi nation
Heal production (Btotofy)
- -Meaaurefnen
S44
54S
690
13
12
13
IS
2M
397
139
au
319
too
21S
736
--Drrdopmant
-Burope
-Patl^
-•Mechanical properties
i
--Metallurgy
••Riaae atudlea
•-PlckUng
--Propertlea
Heat realstaat polymers
--AppUcatlaoa
--Oecompceitioa
--Oevelopmeai
Heat sink
139
26*
•02
777
776
4M
7S4
90
93
775
446
96
461
749
329
330
19*
329
^^7
610
92
753
»
551
39
417
771
153 391
150 420
152 207
152 775
153 390
152 774
152 406
171 376
153 397
150 S4«
147 646
154 619
153 92*
161 a97
152 487
150 932
152 20B
152 373
14S066
152 109
149 661
146 500
I4S917
149 639
152 SS4
l»4a6
171 361
171 362
1S3M4
14*319
397 171 392
153 374
153 370
171602
150 21*
152 02*
152 029
132090
152 031
ISO 215
152 460
153 369
171 140
153 037
152 376
153 296
152 7*4
154 6a6
407 154 066
152 S49
153 337
171 559
0TSS8-45;
151 to*
15109*
171 617
171060
161 216
171597
161 233
171064
171 410
171 112
171 19*
152 4«3
161 223
149 655
171 391
161 235
151096
171565
171 100
171522
171064
171 372
154*15
Sufcjact
Heat tolerance
--Analysis
--Oetemunatlaa
Heat transfer •
--Acouatic factors
--Arctic regions
--Determinstion
--Mathematical aaalysls
-Messuiement
--nyelcal factors
•-Velocity
Heater*
--[>sign
- -Operstion
Heigbi finding
Helicopter blades
Helicopter engines
--Development
Helicopter rotors
- - Flutter
Helicopters
--Cootrol syaieroa
--Design
--Human engineering
-•Ice formation
--Lateral staMliiy
--Longitudinal stability
- -Operstion
--Performance
--Range
Helitron oeclllator
HeUum
--Applications
--Haodliiv
--Preaaure
--Spectra
- -Spectrographic aaalyala
- -Thermodynamic
properties
Helium (Liquid)
--Cooling
--Dielectric properties
--Motion
--Production
--Thermodynamic
properties
Helium Ions
-Motion
Helmets
--Acoustic propertlea
--Design
Helmlfttn coUa
Helminth peraaliea
Hemoglobin
-Production
Hemophilus pertussis
--Culture
Hemopotesia
-Effects of radlatlan
Heparin
- - niyaiological effects
Hepatitla
-AUaka
Hcpcadiyne
--ToKlc effect*
Hickman stUl
Hickory
Hlckoryboarcb
High altitude
- - Elect ricsl effecta
- - Bxploratioo
46
Page n Number
103
102
13*
64
5*6
633
2
327
M
85
196
218
a03
218
348
439
474
726
635
803
617
738
4
561
178
160
2*7
711
2*6
37
326
2*7
2*7
133
416
564
55
616
5*4
740
741
5*2
25*
33*
218
475
409
21*
72
409
466
619
7*3
402
12
143
21
19
267
143
541
39
75*
183
45
416
152 298
152 299
152 428
152 155
154 104
171 485
150 573
152 557
150 634
ISO 621
152 739
152 784
150 243
171 183
152 966
152 829
171 395
155 567
171 484
155 OBI
154 428
154 429
154 725
150 933
150 934
150 935
150 936
171 514
152 527
2*5 147554
152 230
152 625
153*51
149 6*6
171 094
153 195
152,625
152131
171 139
154*06
153|79-
153 J79-
150 492
149 0*7
153 617-
153 617-
154 290-
154 290
153 615
152 946
152 664
474 153 ICB
150*00
153 166
152 60*
150*00
150 282
152 60*
152 6*8
171 493
154 863
153 522
14 150 854
1-48 269
171 160
152 640
150*56
152 690
403 153 543
148 294
152 902
171 030
154 281
171 171
150 806
153 334
Si*)ect
High altitude (con )
- -Instrumenution
--Meteorology
--Physical effecta
••Physiological effecta
Page P* Number
High temperature
rch
--Bibliography
--Instrumentation
- -Teat facilities
- -Testing equipment
Hilbert space
Hoiats
--Teat reaults
HoUoman track
Homeoauta
Homology theory
Homotopy theory
Hooeai John
Honeycomb structures
Horizontal indicators
--Teal results
Homtones
- -Physlolagical effects
Hotshot
Howitzer
--iaBmm-M2A2E2
-BUst
Human engineering
3S
426
555
315
139
140
267
543
High rre<|uency communica-
tion systems
--Bquipmera
High frequency dischsrges
— Aaalyala
H^ pressure resesrch
High speed cameras
--AppI lest Ions
- -BUdlography
--Control systems
--Development
- - Equipment
High apMd photogrsphy
--Applications
721
209
330
459
630
806
308
580
223
341
352
64
308
118
218
276
330
472
S«l
635
770
797
804
804
217
787
636
634
322
ItO
709
84
189
S9«
59*
764
34
437
418
57
13
85
193
195
769
58
14
121
•-Arctic regions
--Bibliography
••Handxnks
-•MlUury requirement*
Humidity
--Control *ystems
-Physiological effects
Humidity cabineta
-Dealgn
Humidity sensitive elements
- -Calibration
Huaky i
Hydatid dlseaae I
Hydrated Ions (
Hydrates
--AppUcstions
--Crystal structure
••Physical propertlea
992
265
392
5
682
259
563
713
138
30
30
153
403
701
40
546
40
150 753
153 231
154 80*
171 306
171 140
152 765
152 763
154 819
155 025
152 487
'l71 348
171 025
171 0*9
154 865
171 352
154 968
150 974
171 191
171 197
152 039
171 352
150 890
171 183
149 675
171 348
153 426
161 932
171 159
154 842
154 572
153 721
171 567
arSSB-453
152 472
154 161
154 966
154 722
152 761
152 762
154 098
171 614
152 802-1
152 803 2
152 203
153 676
153 675
154 456
152 189
150 097
171 40*
152 361
150 442
171 104
152 5S5
149 672
153 553
150 733
150 733
152 13*
150 836
150 837
152 146
153 547
171 333
153 547
148 319
154 522
149 211
171 551
154 638
152 428
152 195
152 195
152 149
153 507
154 659
171 031
153 490
171 031
Subject
Hydrates (con. )
- -Resonsnce
25
152 0**
- -Spectra
409
147 776
Hydrsullc fluid*
-Test reiults
73
171 063
Hydrsullc ptavcr systems
--Development
735
150 903
Hydraulic servomechanlams
*
--Analyats
636
154 966
720
155 147
Hydrazine
' -Determlnatioa
755
154 716
Hydrazine derivatives
--CSiemical reactions
275
149 687
- -Oiidation
149
148 976
Hydrazoic acid
-Ptnolysts
549
153 QSI
Hydnde*
' -AppUcstions
7*2
155 431
Hydrocarbons
- -CrystsI structure
145
171 181
--Decomposition
547
153 6*6
--Elecrtrical propenles
337
149 725
- -Exchange reactions
624
153 237
--Ignition
148
161 9t7
- -Isomerism
697
153 717
•-Molecular ainicture
148
161 967
547
153 6*6
790
153 655
- -Optical propertlea
277
149 631
-Spectra
275
171 300
Hydrodynamics
579
153 276
89
150 871
609
149 782
--Theory
45*
153 650
Hydroelasltcliy
745
149 745
Hydrcfolls
-Bibliography
609
171 502
- -Cavitation
328
147 535
--Dealgn
88
150 47*
150 479
609
171 502
- -Hydrodynamic
characteriaOca
•9
152 416
nyurmen
--Adaorptlon
27
150 536
148
152 127
550
171 512
--Bombardment
618
14* 154
--Chemical reactlooa
408
150 923
--Ctandensation
791
154 457
--Determination
149
149 056
405
171 40»
--Electron tranaitions
100
150 944
--Electron (ranaltlons
204
147 542
623
148 936
--Hyperflne structure
790
153 828
--Molecular rouilon
623
148 936
--Molecular stnicture
790
153 829
--Neutron cross sections
204
171 163
- -Oxidation
406
150 690
--Physical effect*
610
154 749
- Propellam propenie*
311
153 791
Subject
Page W Number
Subject
Page PB Number
Hydrogen (con.)
Hyperaooic nozzlea
- -Proton crxMM aections
100
150 523
--Oeaign
457
153 838
204
150*57
152 133
--Aerodynamic
618
147 543
ckaracterlacica
^
171 195
-SoiubtUty
29
150 461
--Flight paiha
m
152 583
-Spectra
623
148 936
• •Hypersonic
- -Thermodynamic
diaracteristica
120
150 735
propertlea
US
150 762
--Performance
87
150 606
Hydrogen (Liquid)
-•Recording devlcea
293
171 194
-Handling
72
150 283
Hyperaonic wind tunnela
Hydrogen bonding %
40*
148 031
• -Olibratlon
417
153 435
553
153 811
-•Dealgn
173
153 435
Hytlrogen embrlttlemem
610
154 749
--Development
195
152 504
- -Analyals
461
171 394
197
171 142
-Inhibition
92
153 680
-•Equipment
193
152 555
--Meaaurement
778
150 780
195
149 672
171 253
327
149 344
Hydrogen iona
457
152 838
•-Dacainiliiatlan
410
153 356
769
153 553
Hydrofaa overvoltage
25
171079
Hyperveloclty guna
Hj*liugaa peroaide
- -Aerodynamic
- -Chemical reactiona
26
153 095
characteristics
737
153 648
700
150 031
--Development
175
149 071
- -DBCompoaltion
26
153 095
- - Equipment
737
153 846
552
153 769
- -Performance
173
152 554
--Elearalysls
26
150 336
Hyperveloclty projectiles
-Spears
550
154 109
--Erosion
60
148 225
-Stabiliiy
26
153 095
--Exterior^listics
560
154 758
552
153 769
- -Ionizing effects
727
154 5*9
Hydrography
33
150 487
••Launching
173
152 554'
Hydrology
33
150 497
••Penetration
19
152 003
Hydromagnetlcs
89
150 871
58
150 959
HjKlrophones
62
150 925
-Design
302
153 979
175
152 3*0
Hydroxyl radlcala
152 3*1
--Chemical reactiona
146
148 2*9
307
152 729
--Spectra
408
150 923
,
440
153 316
Hyperbolic equations
Hyperveloclty vehicles
-Theory
77
150 641
--Communication system*
120
152 061
187
152 438
- -Control aurfacKa
773
153 693
318
149 646
307
152 778
Hyperflne structure
•-Oiolliv
160
153 257
--Determinstion
790
153 828
43*
171 363
- -Spectre
107
150 430
-Flutter
454
171 407
Hypersonic flow
-Material*
39
171 064
-Analyals
606
153 118
157
171 147
--*oundsry layer
327
152 537
417
171 372
711
153 658
445
171 390
--Heat transfer
196
152 739
--Streaees
437
151 101
326
152 947
Hypochromic effect
544
153 3SS
327
152 537
Hypothalamua
606
150 636
- -Phyalology
140
150 966
--Laminar boundary
HypothermU
layer
804
154 510
--Applications
398
153 544
- -Mathematical analysis
193
152 260
- -Biochemical effects
544
153 374
194
152 426
•Pathological effects
545
153 370
196
148 673
690
171602
♦56
153 106
--Physiological effecta
13
150 218
153 184
15
150 215 '
153 420
139
152 853
457
153 315
366
153 342
772
154 5*3
397
153 369
-•Meaaurement
737
153 846
Hyateresla
39*
153 544
769
153 553
-Analyala
399
153 S42
••Theory
T70
149 328
- -Temperature taaora
lOS"
591
150 644
150*99
Hjrria
95
701
451
171 066
150 133
153 560
47
--Amaictlc Ttfkom
--Arctic Ocean
••Arctic raglaas
- -Btbllofraphy
-•{Momiatioa
• -OrMoUnd
-Molecular atnicniTe
-Radir tnalrala
-Spectra
-Tamperature (Ktcra
-Taatiog atyilpmem
lea
ice cryatala
--Hn»afc»l pTopertiea *
Ice ffff""**"* lAeronautica)
--Mawanirnlral (actora
- -Slraulatioa
Iconoacopea
--ApftUcabcoa
- -BakUoBTaplir
--Oerelupiiiat
Igniter*
-A-l-A
--Interfar
bnafe corralailaa
biM^ fumacea
bnafla iaocce tube,
bnafe atsc
Imltactie laapmaf
In^tcx ttack
-•AaalTsla
- -Ifieaauronenc
--nyalcal effecta
-niyaiological eftecta
•Maaauremei*
ry nUxturea
Bftactlvenea*
Teal raaalta
-•Preparacioa
IncUum anclmooUiea
-•Electrical profiertiea
prcfierttea
bKUuin fUma
- -Superconductivity
Indotea
--Appllcattona
baluatrlal equipment
- -Oe««lapnM»l
biduetTlal productkcn
-Chile
-•Coouol ayatema
•-Bconomlc aapaaa
--Quality control
bKkMtrlal payciulafy
Induacry
•Chile
lDe<rialJtl«8
411
153 480
ISI
152 568
152 388
SS7
153 482
151
152 568
152
152 456
153
152 149
211
171 190
152
152 457
411
153 480
557
153 483
35
150 858
349
152 »t7
25
150 8S8
146
tM2M
152
152 388
349
152 987
151
152 566
152
152 388
2S0
152 775
408
148 021
279
152 977
326
153 195
580
171 108
341
149 643
425
171 386
437
132 654
437
1S3 664
748
154 637
121
150 418
217
152 472
425
171 386
478
171 385
539
171 545
197
171 138
311
153 r2
58
1S0 9S9
62
150 925
161800
307
152 729
440
153 316
602
148 811
148 812
711
171 599
37
152 315
314
171 311
301
152 833
303
149 647
422
171 245
429
152 693
271
152 599
306
152 596
639
153 ItO
«07
171 519
123
171 123
4M
171 406
79*
148 016
626
153 199
171 511
346
152 901
694
154 2M
Itt
150 803
587
153 763
748
148 787
444
150 713
223
152 016
588
149 155
748
148 095
76
152 176
177
149 074
587
153 690
638
154 423
749
149 088
154 869
444
150 713
587
153 763
318
149 646
Subject
loertlal guidance lyatefn*
-•Deal^
laformatlon theory
Page n Number
•-Applicatlaaa
brfrapolynomlala
lofcarad datectqA
•-CaUbnUaa!^
•-MaierUU
-•Senaitlvity
--Signal to noiae ratio
Infrared equlpcneni
- -Calibration
•-Dealgn
Infrared equipmen*
(Airborne)
••De»elopment
Infrared film
--Development
Infrared filtera
--AppUcationa
--Development
--MaierUla
Infrared lamp*
-Deaicn
Miared optical material*
--Development
737
175
9
78
187
222
302
303
351
436
452
478
479
637
684
808
190
539
319
468
307
339
793
625
340
468
39
399
340
341
340
340
339
340
Infrared reaearcfa
Mrarad apectia
-•Aaalyala
- -Meaaureit)em
Infrared speciroacopy
-•AppUcatlana
--Theory
Infrared wave*
--Abeorptlon
--Attenuation
••Maaaurement
--Tranamisaion
InorfBnlc polymera
Inorganic aubatance*
--felymertzatioti
Inatructor*
--Attitude*
Inairument panel*
--Codli«
Inatrumenia
-Calibration
155 252
171 157
150 794
147 588
148 69f
148 686
149 673
153 054
153 038 I
152 7«
153 722 '
153 361
153 360
153 770
153 664
154 064
155 068
150 603
150 904
152 371
171 238
153 100
149 641
153 923
153 456
152 714-3 ;
171 238 I
150 101 i
153 335 i
b I
152 714- J I
152 714-4 !
152 713 i
558 153 920
341
590
620
3
27
117
209
339
413
415
468
550
590
696
792
694
466
582
467
339
415
468
792
340
415
555
156
546
546
360
5
290
152 714-1
149(67
149 641
149 6S7
792 153 467
152 624
171 526
153 450
152 064
150 755
150 955
148 712
148 716
152 076
171 342
153 634
150 697
153 657
154 109
171 515
154 362
149 567
J71 254
153 036
153 136
153 857
153 392
153 393
171 342
153 283
153 667
155 437
152 714-4
153 061
154 808
150 217
152 875
152 875
149 642
171 063
171 209
171 212
171 213
171 306
171 210
171 220
Sublect;
InatrumeMa (con. )
- -Calibration (con. )
Page ft Number
290
293
338
336
406
422
423
434
<«
Inaulating compoinda
--Development
Inaulating material*
Inaulailon
- -Heat tranafer
--Maaaurement
•-Phyalcal (acior*
Inaulln
--niyalologlcal effect*
Integral e<]uatlon*
--Analyal*
--AppUcationa
--Tablea v
• •Theory
Integral (uocuooa
--Theory
Integral iranaforma
i
Intelligence teaU
--Development
•-Effectlvenea*
--SutiMical analyal*
Interferometer*
--Analyal*
- -Application*
--Dralgn
Interior balliatica
-Mathematical analyal*
465
468
434
181
568
802
103
46
IS
320
476
595
760
763
451
*93
774
77
465
77
78
79
187
449
78
763
774
77
319
760
761
686
39<>
394
576
156
340
197
70
306
447
IntermedUte frequency
tranaformer*
--Teat meihoda
' 47
171 331
171 322
171 223
171 206
171 207
171 211
171 314
171 215
171 317
171 318
171 200
171 201
171 304
171 308
171 216
171 203
171 202
171 236
171 339
171 241
171 243
171 345
171 224
171 225
171 226
171 227
171 228
171 231
171 340
171 229
171 230
171 232
171 333
171 334
171 335
171 342
171 244
171 346
171 337
171 238
171 364
161 948
153 776
150 243
150 748
171 118
150 319
149 739
152 431
148 535
153 313
154 098
171 687
150 061
148 735
150 634
153 066
149 396
152 100
152 109
150 993
152 108
150 466
148 693
147 121
147 588
153 486
154 871
150 883
152 972
153 211
150 994
148 006
148 007
148 018
153 294
152 471
152 714-4
152 550
152 351
152 732
153 299
150 679
r
Subject
lona (con. )
- -Chetnlcal reactlona
lona
--Intenalty
-Motion
--Oaclllailon '
- -fhyaiologlcal eAecta
--Production
--Scatterli^
--Source*
Iridium compound*
--Chemical reactlona
Iron
--Determination
--Impurltle*
--faitemal friction
-•MetaboUam
--hirlflcatlon
Iron alloya
-•Hiyaical propertlea
Ironbortdea
- -Magnetic propertln
Iron cry*tal*
--Mlcroatructurc
Iron laotcpe* (Radioactive)
--Meubollam
Iron-molybdenum alloya
- -Temperature factora
Iron -nickel alloya
••C^yaial atructure
- • Btoctrodepoaltlon
--Magnetic propertlea
Iron
-niMe atudiea
-Magnetic propertlea
Iron phoaphidea
- -Magnetic propertlea
Iron -vanadium alloy*
- -DIffuaion
--Magnetic propertie*
Uing lanlce
Subject
Pl
Jackaon polynomical
jahn -Teller effect
Jenny
Jet engine ftiel*
- -Combuatlon
--Contamination
--Impurltle*
- -Motaiure content
--Phyaical propertie*
--Temperature factor*
jet engine noiae
-Analyai*
Jet engine*
--Bihauat gaaea
--Lubrication
--Teat reault*
jet fighter*
•Pire control *yatema
--Performance
Jet mixing flow
--Analyala
--Mathematical analyai*
Subject
Kaehler manlfolda
Kantrowitz problem
Kaut2'* work
Ketone*
- -Bftecta of radiation
Page PB Number
699 149 065
3
348
800
688
607
720
144
111
612
331
776
21
201
150 943
152 789
154 371
171 600'
153 183
152 137
149 847
152 503
150 673
171045
152 691
154 453
152 640
152 074
612 171 045
337
789
796
153 277
154 364
171598
171 160
90 171 060
471
307
621
629
796
95
754
755
337
789
212
466
788
767
153 284
152 520
153 700
153 563
171569
150 850
155 239
155 340
155 341
155 243
153 277
154 364
153 391
153 381
154 103
161 577
Subject
^H'
PB Number
Subject
Pap
PB Number
Intermecalllc compounds
Ionization chambers (coo. )
--■ibllograpby
591
154 846
--Design
617
171 490
--Electrical propertie*
471
150 333
--Performance
99
152 677
--Electron tranaitlnna
309
152 406
Ionization gage*
--Mechanical properties
461
171 393
--AppUcationa
631
153 488
•
591
154 846
--Effectlveneaa
51
171 lOB
- -Phyaical properties
630
153 364
loooaphere
- -Production
69
171 081
-Analyala
31
148 256
- -Properties
793
153 923
283
152 697
- -Thermal properties
69
171 081
153 050
International Geopbyaical Year 33
148 267
415
153 484
34
150 417
558
153 399
,
231
151 377-6
559
147 532
'
258
148 494 .
--Arctic regiona
155
148 668
/
t
281
152 930
- -Elect rtSfnagnetlc
"
308
152 522
propertiaa
107
150 820
. ■
350
151 377-7
120
150 928
392
148 496
155
148 668
Interplanetary maneuvers
439
153 055
148 983
Invention*
149 062
- -Cla**lflcailon
807
149 523
156
149 069
Inverter drculta
•_
* 349
147 558
- -Magnetic effecta
Iodine
734
150792
350
414
152 963
150 071
--Fhoiolyai*
551
152 102
-•knixatlan
415
153 197
Jon beam*
559
153 698
--Analyai*
586
150 320
--Motion
156
152 471
--Application*
312
171 SOB
284
152 696
--Oacillatlon
790
154 460
- -Physical propertlea
57
152 200
- -Production
65
150 861
--Reflective effecta
155
148 668
419
152 319
298
152 823
- -Thermal effecta
419
152 319
298
152 834
--Thruat
6S
150 861
415
161 583
Ion bombardment
432
153 609
• -Application*
333
171 335
636
161 580
622
171 513
731
150 914
Ion exchange
••Wave transmtaaioi
155
ISI 361-2
- -Riyalcal faaors
29
152 132
349
152 466
--Theory
277
153 588
lonoaphere model*
34
150 452
Ion exchange realna
lonoapherlc diaturfaancea
-Applicationa
269
152 470
--Analyai*
432
153 498
•-Theory
277
153 588
--Greenland
336
153 279
Ion propulsion
313
171 30B
lonoapherlc acatter
297
152 9S8
586
150 320
lona
Ion rocket propulsion
310
153 587
- -Chemical propertlea
784
171 572
Ionic collisions .
436
153 636
P»ie PB Number
416
185
95
189
315
71
315
71
315
756
71
418
592
747
57
561
457
607
196
197
153 289
152 444
150 468
152 202
171 306
l«6 402
171 303
161 921
171 303
155 083
161 921
148 689
153 178
154 969
155 383
152 361
153 591
153 361
153 363
153 433
153 250
P«t PB Number
333 152 436
276 153 091
637 153 654
147
171 156
kmic current
--Mea»uremeni
Ionization chamber*
- -Calibration
Subject
Jet mixing flow (con. )
--Superaonic
characteriatic*
--Turbulence
jet plane notae
- -Phyaiological effecta
Jet (>rapulalon
--BlbUography
-•Theory
Jet pumpa
--Theory
jet atream* (Meteorology)
--Analjraia
- -Turbulence
Jeia
•-Acouatlc oacillatlon
•-Analyai*
--Control
--Deflection
-•Theory
••Turbulence
Subject i
Kidney*
--Blood circulation
••hthology
•-Phyalolony
298 149 736
259 148 495
Page re Number
195
87
770
140
64
65
310
586
64
63
711
30
31
413
747
607
195
159
778
86
171 179
152 357
150 866
152 363
153 155
150 613-1
150 613-2
148 777
154 104
152 153
150 964
148 395
148 262
148 363
150 691
155 149
153 838
171 179
152 786
153783
148 6*9
Subject
job analyala *
'--AppUcationa
- -Bibliography
--Effectlveneaa
--Paycbologlcal factora
jolnta
--Load dlairibution
--Vibration
Jordan arc
Jordan curve
journal bearing*
- -Hydrodynsmic
cfaaracteriatic*
-•Lubrication
••Theory
Junior
Jupiter
--Radiation >
Page
nNianber
261
152 783
683
148 313
6
171 075
364
153 no
537
153 855
538
153 854
264
153 110
393
153 853
717
154 654
589
171 556
185
152 372
600
153 710
177
152 145
442
153 128
587
15SQ01
IW
171 144
S3«
147 334
S3B
147 339
P»ae re Number
369 171 343
143 153 366
408 153 193
399 153 543
Subject
Kineplex converter
Klyatron*
--Performance
Kolmogorov teat
Pa|e
reNumbei
49
150 438
399
186
153 948
148 693
L4ibontoi7 anlnials
Latontonr wyilianeiic
■laljraU
-fkf^CMl propaniea
-TeM method*
-Teat reaulta
-ThBrmal pnvertlea
' theory
Laval
--Hi
LCAO
--CiTaial atructure
--MBianira tactora
aad-iaipinliti alloya
--Propntlea
--HaMOffannatlca
LaadMllurfcle
--Electrical properUea
-Aaalyala
-niyslalogitcal factera
-Soclokicical (acton
-Theory
«laMctora
M2
30
693
294
456
634
711
a04
455
456
606
770
75
69
75
75
75
75«
330
182
1«3^
1(4
757
lis
707
331
709
3B7
411
562
158
561
709
287
637
451
451
452
805
806
104
3S1
185
187
475
790
729
90
61
59
794
547
345
137
6
537
6(5
686
11
68S
11
687
9
205
576
Wttanher
135 374
155 375
150 207
155 576
153 489
153 104
153 103
153 668
154 510
153 092
153 184
1S0 3Z7
149 338
161 947
171 039
171 096
161 947
171 096
154 381
171 0*4
171 166
171 16«
171 174
171 175
171 176
154 719
148 715
150 489
149 739
161 914
161 91S
153 639
153 480
171507
153 494
153 583
161 915
153 629
153 875
isoaM-7
150 086-8
150 086-9
153 806
152 135
150 494
149 685
152 490
148 687
154 394
153 665
159 839
154 634
152 170
153 062
148 916
150 545
147 538
171 356
148 392
150 483
154 836
154 8r
154 838
147 902
149 904
152 HI
147 903
152 HI
149 334
150 542
149 674
171 3BS
Suhject
Pace FBNianter
LeainUic
-MachemaUc*! aaalyaia
684
148 756
149 521
150 372
- -Maaauroneni
7
135
171 146
--rhyalotofical iactora
11
6(7
152 101
154 593
136
148 300
685
150 433
- -Statlatical aaalyaia
7
150 178
134
149 962
539
171 545
--Teatmetbode
7
152 103
9
150 503
150 504
, — ■
,.r 360
153 460
538
148 169
153 497
136
148 728
- -Theory
539
150 904
684
149 522
Leaai aquarea
- -AppUcaciona
785
153 908
Lebeague integral
451
150 061
Laheacue theorem
188
152 430
Lee model
115
150 557
Lcfaodre (unctlooa
79
150 466
Leneea
- -Teat reaulta
13
152 001
LUaOB planea
-Electrical ayatema
560
153 933
Ueeqjaciooa
115
150 556
150 557
Liegroupa
318
152 606
Life auoDort (Aatronauta)
561
171 554
Subject
Page
Lift
--Analyals
LIgta
- -DIffractian
--Intenaliy
- -Meaauremenl
■ -Meteorological factori
--Physical effect*
- -niyaiolagical effects
--Folarizatiaa
--Reflection
- -Scattering
--Scattering (con. )
Light ranging ayatema
--Deaign
Llgfacnlng
--Electrical effecta
--Theory
Limit theorem
Limnology
-Alaaka
Lindbeig gyroacofw
principle
Line broadening
Linear accelerators
--Deaign
Linear equationa
326 153 196
792
413
727
792
413
337
266
277
739
71
109
154
277
558
620
624
625
793
38
158
706
621
761
175
467
301
153 130
153 682
155 330
154 530
152 682
149 654
153 326
149 631
171 686
161 921
150 628
152 552
149 631
153 566
153 450
150 f«7
153 123
153 757
149 096
149 0)7
152 350
152 384
154 532
153 916
154 133
413 153 481
171 157
153 392
153 393
152 662
Liquid rocket prope Hants (con.)
- -Combuaticn (con. ) ^
179
1 - 1 447
--AppUcationa
--Theory
187
184
187
150 793
152 160
148 672
761
147 904
Lip4da
-Metabollam
141
268
153 852
153 618
Liquid metals
- -Bibliography
--Surface lenaion
91
96
OTS SB-424
150 637
- -Thermodynamic
Liquid rocket propellanta
- -Combustion
409
64
161 990
152 039
66 148 264
-•Oorroaive effecta
-Handling
--Heat transfer
--Heat reaults
Liquid -solid cyclone
Liquids
--Atomizatlon
--Electrical properties
--Heat transfer
--Meaauremenl
--Molecular structure
- -Physical propertlea
--Raaooance
--Vaporization
-Viacoaity
- -Wave transmlaaion
Lithium
--PreciptutioB
Lithium chloride
- -Corroaive effecta
Lithium fluoride
-Solubility
Lithium hydride
--X-ray analysis
Lithium hydride -d
--X-ray analyaia
Lithium hydroxidea
--Apptlcationa
--Spectra
Lithium hydroaidea-d
-Spectra
Lithium iodide cryatala
--niyalcal prope rtiea
Lithium ions
- affusion
Liver
- -Blacbanilacnr
-EaBymea
-niyaiology
Locking materiala
Logarithmic inatruments
- -Deaign
Loglatica
--Mathematical analyaia
--Theory
Loop antennaa
- -Dealgii
Lopair
Loi«n
--Error a
Lo«\emperature alloya
- -Tenaile propertlea
Lo«r temperature baneriea
- -Development
Low temperature reaeerch
70
72
181
159
755
391
177
442
747
553
474
277
630
553
552
277
458
773
110
470
781
36
639
629
309
209
n Number
150 835
152 502
154 410
154 411
161 215
150 282
161 948
153 280
155 085
154 409
152 546
153 441
154 454
171^35
171 395
153 606
147 848
171 535
150 063
153 606
153 163
154 862
ISO 501
147 120
154 611
152 089
154 807
154 807
171 046
152 076
309 152 076
202
203
211
637
140
400
401
402
746
141
397
401
402
689
104
168
583
442
560
42
303
339
153
776
577
24
25
153 253
152 411
149 063
153 819
152 851
153 536
153 537
153 538
153 539
153 530
15(531
15(532
153 533
153 534
153 535
153 536
153 537
153 538
153 363
153 364
153 525
153 541
155 414
152 531
153 545
153 539
153 548
154 468
152 134
152 385
153 660
153 145
153 931
150 968
149 647
149 641
152 548
151 107
153 935
150 515
ISO 858
i
Subject
Lo* temperature
reaearch(caa.)
--Bibllagraphy
Pat PBNi
26
■— ! —
161 574
109
152 144
408
153 766
767 ■
153 906
791
154 457
801
171 618
802
171 619
753
CITSSB-4SI
(02
171 630
Subject
Lubricant addiilvea
% --Effectiveneaa
Lubricants
--Effects of radiation
--Electrical properties
--MaterUls
--nqraical effects
- -Temperature factors
--Teat results
--Testing equipment
Page P8Nun»ber
992
306
747
562
180
315
71
315
71
154 969
153 258
154 646
171 529
153 254
153 476
171 085
153 476
171 065
Subject
Lubricating oUa
--Sttirage
Lumicon
Lumifieacence
--Analyaia
--Meaatiremeiit
--Riyaical factors
Luminescent materials
--Applications
Lunik III
Lymph
--Electrical properties
Page n Number
715
534
440
617
341
553
440
154 671
153 452
153 316
171 491
152 731
150 895
153 492
171 992
>
•1
^
t
51
F^i WWumber
VI -4277
M-427t
MacMae ibop fracuca
Hii liliw translatica
— Blbttosraplqr
•liin lUojr*
--Corrc»»OB
--Fracture
Maoeslian cryatala
4fec«cture
kfti^X^iMD axidaciTMala
--BomterckiMal
--Oafonnatloa
7»3
7»7
744
4Sl
4S2
7U
766
•06
222
M6
3S1
MB
449
3B
747
74*
173
111
7SIX
613
6M
615
460
213
213
343
794
54
390
154*63
134 164
171251
isoat6-7
130 0t6-S
190<»6-9
130 0*6- 1
150 0t6-2
ISO 016-3
lS0at6-4
lSO0t6-S
ISO 016-6
152 135
OTS S8-439
153105
149 6«5
155 030
171 37«
153 165
154 646
153 694
149 670
150 673
153 924
154 167
155 297
150 502
153 167
149 6S6
ia671
149 6*4
150 55*
171 102
171 541
-daallo^
ira (Itaaatea
BtKXrlcal praf>crTlea
Tbamial propertlea
ic unpUflcra
-Ctxatu
MHiarir compounda
Ic corea
-AppUcatlcna
-MKvUla
cflalda
-Ccatrol
DawcUoa
Blactrlcal aOacta
Btocaana^adc effacta
ilaaalyala
-Rqratcal aftecta
-n^cal efhcta
acicn
iC materlala
-Cryacal atructura
profvrtlaa
-Spactropaiftlc aaalyala
MapMtlc modaa
Magnadc modulatora
--Orctaia
- -DwalOfRnani
- -Farformance
: platOD
190
323
111
20*
7*7
207
7**
210
344
20*
727
192
349
7*6
9*
216
799
112
754
9S
767
79S
111
212
344
337
52
430
S2
3^^gct
P»ae re hhanber
MilJMWIr racordlac ayatema
"AppUcacioBa 115 14* 710
^^ 739 154 Sa*
-DaatgB 565 154 296
730 154 814
--Eoulpmea 571 154 747
722 155 61*
Uc reaooaoce
— AkaorpUoa
--AoiUyaia
--Apptlcatlcaia
--Meaauremeoi
794 150 545
152 637
153 274
190 673
152 394
154 164
152 301
154 0*0
152 760
152*54
152 394
154 114
152 551
152 523
154 243
ISO 776
152 034
194 439
14*917
14*91*
14*919
195 239
155 240
155 241
199 243
ia23l
171573
190 603
193 291
192 462
192 923
130*79
193 494
190*79
190 aio
--Temperature (actora
--Thaory
MagDedc atarma
--Analyaia
Magnetic auaceptlblUty
- -Meaauremem
Magnetic upea
--DcvclopmeiK
--Teat reauMa
Magnettte
- -Cryatal atructure
Maywto- Iqrdrodynamlc
727 154 114
10* 150 378
149 152 4**
147 14* 679
149 14* 67*
29 192 0**
27 150 539
lOi ISO 432
113 150 443
19* 152 lOS
210 152 094
212 152 450
409 147 776
410 149 64*
552 150 063
6X 147 84*
795 1S4 062
701 150 133
19* 152 106
33* 152 86*
106 150 933
11
S69
293
553
153 836
553
153*36
- -Analyaia
47
146 730
— AppUcadona
570
171542
a
130 67*
--BlbUograpiiy
96
-130 46*
1 —Mathematical
47
146 790
-•Propagatioa
SO
149 773
*1
150 4*4
"THaory
alyala
Magneto- Ionic duaa
Magneto-optic roiadoa
--Meaauremem
--Theory
Ma^Mtogaadynamlca
Magnetometara
r-Dealgn
* - Deve lopvneni
--StaUUzatlon
Magitrrnalarinrr effect
MagiMHililiilni
--Theory
115
116
124
216
346
609
633
443
64
312
116
192
473
114
346
*5
607
*ao
390
20*
2
210
*ao
207
105
52
602
466
626
Magnetoatrlctlaa craaaduccra
--DealgD
Magnerron guM
Magnetrona
--DevekjpuiaaA
- - B lectr oroagnetlc
propertlca
«a
-Daalp
-Matarlala
41
966
719
49
92
162
169
ft3
33*
432
7r
794
755
770
almenance
--Arctic regla
52
150 537
154 296
171 194
112 150 633
147 7*0-4
147*3*
149 067
152 419
152 742
153*35
152 656^
152*30
150 777
152 749
OTSSB-426
152 445
153 074
152 67*
152 912
150 630
153 262
155 333
152 963
149 909
149 007
152 549
155 323
152 301
150 927
150 931
149 333
150 695
154 095
152 140
147 49*
153 777
152 309
ISO 4a
152 338
14* 276
149 630
153 960
150 699
153 309
154*64
155 339
155 340
155 241
155 242
171 604
392 193 947
Sublect
MalKeaaacc (con. )
-BtbUography
-ScfaaduUng
Maintenance equlpmem
--Development
- - Ufe expectancy
Maimenaoce peracnnel-v
--Performaace
--Te« methoda
- -Training
- -Training devtcea
Majority gate
Majority prlndpla
Mammala j
--AUaka |
Management engineering
fae
n Nianber
-Thacry
I
Manga neae
-- Deter mlaatioa
--Bconcmlc aapecta
Manonctara
--Dealgn
Many particle ayatama
MaPt*"*
--Equipmeiii
Mapa
--Preparatlcn
Marine biology
-Pacific Ocaaa
Marine borera
--Cooirot
- -CoiBitermeaaurea
Marine meteorology
-Pacific Ocean
Markera
--Deterioration
Markov chalna
MarkD* proceaaea
-^
Mara
--Exptoratlon
--Reflective effacta
Martenetron
Martenalte
--Cryatal atruaure
--Deformation
--Internal fricdon
Maaklng reaction
Maaonry
Maaa energy relation
Maaa apectrometera
--AppUcatlona
--Dealgn
Maaa cranafer
Ma at cella
Maater alave manlpulatar
Maatlcatloa
-Analyaia
Materlala
— MbUography
--Dafcrmatloo
--Development
— Paague
--Fracture
•-Friction
— Handbooka
--Heat craaafar
I -
533
750
173
619
ft
au
an
173
^3
135
*1
*3
22
279
588
748
749
479
63*
111
418
127
557
707
33
283
692
703
283
75*
6*
716
758
706
1*2
77
7*
:»
7
77
30*
2
95
95
7*0
77*
51
163
566
13
590
117
442
147
276
46*
457
19
5
690
65
222
417
752
76*
428
95
776
469
5*9
39
157
417
60S
171 51*
153 756
171 137
153 149
153 142
192 7M
192 7*3
171 137
153 779
152 165
130 4*4
150 973
150 575
153 343
149 159
148 787 —
149 0*8
153 148
154 433
150 673
147 534
152 873
152 493
153 886
150 489
147 175
152 907
150 654
148 079
148 426
154 661
150 954
154 668
154 650
154 566
14*727
152 106
152 3B9
149 717
153 35*
151171
150 521
148 756
152 939
150 741
171 066
150 850
154 553
154 453
ISO 736
149 720
153 250
152 002
171 107
147 90*
150 719
152 679
152 770
150 700
153 315
150 856
152 300
154 363
150 613-1
150 613-2
171 005
171 372
171 612
148 813
150 709
171 0*4
155 153
171 474
171 494
171 064
171 147 ,
171 372
153 56*
SublMX
Page
PB Niinbsr
Sublea
Page
reNumber
Sub^MS
Page
FB Number
Materlala (con.)
Matliemaucal computera(can. )
Mattreaaea
--Magnetic propertlea
95
171066
--Equlpmeia (con.)
190
153*637
--Materlala
143
153 010
--Mechanical propertlea
178
150 392
.
333
153 374
Maximation
79*1
147*44
- -Military requlremeiaa
752
155 3*1
568
149 090
MC-3
709
153*61
--Phyalcal pi'bpertlea
58
161 093-9
765
150 0*6-1
MD-1
464
153 50*
--Propertlea
551
171 497
766
150 0*6-2
Meaaure theory
It*
152 430
--Quality control
764
14*535
150 0*6-3
'
322
152 737
--Retractive propertlea
701
154 518
i
150 0*6-4
760
149 165
--Soreaaaa
104
152 134
150 0*6-5
Meaaurement
460
153 077
150 0*6-6
-- Inner umestatiaa
581
153*36
1
519
153 661
767
153 785
72?
194 114
1
776
• 155 1S3
*07
147 787
Mechantca
-.-Tamperaiure factora
740
155 148
--Error a
190
152 465
--Theory
603
14* 346
753
OTS SB-451
602
149 333
768
153 124
--Tanalle propertlea
603
14*346
--Handbooka
82
152 651
Mechanica (Peraoonel)
--Uhraaonic analyaia
445
171 1*6
--Human engineering
323
153 59^
--Teal methoda
262
152 756
Mathematical computer dau
153 597
Medical cameraa
--Codliv
78
ISO 509
-Mathematical analyaia
601
153 10*
400
153 303
80
150 992
- -Operadoo
82
161 566
Medical reaeardi
138
171 000
1
82
150 599
765
155 376
-AUaka
18
ISO 214
•
190
152 468
152 638
--Fufut iiiaace
81
150 484
171000
--InatrumentatiaB
Membranea
189
,148 290
,
191
152 345
83
150 973
-Vibration
759
14*420
•.
324
149 297
• 1
189
171 144
335
171 341
--Reliability
765
154 0*7
--Analyaia
9
' 150 369
438
152 974
--Scheduling
39
171040
ISO 975
■
597
153 062
79
153 049
540
153 403
600
132 587
80
148 359
--RiyUologlcal faaora
6*7
154 593
767
161 577
82
15050*
9
150 SOS
-•Procaaalag '
1*9
192 202
150 599
150 504
190
190 795 ■ '
171 100
394
153 287
%
191
323
152 989
153 596
s
1*9
147 643
14*60*
Menex
Merchant veaaela
533
171 518
153 597
191
14*733
-ScheduUng
442
153 145
391
152 827
14*733
750
153 756
438
153 220
■■
14*734
Meaomerlc charge aeparaticn 27
150 539
*
451
153 560
14*735
MeaometeorologicaJ analyaia 151
152 2r
767
154 5*7
222
149 673
Meaometeorological network 412
153 232
191
14*735
258
171 196
Meaona
Mathematical coraputera
307
152*45
-Decay
332
149 733
-AppUcatlona
33
150 487
330
153 894
149 737
53
150 764
•
321
153 063
464
150 694
. 55
152 183
323
148 609
--Determination
133
153 210
60
150 799
153 733
--Nuclear reaaiona
204
153 483
82
171 100
' 443
153 181
333
153 911
■
*4
ISO 100
451
153 002
464
ISO 694
135
152 164
586
154 067
616
153 032
,
162
148 711
588
153 562
618
147 306
193
152 555
636
153 681
-- Polar izatioa
332
149 737
234
148 723
73*
153 866
--Production
9*
150 937
263
152 703
763
155 0*7
«
61*
14*154
,
413
150 060
783
154 361
--Scaneriag
202
153 434
1
414
153 134
--Simulation
' 83
ISO SO*
632
153 186
' ; •
440
152 689
554
153 667
--Theory
462
153 309
451
150 0*6-7
"Theory
80
171093
Metaboliam
\
150 0*6-8
189
153 519
- -Climatic factora
14
150 568
452
150 0*6-9
334
171 339
15
ISO 572
479
161 586
601
171 548
16
150 213
601
153 485
806
150 726
150 577
710
155 235
Mathematical logic
331
152 723
150 578
72*
150 906
*06
150 726
17
ISO 230
■
735
154 507
152 135
150 564
1
769
155 578
--Ap^caUona
190
149 652
18
ISO 576
767
153 930
333
149 673
266
153 341
— CaUbradoB
100
152 358
763
152 957
153 351
•-Clrcvtta
70
152 351
767
148 231
267
152 695
*1
153 045
--Theory
76
152 063
268
152 618
190
149 652
Mathematical prediction
269
153 344
299
152 750
--AppilcaUona
335
153 070
402
153 366
-
452
153 206
440
153 492
6*8
171606
601
171 555
--Theory
450
150 714
21
152 640
767
153 906
Mathematica
322
171 006
693
154 592
-DMi«l
•0
149 359
MatMeu equadon
599
153 673
--PntholoKy
142
152 367
*1
150 649
Mathieu (uncQona
763
154 961
545
153 191
*2
150 59*
764
154 960
690
153 720
1-
161 565
Matrix algebra
S3
>S0 599
Matai boridea
1
1*9
14*290
187
148 6*7
--Cryatal atructure
214
152 493
190
14*3*1
33a
153*94
152 454
-
324
476
149 397
153*76
5^
S97
153*33
153*34
Maul carbldea
152 455
764
149 13*
.--AppUcatlOBa
173
14*3*3
- -Chemical reactlona
144
192 92*
82
130 767
18*
153 167
Metal carbooyla
95
171066
191
14*733
--Chemical propertlea
696
195 453
190
150 603
14*733
Meul chlorldea
1 ,
207
153 320
394
149 637
--Thermodynamic
452
153 361
450
150 711
propertlea
69*
194*72
601
150 073
575
153 334
MeulUlma
154 422
--Thaory
594
153 144
--AdaorpdOB
7*6
150*64
765
171 29*
596
153*31
--Opdcal properdea
794
150 642
80S
153*06
•
599
153 133
--Producdon
46
152 360
SO
150 601
153 554
--Reaiadvity
171
149 660
1*9
132 213
11
763
155 0**
--Thlckneaa
799
192 1*0
190
152 46*
S3
r '
-*
nNimber
page
PB Nwnter
ShHmx
pap
m
Metal -fJaas aAMlTM
Mecala(CDii.)
Meteorology (con. )
-AppUcKMW
IS*
1S5 2S9
--SUvaaea (con.)
460
153 077
- -Tropical regiooa
279
149 668
Ueulitmm
462
161 896
152 613
"Ol— Inl rMcdoaa
6*9
153 844
614
154 818
Meteor a
-■Hy*o<y1«
3S-.
150 335 •
171487
131
152 212
MMil-ptoadc adiMlvm
r.'
768
154 958
- -Elearomagnetlc
,
"DvMlofnMal
753
171 5«S
--Surface propertiea
199
152 147
properties
570
153 818
— MMarlaJa
0«
161 863
786
150 864
--Reflective eflecta
635
161 587
— TMtrMtiks
589
171 556
--Surfacea
--Temperature tactcra
201
458
171 150
153 929
--Velocity
Methyl amlnea
131
152 212 1
"IMklgraflq'
453
171 374
611
154 340
- -Exchange reacticna
147
148 679
--Sbraaaaa
93
171 082
--Tenaile propertiea
776
151 107
Methyl haUdea
— TMlmuJra
5«3
153 551
--Teatlog aquipmem
63
150 868
--Speara - -
552
153 549
-VltaMtCM
•3
171 071
611
154 340
Metbyl-d-haUdea
602
153 794
"Thermal propertiea
218
171 183
--Spectra
553
153 549
711
171 594
219
171 185
Methyl hydrazinea
Iftatamc ci7«aU
--Thermodynamic
-Deter ml nail on
755
154 716
— Ml^Mc propeTTlea
95
150 467
propertiea
804
171 567
Metric spacea
332
152 736
111-
150 468
150 541
--X-rajr anaiyaia
Meteor
620
89
171 sr
152 356
Meyer-Peter -MUller
609
154 339
--Ukrmwnlc prcnrtias
MKalMcaoaps ^
I09-*
153 144
Meteor turat
635
161 587
Michigan
222
149 673
Meteorttea
-
369
152 605
"PkOdUCttOM
aot
171 150
--Detactlon
34
148 257
306
152 536
MMBOvgr
65
ISO 613-2
--Simulation
175
152 380
413
152 663
--WtafrMiy
777
OTSSB-452
crrsa-454
Meteoroloflcal balkxaa
152 381
625
707
153 456
153 915
--USBR
329
171 307
--AppUcatlona
34
152 189
802
154 506
Mwilor^nlc compouida
258
148 494
Micro-module .
54
171 136
— IMtavrepkjr
23
171097
259
148 495
55
171 125
"GhHitcal propertiaa
696
155 453
393
148 496
MicroelectroBica
53
161 890
"DM—poHdon
23
171097
- 560
153 643
Mlcrometeorology
- -ftlly^ieTl iKlcn
145
150 485
--FUght paUia
280
152 699
- -Instrumentation
30
152 273
-rnrrnnn
551
171 522
— MaterUlB
757
150 844
34
148 257
— apKtra
696
154 262
758
150 845
: 1
153
152 148
--ay«heat«
406
153 265
--Tracking
411
150 705
153
152 149
,
696
171571
Meteor ologlcal tatter lea
704
148 233
Mania
--Taatlag equipment
42
152 192
--Waahington
151
152 569
--Adnrptive pro^aniea
401
152 685
Metearolog;lcal charta
Mlcroorganiama T
--AvaliabtUcy
329
161 236
- -Anaiyaia
HO
lis
152 563
-Inhibiticfi
71
146 402
HiwIwi itiifil
622
1^1 513
--AppUcationa
151 361-2
-Ftiyalology
33
147 175
— taBikv
6a
161 863
--Nonbern hemisphere
281
152 930
-Viability
270
153 573
--CoadBg*
69
171057
--Prej^ratlon
31
150 867
Microphones
--CcmbiMkB
635
154 842
- -Production '
556
153 608
--Deaign
296
152 603
--CorreMia
14(
152 127
isi
150 388
Microradiography
2B
171 344
Meteoroiaclcal dau
412
153 232
--Applications
461
171 381 .
331
171 301
--Anaiyaia
82
161 566
MIcroachmldl
259
153 278
--CorroaiaB prevenUon
581
154 757
--OreenUnd S
280
152 952-1
Mlcroacopea
\
—Creep
63
150 868
152 952-2
-Oevelopmeat
209
148 681
199
152 147
707
153 715
Microocopy
614
171 487
280
152 952-1
--Applications
796
171 598
-•CMormaclon
301
171' ISO
'
152 952-2
Microapectrophcianietera
330
153 882
^
70S
154 163
--Deaign
209
148 661
--CMffuaka
199
148 675
154 376
Microwave ampllflera
344
152 683
"-Nortbera hemiaptaere
31
148 263
--De*gn
47
152 US
;
446
171 400
"Prooeaslag
279
152 906
433
147 243
4S9
171 025
--Raoordiiig devicea
30
152 273
--Development . ,
42
152 194
20S
153 258
280
152 699
51
150 736
f
619
171 523
--SMtlatlcal anaiyaia
31
152 060
54
150 446
' --BiKtiical propertiea
95
171066
278
152 701
163
149 730
f
629
154 770
280
153 064
300
152 995
^ --BlactrocheinlKry
610
161 235
281
152 769
432
153 240
--Btocxron traneiclcna
215
152 179
-•Sarltzerland
34
152 066
433
147 244
— PaUfue
94
171099
— Tahlea
31
148 256
■
150 716
95
171064
154
1^061
434
153 446
^ --PncMre
330
153 882
380
152 952-1
*'
566
153 2S0
459
171 366
152 952-2
■
570
153 268
i
604
153 856
--Theoretical correctiani
149
152 042
571
153 937
776
155 153
--Tranami salon
278
152 684
153 936 .
"Piicao»
90
150 952
Meteorolo(ical inatrumemi
577
153230
--HoM treaoneri
330
161 213
--Arctic regtona
31
152 070
718
155258
777
CITSSB-454
--Calibration
149
152 042
. ■
722
154 501
"LflMl dlaix llMICiaQ
604
153 856
--Ykeatgn
707
154 528
154 502
--MwMiUf
313
161 225
--Oevelopmenl
30
152 195
723
148 323 '
— MKhntcal profiertlea
201
171 ISO
705
154 532
--Teat reaults
SI
160 683
329
171 198
Metadroioglcal radar
301
152 847
611
154 340
--AppUcaticna
30
150 420
--Appilcatlons
727
154 589
614
154 818
ISO
152 206
-Calibration
2«2
171 204
—MlcrtMtnicnrc
201
152 074
152 307
-Deaign
l»7
IS3S90
461
171 381
280
152 774
435
153 342
— rhralcal propertiea
58
161 093-5
334
152 661
579
153 244
--ndtiii«
610
161 235
43>
153 498
--Dawelopment
165
149 734
--ProoaMii^
m
16129)
784
154 706
214
153 561
■161 221
- - Dtvelopment
411
153 394
293
152 581
329
153 109
-•Bflectivetieaa
412
153.239
421
133 001
444
171 379
--Equipment
566
153 250
--Maierula
297
153 660
-rtatKilm
329
23
161 236
171097
Meteorological radar
(Airborne)
- -Radiation
306
619
153 226
153 8S8
/
i
301
152 074
--AppUcatlona
29
152 193
- -Teaiing equipmem
167
152 241
i --RadtairaiMc analyata
461
171 381
Meteorology
31
150 617
Microwave optica
165
149 734
1 -MMWy
23
171097
--Alaaka
ISO
A52 290
219
153 255
749
171 112
-AaU
279
149 668
--Thaory
jot
190 415
433
151 101
152 613
306
152 301
459
171 366
--hdflc Ocean
279
152 613
■
■
^H
■
\r
Std>J«ct
Page PB Nianber
Mlaalle antennaa
Pap
F8 Number
Sirf^ecl
Page
FB Number
Microwave oacillatora
MoMle holata
--Deaipi
55
50 492
--Deaign
303
149 647
-Teat reaulta
746
154 660
- -Daveiopmett
300
52 995
Miaaile banenea
61
171 114
Modulator tubea
>
571
53 937
Miaaile booatera
-Deaign
723
154 313
722
54 501
-MaterUla
316
153 630
Modulator a
54 502
Mlaalle fuzea
-ClroMU
421
153 004
Microwave preaelector
41
SO 681
--Deaign
583
153 487
733
154 213
Microwave apectroacopy
Miaaile launchera
-•Oavelopment
421
153 001
-BiMiography
624
54 113
--Performance
57
152 122
733
150 109
- -Inatrumentatioo
623
50 701
436
153 161
Molecular aaaocladon
Microwavea
578
54 190
737
148 216
-Energy
86
ISO 346
733
54 196
Miaaile noaea
278
149 659
54 199
--Coatings
771
154 815
456
153 106
--Anenuatlon
423
71234
Miaaile peraonnel
547
153 686
i
71225
--Training
261
152 580
- -Mathematical anaiyaia
112
«/M«f"
i
71226
537
153 288
Molecular beama
180 535
f
71 227
Miaaile tracking syatema
739
153 647
--AppUcationa
703
171228
-Handbooks
361
152 580
786
149 540
--Detection
110
52 310
Mlaalle trajectories
--Reflection
337
152 882-
--Phyaiologlcal efleaa
143
48 277
--Determination
737
153 731
TM
»4 457
--Propagation
220
52 653
--Mathematicaj anaiyaia
736
171 248
— Scattering
ttl
■.J63 768
475
71 377
--Recordliv devicea
174
150 798
--Snurcea
195
-152 504
574
50 896
--Simulation
582
154 970
Molecular cryatala
409
150 921
579
53 243
Mlaailea
Molecular rotation
. 621
53 732
- -Aerodvnamic
--Anaiyaia
624
147 775
•-Reflect] on
790
54 631
characteilatlca
436
153 425
- -Microwave apectra
791
148 563
--Refraction
283
52 951
582
154 970
--Theory
792
149 567
635
71 544
--BibUography
479
152 978
Molecular aleve
309
171 051
MIL-C14157
203
48 979
--Control ayatema
582
154 970
Molecular apectroacopy t
1
339
152 863
Military ctietiUcals
736
171 249
436
153 636
--Hazarda
691
53 843
--Deaign
736
171 247
J
552
152 612
171 248
y
791
148 935
--pireaorlea
174
61 53S(Rev
0
171 249
154 092
- -Human engineering
5
48 319
171 250
794
150 642
--Preaervatlon
73
50 962
--Drag
306
153 068
- -Mathematical anaiyaia
624
153 637
Military fadlitlea '
--Electrical ayatema
58
149 547
Molecular structure
693
153 903
- -Cooling
736
54 626
309
149 704
--Mathematical anaiyaia
790
153 655
--Conatruaion
1
71 106
584
153 944
153 639
Military operationa
--Equlpmeia
48
150 678
--Theory
339
149 MO
-Get^aphlcal tactora
32
50 766
,
174
161 535(Rev.l)
152 663
Military peraonnel
393
53 440
580
153 613
624
147 775
-AUaka
310
393
53 339
53 323
-
153 616-1
153 616-2
Molecular weight
791
154 092
53 329
582
153 614-1
- -Deter minatioa
406
171 401
--Arctic regiona
397
53 373
153 614-2
Moleculea
--Nisrltlon
310
53 339
153 615
- -Adaorptiefe-—
406
152 665
--Performance
398
53 469
584
153 612
- -Chemical reactlona
149
161 406 S-1
--Selection
6
SO 483
153 617-1
--Diffusion
146
150 781
--Training
683
53 865
153 617-2
699
154 536^
Mlbtary reaearch
121
52 146
*
712
153 611
--Electron tranaitions
624
153 637
138
71000
736
153 870
702
148 473
144
71001
739
154 289-3
--Energy
276
153 091
r
157
71004
~*
740
154 290-1
554
153 114
t
306
71002
155 148
--Icnization poteiKlal
467
153 397
206
71003
741
154 290-2
- -Motion
28
150 170
222 1
71006
--Fuel injeolon
756
155 256
66
130 346
477
33 927
--Guidance ayatema '
175
171 157
194
148 694
Military auppUea
736
171 250
607
153 426
--Storage
183
48 7r
--Hydrodynamtc
773
154 156
Military training
charaaerlauca
57
152 122
--Vibratlan
624
153 637
->Effectiveneaa
6
52 142
436
153 161
S
791
153 062
393 A
S3 779
737
148 216
792
149 567
134 '^
49 962
--Insulation
802
150 243
MolUer dlagrama
311
153 791
--Standerda
683
53 865
--Maintenance
173
171 137
Molten carbonatea
410
147 045
Mint
--Materiala "^
58
161 093-S
Molten aalts
553
171 535
--Radioactivity
22
61 371-8
92
151 096
Molybdenum
404
61 371-10
199
151 072-R
-Casting
458
151 098
692
61 371-11
458
161 229
--DeformatlOD
781
ISO 006
693
61 371-12
779
151 104
--Fatigue
754
171 617
Mlllatone Hill
438
53 220
--Performance
736
171 247
--Physical propertiea
613
151 099
Minerala
--Reliability
580
154 811
Molybdenivn alloys
- -Chemical anaiyaia
794 1
48 781
--Rockni propulalon
736
171 249
- -Mechanical propertiea
775
171 597
--Polymer phi am
470
47 173
"Safaty davicea
61
150 626
-•Riyaical propertiea
613
151 099
Miniature electron tubea
"Simulation
601
154 806
--Thermal propertiea
445
171 390
169
48 276
--StablUty
306
153 068
Molybdenum CKldea
Miniature electronic equipment
--Telemeter syatema
45
150 318'
- -Crystal atruaure
797
153 721
- -AppUcatlona
690 1
54 263
583
153 487
Molybdenum-titaniian alloyi
-Clrcidta
54 1
71 136
*
730
171 690
--Phyaical propertiea
458
161 229
55 1
71 125
f£
153 890
Monotone retracta
188
152 543
298 1
52 672
--Teat fadlitlea
152 802-1
Mood diatributlon
76
171 078
427 1
71 380
1
152 802-2
Moon
--Deaign
296 1
52 603
1159
153 280
--Explaration
4
150 933
53 1
61 890
.
172
171 134
ISO 934
293 1
52 922
--Teat methoda
740
155 145
ISO 935
556 1
53 888
"TracklBg
1 58
150 329
150 936
719 1
50 849
174
150 797
2S7
152 846
731 1
71 566
152 063
"Mottna
2S6
171 196
- -Human engineering
682 1
54 522
436
150 070
--Fhyaical eftecta
737
153 947
Mini max
78 1
50 600
Mltochrome
16
ISO 441
-Reflective effea a
2
190 451
Mirrora
669
154 468
349
152 466
--Electroforniing
313 1
53 883
Mixturca
--Surface canditiona
622
171 513
--Preparation
341 1
71 191
--DItrualon
148
148 676
--Surface propertiea
2
1S0.4SI
--Reflective eftecta
786 1
54 243
- -ThermtxlyTiamlc
propertiea
634
154 755
Moon rocket
37
152 315
55
Hm WNi—b
Morse pcie«U)a
Motion meter
■•AmYflB
Motor raactlona
r kctors
SS4
746
3S2
3*6
177
363
394
t
10
153 114
154 676
153*97
152 au
153 oas
152 744
153 sa
152 OM
150 63*
Motor torpedo boat*
- -Hydrodynemlc
cteractaiiMca
--WjroBlag
Movinc target lodlcatara
-TDevclopoaat
• •Bqulpmeit
--Hiimaa enftneerlng
--HyaU to aoiaa ratio
ffe n Number
62 1S2797
32 ISO 766
Subjact
Page PB Number
162
556
171
49
141 711
153 an
153 006
150 5*3
MuMpath tranamlsaloD
--AppUcatlona
- -Couuermeaaurea
^ --Mathematical analyala
Muaclea
--Mechanical profiertlea
2M
164
48
42«,
575
542
152 964
152 226
150 796
153 225
153 S9S
171 495
_, r
»■ *• '
' •' !
V
h
\
»!*<•«
PligC W NuBubw
NA 39
Narol
Naval a(knli>l8tratlaD
Naval avlatloo
"Training davlcea
Naval e<|ulpmem
--Effectlveneaa
--Shock reaiatancc
Naval loglBtlc*
Naval orckiance
--Teat fafllltlea
Naval peraonnat
--Aathropomaciy
--job analyala
--Organlzatlda
--Performance
--Selection
--Teat methoda
--Tialfllng
Naval procurenMst
Naval reaaarch
418
153
752
260
716
441
750
Naval reaerve
Naval ahorc eatabliatonenta
--CUm
--Water ai^y
Naval atructural mechaalca
Naval auppUes
--Quality control
Navler-Stokea e<juatloaa
--Paychologlcal eflecta
- -Paychologlcal factora
Neel temperature
Negative lona
Negative realatance drculia
Nacxiymlian
Neoplaama
--Production
--Therapy
Nervoua ay at em
--niyalolagy
--Stlmuladoo
Neurlator
Neutron bombardment
--Phyalcal efleaa
Neutron counter*
--Power sifipUea
Neutron croaa aecUoBa
--Analyala
--Tablaa
Neutron deiaaora
--Dealgn
- -Materia la
Neutron diffraction analyala
--AppUcatlona
Neutron fluxea
- -Mcaauremeni
--Spectra
Neutron meter*
- -i>evak)pnaei>
Neutron apactromctera
--Dealgn
Neutrona
--Energy
;lc
536
536
6
537
261
683
536
663
6
41
135
393
750
123
224
352
480
639
806
80S
261
781
5S5
742
452
752
457
759
538
10
470
204
348
48
615
746
144
11
S270
271
689
8
767
446
617
618
782
783
7*3
794
471
333
784
617
783
202
203
471
782
616
153 404
152 S48
155 381
149 642
154 648
149 5X
153 756
308 153 867
153 489
148 555
152 136
154 836
154 837
152 626
153 746
153 604
148 774
152 142
150 160
152 164
152 16S
153 779
153 756
161 288
171 314
171 315
171 316
171 317
154(01
171 318
152 626
154 641
153 610
154 642
147 401
155 381
153 4S9
149 534
153 ISO
150 852
147 759
152 133
152 137
150 806
150 6*6
I
155 566
152 570
150 216
153 349
153 330
153 390
155 2*7
152 098
153 785
153 439
154 753
153 140
155 324
171 130
171 134
171 616
155 254
150 642
152 982
153 790
155 323
154 428
154 429
154 4»
155 254
153 253
152 411
152 982
153 863
148 159
ea*
g6
Number
Neutrona (con. )
--Motion
--Nuclear raacdoaa
--Rathoioglcal effecta
- -Penetration
--Riyalcal effacta
- -MarlxatlOB
- -Production
--Reflecdan
- -Scanerlng
--Spectra
Newton methtxl
Newtonian theory
Nickel
--Adaorpdve propertlea
--Bonding
--Cliemlcal reactiona
- -ElearcdepoalUon
--Impurltle*
--Ma^Mtlc pro|iernea
--Phyalcal effecta
-no-lflcatlon
- -Spectrographlc analyala
--Streaaea
Mcfeel alloya
--AppUcatlona
' --Development
--Mechanical propertiea
- -Temperature faaor*
Nickel nima
--Mapieac propertiea
--Reaonance
Nickel ooddea
--Riaae atudlea
Night night
- -Vlaual (aaora
Night aky
- - LumtneacetKS
Night telendon
Nlmonlc alloy*
Nlobe ji
Niobium
--Caaiing
• -Cnatlnga
--Wakliiv '
Niobium alloya
-Fhaae atudlea
--Welding
Nlotaum compounda
--Fhaae atudlea
Nltratea
- -CSiromatographlc
analyal*
- -nfa'^l'V'^*' affecta
Nitric acid
- -Analyala
--Slorafa
Nltro compounda (Organic)
--Detonation
Nltrocelluloae
-Prooeaalng
Nltrodtpbenylamlnea
--Spectrographlc analyala
Nltrofen
- -Chemical reactiona
- -Determination
--lonizatlan
--MetaboUam
--Spectra
Nitrogen (Liquid)
--Thermodynamic
propertiea
Nitrogen fluorldea
-MbUography
- -Chemical reacUooa
Nitrogen lona
--Determination
Nitrogen ootldea
- -Oiemlcal reactiona
--Clarroatve effeatt
--Production
--Speara
Uta
632
404
782
97
98
98
620
98
333
464
197
306
27
331
704
313
211
112
75
94
Jll
331
295
723
610
309
198
621
789
470
154.
61fl
MO
458
591
\m
91
198
991
694
687
560
607
17
622
545
I ^
756
590
331
560
108
309
147 900
153 186
153 189
153 301
155 324
152 000
190 406
190 776
154 812
190 406
149 732
171397
152 492
153 0S8
150 536
152 880
153 662
153 883
152 434
-1« 917
148 918
152 294
150 280
152 434
152 880
152 735
154 450
161 234
153 063
161 323
148 349
148 757
147 759
366 153 336
148 718
161 968
161 234
152 987
151 098
161933
171 159
161 319
161767
161 319
161933
171 159
154 210
148 966
171 115
153 948
153 949
97 150 664
{.«. 150 456
583 153 857
153 567
153 183
150 567
153 807
153 191
153 282
150 282
171 252
154 251
410 153 356
153 764
171 901
153 567
150 096
148 712
ia716
Subjeg
Nitrogen ocycfalorldea
--Decompoaltlon
--Fhotolyal*
Nitrogen oxyfluorldea
--Chemical reactiona
NItroua add
--laocnei lam
Notae
- -Mathematical analjrala
--Fhyalologlcal effecta
--Reduction
Nolae (Radar)
--Analyala
Nolae (Radio)
•-Analyala
--Mathematical analyala
--MeaauremciK
Page PB Number
--Reduction
--Sourcea
--Statlatlcal analyala
Nomographa
--Preparation
Non-deatructive teating
- -AppUcatlona
--Development
--Equipmea
Nan- linear differential
equatlona
--AppUcadona
--Theory
Not epiiiejilii Ini
-- Deter minaUon
Noczlea
--Aerodynamic
cfaaraaeriatica
--Deaign
--Model teat reaulta
Nuclear pfayalca
--Study and teaching
Nuclear power planta
--Greenland
Nuclear propulaion
--Analyala
--Economic aapecta
--Theory
Nuclear reactiana
- -Analyaia
-Energy
-Mathematical analyala
Nuclear apectroacopy
•-AppUcatlona
- - Iniatr umantatlon
Nuclear aplna
--Danalty
--Energy
--Meaaurement
--Reaonance
28
550
549
762
140
744
727
60
573
594
727
3P2
622
120
221
3S0
436
566
806
49
571
734
432
568
186
69
309
418
586
445
741
742
193
542
187
320
595
694
158
417
158
4
462
615
97
442
462
443
101
103
783
203
98
98
202
204
333
633
463
310
203
547
790
791
35
107
153173
150 627
153 764
153 061
153 957
147 529
153 252
155 253
152 965
150 799
152 970
153 600
152 965
153 576
153 577
153 804
151 3n-3
151 377-4
151 377-5
151 377^
151 sn-7
153 400
153 599
151 377-8
150 438
153 937
148 398
153 169
153 999
148 691
171 067
152 988
171 408
171 499
171 186
155 0S9
155 061
155 063
155 068
155 060
152 360
171 495
148«f»S
149 730
154 768
154 364
147 374
154 292
147 374
148 360
152 866
150 696
152 233
560 153 93)
150 719
1531407
152«30
150 516
152 644
153 862
149 700
152 0S8-1
152 068-2
152 424
161 584
152 482
171 163
149 733
153 185
171 402
152 094
150 860
153 814
L53 828
153 829
153 207
152 088
150 429
150 431
Hge WNwBber
NuetMr airtaa (coi. )
■-mmomncr (cam.)
107
itesao
1«
130 374
.-.
150 432
303
ISO MO
634
147 775
Nuct—r Kructure
flwwi iiitiiihiiii
7«4
130 171
"tlMhnMlcal analyala
7M
153 1«7
NueM
303
149 700
inimii T 1'
344
ISS'SM
— Hmd-ob croM MctJaM
6ia
133 140
PH* l»N>»ber
Nuclei (COB. )
-RadloKdvlty
303
150 SAO
--Spectra
633
153 189
Nuclei (Blotocy)
-SumuJatlca
397
153 468
Nucleic adda
- -Analyaia
369
153 740
141
152 532
NucleoMdea
--Spectra
544
153 355
NucleoUdea
- -Chemical reactlOBa
689
153 844
544
153 3SS
ii^^eg .'-'':
Pate n NienfacT
Ntanbera
--Theory
1 "
ISO 883
' 79
150 481
- V ■ '
ISO 652
330
152 894
■ *> ■ 1
332
152 736
596
153 833
760
149 165
1. '
764
148 561
149 138
Nuia (Mechanlca)
- -Corroaloii preventloa
301
161 897
Nylon
--AppUcatlOM
173
153 014
--Bttacta of radiatloB
752
154 529
--Plrepr coring
180
171 136
i ^'
Subjeg
OtMtaclea ' *
- -DatectloB
Ocean battom
--Arctic Oceaa
•-Atlantic Ocean
--Geology
--Pacific Ocean
Ocean currema
--Pacific Ocean
Ocean wavea
- -Mathematical analyaia
Oceanographlcal dau
--Atlantic Ocean
-Prooeaalnf
JU^I.' . f v>
]*
Oceanography
- -Arctic Oceaa
--Arctic regiooa
- -Inatrianentatloa
- -Pacific Ocean
Officer peraonoel
- -Performance
--Seleaioot
--Teat methoda
Offahore clalraa
Oll-allck removal
Oil taaka
--Handbooka
Olla
--Abaorptlon
Opacity meter
Operatlona reaearch
--Analyaia
--AppUcatlona
--Bibliography
Operator a (Maihematica)
•-Appllcatia
--Theory
r -t*"^"
58
Page PBNil^
427 153 101
537
558
282
537
149
33
34
282
414
33
413
414
557
707
153
,707
33
6
■537
261
262
394
683
537
479
716
715
'716
168
121
166
185
222
450
583
638
734
805
636
6
67
477
18S
322
601
217
186
318
.823
760
153 076
153 075
152 W8
153 076
148 340
775 153 783
413 150 060
148 125
150 529
153 625
153 762
150 487
ISO 060
153 114
153 482
154 551
152 149
153 781
148 367
150 483
154 836
154 837
152 636
153 572
148 771
153 746
154 838
153 121
154 648
154 671
154 648
161 579
150 836
150 837
150 838
152 146
148 714
148 715
171 006
150 714
153 660
171 503
155 360
148 401
153 681
152 136
ISO 998
152 914
148 670
152 761
152 762
153 671
153 483
152 442
152 491
149 646
152 747
153 311
Optical Imagea
--Intenalty
--Meteorological factora
Optical Inatrianenta
--Deaign
--Development
Optical materlala
--Radiation
Optical (yatema
--AppUcatlona
Optica
- -Bibliography
OrUt Blmulator
OrMtal worker
Order -dlaorder
tranaformatloBa ' |
Ordnance
--Handbooka
--Materlala
--Scheduling
Orikiance ateel
--Heat treatment
--Temperature factor*
Organic compounda
--Analyaia
--Applicaitan»
--Chetnical analyaia
--Conductivity
•-Bffecta at radiation
"Mnlrriilar atructure
— <Mdatlan
--Photochemical reacQana
'--Separatian
--Spectra
--Vapor preaaure
Organic materlala
--Electrical propertlea
Organic aemlcooduaor
Organic aotventa
- -Chromatographic
aaalyalB
- -Bffectiveneaa
--Solvent propemea
Orlflcea
--Preaaure diairlbutlcn
Oacll later ■
--Bibliography
--Statistical analyaia
Oamotlc preaaure
--Applicaiiona
Oxldaaea
--Fhyalological effeaa
Oxidation - reducti on
reactions
--Analyaia
Oxide cathodea
--Coatings I
--Development
--Performance
--Properties
Page ft Number
533
257
223
792
557
737
792
581
341
174
682
93
581
581
583
742
309
406
212
4<B
342
796
617
781
28
23
276
309
694
23
687
212
181
27
702
194
189
572
f
141
410
23
723
107
295
106
308
622
S9
ISO 322
152 834
152 566
154 530
153 886
153 846
171 254
153 825
149 643
152 439
171 611
150 470
171 480
171 481
171 482
171 483
154 756
154 757
153 660
154 307
153 062
171 409
171 177
154 406
171 340
153 936
171 491
171 596
171 103
171 122
152 770
171 061
153 036
161 571
148 219
171 177
171 033
150 539
148 473
148 694
152 213
152 736
742 154 307
152 264
154 295
171 122
154 4S0
150 450
152 735
150 424
152 538
153 823
Sublect
Oddea
--Phyalcal propertlea
--Speara
--Surface propertlea
Oidmea
--Metabollam
- -ToKlc effects
Oxygen ■
--Chemical reactlona
--Containera
- -Determination
- -Electrocbemiatry
--Electron tranaltlona
--Energy
--Heat tranafer
--impurltlea
--Ionization
--Meubollam
--Physiological effecta
--Propellant properties
--Toxic effects
Oxygen (Liquid)
--Applications
--Chemical reactlona
--Cenulners
--Equipment
- -Impurltlea
Oxygen conaumptlon
- -Meaaurement
Oxygen equipment
--Development
--Teat reaults
Oxygea Isotopes
--Applications
--Exchange reactlona
Oxygen maaka
--niyslologtcal effecta
Ozone
--Bibliography
- -Chemical effecta
--Meaauremenl
--niyalcal effecta
Page n Nfnber
589
414
469
410
272
691
607
157
400
543
26
108
63
217
144
348
11
542
311
399
584
740
406
561
712
144
19
36
543
688
406
36
703
24
412
75
317
757
408
560
34
154
179
171 530
ISO 721
153 094
154 295
149 635
153 841
153 183
153 060
153 303
153 583
150^336
150 949
152 065
148 682
161 946
152 137
150 216
154 436
153 791
153 409
153 612
161 239
153 354
171 554
153 611
161 946
171 ata^
171 087
154 819
171 606
153 354
171 087
148 076
150 538
171 607
153 437
152 590
171 043
171 578
150 923
153 567
152 066
152 553
161 969
hf> WN«i>T
:actd
hpar
--Appttcatlaas
— BJiaas of radUtlan
Hfm capKltora
I of radUQaa
7M
176
71»
171
SOS
49
130
an
ParabcUc bodtas
f)
•Tcac reauka
S14
5*2
ParmoMfiMClc tarn
--Propartl**
: ainpUflera
S42
314
SI
573
7»l
467
46«
701
423
434
Parmatilc HfKUoM
--Aluka
--AlaaiB
ftotlal dtflvMKla]
--Afpttcadoaa
-TWory
hrticJa Mxal
•-Davalopmaai
--Pertornnnca
hrtlci* beam*
--QpUcmJaHlrata
19
402
403
193
464
10
IBS
1(7
311
319
321
322
597
600
759
615
99
IIS
70S
312
147 100
152 793
152 794
ISO 631
153 199
171 533
154 667
150 631
161197
171 111
147 539
153 33*
154 803
171033
153 570
171 141
147 745
154 167
153 794
153 096
154 341
153 219
152 776
150 592
150 610
153 949
4S3 153 3S6
171 311
171 494
171 4M
543 171046
171 OM
171 311
150 736
130 994
153 307
153 291
152 336
150 133
153 494
153 446
19 150 561
f»ae n Nfttber
150 561
153 522
153 507
153 SU
152 163
171 497
150 514
ia670
152 490
14S672
153 71S-1
152 715-4
152 376
171 349
171 330
171 391
171354
171 3S5
153 275
153 306
153 30a
153 307
153 296
149 534
150 696
150 776
ISO 190
150 535
152 999
7t3 154 261
Pamela
(COB.)
hrttcta tra)actarl«a
- -Oaterml nation
••Mathematical aaalyala
--PkotOKrapUc amhnMa
rarticJaa
--AaalyaU
--DMajr
••D— iqr
--OKacika
- •DMermlaatioa
--DlOualoo
--Bncrgjr
- -Hydrodrnamlc
diaracxerinlca
•-kaUzlng eftecta
- -Meaauretnent
•ffaclaar raactlana
•Productlaa
-Scaaarmg
616
206
117
463
616
S47
462
463
333
625
463
7M
616^
609
204
462
210
217
392
766
204
175
lis
202
tatf
, --Valocity
Partlclaa (Alrtwrna)
••AMlyala
•-OMKlnf machoda
thMlfliirliii
- -Mawerotoclcal factcr*
— nqritcal properttaa
•-Pr«cipitatlan
- -KadloactlyKy
304
333
SSI
633
175
197
103
146
564
39
335
33S
101
103
aoB
335
464
541
7»4
719
--Scancring 302
Articulate ftliera
- -AppUcatlooa 309
PartUai ^acclana S96
PMlsn reco(nlUoa procram S7S
PauUna
--Taai ramika SM
714
IM
175
62
•OS
«S
441
•-]atata
PHao apacaa
PaUcta
- -Accclaratlaa
--Pauau-aaoa
Pckiar aOaa
tanmlcaa
taMkUum
taMtradoo protolema
Manaryttaltol tetranltrate
• -Appttcadona
--Spactrccraphic analyala
335
736
173
153 188
152 795
147 90*
158 171
149 0*7
150 700
152 OS*- 1
lS3aBa-2
171336
154 407
153 171
149 690
153 757
154 407
149 540
149 315
154 339
152 420
154 407
152 549
152 493
150 722
154 243
171 163
152 380
150 969
152 421
152 422
152 424
171 163
171 335
149 736
153 499
152 381
171 138
152 646
152 244
153 653
150 663
153 06*
153 070
152 806
152 646
152 2*3
152 795
153 661
153 068
153 070
171 361
171 362
154 402
194 706
199 5*2
152 639
171 061
153 136
171 549
171 525
154 678
152 543
149 071
161 800
171559
190 571
193 912
An 478
150 479
171 341
153 022
149 066
- -Datarloratlaa
NpUdea
--Motacular atructure
--Srolbeaia
--PiycholoflcaJ tectort
l^rcsptroB
PR-dilaryl nuorUle
-•Todc affacta
«0
702 154 374
576 154 544
314
689
392
80
81
152 446
1M214
153 470
171 093
171 092
150 66ft
Pcrlacope*
--Daaifn
Ftrmafroai
--BlbUofraplqp
--Mehlnc
Psrmalloy flbna
PeravaUtea
^ --Maywtlc propertlea
PBroddaa
--Chamtcal reactlcaa
-Combuatlon
ParaooaUtx teata .'
-Aaalyala |
--DavalopraMt
--Effactlreaaaa
-RaUaMUty
Paraoonel
--Paitocmanca
--Teat methoda ,
•-Training I
Peraplrition
--Meaaureman
Pwt
Partiffbatlcn theory
-Aaalyala
-AppUcadoaa
Peieraburg paradox
niaae detectora
--AppUcatlona
- -Clrculta
Fliaae meaauremem
- -Inatrumentatloo
niaae modulatloo
--Equipmem
--lutaaauremmt
Fhaae Alflera
--Aaalyala
--AppUcatlona
- -Clrculta
Fbenocoplea
Phenyl ether
- - DIpolc momenta
Phenyl aujflde
•-Dlpole momenia
mUpa Ion gage
nxwphate coatlnga
--Effactlveneaa
Phoaphlae oxldea
--Cryatal atrucnv*
FboapiilDea
--Chamlcal reactiona
PhoapMnotKrloea
-PolyTnerlMtlon
Fhoaphori
--AppUcailcna
--Bftectlveneaa
- - Ltanlneacenoa
- -ScnaltlTlty
nioapliarua
--Dlffualon
nwaphorua compounda
(Organic)
- -Chemical raacUona
Phoaphorua oxychlorldea
--Solvent propertlea
Rtoaphorylatlan
--Aaalyala
Fhotochamlcal raacdona
-Aaaijrata
Phot ccheml aery
nwtoconductlrlty
Phatodeboronailan
Pap
Pt Number
635
154 750
3*1
171 190
717
154 700
471
153 3*4
HI
703
703
S94
138
936
941
138
364
364
360
366
80
77
107
US
302
320
737
790
214
309
42*
442
4*4
702
775
792
595
727
423
733
573
393
727
42*
297
570
270
276
r6
631
75
472
144
695
54*
452
431
305
637
113
367
o95
697
546
689
409
549
2*
406
407
469
406
150 757
171 355
14*075
153 333
152 166
152 16*
153 604
14*610
147 642
152 913
148 004
147 309
153 341 •
150 991
152 067
150 822 •
150 969
152 423
149 644
153 947
153 821
152 4a
171 337
153 421 ■
153 13*
153 501
148 47S
152 117
149 567
147 547
154 5*9'
150 066
150 913
153 821
152 581
154 5*9
153 421
1S2 9S8
171 542
152 477
149 678
149 678
153 488
152 294
153 310
152 503
148 938
150 520
152 928
143 302
152 S36
154 752
152 185
192 695
148 99
147 841
152 848
154 468
152 611
153 051
150 627
150 690
171 376
153 094
153 215
153 216
Sutoject
Photoelectiic cella
--AppUcatlona
--Development
--Material*
Phoioelearlc materlala •
- AppUcatlona
nKXoelectric ahuneri
- -BlbUograptay
Photoelectric iranaducer*
- -Application*
Photographic emulalcna
--AppUcatlona
--Bombariknent
--nioiocbemlcal reactiona
Photographic film
- - Proceaalng
-Senaltlvity
niotographlc IntelUgence
- - Inatrumeniatlon
--Vlaual factor*
Phaographlc recording
ayatcma
--AppUcatlona
--Deaign
--Development
Photography
--Equipment
Fhotomagneto-electric eflact
Photomemory
nKXometer*
-Oealgn
Phaometry
--AppUcatlona
nidomuJclpUerB
--Development
--Senaltlvity
Photon*
--AppUcatlona
--Energy
•-Polarization
RMtoayntheala
--Analyal*
Phyalcal chemlatry
- -Inatrumentatlon
Phyalcal fltneaa
--Teat methoda
fhyalca
nqralologlcal paychology
--Bibliography
--Theory
PlckUng oompotaida
-•SjrKhaal*
Pldoip reaalon*
Pier*
- -Coatli^a
--Corroalon
Plezoelecirlc cryaula
--AppUcatlona
"Vibration
Plezoelearic mata^I*
- -Bibliography
Piezoelectric raaonatora
* 'Davalopraeai
PI lea
•-Preaaure
--Teat reaulia
PlUnga
Pilot*
--Artormance
-•Training
Page PB NwnbT
•-Training devloaa
--Vlaual factor a
Plach effect
Pinch experiment
277
307
211
342
346
299
341
98
464
462
752
352
478
637
683
121
8
223
637
637
223
109
637
133
154
274
942
463
463
443
462
785
115
278
400
146
314
146
689
206
206
630
638
'137
136
92
101
716
61S
296
306
170
S41
170
735
715
615
561
563
7
133
299
439
386
37
116
799
118
153606
153 100
149 708,
149 706
153 694
153 409
149 643
807 147 787
150 351
ISO 694
153 151
155 438
193 969
171 385
154 752
150 916
150 418
152 107
148 3BS
154 752
147 756
153 566
150 686
147 756
152 3*4
148 718
153 571
161 834
153 131
171 402
150 719
154 407
153 908
ISO 891
149 658
153 127
149 701
152 446
152 244
155 486
171 002
171 003
171 049
171 SOS
116 303S6
193 943
152 6*0
150 516
154 668
171 SOI
152 603
152 536
152 803
149 649
192*09
154 634
154 673
171901
171 506
171 991
152 123
171 199
150 317
153 0*6
1521*9
171094
147 838
154 499
150 890
Subjaa
PIpea
- -Corroalon prcvendon
--Heat tranafer
- -Hydrodynamlc
character!*
- -Macerlala
PI pane*
--Development
Platon nag*
--Lutrlcatlon ,
Platoaa '
--Acouatlc propertlea
--Theory
PItoi tutiea
--AppUcatlona
Planck radiation function
Planetary atmoapherea
--Analyala
Pafe PBNianber
--Danalty
Planet*
--Catalog*
--RK)togr*phy
--Radar aaalyala
' Plama
--AUaka
--Mlcroneala
--Nutritive value
Plaama (Phyalc*)
-Aoalyal*
-AppUcatlona
-BtbUograitiy
-Electrical factor*
-Electromagnetic effecta
-Electromagnetic factora
- -Electromagnetic
propertlea
--Magnacic factor*
--Mathematical analyal*
--Propertlea
--SUMllty
•-Temperature factora
--Thacry
781
803
773
742
803
104
206
276
465
132
534
258
258
131
Ml
997
441
12
997
64
r
98
116
117
118
178
216
301
312
338
L
847
^34
443
472
621
631
632
633
770
7*9
799
800
623
799
115
347
465
631
130
115
117
167
947
215
380
65
117
310
633
473
623
104
116
216
800
347
474
119
116
214
346
347
154 613
155 0*1
154*62
155 250
155 0*1
152 855
ISO 153 254
147 832
149 298
153 091
149 2%
152 464
153 285
152 936
171 196
148 669
152 827
153 S24
153 540
147 100
153 524
150 777
150 606
150 776
147 838
150 988
ISO 890
152 622
152 034
152 847
152 749
152 959
152 664
152 960
153 089
152 742
152 633
153 446
152 830
153 426
153 732
153 488
152 656
153 934
154 572
150414
199 9*4
154 455
154 370
148 936
154 272
150 447
152 996
161 S60
147 748
150 735
150 447
150 734
152 365
152 955
152 996
162 364
152 418
150 882
147 908
152 549
153 432
153 098
153 8X
153 824
154 448
192 113
192 917
194 372
153 636
153 466
147 780-4
150 629
190991
192 9«
152 912
153 636
171 336
Stk>|act
Plaama (Fhyalca) (c
--Theory (con.)
Plaama acceleratlan
Plaama aaglDe
Plaaoajata
--Thrual
Plaama oadllatlona
--AMlyata
--Detection
- -Mathematical analyala
Plaama propulaloa
Plaama protein*
-MecaboUam
Plaama tunnela
Plaatlc coatlnga
--AppUcatlona
--BffectlTeoeaa
Plaatlc flbna
--AppUcatlona
Plaatlc flbna
- -AppUcatlona
- -MaterUla
- -Cplical propertlea
Plaatlc rioar
- - niyslcal effect*
Plaetlclty
- -Mathematical aaalyala
- -Temperature factora
--Theory
Page PB Number
PUadca j
--AppUcatiena
- -Decompoaltlon
--Development
--Dielectric propertlea
--Effeaa of radiation
--Heat tr*n*fer
--Mechanical propertlea
- -Propertle*
--Temperature factor*
--W*ve tranamlaalon
--X-ray analyala
PlaHnotron
473
474
631
63
65
63
214
216
799
800
800
473
178
16
17
60*
73
314
441
593
617
624
794
603
768
453
104
325
452
453
465
602
603
768
59
101
316
588
730
757
752
626
181
757
181
75
181
315
620
54
432
577
PlatlBian
--X-ray analyala 114
Platinum compouada
-StablUty 14*
Platlman- rhodium alloya
--Electrical propertlea 617
Plywood
--Production 182
Pneumatic devlcea
--AppUcatlona 608
Pneumatic ayatema (Airborne)
--fammr auppUea 37
Pneumatic valvea
-Oealgn 580
--Teat reauka 736
Potncare-UgfalhlU-Kuo
method 327
Pointing control 434
Pdnta of dlmenalon 763
PolaaulUe Oov 456
Polarlaoopea
- -ClrcUta 392
Polarographlc aaalyate
--AppttcaQou 19
543
ISO 688
153 466
153 311
150 964
150 882
150 964
149 067
153 419
152 ISO
154 194 -
154 371
154 404
152 622
150 565
150 570
152 5*2
150 962
152*63
193 19*
171 532
171 490
150 657
150 558
171 531
ISO 739
153 124
154 120
171 684
147 362
152 134
153 109
147 401
147 362
154 291
147 402
148 811
148 812
153 142
153 767
154 121
150 825
150 687
153 630
171 525
154 639
171 665
171 612
153 649
153 008
155 572
153 008
171 096
161 948
150 013
171 527
150 446
153 240
153 230
150 749
192 091
194 429
171 167
153 416
152 313
153 613
153 616-1
153 616-2
153*70
192 73*
153 442
153 486
130 9*2
192(72
171 073
193 5*3
~>
Su»ect
Poiiucal tela
FatymCT soluiiana
--Optical propertica
--Sirtece propertle*
Foljrmermtica
of rMlUtlan
479 153 121
--AdsorptUa
-Aftac
--Cry«««l
-Dicampoalttaa
--OMMlrtc propamea
10(1
1 pro^CTtlea
- -Optical propertlea
"ftiMltcy
-Tamperatiore tecura
KilTBaBlaU
-Appttaua
PopuJacifB
--OMpnphtcal tector*
ra
--FrodactioQ
^stable roadway
hMtttoB iadicaux-a
- -Perfamunoa
PoaUrona
703
696
699
97
333
704
75
145
4CB
54«
W7
^2
697
205
277
S93
620
srfO
406
405
24
97
546
644
696
123
54S
•06
575
79
1S5
1S8
319
594
596
599
716
123
ISO
la
179
613
715
716
618
100
--MataboUam
FvaaaluDi bromide cryaula
--Grjratal acrvctura
ruaaaliaii cfckxide cryatala
--Color
--Gryaal Kmcture
--Blactrlcal propenlea
--WtotocoadMrflTtty
PoModal tbecry
110
470
110
63i
341
470
473
79
86
in
633
171
777
777
--MaMrUla
Povdar luatiHurgy
199
53
748
560
78
79
-Thaocy
149 895
148 400
171 570
171 575
152 648
152 649'
171041
148 407
152 590
171 181
150 656
147 170
1716*5
171 612
171 563
153 258
171 310
153 628
147 848
171 570
171 401
150 6S6
152 or?
152 648
152 649
153 875
171 574
171 570
171571
152 035
147 170
154 071
153 234
153 393
153 372
152 444
152 396
152 371
153 860
152 370
153 133
154 682
152 110
161 966
148 676
171 178
161770
154 663
154 665
154 667
430 171
154 817
150 944
543 153 406
15q,543
4
152 604
150 543
153 741
152 731
152 604
153 143
150 466
152 099
153 490
153 872
149 660
154 537
154 536
59 148 914
orrssa-423
161 578
153 847
153 931
150 951
148 199
153 306
Subtect
Pap
n Number
Subfacl
Page
FBNumbar
Pnrer aupfiUea
Probab(Uty(Smtlailca|Ma.)
79
148 199 ■
-HbUograpby
661
171 689
•.
184
152 162
— Circutta
164
152 920
■/.' ■
185
152 161
584
153 944
: < • . - ■
186
148 6*3
429
150 689
317
153 883
--Mllttary requtremanta
560
153 933
>*••
330
153 934
PraampUflers
■ • 1 ' *
596
153 831 .-
--Performance
423
153 494
■ ' - V *,'
153 840
Predpltatiaa
■ i '
759
149 558 '
--B4bllO(ra;iiy
31
150 617
...
760
149 1*5
281
151
153 046
152 448
761
148 906
— Mataorologlcal faacra
ia9a7
—Radar aoalyaia
334
152 661
- -ApiiUcationa
8
150 361
412
153 299
49
150 593
766
150 848
76
152176
784
154 706
f ' "
78
150 600
--Radioactivity
541
154 402
222
148 695
Predpltauaa etatlc
395
152 741
789
154 078
-•■. vi
432
153 306
Prefabricated bulldinga
, ■;
539
171 545
- -Coaatructlan
714
154 625
594
14*419
718
154 652
1--
«0I
153 108
--Teat reaulia
713
154 628
806
148 401
714
154 613
^,
807
iaso3
715
154 666
--DatermlnatlaB
76
150 533
Preaalector
41
ISO 681
77
153 100
Preaa forging
611
171 524
565
147 546
Preaaira
-Tafeiaa
76
171078
--Coacrol ayetems
636
154 966
80
150 496
--Meaauretnen
194
148 694
81
1710»Jj-
206
147 963
-Tlwory
77
150 521 '
465
171 237
152 106
714
154 623
78
152 289
726
155 567
'
79
ISO 481
--MataUurglcal effect*
330
171 348
t
lto652
--flqraicaj effecta
459
171 025
80
150 476
754
171 595
150 477
- -Recording devlcea
735
154 634
. j' .
150 496
Pi'eaaura gagea
"■' "^ . '•■"'
188
149 717
-Calibration
466
171 337
318
171 312
--DevelopmeM ,
714
154 623
320
152 900
--Saoatuvlty
557
154 763
'•
321
149 663
--Taal raauka
454
ISO 067
■171 327
Preaaora regulator*
450
153 358
"Daatyi
583
153 615
153 359
. »
584
153 617-1
478
153 360
153 617-3
594
148 092
--Teat reaulta
584
153 613
599
147 176
740
154 290-1
Profilcmeter
62
150 459
741
154 290-2
Projectile fragments
Preaaure wrltchee
--RecCTrery
60
148 225
--Oevelopneol
583
153 614-1
Projectile*
152 9??
153 614-2
Velocity
437
1S3 615
Projective geometry
739
154 289-3
- -AppUcailona
187
148 696
Preaaure veaae la
Propellant gralna
157
153 060
- -CombuatloB
447
153 299
630
171 049
--Bxtrualoa
71
150 390
749
153 917
-Heat cranafer
308
152 826
Praaa«a-laad cabiaa
315
152 825
-CooUiV
306
171 345
Propallanta
Preatreaaed concrete
753
154 630
- -Combuatloo
70
152 351 '
Preagaaaad timber
715
154 663
71
152 027
716
154 665
179
148 «9«
•
154 667
180
148 699
Pretlco
66
ISO 835
275
153 033
Prlniary bacterlea
--Detonation
738
152 022
- -Arctic reglona
165
149 698
-Material*
61
150 456
-•Blactrode*
: 165
149 697
- -Thermal propertle*
804
154 440
--llaarli^
165
149 698
- -Thermodynamic
PrUnana
propertle*
314
149 665
-AflBf
688
154 594
PropelleT* (Aerial)
--Bflactao<radUtlan
273
152 630
- -Model teat reaulta
711
154 549
404
153 301
-Wake
418
152 873
-niyvoN^y
138
152 428
Propeller* (Marine)
7
150 372
- -Cavltatlun
176
148 721
263
152 744
- -Hydrodynamlc
Primer*
charaaerlatlca
746
153 725
--Develcpsieat
174
152 259 ,'
--Model teal reaulta
774
153 919
308
152 839
--Preaaure dlatrlbullon
176
148 721
309
152 840
Propulalon chemlatry
65
150 613-1
Prlnied drcuita
ISO 613-2
--Coacalner*
51
150 809
Propyl nitratea
ISO 810
--PropeUam propertlea
438
152 316
- -Development
323
153 274
Protective clothing
--Matarlaia
427
171 380
--Aralc reglona
464
153 508
725
154 166
465
153 510
Privation
--CUmatlc (aacra
103
150 778
"itedMHical aflucta
402
153 363
--Materlala
74
171 068
"Wijiliiluglral affeaa
398
153 469
181
171 153
68S
171 610
--niyalologlcal effecta
103
ISO 778
PrdMbiUty (Statlatlca)
78
150 482
152 108
- -Thermal Inaulatlon
206
171 143
62
m
Subject
«^
1
PBNianber
Subject
page
FB Number
Sii>tMt
rv
PB Number
Protective clothiag (con. )
Protona
Pulae ampUflera
— VantlUUoa
102
152 299
--AppUcationa
727
154 114
--Daalgn
16*
152 3*5
103
150 778
- -Exchange reaction*
147
148 679
Pulaa analyzera
152 398
149
148 678
--Clrculta
334
153 621
Protective coaatructlan
1
171 106
--Nuclear reaction*
463
150 693
Pulae cablea
1 Protective coverlnga
632
153 186
--Electrical propertlea
47
152 667
\ . --Developmem
561
171 514
153 189
Pulae communication systema
1 --Teat reaulta
584
171 III
--tathoioglcal eaect*
404
153 304
--Mathematical analyaia
421
153 000
\
786
154 167
--Reaoiunce
409
147 776
Pulae generatora
I Protective ahekara
--Scattering
332
149 732
--Analyal*
430
153 454
\ --Arctic ragloaa
430
153 517
462
153 151
--Application*
344
152 935
\
715-
154 621
Proximliy warning
--Deatgn
«9
150 595
•
154 663
information
710
154 744
430
150 707
\ --Blaat effecta
176
152 256
Paeud-cluater expanalon
784
153 187
Pulae modulation
\ — Coatamlaatioo
743
154 627
Paeudodlabetea
142
152 367
--Appllcatlooa
723
150 109
I — OavakvoMM
294
153 273
Paeudomon**
-Codli«
430
150 707
\ --ft«aauradlatrlbuiion
176
152 286
--Seneltlvliy
403
153 192
153 084
1 - -Safety meaaurea
742
154 622
P*eudomaoaa Infectlona
- -Inatrumenutlon
49
ISO 595
. I - -Teat reaulia
585
154 S03
--Pathology
404
153 194
Pulae Byatem theory
421
153 000
714
154 629
-Therapy
403
153 192
Pulae tranaminera
717
154 617
545
153 640
--Dealgn
430
153 0*4
1 --Veotllatloo
715
154 653
Paychlatry
265
152 764
--Development
723
154 313
743
154 689
PsychoacouatlCB
396
171 403
Pyrene
744
154 674
466
153 170
--RcBonance
108
150 378
Protein atarvation
- -Guatemala
Protetna
--Biochemical efleaa
- -MetaboUam
Protolyala
Proton acceleratora
--Development
Proton beama
--Attenuation
Proton croa* aectlon*
--Determination
--MeaauremeM
142
148 724
17
ISO 471
17
150 567
150 570
690
153 714
746
155 414
147
148 678
148 679
^
153 636
462
153 151
204
147 542
100
150 523
204
150 857
152 133
--Bibliography
Paychology
--Theory
Paychometrlca
Paychomotor teeta
--Analyaia
--AppUcationa
--Ftiyalologlcal (actora
-^Teat reaulta
Paydiotherapy
--Paychologlcal factora
Pii>llc health
--Perlodlcala
- -Preaervatlon
621
138
686
686
398
7
8
269
134
8
395
22
273
33
404
692
«92
693
147 765
171 000
154 462
148 005
153 469
152 123
152 098
171 304
153 215
150 490
153 168
161 371
161 371
161 371
161 371
131 784
161 371
161 371
63
7
9
8
10
R
11
12
149 152 488
Pyridiite derivatives
-StaUUty 702 148 932
--Toxic effecta 691 153 841
Pyrldinea
—Chemical reaction* 145 148 660
--MetaboUam 272 149 635
Pyrlmldiiiea
--X-ray analyaia 269 152 740
Pyrltea
--Electrical propertlea 471 ISO 3n
Pyrogena
--niyalological effecta 689 155 397
Pyrotechnica
--Analyaia 173 149 670
Q-daKXloM
Q-*«taea
QK-TOa
QICS779
QRC-29
QMUtjr oooD-ol
"9HUabcal aaaljnt*
--Ttaory
quudm meckaalcs
U
303
432
S4
425
7S9
SM
too
764
351
74S
IIS
302
216
217
4*3
631
633
693
n Number
171 0>2
149 700
150 699
ISO 699
ISO 446
ISO 698
14S7»2
153 146
153 7S2
148 S3S
152 897
148 787
IS0 5S6
ISO 557
152 421
152 481
152 493
147 900
ISO 946
153 499
153 903
QuBKiMn mechanics (coa. )
--AppU cation*
--Thaory
Quantum aanrc
Quartz
- -AppUcatioaa
Quartz cryitala
-Atlnt
--Blactrlcal propertlea
ffe n H\MnbtT
616
IIS
215
217
473
633
633
425
153 032
ISO 891
150 969
152 214
152 483
153 728
171 533
153 282
171 386
60S 1S3 568
maaauramant
--Frlcaon
— firovth
166
430
343
166
469
343
1S2 231
150 064
149 695
149 696
152 231
171 474
149 692
Subtea
Quanz cryaula (con. )
--Fhyalcal properties
--Properties
- -Tsmperature factors
Quartz raaooaiora
- -Develo|xnetu
--Frequency
measurement
--Frequency ahlft
--OadUator drcuita
--Production
Queuelng proceaa
Quinooe*
--Electron transitions
--Ktjrperflne structure
Page W hfcgnber
109
341
342
166
430
573
170
343
*X
163
m
166
805
549
107
108
150 660
149 721
149 723
149 724
153 231
150 064
153 246
149 7IS
149 696
150 064
149 719
149 723
IS3aM
153 331
148 401
IS2 961
150 430
ISO 431
ISO 433
Rsdar anteiaMa
--Dealpi
- -Bqulpment
Radar beacons
--Equipment
--Psrfarmance
Radar beacona (Alrbcma)
--Derelopmenl
Radar confualon reflectors
--Applications
Radsr corner reflectors
--Design
Rsdar dlaplay ayaiems
--VlalUUty
Radar display ayatams
(Airborne)
- -Performance
Radar duplexers
--Developmeni
--Equipment
Radar echo areaa
--Analyala
--Geo(ra;Mcal faaors
--Mathematical analyala
- -Meaaurement
--Theory
Radar equtpment
--AppUcatlana
--Development
Radar Interception
- -Equipment
Radar interference
--Reduction
Radar mapping
--AppUcatioaa
Radar navigation ayaiema
--Development
Radar operator*
--Perfcrmance
--Psychological faaors
- -Trslning devices
Radar recelvera
--CaUbratloB
--Deal^
- -Mathematics] snalyais
Radar reflections
--Angle of arrival
--Meaaurement
Radar reflectora
--Teat reaulta
Radar scanner*
--Development
Radar (canning
--Equlpmeot
Page W Nmuwr
--Theory
Radar aignala
--Analyal*
--DatectioB
--Proceasiiig
Radar targeu
--Detection
--Velocity
Radar tracking
Radar tracking ayatema
--AppUtatiaas
--Daalp
--Bqulpmear
- -Teat reaulta
Radar tracking systems
(Airborne)
--Equipment
Radar transmitters
--Equipment
RADC reUsUlity notebook
Radial thrust
Radiation
43
735
566
41
•165
ISO
S6
431
300
439
214
132
156
119
476
41
414
730
45S
573
163
427
171
363
41
308
438
734
730
635
3
53
161
430
451
293
162
48
167
428
727
428
4*
171
293
167
739
438
44
174
57*
157
49
304
439
153 188
ISO 903
171 504
171501
171095
152 239
153 196
153 614
143 302
430 171 368
152 668
153 229
133 245
152 S61
153 391
148 386
ISO 650
153 83S
150 740
ISO 071
153 079
152 6iO
150 894
148 711
153 396
575 153 595
153 006
153 325
ISOltO
152 7S9
153 697
155 360
155 079
171544
150 451
299 152 949
171 153 006
146 395
149 059
153 712
153 560
152 655
ia711
150 608
ISO 604
153 217
152 965
153 33S
ISO 593
153 006
152 655 >
150 604
153 647
153 330
153 311
ISO 797
153 303
148 708
573 154 318
150 595
161 894-1
153 OSS
Radiation (con.)
- -Chemical efleaa
-Intenalty
-Ionizing effeas
-Meaaurement
-hthologlcal effeas
-Riyslolaglcal effeas
Page PB Nianber
Radiation belt
Radiation counter a
--Btbllography
--CaUbration
Mdlatlon damage
"BlbUograptiy
- -Coiaiter meaaur es
--Meaauremeot
--Teat facllltlea
Radlatioo Injurlea
--Pathology
Radiation meters
--Applications
--Calibration
--Development
--Performance
--Power supplies
Radio antijamming
- - Inatrumeicstion
Radio sstronomy
• - Instr umenutloB
Radio beacona
•-DevelopmeiK
Radio conununlcatioa
ayatema
--Equipment
--Military requlrementa
--Reliability
Radio communication
syaiems (Airborne)
- -Equipment
Radio equlpnneiK
•-Maifcenanoe
-- Reliability
Radio frequeoclaa
--Sundarda
146
377
551
784
796
558
97
113
340
746
273
691
5
358
392
99
333
56
306
101
317
162
619
784
784
143
273
617
333
551
333
617
718
2
155
428
429
534
535
306
992
572
579
220
577
170
361
S77
163
289
o interference
Countermeasures 164
Measuremem 396
433
739
734
55
729
739
747
749
789
Radio Interference analyzer*
--Performance 734
--niyatcal
--Reduaicn
--Scurcea
148 389
171 310
171497
171 S72
153 936
153 569
152 648
152 649
150 443
152 714-3
15SS66
152 630
171 608
150 801
149 645
150 722
171 134 •
153 768
149 713
149 714
150 687
150 961
153 804
171 533
171 573
155 323
153 476
153 589
171 491
153 632
171 497
153 790
154 753
ISO 901
149 007
148 983
153 335
153 719
147 333
147 324
147 333
147 335
147 336
147 327
147 338
147 329
152 201
152 r2
154 418
153 238
152 333
154 516
171 131
171 132
152 783
152 788
154 516
149 719
149 722
152 658
152 236
153 992
150 712
154 680
154 413-1
154 413-3
148 973
154 651
154 643
154 646
154 637
154 078
154 413-1
154 412-2
Radio recelvera
--Equipment
— Saaaltlvlty
Radio relay ayatema
--Equipment
Radio repeatera
--Development
Radio algMla
--Detection
--Dlatortlao
--Mathematical analysis
--Trsnsmission
Rsdio tranamiaalon
--Frequency
meaaurement
- -Meteorological factors
Radio tranamlaera
--AppUcatlanB
Radio tranamlttera
(SMpborae)
--Development
Radio wave reflectiona
-Tablea
Radio wavea
--Abaorptloa
--Appllcatians
--AttenuatioD
--Mbbography
--Electrical effeas
- -BlectrcmsgDetic
properties
--Polarizatloo
--Propagation
Page PBNianber
-ReOacUoa
-Scaavring
Radloaaivadon analyala
--Applications
Radioactive aubatancea
--HandUi«
--Teat methods
Rsdioactlve waste
--PIsnt metatmlism
Rsdloactlvity
- -Countermaaaurea
•-•Detection
-•RecordlBg devloea
--SUtlatical aaalyaia
RadloMoiogy
--BIbUagrapfay
--Handbooka
■ •InatrumeBtatlan
Radlochendatry
--Theory
Radlochemiatry labor atoriea
--Bqulpmem
Radlotrequettcy ampUflcrs
--Signs) to noise rstio
--Teat reaulta
Radlofrequency attenuatora
--Calltaratlaa
734
431
567
164
7»
302
166
572
130
230
475
690
434
130
80«
3M
151
80S
635
173
130
119
48
119
130
168
331
349
414
534
570
635
636
3«»
S7S
119
349
415
433
6»
731
333
143
144
619
693
303
101
306
785
783
686
693
143
693
22
144
781
277
22
174
434
423
152 992
154 412-1
154 412-2
152 998
153 347
152 226
152 985
152 985
153 576
153 577
148 714
154 483
ISO 735
152 233
150 718
154 363
150 710-1
150 710-2
161 573
147 840
152 696
152 568
161 589
161 581
152 991
ISO 928
ISO 669
152 0I1
150 669
ISO 610
ISO 928
161 579
149 064
149 740
150 071
147 334
153 818
161 587
161 580
147 558
153 821
ISO 650
152 523
161 583
153 609
161 581
161 588
ISO 914
153 071
153 069
152 570
154 417
150 654
148 979
171 091
152 795
153 582
154 717
155 575
154 592
152 349
121 784-R
153 363
152 570
171 596
171 310 a
152 353
152 063
ISO 710-2
171 234
--81bUagraphy
540
ISO 896
Radio navlgatlaa ayatsnia
171 225
--Biochemical eflaaa
31
150 671
(Airborne)
171 226
1
693
1
154 993
1
1
1
--Equlpmea
«S
170
430
171 130
171368
--Developmegt
S7«
154 806
Subjea
-Btocciical proyntlM
—}otaf
--MadHnadcml ualysla
MdMbraqoMcr ■Beruori
IUdlfltr«qu— cy oaclUatora
"CaUlratlon
-DatMXlaa
IUiM<^»y ry tr«n»tf iiiei »
lUdlapHliy
--ApftUcadcoa
Kadloi x,«'i|WK
--FractlowTtop
--nroductlan
lUdloloctcal coanraHiatlCB
"TMIrMulia
Katfafei^CBl variare
—NyihilUlcal aflacu
M*o»ala
--Streaaea
lUdaawa {Airbane)
--BlMXrlcal propertlea
--Oroapth
■ aian apactra
I apaaroaoapjr
dtacriboboB
Tfcaory
r— ctlciia
"ftaMMty
lUraaanha
--Appilcatlana
- -Thertnodjmanilc
propertlea
I (MlUtary)
--Arcdc refiaaa
"HtrBlTa »aluB
tf nftmOmr
9«bt«a
Rawtnaoode dau
47
132 667
M7
193 346
Raylelfh wavaa
RBP-3 1
41
132 191
'
2»
153 003
ReacQoa (Paycfaolofy)
43S
153 242
-Aaairala
57»
153 243
153 244
--Mathemaclcal analyala
41
152 191
572
154 4«3
— autlaclcal aaalyala
S3
161 576
4M
171 342
—Teat loetboda
20»
152 400
49
190 597
4li
152 974
--T«at reauka
- -TemXag equlpnieni
719
155 159
--Theory
Reaction time
309
132 9«
— AnalyaJ*
61S
130696
--MaaauremaK
32.
153 645
Reeaora
53
150*43
--Blaat effecta
«0
146 339
— CaUbraclon
in
193 394
--Cooling
782
194 717
--Bqutpmen
619
147 553
-Haxarda
22
161 371-7
22
161 371-6
--LccaUcn
la
193 600
373
161 371-9
-Shielding
334
193 690
Raadli«
335
193 970
--Oatermloaticn
404
161 371-10
Readii«heada
«r93
131704-R
Readtag macMnea
161 371-11
"Devehllnient
693
161 371-13
743
154 675
1
150 614
Real gaa effecta
150 615
Raaacnlng
1
im
150 616
153 M6
--Btttttacrapky
"hyckotoglcal factora
334
152 S21
147
171 156
--Teat metiwda
--Theory
792
199 437
RecomMnaiicn ramjet
3B
150 753
eaglMa
340
153 714-2
-Deelgn
152 714-3
--Performance
7r
194 061
RecnraMnatloB reaalona
167
190 604
Racordliig ayatema
279
193 90S
--Oaai9i
10«
152 190
RecruMBf
436
193 331
-Paychoioglcal factor a
230
149 060
Recttflera
42
193 193
- - Develofmenf
Redwing ,
159
193 633
Re-entry aerodynamlca
423
171 416
«
30
190 939
31
150 437
702
1M747
-
376
149 601
315
171 306
--bMCrtaneoudon f
79
146 199
413
150 060
--Teat CaclUtl^a
599
147 176
Ra-aaoy turHoaa
410
153 157
214
146 9«1
Raflectloa coeffldenta
702
146 932
Raflectometera
--Deatgn
106
190 434
Raflax Uyatroea
306
152 536
622
153 833
Refractometera
701
194 I9«
-AppUcadOM
-Daaign 7
Refractory coetlnga
«M
155 574
- -Temperature factora
--Teat reaulta
63
150 571
Refractory maierlala
441
193 513
--AppUcatlcna
310
153 339
.-
66
I
Page r^Ntanber
SMt)jea
Page FB Number
31
150 867
Refraaory matertala (cob. )
280
94
427
152 699
171 099
153 950
--AppUcatlona(con.)
- -BtbUograpiiy
296
467
591
152 610
153 683
154 846
153 951 -
-Caatlnc
458
151 098
9
9
265
539
150 503
150 504
152 535 1
147 561
152 837
--Europe
69
179
591
446
171 061
171081
171 178
161932
171 159
161 233
136
152 156
--Mechanical propertlea
591
154 846
137
264
7
150 887
152 621
150 372
--rhaae atudlea
--Phyatcal effecta
447
754
777
171 3»1
152 980
154 537
263
538
6*4
538
152 744
148 169
148 756
149 521
153 497
--niyalcal properUea
179
445
589
590
171 178
171 413
171 520
171 515
171 541
666
155 573
--Propertlea
69
171 101
9
150 794
--Temperature factora
590
171 515
--Thermal propertlea
445
171 390
999
147 561
- -Vapor preaaure
445
171 413
137
150 887
Refrtccrana
150 036
—Heat tranafer
348
99
100
148 647
152 358
-•Vapcrlzaticn
349
30S
150 035
171 345
933
CrTSSB-449
Refrigeration ayatema
463
101
303
150 708
192 806
153 012
--Developmeic
212
802
597
150 800
171 559
152 956
333
153 790
Regreaalon theory
763
148 748
303
153 011
Reinforced concrete
153 012
-AppUcaUona
716
194 668
764
155 322
Relativity dMory
--AppUcatloM
215
192 214
638
171 503
Relaxation time
701
190 133
571
154 747
RcUatalllty
f
807
147 787
--Determination
453
153 397
80
171 093
• -Mathematical analyala
786
148 974
81
806
327
171 092
155 030
152 557
--Military requlremeata
--aadadcal aMlyaia
304
580
80
80
161 894-1
154 811
150 477
150 496
264
13S
8
685
137
153 110
171 146
152 104
147 903
152 272
--Theory
189
451
594
764
a
148 719
150 725
148 419
171 580
192 295
364
■(^48 004
Remote control ayatema
--Appilcatlana
334
152 698
310
148 777
--BtbUocraphy
143
153 0S9
310
153 587
572
154 418
63
152 095
--Human engineering
5
152 300
278
699
149 6S9
149 085
Remote underwater
manipulator
707
153 781
Reatdual atreaaea
201
152 169
573
153 821
Realaa
--Caating
316
171 034
393
193 339
- -Ccmbuatioa
306
152 596
Realatance devicea
95
171 066
48
102
39
157
160
308
327
417
455
150 678
152 646
171 054
171 147
153 357
152 759
152 557
171 372
152 630
Reaiatora
-Bibliography
— CaUbratloB
—Production
134
168
290
291
292
46
CrrSSB-429
errs SB-429
171 206
171 206
171 207
171 211
171 300
152 360
606
153 566
--Temperature factora
725
154 166
736
171 248
Reaonance
771
154 815
90
192 170
86
152 312
Raaptrabcn
87
150 606
--Aaalyala
140
152 433
312
152 856-1
--CoBtrol
19
ISO 788
313
120
152 856-2
152 856-3
161 573
— MeaauremeK
--Temperature factora
Reaplratory dlaeaaea
139
688
397
171 140.
171 607
153 545
341
149 651
--AUaka
Reaptratory ay«em
18
190 566
303
149 629
— Cllmadc factora
Reaplrometera
268
153 337
150 439
152 002
283
152 951
— Dealgn
14
701
154 518
--Teat reaulta
13
Reetraloed coiumna
83
152 143
771
154 815
Retina
794
171 617
--Blood drcalatlon
544
193 401
446
171400
-nqratdogr
140
152 399
152 853
154 120
106
148 254
RaMmlaf teitalquaa
139
179
171 148
Rheologr
768
SutHect
Kheaua monkey
Rhodium compouida
--Syntheala
Rhodium compounda (Organic)
--Spectra
Rhythm
-MenBuremenl
Riboflavin
--Phy Biological effecta
Rletnann aurfacea
Rita
RIveta
--Streaaea
RoMla
- -Cooatructloa
--Matertala
Puc Wl WwnbCT
S^^^ci
rM^c ^B Nmibcr
688
274
409
--Teat reaulta
Robota
Rock
--Caribbean ialanda
Rocket ameiuiaa
•-Dealgn
Rocket caaea
--Maierlala
--Thermal tnaulatlon
Rocket flare*
- -OevelopmeiN
Rocket fuela
--Chemical aaalyila
--Energy
—Matertala
Rocket heada
--Production
Rocket launchera
' --Coatlnga
Rocket motor nUat
- -Counter meaaurea
Rocket motor nozzlea
--Teat reaulta
Rocket motora
--Dealgn
--Exhauat ^aea
--Fuel Injection
--Mark 29
--Maierlala
••ta^ormanca
-Shock realatance
•Temperature
-Teat (aclllUea
-Teat methoda
-Teat reaulta
-Teating equipment
-Thermal Inaulatlon
-Tbruai
18
186
450
340
713
715
716
717
686
554
IM
284
2W
316
749
181
755
992
73
583
314
311
36
311
65
180
66
65
611
66
311
447
747
311
308
159
309
443
586
65
191
311
586
181
61
586
'i
154 594
152 773
147 776
274 152 631
150 576
152 374
153 433
152 714-1
40 152 355
154 632
154 663
154 665
154 667
154 645
154 462
153 735
148 717
152 623
161 786
153 620
153 917
161 948
160 152 079
154 716
150 072
171 115
154 769
171 047
171 308
152 647
161 227
150 882
152 257
148 364
150 972
153 928-1
153 928-2
150 835
153 791
154 410
154 411
155 149
153 272
152 826
153 280
152 988
153 286
171 499
150 972
152 345
153 772
153 449
161 948
150 886
153 449
Rocket OBldlaera
--Ctaamlcal reactiona
--Corroelve effecta
--Haxarda
--Matertala
--Teat methoda
Rocket propella^a
- -C^onibuattoife'
- -OxToalve effecta
--Development
- -Maierlala
--Safety meaaurea
--SuUUiy
- -Thermodynamic
propertlea
--Ultraaonlc analyala
Rocket propelled aleda
--Appilcatlana
--Aerodynamic
cfaaractenatlca
--Development
--Performance
■ -Velocity
Racket propulalon
-•Btbllography
--Theory
Rocket reaearch
Rocket irajactorie*
- -MathemaUcal analyala
Rocketa
--Appilcatlana
--Bibliography
--Mod on
Rodaota
--Arctic reglona
--hraaltea
--Riyaiology
740
331
70
72
702
177
180
442
747
70
443
756
70
442
311
586
418
306
443
581
84
443
581
65
310
736
177
65
177
310
312
442
442
586
747
34
439
559
436
436
22
402
274
161 239
171 301
192 397
171 119
171 355
153 948
153 949
152 546
152 297
153 441
153 493
154 454
161 215
153 181
171 252
152 354
153 493
153 791
171 499
153 404
152 743
152 790
153 825
152 802-2
153 290
153 836
150 613-1
150 613-2
148 777
171 249
171 184
150 882
152 546
153 587
171 306
150 719
153 441
150 320
154 454
150 417
153 388
147 532
153 182
153 182
150 562
153 522
152 631
67
Si*itea
KaU
—Wave tranamiaaion
Rotating mirror cameraa
--AppUcatiooa
Rotating atructurea
- -Acouatlc propertlea
Rotor bladea
--De-idng ayatema
--Preacrvation
Royal Mcfiee
RiMier
--Climadc factora
--Effecta of radiation
--Preaeivatlon
- -Temperature factora
--Teat methoda
Rul)t>er mounta
--BlbUograpliy
Rubber aeala
--Performance
Ruddera (Marine)
- -Hjrdrodynamlc
cfaaratseiiaUca
Runge-tCutta analyala
Runway barrier ayatema
Runway llgbta
--VlalbiUty
P>gc PB Nmnber
--Apptlratlona
--ArcUc regiooa
— Dealgn
--Load diatrlbutiao
--Location
--Matertala
--Surfacea
— Vlaiblllty
--Trafflcahiltty
Rural areaa
--Arctic regtona
Ruthenium
--DetertjU nation
Ruthenium borlOea
--Cryatal atructure
221
739
747
336
561
80
317
317
75
317
317
306
310
753
745
802
709
36
158
562
742
714
287
416
417
714
38
417
418
158
709
40
122
274
214
152 398
171 686
194 646
193 195
171 514
150 992
171042
150 961
152 590
171 043
171 042
,149 674
153793
171 688
149 745
150 243
161 914
192 330
192 384
171 507
154 642
154 619
153 629
171 370
171 369
194 678
171 068
171 369
153 178
152 494
154 743
ISO 436
152 110
152 772
15?^»^
SA-IM
Siddtopcta prvpxty
Saiety valve*
aUhrs
>-AMlytfa
--Chemical aaalysla
SakDoaeUa
--AJaaka
fage Ft hfcanbar
36
230
1S2»6
14*735
712 IS3 611
542
141
154 426
152 21*
401 153 513
--HbUoCraptir
•-Fkjralcal pra^ertlM
SampMnc (Sudatlca)
-AppHranma
--Milttary raqulremasa
--TaUaa
--Tb»orr
Sand
- -MactiaiilaBl praperOea
--Source*
SoKlwtcb paaala
--AaKlrala
--Btoacicltr
"Taai iiiarhwl*
--Taal reaulia
"Vlteatlaa
--IMdtac
Saattary
--OMo
27
553
•0
116 '
479
Sftt
«M
79*
546
189
IM
751
271
7M
«0«
4U
l$2
tot
--Cryattl acrucnv*
--Friction
SaMUtte ttrry
SauUlta vcWda raaaarcb
palllM vaMcl* tra)actarl«a
-Aaklrala
Maljala
-rbjratcal factcra
-ataoadcal aaajyal*
vaWclaa
--■tbUofraptiy
--Coacrol ayaiawa
"OiMcUai
-Pllttri patha
-T—paranra
345
4M
435
57
131
221
23*
278
435
43»
7J»
174
308
436
438
440
«0
61
172
174
309
308
737
439
499
435
439
5
257
2U
558
438
SM
585
438
307
340
422
580
90
305
307
435
584
585
174
438
436
439
M
307
307
.438
CmSB-42S
171535
150 476
148 6*3
171478
1S3897
14*79*
14*7*3
153 14*
148 719
171 161
152 DCS
149*38
134 121
1SS*3*
17140*
1711**
193*3*
193 *»
149 718
Sub)»a
SaMlUta TaMclas (oea. )
•-TracklH
Page F* Number
"Modoo
SMKiaaon aoMona
■K vulcanliatea
9C-27S1
Scabbbit
Scaa-coliann tadex
17* 152 064
152 544
171 474
152 330
152 321
192 2Q0
152 303
149 0*4
149 6*5
152 6*4
153 40*
150 708
154 58*
152 439
152 522
150 070
150 724
153 230
153 493
150 799
130 9*9
ia706
148 697
171337
152 939
153 947
153 218
153 219
153 744
153 055
148 2S*
152 84*
153 080
153 399
193 1*2
17149*
171593
171 J*3
153 100
192 714-9
153 4*4
171 10*
JI52 036
*171345
152 679
192 330
193 321
17149*
171553
150 321
153 953
193 183
190 703
190 777
199 8*9
193 8*5
199952
-Ap^cadOM
-Mathematical analyata
— ShnulatKa
--Theory
ScUauMoma i
-Alaaka
SchUaraa pboiocraphy
--AppUcatloaa
Schuben calculua
«0
62
172
174
308
321
438
174
730
317
304
5*9
63»
191
575
163
330
600
6*3
749
7*3
636
78
sr
996
79*
19
271
30*
318
--<3itM
Sdcnctflc report*
--BtbUofraptiy
"Cadli«
- -Casta
--iHelUflMUly
--rrooeaataf
-SiAtw3 haKttnga
Scteodflc reaearch
--Arctic regloaa
--BlbUograpby
-USSR
SdndUatloo coatera
--Ap^catloaa
--Deatgn
Scopolamine
--Syodteala
Sea breeae
--tdeeawram
150 799
150 647
148 706
149 066
150 321
152 522
153 053
153 230
ia697
153 719
171043
149 712
193 661
153 160
14*734
171549
147 661
149 136
152 934
153 7*2
14*313
154 869
153 486
153 6*1
150 482
153 690
147 363
147 844
150 560
153 332
171 352
192 607
681 OTS SB-442
-AaaljrMa
-Carroatve eftacu
-OaaattawlOB
-Blactraiyala
-rtKlfl^KlaB
131
257
393
630
479
*3*
*3*
122
123
479
639
807
103
121
122
123
131
234
3S2
477
4*0
639
6**
806
808
153
177
106
2
97
463
782
99
30
70*
274
839
331
615
39
40
160
389
712
160
712
566
148 703
153 726
153 440
149 089
152 978
171503
171503
150 SIS
171 123
171 478
153 160
171 519
150 872
150 836
150 837
150 838
150 S39
152 035
161 288
148 703
171 314
171 315
153 633
171 316
171 317
150 338
154 071
171 318
152 149
171 184
161 576
150 517
150 371
150 708
153 171
154 704
171 130
193 ON
^Mea
Hie WHumber
Se«ke«pln(
Scaling cctnpouida
--Developmcm
Search radar data
--Nonngrapha
Saarcb radar recelvera
--Deatgn
Search radar acanner*
--Dea(^
Search radar ayMem*
--S^pwl to notae raUo
Search radar ayatema
(LtaaHl)
--Equipment
--RaUablliiy
Secondary emlaalon
--Ibtatbematlcal analyst*
Sadlmeatatlon
--Aaalyaia
-•BtbUograptiy
—Lake Mead
--Mathematical analyal*
--niyalcaJ propertle*
--lUdiaacttvlty
Seed implaniatlon (lai
Seiamlc vavea
"Aaalyaia
"fropagatloa
Saleroograph*
--ApfiUcailoos
Selenidea
- -Propertlaa
SeleaiiBn
--Cryaul atructure
Selenium (Uquld)
--Polymertatlon
Semantic*
SdmlcoDdualng fllma
--Teal reauba ^
Semlcooduao-a
--AppUcatlona
--Catalytic propertlea
•-CoBdualvlty
--Cryatal atructure
•Deaign
•OBvelopmem
—Bflacta al radiation
-•Blactrical propertlea
- -Electromagnetic
propertlea
-•Electron tranaitlona
194 970
--Heat tranafer
--tanpirttiea
193 571
171344
-Mater UU
149 739
194 809
171030
'
171 031
■
171 129
171 344
154 245
171 129
154 679
154 746 ,
440
440
590
58
573
578
48
567
577
623
32
619
704
32
609
413
619
144
411
704
462
558
793
344
699
S06
113
213
806
49
99
163
334
569
570
622
718
472
109
344
MS
469
629
795
44
111
113
212
344
211
342
346
421
469
475
625
bit
629
796
210
626
794
49
109
SOI
110
470
44
210
211
212
342
548
630
793
794
152 689
152 689
171 107
ISO 684
150 894
153 203
150 608
153 248
154 844
150 717
152 645
154 417
149 216
152 643
154 339
147 311
154 417
152 570
153 422
149 775
153 395
153 075
153 923
152 92S
171 575
lS3tOS
150 812
149 667
154 071
150 609
150 473
149 720
149 297
153 736
153 268
154 S43
155 2S8
153 147
150 686
152 92S
149 679
153 552
153 932
171 573
150 963
150 603
150 537
153 2S1
152 462
152 91S
152 473
152 628
153 001
171 406
171 377
153 873-2
153 873-1
154 770
148 016
152 760
171 511
152 199
150 609
150 666
154 868
150 501
147 120
150 963
152 760
149 706
152 434
171 177
149 706
171 340
153 233
153 264
153 S49
150 545
SU>Jea
Page rv Number
Si^ea
Page
PBNianber
Sublect
Pap
FB Number
Semlcooduaor* (con. )
ShicUllng
Shrouded propellera
•-Mathematical analyaia
114
150 525
—Bffectlveneaa
785
154 697
--Aerodynamic
432
153 169
•-Materlala
101
150 687
cfaaraaeriaQca
287
152 >M
--Fhyalcal propertle*
210
148 690
782
155 429
--Effectlvcneaa
746
153 72S
— Propertle*
111
150 784
f
155 431
--Hrformance
38
150 783
346
152 694
•
155 432
711
153 642
—Surface pro|iertlea
113
150 811
784
155 322
--Preaaure dtatrlbudon
287
152 89*
150 812
155 428
--Teat reault*
564
154 504
21 S
148 671
SUp bulla
--Thruet
746
153 725
• *■*
149 667
-Deatgn I
441
153 632
-Wake
38
150 783
793
153 849
--Materlala
182
171 168
Side -lobe auppreaaion
49
150 597
••Temperaiurc factcra
44
150 963
--Model teei reault*
745
153 706
Signal generator*
469
171 187
--Streaaea
585
171 576
-CalibraUoD
422
171241
--Theory
■627
153 819
--Structural analyal*
62
152 797
171349
SeBaltlzatioa
543
148 9SI
'»
440
153 953
434
171 344
Senaory perceptioa
- -Surfacea
62
150 459
Signal generatora (RF>
--Analyal*
10
150 638
--Vibration
745
149 745
--Calibration
434
171 346
-InhiWtiar
685
171 610
SUp model*
Slgnala
--(>*ychologlcal factor*
599
152 837
--Te*i reault*
586
154 067
--Contalnera
99
190*29
--Teal reaulta
137
150 887
Ship plate*
--Detection
973
194 949
Sequeoclal analyaia
186
148 683
--Fracture
585
171 576
154 946
148 906
SUpe
--Derdapment
160
152 079
761
ia907
— Uaai effeaa
441
149 520
Silica gela
.-'
764
lasss
--Deatgn
440
153 953
--Surface propertlea
410
154 395
--Applicatlona
317
152 883
••Bqulpfneta
744
155 253
SlUddaa
594
153 688
^ ••Flreprooftng
742
155 250
--Cryatal atruaure
114
171 121
Sergeant
309
152 988
--Hydrodynamic
214
152 459
Serle* expanalon*
77
152 100
charaaerlatic*
S8
150 737
152 499
184
152 162
176
150 391
SUIcca
•-AppUcatlooa
78
150 993
'-Maintenance
744
171 251
--Applicatlona
732
194 479
79
150 466
• •Mater Ul*
758
154 281
- -CoaducdTiiy
311
149 0*9
319
152 376
—Model teal reault*
176
150 391
--Dielectric propertiee
943
149 628
574
153 677
-Mooring
746
154 676
- -DUfuaion
211
149 0*3
Sarvomechaniama
—Motion
90
150 842
753
193 914
--Applicatlona
44
152 311
--Performance
440
152 689
--Impurltlea
213
1S2 186
434
153 442
.- -Propulalaa
64
152 130
470
147 1»
568
149 090
- Vibration
310
153 793 ,
*30
193 ««
584
171 496
SMverlng
113
193 U*
,
585
171 553
--Inhlbttlan
270
153 349
313
19318*
735
150 903
271
153 330
Silicon carbide
--Equipment
581
171 481
153 350
--Impurities
211
193 494
171 482
--niyalological effeoa
11
150 216
6r
199 «*3
171 483
Shock
--Riaae atudie*
447
171 1*5
--Operation •
5
152 300
-Spectr*
769
151 932
--Spectrographlc analyaia
311
192 434
--Theory
581
171 480
Shock avoidance apparatua
686
155 575
Slllcan carUde cryaula
SC-21AJ generator
422
171 243
Shock tubea
--Grooth
346
152 628
9C-21AAJ generator
422
171 243
- -Applicatlona
58
150 454
Silicon compounda
Shaft ai^le dlgitiier
58
150 329
194
152 426
- -Chemical reactlona
551
171 522
Shafta
,
439
152 829
Silicon compounda (Organic)
--Imarference
747
154 646
^-Heat tranafer
217
148 682
-Combuation
549
171938
Shaped charge Hnera
Shock wavea
Silicon cryatala
--Performance
436
150 068
--Analyaia
214
152 561
- -AppUcatlona
109
192 959
Sheeta
700
154 509
903
192 669
--Boundary layar
327
193 738
--Attenuation
S*
190 957
--Surface propertlea
U3
150 811
607
153 262
--Chemical effecta
448
153 173
213
149 6*7
•-Cavitatioa
328
149 640
-Dlffraalon
772
155 000
793
153 849
--Corroalco
615
171 501
--Ionizing effect*
699
149 085
Silicon diaxlde
•-Oeformatlon
325
153 109
••Mathematical analyal*
607
153 428
--Abeorptlve propertlea
213
152 186
602
153 739
I - -Meaaurement
347
153 626
--Conductivity
210
149 669
--Fracture
589
153 661
474
153 466
--Surface properttea
113
U21*5
611
153 928-1
-Oeclllatlaa
336
171 302
Silicone reaina
r"
153 928-
I --RKXographic aaalyaia
308
171 352
--Adaorpllon
947
14* 7S*
- -Heat tranafer
336
•152 947
--niyalcal effect*
176
15^256
--Appllcation4
753
171 6*8
459
171 396
194
148 701
Silioane rubber
7*2
196 432
612
153 565
148 702
Sillconea
--Hyxlrodynamlc
408
149 731
--Applicatlona
30
149 346
char*cier>*tlca
328
149 640
t
552
152 612
- -Propertlea
782
1SS4S2
-- Hyper aonlc
739
171686
Stiver
character istlca i
iJ"
150 347
--Preaaure
58
190 957
- -Conduct) Ttty
787
154 8*4
1
^\*J7
153 315
772
155 0*0
--ratrueion
627
159 899
?770
149 328
--Propagation
192
193 446
--Oxidation
549
153 8X7
•-Laminar boundary layer
455
153 092
346
193 912
--rhyaical effecta
210
148 690
— MaterlaU
%
171 083
476
14*525
Silver acetyUde
--Mechanical propertlea
200
161 786
608
154 745
- -Chemical reecttona
145
148 680
779
153 752
'•-Propertlea
466
159 073
--Detonation
59
150 970
780
153 750
--ReOectlaa
*9
ISO 531
Silver chloride cryeula
153 751
SO*
149 633
--Deformation
343
193 891
— Oectllatlon
328
152 906
606
193 475
472
193 964
•-Preaaure dlatrlb«alan
326
171 302
786
149 940
SlIvOT cryaula
•-Production
66
isia*s
--Theory
327
152 537 ,
- -Ocfonnation
6r
193 899
••Su-eaec*
93
171 0*8
607
1991*3
Silver electrode*
118
190 738
632
193*96
- -Electrical propertlea
407
192 871
t
603
154 766
,'
636
193 464
- - Blectrochemietry
36
190 396
1
708
155 090
--Thermal affecta
454
149 676
Sliver iodide
•-Tanalle propertlea
66
330
151095
171 044
- -Thickneea
Shoea
606
152 895
Silver oxldaa
398
149 736
-Vibration
325
152 632
--Cleanlag
464
153 516
--Aaalyaia
165
149*97
604
153 638
--Molaturc factora
592
153 491
- -Electrochemiatry
407
492 871
153 639
Shopair
39
150 101
Simplex ayatem
SSI
192 7r
Shelter occupancy teat
585
154 503
Short take-oA plane*
563
149 354
Single cryaula
Shelter*
149 355
-Color
470
147 174
- -Constructicn
966
153 996
Shroud antennaa
42
150 958
-Oraap
44*
171 9M
69
*(
atagte crytcala (cob. )
--DifoniiatlaB
-Btoctiical propertle*
-Practur*
P^t UNymtxy
ic ^ up«rae«
PDtjrmorptiinri
apactrograpUc aoalysla
cryaJa Qtlwtlltgp)
-OyKal Knicnir*
~ B toctr odtentt Kry
-BtaetroB traaaltloaa
-Pmlpie
ItrKsKa
636
794
34S
343
*27
s»
346
344
7«
794
JO*
36
214
39
111
610
613
111
416
S6S
34
S
465
S3
711
an
603
306
--TrafflcatatUty
- I— ornlngtrti taeurm
rKiw tectort
- -Gcnjcructlaa
3U
M5
7M
7IS
420
S«6
714
7U
2H
766
430
S«S
717
438
717
430
717
313
313
t properties
Sodal commumcatlon
--Bcoaomlc aapccts
•-?ufchote0<»l (actor*
--Taat metboda
--T*»cry
•-VlaMBl teeters
Sodal datfratatUty
Sodal adenoea
--Theory
cUorldt
-Gryaul «ructure
-Matallvgical effeas
dUortda cryataU
234
•
396
394
10
123
•
isi
133
234
SodlaBCjoMd
5SL
779
343
414
149 6M
1S3 729
laosst
171 3S6
149 664
171 S43
1S0S41
110SS7
169 731
152 932
134 063
146 761
153 076
132 069
1S2 4U
192 4S3
152 494
171079
190 666
153 296
154 667
150 666
266 133 326
153 334
154 606
146 2S7
152 300
153 510
152 615
171 994
192 261
171 531
153691
171 353
152 S9S
193 S96
306 152 99S
171 190
153 9S6>
146 33S
194 644
171 375
193 596
194 619
194 644
192 941
190 648
171 375
153,596
154 463
171379
154 463
153 517
154 463
193 330
193 330
709 146 400
193 315
190 490
153 166
193 217
150 691
190 496
190 473
153 166
146 197
153 135
152 114
133 152 264
152 664
153 295
149 664
190 721
Suttma
SocUuni hypodilorlte
--Dacoaumlnatiiig effects
Sodliaii Iodide crysuU
--LuBuneacence
Sodiian oicrate
--OetoDatlca
Sodtum-tiaigatefi alloys
--CryataJ structure
Soilcruaa
SoUa
--Aaalyals
--CoatamlnatlcB
--Broslcn
--Heat tranafer
-•Mechanical properties
-Moiaiurc conenc
-Moisture (actcra
-niyslcal properties
-Ra<lloactlvailoB analysis
-RadloactlTlty
-SUlallzatlaa
-Straaaea
-Teat u»s|ho«1s
-TrafflcaMllty
Solar atmoapheTe
- -Radiation
--Spectra
--SpectragrapMc analyala
Sotor banerlea
--Development
Hge n Ntanber
Solar energy
--Abaorptlca
--AppUcatlOM
Solar flarea
• -ClaaaiflcatlOD
- -Blectrcmafnrtlc aOeaa
--Maaato-eineac
--Kadtatioo
Solar furnaces
--AppHcaUcaa
•-D9««>a9Maa(
Solaraolse data
-Analysis
Soiendds
--AppticatlaBS
I
SoUd deUy lliKS
--Oesi(n
SoUtto
--Catalytic propertlea
--Creep
•-Gryatal structure
--Deforniatlon
--Dltruaioa
--Blaaildty
-Mapirtic prcpenlea
-Mathematical analysis
-Molecular structure
-nyalcal properties
-Propertlaa
-SU'esaes
-Surface properties
70
713
341
797
to*
31
711
32
67
751
1
284
1
39
332
97
40
161
161
40
67
384
716
717
3
3
396
599
3
4
439
977
731
661
311
343
740
131
681
199
415
5
331
26
474
217
392
560
736
27
630
627
73»
148
192
46S
213
617
111
313
344
795
4«S
630
345
794
603
110
194 679
152 731
173 149 670
153 721
154 644
154 339
190 617
153 643
190 444
150 445
150 999
152 006
152 009
ISO 614
150 61S
153 884
ISO 616
150 862
153 071
152 000
171 OM
149 699
149 699
150 436
171 098
ISO 998
150 999
153 864
154 667
154 630
149 00?
190 939
152 946
153 081
153 054
150 936
153 645
153 602
154 535
154 536
193 718
149 706
149 706
171606
148 713
154 585
150 668
153 197
190 801
153 916
190 627
193 466
153 473
153 873
153 613
153 616-1
153 616-2
153 870
735 199 073
193 136
171 049
171 543
171 686
148 676
148 735
154 391
148 671
171 491
ISO 603
153 351
152 462
171 573
154 291
147 848
149 690
150 642
153 767
152 036
Sl^fifT
page
n Number
SaUda(caa.)
f
--Temperature factor a
801
148 970
802
171 619
properties
348
a 171 329-1
V 149 690
--Wa»e tranamlaaton
345
453
152 904
475
147 400
476
148 525
—X-ray analysis
471
152 982
Soludoas
--Electrical properties
554
171 530
--Luminescence
796
153 936
--Riysical properties
702
148 747
--Propertlea
146
149 701
- -Thermal propertlea
554
171 530
Sonagrams
156
149 069
SoMr equlpmeM
- -Hydrodynamlc
char act erlailca
774
154 165
--Maintenance
536
153 561
Sonar peraonnel
--^rformance
136
152 156
364
152 888
399
153 126
153 141
-•Salection
134
152 121
--Training
536
153 561
Soaar signals
--Detection
364
152 888
39:i
153 141
Sorting f
765
155 376
Sotaid
--Abaorptlon
791
153 062
••Attenuation
787
153 906
— niyalcal effects
633
171 485
••Propagation
53
171 069
475
147 400
787
ISO 198
--Paychoiaglcal effeaa
396
171 403
"Theory
104
147 832
630
149 069
--Velocity
25
ISO 458
Sound transml salon
--niysical (actora
787
190 198
SouBdlag rockeiB
--Deaign
175
171 180
— Bqulpmeni '
35
150 873
*
43
ISO 958
53
ISO 931
434
153 442
-- Meteor ologlcal (actora
34
152 189
Space chargea
--Elearical eflecta
337
149 729
623
150 717
— Btectromagnetic effecta
45
152 309
301
152 938
430
153 504
723
148 323
789
ISO 414
--Mathematical aoalyals
574
153 503
727
1S0 9()2
Space rUgbl
439
153 065
--Aoalyals
61
ISO 886
-Hazarda
157
171 147
--niyalcal effeoa
662
171 601
171 611
--niyalologlcal effeaa
7
130 372
14
ISO 439
ISO 440
121
ISO 838
268
152 460
542
153 402
--Paychoiaglcal effecta
265
152 764
--Simulation
36
148 274
263
152 744
435
153 408
710
153 695
--Theory ^
308
152 939
Space medicine
690
155 574
--KbUography
272
171 029
--lnstrumei«atlon
14
150 440
Space obleda
61
150 989
Space perception
--Analyala
394
153 424
--nbliography
268
153 575
-Test methods
392
153 470
Space radiation
206
153 258
Space reconnalsasnce
307
153 100
Space suits
206
171 143
S<iilect
fr
Svb^ea
PjE
re Number
Subled
p»r
m Number
Spaceahlps
Stability
Steel (con. )
--Control systems
737
155 291
--Determination
306
153 058
-FaUgue (con.)
612
154 759
155 252
■-Theory
609
149 782
-Forglag
612
151 102
-Design
121
ISO 838
SuUllty lodicatora
-Fracture
611
153 928-1
441
171 418
--Design
189
152 302
153 926-2
• -Equipment
740
171 60S
Suinless steel
'
778
151 106
"PU^paiha
61
ISO 886
- -Corrosion
96
161 749
- -Heal traatmeat
330
161 213
-MaiarUla
537
151 101
615
ISO 502
459
171 396
--Propulalon
178
153 662
- - Forglrv
612
ISl 102
778
171 188
310
148 777
--Fracture
331
152 880
--Internal friction
331
152 691
153 387
460
153 167
776
154 493
312
152 749
92
151 096
- -Mechanical propertlea
40
152 355
• i
152 959
--Riysical propertlea
92
161 218
199
151 072-R
748
155 345-1
- -Temperature (actors
610
161 231
390
151097
- -Reliability
580
154 811
-Wekhag
286
149 718
"
SB3
153 551
--Rochet propulsion
61
150 886
445
153 263
-"'-^
778
150 780
Spade
334
153 821
Standing wave indlcatora
^
154 870
Spaeroliee
169
148 717
- -Testing equipment
292
171 204
)
171253
Spark machining
- -Meldag
92
161764
--AppUcatlona
313
161 225
- -Measure meu
292
171 204
- -MlUtary requlreraenii
200
161 786
Spectral emittanoe
590
171 515
424
171 233
-PlckUiv
92
152 660
Spectrograptuc data
791
ia939
171 234
--Sireaaea
768
154 958
Spectrometers
171 235
- -Tenelle propertiea
92
171077
--Appllcatlooa
340
152 714-4
Sur trackers
330
171044
-Deaign
222
148 663
-Design
718
171609
499
171396
341
152 713
Sure
-Teat reaults
91
171066
SpectroptMiomecers
--Deiectiao
533
150 322
-USSR
329
171331
--AppUcatloos ;;
409
153 451
534
153 452
Steel caatiogs
r
787
154 161
--Energy
534
153 452
--Developcnent
91
171069
Spectroecopy
339
152 864
--Ideotlflcaclon
535
147 325
- -Mechanical properties
611
171524
--AppUcatlona
336
149 728
-tModon .
117
147 908
Steel tubiiv
465
ISO 922
"Riocafrft^y
259
153 278
- -Corrosion prevention
781
154 612
Speech
-RadUtion
156
152 471
Steel wire
104
ISO 494
257
152 834
' -Fhysical properties
612
154 419
1S7
152 389
- -Sprectrs
3
150 999
-Sufaetitutes
612
154 419
•
152 390
Starvation
Stellar eclipeea
478
153 430
-•Riyslologicat effects
12
152 028
- Analysia
534
147 323
637
153 871
152 029
Step acanner
463
150 708
153 87S
152 030
Steeped zone mirror
106
150 415
Speech tranamisslon
1
13
152 031
206
152 201
- -Effectiveness
6S7
153 871
688
154 168
Stereochemistry
697
154 564
-IntelllglbiUty
55
148 972
Siatlatlcal analysis
187
148 667
171563
122
152 172
561
171 510
Stemida
134
152 255
- -AppUcatloos
449
153 385
■ -Determination
270
153 327
452
153 455
.
748
148 09S
Stereoregular polymers
696
171 570
Spheres
\
807
152 114
Steroapecificlty
697
171 563
788
146 998
--Equipment v^
81
ISO 649
Stiog aupport Interference
193
153 379
■Elaatlcity
104
192 134
-ReUabiUty f
281
152 769
Stocfaaatic approuinatian
78
ISO 600
324
148 406
-TsMaa V
184
171 161
Stochaatic proceaaes
320
152 900
--Heat trsnster
218
192 784
---nwory
184
152 162
Storaf* batteries
--Prepsrstloa
444
190 706
185
152 161
-Electrodes
S3
130 843
--RadUtioa
206
147 966
187
148 664
- -Tempersture factors
729
154 550
ISO 835
318
171 312
Stora^ progrsm tests
S84
171 111
--Reflective eflacta
154
152 592
,
321
171327
Storage tanka
219
192 2S6
450
150711
-Haodbooka
715
154 671
.
598
199 966
595
153 665
Storage ti^iea
625
193 123
596
153 832
-Design
43
152 092
■ -Stresses
339
192 779
153 840
568
153 809
768
171664
597
152 956
569
146 656
Spheroidal wave flinctlone
598
153 669
452
152 928
-AppUcatlona
206
147 965
759
149 750
566
171 504
Spin rstea
542
171 046
760
154 096
171508
Spinal cord
762
147 847
Storms
- - niyslology
542
154 099
154 094
--Detection
705
154 532
SptneU
154 124
--Radar analyala
30
190 420
--Theory
629
153 699
763
148 748
ISO
152 207
Spiral antennae
52
146 995
154 349
280
152 774
Spiral warp mediod
749
153 917
Statiatical diatrlbutlona
595
153 66S
555
153 390
Splrodietoeia
StaUatluI functions
320
152 900
Strain gagea
^
-Bibliography
404
190 062
Siatisticsl Inference
761
148 906
-Design
IS
152 033
Spoalng charfea
148 907
Strainers
-MaterUla
437
ISO 097
Sutistical teaia
186
148 692
' -AppUcsnons
309
171091
Spray tanks
Staiiatica
763
155 068
St rakes
195
171 135
-DeelgD
743
154 655
-llMory
186
148 692
Strategic materUls
444
147 534
Sprays
317
152 883
-Development
610
171 946
--Production
743
154 655
596
153 833
Streak camera
341
171 191
Spriofs
597
153 834
Streamline
196
152 739
-MaterUla
740
155 146
761
154 123
Stress analysis
460
153 on
Sprue
Steam
603
154 765
-Padnlogy
690
153 714
■ - Thermodynamic properties 802
148 353
%
154 766
Sputtering
622
171 513
Steel
749
171 568-2
S<|uare root method
763
159 066
-AppUcatione
713
194 636
--Applicstioas
453
153 386
Squid
64
192 193 ,
714
194 613
766
171664
192 155 1
715
154 666
--Equipment
718
154 644
85
190 951
718
154 652
--Theory
159
152 832
118
190 933
-Availability
330
151097
324
149 796
178
192 194
- -Chemical effects
213
152 186
452
147 401^
328
144 669
--Corrosion
615
171 SOI
602
199142
446
193173
- -Bftocu of rsdlsdon
778
171 188
604
153 749
547
193 666
-Ejctnislon
330
151097
776
155153
366
154 104
562
171 529
797
ISO 053
634
154 432
--Fatigue
67
152 642
Straaa concentration (actms
461
171 410
.
703
ISO 939
92
171 066
Streas atrsin curvca
462
161896
'
190 994
94
150 877
Streaeea
603
148 346
71
n Mwwwi
3M
Scrip mapptag 427
Stnaitiuin Ho«cy (lUdtaactlva)
- PrcclpiEaaaa 1
Stroatiian ooildM
StroadoD titaoat* cryaAla
-Dlaiectric propertle*
--ReaaoBnce
Stmctural men la
Simctunl (lialla
- -DaformaOOB
■•Ctmp
- -Dafci maUoa
-•BlawlcHy
— Loatfdiatiibaclaa
•-MadMalcal propertica
--Optical factora
-Vlkrauoa
STU-1
Scyrwa polysara
-•OMMBdaa
Scyrasaa
--Myiiilnikm
Sutaiarlae bulla
--Acooatlc propertiea
--Maat cflacia
-Matartala
--lUrabOQ
--Wava (ranamtaaioa
Sidmaiioe aoiaa
-Reductiae
SufeBartae peraooael
- -I^at BiailiadB
StAoariaea
-Haat eflecta
- - Propulaioa
--Sainy meaauraa
--Threat
SuimliiUnira elactroo lubea
- - Develofmieac
Sutaniaiacure electroalc
a<|iitpnwnt
SubaoBlc fkm
-Turtiitaaca
Sulfaiea
-Oetermi nation
SuUklea
- -OUpraportiaoaUaa ^
- -CrjMal acructora
- -SyMkaala
Sutfur
- -Appttcacloaa
-Ckainlcal reactlaaa
-•[Xalectric propertiea
- - Separation
754
797
111
76«
4SS
708
83
602
76*
602
769
2S9
40
328
716
83
83
431
9M
57
14S
316
332
119
796
745
62
744
119
744
537
441
462
309
609
170
53
304
770
144
Z76
627
783
25
626
777
149 718
153 396
150 614
150 615
155 239
154 on
150 666
154 958
150 853
153 734
155 090
1S0 416J
148 811
148 813
150 739
147 4021
151 932
171 192
152 355
152 906
154 647
150 416
171 070|
153 221:
153 144
150 664
152 218
149 963
171 041
190 879
153 904
153 707
152 807
155 413
150 879
155 413
154 831
149 520
153 407
171 046
171 061
154 431
149 716
161 890
152 670
150 866
152 393
152 478
154 097
154 118
155 254
190 334
153 649
171 384
Subjact
Sutfur cofnpouoda (Organic)
--Oemlcal reactiooa
- -Molacular atrucnire
Sulfur (UoxKla
-Spectra
Sulfur oxidea
--Ckemical reactiona
Sun
- - Riottifrapfay
--niyalcal i
--Wave tranamlaaioo
Suparserodynamica
Su|iaratk>ya
Supercooductirltr
- -MeaauremeBt
--nijralcal bctora
Si^wrcooductora
-Acouatic propertiaa
Superelevation
Superoxidizera
Superpoarer catltod )
Supe r refene ration
Superaoaic airfotla
Drag '
Superaonlc now
Ibuadery layer
-IMactMmatlcal analyaia
• -Maiaoi'ologlcal tacura
-Tatolaa
Superaonlc noszlea
Analyaia
- -Configuration
Stqieraoaic wind tunnela
- Aconauc propertiea
-Boundary layer
- OeatgD
- -Electrical factora
-Preeaure dtatrlhution
Suppltea
' - [>eterioraUon
[Xapoaal
-Sdiadulli«
Supply depota
- -Simulation
Surface -active agents
- Effcctiveneaa
■-niyalcal effccta
Surface fllma
Surface targeta
Radlauon
Surfacea
-Adaorptive propertiea
-Caulytic propertiea
--OoaUafi
--Prtctka
72
'm
mNuniiar
Subtect •-,■•■
~e
ra Number
409
193 451
Surfacea (coo.)
'"[-'■ "
276
152 746
--ftyalcal propertiea 623
153 768
- -Recording devicea 62
150 459
277
153 158
-■ Reflective effecta 119
152 616
■ Temperature 85
150 621
698
154 118
Surfacea (Mathematica) 600
153710
762
154 452
-Analyaia 186
152 374
-Theory 450
153 433
223
148 299
Surgery
317
171 042
-niyaioloflcalefiacta IS9
152 766
737
153 947
Survival
2
150 S73
-Arctic regtooa
«S
~ 150 571
681
153 718
263
153 325
132
152 391
269
153 344
196
152 480
397
153 524
773
154 158
441
153 540
776
161 236
-Oletary tactora , 12
153 oaa
152 099
796
152 220
193 030
797
154 232
13
193 081
346
152 901
397
493 924
Survival kita 102
171 119
- - A rctic reglona ,'. 335
193 346
109
152 144
Swttchea (RP)
«
738
153 866
-Teat reaulta
150 698
702
171 255
Switching circuita
337
152 962
AppUcationa ! ^ 491
19>3a02
42
152 194
-Deaign i 167
153 236
170
149 716
172
192 3a
207
192 520
454
150 069
-Developoient 214
192 561
767
148 231
604
153 743
806
150 227
193
152 260
-Bqulpniem SO
149 773
197
152 492
576
154 771
456
154 403
-Materia la 95
171 066
770
171 593
- Mathematical analyaia 601 ,.
171 548
773 ^ 154 158
Syndteaia 299'
152 750
325
152 602
-Temperature tactora 735
155 321
454
153 477
-TTieory 167
153 236
429
153 579
457
153 378
575
171 549
36
152 647
601
171 555
719
149 816
326
152 529
Symbolic logic ' tOt
171 548
193
152 758
Syndiroirona i
173
152 435
Dealpi 1, 462
152 866
325
152 602
326
152 529
Synthetic alloya 777
Syndietlc ftbera
154 536
619
153 149
-Color 111
171 153
103
152 124
-Development 793
171 612
103
152 124
-Plreprooflng 180
171 136
600
153 782
- Mecfaanica 1 prope rtiea 589
171 494
638
153 691
-Propertiea 73
150 548
749
154 869
-Temperature tactora 143
153 010
759
149 558
Synthetic lubricanu
-Developmeni 756
155 062
583
153 660
Materiala 992
Synthetic mica
154 969
713
171 479
- -CryatallizaUan 630
154 515
199
152 147
79i
155 154
201
171 150
7W
155 155
155 156
792
155 437
155 157
Syaiem reaearch 121
150 836
550
171 512
150 839
28
152 152
Syaiama engineering 561
171 510
25
150 334
734
155 260
335
153 570
-Bibliography 477
153 129
90
150 952
152 914
192
148 674
-Theory
262
152 757
Subject
T54EI
Pye
Sf3
m Number
194 769
Subject
Tellurium cryamla
fME
PB Number
S<ri4ect
Tbermochemiatry
1^
PB Number
407
171 576
Tachiatoacopes
- -niococonductlTlty
625
153 456
700
154 709
- Applicationa
684
154 063
TEM diode
425
159 579
--Inatrumentation
147
152 679
Tanalitfa
182
171 167
Temperature
Thermocouplea
MS
171 170
--Determination
283
152 669
--AppUcationa
802
154 SOB
171 171
803
154 720
- -Bibliography
16*
OTSSB-430
Tairiu
• -Meaaurement
45
150 318
- -Shielding
31
152 070
-Fire control ayatema
738
153 8661
347
153 626
Tbermodynamica
767
153 930
Tanialam
634
154 722
-Tablea
80*
171 567
- Bomtaa rdment
619
147 553
802
154 SOB
-Theory
473
150 688
-Caaiing
458
151 098
--Northern hemlaphere
803
154 449
578
154 190 .
Tapea
992
171 486
Temperature control
733
154 198
Target recognition
-Equipment
573
153 246
154 199
- Study and teaching
683
150 916
Tenaiometera
Themoalectrlclty
548
153 293
- Viaual factora
263
153 387
- -Calibration
338
171 303
552
153 836
269
152 605
-Deaign
63
150 868
629
154 770
4 "'■ ■
395
147 533
Tenaion cootrollera
751
154 698
730
171 691
664
154 063
Teoaor analyaia
192
152 163
788
152 061
Targeta
Ternary diagrama
199
171 154
794
152 199
-Configuration
6B4
154 063
Terreatrial magnetiam
802
171559
-Oeiectlan
269
152 605
--Analyaia
332
149 650
- -Bibliography
168
OTS SB- 432
428
153 225
392
150 722
Thermolumlneaoence
212
152 451
491
143 302
-Meaaurement
207
152 159 ,
Tbermopilea
1
«M
154 064
788
194 102
-Bibliography
111
I OTSS8-430
Tarur
61
150 626
-Sourcea
207
152 158
Thiazolea
^
Taak aummariea
138
171 000
-Theory
202
152 639
- - Propertiea
695
154 269
144
171 001
207
152 158
Thin fllma
1 . 1
157
171 004
152 208
-AnalyaU
201
152 261
» i
305
171 002
Terrier
61
150 626
--AppUcationa
298
152 672
206
171 003
583
153 487
--Conductivlry
797
154 232
222
171 005
Territorial watera
479
153 121
--Electrical factora
789
148 757
Taylor-Maccoll equation
772
154 583
Teat faking
536
153 604
796
152 220
Taylor aeriea
Teat aeta
- -Electrodepoaitlon
171
149 660
- Applicationa
77
152 109
--Deaign
42
152 192
- -Heat treatment
610
153 701
-Theory
594
153 139
162
148 284
- -Maptetlc propertiea
81
149 593
Tchebycheff inequality
321
149 663
433
190 712
82
150 767
TDU-4 B
709
193 861
420
150 703
207
1)2 520
TDU1(»
709
193 861
--lyrfqrmance
729
154 660
610
153 701
Teaching machine/
199
152 164
Teat veblclea
796
152 220
360
153 460
-Teat tacllitiea
419
152 716
171 569
Team training
134
149 962
Teaiaa
- -Optical propertiea
469
153 094
Teedi
- - Fhyalology
22
150 562
- -PreparaUon
601
1501)73
- Chemical analyaia
18
150 239
Teau
731
171566
- X-ray analyaia
544
153 865
--DealfB
477
153 927
-Propertiea
167
152 365
Teichmuller apace
186
153 374
Tetradymite
• 627
154 0»7
346
152 901
Tektronix ISOA generator
422
171 241
Tetrodaa
621
148 349
Telegraph jignala
-Teat reaulu
1 296
149 694
Thorium
Coding
289
152 926
Textllea
-Propertiea
719
153 907
• Telemeter ayatema
--Coatlnga
73
190 962
Thorium oxidea
- -Deaign
45
150 318
--Deierioratioo
448
171 417
--Phaae atudiea
754
152 980
730
171 690
--FIreprcxifing
180
171 136
Thrombin
174
150 797
Theodolltea
- -Fhyaiologlcal etiecu
690
154 437
737
153 648
-Applicationa
34
152 189
Thruat atand
586
153 449
741
153 890
411
150 705
Thunderclouda
-Equlptneni
174
152 063 «
Thermal radiation
-Electrical propertiea
705
154 532
490
150 707 •
--Abaorption
307
153 885
Thyratrona
434
153 235
-Analyaia
35
148 255
--Development
163
150 074
983
193 487
708
154 556
Thyroid glanda
Telemetering recelvera
-Mathematical analyaia
194
148 730
■ -CUmatic factora
398
153 372
- • Equipment
427
153 950
- -Meaaurement
474
161 228
-Fhyalology
15
150 219
-•Operation
427
153 951
--hthoJogical effecta
546
154 803
269
153 344
Telentetenng iranamittera
- -Riyaical effecu
589
154 754
403
153 515
--DaalCB
174
150 798
-Theory
217
161 222
Tie rod yoke
746
154 649
Telapiione cablea v
Thermal atreaaea
Tlli-wtng
563
149 354
-Cori'oalon
729
154 624
-Analyaia
422
171 416
149 355
Telephone communication
--Maifaamaiical analyaia
88
150 853
710
155 2S»
ayatema
117
130 474
Time
- Circuita
167
351
153 236
152 933
118
190 798
193 061
- -Meaaurement
Time-Interval countera
'j67
153 249
- Development
171
152 513
801
148 948
--Applicationa
567
153 249
573
153 803
»
148 970
--Development
334
153 621
--Equipment
579
730
153 228
154 639
--Theort
Thermloni^ emiaalon
603
42
153 767
152 040
Tinte mark generator
Time aeriea
422
171341
Telephoio lenaaa
-Teat reaulta
Teleacopea
■Applicationa
233
131
152 567
148 669
43
44
150 815
150 813
150 814
150 816
-•AppUcationa
--Theory
450
594
759
762
150714
153 600
149 750
154 094
154 134
153 478
--Deaign
259
153 271
105
150 424
T^letypa ayataaM
156
150 217
Tlmera
437
--OrmlopiiiaM
300
148 282
208
152 538
Timing circuita
--Deaign
--Development
- -Maintenance
Tin
--Equipment
Televelofax
Televlaion
- Applicationa
174
151
100
150 798
150 388
152 39fr
,
295
571
622
719
152 735
153 421
153 823
153 907
437
430
491
153 478
153 084
193 221
Tkleviaion cameraa
-Applicationa
580
533
171 lOB
150 322
-Btbllugraphy
--Mathematical analyaia
723
168
106
154 450
UK SB-431
148 254
■ -Conductivity
Tin compounda (Organic)
--Ctaaaucal reactiona
797
696
194 232
171 571
Televialon equipment
-Deaign
302
161 9«6
296
467
152 610
153 683
--Syntheala-
274
547
'30
149 683
192 877
150 488
Tellurldea
- -Electrical propertiea
471
150 323
Tbermiatora '
937
152 962
- -Toxic effecta
Tin cryatala
-Electrocfaemlacry
Propertiea
627
793
154 097
153 923
■ -AppUcationa
• -BtbUography
804
168
154 440
GTS SB-429
35
171079
)
1
Tbtrmabalance
694
153 163
73
Tins
---ftM
Tlroa
AdMrptive profvrtiea
rmture fictora
-Cbenlcal reacdoaa
OUfuaioa
-Eztruaion
--Mackanlcal properties
-PMrtflcMlan
TloataB alloya
-AMrilcackMM
--■nsiat
--Cnap
- -Crymtal strucnire
--Fatigue
--Forflnf
-HMt trvetnent
-Mackanlcal pnpnxifm
-MMaUurglcal aaalysla
I aludlea
--T^MiyaTatuFa fccioii
Tltaniun) oxides
--Crystal structure
irs
Tlcradoa
na trices
ToofHe ct (be ocean
Topokv
-Theory
- -Mathematical analysla
- Meaauremeac
Tory ll-A
Toco
Tovsd bodies (Aerial)
-Dtm
Tcnrtag caMes
- - Test reeulu
Traca
^
mNwnbar
Si*lact
fr
n Number
' Sub^t
Page
n Number
790
152 006
Tracers (Ordnance)
--Applicatioaa
496
190.068
Tranalormatioaa
(Ma'hematlcs)*:on.)
1 '
757
171 578
Track chamber
435
193 408
--Design
719
149 816
278
152 684
Tracked vehicles
•-Developfnem
109
152 599
707
153 781
303
152 659
543
148 931
--Modoa
751
152 007
735
155 321
19
130 856
152 008
- -Effects al radiation
162
152 804
13
152 033
--Pressure
67
152Cf73
- - Life expectancy
50
150 601
544
153 374
Trackiof
- -Materials -
733
154 479
- -Coairol systema
14
152 138
- -Teal reaulta
731
171 566
7M
153 5SB
93
148 849
--Theory
43
152 657
740
161 239
--Equipment
263
152 703
XtaasWon elements
753
153 914
; -Psychological factors
' 7
152 123
""■--Cryaial structure
212
150 596
567
171 529
399
147 533
--fhaae studies
628
171 113
779
155 ISO
535
153 202
"Properties
344
152 854
581
154 756 •
--Teat rssulis
682
149 444
TraaalaUons
UO
154 749
-Training davlcaa
299
150 317
--Indexes
268
153 575
Ul
152 074
Tradciag laleaiopna
Tranamlaaion lines
--Drvelopment
58
^150 329
--Applications
575
153 598
749
153 917
Tracks (Aerodynamlca)
- -Electromagnetic
780
153 598
--Design
495
fS3 408
properties >^
161
148 706
93
171 082
• --Develofmieni
84
152 802-2
--Equipment
43
150 552
201
151 094
308
153 867
--Imperdance
568
171 498
96
171 064
84
152 802-1
- -Mathematical analysis
345
149 679
459
151 100
Trailers
433
147 243
611
153 9381
-BiNiography
752
153 708
629
153 932
779
153 295
--MaaeuverabiUty
752
153 703
- -Opcrstlon
575
171 557
66
151 095
Traimng
--Posrer
566
171 498
612
153 565
-Bibliogrspiiy
260
171 332
-Radiation
729
154 618
66
151095
--Psyckotoglcal (ictora
137
150 887
--Theory
575
171 557
461
171 394
260
147 305
Trsnaminer -receivers
610
154 749
665.
147 903
--EquipmeM
736
150 846
745
153 707
-Test methods
10'
150 639
Transonic fkw
779
151 104
--Theory
360
147 305
--9oundary layer
194
152 413
153 752
Traialag devloea
s
196
152 245
161 237
-Analysis
260
153 460
- -Mathematical analysis
606
153 644
780
153 7S0
-Design
10
150 639
Tranaonic wind tunnela
153 751
771
149 778
--Performanca
159
153 280
460
171 412
-■Development
135
152 164
Tranaparent panels
95
150 855^
-Effectiveness
260
149 642
--Attachment
159
153 259
201
151 094
-Human engineering
133
171 139
Tranaparent rocket motor
443
153 286
581
154 756
168
153 007
Tranapon coefficients
799
149 911
612
153 565
259
150 317
Traaapcrt equation
600
152 587
436
171 419
Transport number
110
150 544
551
171 522
--Simulation
418
171 404
Transport phenomena
626
171 511
548
153 233
Tranaducers
Tranaport planea
-AppUcationa
89
ISO 540
--Commtailcation ay sterna
561
171 505
797
1S3 721
208
152 394
Tranaportation I
-Btbliograpliy
^
OTSSB-428
-Analysla
67
150 611
9U
193 627
,
293
153 496
150 612
391
153 S05
- -Geographical faaors
588
153 605
144
149 065
- -Oealgn
«-
171 104
'--Scheduling
447
153 078
449
153 305
175
171 157
Trsasverse pinches
98
150 776
282
153 625
--Devekspmeot
557
154 762
Tranaword
300
152 721
; 76
148 063
Effects of radiation
726
155 568-3
Traumatic ahock
■^
152 067
-Impedance
206
147 964
- -Comtenneaaures
403
153 193
78
150 951
149 298
Traveling saleaman problem 763
153 486
IW
148 665
150 833
Traveling wave lubes
152 543
- MaierlaU
736
155S68-1
--Applications
727
154 061
318
152 606
-Mrformaoce
299
153 496
-Design
115
150 447
332
149 649
-Teat methods
293
153 496
^ ,
301
152 937
333
152 747
-Theory
736
155 567
347
152 996
594
153 860
155 568 1
165
132 562
S96
153 678
155 568-2
295
152 994
597
153 680
155S68-3
425
171 414
598
153 267
195 969-1
571
153 938
iOO
153 413
Tranafer function
164
152 253
734
148 398
153 710
Transfer irsining
259
150 317
--Madiematlcal analyals
723
148 323
<ei
153 671
Tranafbnnatloas (Mathematlca) 78
147 588
727
150 902
760
148 212
188
148 685
-Tbsory
107
150 820
187
148 693
153 396
Triaaflaiar wings
294
149 636
330
153 431
--Aerodynamic
575
153 234
323
133 762
characteristics
195
171 162
188
152 545
329
152 436
772
149 214
450
153 685
MB
153 710
--Stresses
160
152 437
451
153 684
--AppUcadoBa
sts
171 334
--Supersonic
998
153 266
- -Brrora
333
152 736
characteristics
39
152 352
153 675
--Theory
186
152 439
Trlaxlal test
161
149 699
153 676
188
152 543
Trlazlnea
600
153 177
490
153 412
-•Btactron tranaltiona
148
148 726
760
147 599
595
153 313
Trtaaolea
764
154 456
760
153 211
--Syabesta '
695
154 369
Tranaiatora
Trldlagonal matrlcea
594
153 144
90
152 681
--Anntyals
630
153 603
Trigger circuits
453
153 734
--AppUcatlOBa/
35
■- 150 753
--Design
296
147 313
431
130 319
81
152 045
731
171 566
747
199 383
300
152 721
Trtgonotnetrlc ftnctionn
282
153 635
433
150 712
--Appllcstlons
282
152 800
70»
153 861
--8Hbbography'~,'
724
169
190 T»2
drSSB-433
Trigonometry
--AppUcationa
736
154 595
-arcuita
164
152 920
Trinitrotoluene
?
709
153 861
289
152 629
-Thermal propertlea
738
171 256
565
171 309
--CaBtalaers
74
91
1
150 809
190 810
Siiblect Page
Triodea
--Development 170
--Teat results 54
Tropical cyclones
--Radar analysis 281
Tropical deterioration %
- -Teat methods 728
Tropical reglona
- -Meteorology 706
Trouble ahoodi^ 135
Truth funalona 321
Tularemia
-AUaka 20
ri
Tundra truck 313
Tungsten
--Brazil^ 198
- -Caaili« 458
- -Chemical reactions 408
- -Electrical propertlea 219
--niyalcal propertlea 614
--Propertlea 719
--Thermal properties 219
--Welding 19*
n NuDiber
149 716
152 753
152 870
161 749
194 487
154 S66
152 165
152 723
150 574
152 619
152 940
161224
151 ON
171 373
171 185
151 084
153 907
171 185
161 224
i
|. ..
Subject
p-r
re Number
Sublact
ff
t% NunBOMT
Tungsten alloya
--Mechanical properties
614
151 084
Turbulence (con.)
Tungsten bronzes
472
153 147
-Matheipatlcal analyals
606
153 737
Tungsten carUdea
--Theory
328
149 689
-Applications
782
155 429
Turbulent boundary layer
-Denalty
784
155 428
-Analysis
193
147 878
Tungaten oxides
196
148 521
--Catalytic propertlea
472
153 147
772
154 816
- -Electrical propertlea
210
148 690
- -Heat trsnatar
474
153 105
Tungaten wire
711
153 658
- -Coatlnga
329
171 193
--Mathematical analyaia
87
150 802
Tunnel dlodea
625
153 873-2
326
149 666
627
153 873-1
771
148 317
Tunneling current
342
132 473
--Preaaure
89
150 540
TurUne bUdes
--Shear atreaaea
456
150 962
-Drag
443
193 939
Turbulent flow
Turfalnea
--Analyaia
89
190 331
- -Coolliv N,
533
CrrSSB-449
--Mathematical analysis
328
149 689
Turbojet englnea
- -Measurement
89
150 540
--De-lcing syatems
416
153 389
--Shear streaaes
86
152 173
Turbojet ediaust nozzles
Twin triodes
35
152 641
--Deterioration
576
154 544
Turbulence
Two-body problem
632
153 679
- -Acoustic effecta ;
787
199 906
Typhoon resolver
82
152 651
^
75
-?
V-2
UkrMoalc radUUon
••Ataorptioa
--AppUcaaooa
Ukraaoolc*
--AppUcaOoaa
- -laaErwnentuion
Uferavtoiac radUtlon
ileal •Oaas
1 aftaas
1 cflacta
306
uo
94
10»
34S
S72
7»2
U
M
313
445
sa6
428
Ul
44a
341
21
21
1S4
PtNMniber
171 361
171361
155 OK
153 247
152 041
150 610
152 46*
1S2 620
1S0M7
152 150
M7MI
171 OM
152 144
149 690
153 775
153 IX
152 032
171057
161225
171 IM
171 499
153 697
152 S32
171 417
149 651
171072
171 072
152 553
Ukravloiai ipactra
"ADaijrala
UaderfTouod Kruciures
- -Blaat effects
Page re Nianlier
Sutnact
Hge re Nianber
276
544
sa
440
785
60
60
-aHeUHnf
Underwater balUatlca
--Mattoaiiiatlcal analyu*
UMderwater cammunicailon
ayaccfiia
•-Development 431
Undarvaier equi proem
--Desl^ 707
UDderwater exploalaaa
--■iaai 441
Uadervacer objecta
— Fouling 39
Uaderwacer ptxxocraphy
"Ailanttc Oceatf 2t2
Underwater lound
--Preaaure 604
Underwater found eqUpmam
--CalUa-atlon 302
Underwater aound generaicra
•-Preaaure 206
Underwater iwlmmlng
--Bibliocraptiy 620
--Equlpnient 620
Underwear
--Thermal Inaulatlott 713
Unlforma 73
Unlrooleollar reactlonr 149
Ualveraal algebra 4S0
Unlveraal turlng machine 82
152 746
153 355
150 957
154 406
154 697
150 830
150 831
153 9S4
153 781
149 520
150 769
152 908
153 502
152 979
147 963
i7l 577
171 577
154 169
171 009
161 408 S-1
153 458
ISO 508
ure
--CryauUlxatka 141
--ajnaliaala 141
Urethaiw polymer a
- -AppUcatlcna
Unne
•-Anaiyala 694
--Chemical analyala 270
--Excretion 269
LMUly fvaictlcna 223
UiriTeralHea
--Sundarda
Upper atmoaphere
--Analyata
--Chemical anaiyala
•-Denalty
- -InatrtanancatlOB
--lonlxailon
— Meteor dogy
--Propertlea
--Spectrographlc anaiyala
--Temperature
Uranium isotopea(Radloactlve)
--Spectra
Urea
--Chemical reaaions
152 247
152 247
443 153 286
154 264
153 327
171 343
152 016
148 723
150 452
148 286
153 567
150 421
153 586
148 257
150 873
150 598
153 442
152 055
148 262
150 417
150 721
152 669
152 644
153 03O
171 574
224
34
156
560
35
559
34
35
42
434
63
30
34
414
283
102
334
644
•> • -
\
K-
«'
1
I "
Subina
V-pamctea
--Theory
Vacuum (umacea
-•Appilcatlcna
Vacuum matting
Vacuum metallurgy
Vacuum ayatama
--AppUcatloaa
- -Teali^ aqid
Valvaa
•-Oaaign
--BqtMpmani
Van Allen radlatlaa
Van der Pol aqiatlon
Vanadlian ootldea
--Cryaul atrucrure
Vapor cycle cooUi^
Vapor praaaura
--Tablaa
VarUble realaiora
--Calibration
--Developmem
VarUbk atari
- -ClaaalflcatloB
Vamlahaa
--Anatyala
-•Prooa4alag
VaUcla whaaU
--Te« reauhs
VehTclei
--Aerodynamic
characterlatica
•-Electrical ayaiema
--Human enginaarlttg
--M19C
--M-35B7
"M-109
- -MaaauTwra^ty
•-Modon
*-9l>tyulatlan
--Propulalon
Vakua theorem
Vanua
-•Meteorology
Varbal batwvlar
"AMlyala
"Paychologlcal factor a
--Taat nlethoda
Vartlcal guai recordars
--Daalpi
Vertical Indlcatora
--Error a
Vartlcal taka-off pUnaa
--DaatSB
-•B<|tripment
"FUgbt taat raauka
"Laailli«
^aga re Nianber
92
330
613
92
no
419
61
740
5
258
597
797
305
422
735
181
171
455
729
177
67
S«
588
717
988
988
45
322
132
104
637
686
136
137
807
706
216
711
709
417
711
152 0S8-1
15:iuS8-2
161 764
161 213
171 521
161 764
153 573
152 319
150 626
155 la
190 801
149 645
153 668
153 721
171 345
161 371
171 245
155 384
299 152 171
171033
153 380
750 171 ^3
171 388
154 643
193 006
152 073
171 929
171 525
154 630
153 562
153 562
171006
153 275
152 464
150 494
153 875
147 530
148 300
1S2 389
152 390
150 903
150 504
152 114
154 527
718 171 609
149 666
154 549
154 580
153 083
153 642
Suyoa,
Vertical take-off planes (con
--Uft
"MUlwy raqulrema«a
"Modal te^( results
--Perfbrmance
--Slmulatlao
— Stab4Uty
V
)
326
418
36
159
564
36
Mb
419
710
563
Vary high fraquancy antennaa
--nealgn 169
Very high frequaacy
communication ayaiems
--Performance
"Teat fadUtlaa
636
432
731
Very high fraquancy racalvera
--Dealpi 725
Vary low fraquancy
communication ayatema 5
Vibration
- -Comer meaaures 602
--Frequency measurement 735
• •Mathematical aiMlyala 83
90
453
--Flqraical efiecta
-•RaductlOB
--Teatlng equipment
--Tliaory
Vibration Isolators
--AppUcaclans
--Bftoctlveness
--Matarlals
--Madwrnadcal anaiyala
--Teat reauhs
Video delay Unea
- -Mater lala
Video licagratlaa
-Bqulpnieat
Video mappliV
Video alcaala
- -Tranamlaaloa
Viewer
Vigilaaoe performance
Vinyl acetate
--Polymerization
Vlayl compounda
--l^nlfaeels
Vinyl polymers
- •ApipUcatlona
--Faagua deterioration
Vtrlal coefriciem
Viscoelascic materlala
759
635
735
172
38
83
336
711
744
735
178
735
310
/| «
596
48
^136
499
696
547
757
728
145
315
77
re Number
153 196
152 873
152 752
152 780
153 740
152 752
149 666
150 742
155 255
149 354
149 355
148 982
161 580
153 609
150 914
190 847
148 258
153 794
154 507
171 070
152 681
153 734
153 501
148 420
171 484
155 084
171 134
171 090
171 071
149 682
171 594
155 253
155 084
150 392
154 507
153 793
150 609
153 aa*
150 9*4
150 594
148 285
152 566
152 157
153 136
171 570
152 877
171 578
171 579
154 487
152 218
150 013
VlaUAUty
--Maaaurement
ftige re WuBiber
38
158
Vlalon
--niyalologlcal factor a 140
Vlaual acuity 8
- -Arctic reglona 266
Vlaual perception
--Anaiyala S3
- -Meaauremeia 682
683
-Maceorologlcal faaora 413
~ ■ " 561
665
716
269
135
392
684
38
-nijraical tactora
-Statistical anaiyala
-Teat methoda
Vlaual range meter
Vlaual algnala
--Detection 289
- -Idemlflcation 363
Vlaual diresbolda
--Acouatic factor a 140
-•Meaauremea 752
Voice commvBilcatlan ayatema
-BlbUograiAy 122
-Coding 55
452
--Dareloiaitei* 134
--BqiMpmes 431
- -iBMlllglhmty 561
- -Paydiaiaglcal (actora 137
Voice dau proceaalng
ayatem
Voltage
--Measurement
Voltage regulators
--ElectraroagDedc effecta
Vokmecera
--Calltaratlon
Vortloaa
--Aaatrala
- -Marhanntlcal aiMlyala
"MoUoi
VoUnggame
Vosrel dlacrlmlnatlon
Vulcanizatea
--Deterloratlao
- -Preaervatlon
--Streaaes
- -Temperature factora
VZ-7Af
452
72?
289
289
391
292
196
86
326
457
772
457
76
478
317
179
316
179
711
152 350
152 384
152 399
153 107
153 326
149 849
171 601
190 916
152 682
171506
171 610
154 647
152 605
171 146
153 470
154 064
152 350
152 926
171 313
153 252
153 900
152 173
148 972
153 455
152 255
ISS9S4
171 SOS
153 989
152 390
153 455
171079
154 643
171 209
171 212
171213
171 214
171 215
171317
171 318
171 316
148 531
152 047
152 479
153 499
149 214
153 848
153 499
152 177
153 430
171049
161969
153 172
161969
153 899
Wair**' iMooueiixni
Waalcui
Wutttoumtt
807 147 «43
715 1S4 631
liMlyita
713
Its
745
-rialflcatlaa
--R«flsctlv« (
--Spaccri
--Stcrafe
--Vapor preaaure
Water activated baaeiiea
* - Development
Water exit
niter I
-KadtoacriTfcy
--Aredc reflaaa
Water tianela
' OitcnBAsfloOB
440
440
743
t«0
630
703
sa
748
436
«0
S43
74S
101
se
23
101
40*
693
693
743
713
333
91
550
154
3S
703
2S4
406
3
-•HHnnodyiieinlc propertlea 748
■r^vavea
Amtfwu
Hyvh-odfaamlc
I
laMlyala
608
60)
-Vaiactiy
-ffajraical effecta
ace
I propertiee
[!<■
Otera
atata
awltdiea
wtadcera
-Pallva
-AmtftU
-Dlalectrlc propertlea
608
90
458
608
609
413
74*
493
774
458
609
to
41
57S
439
173
167
301
S74
73<»
733
2C8
154 638
148 713
134 616
iC effecta 739 154 651
133 519
133 346
134 679
154 677
171 145
134 812
148 747
147 346
153 847
133 231
190130
130 t31
133 610
193 402
134 664
132 630
171091
133 610
161 371-8
171091
161-371-11
161 371-1
161 371-1
134 642
154 670
153 574
161696
171 512
149 061
148 295
134 396
150 618
150 690
152 064
153 847
149 891
190 510
134 745
150 842
153 159
154 767
190 510
147 311
134 676
147 125
190 634
147 125
190 510
190 914
190 681
193 99«
193 693
133 343
133 467
133 652
130 897
134 956
134 957
135 299
192 524
Suti^ect
Waveguide* (coo. )
- -ElecXTcmacBetlc
propertlea
--EqtMpmeat
--EidtailoB
--Matbematlcal analyala
--Theory
--Wave traaamlaalan
Wkaea
- -Etrecta of radtatlOB
Wear tnechaidca
Weather conimiailcatlana
--ReccrcUnc devtcea
Weather forecaaUag
--Errora
--Germany
--HanlKnka
--Mathematical aaalyaii
--Radar analysis
--Stadatlcal analyala
- -Teat reeults
Weather atatlooa
--Location
- -Organliatloa
Weather atatlooa (Automatic)
--Dealjn
--Eqvdpnient
Pat re Number
301
427
393
974
49
106
434
\J72
230
435
176
469
191
191
999
411
190
555
956
ISO
31
413
596
2M
412
707
151
536
-Reflective effecta
--Supersonic
characierla^ca
Welerairaaa producta
WelftatJeaaneaa
--Riyaical effecta
--niyaidoclcal effecta
Welded jotma
--Aoalyals
--Teat reeuJM
Welding
"MHertala
WeUa
--Mechanical propertlea
--Radlofraphlc analyaia
--Streeeea
--Teat reauka
Weat Pord
Wetting agents
--Eflecttveneaa
--niyaical effecta
Whiakers
Wtdatler*
White notae
Wtdte oak boarda
White oak lamlaatea
Wlener-Hopf equation
Wiener -Hopf method
Wind
--Botavlary layer
--CklifornU
- -Oophyalcal taaor*
--MeaaureraeM
454
319
134
682
542
<33
748
445
-New York
-North America
796
309
40
983
439
739
277
703
796
107
156
336
140
183
183
184
78
449
708
704
556
705
31
150
380
708
706
785
706
70S
7t
152 652
152 7»
152 581
150 897
152 693
150 413
153 555
153 775
149 735
153 417
152 794
171 474
150 388
152 448
153 745
153 204
152 563
153 699
153 443
152 206
152 OSO
153 607
153 550
132 700
153 232
154 528
149 711
153 601
350 153 088
150 069
152 972
152 215
171 611
153 402
171601
153 694
153 363
198 161 219
153 904
152 988
152 395
153 991
193 218
153 219
194 988
190 619
148 400
171 598
150 830
149 069
193 279
147 529
171 173
171 174
171 175
152 108
147 121
154 533
155 089
153 443
154 447
150 867
152 196
152 699
194 931
154 527
153 583
154 570
154 163
Suhlect
Page re Nianber
Wind (con )
--North America (con.)
--Nciflc Ocean
705
706
154 376
154 566
--Fhyaical effects
608
149 891
--9iear streaaea
704
155 089
706
154 531
707
154 563
--Simulation
70S
154 533
--Temperature factors
706
134 447
--Turbulence
707
134 562
"Velocity
34
152 189
35
150 421
704
155 089
Wind tunnel models
--Aerodynamic
charactarlatlca
193
153 379
--Teat reeults
564
154 504
Wind tunMl noszles
--Callbratlaa
3V
149 344
Wind lunoels
--AppUcaticna
477
153 633
--Deaign
114
152 678
770
154 572
— Equipment
85
171 104
-
197
152 550
434
ISO 067
--HeaUag
608
152 582
Wlndahtelda (Airborne)
--Human engineering
37
171 094
Wing slots
- -Modal test results
710
135 146
Wlnga
--Aerodynamic
charaaeriatlca
158
147 374
"Flutter
606
152 687
--Hypersonic
char act erlatica
36
150 965
--Uf»
159
152 786
336
153 196
418
152 873
--Model test results
158
147 374
— Preeeure dtatribudon
36
ISO 985
--Supersonic
characteristica
770
171 593
Wlnterlzation kits
- -Arctic regions
715
154 669
Wire
--DbMbbUo^
788
155 573
--Mechanical propertlea
66
152 197
--Tenaile propertlea
444
161 230
Wiring diagrama
"AMiyala
636
153 876
"Theory
570
152 915
Wood
--AppUcatiOBa
719
154 663
716
154 665
194 667
--Pungua deterioratloa
541
153 122
—junta
717
154 654
--Preaervatlon
68
130 954
182
148 727
716
154 668
738
154 650
171 330
"Teat reeuka
182
171 165
• • ■ t
171 166
■ 1 ■ ;
183
171 169
171 170
■'- .'
171 171
1
171 172
171 173
171 174
184
171 175
171 176
Woolen textllea
--Test results
73
130 348
Woiaala i
-
--Analyals '
19
152 003
n
152 368
--Physiological efteaa
141
152 852
Wronaklan
490
153 711
Wullcmreber antenna
425
150 698
x-x
X-15
X -radiation •
--Aneouatian
--OsMalon
"DoMffe determination
Page re Number
715
716
716
36
6X
619
692
154 663
154 665
154 667
148 274
171 527
153 858
155^4
Sublect
X- radiation (con.)
--Intenaity
-Pbyalologlcal effects
- -Production
--Scattering
--Sources
552
21
692
619
639
2
Sufat«:t
fie
172
183
62
94
94
Yagl-Adcock ayatem
Yellow pine boarda
YP-110
Yttrium
--Mechanical propertlea
--Phaae studies
149 058
171 170
152 797
171 006
171 085
Subtect
•
1
reNiaabe
Zinc
--niysical ettecta
ZlBC coatlnga
--Metallurgy
344
591
152 97 J
161 932
re Number
150 895
152 640
155 375
153 858
154 807
150 517
192 865
Subject
X-ray diffraction analyala
--AppUcatlona
- -Inatr umaotation
X-ray apectroacopy
P»ge re Number
114
210
269
330
553
150 749
152 469
152 740
171 348
ISO 899
J
-Teal reaulta
149
171 159
149 056
Subject
Zinc cryaula
--Fatigue
Zinc oxides
--X-rsy analysis
Zinc sulfide crysula
--Electrical prcpertiea
I ■( • ■
Page renumber
610 153298
469 153 552
349 171 338
Subject
Zirconium
- -PurlflcaUco
Zirconium oxides
--Thermal properties
ZodUcal Ught
--Spectra
I^je re Number
301 192 074
990 171 941
132 192 381
?~N'
i
r
^ i
t
n
Source
AuiMB U. . DeaiBart
Acoiadcs Reaearch Lab. ,
Harvard U., CambrUtga
Maaa.
Admiral Corp., Ortcafg 111.
...ca. .^r-«"^"-
593
7t7
2^2
9*3
Santa Ana
"SJSf'
Advanc«l Men la RMMrcti
Corp. , Socnemlle, Maaa.
Advanced Semiconductor L«b. ,
General Electric Co.,
Syracuac, N. Y.
Aerial Recoiuwlaaanca Lab. ,
Wright Air Development CMv.
Wngta-Patteraoo AFB, Ohio
Aero Ceo Aatro Corp. , •
Alexandria, Va.
Aero Service Corp. ,
nuladelphu. H.
Aero-Space Laba , Morth
American Aviation. Inc. ,
Downey. Calif.
AeroChem Reaearch Lata. ,
Inc. , Princeton, N. J.
Aeroelaatlc and Slructurea Re-
aearch Lab., Maaa, Inat. of
Tech.. Cambrt4|a
Aero^t General Corp.
Azuaa, Calif.
m
564
625
565
161
2M
420
557
310
Aeronautical Acceaaortea Lab.,
Wright Air Development Dtv, ,
Wnghi htteraon AFB, Ohio
Aeronautical Chart and Informa
tion Center, St. Louia, Mo.
Aeronautical Electronic and
Electrical Lab:, Naval Air
Development Center,
Johnaville. Pu.
Aeronautical Ei^ne L«b. ,
Naval Air Material Center,
nilladelphla. Pa.
Aarooautical Inatrunwnu Ltb.,
Naval Air Development Center,
Johnaville. Pa.
Aerooauiical Materlala Lab. .
Naval Air Material Center,
Riiladelphia, Pa.
29
16i
35
735
709
Aeronautical Reaearch Aaaocl-
atea a< Princeton, Inc., N.J.
Aeronautical Reaearch Lab.,
Air Force Reaearch Div.,
Wrigbl-Paiteraon AFB, Ohio
457
(
n Number
1^305
153 6i4«
ISO 19*
mm
153 416
153 712
153 663
153 873-2
154 2*6
149 (B9
152 728
153 712
153 886
257
152 846
580
153 M 3
604
153 743
736
153 870
148
r
285
147 554
454
171 415
708
155 OM
63
152 065
146
148 289
177
152 546
442
153 441
548
155 002
560
154 758
580
154 968
747
154 4^
172
171 134
305
171 345
171 067
153 260
152 641
171 237
154 5S5
94
150 877
329
149 655
330
152 463
778
150 780
SOURCE INDEX
Source
Aeronautical Reaearcb Lab. ,
Air Force Reaearch Dtv. ,
Wright -Patteraoo AFB, Ohio
Page n Number
(con.)
586
633
769
153 459
184
171 161
205
171 143
435
152 320
152 321
449
153 385
533
150 322
542
171 048
561
153 583
580
171 108
Aeronautical Turbine Lab.,
Naval Air Turbine Teat
Station, Trenton, N. J. 416
Aeronatronlc, Newport
Beach, Calif. 435
Aeroapace Medical Div. ,
Wrii^t Air Development Div.,
Wright-Patteraoo AFB, Ohio 5
36
102
260
265
397
Air Crew Equipment Lab. ,
NaVal Air Material Center.
Philadelphia, Pa.
Air Force Balliaac Mlaalle
Div., Air Reaearch and
Development Command,
Inglewood. Calif.
Air Force Cambridfc Re
aearch Laba. , Bedford,
Maaa.
406
536
580
736
57
68
119
154
161
162
172
184
U9
205
9M
-. 411
4tt
4C7
548
593
704
Air Force Command and Con-
trol Development Div. ,
Bedford, Maaa, 6B2
684
Air Force Flight Teat Center,
Edwarda AFB, Calif.
Air Force Inat. ol Tech. ,
W right -Patteraon AFB, Ohio
Air Force Mlaalle Develop-
ment Center. Hollbmao AFB,
N. Mex.
36
70
961
755
310
718
Air Force Special Weapona
Center. Kirtland AFB,
N. Mex.
2H
306
993
4SS
4«2
«74
797
202
Si
150 320
171 485
155 144
153 289
153 744
152 300
171 053
171 087
171 119
171 332
171 333
171 392
153 354
153 489
154 811
171 247
171 248
171 249
171 250
152 200
150 412
152 616
149 061
148 705
148 709
148 706
149 058
148 707
152 202
152 283
152 684
152 701
153 884
152 964
152 985
152 987
153 394
153 395
153 392
153 393
154 748
153 806
155 089
154 303
154 063
154 064
152 296
152 297
153 591
154 716
153 587
171 609
150 372
152 802-1
152 802 2
150 371
152 428
152 744
152 743
152 686
153 408
150 719
153 465-
153 731
152 639
Source
Pap
n Number
Air Force Special Weapooa
Center, Kirtland AFB,
N. Mes. (coo.)
334
152 698
620
171 527
783
155 254
Air Proving Ground Center,
Eglin AFB, FU.
57
152 361
162
153 067
709
153 861
Air Reduction Co. , Inc.,
Murray Hill, N. J
583
153 5S1
Air Weadier Service. Scoa
AFB, III.
149
152 042
279
152 977
Air Weadier Service.
Waahington, D. C.
555
153 659
Airborne loatrumenta Lab. ,
Daer Part, N. Y.
162
148 711
416
171 370 T
5«5
171 so> :
Airborne Inatrumenu Lab. ,
I
Melville, N. Y.
41
171 095
SS«
153 888
718
150 901
Airborne Inairumenia Lab. ,
MIomU, N. Y.
41
150 681
966
171 504
171 SOB
709
154 743
f
7U
155 258
Aireaearch Mfg. Co.,
Phoenix, Arlx.
580
153 616-1
153 616-2
Alabanu Polytechnic Inat. .
Auburn
581
153 825
153 826
AlaakaU.. College
411
153 371
441
153 540
478
153 520
153 521
AU American Engineering Co.
Wllinli«ion, Del.
709
161 914
161 915
Allied Reaearch Aaaoclatea,
Inc., Boaton, Maaa.
57
152 122
84
150 634
436
153 161
737
148 216
American Brake Shoe Co. ,
Mafawah, N. J.
91
171 065
Rsiladelphia, Pa.
420
153 227
719
153 594
American Inat. fcr Reaeardi,
Pittaburgb, Pa.
6
171 075
41
150 160
133
171 139
162
148 284-
260
149 642
153 460
392
153 165
420
150 703
537
153 288
538
153 497
662
154 522
American Inat. for Reaearch.
Waahington. D. C
6
152:136
American Machine and Foundry
Co., Nilea, 111.
160
171 145
Anterican ftiwer Jet Co. ,
Ridgefield. N. J.
992
153 547
Amharat Coll. . Maaa.
538
153 150
696
154172
154 ITS
154 874
Amperex Electronic Co. ,
Hickaville, N. Y.
162
152 228
Amphenol Electronica Corp. ,
Chicago, III.
719
150 849
Anderaon-NichoU and Co. ,
Boaton, Maaa.
805
155 090
Antenna Lab., Calif. Inat. of
Tech., Paaadena
421
153 224
Antenna Lab. , Ohio State U.
Reaearch Foundation,
Colunbua
41
150 740
219
152 242
H^» WWiaabeT
AMtock CoU. . Yelkw Sprlnci.
..^ aadcm «nd
Swa«rtr« Lata., Stanford
U.. Calif.
219
219
as
146
263
7
75
7«
IM
Its
192
317
449
538
sr7
994
63t
74*
7M
739
AffUad Madiaiuca Lab. , Maaa.
laac. oChdi. , Cambrulie
A|ptt*<> Aqratca Lab. . Jofana
I U. . SU««r Sprlnta.
Afpilad PayclK>lo(ical Serrtcea,
Wayaa. Pa.
Arctic Arnmadlril Lab.
APS. Alaaka
152 2SS
153 255
152 669
149 701
171 313
1S2 178
132 175
152 063
153 176
1S2 177
141978
152 160
152 162
152 161
152 163
152 883
147 121
148 169
153 690
148 092
148 419
153 139
153 144
153 688
153 689
153 860
15S691
148 756
149 521
149 522
148 095
147 844
148 420
148 782
149 534
149 558
149 750
147 842
147 843
149 523
171 099
KB
130 872
146
150 781
699
154 538
6
152 142
393
153 779
683
148 774
752
153 900
12
152 028
152 029
152 030
13
150 218
152 031
152(03
16
147 745
isosn
150 578
U
147 476
150 214
190 229
190 566
190 576
153 032
63
190 571
l»
152 849
152 850
152 853
140
152 851
141
152 852
263
153 32S
265
153 336
266
153 326
153 328
153 341
153 3*2
153 SSI
153 SSS
287
152 695
b
153 S3«
153 3S2
273
153 331
310
153 339
313
153 320
sas
1SSS46
Source Pfe
Arctic Aerooiadical Lab. .
LaddAFB. Alaaka (cob.) 393
394
397
39*
402
403
411
412
420
440
441
464
627
548
627
549
465
478
944
545
«M
789
786
Arctic fawt. of Nonb
America. Waahliwuai. D.C. ISO
707
ArfOOM Natloaal Lab. . HI.
AxlaaaaStawU.. Tempe
ArtaoaaU.. Tucaca
Arfeaaaaa U. . Payettenlle
Amad Porcea NRC CoaunltiBe
on Haarli^ aad Bto-Acouatica,
WaaUngtoo. D. C. 398
Armed Porcea -NRC Vlaloo
Ccmmiraee. WaahlagHo. D. C.53S
Armed Servlcea Tectaical
btformatlaa Afleocy,
ArtliMlaa. Va. 1
533
681
807
Armour Reaearch Povndatioo.
Chlcaao, UL *i
92
146
336
337
341
• 348
460
469
561
566
611
612
691
719
781
783
Amy BalUatlc Mlaalle A«eiicT.
RedetcM Araenal. Ala. 737
n Number
153 329
153 321
153 322
153 369
153 S7S
153 545
133 372
153 544 .
153 522
153 507
159 513
153 515
153 518
15SS43
153 514
153 S24
153 517
153 519
153 546
1S3S12
1SSS23
153 508
153 509
153 516
ISSSIO
159 3617
1SS374
153 370
194 168
154 169
154 167
152 290
154 551
153 839
153 233
153 839
153 827
Army Cbamlcal Corpa.
Port Detrlck, Md.
Army Otemtcal Corp* Eafl-
■aarlag Coanaad. Army
rina^i il Md.
Army ChaBlcal Reaearch aad
DBvctopmaac Laba.. Army
Ctemlcal Caawr, Md.
759
471
to
13
19
»
39
97
99
271
272
Source
Army Chemical Reaearch and
Develoiimefit Laba., Army
Chemical Center, Md. (coo. ) 306
153 778
153 755
171 106
171 SIS
171 689
171 519
152 140
171 057
171 086
152 244
152 730
152 962
152 731
171 329-1
153 167
171 474
171 554
147 498
171 524
199 S6S
171608
153 TH
171 596
150 908
153 947
155 251
155 252
155 OtS
152 927
ISO 992
152 001
152 002
152 003
ISO 669
ISO 101
ISO 663
ISO 664
150 IW
152 000
171 1 24
152 599
149 634
149 635
Army Enfineer Reaearch and
Developinent Lata., Port
BelTotr, Va.
Army Engineer Waurwaya Ex-
perlmeni Satioa. Vlckaburg.
Mlaa.
Army Orckiaace Corpa.
Waahli^ton. D. C.
Array Ordnance Human Engl-
neerl(« Lata. , Aterdeen
ProTlag Ground, Md.
Army Reaeaith OCTice,
WaaUogno. D. C.
Army Rodcei and Guided
Mlaalle Agency. Redatone
It; Ala.
n*
FBNumter
306
152 595
152 596
152 597
339
149 641
396
153 174
691
153 841
153 843
153 84S
■--
154 438
752
171 612
101
152 650
447
153 078
460
153 077
40
150 436
171098
67
152 073
70
152 354
981
154 756
154 757
171 480
171481
171 482
171483
58
150 733
392
153 470
398
153 469
198
171 000
144
171001
157
171004
206
171003
222
171006
699
171 155
699
153 619
800
1S4 208
Army Signal Mlaaile Sun»n
Agency. White Sanda Mlaalle
Rai^. N. Mex.
Army Signal Reaearch and
DeveloiKnent Lab. . Fort
N.J.
436
2
29
30
34
41
42
58
69
101
104
109
ISO
191
162
163
172
223
288
317
352
411
421
4S1
475
S«6
567
706
153 182
ISO 451
152 193
152 195
ISO 452
152 189
152 191
152 188
152 192
153 194
150 664
193 806
1S0M7
153 190
190 666
193 196
152 568
192 804
153 990
ISO 074
152 991
152 566
152 567
153 003
152 674
153 67S
153 564
153 565
153 997
150 705
150 704
153 998
153 000
153 001
ISSOM
190 706
199 003
171 377
193 230
193 247
193 248
193 349
194 991
194 932
r:
-t
Sourca
Army Signal Reaearch and
Drrcloproeni Lab..
Fort Monmoudi, N.J. (con.)
Army Saow, lea. and Pernv -
front Reaearch BatabUahmeot,
Wllmetm, 111.
r»m FVNMntar
705
752
789
792
192
Amy Tranaportatlon Reaearch
and Baglneerlag Conanand,
Port Euacla, Va.
281
565
Arnold Baglneerlag Deralop-
maoc Center, Tullahoma,
Tana.
i
36
419
S61
608
709
790
36
85
199
179
193
154 533
154 529
193 716
1^930
192 317
192 918
152 496
152 4S7
171 190
153 556
192 792
190 073
171 914
193 416
134 380
171 614
171 613
190 985
192 647
171 urn
193 2M)
133 9M
147 871
Source
Arnold Engineering Oevelop-
meni Center, Tullahom*,
Tana. <con.)
Paaa PgNumtar
Atlantic Reaeardi Corp. ,
AleundrU, Va.
Audloiegy Lab. , Nortfaweatem
U. , Evanaion, 111.
Automatic Mfg. CMv. , General
Instrument Corp. ,
Newark, N. J.
AvcoCorp.. Naabvllle, Tana.
Atoo Corp. , Wilmington,
193
306
325
338
348
454
737
769
275
139
719
157
285
217
445
620
621
192 260
152 555
192 758
153 379
153 068
152 556
1S2 843
152 664
152 966
153 477
153 648
153 846
153 553
153 093
152 766
155 159
152 343
152 967
193 472
171 413
153 490
153 916
Souree
Avco-B«erea Reaean
Maaa.
<fiLab.
nNunter
Avlatloa Medical Acceleration
Lab. , Naval Air Development
Center, JohnaviUe, Pa.
63
150 964
64
190 777
114
192 678
117
1S0 95S
194
148 730
192 426
210
149 669
214
149 067
346
192 912
494
149 676
598
153 569
605
153 568
13
ISO 442
14
ISO 499
158 440
16
150 441
36
148 274
210
152 469
269
152 470
689
154 468
710
153 695
748
153 694
ATladoo Paychoiogy Lab. , U.
of UllnoU. UrtaM
263
163 703
*a
U
tmi nytmotmr
BitUMc fUMarek Late.
Aberdeea I^ro*t■( Grtiuod,
34
42
S6
99
121
173
306
X7
32S
422
436
440
442
4S4
466
626
BBTtol Kwrdi PouadtUoo.
PraakUa laat. . SvarnBora.
pa. 209
615
719
BanaUa-laadnaB.V..
Pi^dWt-a*-Mala
(WaacOanaar) 340
I Miwnrtal laat. ,
39
108
133
isi
161
203
210
233
339
399
391
MO
«n
606
794
779
793
gauack aad Looik Optical Co. ,
KutlwaMr, N.Y.
iaylor U. CoU. at Madldna.
Heyacoa. Tax.
MMTloral SctMCM Lab.,
Wrt#K Air DiiBlopBHar Dl».
Wrl^K-Panaraoa AFB. OWo
Co..
lo. N. Y.
iaU Aircraft Corp.
Mlble. N. Y.
■an and HomU Baaaarcfc
niiilm. CaUf.
■aU HaUceptar Corp. , Port
Wgnk. Tta.
■aU Talaptaw Laba. . lac. .
Murray HIU. N. ].
■aUl^laphna Lataa.. lac..
Nav Ycffc
•U
R J.
21
76
139
149
173
310
a«9
3U
4M
«93
64
609
179
283
44S
7«9
T.
406
416
996
43
109
1*3
ISO 417
190 993
190 329
190 494
190 957
ISO 999
149 647
150 418
192 435
149 633
152 7J2
152 729
152 602
150 066
153 494
ISO 069
190 070
190 724
153 425
154 406
153 493
ISO 067
190 069
153 073
153 649
149 700
150 696
153 907
149 657
171 030
130 424
193 019
193 494
171149
132 933
152 760
171 344
171 19«
171 342
194 409
199 929
171406
193 799
194 749
199 929
193 199
171911
171 617
198190
199 923
193 920
152 640
171 079
171 146
199 089
171 137
171 332
171 313
171 312
171 419
171 401
171 611
171 600
193 089
193 «r
171 149
171 192
171 390
194 219-1
194 219-2
171 409
194 406
153 931
193 657
ISO 690
149 719
3ourca
Ball Talaptnaa Uba.. Inc.
WMpyaay. N. ). (coa. )
Beadlz Ariatloa Corp. ,
Detroit, Mlcto.
Beodlx Radio CM*. . BaodU
Aviatiao Corp. . Baltimore,
Md.
Benaoe- Leiner Corp. ,
SanuMoolca. CalU.
Btooiedlcal Lab. . Wn^i Air
Derelopmam Dlv. . Wngbl-
Panaraoe APB. OhlD
Biopbyalcs Lab.. StaaJord U.
Calif.
Btotadnolocy Lab. . U. of
Califomla. Loa Aafltlaa
airmli^bamU. <Ct. Bnt.)
BUlty Elactrlc Co. . Erie, Pa.
Block Aaaodaaa, Inc. .
rat WNaoJtar
163
149 720
239
149 722
152 699
341
149 721
149 723
342
149 724
601
154 906
Blue HIU Maiaoroloflcal
Obaerratory. Mllfon. Maaa.
Boeli« Alrplaae Co. .
Saactle. Waah.
Boelaf SdaodOc taaaerrti
Laba.. 5aaala. Waafa.
Bolt, ieraaak aad Nevmaa.
taK.. CaaBbrldgi.
■oaa U. (Waat Oemiaay)
■ordM caamlcal Co. .
FWladalpbla, Pa.
Boaioa Coll. , Chaatnut Hill,
I BoMoaU.,
I Baatoa U. School of MwUclna.
Brl^t Star Induatnaa,
CUftoa. N. ].
Britlah ColianMa U. (Caaada)
157
223
764
19
139
143
273
31 1
39B
949
M2
289
610
690
307
340
341
194
422
786
J7
119
194
199
197,
936
339
422
M2
276
406
753
567
622
7
690
43
207
274
467
Brttlah CoctOB laduatrr Kaaaerdi
AaaocUtlaa 944
Brooke Army Medical Caaier,
Port Sam Houaioa. Ita. 142
271
403
404
343
949
■ Nado
Upcoa. N. Y.
il Lab. ,
Brooklyn ColL , N. Y.
U., Provldaoce,
24
693
19
L 25
^ 177
223
990
7S1
793
Source
9ran U. DIt. of Applied
MadMmatlcs. Piortdence.
R. L
n Number
149 709
148 977
150 909
171 073
171 140
171 160
171 309
171 309
171 367
152 961
149 444
152 926
153 298
153 714
152 673
152 714-1
152 714-2
152 714-3
152 714-4
152 713
149 719
171 416
149 974
171 076
150 879
152 255
132 519
171 138
171 902
152 906
153 175
153 739
153 794
152 770
ISO 690
171 565
153 822
153 820
152 103
171 602
ISO 804
152 209
149 683
153 997
171 574
152 366
152 367
132 369
199 192
199 193
199194
193 406
199 406
199191
193 640
199 641
150 539
153 872
190 961
190 999
149 074
192 016
194 109
192 005
153 949
9rovnU. Dlv. of Baflaeerlaf.
Provldefice, R. I.
Bruata 9erylllum Co.
CleveUnd, Oblo
Brueaela U. (Belglian)
Bryn Mavr Coll. . P«.
Bitftalo U. Sdwol al Medicine,
N. Y.
Bureau of Mlnea,
Bartleavllle, OkU.
Bureau of Mlnaa, nttaburgb. Pa
Bureau of Naval taraoanel.
Waehtngtaa. D. C.
Bureau of Naval Waapona,
Waahlogtoa, D. C.
88
150 528
192
148 725
327
152 857
328
152 8S8
452
147 401
458
153 162
465
154 291
473
153 074
475
147 400
968
153 599
594
153 600
«02
147 402
148 811
148 812
153 142
605
153 737
760
149 165
769
148 813
154 130
154 121
773
154 862
801
148 349
63
150 869
90
152 170
117
150 474
119
152 059
161
149 699
194
152 413
201
152 169
219
148 296
346
152 742
453
147 362
603
148 346
605
153 644
768
150 739
801
148 970
66
152 197
69
171081
460
171 389
«4*7
153 299
994
153 424
19
150 788
549
171 529
694
153 036
.549
153 M7
738
152 022
97
152 233
536
153 561
153 604
693
153 746
299
171 209
171 212
171 213
171 219
290
171206
171 210
171 220
171 221
171222
171223
»1
171 206
171 207
171 211
171 214
171 215
171 217
171 218
292
171 200
171201
171 204
171 309
171 216
S29
171209
996
171 202
409
171 296
423
171239
171 241
171243
171 249
423
171 224
171239
171236
171 2r
171239
171231
171 340
Source
9ureeu ol Naval Waapooe,
Waahloftoa, D. C. <caa. )
\>
PiiBB ^B Nupib<f
Source
i
■ureau of Shipa,
Wuhli^oo, D. C.
■■^i-
9ureau of Shlpa,
424
171 229
171290
171293
171239
171 294
171 239
171 343
171 244
Waablogtoo, D.C
1
171 240
\
469
171239
740
199 299
90
192 279
i
90
192 691
299
171 209
171 213
171 U3
171219
1
290
171 208
171 210
171 220
171221
171 222
171 223
ft* njNunter
(coo.)
'» f
I I
f
291
171 206
291
171207
171 211
171 214
171 215
171 217
171 218
292
,.- 171 200
171 201
171 204
171 208
171 216
329
171 203
336
171 202
405
171 236
422
171 239
171 241
171 243
171 245
423
171 224
171 225
171 226
171 227
171 228
Souros
*^y ^B Nunibci
Bure«u of SJilpe,
Waahlngion. D.C. (coo.)
423
171231
17) 240
424
171 229
171 230
171 232
171233
171234
171235
171 342
171246
469 •
469 '
171 237
171 239
744
199 413
171 291
Bureau of Yarda and Docka,
WariUngton, D. C.
101
171091
785
153 909
Burke Reaearch Co. .
Pompano Beach, Pla.
757
171979
Burke Reaearcb Ca ,
Warren, Mich.
757
171979
Buma and Roe. Inc. ,
New York.
560
153 931
85
M
I U. (Fraaoa)
Calllonua Inat. of Taeh. ,
CaUfonla San tolinacialc
CaU.. Sao LiMa OMapo
I U. . Bertelty
U., LaaAa«Blea
CaUforaUU.. Um Aagalaa,
Sctaoi a< MwUdaa
CbM* Colt . Craad Mpida.
lU. (0(. inc.)
u
sat
S43
474
77
106
IBS
217
2S2
318
319
331
336
3*9
42S
349
sso
616
790
801
7
8
103
109
135
139
134
163
189
271
993
411
42S
466
5S5
398
368
«01
630
636
638
705
7U
719
730
7M
784
807
11
270
271
407
142
203
314
U. CoU. (AuKralla) 761
U. (Nbw Zoalaad)
Co..
Palia. N. Y.
Caiaagia laat. of T^di.
34S
69
179
t05
18S
191
SU
SSf
9M
604
613
614
6S3
691
7U
7t7
ISO 883
1S0 8S4
147 S3S
134 099
1S3 46S
1S2 106
ISO 880
148 670
1S2 464
1S2 892
152 893
149 646
133 806
193 <07
133 715 1
153 715-2
133 375
152 916
152 869
153 409
171 414
133 061
153 448
133 764
133 082
153 655
154 4S8
190 498
133 104
133 299
133 144
190 900
133 113
192 353
193 953
147 651
149 136
153 213
153 330
133 686
153 204 '
153 438
153 099
153 745
153 S66
149 090
154 422
149 089
153 729
154 423
134 447
154 245
149 816
149 137
^ 149 138
171 572
152 114
150 216
153 349
153 350
152 871
152 540
152 421
152 422
153 424
152 423
154 088
154 123
147 558
171 061
171 178
1S0S26
149 661
153 490
152 105
171 334
152 882
153 776
171 496
153 749
154 867
153 742
153 768
147 748
154 863
154 864
154 tM
Fit KWBBibar
Carnefie Inat. of Tedi.
Graduate School of InduairUI
Admlnlatratloa, Pluaburfii.
Pa. 78
444
490
«t3
748
749
Camr OtmerymtoTf
(New Zealand) 2
Caae laai
OUo
ofTkdi.. dareland.
Canlyala Reaaardi Laba.
AtfradU., N. Y.
CaihoUc U. of America,
D. C.
43
106
163
43S
636
638
24
326
790
CIS BtactroiUca Div. .
CohaaMa Broadcaatlng Syatem,
Inc., Danver*. Maaa. 730
Oanr lor Documeoucion and
ConununicatioB Reaearch.
Weatem Reaerve U.,
deveUnd, Obio 123
Center for Incernatiooa I Studlea.
Maaa. Inat. of Tech. ,
Cambridge 394
Center for Radiophyaica and
Space Reaearch, Cornell U
M»ca. N. Y.
Central Inat. lor Induitrtal
Roearch (Norway)
Central Technical Inac. T.N.O.,
The Hague (Netherlanda)
Centre de niyaique Ekecironique
et Corpuaculaire (France)
Cencro dl Studio per la Plalca
delta Microande (Italy)
Ceotro Radioelenrlco Sqer\ -
mencale "G. Marconi",
Rome, luly
Qwtanera U. of Tedk i
(Sweden)
Cheeapeake Bav Inat , }ohna
Htvklna U , AnnapoUa, Md
Cheaanfake Bav tnat . johna
Hopklna U. , lalclmore. Md.
Cheeapeake Inatrumeet Corp.
Shadyalde. Md
Chlcafo Midway Lab*. , U.
o( CHcago. 111.
ChicafoU., 111.
Chryaler Corp., Oetrotc, Mich.
Clark U. . Woroeecer.
Cleveland nteumatic Tbol Co.
Ohio
Ckevlta Reaearch Caoter, '
CtereUnd. Ohio
CHflon Corp. . Waahiofion. D. C
Climax Molybdenum Co. o<
Michigan, Detrou
Coaaul Siudlea Inat. , Loulalana
Scue U. , Bicoa Rovfe
86
2
349
799
143
276
43
566
569
108
131
206
119
789
276
SSO
693
608
f92
178
30t
39
157
S90
147
279
412
534
999
998
794
157
285
707
778
342
569
536
775
554
704
150 482
ISO 713
190 714
14B313
141787
149 088
1S4 869
150 941
130 942
190 648
152 on
152 262
153 417
153 876
171 503
ISO SIS
149 686
153 828
153 829
ISO 912
171 123
153 287
149 007
152 523
154 272
171 181
149 67S
153 092
1S3 809
148 656
150 41S
152 212
152 201
150 690
ISO 414
153 090
153 091
171 512
150 t54
149 891
150 664
ISO 392
150 833
17t 064
171 147
171 526
152 679
171 156
152 905
153 232
153 452
153 664
153 669
148 781
153 060
153 624
ISO 489
154 870
149 692
154 541
148 555
171 597
153 735
149 216
Source
Coating and Chemical Lab. ,
Aberdeen Provlaf Ground.
I U. (Weal Germany)
Cotorado School of Mlnea,
Golden
Colorado U.. Boulder
CplumMaU., New York
?tm WKtanber
ColumbU U. School of Engineer
Ing. New York
24
150 089
181
171 033
407
171 128
738
171 330
143
152 476
738
171 236
11
150 527
76
152 071
407
171 376
623
ISO 701
791
153 207
76
148 063
. 1
150 522
77
ISO 521
152 100
152 106
107
ISO 429
ISO 430
150 431
^08
150 432
449
153 7S4
453
153 734
S«S
147 546
595
147 547
619
153 149
760
154 098
806
148 401
103
152 124
164
152 253
220
152 474
292
152 254
319
152 896
351
152 897
569
153 736
S95
153 665
Combuatlon and Bxploalvea
Reaearch, tec., Plttaburgti.
Pa.
Compagnle de Recherchea et
d'Etudea Aeronautlquea
(France)
Compagnie G^ntrale de
Telegraphle San FII(France)
Compuutioo Lab. , Harvard U.,
Cambridge. Maaa.
Computer Engineering Aaaoci-
aiea. Inc. , Paaadena, CaUf.
Connecticut U. , Storra
Cooaolidaced E lectrodynamlca
Corp.. Paaadena, Calif.
Cootrola for Radlacion. Inc. ,
Cambftdgi, Maaa.
314
Convair. Fort Worth, Tb«.
Convair, Pomona, Calif.
Convair, San Diago. CaUf.
Cook Reaearch Laba. ,
Morton Grove, 111.
Copenhagen U. (Denmark)
Cornell Aeronautical Lab.,
Inc., BuMilo. N. Y.
Cornell DuMller Electric Corp.,
IndlanapoUa, Ind.
Cornell U., Ithaca, N. Y.
88
720
794
80
454
23
185
31 S
617
100
101
784
118
770
779
636
720
997
80
81
85
217
326
605
710
760
770
'293
38
110
210
276
279
463
540
569
694
149 665
ISO 368
153 719
150 545
148 2S9
171 407
ISO 407
152 444
171 303
154 428
154 429
154 430
152 3S8
152 359
152 806
15S322
150 738
150 866
153 295
154 966
155 147
153 4M
171 093
171 092
1S0S31
148 682
152 947
153 125
153 463
154 744
147 539
149 338
149 703
148 870
152 036
148 690
149 681
153 343
153 131
133 080
153 830
149 893
SoMTce
Cornell U. Gradiate School of
Aeronautical Engineering.
Idiaca. N. Y.
Cornell U. Medical Coll.
New York
Oornell U. School of Electrical
Snglnaering, Idiaca, N.Y.
ffiippB ^B wmiiBti'
85
ISO 620
ISO 621
455
153 p92
266
133 328
412
153 324
546
154 803
43
ISO 817
392
1S2 872
414
ISO 071
569
154 430
Source
Courtney and Co. , y .,»
Philadelphia, Pa. •'"^
Croaby Laba., Inc.,
Syoaaet. N. Y.
Crown Zellerbach Corp.,
San Leandro, CaUf.
Crucible Steel Co. of America,
MidUnd, Pa.
Crufi Lab., Harvard U.,
Cambridge, Maaa.
Cryogenic Engineering Lab..
National Bureau of Sundarda,
Boulder. Colo.
Pi|e
F« Number
Source
Cryogenic Lab. , Ohio State U.
^V
pa Number
417
ISO 920
Reeearch Foundation,
561
171 510
Columbua
Cryatallography Lab. , U. of
407
154 056
164
152 226
Plttaburgh. Pa.
Curtiaa- Wright Corp.,
S46
153 490
176
1S2 794
Caldwell. N. J.
90
171 060
610
171 546
Curtiae- Wright Corp..
95
171084
Quabaana. Pa.
720
149 847
43
ISO 552
Cuniaa-Wrlght Corp., Santt
Btrbara, CaUf.
286
293
171 195
171 194
58
801
161 093-5
171 618
626
770
154 096
171 604
802
171 619
171 UO
:l
<•
Sbiirc*
nNonbn-
Qetnae Matala Infomuttoi
CarloOialiaKl
412
153 093
Cancer, tectelke Memorial
OmMi NBOonal CoaamlOM of
bat.. Columbua. Obio{a».
) 776
151 108
UKSI
336
153 279
161 236
DuTBOMh CoU, Huovar. N. H.
411
153 460
77S
151 106
413
153 461
779
151 104
557
153 462
151 106
Dwtd STBQg tonif c» Omatr
161 237
Prtncflcoo, N.J.
43
ISO SIS
Dearer Veterana Admlolatra-
44
1S0S13
1S0S14
tlon Hoapttal. Colo.
Department of the Smrf,
30
150 207
1S0S16
WaatalBgton, D. C.
752
159 381
ISO 963
> PauJ U. . Chlcafo, HI.
Detroit Teatlng Lab. , Mich.
695
154 269
SI
152 045
461
171 394
42S
171 366
De«>8cber Wenerdlenat,
570
153 366
Hotenpeiaaenbarg.
153 SIS
(Weai Germany^
261
152 541
731
154 523
Derekipmeat Eaq|laeerlng Corp. ,
154 525
Waahli^coo, D. C.
721
155 025
154 526
3e«ey, G. C. . widCo. , toe.
,
DiTld l^ylor Modal lulii.
New Yoric
7S2
155 324
WuUi^taii. D. C
62
ISO 459
Stamoad Ordnaofe Fiae Labe
152 797
Waahlngtoo, D.' C.
'ij
153 313
153 607
153 315
M
1S0 7J7
44
152 311
176
150 391
45
1S0 31S
2S7
153 726
152 309
310
152 734
152 314
S2i
153 574
171026
440
152 669
♦
SS
149 547
*.
153 953
S6
152 312
99S
154 766
110
152 310
608
154 76S
164
152 920
154 766
211
152 91S
•
601
1S4 767
220
152 653
> — ,
721
156 577
293
152 S61
735
154 507
ISSOM
1,
152 655
152 922
744
ISS2SS
153 496
745
149 r4S
311
171 050
153 706
337
152 923
153 707
991
153 505
765
15SS7<
i I
425
153 579
774
153 919
1 1
437
152 654
154 165
\
152 917
OvrUwa Lab. . S«at«aa laat. of
153 478
TadL. HobokM. N.].
64
152 130
469
171 187
730
153 713
722
155 618
Dayatron Irm i waai.
!
171 582
Ardilald. PB.
43S
150 696
7SS
148 958
Dayioa U. . OWo
736
155 063
i
S02
171 559
Oaytoa U. ■wMriii Ibm..
3tekectrtc8 Lab. . Joboa
GWo
635 .
171 544
Hopkliw U. . aeltimore. Md
45
150 806
Datnaa Atoalc Sufvort AgMcy,
nglial Caaip«er Lab. . Maai
WaaW^ua. D. C.
334
153 030
taal. ofTacb.. Cambrldfe
45
150 754
464
171 361
765
155 376
541
154 402
[)lglul Compuier Lab. , U. d
Daltaai Matala ta^fmailaa
IlUaota. Urbaaa
77
152 109
Ca«ar. laaaUt llwiiiiui
570
152 915
hML. Onli-bin. OMo
66
151095
995
153 415
^4
70
161 215
774
148 394
92
1SI096
161 216
nkOTTOod Corp. ,
7SS
154 103
93
161216
Attwquerqiie. N. Mex.
599
ISO 904
«•
161 219
Mrectoraie at Adranced
19*
161230
161221
riiimii Tack. . Wrlftat Air
niiilii>iaiM n Wrlfht-
161 233
httaraoo APB. Ohio
768
171 256
.
161 234
CMractoraie of PU|iu and All-
199
151 072 -R
Waaiker Taaiinf. Wrifbt-
301
151094
Patteraoo APS, Ohio
286
153 630
217
16t 222
Dtractorate of Kaaaarcb
311
166 227
Aaatyala. Hollofnaa AFB,
SIS
161 23S
N. Mex.
961
153 825
sa»
161336
-
153 826
SM
151097
DouKlaa Aircraft Co. , lac..
161 213
Loa«Baadi. CaUf.
446
171 398
4S7
151 101
464
161 290
Saata Monica. CaUf.
S62
154 970
446
161 233
786
152 061
4»
IH 096
161 229
[)id>Mn Inac. (or Advanced
809
ISO 243
4M
151 100
Scudlaa (Eire)
333
152 768
4M
151 103
Dugvay Provlnf Groind. Utat
760
146 212
474
161 22S
DiAaU., Durbam. M. C.
77
152 066
610
161231
152 067
161233
118
152 066
161234
193
152 069
161 235
Di*e U.' Medical Caeaer.
663
151 102
Otttam. N. C.
539
152 837
6U
151099
timtmm Lab. . Tale U. . -
114
151 OM
Ne* Haven. Conn.
570
171 542
740
161 239
77»
151 107
- ••
SOMTce
Oailap and Aaaoclatea. Inc.
Stamford, Cono.
r^t FBNuaibar
Durbam U. (Gt. Btlt.)
Dynamic Aoalyala and Control
Lab., Maaa. Inat. cfTbcta. ,
Cambridfe
Dynamic Developmenca, Inc.,
Babylon, N. Y.
Dynamic SimuUtkxia Lab. ,
Ontoaoce Tank- Aiitomotl««
Coofmand. Center Line,
Mich.
259
ISO 317
260
147 305
571
153 758
722
150 910
ISO 911
90
150 929
98
150 937
443
152 525
535
153 202
807
147 787
88
150 478
150 479
307
152 845
S88
153 562
738
153 866
... I-
!•
Source
Eagle-Plcher Co. .
JopUo, Mo.
Eafle-Plcher Reaaarch
Laba. , Miami, OUa.
Eaai Coaac AeronauUca,
Inc. . Pelham Manor, N. Y.
Eaacman Kodak Co. .
Rocheaier, N. Y.
Ecole Natlooale Superteure
de Chlmle de Straabourg
(Prance)
Ecole Normale Si^rleure
(Prance)
Edlnbui-ghU. (a. Brit.)
Educaaonai Research Corp. ,
Cambridge, Maaa.
PB Numbar
E<hicatlooal Teetii^ Servlc^
Prlncetoa, N. J.
Eltel-McCulkM^. Inc.,
San Carlos. Calif
Electric Storage Baaery Co.
Weei Orange, N. J.
Electric Storage Baaery Co.
YardJey, Pa.
Electrical Engineering
Reaearch Lab. . U. o(
llUnola, Uriiana
436
153 231
211
149 708
294
153 273
164
165
149 703
152 239
466 153 281
Electrical Engineering
Reaearch Lab. , U. of
Texaa. Auatln
463
23
5
361
135
394
595
68S
571
4S
165
46
189
214
294
476
804
81
155
30r7
220
283
559
788
804
150 693
171 122
171 063
153 631
148 393
148 018
147 363
150 433
171 492
152 ir
149 697
152 131
148 290
152 S61
149 636
149 637
152 486
152 489
152 876
154 448
150 649
148 710
152 158
152 159
149 060
152 951
153 081
154 102
147 840
Source
Electro-MecbanlCB Co. ,
Auatln, Tex.
Blectro-Opclcal Syatema,
Inc. , Paaadena, Calif.
Page PB Nianber
105 150 927
Electron Phyaica Lab. ,
U. at Mlchlfu, Ann Arbor
Electron Tube and Mlcrxiwave
Lab. , CaUf. Inat. cf Tech. ,
307
342
788
722
Electron Tube Reaearch
Lab. , U. of Mlnaeoou,
Mlnneapolla
Electrxinlc Communlcatlona,
Inc. , .Tlnxmium, Md.
Electronic Defense Lab. ,
Sylvanla Electric Producls.
Inc., Mounuin View, C:aUf.
Electronic Syatema Lab. ,
Maaa. Inat. ol Tech. .
Cambiidfe
Electronic Tech. Lab. ,
Wright Air Development
Olv. , Wright -Paneraon
APB. Ohio
Electronics Reaearch Lab.
Northeaatern U. , Boaioo
Maaa.
Electroolca Reaearch Lab.
Stanford U. , CaUf.
115
347
723
295
723
208
723
286
451
622
158 100
149 706
155 573
154 501
154 502
I
150 447
152 996
148 323
152 735
154 450
152 536.
154 89
152 885
153 560
nS4 843
34
46
185
436
165
153 360
17^ II6\
148 257
150 645
148 715
153 722
153 381
Source
Electronics Reaearch Lab.
U. ofCaUfornla, Berkeley
Pais PB Number
Elk Electronic Laba. , lac
New York
Engelhard Induatrlea Inc. ,
\ Eaai Newark, N. J.
Engineering Div. , Air "
Materiel Command,
Wright -Patteraoo APB,
Ohio
Engineering Research
Associatea, Inc. ,
St. Paul, Minn.
Erie Realator Corp. ,
State College, Pa.
Eaaex Electroolca,
Berkeley Helgbu, N. J.
i 47
146 TSO
150 511
152 115
108
150 374
165
149 734
152 562
230
149 735
295
147 314
152 741
152 899
152 861
152 994
396
147 313
152 860
319
lasoo
338
152 960
436
153 400
467
152 931
571
153 937
153 938
595
153 313
631
153 488
733
150 109
724
148 OM
150 792
153 704
153 705
760
193 211
807
148 502
296
152 992
165
149 698
103
152 298
158
147 374
417
154 292
612
154 759
571
154 747
724
153 723
47
150679
I
>
W»br\c Research Late.
lac. . Oedham, Maaa.
Pacuite dea ScMacaa,
Oraay. Praace
rHicMU Aircraft aad
MteaUanT.
314
100
710
f»N>anter
171 311
ISO 349
1S2 494
1S5 146
PalrcMld Camera and
laMrumm Corp. , Syoaaet.
N. Y. 223
PaiJrctilid Uaaaca 01*. .
PaUcMU Ei^tM aad
Alillliii Corp.. NMYork 7S
Padaral A*laik)a Ageaey.
Ailair Oty. N. J. SS£
Hartoaal A*lad«a Paciimea
rinniiaaial Caawr.
AilaadcClty. N.^
Pcla Ora^ DrnaiBlca Ca«cr.
U. of Delaware, Nawark I
539
' All— I. Ooror,
N. J.
taMarch Lata. .
' Aiiiaai. OD««r,
M- J-fea^)
60
6*
70
MO
173
315
316
437
43*
453
St2
693
73«
141 2*5
171096
150 472
171 545
141662
14*914
141916
149 960
150 825
150 970
146 225
161 163
152 351
152 079
149 066
149 670
150 013
149 963
150 097
152 316
1J3 HI
171 326
153 3*6
153 627
153 857
150 730
153 022
Sourca
f Ugfat Acceaaortea Lab. .
Wrlghl Air Developfneat
a*.. WrtftM-Paaeraaa
API. OWo
I 'U^ aad Eaglaeennf Teal
Group, WrlgM Air Devetap-
Dl». , WrlflJi- Patter -
API. OMo
'U^ Coatrol Lab. .
WrIftK Air De'velopcneot
Dl». , Wrlght-Pattereoo
API. Oklo
'UgW Safety PoundaOoa.
• lac.. Phoenix, Arta.
'lorida State U. .
TUlateaaee
Florida U. CoU. al
Agrlculcure. OalaeaviUe
lortdi U. Eaglaaerlng and
laduanial Eapertmcin
Siattoa. OalaasvlUe
Fluid Dyaamlci Reaearch
{ Lab., Maaa. laat. of
I Tteh. . Camtrldae
Pood aad Drug Reaearch
[Late. , lac. . Htm York
ford laliiaiiwr Co. .
Loag lalaad City. N. Y.
IPoreal Producta Lab. ,
Wto.
.tut fOr
nqntk dv Sirahlaatrleto
a. T. . StuRfUt
(Weal Germaay)
Poaiar. ]ote ]. . MTg. Od. .
OoauMeaa, Calif.
fm
FINuater
Source
Prankford Araeaal.
Par
FSNumter
PkiladalpiiU. Pa.
173
153 014
PiMkfurtU.
49i
171363
(Weal Oerraaay)
442
130 719
478
171 385
Prai*lln Inat . Late, tor
562
171552
Raaearcb and Develop-
meot. nmadelphla. Pa
95
201
442
'ISOBSO
152 074
153 128
770
783
171604
171 616
5*7
627
155 001
171 543
pranklln Inat. .
Philadelphia. PH.
612
171 OtS
Pretank Co. . Ocndale.
37
171 116
Calif.
582
153 614-1
710
155 255
153 614-2
•m
171593
739
153 615
154 289-3
38
14*870
Pree U. of BerUa
(Weal Oermaay)
150
152 563
147
148 678
148 679
Prick Chemical Lab. .
631
153 311 :
695
14*937
PrtacetoB U. . M. J.
23
ison*
14*93*
40*
14*021
150 923
687
14*966
.'^
9W
154 109
' 152*95
1
M6
699
149 0*3
348
152 137
171575
550
152 409
Prlti Enflneerlng Lab. .
696
154 251
Lehigh U. . Bethlehem.
Pa.
Prlis-Hater-lBstltui der
83
152143
296
152 603
Max-Planck Oeaellac haft.
Berlin- Da hlCTH
21
150 671
(Weat Oermanv)
Puela Reaearch Lab. .
145
152 21*
724
150 900
Maaa. laat. of Tech. .
Carobridfe
315
171 306
M
148 7r
Pulmer Raaearcb laal. ,
171 l«S
Ud. (a. Irtt.)
201
152 261
710
473
171 166
171 167
171 16*
134 935
150 6**
149 71*
550 153 443
Source
Caa Dynamlca Lab. . North-
weatern (J. , E¥anaton, 111.
Caa Pynamlca Lab. ,
Princeton U., N. J.
Galea aad CrelUn Late, of
Chemlairy, Calif. Inat. of
Tech., -
PM» pi Ntanbar
21* 152 443
28 150 170
General Applied Science
Late. . Inc. . Weatbury.
N. Y.
Oeaeral Atomic. San Dteaa.
Calif.
General Broaxe Corp.
Garden Qty. N. Y.
General Electric Co. .
Detroll. Mich.
General Electric Oo. .
Evendale. Ohk>
General Electric CO. ,
Owenaboro. Kj.
406
551
•6
177
791
799
725
330
770
47
426
Oeaeral Blectric Co.
Richland, Waah.
General Electric Co.
Scheaectady, N. Y.
153 136
152 102
US US
148 6*9
171 1*4
154 457
153 584
153*64
171 34*
154 572
171 117
154 4*4-1
154 4*4-2
206 152 283
General Electric Co.
Syracuae. N. Y.
47
106
177
296
342
467
5*7
48
297
725
152 667
14*234
152 145
149 694
152 610
171 340
153 683
14*011
150 805
152 660
152 93*
155 073
A
90
Source
General Electric Reaearch
Lab. . Scheaectady. N. Y.
PB Nianter
Oeaeral Electroalc
Inc. , Cambfidge,
General Mllla. Inc. .
Mtnneapolla, Mlu.
General Telephone and
Electronics Late. . Inc.
Bayalde. N. Y.
Geo^apMachea Inatltui der
Unlwraltli ZOrlch
(Switzerland)
Qeophyalcal Inat. , U. of
AUaka. Oollege
Geophyalcs (>>rp. of
America. Boaton.
George Wtihington U
Waahington, D. C.
211
330
342
439
461
462
475
619
6»
734
426
725
165
623
627
705
211
40*
571
6r
( '
M
149 063
171 34*
152 473
171035
171993
152*66
150 71*
171 523
133*19
153 *73-l
171 395
153 241
150*47
1S0*«3
1713*3
134 0*7
134 MB
134 37ft
152 434
171373
153 431
153 682
752 155 438
2
150 378
lOS
150 933
ISS
14*66*
14*9*3
149 062
230
153 333
13*
17100*
144
171001
157
171004
305
l71<Rtt
30*
171001
Source
"r
PB Numter
George Waahli^lon U. ,
Waahington, D. C. (con.)
222
171003
442
153 145
750
153 756
OeorgU laal. of Tach.
Engineering Experiment
Sudon. Atlaau
166
152 231
ro
153 343
343
149 693
149 696
348
152 7*9
590
154 751
725
154 166
Oaorgla U. , Athena
414
150 721 ,
Duarte. Calif.
736
133 36*- 1
155S6*-2
15SS6a-3
15SS69-1
abte and Cox. lac. ,
New York
*9
152 416
Gordon McKay I ,aK, of
AppUed Science, Harvard
U. . Camtarldge. Maaa
343
149 62*
GBttingen U.
(Weat Gennany)
221
14*287
Graager Aaaoclatea,
Palo Alto. C:allf.
Grumman Aircraft
Engineering Corp. .
Bethpage. N. Y.
148 288
297 152 671
779
780
Guggenheim Aeronaudcal
Lab. . Calif. Inat. of
Tteh. . Paaadena
Guggenheim )et Propulaloa
Center. Calif. Inat. of
Tech. . Paaadena. Calif. 633
791
Gultoa Induairlea, Ik. ,
Metuchen, N. J. 736
Cuataf Werner last, for
Nuclear Cbemlatry
(Sweden) 4(h
153 753
153 750
153 751
7*6 149 540
14*936
148 935
155 S67
153 304
fie PB Number
Haiotd Xerox, lac.
RochrateT. N. Y.
427
171380
HMnbuTf Model BMin
(Weat OeriMny)
I7«
148 721
Harpux CoU . Sum U. ol
Now York. Badican. H. Y.
479
133 121
Hkrni Reaearch Laba. ,
73
IS0S4S
HprowdCoU. ObMroacory.
CHBkrl^e. Meet
2
150741
131
148 6*9
148 713
534
153 285
Ml
154 585
Hanard Onduaa School a<
■aalaMa A^ataiatrabai.
Cmbrfaiie. Maaa.
394
153 287
Harvard Medtcal School.
Boacao. Maaa.
141
152 364
Harvard Sctml at PubUc
Haakk. BoaKB. Maaa.
177
153 OOS
HarmrdU. . Cambrtdfe.
Maaa.
140
150 966
1«5
152 372
152 373
IM
132 374
319
152 369
152 371
152 375
152 376
4t3
147 900
596
152 370
624
153 154
696
171 571
ttanard U. Ut. of
B^Mail^aad AppUed
Phyatea. Onikrld«e.
Maaa.
192
149 627
6<a
171 531
mnmr AliaataMB. hK. .
Tbrrmme: CaUf.
562
171 529
Havwlyd OoU. . Pa.
427
153 101
HmmU bat. or Oeopiiyatca.
Hoooluiu
m
149 668
152 613
706
154 566
HMvkar SMdetey NiKlaar
taMrCb., Ud.
». Irtt)
753
153 914
Source
f*r
n Nunber
Source
rsm.
n Nimber
Haacltlae Elactroolca Corp.
Homrd loduatrlea. lac. .
UtUa Mack. N. Y
' 572
154 418
Racine. Wla.
725
ISO 846
Heat Tranafer Lab. , Maaa.
HiKteon Uba. , ColumbU U. ,
UK. of Tech. Cambrldte
32
150 444
150 445
Mr* York
Hi^bea Aircraft Co. .
707
153 781
Htferc* U. (larael)
186
152 439
152 440
Culver aty. CaWf.
166
148 297
148 729
152 441
212
171 177
152 442
263
153 387
212
152 450
•
551
171 522
449
153 306
Hufhea Reaearch Laba. .;
153 308
MaUbu. CaUf.
298
152 841
551
171 497
427
153 396
Heidelberg U.
726
154 595
(Wea( Oemaay)
141
152 539
154 596
Hanry Ford Hoaplcal.
Detroit. Mich.
Hemea Elactrooica CO. .
4aa
153 164
Hianan Pactora Reaearch,
lac. , Um Aofelea. Calif.
136
152 156
152 157
Cambrld«r. Maaa.
81
150 484
264
152 888
Heinwa Elactroalca Co. .
395
153 126
Ounbridfe. Maaa. (cob.)
297
149 708
149 709
149 710
154 087
Human Reaourcea Reaearch
153 141
Haaae-Eaatera DIv. ,
765
Omce, Oeorge Waahlngtoo
U. . Waahli^KM, D. C.
136
361
148 728
152 580
PUglaex Pabnca, lac. .
152 788
Cambrtdce. Maaa.
311
153 272
537
153 2U
HM^ Altitude Obaervatory.
683
153 865
Baulder, Cok>.
106
150 932
Hunan Sclencea Reaearch,
258
152 946
Inc. , ArUnftoo, Va.
121
150 836
706
154 275
150837
150 838
Slaalord U. . CaUf .
616
148 155
^
150 839
618
148 154
152 146
619
147 553
334
132 821
#
784
150 171
477
153 129
HUler Aircraft Corp. ,
Hvdel. Inc.. Wattham,
Palo Alao, Cam.
38
150 783
Mua.
637
147 756
158
149 075
Hydraulic Eogineertng Lab.,
417
153 083
U. of Callforola. BerUley
32
152 645
NUler HeUcopier Corp. .
Hydrodynamlca Lab. . CaUf.
Hk> Alio. CaUf.
711
153642
Inat. of Tech. , Paaadena
608
154 745
Ifefatra CoU. . Henpatead.
T74
154 871
N. Y.
140
147 529
HoaeyweU Reaaarch Center,
Hopkloa. Mlaa.
343
149 684
152 891
1-
794
150 558
,1
HorlaoM. tec., deielaad.
..
OMo
589
171 5X
t
"-
- * I
I
Source
flMiwtr
i\
UllMUIaat. B<1Mi..
CMcafo
9S
150 470
144
152 528
14S
148 680
J
199
152 017
324
147 310
468
1S3 552
996
153 146
"■
7«
148 095
•
7«B
153 124
nuaola Staia Waiar Sirvay.
Urbane
in
152 227
4^2
153 239
llUaota U. . Urbav
i
150 490
ISO 830
•
\ 'J-y>-
150 831
l|» ■
150883
no
150 543
130 544-
142
148 724
1
147
171 141
1
199
148 675
203
150 860
212
152 291
, 1
319
152 972
" ■
329
171 193
344
152 683
395
153 168
453
153 119
■ »■ ^
171 S74
462
159 151
470
152 604
■ » - ; .
551
152 884
»
585
171 576
596
153 155,
\ »
616
149 315
1
627
153 839
628
153 138
153 772
•
717
154 114
768
154 958
780
154 553
llUaoU U. CoU. of MadtclM.
Chlcafo
16
150 565
17
150 570
746
155 566
IlllaoU U. B«laaerli« Bx-
perlmaot Statloa. Urtaana
552
153 836
628
171 113
Imperial Coll. , Loadoa
(Ct. Brit.)
30
150 420
i '
ISO
152 206
152 207
2ao
152 774
152 775
153 S9f
sss
153 390
ladUaa Siaal aad Wire Co. .
lac.. MuDCia
612
154 419
ladlaaa U. , Btoomlngcoo
554
149 821
805
153 805
ladlaaa U. Sdiool of MmUcUm.
IndUaapoUa
400
153 903
544
153 401
InduatrUI Teal Lab. , nuiadal-
phU Na*al Shipyard. Pa.
143
153 010
782
159 250
92
lageraoll Kalamasoo DIt
•org-Warner Corp. , Mlcfa.
laatltut lUr AalinaUactae Flayalol
acta der J. W. Goadia Uaivar-
aldlt (Waat Garmany)
laadOK Paaiaur. Parle (Prance)
I lor Advancad Study,
N.J.
laatltuie lor AppUad Bxperlmea-
ul Paycholonr, TiAa U. ,
Medford. Maaa.
749
laatltuH tor CooperaUva Ra-
aaardi U. al taMayhaala.
Fill lade IpMa
Inetltute for Fluid Dyaamlca
•od Applied MadMoatlca, U.
of Marylaad. Collafft Part
479
153 917
267
408
152 690
152 685
186
596
152 491
159 678
8
14
122
399
477
192 107
192 198
190 495
147 593
152 914
199 770
77
190 641
86
192 047
192 179
920
149 729
149 790
924
192 609
Sourca
Inatltuia for Fluid Dynamica
and AppUed Madietnattca, U.
of Marylaod. Collafi Park
(con.) :
laatltuie for QuantliaUva Re-
aearcb In Ecooomlca aad
Maaagenient, Purdue U. , ^
Lafayeaa, Ind.
Inatltuia fbr lUaaarcti In SocUl
Sdance, U. of Nonh CaroUna,
Cbapel Hill
Inadtuie fbr Syatem Reeearch,
U. of Chicago, III.
Paie PBNMBber
406
700
761
788
224
479
940
81
InatltuM for die Study of Meula,
U. ofOilcatD, 111.
95
408
806
InaUtute for the Study of Rate
Proceaaea, U. of Utah,
Salt Lake City 700
Inetltute of Aeroptayalca, U. of
Toronto (Canada) 194
Inetltute of Anatomy, U. of
UppaaU CSweden) 404
laatltuie of Andean Biology,
Lima (Peru) 267
Uwdtute of Eoglneerliv Ka-
aearch, U. of CallforaU,
Berkeley \ 83
89
118
324
470
474
",«3
606
609
774
776
78
476
761
Inatlnna of Plight Structuree,
ColumbU U. , New York
Inetltute of Geodeay, Photogram-
metry and Cartography, Olilo
State U. Reaaarch Poundailao,
Columbue 282
Inetltute at Gaophyalca and
Planetary Riyalca. U. of
California, Loa Anpelea
inabtutt of Matepiatlcal
Sd^acaa. NeirYorfc U. , N. Y.
557
Inetltute of Meula aad Ex-
ploelvae Reaearch. U. of Utah,
Salt Lake City
Ineutuie of Opdca, U. of
Rochaenr, N. Y.
221
100
108
186
192
221
320
924
944
949
427
476
572
691
761
779
Ineutuie of Polymer Reaaarch,
PDlytadulc Inat. of Brooklyn,
N. Y.
laadtuM of Raaaarch.
U.. BadiWiem. Pa.
laeitlHH of Rubber Raaaarch.
U. ofAkroo. Ohio
to
219
941
628
547
390
75
916
757
798
149 731
154 509
147 904
154 080
152 125
153 148
147 767
171 080
m 144
171 987
171 388
150 467
150 468
153 765
154 865
154 709
148 694
153 904
152 763
150 524
150 540
150 762
148 406
171 360
154 293
153 767
153 118
150 510
150 624
155 153
150 993
148 525
150 994
152 799
152 800
154 810
152 174
150 944
ISO 945
148 691
192 449
148 299
192 491
149 691
192 725
192 842
193 7r
152 781
152 726
190 946
148 906
148 907
192 117
150 747
149 070
149 651
153 670
148 788
153 882
150 491
199 172
190 844
ISO 845
Sourca
Inadtuie of Sclanoe awl Tech. ,
U. of Michigan, Aaa^rbor
Inadtuie of Stadadca, U. of
North CaroUna. Chapel HiU
InaaiUM of Tach. , U. of
Mlnneaou, MlnneapoUa
Inadtute of Theoretical Aatro-
phyalca. U. of Oalo (Norway)
Inatitute of Theoretical niyatca,
Sunford U.. Calif.
707
802
186
187
222
996
997
761
762
110
320
470
597
692
762
632
616
692
Inadtuie of Tranaporutlon aad
Traffic Englneertng, U. of
CaUfornla, Berkeley
784
Inadtuu da Qulmlca Flalca
(Spain)
IntermounraIn Waaihar, lac. ,
Salt Lake City, Utah
Intemadooal Bualneea Machlaaa
Corp., Klngatoo, N. Y.
Internadooal Buaiaaaa Machlnee
Corp. , Yorktown Heltfia,
N. Y.
98
417
562
25
700
412
599
296
323
IniemaHaaal Inat. of Meteor ol-
ogy, U. of Stockholm
(Svadeo)
toooaphere Raaaarch Lab.
Ptanaylvania State U. ,
Unlveralty l^rk
451
452
765
766
90
31
Iowa Engineering Bzperimeot
Sudoo, Amaa
Iowa laat. of HydrauUc Ra-
eearch, Iowa City
Iowa State U. , Iowa City
Iowa Sttie U. of Sdaace and
Tech., Amaa
lac., Waeiwoad.N.J.
larael Inat. of AppUad Social
Reaaarch
laraal laat. of Tech. . Haifa
ladtun dl Chlmica Flalca
delllMvaralta, PavU (Italy)
91
119
195
389
384
298
415
559
791
86
2
9
•7
29
597
8
926
276
PBNiaiiber
159 915
194 508
148 6B9
148 692
148 684
148 667
148 696
148 tM
148 695
199 891
199 892
199 893
139 840
199 894
154 088
154 123
154 094
154 124
ISO 501
149 644
147 120
159 660
193 679
194 452
152 656
159 188
159 189
153 186
L59 189
153 187
171068
171 369
171 S07
150 394
154 465
153 911
153 634
153 695
152 672
159 274
150 086-7
130 086-8
150 086-9
150 086-1
150 086-2
ISa 066-9
150 086-4
150 086-5
150 086-6
148 262
150 930
148 263
148 256
150 669
150 668
152 697
192 696
152 829
192 824
193 197
147 992
199 082
152 099
150 517
152 057
150 518
150 498
199 668
171 362
150 961
152 479
149 678
Source
iMttiKO dt Plaica, LUvvnta
« PhIov* (lulT) 40*
IMnao dl Pislca daUIMvar-
■ta. TrtMCe (luly) XM
iMluxo (U Picica SupBTiora,
UMveraiu dl Pavia (taly) 552
IS2«0S
152 OO
190 063
p^i n
■tltiMo Blactnxacolco
{ Nastoaal* ~CaUlao Pcrrarla'
I (Italy) 212 152 451
lacltMo Btactroaacaico Nazioaata
I "GaUleo Pemrta " (Italy) 4«6 ISO MS
PijB ro Nunilxr
(
latltMo Nadooal da Tacnlca
Aaroaautica Bataban Tcrradaa
(Spala) 179
m Lata. . Port Wayna, Ind. 552
ITTLaba.. Nuilay. N. ]. 41
110
152 502
171 197
ISO 678
ISO 547
K
r ,
r
Sourea
). G. Boflaaartiig Reaaarch
Aaaodaiea. Baltlmora, Md.
)a<D*a Porraaul Raaaardi
Oaacar, Prlocciaa, N. J.
Jaaaa fkatorlza Aaaoelaiaa,
lac., ■oaton, Maat.
JaBaiaoa Divla Hoaptul,
Houaioa. Tax.
n Numbar
90
1S0 4S0
336
149 6*2
64
1S2 15S
152 155
ITS
152 154
200
149 06*
32t
149 6*9
9M
154 104
174
152 429
21
153 640
Page PBNumbar
Jai Propulaloo Cantar, Purdue
U., Lafayettt. lad. 747
)at PropuUlcn Lab. , Calif. Inac.
oCI^di.. Paaadeoa 507
311
427
49(
447
Jnhannaa Gutenberg-Unlvcrattit
Malax (Weat Garmaay) 6*1
155 149
153 StS
153 791
153 990
1SS9S1
193 952
154 410
154 411
153 94*
153 949
153 718
S<mrc«
Jobo CarroU U. . Clevelaad,
!>■» WWimtar
Jobaa Haptboa U.. Baltimore,
Md.
Joboa Hivklna U. Scbooi of
Enclneertng. Baltimore, Md.
94
152 151
906
152150
572
153 775
71
ISO 646
166
14*714~
U7
l4*6tiS
194
14*677
727
152 965
7*2
154 261
572
154 4*3
775
153 7*3
Source
Kaoaaa State U, , Meobattan
KaaaaaU., Lawrence
Page n NuBbw
10*
ISO 096
209
148 712
14(716
19
1S0SS6
144
149 063
271
152 619
320
152*94
Source
^ge PB Number
I U. Scbooi of Ftaarmacy,
Lawrence 8
KaroUoaka Inatltutet,
Stockholm (Sweden) 12
KearlonCo.. lac., Unle
PalU. N. J. 307
Kellen Aircraft Corp.,
Wllkw Grove, Pa. 711
152 ON
14*269
152 778
153 851
Source ptge
KelloB lUdlactoa Lab. .
CaUf. Inat. otTacb..
Paaadena 99
Kentucky Research Foundation.
Laxla(ioa ||l
Kentucky (J. . LexU^toa 27*
409
PB Nianber
190 479
150 784
152 746
159 451
"U
Cdr/r-F
99
SOUTCT
Lataruotr* Centnl dn India -
trie* Blectnques (Franca)
Laborstolre d'Ii<r(Rot^
Tacbalque et Applique. Ctf-
■ur Yvette (Frmnce)
L«bor«tolre de FtiTototg-
vrntiamt, liwclnji de Fhyslqua,
Scrasbourf (Frince)
7»4
T92
SS7
7»9
iMbOTtoiTt Medltei I'ln— n da
Mdkerdwa Thermodyiiaml -
<|uaa (FTaace) 199
LabaratDtio dl Blanroctilmlca,
Chimlca Piaica • MMallurpa
del PDUtecsico dl Uilmmo (Italy) 25
L^bocasodo dl MeccaBftca
ApyilcaiB del FoUucaloo dl
i(kalr) M
lor Blactroalca. lac.
87
•1
aaarck, Maaa. laat.
Ra-
ce Tech.
I afciMaini'i at AatraiAyalca
aad rkyatcal Mawcaolnty.
Jotae Hopkloa U. . ■akliiiora.
Ill
2ta
SM
SS7
4«5
470
sn
628
3
109
UtanNory a( Aioalc awl SoUd
Slate nayaica. CoraaU U. .
Illiaca. N. Y. 25
Laboratory of Chemical aad
Soild-Siaia niyalca. Maaa.
iMt. of Tech.. Cantaldfe 794
Labaraury of CUmaiotogy,
nNmbar
152 199
193 407
153 277
154 364
152 304
171 079
150 346
ISO 347
149 993
150 541
149 726
149 72S
149 725
190 709
190 922
147 173
147 174
147 799
192 128
199 741
152 054
150 628
152 088
190 642
Source
Ca— ftoa. N. J.
1
190 614
190 619
190 616
31
190 617
706
154 527
Laboratory of Stanattcal Re-
eaardb. U. <rf Waabloctan.
■jaatrli
320
152 900
762
147 847
7S6
148 974
Laaoat Gaolocical Ofaaervaiory
ralUadea. N. Y.
'2S2
152 906
537
153 076
99S
153 075
Lead Locaantiaa Lab. , Ord-
Hbca Tkak-Aanana^
Camtmmt. Caaaer I Jan, Mich
67
150 999
790
152 004
152 006
791
152 006
192 007
192 001
152 009
Laagtay Porter Nauro^ychlatrlc
laat. , Saa Pranciaco, Calif.
539
147 561
L^CMWrU <Ci SrU.)
344
152 925
Ltrhrtrllmartarhea Ofcaanra-
tortun Aroaa (Swltaertaad)
34
192 006
UafB U. (hlilUB)
3
190 991
190 m
190 940
190 943
4
190 926
117
152 436
597
153 307
LUa Sa^pon Syaana Lab. ,
Wrt^ Air Diiilnpnunr DIt. ,
W n#u - Pfenwaoa AFIk OMo 711
171 599
154 273
194 767
190 369
110 7M
190 975
190 SM
190 606
?»m W Number
/■
Maaa. laat. of
(coa.) 46
50
60
78
82
87
111
119
120
136
166
167
174
167
190
190
207
212
218
223
264
296
299
300
308
330
321
323
344
349
391
391
415
426
429
436
499
492
495
471
544
599
573
997
601
610
190 796
192 041
152 295
148 366
150 438
130 592
150 593
ISO 595
150 597
150 609
149 773
150 601
150 799
147 S68
1S0S09
150 600
150 951
ISO 508
150 598
ISO 599
171 100
ISO 606
ISO 603
ISO 673
ISO 757
150 507
ISO 610
152 542
ISO 60S
150 604
152 241
152 467
ISO 797
150 798
152 063
ISO 793
148 281
150 602
ISO 795
152 465
152 466
152 637
152 638
152 »1
150 596
153 251
150 800
150 974
152 621
153 095
149 741
152 409
152 629
152 750
152 948
rt2 949
152 721
152 759
152 934
152 723
153 053
152 722
152 462
152 932
152 973
149 740
152 466
152 787
152 933
152 827
153 464
152 974
193 217
193 225
153 421
153 697
153 696
153 220
153 218
153 219
153 361
192 630
199 264
150 607
153 698
152 970
153 803
192 996
193 092
152 826
193 108
153 465
153 701
Source
Par
FB Number
Uacola Lab.. Maaa. laal. of
Ttoch. , Lexln(toii (con. )
621
153 700
622
153 804
629
153 563
153 699
727
154 061
154 589
739
154 588
762
152 957
■■I- 1
763
153 486
.
767
153 906
• .
*■' t
154 587
795
154 062
171 573
Uabon U. (Portugal)
803
154 449
Uttle, Arthur D. , Inc. ,
Cambridge, Maaa.
23
171097
72
150 282
•■■
446
171 405
1
559
153 566
1
573
153 246
590
171 515
756
155 256
Utton Induairlea, Salt Lake
City, Utah
429
153 245
Lockheed Aircraft Corp. ,
Marietta. Ga.
333
153 790
1 nckheed Aircraft Corp. .
Sunnyvale, Calif.
50
152 026
171 127
61
ISO 886
65
ISO 613-1
ISO 613-2
69
171 101
71
152 027
93
171 068
111
ISO 666
131
148 703
174
148 697
179
148 698
180
148 699
190
149 652
192
148 298
1
194
148 701
'. i 1
148 702
300
152 377
152 378
'( '
208
148 700
1
258
171 196
308
152 939 •
u
412
153 457
•
417
153 435
171 372
1
439
152 693
152 719
153 645
439
153 055
444
171 379
•
453
153 357
s
455
152 844
•
552
171 534
604
153 502
609
171 502
613
171 521
632
171 533
756
171 252
763
154 349
Lockheed Electroolca Co. ,
Metucheo. N. ].
Loewy-Hydropreaa Div. .
Balwln- Lima -Hamilton Corp.
New York
London U (Oi. Brit.)
Loulalana Slate U. ,
Baton Rouge
Lovell Technological Inat.
Reaearch Poundatloo, Maaa.
I U. (Swadan)
Lyman Lab. of Ftiyaica,
ItanrardU., Cambridge.
300
749
762
9
26
539
665
700
308
573
276
624
Source
McCrone. Walter C. ,
Aasociatea. Ohicago, III.
MacOonaU Ftiyalca Lab..
McCill U. (Caaada)
McOoaaall Aircraft Corp. ,
St. Loula, Mo.
McOill U. (CaiMda)
McCraw-Hlll BookCo., lac.
New York
MalUockrodi Chamlcal Lab. ,
Harvard U. , Cambridge,
Page WKhMbair
Mallory, P. R., and Co..
ladUnapolla. bid.
U. (Ct. Brit.)
Maai^cturli^ Laba. , lac. ,
Ombridge, Maaa.
Marine Lab. . U. at Miami,
Coral Cablea, Pla.
61
415
266
260
413
569
467
634
791
91
439
4
319
95
446
39
66
74
282
Marine Riyalcal Lab. , Scrippa
laatltudoo of Oceanography,
San Diego, Calif. 106
149
573
Marquardt Corp. , Van Nu^^.
Calif.
Martin Cov , Baltimore, Md.
MaryUodU., Collage Park
152 935
171 568-1
171 566-2
154 094
154 134
150 542
150 870
153 760
147 902
147 903
150 967
152 522
153 821
152 478
193 337
i
r
Maaaachuaetu laat. at Tech. ,
Cambridge
t
707
747
201
96
119
136
193
167
313
215
396
333
392
467
554
633
766
799
20
26
29
87
69
99
112
116
151
334
399
346
349
447
436
460
155 363
171 ISO
152 096
152 096
190 996
190 98^
190 691
150 969
146 300
147 646
146 672
192 447
152 179
152 314
193 936
149 690
149 732
149 733
150 723
153 291
153 735
153 r3
154 343
153 160
152 096
153 099
ISO 662
153 357
153 396
ISO 690
ISO 699
146 918
190 466
150 593
153 446
153 661
149 699
149 660
193 663
ISO oat
150 039
171 391
153 430
171 399
Source
BigB PB Number
152 062
153 061
149 666
152 952-1
152 952-2
150 723
171 494
153 153
154 113
154 262
155 459
146 569
190 609
190 610
190 669
ISO 993
150 994
150 935
150 936
149 070
171 066
171 400
150 769
ISO 954
ISO 766
150 770
150 771
150 772
150 773
150 774
150 775
153 625
152 676
146 240
154 545
194 546
153 761
Maaaachuaetta hwt. at Tech. ,
Cambridge (con. ) 466
471
•547
5S2
563
6S3
6B4
636
669
700
771
784
791
ao2
803
Maaaachuaetta Meoul Health
Center, Boatoo
Maaaachuaetu U. , Amherat
Material Lab. , New YotvT^
Naval Shipyard. Brookiyh
MaterUl Laba., Pt^et Sound
Naval Shipyard, Bremerton.
Waah.
Matertala Reeearch lab.,
U. of California, Berkeley
685
9
375
277
278
405
593
624
701
218
727
Maisriala Reaearch Lab. ,
WaiertoBm Araeul, Maaa.
314
756
213
«71
781
795
112
344
' 624
1 MaierUla Lab., Wright Air
2 Development Div. , Wrigbl-
Patteraoo AFB, Ohio 270
Mithematlca Reaearch Center.
U. of Wiaconain. Madiaoo 324
Melaba Inc. , Palo Alto, Calif. 51
Mellon Inat., Plttaburgh, Pa.
Malpu-.
Ya.
Inc. , Palla CSairch,
Mtlpar. Inc., Watenmra.
Meul Hydridee, tac. .
Beverley, Maaa.
Meala and Ceramica Lab. ,
Wright Air Development Div
Wri^-Patteraon AFB. Ohio
573
209
992
604
696
300
452
61
553
Reaearch, Lid.
MetaU R(
(Ct. Brit.)
Mocala Reaearch Lab. ,
Bnnre U. , Providence,
92
329
459
461
614
109
Meula Reaearch Lab. ,
Ckmegie laat. , of Tadi.
Pittabur^, ?m.
Mamorotoglc Lab., U. of
UUnola, Urbane
Michael Reeee Hoapiul.
Cklc^o. 111.
R.I. 349
446
629
36
604
tSl
399
152 874
152 962
152 877
153 769
153 660
153 675
153 676
154 967
154 432
153 661
148 214
ISO 031
149 778
154 706
154 092
148 353
154 449
171 610
150 503
IS0SO4
149 667
149 631
149 638
150 656
153 628
ISO 657
154 516
171 183
155 320
152 862
194 2B1
149 656
152 427
146 924
171 371
150 006
146 516
148 830
146 917
148 918
148 919
152 854
ISO 708
150 068
153 573
149 756
150 663
150 736
150 894
152 076
153 549
1S3 749
171 570
146 282
193 499
ISO 969
171 469
171 077
171 307
171 411
171 394
171 410
171 467
171468
190 644
149 690
153 439
148 559
152 069
153 656
152 227
153 365
Source
Michelaon Laba.. Naval Ord-
nance Taat Sndon,
China Lake, Calif.
Mlchlgin Sute U. , Beat
Lane log
Micfai^nU. , Ann Arbor
P»te PB Number
Michlpin U. Coll. of ^i^lneer-
tng, Ann Arbor
Michigan U. Coll. of Literature
Science, and the Ana,
Aon Arbor
209
443
321
397
762
20
67
195
347
456
459
539
609
803
96
463
466
476
775
792
409
552
S96
Michigan U. Ri
Ann Arlior
rch Inat.,
Microtech Reaearch Co. ,
Cambridge, Maaa.
Microwave Aaaoclatea, Inc.
Burlington, Maaa.
Microwave Lab.
Calif.
Stanford,
Microwave Fhyaica Lab. ,
Sylvanla Electric Producta.
inc. . Mountain View, Calif.
Microwave Reaearch Inat. ,
n>lytachnic Inat. of Brooklyn.
N. Y.
806
40
51
195
300
418
616
727
746
52
300
429
301
430
496
479
S74
347
S74
52
167
Mldweat Reaearch laat. ,
Kiuisaa City, Mo.
Milan U. (Italy)
Mine Safety AppUaacM Co.
Callery, Pa.
MiaaaapoUa-HoMywaU
Rngulator Co. , HopUna,
Mian.
215
901
313
336
349
390
430
974
S7S
999
619
736
796
143
195
26
144
409
963
148 661
153 286
149 663
153 524
153 669
147 847
150 488
ISO 998
171 179
171 336
150 982
171 366
154 866
149 782
150 534
150 637
153 171
152 836
152 835
148 951
149 567
152 611
152 612
153 200
153 266
153 267
150 726
152 135
152 3S5
171 105
149 672
152 995
171 404
148 215
150 902
153 847
1S0 4M
152 666
153 229
152 847
152 937
152 938
153 S04
153 650
153 098
153 503
152 633
150 896
ISO 875
148 960
148 984
152 365
152 364
152 662,
152 724
153 069
149 679
153 068
153 454
150 897
153 663
153 677
153 234
153 598
153 554
153 932
150 906
154 804
155 160
171 569
152 349
171 162
ISO 336
152 509
154 406
154 769
Pla.
Co. . St. Rnarburg.
U.. MlnaMpoItt
32
4
Si
71
U
"M
112
t«
154
3il
sn
918
M4
711
130 931
14t 260
1710)0
152 10*
152 2n
171 070
171 071
171064
190 633
14(676
145 291
171 199
153 433
153 626
171 556
153 646
1«7 176
153 133
158 771
154 111
171994
fm n
U. School a<
poUa
V. 5ctoolaf
!■■— rwi U. Sduol of
VMBrtBuy Madtclna.
$t. rami
14— l—IW< S
Itedasburf
SoiateniCoU..
14— tartppt StawU., Staw
CoUif*
I4»ip»»fr U. (Pruoa)
lAxn* SdHol of ElKOical
fcoclaaerlBg. U at Maaayl-
nola, nulffcilptili
693
299
992
534
21
199
996
711
319
U
167
191
198 754
149 645
141496
146 496
153 444
190 969
152 390
171 403
146 995
145 317
152 972
152 651
153 236
152 969
SOMTO '
ktoora Scteol at Btocolcal
BuflDMrliic. U. of PetuMTl-
maU. nuiadslphM (coa. )
M— rah, tac.. Chtcaflo. ni.
Mmotefa. be.. IkoaaU.
ArU.
Monrota. lac.. Rlvanldi,
CalU.
Monrota. lac.. ScottMiite.
Ariz.
MouBi Wuhtoctoa Otaarratory.
Goctea, N. H.
Uomt Wltooa Okaammry
323
153 596
153 597
334
171 399
431
153 954
575
171 549
171557
601
171 545
171 555
430
190 692
390
152 993
36
152 390
195
152 354
165
152 355
575
153 995
766
150 S4S
131
152 902
U. Outy)
NariDco laduacrtaa, lac. ,
San Diafo. Calif.
Narragaoaen Marlaa Lak. . U.
at Rhoda lalavl. ICli«itae
^4ar^lcol Corp. . Fhlladalfiua.
Pa
NaUoaal AaroaauUca aod Space
A^Blaiacradoa , Waahlogtaa,
O.C.
Nadoaal AvUdoa PaclUdaa
Bsparlmental Cauar, AiUotlc
Cttir. N. J.
115
120
199
253
592
'n
.-ICll
iil
Natioaal Suraaa of Swadarda.
Souldar. Colo.
Natioaal iuraau at Scaadarda.
Waahlaftoa, D, C
'r
Natioaal Caaoar laac. ,
Satheada. Md.
Natioaal Cartea Co. . lac.,
Pauna. Ohio
National Caah Raglatar Co. ,
Hawilioraa. CalU.
Natioaal laat. ol Ooaaaography
(St. 5rU.)
NatloMl laaUtutaa at Haalifc.
Natioaal Ubrary of Madlrtaa.
Waahlagtoo. D. C.
Natioaal Raaaarch Couadl.
Waahlogtaa. D. C
Natioaal Raaaarch Laha.
Ottawa (Caoadi)
Naval Mr Tmi
Panoaai Rlvar. Md
Naval ATladoa
SiaHoa.
36
472
37
35
99
430
961
n
130
ISB
l«
m
mo
619
450
696
767 1
505
23
26
52
102
106
112
156
20a
405
465
479
990
775
144
447
207
34
22
404
73
142
557
159
200
215
277
315
326
441
477
559
tat
611
711
729
735
301
Ttot
7». 792
130 556
190 925
153 259
152 907
171656
145 274
155 564
171094
171 02s
171 040
171 365
171 SOS
171 906
161 575
151 877-
151 377-
151 377
161 573
151 361-
161 579
151 377-
151 977
161 953
150 064
161 551
161 957
161 955
161 950
161 sn
151 sn-
161 559
161 571
161 574
161 565
161 575
161 576
161 565
145 691
161 554
150 923
161560
161 956
171 541
171 293
152 570
171 365
. 152 526
150 529
152 555
150 062
150 963
145 734
153 763
152 750
152 756
152 532
152 755
152 754
153 606
153 476
152 519
153 195
153 196
153 632
153 633
154 095
154 087
153 475
154 399
154 340
154 549
154 590
154 725
152 558
158 437
Settrea
Naval Arlonlca Facility,
Indlanapolla, Ind.
Naval Civil Eaglneerlag I
ton llaaaama. Calif.
Win n
Nival Bngloaarlng Bxperlmam
SnUoa. Anoopolla. Md.
Naval Baftaaarlaf Bipartiaaai
725
19f 457
Md. (oaae)713
155 565
803
196 051
181
171 152
• Naval Medical RaaM
rch loat. ,
313
182 940
153 942
Sadiaa<te, Md.
692
155 374
158 875
411
153 175
Naval Miaalla oad Aamaaodca
420
171.375
Caaiar. nKatMugu, CalU.
544
153 385
955
153 610
659
153 544
619
171901
Naval OrdMaea Lab.
, Coroaa
701
154 699
CalU.
61
171 114
712
154 615
122
152 055
154 679
430
150 707
719
154 625
976
153 394
154 633
601
150 073
194 635
730
171690
714
154 613
792
171254
154 614
506
154 071
154 619
Naval Onkaace Lab.
, Whla
154 633
Oak. Md.
89
145 178
154 625
302
171353
154 629
308
171 353
154 672
331
171 349
154 678
171 380
715
154 621
154 653
154 663
171381
171354
171355
154 666
345
149 735
154 669
553
154 813
154 670
576
154 771
154 671
630
154 812
154 673
629
154 770
716
154 647
634
154 722
154 6«
730
154 814
154 665
739
154 578
154 667
171656
154 665
753
171655
154 652
756
154 721
154 653
757
154 719
717
154 463
171 655
154 617
•
763
171-657
154 630
765
171654
154 633
771
154 515
154 645
772
154 816
• 154 654
795
155 386
154 700
796
155 385
718
154 644
503
154 730
154 652
Naval Ordoaace Taat Siatiaa.
729
154 618
Chlaa Laka. CalU.
31
150 867
154 624
99
153 352
154 643
61
150 456
154 651
71
150 990
154 650
191
152 345
154 651
250
152 699
790
154 699
152 700
154 686
305
152 826
735
154 684
153 867
736
154 626
313
153 853
742
154 622 .
315
152 525
154 642
321
171 327
743
154 627
935
152 632
154 655
387
149 654
154 657
341
149 643
154 675
418
153 404
154 677
t
430
153 054
154 659
431
158 221
744
154 674
f
499
153 056
745
154 616
154 640
154 664
443
152 790
153 181
153 290
746
154 649
456
154 403
154 660
462
155 407
154 662
353
155 457
154 576
556
153 449
747
154 635
154 646
625
634
154 730
154 755
748
154 637
694
154 210
751
154 695
799
153 647
753
154 620
153 730
154 636
767
153 930
795
154 690
154 661
504
156 440
•rdi
751
154 611
PlaU Activity, Sao
DJapo.
154 612
CaHf.
134
152 131
154 641
.
361
153 636
755
153 905
Naval PoacgnAMi Schaat.
154 697
MaMray. OalU.
]5§
153 063
790
154 631
797
158 064
154 333
67
192 642
Naval Radiotatlcal DMhaaa
150
153 254
Lak., Saa Praadaco, OaU.
99
152 677
SIO
153 793
102
152 644
965
154 746
152 646
•15
154 509
<
302
153 283
Pige n NmnlMr
Source
Source
1 Kadtok^pcal
Lab., Sao Pranclaco,
CatU. (con.)
Naval iMMTck Lah.,
D. C
NMMlScteeiafA^
Pk.
Nmal SuparMSlc Lab.
taai. of Tach. , Camtarl^pi
MrvBl St^piy Kaaearcti i
Oevelofiaieat PadUty,
■ayoaaa. H. J.
Naval TruolDC Dartoa
Port Waaiuofiaa, N. Y,
NanI Weapoaa
OabJcraa. Va.
206
219
X7>
274
277
332
333
334
ses
9i9
7*2
7*3
783
32
71
92
96
IM
US
14«
im
IM
200
309
223
234
277
2M
SOS
309
»*
3S2
409
431
441
4«5
4M
M2
363
S76
990
991
M7
639
713
730
769
771
M»
769
US
327
436
474
103
441
393
!«•
61
65
479
963
740
7M
152 795
171 ISS
153 569
153 571
153 566
133 071
153 622
153 621
153 066
153 070
153 570
154 303
134 754
154 717
153 691
153 S62
146 395
149*49
146 402
161921
161 696
161767
161 764
161 749
147 632
161 2M
161946
161 967
161 966
161716
133 011
153 012
147 963
147 964
149 296
166 663
171 314
130 619
150 618
153 576
153 577
161 9«6
171046
171051
149*30
149 297
171 315
161 990
143 302
150 319
149 520
149 296
171 316
161 (34
171 0S2
171 396
171 107
161933
171 199
171490
171 491
171 317
171 479
171691
131932
171 16*
171 31*
155 067
147 7*0-4
149 344
153 104
153 106
133 106
133 103
ISO 77*
153 196
171 532
133 007
190 626
150 972
152 97*
133 S51
139 296
139 904
$aTy Btectroaica Lab.
iSaaOeflD. CaUf.
SSI
611
32
S3
kitodical NaumpaTdUatrlc
Beaearcfe Uail. Saa Oaft.
Calif. 467
^▼y Uadarvatar Souad
lalwaiii » Lab. , OrUado.
Ph. 302
fapaDlT., Palrcblld Boflae
aad Alrplaae Corp. . Oak
RUiia. Itaa. 763
^iatfaerUada Ship Modal hwla.
Wagralafeo
ilew Oapartura Dtv. , Geaaral
iMoMnCorpa
i Coaa.
lU.
BnatoL
F
7*4
746
199
406
534
mm Jaraey Ceramic Reaaarcfa
I SodoB. Riaaara State U.
Is
Maslco State U. ,
tJWaeraity Part
Ilew MezlcaU.. Albuquerque
Vam Mexico U. BafUiKrlag
I Bxpertoaaat Stadoa.
I Albuquaniue
Um Yock Medical Coll. . N. Y.
^aw Yort Saa CoU. al
I Cerantca. Alfred U.
YortU.. N. T.
591
799
299
799
7*2
4av Yocfc U. CoU. st
Bi«laaarli«. N. Y.
lOcboto CbanlatrT La6..
YortU.. N. Y.
DiT., AlUad
calCorp.. Ilopaanll. Va.
«t riyalca.
i(SMdaa)
Jbc ktaarlato Lab. .
Wrl^ Air DrvelopoMM DIt.
Wn^-haeraoa APB, Ohio
ktorake MetaorolotlakB
■aadnti (Narway)
^tonfc AaMrtcaa AvtaOoa. Ik.
CaHf.
730
546
113
la
349
991
734
10
93
113
341
345
460
471
940
9SS
796
31
SS
195
199
216
221
619
49*
960
706
560
331
431
71
72
1*0
474
261
Monk Aaerlcaa Avtattaa. Mc
m A^Blaa. Calif.
Nor* CaroUaa S(a« CoU. .
MO
199
19
aos
776
100
149 799
193 93*-
153 926-
152 643
192 615
154 593
192 979
195 429
199 431
199 432
199 426
193 729
171 131
153 215
153 216
153*7*
150*99
150 915
152 966
149 911
154 704
155 079
153 152
130 537
192 344
192 944
171 990
192 960
190 639
171 062
150 443
152 634
171 396
171 412
150 323
199 0*0
130*99
153 936
150 437
190 764
192 921
171 194
14*722
192 396
193 034
193 791
199 009
190 060
199199
193 649
194 970
153 567
171 301
130 720
171 059
171 063
171 196
171 918
192 769
154*0*
159 14*
171 199
190 960
171 143
199 3S2
190 702
1S9 673
19SC73
Hga n Number
North CaroUnaU.. Chapel HIU 450
472
763
796
North CaroUoa U. School of
Medlclae. Chapel Hill 66*
North Dakota U. , Graad Porta 399
Nonheaaara U. , aaatm. Maaa.799
Northrop Corp. , Havthorne,
CaUf. 267
Northveaarn Tacfaoologlcal
Inat. , BTanatco. III. 78
79
133
224
999
63*
Bvaaatoa. lU. 27
Northvaaara U.
Notre Dame U. . lad.
Noyea Chemical Lab. . U.
UUaoto, Urbaaa
79
132
331
345
776
196
624
210
409
947
634
701
Nuclear Drvelopmeot Corp.
of America, Whta Plalaa,
N. Y.
Nuciaar Meala. lac.,
Coacord. Maaa.
Nianarlcal Aaalyala Raaearch,
U. at CalUbmla, Loa Aagalea
600
96
447
322
150711
153 564
155 06*
152 230
171 607
153 542
154 455
171 32*
150 462
146 199
150 481
146 197
146 196
14*200
14* 19*
190 996
152 126
190 652
192 9r
192 691
171 336
194 4SS
14 521
193 154
132 094
147 776
190 921
199 614
147 779
190 199
192 9*7
171069
171 391
159 379
Source
Pat nttunbtt
Ohaervaioira da Hauw-
ParU (Praooe) 47a
Office of Deteoae Baaaarch aad
Engtneertag, Waahlagtoo, D. C. 72
174
Office of Naval Raaearch,
Waahlogtcn. O. C.
Office of Ordaaaoa Raaearch,
Durham, N. C.
OCOca of Sclaotlflc Raeearch
aad Development Dlv. 9
Office al Sclentlflc Raaearch
aad Oevelopmeot. Dlv. 19
Office of Technical Serrlcea,
Dapt. of Cammerca,
Waahlagian, D. C.
533
740*
93
137
477
740
713
431
23
27
93
91
116
l«6
169
199
20*
222
391
152 9**
171 115
161 539
<Rev. 1)
171 518
199 149
161'*wll'
116 303S6
152 927 .
155 149
194*79
153 996! I
Soatce
Office of Technical ScrvtcM,
Dapt. of Commerce,
Waahlagton, D.C. (coa.)
Pape FBHtanber
Ohio Sua U. , Columbua
Ohio Sua U. Reeearcb
Pouadaclon, Columbia
ens 96-421
OnSi-422
OTSSa-42S
OT5SB-42S
OTSSe-424
073 SS-426
OTS 98-439
OTSSS-430
OTS Se-431
OTSS8-432
OTS S8-433
OTS SB-423
OTS 56-434
OTSS6-439
OTS SB 437
Ohio Sua U. Reeearch
Poundatlon, Coluntbua (can. )
690
153 603
991
OTSSB-43B
637
153*75
448
OTSSS-440
701
154 196
460
OTSS6-445
154 959
155 333
472
OTS SB-435
800
933
OTSS6-449
Oklaboou Sua U. Reaearcfa
661
OTSS8-442
PouBdaQoo. Sdllwaar
35
150 873
744
OTSS8-448
141
152 247
753
UnS SB- 451
Oklahoma U. Reeearch
777
OTSSB-452
laat., Norman
20
150 574
OT5SB-454
160
171 129
804
OTSSB-453
Oklahoma U. School of
135
171 146
Medicine, Oklahoma City
266
153 337
542
171 495
Olin MadUeaon Chemiral Corp.
NewHavan. Coon.
69
171 099
10
190 859
702
171 295
27
150 755
Ordnaooe Teat Activity,
113
152 185
Yuma, Aril.
568
171 525
122
152 172
Oregon Sua Coll.,
134
149 962
Corvallla
472
153 143
140
153 252
703
146 079
213
152 186
Oregon U. Medical School,
299
152 171
Portland
14
147 744
264
152 913
17
150 564
415
150 697
Oaaka U. Oapan)
776
154 453
193 2*3
Oalo U. (Noraay)
216
152 419
418
171 40*
333
148 299
467
153 392
Oxford U.
4«e
153 657
(Gt. Brit.)
209
152 4*7
478
152 588
350
152 41*
153 430
595
154 76*
544
152 865 '
560
150 896
629
154 807
t
101
fmextkc 'ill— <■ Boaxii,
Nutoaal Umamrth Coiaell,
WuklapaB. O. C.
mctfic SamicoadacnrB, lac.,
CnhMr Clry. Caltf.
12
109
113
Sae OMflD. OklH.
Hna U. (Piwea)
•deal
hrlHT Aircraft Co. ,
Lm Aasilaa. Calif .
ntmtwom. Mooa Dlv. , ^
UMmnal Wta«ag Co. .
H. Y.
tICorp..
Pa.
f Nuu Sum U. ,
Uataanlty Paik
I U. CoU. of
raadriqnlca.
IMvwattylkit
NMirlraau Shh U. CoU. at
kfUoeral liiilwti >— .
UBHonlty Part
131
M
tfO
473
633
t37
73
S3
149
14t
6M
M7.
SS
14t
339
410
44t
547
S«9
MS
m
702
796
34
27
393
rianijt mil 1' nriladalpUa
hmaU U. School of
nuiadalftiu
U. SdMiolaf
/ MrklM(
DalBwan, QWo
NrinMal Lak.. Wrl^ Air
Pi iliipaiai Or.
An. Ite.
7«2
14
IS
139
196
416
746
114
137
299
IM
137
2*1
Ma
»i
9P9
SS7
147 100
192 999
190111
190 312
149 667
192 699
193 609
190 914
192 302
190 647
193 496
193 726
193 263
193 664
190 3U
190*43
190 469
193 091
193163
147 t*!
171 099
14*736
193 109
193 157
193 173
193 6*6
199 661
199 432
194 964
14*932
171 99*
190 99*
190 939
193*11
194 299
194 297
192 249
192 990
193 422
194 962
192 127
14*976
14* 6*9
192*34
193 166
14* 219
171 606
193*62
190 96*
190 572
192*49
130 217
153 334
155 414
190 6S1
193 3*9
192 390
192 171
130 790
192 79*
192 272
152 7*3
153 306
153 572
153 110
153*32
1S»*99
134(36
a-m. n
Ibraaaaai
{OhloSci
JFOMdM
tl Kaaaarcfc Poaid.
lOhloSCBMU. Maaarcb
(CO..)
^looporp.. miadatpiila. Pa.
llriUpa Lataa.. lac..
ilrrtayaa-oa-Hudaaa. N.Y.
^lU^ PaCToteum Co. .
i*artla*Tllle. Okla.
adoa. tec.
alcal Keaaarch Lab. ,
Space Tach. Laba., lac.,
Loa Ai^lea, Caltf. Saa
Spaoa Tadtootofy Laba. ,
tec., Loa Ai^laa. Calif.
dtyalcal >aaa<rcb Laba. ,
■oacaaU., Maaa.
Atyalcal Sciaaoa Lab. , Naa
Mexico Suu U. ,
lUalvaralcy Park
diyalcal!
Ordaaaoa Tkak-Autoaud*
Mick.
l£^
Baglaaarlag.
Coip. , Bouldar.
Cole.
Iliyatca Lab. . Wr<^ Air
D*i«ki|iaMai DiT. . Wrlflii-
tanaraoa AFB, Chk>
f tqratca Raaaarcb Lab. . U.
of llUaoU, Urtaaaa
Ackard aad Buraa. lac.,
Nenkam. Maaa.
flaa U. (luly) ^
Praafcford Araenal.
nuladalphla. Pa.
IttaburgiU., N.
Maama I
jPanali
. ProfMilaloa Lab. ,
iEayuMic ATiadca Corp. ,
Panalaplala. N. Y.
Ifaamadyna Corp. , Saaa
Aim, CaUf.
N. J.
f laadca Tachatcal BraluaUaa
Caatar, PIcatlaay Araaaal ,
Ooaar. N. J.
B. H., AaaodaHa.
lac., Loa Aafataa. CalU.
ifelyiacbBic laat. of Brookivii,
N. Y.
S37
340
731
754
798
992
153
6*3
169
303
461
5*3
21
39
377
341
406
463
61*
169
9*3
9M
MS
7*0
7*1
100
204
400
61*
116
312
347
204
390
74*
697
S04
79
1*1
316
432
633
13
*7
196
SS
327
39*
499
473
*a>
103
194*37
194*3*
154*35
171 566
199 239
199 240
199 341
199 242
190 072
192 309
130 916
14*717
149 647
171 3*1
193 447
171072
171 600
171 054
171 310
171 191
171 401
171 402
153 140
14*9*2
130 33*
154 424
193 944
161 770
199 934
193 9*1
190 923
147 942
190*97
193 19S
19S127
147 943
147*3*
152 749
152 935
171 163
152 929
155 349-
171 563
171 S67
161 947
161 9M
171 094
153 49*
153 499
ISO 416
192 139
192 249
193 6S3
1SI779
192 937
192*6*
193 3U
193 1*4
193*3*
199 147
199 296
147 757
199 63*
Source
Polytacbaic laat. at Brooklya.
N. Y. (coa.)
PDlytBdmlc Raaaarcb and
Davetopmaac Co. , lac.,
Brooklyn. N. Y.
PoaliflcU Univeraklada CatoUca.
Rio de Janeiro (Bimzil)
Portland Cemeat Aaaocladoo,
Skokie III.
nirtanxnah Na*al Shipyard,
N. H.
ftMiker Laba. , Suaford R«- '
aaarch bat., Meolo Part.
CaUf.
Poadar Matallurgjr Lab. ,
Ml. of Tack.,
N.J.
lU., N. J.
440
777
1**
196
2*7
922
sr
410
41*
419
444
963
96*
%9
638
702
763
772
Propulalon Lab. , Wrl^ Air
Davckopoiani Ceoiar, Wrt^-
Paneraon AFB, Cblo 2*7
992
796
7*5
Paycko-AcouBClc Uab.,
Harvard U., Obnbridgt.
Maaa. 621
Paychotaglcal Lab., U. of
Southern California,
Loa Aofclaa 6
264
9tD
6*6
Paychologlcal Laba., Cai
Inat. of Tad||k Plnabur^ Pa.
Paychoiogical Raaaarcb Aa-
Bocueaa. Inc., ArllafHa, Va.
Paychophyalcal Raaaarcb IMt,
Mourn Holycka Coll. , Sou*
Hadlay. Maaa.
Paychooietrlc Lab., U. of
North CaroUaa, Oapal Hill
PiAlic Health Serrtca,
Waahiiwwa. D. C.
Puerto Rico U. Coll. of
Agriculture tod Heche ale
Arte. Mayafuez
Purdue Reeearcfa Poundatloa.
Lafayette, Ind.
11
137
1S7
196
120
1**
937
PS Numbsr
604
153 699
606
130 327 ,
ISO 636
607
153 1*3
153*37
153*3*
621
14*349
702
ia473 .
772
153*4*
7*9
14*757
796
171 569 .
7S1
154 996 >
194 997
732
199 299
576
193 107 ).
336
192 730
149
149 096
193 316
154 537 '
152 549
14*673
152 739
152 629
152*31
149 649
149 677
152 73*
149 6a
152*73
150 07S
147 534
149 354
149 355
149 155
154 417
150 469
14*747
148 74*
149 214
154 3*2
154 3*3
155 0*0
153 629
154 969
153 0*3
155 257
147 765
190 4*9
14*004
14*006
14*007
14*009
152 HI
14* 292
152 123
130 **7
103
150 892
6*6
154 459
154 462
22
161 371-7
161 371*
rs
161 371-9
404
161 371-10
692
121 784-R
161 371-11
693
161 371-12
152 471
ISO 874
152 543
153*59
y}
Sourca
Purdue Reaaarch Pouadedoa,
Latayetie, Ind. (coa.)
Purdue U., Lafayette, lad.
Pa^ PB NuDibay
53*
323
153 854
132 761
193 763
Source
Purdue U. , LafayetM,
lad. (cm.)
796
IV NunfeDBT
193 369
14*016
Purdue U. Dhr. of Ei«lneerli«
Sdaacae, Lefayette. Ind. 493
Pat PBWiMbar
193 904
t *
"}
Quaiman. lac.,
Wtlhr^ford, Conn.
QMrtermaater Field
Evaluation Afeocy,
• Port Lae. Va.
97
205
336
592
ra Number
152 648
192*49
149 674
149 6*8
193 491
Source
Quertermaater Reeeerch and
Engineering Center, Natick,
Htfi n Number
Source
Maaa.
9
14(319
31
190 765
192 070
32
190 766
73
190 94*
190 962
171062
1710*9
Paae PB Number
Quartermaaier Reaearch and
Engineering Center,
Natick.
Maea. (coa.) .
103
190 74*
1*1
171 193
465
132 66*
555
153 427
993
153 62*
Quaaa'a U. , Belfaat
(Northera Ireland)
279
153 0*9
V
^
^1
I
m
Sourc*
Page mtiMobtT
Mdianan Btfecu IniomiMkia
Center, Battalia Memorial
Inai , Columbua. Ohio 206
Mdutioa Lab. , Joluia Hopiaaa
U., MUaon. kM. 7M
7M
RadUtion Reaaerck Cotp. ,
Weat Palm Baadk. PU. tt7
Radio Corp. at Aiaarica.
Camden. N. J. 54
Radio Corp. of Anertca.
HuTtaon. N. J. 54
576
Radio Corp. ol Amaiica.
Lataarar. Pa. 54
IM
Radio Corp. of Amaiica,
PnacatoB, N. ]. 577
Radio Corp. of America,
Saaamlla, N. j. 732
Calif.
y
153 258
154 961
154 960
154 753
171 136
152 753
154 544
149 707
152 S«0
153 603
154 479
hMC. of 'ftch. . OvwM Valley
534
147 323
147 324
SS5
147 322
147 325
147 326
147 327
147 32S
147 339
rtm», Aaatia
23
153 353
404
153 301
6M
155 575
<M
154 594
«98
155 576
RaiBO-WooldiidaB Olr. .
Caufi Park. Calif.
790
154 460
Ramo-Waoidr«d|i Corp. .
LoaA^IBtea, Calif.
216
153 517
Ray-O-VacCo. , Madlaoa. Wla
54
171 102
577
153 935
Ray*H»Co.. BurUi«iaa.
ti^».
577
153 230
RayMMoaCo.. Newton, Maaa.
170
149 716
RaydMoaCo.. Wtltham. Maaa.
54
150 446
169
14(276
309
149 629
149 630
346
152 628
4S3
ISO 699
•
153 240
«80
15S23t
7W
154 077
RCA Detmae Electronic
Producu. Camden. N. ].
55
171 125
619
171 493
RCA Service Co. . Camden. N.J
577
154 516
154*44
7S2
155 151
155 152
RCA Semoe Co. . Cherry Hill.
N.J.
»70
171 ISO
171 131
171 132
RaacUoa Mocora DIt. . Thlalcol
C^mlral Corp. , OHvllle.N.J.lW
152 257
Read Raaaarcfc. lac..
WaaMi^na. D. C
<09
154 431
REP M%. Corp. .
MlMOia, N. Y.
7«
171 COS
Source
Rbnectoae Elactroalca. lac.
^lamlorct, Coas.
Blotnn Arma Co. , lac. ,
Com.
Blagton Read Unlvae DIv.
Brry Rand Corp. .
illadelphla, Pa.
ilaer Poiytecknlc laet.
"roy, N. Y.
Page PR Ntanber
H epubllc ATlatloa Corp.
Pannlnffdale, N. Y.
rdi Center (or Cro«4>
Dynamlca, U. of Mich.,
Ana Arbor
rck Ctaemlcala. lac.,
Burbai^ Calif.
436
174
30t
309
79
S2
122
123
699
S9
90
192
196
197
322
410
4S7
553
ta
T7S
m
309
10
94
Rbaearch laat. , Temple (J. ,
Phi lade Iphli. Pa. 635
M saaarch Lab. at Blectraalca,
Maaa. Insi. of Tech. ,
Cambrtdfe 55
140
190
544
S7I
733
7t7
Rkaearch Lab. of Haai
Traaater la Electroolca,
Maaa. Inac. at Tech.,
Cambrtdfe 635
11 saearch Lab. of Riyalcal
Blectronica, TirfU U. .
MedtOrd. Maaa. 170
sarch Laba. for ite
Eoflaeerti^ Scleacaa. U. at
VlrfliUa, Charlotteeinlle 410
773
RlilneUnder Paper Co.. Wla. 176
I IAS. Baltimore. Md. 450
I Ice U. , Houaioa, Tax.
J
too
777
114
lU
104
171 419
152 259
152 839
152 840
152 049
150 767
190 811
ISO 119
153 160
ISO 871
150 952
148 674
152 480
152 250
153 382
147 045
153 315
153 2M
153 SOI
171 535
1S9 262
149 210
150 321
171 337
150 638
171 085
171 086
154 842
148 972
153 999
149 6S2
150 607
154 190
ISO 913
154 198
154 199
153 906
171
152 803
153 356
154 158
152 793
153 412
153 414
159 711
159 413
IS9 710
154 536
ISO 749
152 490
SoTce
Richmond Reaearch Lab. ,
Scairfler Chemical Co. . CaUf.
Rohert A. Tafi Sanitary Eagl-
naerlaf Cenur, Ctnclnnatl.
Ohio
Robertahaw- Pulton Controla
Co., Anaheim. CaUf.
Rocbealer U. , N. Y.
Page PR Number
Souroa
P>ie WNumher
Source
546
152 S7S
Rocheater U. School of
Medicine and Denciatry,
Rock lalaad Araenal Lab.
176
S84
275
zn
396
399
693
702
N.Y. 143
III. 75
179
201
314
317
Rocfcetdyae, Caaoga ^rk.
Calif.
Rome Air DevelopmeM Center,
Crtmaa APR, N. Y.
333
»4
756
65
312
419
580
584
736
740
741
S3
143
153
170
309
304
432
619
630
637
106
142
Roaemount Aeronautical Laba.,
U. of Mlnneeou. Minoeapotla 197
Rowland and Co. ,
Haddoofteld. N. J. 299
Royal Holloway Coil. , U. of
LaBdan(Gt. Brtt.) 275
348
Royal Hoapltal for Sick Children,
Edinburgh (Scot. ) 690
Royal Inat. of Tech. (Sweden) 28
89
Z7*
I U. duly)
Royal Mlllury Coil.
Rutgera Sute U. , N
Brunawtck. N. J.
of Canada 475
iw
10
93
265
764
RMgara State U. School of
Chemlatry, New RrunewIck,
N.J.
703
152 064
153 617-
153 617
149 664
153 158
152 881
147 778
153 903
154 374
148 277
152 294
152 590
161 969
161 897
171 047
150 961
171 042
171 043
171 041
171 111
155 082
150 861
171 309
152 319
153 613
153 612
153 870
154 290-1
154 290-2
ISO 973
148 277
152 548
152 547
152 405
161 894-1
153 205
171 420
153 858
153 264
153 871
150 413
152 534
171 142
149 211
152 767
152 789
153 720
150 335
ISO 331
152 772
152 773
153 166
148 2««
152 680
152 889
148 561
148 400
m
St. LouU U. , Mo.
St. Loula U. School of
Medicine. Mo.
St. Liice'iConraleacent
Hoeptial. Greenwich. Conn.
St. Lufee'a Hoapiul.
New York
Saaliary Englaaarli^ Reeearch
Ub., U. of CaUfbrala.
iaikeley
Saaik Barbara Dtv., Curtlaa-
WrlgbtCorp., Calif.
Sarah Mellon Scalte Radiation
Lab.. U. of Ptttaburah. Pa.
Saakatchewao U. (C:aaada)
School of Aviation Medicine.
Brooke APR. Tm.
SclMc* aid Tftcfa. DIv. , S
Library of Coograaa,
Waahtngton. D. C.
Science Reeearch AaeocUtea,
Inc., C3ilcago. 111.
Scientific Radio Producta, Inc.,
Love land, Colo.
Scrlppa Inatltutloo of Oceanog-
raphy, U. of CalltomU.
Sea Olego
Start -Coeoda, Cllchy (France)
ShafHeldU. (Ct. Brit.)
Shall Development Co. ,
Emeryville, Calif.
Shon Broa. and Harland. Ud.
(Ci. Brit.)
SladelS. p. A., (Rome (Italy)
145
268
17
17
32
711
101
468
618
132
133
135
140
141
365
368
273
9M
543
543
689
690
693
694
272
620
994
170
33
457
278
72
171
330
622
Sklatran Electrooice and
Televlalon Corp. , New York 452
Small Croupe Reeearch Center.
Waahlnron U. , St. Loula. Mo. 10
Smith Coll. , Nordiampton,
Saell, Poeter D. , Inc. ,
New York
Solar Aircraft Co. ,
San Diego, Calif.
Sonotooe Corp. , Elmetord.
N. Y.
Soudtem Medwdlat U. ,
Dallaa, Tex.
Southern Reeearch Inat. ,
Birmingham, Ala.
SoMbweat Reeearch inat. ,
San Antonio, Tkx.
Space Sclencee Lab. , General
ElectrtcCo.. Philadelphia. r».
540
686
171
55
304
633
275
197
753
5
28
87
108
192
152 085
Space Sclencee Lab. . General
ElectrtcCo.. nuladelphla.
152 617
Pa. (con.)
160
178
153 2S7
152 622
150 471
312
152 999
a
440
153 492
150 471
609
773
153 835
153 692
159 693
152 645
804
154 510
. Space Tecfaooiogy Laba.
Inc..
153 859
Loa Angelaa, CaUf.
65
98
150 882
150 776
150 516
P
116
152 113
150 700
'
118
ISO 890
154 817
216
152 034
152 281
346
152 901
152 282
439
152 829
152 284
443
473
152 890
154 404
149 246
636
153 464
150 207
736
171 247
152 215
171248
152 263
171 349
152 433
171 290
152 765
797
154 232
152 216
800
154 154
152 764
154 971
152 460
154 S72
152 630
147 778
153 302
153 402
154 426
153 983
154 819
159 486
154 263
154 4Z7
155 574
154 592
1SSS76
154 264
171 029
171 577
148 771
149 71S
147 175
153 378
149 658
149 659
152 755
149 660
152 963
153 807
152 928
150 851
150 852
147 767
147 748
149 904
159 150
150 876
152 527
150 449
149 693
171 485
171 300
171 417
171 152
153 703
150 801
150 170
150 802
190 949
192 464
Spectroecopy Lab. , Panneyl-
vanla Stale (J. , Unlveralty
hrk 339
Speech Reeearch Lab. , U. of
Michigan. Ann Arbor 104
466
Sperling Labe., ArUngton. Va. 143
541
Sparry Cyroecope Co. ,
Greet Neck. N. Y. . 116
Sperry Microwave Electronlca
Co., Cleerwater, Pla.
Sperry nioenlx Co. , Arti.
Springfield Armory, Maaa.
Standard Preaaed Steel Co.
Jenklntown, Pa.
Stanford Electronlca Laba.
Stanford U., CaUf.
419
578
160
144
208
445
712
55
Stanford Reeearch Inat.
Menlo Park. CaUf.
56
107
114
133
156
433
433
578
602
622
623
733
734
767
800
806
35
56
151
156
181
213
221
904
411
452
556
578
579
591
105
152 864
150 494
153 170
148 294
152 902
150 639
150 991
154 398
154 809
153 390
152 393
152 394
153 223
155 OM
ISO 492
ISO 493
152 183
150 823
150 820
150 823
150 525
152 391
149 069
153 169
147 243
147 244
150 715
150 716
148 411
149 333
153 824
150 717
148 332
149 235
148 998
149 236
155 260
153 785
154 970
150 327
150 627
152 152
171 103
148 255
152 614
149 711
148 286
153 008
148 671
149 064
152 670
153 314
153 306
153 601
153 203
153 097
154 846
Staoiord Reeearch inat. ,
Menlo Park. CaUf. (one.)
Stanford U. , CaUf.
Stanford U. Graduate Sckooi of
BuBlaeaa, CaUf.
Stanford U. School n( Medlclaa,
CaUf.
Stanley Thoopeon Labe. ,
ColumfaU U. , New York
Stelma, Inc., Stamfbrd, Coon.
Stevene Inec. of Tech. ,
Hoboken. N, J.
708
767
789
U
108
149
475
565
762
797
67
Stockholm U. (Sweden)
Stoddan Aircraft Radio Coj,
Inc.. HoUywood, CaUf.
543
689
199
786
171
56
205
633
365
797
433
734
Structural Mechanlca Reeearch
Lab., U. ofTexaa, Auatln 68
Strultaera-Duna. Inc..
Pitman. N. J. 309
Sundetrand T\irbo DIv. ,
Sundatrand Machine Tool Co. ,
Pacolma. CaUf. 63
66
312
313'
Sylv«nla Electric Producta. inc. .
Seneca Palla, N. Y. 304
Sylvanla Reeeerch Labe.,
Beyalde. N. Y. 94
Synthetic Mica Co. . Caklwell.
N. J. 630
798
Syracoee U. , N. Y.
Syracuac U.
N. Y.
Reeearch Inat. ,
Syatema Corp. of America.
Loa Angelea, CaUf.
Syaieme DevelO|iaient, Inc. ,
Blngbnmton. N.Y.
Syeteme Development Corp. ,
Dnyton. Ohio
Syeteme Dynamic Analyals DIv.
Wright Air Development DIv. ,
Wrlght-Patteraon APE, Ohio
Syatema Reaearch Pie Id Lab. ,
Jo^ Hopklna U. ,
SystBOM
laglewood. CaUf:
79
188
322
333
490
478
541
40
904
459
985
735
637
175
171
563
154 556
148 231
154 078
ISO 853
150 378
152 488
154 294
147 546
147 847
150 059
190 ill
190*12
148 931
155 297
152 147
190 864
152 513
149 713
149 714
153 934
152 535
153 721
150 712
154 412-1
154 412-2
ISO 631
149 704
150 834
148 264
150 835
152 896-1
152 856-2
152 896-3
149 712
190 2M)
154 515
155 154
155 155
155 156
155 157
152 292
149 717
152 736
152 797
171 335
153 958
153 999
153 360
153 122
171 031
152 986
171 996
17149*
171599
150 903
154752
171 180
153 006
171 551
Soitroe
TKftoical Op*r>claa. lac.,
ArllagioR, Mas*.
Tadwical R«*earck Cro<^
Somemlle, Maaa.
TKkaical Haamrtk Otxn^
SyoMM. N. Y.
Tadniacbe I
Graz (Austrii)
TWtelacte HodMCbule.
Ku-tanihe (Waat Gcrmaay)
(W«M Owaaay)
(W— t Otiiiiy)
(AuKrta)
Ifc-WThnnt. Delft
QlMtarUadB)
I A. iHiM. ColL.
CoHaji Siatlaa
462
305
120
333
336
464
593
2««
697
197
347
«74
546
379
697
141
32S
1»
579
62
717
137
263
26S
33
131
413
SOMTO
[■Bd
hramouat.
out.
Ukraaoalcs Lab., Mlcfelcui
ScnaU.. Bat I ■— tag
Ultraaaanca Haaaarek Lab..
Waaian lliaai >a V. ,
Cla»ala«rt. Ohio
UUoa Svttck $mt Sl^al DIt. .
Weatinftiouaa Air Braka Co. ,
Swtaawke. H.
Uoitsd Aircraft Oecy..
Eaat Hartford. Coma.
UalTeraal Match Corp. ,
S(. Louia. Mo.
Uuvcraic; CoU.. Cock
<Bli«> \
UmacrttyCoU.. D«Mia
Otrto)
Ualvaraal-Cyclopa Scaal Corp. ,
■mpiilla. h.
UMvaraity Hoapliala. lova
Qqp, Iowa
UMaantqr of SoMkarii CalUor-
■ia, Loa ^a^itaa
366
792
29
ft
134 407
152 776
152 051
171 341
152 777
171 997
133 339
133 087
153 717
152 492
153 626
133 466
152 M*
133 276
154 137
1S»532
149 640
150 3M
153 228
130 925
134 161
132 »1
158 n
153 782
150 467
152 569
150 691
171 499
133 120
132 132
56
132 796
364
134 304
175
171 1S7
188
149 073
469
153 094
613
133 392
IS
1S2 118
22
34
133
322
348
ISO 362
130 319
152 164
152 165
148 066
130 330
SoMTca
Huaa A. andM. Baaaarrti
Pouadatlaa. Colka(B StaAoa
I laacrunaaia, lac. ,
Dallaa
"^naa Nuclaar Corp. , Aueda
I U.. Auada
1 naa U. Madlcal Branch.
Oahaawa
1 BOlla Baaaarcfc laat. ,
PrlacacoB. N. ].
1 baoradcal Chemistry Lab. ,
U. ofWlscaaslo. Madlaoa
"perai Adraacad Raaearch,
N. Y.
•^iinnibjali al Fropertlee
I Caawr. Purdue U.
I Corp.,
Md.
]ata I . . aad Co. .
D. C.
Ramo Wooldrldve.
l^lewood. CalU.
BaglBaerlaf Co. ,
a C.
707
360
99
28
620
691
348
149
554
79
479
316
441
434
183
184
216
-iDrlaoU. (Italy)
'fraaa Tkch. lac.,
iRocfcTllIe. Md. 305
'franaportatlaa Center. Nonh-
atara U. . BTanacoo. lU. 588
Sourca
(^veralty d Southern Calt-
ionla. Loa Aofelea (coa. )
l|nl*erslty at SoudMm Call-
lomla. Bocinaerlaf CeBCer,
Loa Aa^elaa
dalTeralty of Soudara CaU-
toraU. School of Madtclne,
Loa AnfBlaa
llppar Air Lab.. U. of
Cotondo, Boulder
106
154 528
153 933
171 120
152 097
147 848
146 415
147 170
161 4083-1
153 114
150 466
171 478
153 620
171 41S
153 235
171 169
171 170
171 171
171 172
171 173
171 174
171 173
171 176
152 481
153 226
153 605
334
153 667
171 530
703
148 075
148 076
148 077
117
130 734
ISO 988
lao
150 735
IP
153 551
ifc
152 550
210
152 549
327
152 557
434
153 446
607
153 42r
IS
150 219
150 563
17
150 567
3M
171 304
171 343
273
153 348
399
153 511
33
150 733
4»4
133 442
Sourca -i
Travalara Uli laauraaca Co.
Hartford. Coaa.
Trlalty CoU. . Dublla (Eire)
Ti«bU.. Madford. Maas.
Titfta U. Sduol of MadlClna.
Boaton, Maaa.
fmtft UNiBPbar
TulaoaU.. New Orleana. u;
Tuog-Sol Electric lac. ,
Bknoflald. N. ].
31
152 OSO
556
153 5S0
270
152 477
199
152 853
17
147 743
140
132 SSI
141
132 331
132 832
268
132 618
400
133 536
153 327
153 528
153 529
153 530
401
133 SSI
133 332
133 533
•<»,
133 334
V-1
133 333
153 536
153 337
153 338
133 S99
402
153 363
133 364
153 523
, :
153 341
133 548
268
153 575
107
ISO 430
Upper Air Reaaarch Lab. , U.
of Utah. Salt Lake Qty
Uppaala U. (Swadaa)
Bijl n Number
UHhU., Sate Lake City
284
1S2 623
98
150 351
114
171 121 ,
132
152 204-
133
132 209
152 210
132 211
lA
132 205
214
152 452
152 453
132 454
152 455
464
ISO 694
472
153 310
11
ISO 475
70
171074
175
149 071
152 380
152 381
630
171 049
t 1-
Sourca Pim
Van Camp Laba. , Terminal
talaad. Calif. 399
Varlan Aaaoclataa, ■ i
Palo Alto. Calif. I 36
Vehicle Reaaarch Corp. ,
Paaadena, CaUf. 419
Vertol Aircraft Corp. ,
Morton. P^ 564
I
Sourca
Waahburo Obeervatory,
Madison. Wis.
Waahiogtoa Sute U. . Pullman
Waahin(tan U. . St. Loula, Mo.
Waahlnftoo U. . St. UwU,
School of Medicine
Waahl^umU., Saania
Mo.
WaahlBgloo U. Saania. Coll.
al Engl nee ring
Washli^lon U., Seattle. CNv.
al CounaeUag and Teatiog
Sarrlcee
Waahii^ion U.
ct Medicine
Seattle. School
WaiartovB Arsenal Laba.
Source
Yale U. . New HavMi. Com.
YciiuM ObM mtory ,
* WUlUma Bay, WU.
I
re Nunibsr
153 511
171 069
130 742
153 740
153 879-
153 879-
Souroe
Pegs n Number
Veterans Administration
Hoaplul, Denver, Colo. 20
Veteraaa Administration
HoaptiaL Loi« Beach. Calif. 271
Vldya.lnc.. Palo Alto, CaUf. 608
Vienna Inet. at Tech. (Auetna)160
yiaoM U. (AoatrU) 204
462
708
.149 246
153 330
152 582
152 437
152 482
153 309
154 155
EME
FB Number
153 136
Source
Watertown Arsenal Laba.,
f*r
m Number
468
,•,«
540
153 403
Maaa. (con.)
11
152 HI
330
171 044
IBS
152 996
445
171 186
323
152 747
153 263
331
149 736
741
155 059
332
149 737
155 061
333
152 911
155 062
616
149 087
742
155 058
687
149 324
757
155 060
153 572
11
152 101
777
171 384
687
154 593
780
153 558
691
149 336
Waiervllet AraeiHl, N. Y.
462
161 896
29
1SP461
742
154 207
33
148 267
749
171 112
150 497
777
171 564
138
147 642
152 166
Wayne SuieU., Detroit, Mich. 80
150 476
150 477
153
152 168
152 148
i
189
150 496
148 719
152 149
'<i ■■
323
152 436
188
152 167
346
152 694
283
148 426
351
149 685
314
152 446
451
ISO 723
402
153 366
600
153 177
430
153 683
623
153 123
451
153 684
153 757
600
153 132
703
1 48 406
618
147 306
704
148 407
698
154 118
764
154 456
704
148 233
793
171 580
149 096
57
150 457
149 097
351
434
152 961
153 353
Weedier Bureau, Waahington.
. D. C.
707
153 713
Weather Foracaatlng Raaearch
189
147 643
Caoiar, U. at Chicago, 111.
281
153 046
148 608
556
153 443
191
148 732
Wcizmann Inst, at Science
148 733
Oarael)
217
132 483
148 734
152 493
148 735
704
149 775
224
148 723
Wanaer-Crea Aeronautical
323
148 609
1 Raaaerch Lab. , Lexington,
541
148 610
Ky.
Waal VlrglnU U. ,
263
132 744
17
150 230
Morgsntrwn
704
153 662
269
153 344
Weatem Development Labe.,
270
153 327
nulco Corp.,
*
399
153 335
Pak) Alto. CaUf.
Western Electric Co.,
171
153 236
62
161 800
Wloatoo Salem, N. C.
171
153 380
84
149 295
Western Ontario U.
91
150 917
(Canada)
436
153 636
161 989
624
133 637
309
152 988
Western Reserve U. ,
133 062
CleveUad, Ohio
117
147 908
H^i W Number
Source
7
152 123
104
152 134
547
147^
601
153 671
•7>
239
1S|!S278
Zator Co., Cambridge, Maaa. BOB 133 068
107
Sourca
Virginia Agricultural Experi-
ment Statioa, SlaCkaburgh
Virginia U. , Cbarlooaavllle
VlrglnU U. School of Medicine,
Charloneaville
Vitro Eoglneerlng Co. .
Waahln^on, D.C. 741
Vougbt Aacronautlca DIv.,
Chance Vougbt Aircraft, Inc. ,
Dallaa, Tex. 419
Page n Number
600
133 7U
764
148 533
98
130 406
686
147 S30
703
150 533
22
150 575
153 890
153 716
Source
Page
PB Number
Weatingbouae Electric Corp. ,
Baltimore, Md.
171
152 219
172
148 283
303
152 411
434
130 710-1
ISO 710-2
^*»\M^ttomm Electric Corp. ,
Bloomfleld. N. J.
613
154 542
Weatingbouae Electric Corp. ,
Eaat Plttaburgh. P>.
214
148 981
Weatingbouae Electric Corp. ,
Youngwood, Pa.
735
155 321
Weatlnghouac Reaaarch Laba.
,
Plttaburgh, Pa.
172
152 348
172
152 348
331
152 880
434
171 364
447
171991
613
ISO 303
Waatoo Inatnanaata,
Newart. N. J.
Wbitialcer Controla,
Los Angeles, Calif.
Willow Run Laba., U. of
Michigan. Ann Arbor
I
Wllaon, NutuU. Ralmood
Bsgl Basra, lac. .
WlacoMla U. ,
WlecOMla U. School of
Medicine, Madlaoa
Wooda Hole Ocaanographlc
Inatltutlan,
Wright Inatrumente lac. ,
VeauL N. Y.
Wyandotte Chemlcala Corp.
Mich.
Wyman -Gordon Co.
Grafton, Maaa.
735
712
35
222
269
305
413
625
787
750
122
208
Z74
999
413
435
431
556
579
15
33
34
80
90
281
413
414
5S7
74
445
155 384
153 611
150 421
149 673
132 605
152 536
152 682
153 436
155 382
153 713
152 110
149 909
152 631
153 347
153 607
153 242
150 061
153 608
153 243
133 244
1S0 21S
148 12S
130 529
150 514
ISO 842
152 870
147 311
153 134
133 762
154 762
most
171 S7S
*0.a. OOVUIMMKMT PBDHTINO OmCB : 1942 O -4UMa
. S. (.oierniuoiil
mm.
lEPORTS
T
n this issue:
Cathode Rav Storage Tubes U'B 171 127)
Electron Tube Emission Stability
(PB 171 117)
Faperlined Magnesium Dry Cells and Bat-
teries (PB 171 192)
Soil Stabilization: Investigations of a
Chemically Modified Oment as a Sta-
bilizing Mater M- (i*fl Si W8)
VHFand UHK Power Generators for KF
Instrumentation (I'B 161 S78)
Continuous Filament Ceramir Fibers
(PB 171 061)
Design Manual for Glass Reinforce*! Plas-
tic* in Naval Applications (PB 171 0%)
Flake-Glass Laminates (PB 161 947)
! Ultrasonic and Ceramic (boatings
(PB 171 057)
An Introduction to Digital Computing
(PB 171 100)
A Miniature Wafer-Style Pressure Trans-
ducer (PB 171 101)
Com/tlfif linl of ftriHIfd rr/mrtx
txflins tin ftani' iii
January 13, 1961
Vol. 35, No. 1
A monthly listing of
Government research reports
available to indust^>^e^^ . ^
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U. S. DCPARTMCNT OF COMMEKC.
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CONTENTS
'-'"s
3182
51- »'
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PRINTED REPORTS AVAILABLE FROM OTS ANNOUNCED IN THIS ISSUE .
JUIJOGRAPHY ...••••••••••••••••aa»»«»««»a.«»»««»«»»«»««««»«
plftnt Cultiv*tloii o ••%•••••••••••••• • ••••••••••••••••••••••••••••••• •••••••••••••• 1
FRONOMY t^ •••••• «•••••• 2
••••••••••••••••••••••••••••• \
••••••••••••••••••••••••••••• \
>•••••<
•••••••••••••••••••••
• ••••••••a«**«*«o««**«a»«
ASTRONOMY
Astrophysics ..••.•••••••••••••••••••••«••••••••••••
lEHAVIORAL SCIENCES .
Human Engineering
Personnel and Training . .
Psychology ||i.j
BIOLOGICAL SCIENCES .-. . .
Anatomy and Physiology .
Biochemistry .«.
Pathology
Ptermacology and Toxicology
••••••••••••••i
»•••••••••••••<
•••••••••••••••••••I
24
29
29
32
32
34
35
35
39
40
2
5
5
6
7
II
12
16
18
^ 20
Radioblology ,,,,...,.....«..«•.•.••••••••••••••••••••«••••••••••••••••••••••••••••••••••••• •'
22ool0gy .....•••••• • ...•...«...•••••• •••••••••••••••••••••• a2
CHEMBTRY. *H***i * * * '** S
taorganic Chemistry . « '. ^
Organic Chemistry » t •^ ^
Physical Chemistry i .«
EARTH SCIENCES x
Climatology and Meteorology •
Geology • •
Oceanography « • • • •
Physics (rf the Atmosphere ■f —
ENGINEERING i "^
Aeronautical Engineering ............*
Chemical Engineering , , • • •
QvU Engineering - *S^:S^"
Electrical and Electronic Engineering **
Ordnance, Missiles, and Satellite Vehicles 57
Ship Building {J
POOD, HANDLING, AND PACKAGING EQUIPMENT • » 63
MACHINERY, FABRICATION, AND ACCESSORY EQUIPMBNT i; W
Engines and Propulsion Systems • 63
Manufacturing Equipment and Processes ,.'......•••>•••*.•••••••••••••••••••••••••••••• 00
Transport, Traction and Hoist Facilities ,,.,...«........•.....••••••••••••••••••••••••••••••• •«
MATERIALS • ,....,,,,.,...,..«....«.......«•••..••••••••••••••••••••••••.••• ••
Ocramics and Refractories ,,.,.',.,.........••...•».•••••••••••••••••••••••••••••••••• W
Fuels, Lubricants, and Hydraulic Fluids 70
Leathe r and Textiles » • n • « . 78
Paints and Finishes , 74
Plastics ..» '*
Rubber and Elastomers " 75
MATHEMATICS 2
Computing Devices • ^
MECHANICS 2
Aerodynamics and Pnetunatics * ^
Hydrodynamics, Hydraulics, and Hydrostatics .........••••• •>•.%• W
Statics, Kinematlts, and tCinetlcs ..•.•.••.•*•........... ^
METALLURGY JJ
F errous Metals * '^
Ught Metals JJ
Nooferrous (except light) Metals ^
Stniaural Metallurgy and Corrosion - • • ^
NUCLEAR PHYSICS- AND NUCLEAR CHEMBTRY • JJ
Cosmic Rays C# ^
Elementary Particles ...,.,,,,,.,.,...............•.......................•....».»•••••••••• T'
Instruments and Installations ...........••....*•............•. ^f
Nuclear Engineering and Power ..^^ «...- "
I
Nuclear Reactions , , ^ -jjjR
RadloactJivity , **"■•
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT .'.*.!!.*!.*!!!!!.* *"" 103
PHYSICS ..J '. .*.*!!!.*.*.'.*!!!.'!.*.'.' m
Acoustica .^ !!!!!!!!!!!!!!!!!!!!!!!!*! 104
E lectr Iclty and Magnetiam !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!* 104
Electronics !•»!!!!!!!!!!!!!!!!!! los
Molecular Physics and Spearoscopy '. !!!!!!..!!!!!!!! 107'
Optics »..*!!!!!!!!!!!!!!!* loi
Solid State Physics 109
Theoretioai Physics f. .'!!!!!!!*!!!!!!!!!!!!!!!!!!*!!!.* iw
ThermodyHam ics !!!!!!*!!!!!!!!!! ♦•••• ^^^
Wave Propagation !!!!!! * * ♦ • • • •
RESEARCH METHODS, TECHNIQUES AND EQUIPMENT ....'.'.'.*.'!!.'!!.*.*!.*!!!!.'. .*!.*!.**!!.*!!.*|!.*!! 121
Communication Theory ....* *" ^22
soa A L sa ENCEs r !!!!!!!!!!!!!!!!"""* * ''[ 122
IX)Cumentation
123
MISCELLANEOUS . . , ....'.'.'. 123
ATOflC ENERGY CC»4MISSI0N REPORTS
biology and medicine
CHEMISTRV
General
PHYSICS AND MATHEMATICS
PROGRESS REPORTS
RAtXOACTIVE WASTE
REACTORS;
General
o
11
125
12S
126
127
Radiation and Radlochemistry ^ ^ ^
Separation Processes for Plutonium and Uranium '..'.'.'. " * * " 177
CONTROLLED THERMONUCLEAR PROCESSES * ,5,
CRmCAUTY STUDIES " * *
ENGINEERING AND EQUIPMENT !.!!.'!.*.!!!!*].* * * ' *
GE(XOGY AND MINE RALOGY
HEALTH AND SAFETY 4
INSTRUMENTS !!..*.'!!!!!!
METALLURGY AND CERAMICS !.*.*!!."!!! *
NUCLEAR EXPLOSIONS - PEACEFUL APPLICATIONS ..,.!.".'.'.'.' J^
PA RTICLE ACCELE RATORS AND HIGH-VOLTAGE MACHINES '.'''' i m
127
127
127
127
ir
121
128
128
RADIATION EFFECTS ON MATEwiois ...'.*!!!!!!!.*!.'.'.'.*!!! J2
129
129
129
129
Power
STABLE ISOTOPE SEPARATION .'!!.*!.'."!.*.*.*.' "*' )2
TECHNOLOCy fr?
Feed Mat eti «1« .'.*.'.".* * ' " ! S
SOURCE INDEX , *
SUBJECT INDQX *"*: * ' , .J
NUMBE R iND^ !.*.".'!!!.*.'!!!.'!!!!!!!!!!.'! , ' 1 J
Jj
Printed Reports Available From OTS Announced in This Issue
BBHAVIORAL SCIENCBS
Method of estimating surface color discriminabllity for coding training
e<pilpnient and predicting label legibiUty. May 60. 12p.
(PB 171 053) SOcents 5
Survey at die literature oo predictloo of Air Force personnel require-
ments. JulybO. 388p. (PB 171 075) $5.00 » 6
BPLIOGRAPHY
Alkali meuls: litliium. sodium, potassium, rubidium, sod cesium.
July 60. 37p. (OTSSB-421) 10 cents 23
ABcaline earth elemenu (barium, calcium, and strontium). July 60.
21p. (OTS SB-422) 10 cents- 25
Liquid metals. Aug 60. lOp. (OTS SB-424) 10 cents 91
Magnetohydrodynamics. Aug 60. 8p. (OTS SB-426) 10 cents ill6
Molten and fused salts. Aug 60. 9p. (OTS SB -425) 10 cents i... - 27
Protective construction: A report bibliography. Nov 60. 85p.
(PB 171 106) $2. 25 , .' 1
Transducers. Aug 60. 7p. (OTS SB-428) 10 cents 53
BPLOGICAL SCIENCES ' . ,
Biomedical effects of ejqxseure to electromagnetic radiation. Part I:
Ultraviolet. May 60. 187p. (PB 171 072) 53.00 21
New chronic polarographic implant unit for measurement of cerebral
oxygen availabiUty. May 60. 12p. (PB 171 073) 50 cents 19
Radiological health data. Volume I, No. 7. Oct 60. 68p.
(PB 161 371-7) 51.00, 59. 00/yr 22
Radiological health data. Volume I. No. 8. Nov 60. 55p.
(PB 161 371-8) 59. 00/year 22
CHEMISTRY ''
Alkali meuls: lithium, sodium, poussium, rubidium, and cesium.
July 60. 37p. (OTSSB-421) 10 cents - 23
Alkaline earth elements (barium, calcium, and strontium). July 60.
21p. (OTS SB-422) 10 cents 23
Molten 4nd fused salts. Aug 60. 9p. (OTS ^-425) 10 cents 27
Reactions re Uted to oxidation. Sep 60. 34p. (PB 171 121) 51.00 23
Researcties on hydrogeu overvoluge on meulUc single crystals: Tin.
July 60. 19p. (PB 171 079) 50 cents 25
Some experiments on the deposition of gases at 4. 2*^. Oct 60. S^.
(PB 161 574) 51. 00 26
Survey of tiie Uteratur' on tihe use of organometallic compounds in tlie
preparation of ultra pure metals. July 60. 42p. (PB 171 097) 51.25 23
Theoretical study of hl^h tenqwrature compounds. Dec 59. 27p.
(PB 171 103) 75 cents 28
Vapor pressures of organic compounds in the range below one milli-
meter of mercury. Oct 60. 26p. (PB 161 571) 75 cents 23
EARTH SCIENCES 1 1 ' |
Geodkic distance and azimuth computations for lines under 500 miles.
Sep60. 84p. (PB 171 067) 52.25 **
\ 9
ENGINEERING
Abrasion resistance of high -temperature coaxial cable Jacket maoerials.
Apr 60. 8p. (PB 171 118) SOcents
46
ill
ENGINEERIN9 (con. )
s! ■:-.'■.•
Analysis of relative perfonnsncse d ablating materiili coopated to a
heat sink material. June 66. I3p. (FB 171 054) 50 cents 39
Cathode ray storage tubes. Apr 60. 34p. (PB 171 127) $1.00 50
Cryogenic materials data handbook. Sep 60. 87p. (F$ 161 093- 5) $2. 25 58
Electron tube emisaioo stabiUty. Feb 60. 103p. (FB 171 117) (2. 50 .T. 47
EvaluBtiaa of a flame surveillance-type detector. Apr 60. 28p.
(PB 17 1 028) 75 cents 38
EvaluatioD of air traftic control radar-beacon systema (ATCRBS).
Oct 59. 285p. (PB 171 095) $4. 00 > 41
Field measurament of community noise ezpoaure near Haoscom Air
Force Base, Mass. Aug 58. 28p, (PB 171 076) 75 cents 37
Fused salt vokaic cells. An annotated bibliography of die tmfhnir^^
literature concerning cell potentials. July 59. 41p.
(PB 171 11-^ $1 . 25 61
Influence ct natural frequencies and aource correlatloa fields oo ran-
dom response of panels. July60. 7^. (FB 171 090) $2.00.$: i. 38
Lam noise badcward-wave amplifier (VA-191) developoient. Mar 60.
64p. (PB 171 069) $1.75 L 56
Madiematical model for locating exit cazlwaya. Dae 59. 52p. T
(FB 171 066) $1. 50 ....) 38
Meullurgica) observations of high velocity impact. Sep 60. 2^.
(PB 161 800) 75 cents .- 62
Micro- module production prognun. 1959. 266p. (19171 125) $4. 00 55
Micro- module production program. 1960. 169p. (PB 171 126) $3. 00 . . < / 54
ONR study gxaup on microelectronics. June 60. 18p. (FB 161 890) "
50 cents
Paperlined nu
lium dry cells «jid batteries.
00
1960. 35p.
53
54
lagnesl
(PB171 102) $1.
Probability at atuining a given flight path as a functioD ct the tuxn
radius, turn initiation error, and »'*i*^ng change. Ai^ 60. 12b.
(FB 171 116) 50 cents 37
Programming IBM 650 RAMAC computer for data processing in an air
route traffic control center. Oct 59. 10^. (1% 171 040) $2.50 39
Pr(^)agatian distortion erf bands at large -amplitude acoustic ooise. IT.
An experimental investigation at certain plane wave caaea. May 60.
31p. (PB 171 059) $1.00 53
Propertittp of gaa hydratea aod dieir use In deminerallzing B«a water.
Sep6(r 74p. (PB 171 031) $2. 00 4O
Soil atabilizadon: investigations at a chemically modified rmmfi^nf t»
a stabili2in| material. July 60. 60p. ( FB 171 096) $1.50 ♦.. 40
Study at helicopter pilot'a eye movement* during visual flight oooditkaM.
Nofv59. lip. (PB 171 094) $2. 50 ^ 37
Study and development of die Hickman aea-water still. Sqp 60. l§2p.
(PB 171 030) $3.00 \ . 39
Study G< electrical propulsion d ordoance land vehicles. Sep 60. 33p.
(PB 171 026) $1.00 ^ 45
Theoretical and experimental investigation at radioactive lonizatioo
gauges. May60.. 199p. (PB 171 105) $3.00 51
Transducers. Aug 60. 7p. (QTS SB- 428) 10 cents 53
Usase ratea Gf aircraft oxygen. May 60. 20p. (FB 171 067) 50 cencs. . . . « 36
VHF and UHF power generators for RF instnonenutlan. Sm 60. 24p.
(PB 161 578) 75 cents 'S2
MACHINERY. FABRICATION. AND ACCESSORY ECjUIIllENT
Statistical analyala at tensile properties at heat-treated Tl-4Al-aMo-lV
aheet. Sep
MATERIALS
pO. 4Sp. (FB 151 095) $1.25.
■Tf
Adbealve bonding at meuls for advanced ordnance^ appIicatloiM. Sep 60.
21p. (FB 161 863) 75 centa
Compatibility at rocket protelUms with msierials of ooiMtructian.
Sep60. 65p. (FB 161 215V^cema
66
66
70
MATERIALS (con.)
XX«tlnuouB filament ceramic fibers. June 60. 84p. (PB 171 061) $2. 25.... r ^
Design manual for glass reinforced plastics in naval applicationa. ^
Jar58. 7l6p. (PB 171 096) $8.00 -t-- ^5
Pevelc^iment of a fabric to provide personal protection from toodc
inateriaU. June 60. 45p. (PB 171 058) $1.25 '*
Development at ahade standarda and tolerances for USAF blue 84 and
blue 584 aervice and optional wear uniforms. May 60. 247p.
(PB 171 069) $3.50 ^*
Development of shade standards and toleranoec for USAF Tan 505
May60. 63p. (PB 171 062) $1.75 ;J
Flake - glass Uminates. Oct 60. 130p. (PB 161 947) $2.75 {^
Investigation of glass flake laminatea. Feb 60. 52p. (PB 171 039) $1.50 **
tovesugation of intermeullic compounds for very hlfh temperature ^
appUcations. July 60. 130p. (PB 171 081) $3.0a '*
Load support and ami -scuffing properties of lubrlcadta. Part II. WADC
universal gear and spline lubricant tester. May 60. 21p.
(PB 171 055) 75 cents. ''
F^rformance of petroleum baaed hydraulic fluids In a pump loop at
3000 psi and 275°F. Jime 60. 87p. (PB 171 063) $2.25 72
Pippertiea of refractory materiala: Collected dau and references.
JuDe60. 114p. (PB 171 101) $2. 50 ••
Study by light scstterlng of the effect of high temperature on the forma.-
don of insolubles in,)et fueU. Oct 60. 19p. (PB 161 921) 50 cents '*
Surface and environmental effects on ceramic materials. Aug 60.
29p. (PB 171 074) 75cents. : • "*
Symposium on analysis of nitric acids sponsored by the panel on fuels
requiring oxidizers. Dec 51. 87p. (PB 171 115) $2.25 : ..'. 2
UUrssonic and ceramic coatings. May 60. 52p. (FB 171 057) $1.50 ..•• •*
MATHEMATICS ■ j
Contributions to perceptron dieory. June 60. lOBp. (TO 171 093) $2. 50 *
Design and operation of the ceilometer computer. Oct60. 77p. (PB 161 565) $2.00 ••
Introduction to digital computing. Aug 60. 46p." (PB 171 100) $1.25 "
Tables for Mood's distributlan: free interval eatimatlon cechnl(rie for
differencea between two mediana. Msy 60. 2^. (PB 171 078)
75 cents ^6
T^les of Q-functloi& for two peroepcron models. May 60. 14^
(PB 171 092) $2.75
TSsting continuous computers.
MECHANICS 1/
81
Feb58. 206p. (PB 171 060) $3. 50 •*
Bflea of viscoelaatlc foundation on forced vibration of loaded rectangu-
Ur pUtes. July60. 2^. (PB 171 071) 75 cents . .- » ■*
Miniature wafer -style preasure transducer. Oct 60. 34p.
(PB 171 104) $1.00 ^
()uasl- orthogonal nxxles of dynamical systems. Aug^. S8p. '
(PB 171 070) $1.50 - "^
METALLURGY il I ' {
Beryllium crack propagation and effects of surface cooditiOD. July 60. ^
197p. (PB 171 068) $3.00 '*
Beryllium reaearch and development In the area of composite materials.
Julr60. 121p. (PB 171 083) $2.75 - '*
Comparison df shear strengdi values obuioed from three types of shear
tests. 7075-T6 aluminum. Oct 60. 15p. (PB 161 989) 50 cents '*
CoTosion of meuls in tropical environments. Part 5: stalnlesa ateela.
Sep 60. 24p. tPB 161 749) 75 cents ^
'>esign information' on 17-7 PH stainleas steel for aircraft, and
miaailes. Sep 60. 37p. (FB 151 096) $1.00 '*
" tection of fatigue damage with Rayleigh wavea. Aug 60. 57p.
(FB 171 099) $1.30 **
MBTAmfRGY(con.^ ^'
Development erf low alloy steel compoeitionB suiteble for hi^ streagth
steel castings. Jaly 60. 7^. (PB 171 065) $2.00
Elevated temperature diffusion in die systems Nb-Pt, Nb-Se. Nb-2^
Nb-Co, Ni-Ta, and Fe-Mo. Sep 60. 13p. (PB 161 767) 50 cents . .
Fatigue and stress n4>ture properties of Incooel 713C. V-57C and
dianluit alloys 7Al-3Mo-'n and MST 821 (8Al-2Cb-Ts-Tl).
July 60. 92p. (PB 171 064) $2. 2S
High temperature oxidation of iron-chromium binary alloys in water
vapor, Part 1: a preliminary study of the mechanism at oxidation
d iron-chromium binary alloys in water vapor. Sep 60. 27d.
(PB 161 1696) 75 cents .,
Investlgadto of creep buckling o€ columns and plates. Part II. Creep
buckling experiments and columns of Ti-7Al-4Mo titanium alloy
July60.|54p. (PB 171 082) $1.50
Uquld metals. Aug 60. lOp. (OTS SB-424) 10 cents
Martenetran materials for use in binary resistance devices. Ian 60
48p. (PB 171 066) $1 . 25 !^.* .. .
Metallurgy (rf yttrium and die rare earth metals. Plirt I. Phase
retatiooihips. May 60. 246p. (PB 171 085) $3. 50
MeuUurgy of yttrium and the rare earth metals. Part II. Mechanical
properties. June 60. 73p. (PB 171 086) $2.00
Physical and mechanical properties of the cobelt-chromium-tungsten
alloy WI-52. Sep 60. (PB 161 216) 50 centa
Research oc properties of high strength materials suitable for high
temperature applications. July 60. 6lp, (PB 171 060) $1. 75
Some physical properties of martenaltlc stainless steels. Sep 60.
31p. (P» 161 218) 50centa....l
Some quantitative aspects of fatigue of materials. July 60. 292p. * *
(PB 171 084) $4.00
Status of research and development for high strength aircraft steels
July60. 36p. (PB 171 077) $1.00
Study of fatigue properties of ultra -high strength steel. June 60. 65p!
(PB 171 056) $1.75 __
Vacuum induction melting: oxygen and carbon in iron. Sep w! 20d
(PB 161 ^) 50 cents
\-:
PHYSICS (coo.)
Quarterly radio noise data. June. July, August 1959. Sep 60. 6Sp.
(PB 151 377-3) $1. 00
(Quarterly radio noise data, September, October, November 19S9.
Sep 60. 64p. (PB 151 377-4) $1. 50
(Wrterly radio noise data, December, January, February 1959-60.
Oct60. 66p. (PB 151 377-5) $1.75
Soviet research in field electron and ion emission, 1955-1959: an
annouted bibUography. Oct 60. 41p. (PB 161 576) $1. 25
Table of magnitude of reflection of coefficient versus return loaa.
Sep 60. 47p. (PB 161 573) $1. 25 :
Page
4 \
MISCELLAyBOUS
Report of NkL Progress. Dec 60. (PB 161 288) $1.25, $10.00/year.
NUCLEAR IHYSICS AND NUCLEAR CHEMISTRY
%
n
ft
n
12$
A proton-retoil organic scindllatioo spectrometer and investigation
into a variable threshold spark counter. July 60. 35d.
(PB 171 120) $1. 00 .^.
Radioactivity in water supply and waste water systems: peacetime
detection and control. June 60. 88p. (PB 171 091) $2. 25
Scattering of cobalt-60 gamma radiation in air ducts. Oct 60 25o
(PB 161 575) 75 cents ^'
Survey of solid-state gamma/neutroo deiectloo systems.
64p. (PB 171 124) $1.75
July 60.
101
102
PERSONNEL SOFPUES AND PERSONAL EQUIPMENT
Guide to aircrew personal and aircraft insulled equipment. Sep 60
156p. (P« 171 119) $3. 00 . . 102
PHYSICS
1 > , . -,
Borides and filicides of the transition metals. July 60 114d
(PBl71iai) $2.50 ......'.....'. 114
Magnetohydrodynamics. Aug 60. 8p. (OTS SB -426) 10 cents! !! ! * n*
On die nature of die crystal field approximation. Oct 60. lOOp.
(PB 161 56B) $2. 25 _ 112
SOCIAL SCIENCES
Cbemical notation study:
operations. Aug 60.
Dysoo-Wiswesser noution systems; encoding
53p. (PB 171 123) $1.50....
120
lao
120
106
120
123
for your convenience OTS order blanks (Form TS-37) are
available on requeur from the OFFICE OF TECHNICAL SBRVICBS.
'' v^
vU
V
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
Oma Of TfCHNICAl SKVICB ch.mMnr •
z
PkfM 1-130
January 13. 1961
BIBLICX7RAPHY
' Azmad Service* Technical Intbraatlco Agency,
Arli«um, Va.
PROTECTIVE CONSTRUCTION: A REPORT BTOLT-
CXSRAPHY. Nov 60. 85p. 406 red. AD- 242 653.
Order from OTS $2. 23 PB 171 106
TWi report released for sale to the public 17 Nov 60.
This bibliography comprises a selected list erf refer-
ences related to construction of "hardening" at
strategic military facilities to resist either nuclear
or qpnventional explosives. References are limited to
unclassified reports without specific discrlbutlaa
Umlutlons. Literature coverage is restricted to
documents within the Armed Services Technical In-
formation Agency's collection, cauloged from 1952 to
September 15, 1960. Entries Include references to
reports pertaining to characteristics of nuclear ex-
plosions, propagation of shoclc waves, underground
explosions, soil mechanics, and response to struc-
tures to blast.
■ I'
AGRICULTURE
Plant Cultivation
LaboratcH-y of Climatology, Centerton. N. J. I
THE CLIMATIC AND HYDROLOGIC FACTORS AF-
FECTING THE REDISTRIBUTION OF SR^. by
J. R. Mather and J. K. Nakamura. Final rept. (Tech-
nical rept. no. 1) on Contract AF 49(638)409. June 60.
2^. AFOSR-TR- 60-101; AD-24I 890.
Order from LC ml$2. 70. phH 80 PB 150 614
The influence of climatic and hydrologlc factors on the
redistribution at strontium in the upper layers d the
soil has been studied. Starting with the resulta d a
laboratory study of the nwvement of strontium- 89 under
the action at different volumes of several leaching
agents, it was possible to work out a mathenutlcal
model at movement which corresponded very closely
with die laboratory results. The model resulted In the
uniform downward leaching of a given percentage d the
strontium in each layer In the soil for each unit o#
leaching solution applied. The actual leaching efficien-
cies of CaCl, Naa, and delonlzed water were deter-
mined from the available experimental results. Test-
ing of the madjemadcal model of movement by comput-
ing the actual distribution of strontium with depth in the
soil at five different sites verified the usefulness of the
model and showed a definite cUnutlc Influence on the
leaching efficiency. (See also PB 150 615 - PB 150 617).
[Laboratory of Climatology. Centerton. N. J.]
EQUATION AND TABLE FOR DETERMINATION OF
THE WAVE OF LEACHING IN THE SOIL, by
C W. Thomthwalte and Sally Thomthwalte. AppendU
na 2 to Final reoL , Technical note na 3 on Contract
AF 49(638)409. [1960] 28p. AFOSR-TN-60-875;
AD- 241 892.
Order from LC ml$2. 70. phH 80 PB 150 616
A consideration of distributions obtained In various
leaching experiments suggest that there Is an organized
movement of the leachate downward in the soil in re-
sponse to the spplication of a leaching solution such that
a certain percentage of the original concentration moves
downward to the next lower layers In the soil with each
unit of water applied. The equation developed to describe
the wave at leaching In the soil la Identical to the equa-
tion of the binomial dlstrlbutlan. (See also PB ISO 614,
PB ISO 615)
Laboratory of
THE ROLE OF
DISTRIBUTION
John R. Mather,
nlcal note na 1
8 refs. AFOSR-
Order from LC
Climatology, Centerton, N. J.
THE WATER BALANCE W THE RE-
OF STRONTIUM IN THE SOIL, by
, Appendix na 1 to Final rept. , Toch-
on Contract AF 49(638)409. [1958] 13p.
TH-60-97; AD-241 891.
ml$2. 40. ph$3. 30 PB 150 615
Knowledge of the water balance ia basic to any under-
standing of the distribution of strontium both gepgraph-
Ically and with dqpxh in the solL The studies at the
chemistry of the soil and of rain water have been under-
taken to provide Information on the leaching efficiency
of different solutions, whether rain water or soil solu-
tions. Knowledge of leaching efficiency la of llcUe value
»
unless there is siso precise informstloo on the csdon
exchange capacity of soils both with depth and in areaJ
extent. The two (actors of leaching efficiency ot the
solution and exctisnge capacity of the soil must go hand
in hand in any determination oi the rate of movement al
strontium in the soil. The work undertaken so far merely
represents a first step In a long range study designed to
provide a clearer understanding of the nature and char-
acteristics c4 8montium-90 and its relation with the
moisture factor ^ climate. (See also PB ISO 614).
ASTRONOMY
Astrophytics
Army Signal Rfsearch and Development Lab. . Port
Monmouth. N. |.
THE ANGULAR POWER SPECTRUM OF LUNAR
RADIO ECHOES, by Fred B. Daniels. 25 May 60, Up
7 refs. USASRDL Technical repc 2129; AD- 239 464.
Order from LC i^$2. 40, ph$3. 30 PB 150 451
The theory al ra4ar reflections from the moon devel-
oped in an earlier report is extended to the deternUna-
tion of the angular power ^>ectrum, and comparisons
are made with e}9>erimental results. Satisfactory
agreement is foutxl except for weak Lambert- law
scattering that occurs near the limb. The possibility
is suggested at u$ing simultaneous pulse and fading
measurements ta determine the rate of rotation of a
planet. Results c^f both pulse and fading tests are in-
terpreted as due to scattering from the small-scale
surface features ol the moon. (Author). (See also
PB 146 937).
Carter Observatory (New Zealand).
HEIGHTS AND LOCATIONS OF THE AURORA
AUSTRALIS FROM DUPLICATE AND SINGLE PHOTO
GRAPHS. 1938-1941 [AND] ANNUAL, DOJRNAL AND
GEOMAGNETIC LATITUDE VARIAT1(»4S OF THE
AURORA AUSTRALIS. by G. W. McQuistan and
B. L. Frankpitt. Scientific rept. nos. 7 and 8 on Con-
tract AF 64(500)4. [1959] 78p. 10 refs. GRD TN-
60-628.
Order from LC n)iS4. 50. ph$12. 30 FB 150 942
The present report conuins the results at the measure-
ment of parallactic and single station photographs of the
Aurora Australi8„ exposed between the years 1938 and
1941 inclusive. This completes the analysis d all
plates up to 1951 held at the Carter Observatory. An
amended method ^f calculating the base line constants
is given and has been used to compute the constants
for this report. (See also PB 138 236)
(fee
Carter Observatory (New Zealand).
OBSERVATIONS OF THE AURORA AUSTRALIS, 1957
AND 1958. by G. W McQuisUn. Scientific rept. no. 9
on Contraa AF 64(500)4. J1959) 81p. AFCRC TN-
60-414.
Order from LC n4i$4. Sa ph$13.K) PB 150 941
Visual observations al the Aurora Australls collected
in New Zealand, New Zealand Antarctic stations and
adjoining regions over the period 1957 and 1958 are
here recorded in a form suitable forfurther researches.
The arrangement at the report has been designed in
semi -analytical form which it is hoped will retxler it
more suitable for future work. (Author) (See also
PB 150 942)
Ceixer for Radiophyslcs and Space Research,
CorneUU.. Ithaca, N. Y.
FARADAY DISPERSION IN THE SOLAR ATMOS-
PHERE, by Kenji Akabane. Radio Astronomy Tech-
nical rept. no. 4 on Contraa Nonr-401(27). 30 Jan 60,
34p. 12 refs. Research rept. RS2: AD-239 772.
Order from LC ml$3.00, ph$6.30 FB 149 007
The degree at linear polarization in solar bursts was
measured simultaneously at two bandwldths, 10 kc and
22 kc, each having the same center frequency, 201 . 6
mc. A number of partially linearly polarized type in
bursts were seen, and in every case the burst wss
more polarized in the narrow band than in the wide
band. According to the theory ol Faraday dispersion,
the ratio between the degree of polarization observed
at each two bandwldths gives the degree ot polarizatioo
at the source ^Q, the Faraday rotation angle 4, and the
dispersion angle 6.
Geophysical bist. , U. of Alaska, College.
SOLAR RADIATION AND RADIANT HEAT EXCHANGES
IN ARCTIC REGIONS, by Carol Echols. >ily 60, 25p.
4 refs. AAL Technical rept. 58-27.
Order from LC ml$2. 70. ph$4. 80 PB 150 575
Studies at the microclimate were conducted in an area
north of College. Alaska, at BslUine's Lake Field Sutioo.
The work, was limited to studies al the radiation enviros'
ment. with particular emphasis on winter conditions.
Measurements were nnade of snow and air temperatures,
and also of total incoming radiation and the net radiation
exchange.
■i
Hsrvard Coll. Observatory, Cambridge, Mass.
PHOTOMETRIC OBSERVATI(»IS OF MARS IN 1941
AND 1958. by Gerard de Vaucouleurs. Scientific rept.
no. S on Contract AF 19(604)3074. 15 Aug 60, 36p.
GRD TN-60-616.
Order from LC mi$3. 00. ph$6. 30 PB 150 741
Mean relative brlghmess values are given for 113
regions of the surface at the planet Mars in white,
green and red light, from 2551 eye estimates obuined
in 1941 and 1079 In 1958. (Author)
Iowa Stste U. , Iowa City.
BALLOON OBSERVATIONS OF X-RAYS IN THE AU-
RORAL ZONE I. by Kinsey A. Anderson. [1959] 36p.
12 refs. Rqx. SUI-59-22.
Order from LC mi(3. 00, ph$6. 30 PB ISO 517
From several high altitude balloon flights made in the
Northern Auroral Zone observations have been on fre-
auenUy ^>pearing fluxes of x-rays. By use at sodium
iodide scintillation crystals and pulse height analyzers
tlao carried in the balloon instrumentation detailed
measurements of the photon energy spectrum in the re
Klon 40 to 340 kev hsve been obuined. These x-rays
generally appear without definite geophysical or solar
correlation. They are beUeved to be directly related
to the soft radUtion investigated by rockoons and also
to processes occurring in the outer Van Allen radiation
zone. The rapid intensity and spectral fluctuations
that are observed suggest that in addition some proc-
ess possibly atmospheric discharge, may also be Im-
portantT The relation of these x-rays to visible auro-
rae is not clearly established here. (Author).
kiwa State U. , law. City. '
PRMARY COSMIC RAY INTENSITY NEAR SOLAR
MAXIMUM, by Frank B. McDonald. Rept. on [Contract
N9onr-938(03)]. [1959] Up. 6 rrfs. SUl-59-11.
Oixler from LC mlJ2. 40. ph$3. 30 PB 152 057
lbs direct measurement of primary cosmic ray proton
and alpha particle fluxes and energy spectra has been
previously reported for s period of relatively low solar
activity (1955- 1956). These cosmic ray measurements
have now been extended to the recent period of high so-
lar activity. Strong constraints on the nature of the long,
term modulating mechanism are provided by the simul-
taneous determination of the spectrs of two components
widi different charge to mass ratla j
Laboratory of Astrophysics and Physical Meteor-
ology. Johns Hopkins U , Baltimore, Md.
THEORETICAL STUDIES OF INTENSITY, LINE-
wnyra and line shape in resolved infrared
SPECTRA, by WilUam S. Benedla. Final rept. for
1 Sep 55-31 Aug 58 on Contract AF 18(600)1557. [1958]
ll«p. 149 refs. [AFOSR] TR-59-61; AD- 216 657.
Orderfro»nLCmi$6.00, ph»18.30 PB 152 054
The researches have made a number of detailed ad-
ysaces in the understanding of the spectra ct NH3 and
included In the report are:
Interaalon ot stretching vibrations and Inversion In
ammonia, pub. In The Jal.at Chemical Physics
24:904, Apr 56
Struaure of perchlorylfluoride from high-resolution
Infrared spears, pub. In The Jnl. 9* Chemical
Physics 25. 594 - 595, Sep 56
Identification at H2OI8 and Hjp^' teUurlc lines in
the infrared solar spearum, pub. In M«moIres de
la Societe Royale des Sciences de U^e 18:557-571.
1957
Comments on the spectra of telluric H2O and CO2 •■
observed in the solsr spectrum 2.8 - 23.7 microns,
Special volume 2:18-30. 1957
Vibration- rotation bands of ammonia:
I . The combination bands 1/2 ♦Cl. ^2)' I**- ^
Jnl. of Research of the National Bureau of
SlMdards 61:123-147. Sep 58
n . The molecular dimensions and harmonic fre-
quencies of ammonia and deuterated anunonia.
pub. In Canadian Jnl. of Physics 35:1235-1241,
1957
m . The region 3. 2-4.3 microns, pub. in The Jnl.
4^ of Chemical Physics 29:829-845, Oa 58
Calculation of line widths In H2O-N2 collisions, pub.
In The Jnl. of Chemical Physics 30:388-399, Feb 59.
Uege U. (Belgium).
EXCITATION AND ABUNDANCES IN COMETS, by
P. Swing. Technical note no. 5 on Research 00 Rela-
tions between Cometary and Upper Atmospheric
Physics. Contraa AF 61(052)24. 6 Apr 60. ISp.
16 refs. AFCRC-TN-60-439. ..«„.,
Order from LC mi$2. 40, pW3. 30 FB 150 943
Intensity anomalies observed in the rotational lines of
Swan bands of comets are due to the presence of ab-
sorption lines in the exciting solar rad'ation. It is thus
proved that the Swan bands are excited by fluorescence
although their lower level ^Tf^ is not the ground elec-
tronic BUie of C2. The nuclei of the periodic comets
1957£and 19S9b_have radii of the order of one kilo-
meter. The relative abundances of CO*(in the tail)
and CN (In the head) In Comet Bester 1947k have been
determined. At nucleocentrlc distances less than
130.000 Km the CO^ions are ten times ss abundant
as CN; at the edge of the head (150. 000 Km) N(CO-»)
'--20 N(CN). The abundances of CO* are much
greater than usually considered. (Author)
Ll^e U. (Belgium). ^ ^
HELKX31APHIC POSmONS OF TEN COMETS. Tech-
nical scientific note no. 3 on Contract AF 61(052)24.
Jan 60. 42p. AFCRC TN- 60- 296.
Order from LC mi$3. 30. phr. 80 PB 150 938
Considering the Interest shown recently In die effect of
"solar wind" on comets It has seemed useful to us to
prqMre tables of heliographlc coordinates for a number
of recent comets, also for Periodic Comet Encke 1960
which wlU be observable in 1960 and 1%1. Comparison
of cometary- soUr- and geophysical phenoma will thus
be easier. (Author).
Liese U. (Belgium). _
REUiTIONS BETWEEN COMETARY AND SOLAR AC-
TIVITY. Technical scientific note no. 4 on Contract
AF 61<P52)24. Mar 60, Up. 37 refs. AFCRC TN-60-
401.
Order from LC mi$2. 40. ph$3. 30 PB 150 940
This note Is concerned with a comparison of the behav-
ior of dust- and gaseous cometary heads In relation to
solar activity. The available material seems to Indicate
that the brightness of s dust- head is not related appreci-
ably to solar sctlvlty, while a gaseous head may be. It
is suggested that Comet Encke be carefully observed
photometrically at Its next return, late In 1960 and early
in 1961. (Author).
Liege U. (Belgium).
RELATIVE INTENSITIES OF FORBIDDEN 01 LINES
IN AN EXPANDING CTELLAR ATMOSPHERE. Tech-
nical scientific note no. 2 on Contraa AF 61(052)24.
Jan 60, 25p. 8 refs. AFCRC TN-60-297.
Order from LC ml$2.70, ph»4.80 FB 150 939
The reJatlve intenaitie. erf the red and green [Oil Unes
have been computed for eight types of diluted atmos- '
pheres expanding at a uniform rate. The alze al these
atmospheres may he deduced from the relative
intensities of the red and green Unes or from the red
lines only. (Author;)
I
i
Liege U. (BelgiunO-
^rlf'?iLt*^ii!!i^*^ OF THE RED SYSTEM
OF CN. by N. Godfrlnd. Technical sdentlflc note
no. 1 on Cootraa AF 61(052)24. Feb 59 22d 14ref«
AFCRC-TN-59-270. r^ jy. ^^. i4ref«.
Order from LC m4^. 70, pii$4. 80 PB 150 926
The red system of (k has been photographed In the
XH^^^ ' ^^ fO«-gratlng in the region A7800 -
■^HJOO. The rotatloMl structure of the (2,0) and (3 1)
baxKls has been analyzed. Various constants have b^en
oetermlned. A comparison with cometary spectra has
been published by J. Dufay and P. Swings. AMmpari-
•on with the solar spectrum described by H D Bsb-
cock and C. E. Moore is made; 86 good coincidences
^If^ f*'^''*^ previous asslgnmeMs to CN appear
<»ubtful. A convindug and definite solution cJrthe
problem of the Identification of the red Wfwom <d CN
In the sun requires new observational aad kborstorr
oats. (Author)
Manchester U. (Gt. Brit. )
S^^p.^J.i^^.lS!^'*^'**^ ^' MEASURED
PROFILES OF THE MOONS SURFACE. AND THE
^^^ ALTmJDE. by Gilbert Fielder. Technical
scientific note no. 4 <jn Contract AF 61(052)168. Nov 59
47p. 2 refs. AFCRC TN-60-268. ; «o. rwv w.
Order from LC ml$3. 30, ph$7. 80 PB 15^ 933
JZ^I.t^^lT^*' !""■" ^ ^ *^^"**«' of measured
Sil 1^ ! . **^"" ^ ^"■°'' ^ *« coordinates o* die
peak which is casting the shadow. TTie aim oT die first
pw^ or this note is to Investigate the variation al these
^^.n^T^"^^ "^'^ "^ the Moon and to estimate diefr
m«ffiitudes. -nies€C(«l part win present measured
^«3fUes of parts of the terrain lying close to the 'neck'
^ ^*^'L*^^ '^'^*"™ •«* Mare Serenltatls, and
T5?thS^'t*l°*"^if^ ^ ** Caucasus Mountains.
The dUrd part gives altitude measurements made on
•niaU cratCTs in die Hyglnus region, and the note ter-
SS^^ /l! Pf°' -*° ?* ""^ ^"»«- Ptolemaeu. A.
(Author). (See also PB 146 133).
MancheaterU. (Oi. Brit.).
STUDIES IN LUNAR TOPOGRAPHY V A SYSTEM
A« .iJSP'^^^^^TRIC TECHNIQUE ANDTTS
AmJCATT^JTO FORMATIONS IN irffi MaTe liT
BRn^ ^ TTwmaa Rackham. Technical scientific note
»CR?^(SS9'^"<°^^^^- ^59. 40,. 7 refs.
Order from LC mli3.00. ph|6. 30 FB 150 934
1^ 2r^*^ ** *^ P**' diacusse. a special applica-
tion of mlcrodensltometric techniques as used InTSe
systematic measurement of lunar shadows obtained on
35mjn Cine film at die «c-du-Mldl ObaervawTy^n^
J2^. *!^^^°". «*"^« *• resultant tabulated relative
heights and relevant datp for Aristiliua, Auiolycus.
Plton. Archimedes C, and Archimedesi. Scaled diagrams
of die first four objects are also included. (Author)
(See also PB 150 933). ''
'Manchester U. (Gt. Brit. ).
jnj^ IN LUNAR TOPOGRAPHY. VL MEASURED
^o'yjl ?f. MOUNTAINS IN TOE SOf^T^^^^Yi
PART OF MARE TRANQUILTTATIS. by Geothey
Turner. Technical scientlflc note na 6 on Contract
AF61(M2)168 Nov 59. 21p. Z ref.. AFCRC tS-^27Q
Order from LC mi|2. 70, phH W PB 150 935
Measuredhelghts for craters in die South Eastern ^art
Mare7r«n<iullltatls are given for the western Innw
walls and eastern outer waUa. The new values are com-
pared with earUer determinations made by other tech-
nlquea. Panoramic profiles of the apparent skyline hava
Been made fbr two points In die region which llluitrate
die ahort range of vlalbUlty of features due to die
moon s curvature. The Photometric determination of
tha gradient of genUe slopes Is discussed and some ro-
eulta are given. (Author). (See alfo PB 150 934)
Manchester U, (Gl Brit. )
STn^ IN LUNAR top6graphy. VIL MEASURE-
^^NTS OF THE HEIGHT OF THS WALLSOTTlffi
CRATER ARCHIMEDES, by Geoffrey Turner. Tach^
?i!re^^f^*f note na 7 on Contract AF 61(052)168
Dec 59. 19p. 6 refs. AFCRC TN-60-271
Order from LC ml|2. 40. ph$3. 30 PB 150 936
R^ts are jdren for the measurement of negatives
iS^ ^ *!"'' "*" ***" ^ '956 and 1959. Tile average
bright for die Inside of die East and West walls are 1731
^,U JT%* respectively, and 1623 meters for die
wtalde of die East wall TTie present work is compared '
wlA earlier results and profUes lUustrate die abaanee
of jagged waUa. (Audior). (See also PB 150 93^7^^
Minnesota U. . Mtameapoilt.
OOSMIC RAY PROGRAM Annual progress rent and
technical repts., 1 Sep 56-i Sep 57. on Cootraw
Nonr-710(19). [1957] 109p. 44 ref«. AD-155 313.
Order from LC mlJS. 70, ph|16. 80 FB 148^60
TTie primary alpha nartlcle spectrum over North Amer-
ica and geomagnetic cutort energies r ilia m,„ii,m\^
<^"^c ray latitudes in the US are 6° higher diancoo-
vaitlonal geomagnetic latitudes, and British andContl-
naital latitudes are 6° lower. TTiis has great bearing
oo the calculation of energy spectra from observations
of cosmic rays at various latitudes. Angular cor rela-
aiiout 6200Voecay8 show that die measured dlstrlbu-
tlon i% significantly different from isaropy. both in
latitude and longitude. A cosmic rav let in rha inlS
1^!^^^ qa-arraag: A 22. 4-1 'stack o/emulslom
mJLf^iTSJ^t^'*^^ Sept 1956 in a balloon
fljght at 116, 000 ft. In the 9 radiation lengdis of die
Mlnn«ota portion of die stack, the jet multiplied from
miSS^S^iHilf*:!;?- to 8a» articles. Geo-
magnetic effects on heavy prtmarv coamic radiation mt
iCJUat: Tlie results indicate diat die eatt-west^ect
is normal In direction, and diat angular disfrlbution. as
a function of zenith angle, shows none of die shadow
cone effects predicted by Schrempi Large cosmic ray
H«;rease accompanying «ol«r maximum 1957: Two
t^nes erf observations at balloon altitudes show a very
lijrge decrease compared wltfi 1955 and 1956. Bis.
primary alpha particle intensity at sunspc* mavtmupi-
The alpha particle data showed that a decrease oc-
curred throughout die spectrum and diat, even diough
bodi low and high energy particles are reduced in In-
tensity, tome lo» energy particles can still arrive,
tyim.ifhal alpha particle distribution at Guam: Pre-
Umlnary results indicated that the east -west asymmetry
is not as large as expected.
Siwce Sciences Lab. . General Electric Co. . Phila-
delphia. Pa, . ^.«„ w
CHARGED PARTICLE RADIATION IN SPACE, by
T R. Rlethof. Aug 60. 33p. 117 refs, Jechnlcal In-
formation Series R60SD391. .e«««i
Oxder from LC ml$3. 00. ph$6. 30 PB 150 801
The enlarged particle radiation In space Is reviewed,
with particular emphasis placed on charged particles
trapped in the earth's magnetic field, the "Van Allen"
belts. The vehicles and techniques used in measuring
die charged particle radUtlon are considered in con-
junction with die results of some of the measurements.
The data Is analyzed to obtain some Idea of the dis-
tribution of charged particles both with respect to loca-
tion In space (latitude, and distance from die center of
die Earth) and wldi respect to dielr maas and energy. ■
A summary of some of die Ideas for die origin of die
Van Allen belts is Included. Cosmic rays and solar
flares are briefly considered. Some effects of particle
radiation are briefly considered, with emphasis on
dielr Influence on space tr^yel^ and possible protec-
tlTe techniques. (Author).
Yale U- Obaeryatory. New Haven. Conn.
A VERY LOW FREQUENCY RADIO EXPERIMENT
FOR SATELLITE AND PROBE TRAhCPORTATlON. by
tN. Douglas, G. R. Huguenln, and A. E. Lllley.
inal rept. on Contract AF 19(604)3069. Jan 6a 57p.
3 I'efs. AFCRC TR -60-210; AD-234 974.
Older from LC ml$3. 60. ph$9. 30 PB 148 258
Theoretical and experimental investigations were made,
of die ionospheric regions above the maximum of the F2
layer by utilizli^ observations of extraterrestrial low-
frequency radio noise made In rocket probes and satel-
lites. The following sources of VLF radiation are ex-
amined: general cosmic environment, synchrotron ra-
diation, plaama and shock wsvcs. Cerenkov radUtion.
parametric oscillations, free-free transitions, solar
disturbances, non-thermal planetary radiation, and ter-
restrial diaturbances. Based upon predicted VLF Inten-
sities to be expected from cosmic sources of radUtion.
performance specifications on the antennas and radiom-
eters' were developed. Three complete satellite aayloads
were constructed for rocket probe and satellite kans-
portatlon. Each payload operates at 13. 25, 7.0^2. 2.
and 0. 7 mc Ground -baaed jadlometers and grdmd-
based tranamltters were tonatruaed for terrestrial
correlation studies and closed-loop tests of loooepherlc
leakage.
BEHAVIORAL SOENCES
Human knginoering
Aerospace Medical Dlv. , Wright Air Development
Div.. Wright -Patter eon AFB, Ohio.
A METHOD OF ESTIMATING SURFACE COLOR
DISCRIMINABILITY FOR CODING TRAINING EQUIP-
MBNT AND PREDICTING LABEL LEGIBILnY, by
Cbarlea E. Guatafson. Rept. oo Human Factors in the
Design of Training Equipment. May 60, 1^. ♦ refa.
WADDTechmcal note 60-83. „.„«.,
Order from CJTS $0. 50 « 171 053
Using luminous refleaance val«s for Feder^ Sund-
ard colors, the classic formula for contrast Is sug-
gested as a convenient method of eatlmatlng surface
color diacrlminabllity for purpoaes of coding training
equipment and predicting the legibility of panel labels.
Errors In discrimination increase as brightness con-
trast decreases, without regard to contrast In hue.
Specific applications of tht method are discussed, and
coocluaions are drawn concerning contrast limitations
for opHmian color dlscrlmlnsbllity and label legtbiUty,
(Author) (See also PB 143 821)
Quartermaater Research awj Engineering Cancer.
Natick, Maaa.
QUARTERMASTER HUMAN ENGINEERING HAND-
&K SERIES: VIL THE SIZE AND SHAPE OF THE
AVAILABLE VISUAL FIELD DURING THE WEARING
OT ARMY HEADGEAR, by John L. Kobrick and Brian
Crist. Msy60. 25p. 7 refs. Technical rept. EP-133:
AD- 238 090. ^ ,.o„n
Order from LC mi$2.70, pW4.80 PB 148 319
This report furnishes Information in tabular form on
the size and shspe of available visual fields durltig the
wearing of 12 Army headgear ensembles. Schematic
diagrams are also provided to aid in visualizing size
and shape of the visual fielda. (Ai«hor)
Aerospace Medical Dlv. , Wright Air Development
[Dlv. ]. Wright- Patterson AFB. Ohia
TASK PERFORMANCE WITH THE CRL MODEL 8
MASTER -SLAVE MANIPULATOR AS A FUNCTION
OF COLOR-CODIN<J. DISTANCE. AND PRACTICE,
by D. Frederick Baker and Billy M. Crawford. Rept.
on Human Factors in Advanced Flight. Nov 59, 19p.
7 refs. WADC Technical rept. 59-728;. AD- 233 457.
Order from LC mi?2. 40, ph$3. 30 PB 152 300
This rqK>rt released for sale to the public 26 Oct 60.
The ability of Master- Slave Manipulator (CRL Model 8)
operators to identify the slave hands and dielr move-
ments with corresponding components and functions of
die human body (specifically forearm, wrist and finger
movement) was Investigated. A handling task involving
rearrangement of blocks was devised to be performed
under two different conditions: (1) wldi standard slave
aws (red aw^ and (2) with slave jaws modified so
Jut the jaw correafonding to the thumb of the operator
was green. The uak was performed at dlstancea of
9 in. . 36 inc. . and 63 in. from die radiation shield.
Work time as a function erf task distance was investi-
gated and work rati^. based on mean time scores for
direct handling vs. gemote handling, were determined
(Author).
Personnel and Training
American Inst, foi* Research, Washington, D. C
OPERATIONAL ANALYSES OF THE NAVAL PERSON-
NEL SYSTEM PART L DEVELOPMENT OF A PER-
SONNEL SYSTEM MODEL, by Richard H. Gaylord
Alfred ;. Farina and Paul ^)ector. Final rept. on Q>n-
tract Nonr-2872(00). Dec 59, 59p. 3 refs. AIR-33-59-
FR-218; AD-2» 545.
Order from LC ml$3. 60. pb$9. » PB 152 136
An amplication at the techniques erf operations research
to the analysis of the Navy Personnel System is de-
scribed. The Personnel System is conceptualized as
that portion of the N«vy which is directly concerned
widi the information, decisions, and acUons necessary
to insure die availability of the right people at the
right time and place to operate, maintain, and support
the Naval weapons system In a maximally effective man-
ner. Thefollowingmajor steps were taken In die study
(1) definition of the b»sic purpose of die Personnel
System; (2) Identification of die major functions served
in accomplishing the system's basic purpose; (3) iden-
tification of the major areas of interaction between me
Personnel System and other systenis of the Navy; (4)
identification of the major processing programs of
Personnel System operations; and (5) development of a
mathematical model to estimate die effectiveness of
alternative personnel programs in supplying required
skiUed manpofwer. Also included is a long-range re-
search plan for extending die general analysis oT die
Personnel System.
American Inst, for Research. Pittsburgh Pa
A SURVEY OF THE LITERATURE ON PREDICTION
OF AIR FORCE PERSONNEL REQUIREMENTS, by
John D. FoUy, Jr. , ;e#ji B. Falrman. and Edna M.
Jones. Rept. for 1955-.1960 on Weapon System Quallu-
^X®,^f*^"*^ Requirements and Uiillaatlon. Contract
AF 33<616)6427, July 60. 388p. 121 refs. WADO Tech-
nical rept. 60-493.
Order firom OTS J5. 0(1 n 171 075
A survey of methods for predicting personnel require-
ments for future Air Force weapon systems is pre-
sented widi abstracts <3f 121 unclassified, professional
documents. Emphasis is placed on identifying proce-
dures for deriving per»onnel requirements information
and die supporting rationales. The current state of die'
art IS evaluated and presented widi implications for fu-
ture research requirei^nts. Conclusions from die
study show diat fairly thorough procedures exist for
describing tasks and positions and for combining tasks
into positions. Howevqr, no evidence was found of any
systematic evaluation qf diis mediod. Estimating man-
power requirements of|en has been done but only one
report describes a procedure for doing diis. Determin-
ing skill level requiremenu and criticality of usks has
received UtUe methodological attention. Most attentioa
has been directed toward the rating of skill levels
radier than toward any objective determination o( skill
requirements. One exception provides a seven-point
scale of c^jerationally defined performance levels. Like
the other techniques found in this survey, this one has
never been evaluated. (Author)
Applied Psychological Services, Wayne, Pa.
POST-TRAINING PERFORMANCE CRTreRION DE-
VELOPMENT AND APPUCATION: TECHNICAL PER-
FORMANCE CHECKUST CRITERIA WHICH MEET
THE THURSTONE AND GUTTMAN SCALABILITY
REQUIREMENTS, by Arthur I. Siegel and Stephen
Benson. Rept. on Contract Noor- 2279(00). Dec 59
97p. 7 refs. AD- 230 244.
Order from LC mi$5.40, ph$15.30 PB 152 142
The result* of five separate but related substudies are
presented: Substudiea \ m^ [] investigated the hypothe-
sis that skills are scalable in the same manner as are
the attitudes and the sensory phenomena which have
been previously scaled paychophysically. Three scales
meeting the Thurstone criteria were developed for the
skiUs underlying the tasks performed by the Nsval
aviation electronics technician. It was also shown that
these scales meet die Gutrman criteria of acalabllity
Substudym Investigated die hypothesis diat the meas-
ured level of performance of aviation electronics tech-
nicians will show a positive correlation with Naval
attitudes as measured through an attitudinal inventory.
Little or no relationship was found to exist between
Naval attitudes and fleet proficiency. Subtudy IV in-
vestigated the reUtionship between various "predic-
tors" and the post-training performance effectiveness
of Naval aviation electronics technicians. Of the
predictors investigated, no one predictor «r se was
found strong enough for praaical IndlvlduaTpredlction
of fleet performance. Study V compared, in terms of
maximum possible prediction, the power of the
manifest struaure analytic technique with the regres-
sion technique. The regression technique was found
to be more powerful. (Author)
Psychological Lab. . U. of Southern California
[Los Angeles]
A STUDY OF MILITARY LEADERSHIP IN RELATION
TO SELECTED INTELLECTUAL FACTORS, by
Alvin Marks, J. P. Guilford, and P. R. Merrifleld.
Rept. no. 21 on Studies of Aptitudes of High-level Per-
sonnel. Contract N6onr-23aiO. Nov. 59, 26p. 50 refs
Order from LC mi$2. 70. phH 80 PB 150 483
This study was designed to investigate die relationship
between certain intellectual-aptitude factors and mili-
tary leadership, b was also designed to develop a rat-
ing scale which would evaluate die degree of dispUy of
these aptitudes widiin die individual military leader.
It was hypothesized diat eleven Intellectual aptitude
factors are important in military leadership: percep-
tual foresight, conceptual foresight, penetration, ex-
periential evaluation, sensitivity to problems, adap-
tive flexibility, spontaneous flexlblUty, general rea-
soning, verbal comprehension, originality, and idea-
tional fluency. The general criterion (leadership rat-
ing) correlated significantly wldi only three of die apti-
tude composite scores, for the factors of originality,
sensitivity to problems, and verbal comprehension.
All correlations between rating and aptitude compos-
ites were very small. The individual rating items did
not correlate strongly with any of the aptitude factor
composites.
Psychological Research Associates, Inc. , Arlington,
Vk.
USE OP ANALYTICAL INFORMATION CONCERN-
DC TASK REC^JIREMENTS TO INCREASE THE EF-
PBCnVENBSS OF SIOLL TRAINING, by James. F.
Parker, Jr. and Edwin A. Fleishman (Yale U. ) Rept.
on Contract Nonr- 2489(00). Dec 59, 44p. 10 refs.
Order from LC ml$3. 30, ph^. 80 PB 152 123
Tie present report describes an approach to training
design which has not received much attention. The
emphasis is on the development of a training program
which makes use at analytical Information about spec-
ific ability requirements of the task to be learned. Two
types cf analytical Information are used. The first In-
volves knowledge about the abilities which contribute
to Individual differences in performance at different
stages of training on the task In question. The second
type at Infomution is represented by knowledge cf the
relative contribution of the different task oomponents
to over-all usk proficiency.
Psychology
Air ^orce Missile Development Center, Hollaman
AFB. N Mex.
THE MEASUREMEm" OF CONCEPT FORMATION IN
THE CHIMPANZEE AND ITS RELEVANCE TO THE
STUDY OF BEHAVIOR IN SPACE ENVIRONMENTS,
by Frederick H. Rohles, Jr. . Richard E. Belleville, and
Marvin E.Grunzke. July 60, I7p. 8 refs. AFMDC-
TR-60-20.
Order from LC ini$2. 40, pl«3. 30 PB 150 372
This report describes a new procedure for measuring
higher intellectual processed in the chimpanzee. The
fully automatic equipment employed eliminates con-
tinuous monitoring by the experimenter and can be
modified readily for conducting similar research dur-
ing space flight. (Author)
Applied Madiematics and Statistics L^bs. , Sunford
U. . Calif.
MARKOV LEARNING MODELS FOR MULTTPERSON
SITUATIONS, II. METHODS OF ANALYSIS, by Patrick
Suppes and Richard C. Atkinson. Technical rept. no. 27
on Contract Nonr-225(17). 28 Dec 59. 65p. 7 refr,
AD-231 213.
Order from LC mi$3. 90. ph$10. 80 PB 152 178
Maximum likelihood estimates for the learning param-
eters are considered for the case of noncontlngent rein-
forcement and then for the 2 -person Interaction situa-
tion. The assumption of exactly one element In the
stimulus set of each subject Is required. The methods
of parameter estimation are extended to models which
assume more than one stimulus element. The methods
resemble the maximum likelihood methods, but do not
have the maximum likelihood property. A method for
estimatii^ jointiy the number N of stimuli and the value.
0 of the learning parameter is also considered. Vari-
ous x^ tests are considered for testing hypotheses that
the transition probabilities of a first order chain are
consunt, that they are specific numbers, and that the
prxx:ess is a u* order Markov chain. Methods of esti-
mation are also given for making an almost maximum
likelihood estimate of the learning parameter. A gen-
eralized conditioning model is developed in which the
single parameter 9 is replaced by several conditioning
parameters. Simple maximum likelihood methods of
estimation for these new parameters are derived.
(Author)
Boston U.. Mass.
ANNUAL TECHNICAL REFT, by Warren G. Bennis,
Arthur M. Cohen, and George H. Wolkon. Repc. on
Coniraa Nonr-492(05). [1959) 25p. 13 refs.
AD- 229 368.
Order from LC mi$2.70, ph$4.80 PB 152 103
The effects of continued practice on the behaviors c<
problem -solving groups: Groups were assigned to 2 -
experimental CMioilions. The Wheel pattern was more
Btruaured and hierarchical. The Circle pattern had
equal conimunicatlon opportunities and was less re-
strlaed. Learning continued to take place In both pat-
terns longer than expected, and was of two nuj or kinds:
(a) a division of labor In the form of stable answer and
information exchanges; and (b) progressively more ef-
ficient operations within sudh divisions. The rate of
learning In the Wheel groups was faster than that of the
Circles, and they reached a point of optimal efficiency
while the Circles did not. Wheels also had more cor-
rect trials, fewer changes, and fewer final errors.
The effects of changps In communication patterns on
the behaviors of problem -solving groups: Groups were
under 4 experimenUl conditions: (a) Circle-to- Wheel
(CW); (b) Wheel-to-Circle (WC); (c) Clrcle-io-ClrcIe
(CC); and (d) Wheel -to- Wheel (WW). This made it
possible to study bcfw problem- solving groups behaved
when changed from a condition erf greater to one of less
hierarchy and restriction and vice versa, as compared
to groups which had not experienced changes in pat-
terns. WC groups took shorter times to solve prob-
lems and had more correct trials than CC groufm,
while CW groups took longer times to solve p-oblems
than WW groups but did not have fewer correct trials i
It was found that training was transferred from one
panem to another. The WC groups were more gener-
ally satisfied than the CC group*. CW groups showed
decreases in satisfaction under conditions of re-
stricted decision-making.
CaUfomla U. , Lo« Angeles.
A BIBUOGRAPHY OF PUBUCATIONS RELATING TO
THE SMALL GROUP, by Bertram H . Raven. Tech-
nical rept. no. I on Dynamics of Social Influence,
Contract Nooi- 233(54). Nov 59, 119p. 1445 refs.
Order from LCinl$6. 00, ph»l8. 30 PB 150 498
A bibliography of 1445 articles and books relating to
the small group Is presented, with index. Also in-
cluded is a discussion of a punch-card coding aysum
for the bibliography, together with suggestions for the
establishment and use of such a system. (Author)
Ctltfornl* U. . Ld« Ai^es.
AN OPERATIONAL DISTINCnON BETWEEN BELIEF
AND AnTTUDB. ky Martin Flahbein and Bertram H
Raven. Technical nept. no. 2 oo Dynamic* <rf Social
Influence, Contract Nonr-233(54). 4 Dec 59. 22a.
16 refa. AD- 233 352.
Order from LC ml|2. m ph$4. to FB 152 104
Stemming from Osgood' a analy^a ol attitude through
hla aemantic differential, a scale was developed which
permita an ope rational distinction between belief and
attitude. Attitude It defined as die evaluative dlmeiiaioo
d a concept, belief as the probability dimension ("1« It
probable or improbtbler). The adjective pairs that
•erve to discriminate these two dlmenalona were em-
pirically determined through the use otf a role -play pro-
cedure. The AB scale, djus developed, wat dien tested
for generallzabillty. and for Independence at dlmen-
Bions, and proven useful. Beliefs and attitudes were
independently mani^ailated. The relationship between
this finding and thoae al prior Inveatigation* la dis-
cussed. (Author)
Pels Group Dynamica Center. U. at Delaware
Newark.
^fSkI?? ""^t^i^^,^ COMMUNICATION
EFFICIENCY, byJo^T. Lanzetu. Annual progress
OrderfromLCmUl.BO. ph$1.80 PB 150 472
Selected personality, group, and lituatiooal variables
were examined in terms of djeir effects upon the char-
acterisdca d emitted meaaages and the acceptance at
ttansmitted messages. Five studies were completed
during the yer and (Xie other study is currently being
deslpied. The ezpioratory studies fall in two general
areas. One area invtstigated Is concerned with cbar-
aaerisdcs o* traaamttted and desired Information a«
a function d personality attributee at the sourca tad
conditions ct group interaction. Related to thia latter
*rea waa a study in which visual interaction waa con-
ceptuallied aa a form at communication activity
Anotherarea, dealing with the acceptance, retention
aiAi^ categorization at meaaages under specified con-
ditions or source and piedium, has been studied.
niinois U. . Urhana. '
WTERPBRSONAL PERCEPTION AND INTERPERSONAL
ja^TIONSHIPS IN THERAPEUTIC COUNSELING, by
Rolfe LaForge. Annual rept. no. 3 on Contraa Nonr-
1834(11). 15 Nov 59. 38p. 4 refs. AD- 230 445.
Order from LC ml$3. 0a ph$6. 30 PB 150 490
Ratings were obtained al interview recordii^ at Intar-
personal comnuinlcaaon in the dierapeutic situation, and
were used aa criteria In 0^ investigation of the D^-
statlatlc which measures the dissimilarity betwaen two
seta d ratings on corresponding Itens. The relatively
Urge correiatlona found between D**s calculated for
Pi*««a«bly independett variablea was atudied, and Q-
correUtiona were calcwlated for each subject and inter -
correUted with other componenta. An inveatigation waa
alao conAicted d die relationahip between clienta' rmi-
Inga d counselors and the Unera ratii^a d therapeutic
outcome. Ii waa found that interpretations based on d2
alone can be considerakly sharpened by comparing the
behavior d tbe componenta d elevation and the tendency
touse extremes in ratings made by hoapiulized patients
and co«nmuniiy oersona. (See alao PB 143 454)
A
Inadtute tor ^Iled Experimental Psychology
Tufts U. . Medford. Mass. ^^
VISUAL FACTORS AFFECTING EFFICIENCY IN THE
TASK OF PHOTOINTERPRETATION. by Mason N.
Crook. Annual summary rept. on Contract Nonr-494(17)
Dec 59. lOp. 12 refa. AD-232 175.
Order from LC mi»l. 80, ph$l. 80 FB 152 107
Factora affecting visual performance In phocolnterpreu-
tion are outlined. Thcae are (1) factors reUted to the
operator; and (2) factors related to work spaces, mate-
riala, and equipment. The foUowlng specific problema
were diacussed: (1) general iUumlnation. (2) lllumlnants
for colored tranaparencies; (3) differential Illumination
in atereo viewing; (4) binocular viewing of duplicate
pbotographa; and (5) visual fatigue. A work situation is
being developed to impose visual atresses analogoua to
dioae which might occur In photointerpreution. The
laak being used is reading of printed material, which la
positioned In duplicate in the Instrument and fused by
the subject. Preliminary experiments indicate that the
following proceaaes are interacting: (1) learning; (2)
adaptation; (3) blocking; and (4) fatigue.
Israel Inst, of AppUed Social Research.
FACET DESIGN AND ANALYSIS OF DATA ON PER-
SONAUry AND ATTITUDES RELATED TO HUMAN
ORGANIZATION, by Uriel G. Foa and Louis Guttman
Technical aummary rept. for 1 June 58-31 May 60 on
Cwitract AF 61(052)121. [1960] 36p. 8 refa. AFOSR-
TN- 1008.
Order from LC ml$3. 00. ph^. 30 PB 150 361
TTie present research project is devoted to problema
of content, statistical structure, and deductive meu-
djeory for special areaa of empirical dau on human
organization and personality. TTiree levels of content
problems are discussed in die present report. In view
of die Importance of concept cUsslfication in scientific
development, a diree structure for the cUsslfication
d behavioral data haa been developed. This consti-
tutes die most general level; die suggested structure
la formal, but it providea a framework for the classi-
fication of the facets of a specific study. Finding facets
which will predict the sutlstlcal structure of a ^.ven
set d variables exen^lifles die most specific appro**
to die content problem. Proceeding from diese two
extremes toward the middle It may be possible to de-
velop faceta for a apeclfic behavior area, radier'dian
for a single study. This haa been done for die analyaia
d interpersonal behavior.
Kanaaa U. School d Pharmacy, Uwrence.
THE DOSE -EFFECT AND DURATION OF ACTION
OF SEVERAL CNS STTMULAKTS ON MOTOR AND
PSYCHOMOTOR PERFORMANCE, by Duane G. Wenzel
!,"* ^J^^P Rutledge. Technical rept. on Contract
Nonr-583(09). 23 Dec 59, 28p. 24 refs. AD- 230 246.
Order from LC mi$2. 70, pli$4. 80 PB 152 098
&uaes were made in an attempt to evaluate the effecta
central nervoua system stlmulanta have on human
performance. The teats employed meaaured several
components d what may be regarded as total psycho-
motor performance. No attempt was made to dlrealy
evaluate the eubjecUve or behavioral efftecta d the
druga in queMon. although such effects undoubtedly
Irfluenced the resuks obtained. The testa employed
«ere concerned primarily with motor response and did
lot permit adequate Judgment d overall performance.
Oeruin findings did appear to be worthy d conaidera-
don. Caffeine, for example, was usually most etfec-
dve at the lowest dose. The reaponse patterns with
thia drug gave reason to suspea that If the dose were
10 be Increased beyond the 300 mgrn maximum, the
level of performance could fall below that obtained
with placeboa. In general, phenmetrazine and methyl-
pbeoidylacetate were more effective in the dose
raiqpa tested than was d- amphetamine. The marked
daterioration d performance in the choice reaction
iMt produced by the 50 mgm dose of phenmetrlzlne
BMjr indicate some impairment of mentation.
Lincoln Lkb. , Mass. bist. d Tech. . Lexington.
REMEMBERING THE PRESENT STATES OF A NUM-
BR OF VARIABLES, by D. a Yntema and
a E. Mueser. Rept. on Contract AF 19(604)5200.
16 Mar 59, 13p. 5 refs. Group rept. 58-2.
Order from LC ml$2. 40, ph$3. 30 PB 150 975
The subject attempted to remember the present states
tf 2, 3. 4. 6. or 8 variables. He was read a series d
messages, each saying what state one of the variables
had assumed, and recorded each message on a status
board. It was found that the fraction d the questions
■Bswered correctly decreases as the number d var-
iables Increases and, if there are more than two var-
iables, is lower when they represent one attribute d
several objects than when they represent several attri-
butes d one object. The probability diat a particular
question would be answered correctly was found to be
tsfluenced by (a) the number d questions and messages
intervening between the question under consideration
and the message that determined Its correct answer.
(b) whether any d those intervenlna Items were Ques-
tions about the same variable, and (c) whether the
neasage that determined the correa answer was the
same as the previous message about the same variable.
Sources of error variance were considered. A few Im-
plications for the design d control centers are dis-
cussed in a separate section.
Lincoln Lab. , Mass. Inst, d T^h. , Lexington.
REMEMBERING THE PRESENT STATES OF A NUM-
BER OF VARIABLES: IIL WHY IT IS DIFFICULT TO
KEEP TRACK OF SEVERAL VARIABLES WITH THE
SAME SET OF STATES, by D & Yntema and
G. E. Mueser. Rept. on Contract AF 19(604)5200.
17 A(« 60, 13p. 2 refs. 58 G-0013.
Order from LC mi$2. 40, ph$3. 30 PB 150 369
Keeping track d the current states d a number d vari-
ables has been found to be more difficult In the case
where the variables are the same attribute of several
Bonsensical objects (in which case all variables have
the same set of states) than in the case where the vari-
ables are different attributes d one nonsensical object
(In which case each variable has Its own distinct set d
sutes). The present experiment showed that the differ-
ence may be ascribed entirely to the fact that ^ cannot
identify the variable from the name d its current sute
in the single-attribute case; explanations involving in-
terference among the Items to be remembered are un-
necessary. Tttie present ejoerlment also compared
the tasks d keeping trade d six attributes of one ob-
ject, three attributes d two objects, two attributes of
three objects, and a single attribute d six objects.
Performance was found to deteriorate in a regular
fashion as the number d attributes per object de-
creases. (Audior)
Lincoln Lab. . Mass. Inst, d Tech. . Lexington.
A THEORY OF COGNITIVE PROCESSES by Ulrlc
Neisser. Rept. on Contract AF 19(604)5200. 23 Feb 60,
22p. 27 refs. Group rept. 54-19.
Order from LC mi$2. 70, ph$4. 80 PB 150 794
Louialana State U. , Baton Rouge.
TEST OF A PROPOSED THEORY OF LEADERSHIP,
Bernard M. Baaa. Annual rept. na 5 on Behavior in
Groi^M, Contract N7anr- 356(09). 15 Nov 59, 6p. 6 refs.
AD- 229 624.
Order from LC mi$l. 80, ph$l. 80 FB 150 542
See also R 143 422
Massachusens ll. , Amherst.
PAIRBD-ASSOCIATES LEARNING AND PERFORM-
ANCE AS FUNCTIONS OF OCCURRENCE OF RE-
SPOtiSE MEMBERS (REINFORCEMENT) AND OF
STIMULUS CHARACTERISTICS, by Albert E. (3oss,
Harvey A. Tsub, and Bruce N. Gregory. Technical
rept. no. 1 on Contract Nonr- 269 1(00). Nov 59, 30p.
9 refs. AD-230 535.
Order from LC mi$2. 70, pbK 80 PB ISO 503
Massachuaetta U. , Amherat.
PAIRED- ASSOCIATES LEARNING WITH VARYING
RELATIVE PERCENTAGES OP OCCURENCES OF
ALTERNATIVE RESPONSE MEMBERS, by Marilyn E.
Sugerman and Albert E. Goes. Technical rept. no. 2 on
Contract Nonr-2691(00). Nov 59, 43p. 17 refa.
AD-230 536.
Order from LC ml$3. 30. pl47. 80 PB 150 504
Paired -aaaociate learning waa investigated with units
whldi had 2 rather than a aingle response unit. The
relative percentages of occurrence of alternative re-
sponse members of paired -associate units and of the
number of paired -associate units is described. In order
to control for effecta of time Intervals between succes-
Ive presentation of the same unit, there were 3 condi-
tions of presentation: (1) a consunt 3 -sec interval be-
tween successive presentationa of a unit; (2) longer,
variable intervala between succesaive presenutiona of
a unit; and (3) longer, variable iiKervals filled with pre-
senutions of randomly-paired stimuli. There was a
direct relationahip b^Ween mean percentages of antici-
pation of the more frequent response members and the
actual percentagea with which those members occurred.
During the last 3 blocks of triala, the interaction of
relative percentagea and conditiona was significant. The
aignlflcance of theae flndinga for the experimental for-
mation of response hierardiiea waa also noted.
New York U. . R Y.
PSYCHOLOGICAL STUDY OP MOTOR SKILLS: PHASE
{,' ,^7 ^wrence f arlin. Rept. on Cooiraa N6 1339 -558.
ii'iJ^^ ,^^P- ^? '■*'■• Technical rept. NAVTRADBV-
CEN 558*1.
Order from LC i|il|3. 6a ph$9. 30 PB 150 639
The present study was concerned with compariiw the
effectiveness of different types of cue on the learning
and retention of 4 simple motor skill (rate of crank-
turning). In addition. It studied the effectiveness of a
preliminary lecture and of Intermittent presentation at
these cues. In all, thirteen condltlona were studied
using as many independent groups at ten subjects each
The results showed no clear superiority in acquisition
or retention for any one of the sii^le cues. There was
• definite suggestion, however, confirmed by one sig-
nificant finding, that the visual cue was generaUy su-
perior in acquisiUon and inferior in retention to the
other cues. The data also suggested that individual
habits ci learning might have interacted with the varlout
types of cue to produce differences in acquisition and
retention. The effect of using various combinations of
cues were also explored. The combinations differed
significantly in acquisition and seemed to divide them-
selves into group0 in which the verbal, verbal -kinaes-
thetic and auditory -kinaesthetic were superior in both
acquisition and retention to the audio- visual and kina-
esthetic -visual gr^nips. No statistically significant dif-
ferences in perfortnance were found from the use at
either a lecture on an intermittent mode of presentation.
Ohio State U. Reaearch Foundation, Columbus
ORIGINALITY IN GROUP PRODUCTIVITY, by Pauline
N. PepinskyandHvoldB. Pepinsky. Annual summary
rept. 16 Nov 58-15 Nov 59, on Contract Nonr-495(15)
]^9%^' ^ '*"* ^^ ^°^- ^'®' ^^ «>■ 8;
Order horn LC mill. 80, ph$l. 80 PB 150 859
r
This research is directed toward the identification and
measurement of behaviors that are Independent and orlg
Inal but contribute qo group productivity; and the deter-
mination of conditictis leading to such behaviors, and th«
experimental testing of such effects. (See also
PB 144 851). ■
L
Group Dynamics. U. of Mich.
Research Center
Ann Arbor.
STUDIES ON DRIVE AND INCENTIVE IN PERCEP-
TION. II. THE EFFECT OF DRIVE PRODUCED BY
PROPNOCEFnVE STIMULATION ON GENERAUZED
RESPONSES TO LOUDNESS AND PITCH, by Arnold H
Martin. Technical rept. no. 6 on Contract
AF 49(638)367 and National Science Foundation Grant
G-4951. July 60, 34p. 32 refs. AFOSR TN-60-1054
Order from LC miSi 00, ph$6. 30 PB 150 638
This study represented an attempt to determine the
validity of the hypothesis that perceived stimulus
intensity is a function of drive multiplied by the physi-
cal stimulus intensity. The effects of proprioceptive
stimulation on generalization gradients along qualiu-
tlve and quantitative dimensions were Investigated
The findings regardieg the quantitative dimension
gra^ents were consiwently opposite to what had been
predicted. The predictions concerning the qualitative
dimension gradients were^n general confirmed. Ex-
pUnatlons both within and outside the D x S framework
were set forth to account for the significant reversal
d the expected effea o* drive on the quantitative
dimension gradients. (Author) (See also PB 146 641)
Rutgeri State U. , New Brunswick, N. I
HOMEOSTASIS THEORY OF a«ALL GROUPS in. by
P. K. Berrien and William H. Angoff. Technical rent
no. 4 on Contract Noor-404(10). Mar 59. 14p
Order from LC ml$2. 40, ph$3. 30 PB 148 268
The homeostatU theory at small groups suggest* ttiat
tf a dlsturhwice occurs which would tend to lower either
Formal Achievement (F. A. ) or the Group- Need Satis-
factions (G. N. S ) some sort at compensatory effect
will occur within conditions predicting F. A. or G N &
»o that these latter criteria will remain stable. This
hypothesis was tested by an analysis at attitude survey
data taken from telephone operators in 32 exchanges
TT>e analysis neither supports nor refutes the hypothe-
sis. Instead It suggests that more predictors are nec-
essary fora definitive test at the hypothesis. (Author)
(See also PB 142 092)
i/
[Small Groups Research Center] Washington U.
[St. Louis, Mo.]
AMBIGUnr AND THE RATE OF SOCIAL ADAPTA-
TION, by Robert L. Hamblln and James A. Wlgglna
Technical rept. no. 1 on Contract Nonr-f816(ll)?
Nov 59. 20p. 10 refs. AD- 228 635.
Order from LC mi$2. 40. ph$3. 30 PB 150 851
A theory involving ambiguity of cues, the disruption at
utility and non-utility discrimination processes and the
rate d social adsputlon as evidenced by the frequency
0* ritualistic and innovative behavior during a period of
disequilibrium was investigated. Two hypotheses were
developed and tested. As predicted, groups who experi-
enced ambiguity of cuea regarding the loss of utl llty during
the dlsequiUbrlum period and groups who experienced
ambiguity of cues regarding presence of utlUty prior to
the disequilibrium period engaged in more ritualistic
behavior and less innovative behavior than groups which
did not experience ambiguity either before or during
disequilibrium. In Addition, there were 2 unanticipated
results of the experiment: (1) Deese's theory that
amttgulty during a learning period inhibits adaptation
by disrupting the discrimination processes was given
some direct suppori; and (2) the data indicate that the
model developed In connection with the theory should be
modified In one respea. as the Inertls phase of this
disequilibrium period was typically and unexpectedly
Interwoven with the search phase. Although statistically
significant, the differences were not huge. The sug-
gestion is that ambiguity may be one of several varia-
bles which may account for variations in the rate at
social adaptation. (Author)
Small Groups Research Center, Washington U.
St. Louis, Mo.
STRUCTURAL FACTORS AND INDIVIDUAL NEEDS IN
GROUP BEHAVIOR, by Richard deCharms and Robert
L. Hamblln. Annual technical rept. on Contraa Nonr-
816(11). Nov 59. 12p. 5 refs. AD- 228 638
Order from LC ml$2. 40. ph$3. 30 PB 150 852
10
Oootents:
Jtruaural factors In group behavior, by R. L. Hamblln
Iiteractlon and coalition patterns, influence, and
group size
The effects of balanced and imbalanced cross linkages
Situational ambiguity and social adaptation
Competence and morale
Individual need in the group situation
Studies in vicarious satisfaction- 1: Aggression and
hostility, by R. deCharms
Studies In vicarious satisfaction -II: Catharsis, self-
esteem and reduction at hostility, by R. deCharma
aodE. J. WlUdns
Studies in vicarious satisfactlon-III: An atten^X to
reconcile experiments I and n, by R. deCharms,
B. J. Wilkins and D. Smith
Studies in vicarious satisfactlon-IV: Task completion
and satisfaction, by R. deCharms and E. J. Wilkins
Status revocability, self-esteem and social conformity
by R. deCharms and M. E. Roaenbaum
Achievement and affiliation motivation In the class-
room, by W. J. Bridgenoan and R. deCharms
The development of affiliation motlvatloo, by H. Gall
and R. deCharms
UtahU. . Salt Lake aty.f
VARIABLES RELATED TD ACCURACY IN INTER-
PERSONAL PERCEPTION,; by Victor R Qlne and ^nies
M. Richards, Jr. Annual rept. no. 2 on Ccotract [Nonr
1288(04)]. 15 Nov 59, 25p, 26 refs. AD-230 538.
Onler from LC ml $2. 70, ph$4. 80 PB 150 475
Seven cross validations and replications were made to
lee If earlier findings suggesting that judging ability wat
to lotne degeee a general trait would hold up. A large
scale testing program was conducted using 295 college
students to determine what the external test correlates
of J\tdglng ability might be. Using patients (and some
sotf) In 2 state mental hospiuls, an attempt to relate
type of diagnosis, age. sex. education, etc. to Judging
alitllry was studied. Comparisons with normals were
also made. An investigation at the behavioral corre-
lates at Judging ability was made by having members of
test groups participate In comprehensive "self" and
"other" rating procedures, and relating these variables
to ludging ability. A comparison of the accuracy of
\\iagments at indivlduali y^. groups (where group mem-
bers collaborate in dedsicjp and jud^ent making) was
slto made. (Author)
Washington U. . St. Louis. Mo. School of Medicine.
THE EFFECT OF ELECTROCONVULSIVE SHOCK
ON MALE ALBINO RATS WITH EXPERIMENTALLY
INDUCED SENSORY C^FiaTS, by John A. Stern and
David G. McDonald. Technical rept. on Contract
Noar-816(06). 1 Dec 59, 20p. 6 refs.
Order from LC mi$2. 40, ph$3. 30 PB 152 101
Previous work has led to the hypothesis that a series at
electroconvulsive shock produces an Increase in reac-
tivity to a variety of environmental stimuli. The evi-
dence for the hypothesis at Increased reactivity is to
date man Inferential than objealve. There has been a
need for a decisive test at this hypothesis and such is
the Intent at the present investigation. (See also
FB 144 182)
Washii^on U. [St. Louis, Mo. ]
EMERCXKF LEAIKRSHIP AND SOCIAL INFLUENCE,
by E. P. Hollander. Rept. on Variables Underlying
Group Expectancies and Leadership, Contract Noor-
816(1^). Dec 59, 21p. 33 refs. AD- 232 745.
Order from LC ml$2.70. ph(4.80 FB 152 111
Attention was directed toward leaders deriving status
from followera who may accord or withdraw it in an
essentially free interchange within a group context.
Group consent was a central feature of the leader -fol-
lower relationship. The effects upon influence accept-
ance produced by the nonconformity to procedural
norms at a usk competent member were tested.
Twelve groups, each composed of male students were
engaged in a task involving a sequence of IS trials re-
quiring group choices from among row alternatives in
a 7 by 7 pay-off matrix. The alleged object was to
anticipate a synem and maximize winnings. A con-
federate, always tl^ same individual, Irrespective at
treatment, was presented in all groups as a fifth
member among 4 subjects. All communication was
carried out through a sound- system of microphones
and headsets. The participants had only aural contaa
with one another. Findings Indicated that the task
competent foUower who conforms to the common ex- •
pectandes of the group at one suge of time may be-
come the leader at the next stage of time. And corre-
spondingly, the leader who fails to fulfill the expect-
ancies associated with his position at Influence may
lose credit among his followers and be replaced by
one ci them.
BKXCX;iCAL SaENCES
California U. , Los Angeles. School of Medicine.
NERVOUS CONTROL OF SHIVERING, by Allan
Henoingway. June 60, 9p. 1 ref . AAL Technical
rept. 58-22.
Order from LCmtfl. 80. Ffa»l. 80 FB ISO 216
Measurements at oxygen consumption rate at shivering
and non- shivering animals before lesion was produced
indicate that the metabolic response of shivering
caused by decreasing rectal temperature by cold and
anesthesia and returning to a warm enviranment is
similar to the metabolic response caused by a cold
environment without decrease of rectal temperature.
In both tests shivering increases oxygen consumption
rate 3.5 to 4.0 times the so-called "basal ' vakie.
Colorado U. [Boulder]
MAGNETIC SUSGEPTBILITY OP SINGLE BIOLOGI- '
CAL CELLS, by S. J. Gill and M. Downing. Annual \
progreas rept. for 1 June-1 Dec 59 on Contraa Nonr-
1147(08). 27 Nov 59. 7p.
Order from LCmtf 1.80. phi 1.80 PB 150 527
A method for calibrating the force properties of an
inhomogeneous magnetic field was put into operation.
The method is one used in molecular beam work, and
is based upon determining the deflection of a quartz
fiber, to which a piece of platinum or bismuth wire has
been atuched. The magnetic field may be probed and
nupped by such a device. An electromagnet which '
li
was designed to produce an inhomogeneoua field waa
calibrated with the test probe. A simple optical aya-
tem and sample container were incorporated into the
magnet. Particles at the range of 8 to 30 microns have
been examined. Some preliminary tests on suspended
blood cells have indicated that measurements are
feasible, buf a constant current supply is requlrfed as
the deflections of the blood ceUs is conalderably slower
than that of the latexes. Improvemeia at the observa-
tion of the particles has proceeded in a separate
fashion. A phase contrast microscope was acquired
and is being adapted to observe a smaU region between
the magnet pol«a. Since apadal requirements severely
Umlt the size d the magnet which can be easily placed
into the microscope, a design erf a permanent magnet
has been consiclered and buih for use with the micro-
scope. Some prebminary tests have been made on the
field gradient product and have shown values of 2 x 10^
Karollnska Inabtutet, Stockholm (Sweden)
CONTINUED STUDIES ON NEW AND IMPROVED
ELECTROPHORETICAL METHODS FOR THE ISOLA-
TION AND PURIFICATION OF BIOLOaCALLY AC-
TIVE COMPONENTS OF BACTERIAL CELLS, by
Berndt Malmgren. Final technical rept. for Nov 5«-
Nov 59 on Cortraa DA 91 -591 -EUC-948-OI- 1059-59
[1959J 17p. 3 rels. AD- 231 368.
Order fran LC |ni$2. 40, ph$3 30 PB 148 269
Large scale cultivation o* virulent hemopWlua pertua-
sls was carried out. Disruption ot the cells in the
frozen state in a modification at Hughes press followed.
A new method for the removal of water from protein
solutions was devised, based on the capacity at cmt-
boxymethylcellulose (CMC) In the dry state to attraa
water across a cfalysis membrane. Cells could be
brought into solitlon completely because the residue
remaining after salt extraction could be dissolved in
water to form a atable. lyophlle suspension. This
residue amounted to about 1/5 of the dry weiriit c* the
starting material. It had an immuno^c^iSty
COTresppndlng to at least 505^ of that which could be
demonstrated if the material was tested in the common
vaccines form. The fraaion which was lipopoiysaccha-
ride-protein in cliaraaer could be freeze-dried without
loss in activity o* solubility. Neurotoxic activity was
demonstrated In a procdn fraction which did not contain
nuclrtc adds. Chromatography of the fraaion showed
^ the neurotoxic activity was concentrated in two
distinct peaks Both peaks also contained some
dermatonecrotlc activity. The tendency of the neuro-
toxin to combine frith other proteins and perhaps alao
wlUi nucleic aclda makes Its isolation rather difficult
in long distance electrophoreals the neurotoxin was
adsorbed by the ceUuloee and/or Inactivated. (Author)
Pacific Science Board, National Research CounclL
Washington, D. C. v>«™^
THE VEGETATION OF MICRONESIA. PART 1. by
F. R. Fosberg. Rqjt. on Scientific Investiaatioos In
Kflcronesia. 1949-, Coqtraa N7onr-291(54). 8 Dec 59.
l;76p. 43 refs. SD4 rept. no. 25; AD-236 461.
Order from LC ml|$8. 10, ptx$27. 30 PB 147 100
Comencs: I
Essay on the nature of vegetarlcxi
General descriptloti of Microneslan vegetation
Location and nature of Micronesia
Major climatic and topographic features
Map showing cUmadc and geologic lines
Classification cf vegeution
Outline of Mlcrooesian vegetation
Vegetation qrpes as practical indicators
Gaicral description of vegeution types
Mangrove formation
Strand
Vegetation of raised coral limestone
Vegetation of rough lava flows
Casuarlna forest
Coconut plantations
Vegetation cf coastal plains
Lower primary forest
Secondary forest on slopes
Montane rain forest and cloud forest
Dwarf vegetation on open crests
Savanna or grassland vegetation
V^etation of the Marianas Islands
The Northern Marianas— general
The Southern Marianas— general
General picture of Guam vegetation
Anatom)^ and Physiology
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska
CARDIOVASCULAR EFFECTS OF REFEEDING
STRESS FOLLOWING STARVATION V. THE EFFECTl
OF REFEEDING PURE O^UCOSB, by B. Conner ^
Johnson and Vincent Florlca. Jan 59. 22p. 4 refa Tet*
nlcal note AAL-TN-59-18. ' ' ^
Order from LC mi$2. 70, phK 80 FB 152 028
This note presents the results of feeding pure glucose
of feeding glucose plus sodium chloride, and of feedlM
a diet that Is high In glucose to pigs starved for a tool
period. Cardiovascular changes occurring during wjors
(PB ImSS?-'"''* been presented in s previous repon
Arctic Aeromedlcal Lab. . Ladd AFB. Alaaka.
CARDIOVASCULAR EFFECTS OF REFEEDING
SntESS FOLLOWING STARVATION VL STARCH RE
FEEDING VERSUS GLUCOSE REFEEDING. by
M. S. MameeshandB. Connor Johnson. Oct 59, lip.
5 refs. Technical note AAL-TN-59-19.
Order from LC mlJ2. 40, ph$3. 30 PB 152 029
Thla note presents the results of feeding two carbohy-
drates differing In digestibility to pigs starved for s
short period (6-8 days). Cardiovascular changes occur-
ring during pure-glucose refeeding hare been presenisd
in a prevloua report (PB 152 028).
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska.
CARDIOVASCULAR EFFECTS OF REFEEDING
STRESS FOLLOWING STARVATION VIL REFEEDING
FOLLOWING SHORT-TERM STARVATION PERIODS
£.?•«?* Sr^*; ^ ^ Mameesh, and B. C Johnson.
May CO, 15p. 4 refs. Technical note AAL-TN-60-8
Order from LC ml$2. 40. ph$3. 30 PB 152 (130
U
This report c<incem8 the effects of refeeding with pure
protein, pure fst, and glucose plus sodium chloride fol-
lowing short-term (6-8 days) survatlon perloda. The
four pigs which have been described In previous reports
were used In these experiments. (See also PB 150 024,
IB 152 028. PB 152 029). -
Arctic Aeromedlcal Lab. , Ladd AFB. Alaska.
CARDIOVASCULAR EFFECTS OF REFEEDING
STRESS FOLLOWING STARVATION Vm. LONG-TERM
EFFECTS OF FEEDING- REFEEDING EPISODES, by
C. S Snalth. M. S. MameeshandB. C. Johnscm. May60.
I6p. 2 refs, Technlcsl note AAL-TN-60-9.
Order from LC inl$2. 40. ph$3. 30 PB 152 031
»
This report Is concerned with the effects of jHire nutrient
refeeding following a long-term starvation; the response
to increased level of nstural diet following the pure nu-
trient feeding phase; some general aspects of rq>ested
stsrvstlon- refeeding episodes, and the possibility of
"carry over" effects from episode to episode; and the re-
sults of gross* examination of the cardiovascular systems
of the pigs, post mortem. (Author). (See also
FB 152 030)
Artie Aeromedlcsl Lab. . Lsdd AFB. Alaska.
THE CONSTRUCTION OF A SMALL MERCURY
STRAIN GAUGE, by C. J. Eagan. Rept. on PubUc
Health Service Training Grant HTS 5147 and Contrsct
AF 41(657)216. Ai« 60, 10 refa. Technical note AAL-
TN-60-14.
Order from LCinl$l. 80, ph|l. 80 PB 152 033
The construction of a small, low- tension, mercury
strain gau^e is described. Dimensions of the active per
tion are ^jpraxlmately 45 mm In length and I. 25 nun in
diameter. It can be used for essentially Isotonic mma-
urement of physiological change in linear dimension of
sny part to which it can be securely attached; it la par-
ticularly suitable for plethysmogrsphy of the human
finger and the rabbit ear. If connected in a suitable cir-
cuit, the following specifications can be schleved: (a)
high sensitivity; changes In length of the gauge of 1 noi-
cron can be recorded; (b) useable under conditions of
changing temperature or pressure within the whole
range of these environmental f*f^* which tissue can
endure. (Author). »
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska.
EFFECT OP COLD OH THE ISOLATED PERFUSED
MAMMALIAN HEART, by Benjamin G. Covino and
Adam Resendez. June 60, 29p. 20 refs. Technical
rept. 57-38.
Order from LC mi$2.70, p«4.80 FB 150 218
The effect of cold on the properties of cudisc tissue
waa studied in the intact and isolated heart of the
rabbit. A prdgreaslve depression of rhythmldty, con-
ductivity, and excitability occurred aa the heart tem-
perature was lowered. Confractlle farce increased
significantly aa temper«rure fell to 20°C. Below this
point, the force of coocraction diminished sharply.
All electrical and mechanical activity ceased »t s
mean temperature of 14. 1°C. in the Isolated heart and
15. 400. in the inuct rSbfalt. Coronary flow was re-
duced by a faaor of 57%-
Army Chemical Research aqd Development Labs. ,
Army Chemical Center. Md.
BYE PROTECTION AGAINST HIOI-SPEED MISSILES,
by George M. Stewart. Rept. for Oct 56-May 60 on
Wound Ballistics. July 60, 24p. 3 refs. Technical rept.
CRDLR X07 .
Order from LC mlJ2. 70, phM. 80 PB 152 001
This report desls with the resistance to penetration of
the rabbit eye and lenses by spheres, cubes, snd cylin-
ders in the wel^ rsnge of 4. 1 to 14, 645 mg. Rabbits
vsrying in sge from 5 to 7 months were KUed and the
eyes removed snd mounted in gelstln for ballistic eval-
uation. Lenses Included unhest-trdtted glass, hest-
trested glass, laminated glass, snd plastic, CR-39
Allyl casting. Lenses were in 2-bsse curves: 9 and 12
and three thidmesses: 2.5 mm, 3.0 mm, and 3.5 nun.
Lenses under test were mounted in s specislly con-
struaed rubber Jig. Bssed on test results, it is sug-
gested that under those working conditions In whidi die
eyes may be subjected to Impaas of very small mis-
siles, of less than 2-mm diameter, that protective
lenses made of either plsstic. laminated, or unheat-
treated glass be used- For the greatest over-sll
protection erf the eyes, plsstic lenses would seem to be
the first choice. (Autbor)
Army Chemical Research and Development Labs. ,
Army Chemical Center. Md.
PRELIMINARY TEST OF APPARATUS FOR RE-
CORDING INHALATION "DURING THE MASKING RE-
ACnCW IN THE FIELD, by W. V.Blevlns,
H. M. Frankel, and P. N. Craig. Rept. for Aug 59 on
Basic snd Allied Physiology. July 60, 30p. 15 refs.
Technlcsl rept. CRDLR 3013.
Order from LC mi$2.70, ph*4.80 FB 152 002
The first 5 units of the breath -recording system de-
veloped for the CARAMU program were tested on 7
days wldi 5 enlisted men from the medical voluaceer
deucfament. Of the 35 trials, 21 complete records
were obtaAied. In general, the recording system was
satisfsctory, and the failures srose mialnly from the
remote-coocrol components. The apparatus did not
Interfere with the masking resctlon. Both good and
bad control of breathing during the nutsklng reaction
are illustrated. Volumes of individual breaths hsve
been tabulated and calculations of dose inhaled made
from aample concentration histories. (Author)
Aviation Medical Acceleration Lab. , Naval Air
Development Center, Johnsville, Pa.
HORMONAL DETERMINANTS OF MAMMALIAN"
TOLERANCE TO ACCELERATION STRESS, by
B. David Polls and Anne Zella. Rqlt. no. 2 on ProJ.
MR005. 15-0002.7; Pro|). TED ADG RS-7045 (5915-M).
12 Aug 60, 15p. 7 refs. NADC-MA/-6025.
Order from LC mi$2. 40, ph^. 30 PB 150 44?
The pituitary-adrenal hormonal axis has been impli-
cated as a critical factor in the survival of the rat to
acceleration stress. Tbe physiological sndpolnt for
the tolerance of animals to high positive acceleration
stress was obtained by determining the dme to reduce
the heart rate from eight to two beats per second at
20 G. ynxh dils technique a significant Increase
(300 percent) in the surylval time of rats to 20 G was
13
found following bvpqphysectomy. A significant loss
(60 percent) erf tcjerance to hlgji acceleration stress
was found in adr«nalectomized rats. The procedures
of hypophysectomy and adrenalectomy essentially
cancelled the effect d each operation alone in the rat
to yield an animal appraxiniately similar to the nor-
mal rat in its ability to tolerate acceleration. Possi-
ble mechanisms for these effects are ctfered.
(Author)
Aviation Medical Acceleratlco Lab. , Naval Air
Development Ce<iter. Johnsville. Pa.
NADC BIOLOGICiL INSTRUMENTATION SYMPO-
SIUM OF 10 DECEMBER 195«. by R. Jensen.
J. J. Gordon and cXhers. Lener rept. no. 6 on Prolects
MR 005. 15-0002. J, TED ADC AE 1412. 1 and TED
NAM AE 1403.1. ,5 July 60. lOp. 1 ref. NADC-MA-
L6018.
Chrder from LCmisl. 80, ph$ 1.80 PB 150 439
The present communication constitutes a sinunary at
the Investigations carried out on three types o*
respiration sensor systems which have been developed
and evaluated at the Aviation Medical Acceleration
Laboratory (AMAL) during the past nine months.
Aviation Medical Acceleration Lab. , Naval Air
Development Cemer, Johnsville, Pa. /
NADC BIOLOGICAL INSTRUXffiNTATION SYMPOSIUM
OF 10 DECEMBER 1958, by R. Jensen, J.J. Gordon and
others. Letter rept. no. 7 on Projects MR 005. 15-
0002. 2, TED ADC AE 1412. 1 and TED NAM AE 1403. 1 .
13 July 60. 8p. 7refs. NADC-MA-L6021.
Order from LC mil 1.80, ph$ 1.80 PB 150440
This is a preliminary report at teats carried out on the
Aviation Medical Acceleration Laboratory (AMAL) Bio-
instrumentation package during which six channels were
transmitted on an assigned frequency al 232. 4 mega-
cyclea from the pacJcage mounted in the AMAL centri-
fuge gondola to the AMAL monitoring and recording
system. *
California Inst, of Tech. , Pasadena,
FACTORS STIMULATING PRODUCTION OF HEMO-
GLOBIN AND RED CELLSw Final rent, on Contract
Noor- 220(09). 23 N<nr 59. 4p. 5 refs. ^^^'^^
Order from LC mi$a. 80. ph$l. 80 PB 150 854
Since the last progress report the foUowing has been ac
compllshed. Unboiled plasma, whether normal or
anemic, provokes la heterolofous apecies the formation
of antibodies and thla process is associated with a drop
in hemoglobin and red cell count and thus, when anemic
plasma is used. It erythropoietic effect is masked.
Boiling (even heating to 75°) destroys the antigenic char-
acter of the pUsma. even tfiough much protein may re-
main in solution or suspension. The erydiropoietic fac-
tor resists boiling and it was found (in boUed pUsma fU-
trates) diat It had no species specificity. Anemic rabbit
plasma filtrate was Ictlve in rats and mice; dog plasma
fUtrate was active iri mice. (See also PB f 38 650)
14
I
Institute for Applied Experimental Psycholocy.
Tufta U. , Medford. Mass. •~~^» r
THE FEASIBILITY OF USING THE EYE AS A
SOURCE OF CONTROL SIGNALS IN TRACKING, by
Philip B. Sampson, Paul D. Coleman, and Edwin H.
Elkin. Rept. on [Contract Nonr- 494(16)1 Dec 59, 43d
43 refs. AD- 231 516. ^'
Order from LC ml$3. 30. ph|7. 80 PB 152 138
The idea that eye movements could be made to produce
signals which could be used for machine control pur-
poses was considered from the point of view of its fea-
sibility. Findings indicate that (1) there are sltuationa
In which the use of the eye as s control mechanism
would appear to be advantageoua; (2) extremely fine
eye movements can be detected by the more sophisti-
cated laBoratory techniques; (3) a class of eye move-
ment detection devices, called mechanical- electrical
techniques, seem to offer some advantages for the con-
struction of a practical general purpose eye movement
control; (4) what is known of the tracking characteris-
tics of the eye is not inconsistent with the notion that
the eye could be used as a tracking device; (5) a prac-
Ucal eye movement control device should impose as
little restriction to the movements of the operator as
possible; (6) best tracking performance with an eye
movement control would probably be found for a zero-
order, lag-free system with a pursuit type display; and
(7) it is doubtful that the advantages found with manual
control systems for first and second order controls,
compensatory displays, quickening and manipulation of
the C/D ratio could be realized with an eye movement
control. (Author)
Oregon U. Medical School. Portland.
TISSUE GLYCOCEN SYNTHESIS IN ADRENAL-
ECTOMEED RATS FED GLYCINE -CONTAINING
DIETS AND GIVEN HYDROCORTISONE, by W. R. Todd
and Mariloulse Allen. May 60. 7p. 8 refs. AAL Tech-
nical rept. 58-23.
Order from LCmlJ 1.80, ph$ 1.80 PB 147 744
Adrenalectomized rats were fed diets with or without
added glycine for 36 hours. Four hours later they were
made to swim in 140C. water (the stress). Uver and
muscle glycogen determinations at this time showed the
levels to be essentially the same in the two groups of
rats. When 1 mg. of hydrocortisooe per 100 gm. body
weight was given twice a day for 2 days prior to the
stress, the glyclne-fed animals showed nearly twice as
much liver glycogen as the animals prefed the control
diet. Muscle glycogen coocentrationa were not differ-
ent. A<kreaal hormone, glycine, and stress are re-
quired to demonstrate the •protein effea" of glycine. It
now appears, however, that increased adrenal hormone
is not a prerequiaite. (Authcn:)
■ •■■ I- ■
PfcnnsylvanU U. School of Medicine, Philadelphia
METABOLIC AND THERMAL RESPONSE TO CHRONIC
MODERATE COLD EXPOSURE, by H. T. Hammel.
June 60, 47p. 14 refs. AAL Technical r«pt. 57-51.
Order from LC ml$3. 30. ph^. 80 PB 150 568
Measurements of die diermal and ntecaboUe responses
of die AustralUn Aborigines exposed to moderate cold
itress have shown d»at there exists a small lait Impbr-
tant difference between these subjects and white controls.
During an exposure to cold while sleeping at night,
whites Increased their heat production by 25% to 30%
(averaged over the period of shivering) by shivering in
bursts, whereas the metabolism of the natives declined
continually throughout the night giving a Qiq of 2. 5.
Without metabolic compensation, the mean body temper-
anire of the native fell continually during the iiight to a
temperature 1° C, lower tlun the whites. The meail
body temperature of the natives fell more than that of
tfje whites because both the recttl and the average skin
temperatures fell more. During the fall, cold acclimati
ration was Induced in eight Norwegian young men by hik
Ing and sleeping in the mounuins, with light summer
clothing during the day and a single blanket -with wind
cover during the night, air temperature near freezing.
Measurements of the thermal and metabolic responses
of the acclimatized subjects and controls, while sleep-
ing during moderate cold exposure, revealed that the
acclimatized subjects mainulned a higher metabolic
rate than did the controls. Because of the higher meta-
bolic rate of the acclimatized gtoup, the skin tempera-
tures of these men were malnuined higher than the
skin temperatures of the controls. The rectal temper-
atures of the controls and acclimatized men were not
different.
Pnmsylvania U. School of Medicine, Philadelphia.
THERMAL AND METABOLIC RESPONSES OF THE
AUSTRALIAN ABORIGINE IN SUMMER WHILE EX-
POSED TO MODERATE COLD LJURING SLEEP, by
R T. Hammel. July 60, 41p. 19 refs. AAL Tedinlcal
rept. 58-21.
Order from LC ml$3. 30, ph$7. 80 PB 150 572
Measurements of the thermal and metabolic responses
of the central Australian Aborigines exposed to moder-
ate cold during sleep were repeated during the summer,
and have shown that the small but important differences
between the central natives and control whites exist in
the summer to the same extent as ^ the winter.
(See also PB 150 568)
University Hospitals, Iowa City, Iowa.
DIMENSIONAL ANALYSIS OF COCHLEAR MODELS.
by JuergenTonndorf. Apr 60, 9p. 16 refs. APSAM
rept. 60-42; AD- 238 114.
Order from LC ml$1.80. pb|1.80 PB 152 118
An attempt was made to apply the principles of dimen-
sional analysis to cochlear models. Dimensional
analysis of displacement amplitudes In the model In-
volves: (1) correction for the ratio of Ic differences;
and (2) correction for frequency differences. Data
ivere obtained which lend support to the hypothesis of
the hydrodynamic origin of intracochlear dlstortloo.
University of Southern California. School of Medicine,
Los Angeles.
THE EFFECT OF INSUUN ON THE THYROID
GLAND AND ITS INFLUENCE OH HEAT REGULA-
TION, by Boris Catz, Ernest Gelger. and Herlberto
Thomas. May 60, 12p. 20 refs. AAL Technical
rept. 57-47.
Order from LCini$2. 40, pta$3. 30 . FB ISO 219
Wlstar strain rats, male adults, weighing from 90 to
125 grams, received 0.5 units of regular insulin twice
a day for 8 days while at normal temperature
(240-260C. ), or In the coW room (3®C. ). In li
libitum feeding at normal temperature, the insulin-
treated animala gained significantly more weight than
did the cootrola, and revealed a significant hyperplasia
of the thyroid gland. Probably due to increased food
Intake, die cold-exposed animals receiving insulin did
not show the initial loss of weight usually observed
after exposure to cold. Their thyroid glands were less
hyperplastic than those of the controls. In paired
feeding experiments, the weight curve of the coM-
expoeed insulin animals was similar to that of the cold
controls. The thyroids of the insulin-treated, cold
animals, however, in spite of restricted food intake,
were less hyperplastic than those of the pair-fed
control rats. (Author)
University of Southern California. School of Medi-
cine, Los Angeles.
A STUDY OF THE CARDIOVASCULAR ADJUST-
MENTS TO THE INCREASED STRESS PRODUCED
BY NARROWING OF THE ABDOMINAL AORTA, by
Douglas R. Drury. June 60, 23p. 4 refs. AAL Tech-
nical rept. 57-33.
Order from LC ini$2. 70, ph$4. 80 PB iSO 563
A study was made of the cardiovascular adjustments
that occur in rabbits after narrowing the aorta just be-
low the coeliac axis. The relationship between Biie of
orifice, and (1) survival time. (2) development of hy-
pertensi6n, and (3) cardiac hypertrophy were deter-
mined. An orifice of diameter 1. 65 nam, causes hy-
pertension and congestive failure in 2 to 3 weeks in
most animals. A diameter of 2. 0 nmi. leads to hyper-
tension with cardiac hypertrophy. The performance of
the hearts of these animals was measured by deter-
mining the maximum pressure they could sustain. The
hearts from the experimental animals had increaised
performance and this was related to the cardiac hy-
pertrophy. The peak performance was not changed by
ctwling the heart. Cardiac arrhythmias were frequent
In the hypertrofihled hearts. (Author).
Wisconsin U. School of Medicine, Madison.
cgmparahvb effects on anesthetic agents
ON CARIXAC IRRlTABILnY DURING HYPOTHER-
MIA, by John B. Stelnhaus, Karl L. Slebecker, and
Junes R. Kimmey. May 60, ISp. 8 refs. AAL Tech-
nical rept, 58-24.
Order trstm LC mi|2. 40. ph$3. 30 PB ISO 215
The effect of four anesthetic agents administered
singly or in combination on the incidence of ventricular
fibrillation in dogs during hypothermia was investi-
gated. Arrhythmias were initiated with the application
of mechanical stimulation in the form of cardiac mas-
sage. At 27** C there were no instances of fibrillation
despite periods of high p002 and hypoxia. At lower
temperatures cyclopropane anesthesia resulted in the
highest incidence of this serious arrhythmia. Tlilo-
pental-nitrous ootide anesthesia supplemented with lldo-
calnc noarkedly reduced the occurrence of dds arryth-
mla; however, cardiac failure occurred frequently.
At a temperature of 22-230 C failure was markedly
reduced when Ildocalne was used as a supplement
(Aut)»or)
15
Biochemistry
Arctic Aeromettlcal Lab. . Ladd APR Alaska.
BLOOD CHailSTRY OF THE COLD ACCLIMATIZED
RAT. n. CROSS METABOLITE AND PHYSICAL
CHANGBS. by J*n P. Haimon and David W. Young.
Apr 60, 33p. 32 refs. Technical rept. 607^6.
Order from LC «ii$3. 00. ph$6. 30 FB 150 578
I
The gross blood compotltion of adult, nule, Sprague-
Dfcwley rats was determined under control conditions
and conditions of prolonged cold exposure. In addition,
the effects al fasting were determined under each at
these envlronme«ts. It was observed that cold expos-
ure Induced a slight, but significant. Increase in hemo-
globin levels, but had no effect on the hematocrit.
Fasting, on the other hand, did not alter the hemoglobin
concentrations at either the control or the cold -exposed
animals, but it did produce a slight lowering of the
hematocrit. Cold exposure also resulted in a plasma
, dilution as indicated by a significant Increase in plasma
water, and significant decreases in plasma spjeclflc
gravity and plasr«a protein levels. Fasting was ob-
served to superimpose a further reduction in plasma
protein levels un<ler both control and cold-exposed con-
ditions. Measuraments of the levels of various metab-
olites indicated tkat the levels at blood glucose and
total plasma lipids were unaltered by cold exposure but
that each was significantly reduced by fasting. On the
other hand, it was observed that cold exposure led to
significant increases in the non-protein nitrogen, phos-
pholipid, cholesterol, and ketone levels of non -fasted
animals. Superimposed on these changes, fasting pro-
duced a decrease in the levels of non-protein nitrogen
and phospholipids and an increase in the level d ke-
tones, but it had no effect on the level of cholesterol.
Significant differential effects of fasting on the two en-
vlronmenral groups were found for non-protein nitro-
gen, phospholipid, and ketones. Thus, fasting in the
cold-exposed aniifuliL caused greater reductions of
non-protein nitrogen and phospholipids and a smaller
increase in blood ketones as compared to controls.
(Author) (See als^ PB 150 577)
Arctic AeromedicaJ Lab. . Ladd AFB, Alaaka.
THE EFFECT OP COLD ON THE WEIGHT, FOOD
WTAXE, AND ACETYLATING ACTIVITY OF PAN-
TOTHENIC ACID* DEFICIENT RATS, by D«vld A.
Vaughan and Luclle N. Vaughan. Apr 60, 15p. 11 refa.
AAL Technical rept. 59-23. «.
Order from LC mH2. 40. phJ3. 30 FB 147 745
. Growth, food intaie, and acetylating activity were
• measured in rata kept at 5° Cand 25° C. while receiv-
ing a pantothenic •cld-deflclent diet aupplemented with
0. 5. 1. 5. and 5. 0 pg calcium pantothenate per gram of
food. Respective mean weight changes at diese levels
d calcium pantothenate were ♦IS. ♦SO, and ♦lOO gm.
for the warm rata and ♦2, ♦U, and ^83 gm. for the
cold rats. Food intake increased as the level of cal-
cium pantothenate increased, but the difference in food
Intake fcietween the warm and cold rats remained con-
stant at all levels of calcium pantothenate Acetylating
activity was not affected by exposure to cold, although
It decreased with decreasing dietary levels of csicium
pantothenate. (Author).
16
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
INTERMEDIARY GLUCOSE METABOLISM IN THE
COLD ACCLIMATIZED RAT. by John P. Hannon.
Apr 60, 28p. 30 refs. Technical rept. 60-15.
Order fr/aro LC ml$2. 70. phK 80 PB 150 213
"IJie efl4et» (^.3-4 weeks' cold exposure (5 1°C ) on
the a($ivltl4« at glucoklnase. glucose- 6-phosphause.
gluco8e-6-pbo€phate and 6-phosphogluconic dehydro-
genases, total phosphorylase, phosphoryiase a aixl b,
phosphoglucomutase and pyruvate formation over the
terminal glycolytic span of enzymes were assayed.
Various shifts in the pattern of intermediary hexose ,
meubolism as a result of cold exposure are discussed.
(Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
TISSUE ENERGY METABOLISvl IN THE COLD
ACCLIMATIZED RAT, by John P. Hannon. Apr 60.
33p. 33 refs. Technical rept. 60-14.
Order frotn LC ml$3. 00, ph$6. 30 PB 150 577
Data are given relating the effect of duration of cold
exposure on liver slice and whole body carygen com sump-
tion of laboratory rats. Dan are also presented on the
effect of cold exposure on various liver oxidase ac-
tivities, oxidative phosphorylation and adenoslnetri-
phosphatase aaivities. The comparative study of elec-
tron transport components in liver and muscle is given.
These data are discussed in relation to the develop-
ment of nooshivering thermogenesis and the cellular
metabolic control mechanisms in the cold acclimatized
animal. (Author)
Aviation Medical Acceleration Lab. , Naval Air
E)evelopment Center, Johnsvllle, Pa.
IMMUNOCHEMICAL STUDIES ON MITOCHROME, by
E. R. Stlehm. Rept. no. 10 on ProJ. MR005. 15-0002.7;
ProJ. TED ADC RS-7045-5915M. 11 Aug 60, 19p.
7 refs. NADC-MA-602a
Order from LC ml$2. 40, ph$3. 30 FB 150 441
A precipitating antibody to rat liver mltochrome was
prepared by immunizing rabbits using the Freund adju-
vant technique. This antibody was charaaerlzed by
quantitative precipitin techniques and was found to be
directed against a small portion of the mltochrome.
Albumin and cytochrome c, which have been shown to
interact with mltochrome, do not inhibit its immuno-
logic activity, demonstrating that the metabolic and
the Immunologic sites of mltochrome are distinct.
The antibody has the ability to decrease cytochrome
oxidase activity of whole mitochondria, but has no effect
on the aaivlty of purified cytochrome oxidas e, s ugges t-
ing the non-identity of mltochrome and inactive cyto-
chrome oxidase, contrary to a recent report. (Author)
Illinois U. Coll. of Medicine, Chicago.
THE EFFECT OF ENVIRONMENTAL FACTORS ON
THE METABOLISM OF PLASMA PROTEINS. L THE
MEASUREMENT OF TURNOVER RATE, by Richard J.
Wlnzler. June 60. 18p. 14 refs. AAL Technical
rept. 57-35.
Order from LC mi$2. 40, ph$3. 30 FB 150 565
The turnover rates cf the electrophoretlc plasma pro-
tein fractions were determined for normal adult rats.
When the isotopically labeled plasma protein was used
as a source of tracer labeling, accurate measurements
of the pool size, half,- life, and replacement rate of
albumin and gamma glc^lin were possible. Certain
technical difficulties are still present in the turnover
rate determination of the alpha and beta globulins. It
was also shown that the label of the albumin was incor-
porated into the various globulins, and that the label of
a globulin was Incorporated Into albumin. (Author)
Illinois U. Coll. of Medicine, Chicago.
THE EFFECT OF ENVIRONMENTAL FACTORS ON
THE METABOLISM OF PLASMA PROTEINS IL THE
EFFECT OF THE LEVEL OF EHETARY PROTEIN ON
THE TURNOVER RATE OF SERUM PROTEINS, by
Richard J. Wlnzler. June 60. 19p. 27 refs. AAL Tedj-
nical rept. 57-54.
Order from LC mi$2. 40, ph$3. 3^ PB 150 570
The turnover rates of serum albumin and the four elec-
trophoretlc fractions of senim globulins were deter-
mined In rats maintained on low (0-5^, adequate (12^,
and high (30-40%) protein diets. It was found that the
turnover rate of serum albumin Increased as the pro-
tein intake increased, i. e. 4. 1 days, 3. 8 days, and 2. 1
days for animals on low, adequate, and high protein
diets, respectively. The turnover rates of the four elec-
trophoretlc fractions of serum globulins were unaffected
by the level of dietary protein. Furthermore, the pro-
tein pool size was foiind to be dependent upon the size of
the animal rather than upon the protein intake. (Author)
(See also PB 150 565)
Oregon U Medical School, Portland.
MAINTENANCE OF CARBOHYDRATE STORES DUR-
ING STRESS OF COLD AND FATIGUE IN RATS
PREFED DIETS CONTAINING ADDED GLYQNE. by
W. R. Todd and Marilouise Allen. June 60. ISp. 8 refs.
AAL Technical rept. 57-34.
Order from LC mi$2. 40. ph$3. 30 PB 150 564
Previous dau Indicated that rats prefed a diet contain-
ing 10 percent added glycine showed higher levels of
glycogen storage during the stress of fasting or of ad-
ministered insulin than did animals fed the same diet
but without added glycine. The present report indicates
that the glycine feecUng allows increased carbohydrate
storage during the stress of cold (8°C. in cold room)
and of cold plus fatigue (swimming in U^C. water).
The trichloracetic acid- soluble fraction of liver glyco-
gen is quite labile toward the stress of swimming, and
leaves the liver to a greater extent under the stress of
insulin. Glycine feeding tended to lessen the loss of
the soluble fraction under the latter stress. The data
are taken as additional support for an earlier postulate
that glycine prefeeding stimulates glycogenesis during
Stress -probably mediated through adrenal cortical
action. (Author) !
St. Luke's Hospital. New York.
PROTEIN AND AMINO AQD NUTRITION, by Anthony
A. Albanese (St. Lulce's Convalescent Hospital). Annua]
progress rept. for 1 Jan-31 Dec 59 on Contract Nonr-
1167^). 15 Nov 59, 15p. 10 refs. AD-229 379.
Order from LC mi$2. 40, ph$3. 30 PB ISO 471
Contents:
Protein needs of young children
Specific amino add needs of Infants
Cereal food studies
White bread studies
Specific amino acid needs of the aged
Nutritional effects of hormones
Anabolic steroids
Corticoids
Factors influencing blood cholesterol
Investigations on body composition
Biochemical methods
Organizational activities
Tufts U. School of Medicine, Boston, Mass.
LIPOGENESIS FROM CARBOHYDRATE IN THE NEG-
ATIVE CALORIC BALANCE STATE INDUCED BY EX-
POSURE TO COLD L GLUCOSE LIPOGENESIS IN
RATS IN NEGATIVE CALORIC BALANCE, by
E. J. Masoro, Carmen L. Asuncion and others. Apr 60,
lOp. 9 refs. AAL Technical rept. 57-31.
Order from LC ml$l. 80. ph$l. 80 FB 147 743
The ability of rats exposed to 0-2° C. for 1 or 2 days
to Incorporate dietary glucose Isotoplc carbon into
fatty adds was studied. Under these circumstances, in
spite of a large intake of food, there is a loss In body
weight and fatty acids. Whether calculated on a per-
centage or on an absolute basis, there is under the con-
ditions a considerable incorporation of the label into
fatty acids. It is concluded that not only in the steady
sute, but also In a state of negative caloric balance,
lipogenesis is one of the obligate^ pathways of carbo-
hydrate metabolism. (Autlior). ^
University of Southern California. School of Medi-
cine, Los Angeles.
THE NITROGEN CONTENT OF THE GASTROINTES-
TINAL TRACTS OF RATS DURING THE ABSORP-
TIVE reRIOD. by E. Geiger. L. E. Human, and
M. J. Middleton. June 60, 9p. 8 refs. AAL Technical
rept.' 57-48.
Order from LC nU$l. 80, ph$l. 80 PB 150 567
By feeding rats protein-free test meals and determi -
ning the nitrogen levels in the gastrointestinal con-
tents, it has been found that the basal level cd endoge-
nously supplied nitrogen is about 5 mg. after 1 1/2
hours, and that this level is unaffected by protein de-
pletion. On feeding skim milk powder. 22-27% of the
ingested protein disappears from the gastjpolntestlnal
tract within 3 hours. Under the conditions of these ex-
periments, any homeostatic action of the gut in supple-
menting amino acids to deficient protein meals is neg-
ligible. (Author).
Washington U. . Seattle. School of Medicine.
THE CHANGES IN THE RED CELL AND PLASMA
VOLUMES OF THE RAT AND OF ITS INMVIDUAL
TISSUES AND ORGANS DURING ACCLIMATION TO
COLD by Newton B. Everett. Rept. on Contraa
AP 41(657)104. June 60, 13p. 12 refs. AAL Technical
rept. 58-18.
Order from LC mi$2. 40, ph$3. 30 FB ISO 230
17
The red cell and platma volumes at the toul nt and
of In Indlvidu&l tissues and organs have been deter-
mined for. animals exposed to 5oC. for 4 hours, 24
hours, an|Ei2weeks. In addition, the tissue hemato-
ive been
-Ubeled
„ Intraven-
ously and after nrixlng; the rats were frozen In liquid
nitrogen. The orgatu and tissues were removed In the
frozen state, assayed for radioactivity, and blood cell
and plasma volumes were calculated on a unit weight
basis. Signlficanc changes in blood cell and plasma
volumes were observed for the total rat and for moat
at the Individual organs. The toul body blood volume
Increased 18% In the 2 -week group, in general, the
somatic parts had Lncreaaed blood volumes whereaa
die vlacerai parts had decreased volumes. (Author)
Pathology
Arctic Aeromedlcal Lab. , Ladd APR Alaska.
CLINICAL EXPERIENCES IN TREATMENT AND RE-
HABILITATION OF FROSTBITE IN ALASKA, by
WUliam J. MUls, ^ck £X ODi«las and others. Apr 60,
lOp. 4 refs. Technical rept. 59-24.
Order from LC mi$l. 80, ph$l. 80 FB 147 746
L
Arctic AeroroedlUl Lab. , Udd APa Alaska.
THE EFFECT OF A RIBOFLAVIN DEFICIENCY ON
COLD- ADAPTED RATS, by Divld A. Vai«han and
Ludie N. Vaughan. June 60, 13p. 11 refs. Technical
rept. 59-8.
Order from LC ml|2. 40. ph$3. 30 Pi 150 576
/ Fifty riboflavin -deficient adult rats (175-250 gm. )were
divided Into two groups. Twenty-five were subjected to
malerately severe cold (5° C ); 25 were maintained at
25 C Each group was divided Into five subgroups,
which received a riboflavln-defictent diet for 28 days,
supplemented with the following levels at riboflavin:
0.5^./gm. diet. l.O^./gm. . l.Sv^./gm..
2. 0 |ig. /gm. , and * 0 ug. /gm. Respective mean weight
changes at these levels of riboflavin intake were:
-4gm. , -^31gm. , -fiagm. , ^77 gm. , and •»63 gm. for
the cold rats; -6 gm. , +34 gm. , -^73 gm. , -^88 gm. .
and ♦lOO gm. for the warm rats. A statistical analysis
indicated that there wms no significant difference tn
weight response between the warm and cold rau at
deficient levels of riboflavin Intake. Data obtained.oo
the food intake cf these animals Suggest that the growth
response to various levels of riboflavin Is a function of
both appetite and eftlciency of food utilization. (Author)
Arctic Aeromedictl Lab. . Ladd AFB, Alaska.
THE EVALUATION OF THE USE OF ULTRASOUND
FROSTBITE THERAPY, by Jack D Dowlas. Aug 60,
lOp. 5 refs. TechnHcal note AAL-TN-60-11,
Ordw from LC ml|l>. 80, ph$l. 80 PB 152 032
The use of ultrasouad as an adjuna to 42*^ water in
immediate, rapid rtwarmlng of frostbitten tissues was
evaluated. Results of these saddles using rabbits did
not indicate that any benefit was produced. However, it
is felt that further sttudleJ should be accomplished with
larger anlmalj before a final verdict is rendered re-
garding the value of ultrasound In frostbite therapy.
(Author)
Araic Aeromedlcal Lab. , Ladd AFB, Alaska.
FLUORUffi CONTENT OF ALASKAN ESKIMO TOOTH
SAMPLES, by Glale Bang. May 60, 14p. 21 refs. Tech-
nical rept. 59-7.
Order from LC ml$2. 40, pti|3. 30 FB ISO 229
The chenUcaJ analyses of die tooth samples from an-
; cient Point Hope Eskimo skulls revealed much higher
V average valuea for the fluoride content in the enamel
and dentin than would be expected, considering die
• probable low fluoride content of the drinJcing water in
«iChe area. The average fluoride concentrations In en-
' amel and dentin of teeth from contemporary Alaskan
Eskimos were comparable with values from other com-
munities with similar low contents of fluorides in the
water si^ipUes. The fluoride analyses of teeth from
fl|anemporary Baklmos revealed no significant dlffer-
iBC«i between samples from persons with and without
caries or between anterior and posterior teeth. (See
also PB 144 833).
Arctic Aeromedlcal Lab. , Ladd AFB. Alaska.
INCIDENCE OF UPPER RESPIRATORY DISEASE
AMONG MILITARY POPULATIONS IN ALASKA, by
E. Lee Treece (U. trf Kansas) and Jerome P. Schmidt.
Aug 60, 48p. 30 refs. AAL Technical rept. 57-44.
Order from LC ml$3. 30. ph$7. 80 PB 150 566
The Incidence of iqjper respiratory disease in military
populations at Ladd Air Force Base was studied and the
ability of an experimental Influenza- adenovirus vaccine
to reduce the Incidence of upper respiratory infections
was evaluated during the winter of 1956-57. The in-
cidence of bacterial and viral p>athogens found In asso-
ciation with clinically recognized Infections was low.
Ot seven types of bacterial pathogens isolated, beta
hemolytic streptococci was encountered most fre-
quendy. Serological analysis revealed the presence of
both Influenza virus and adenoviruses. Influenza virus,
type A, waa the most frequently occurring virus. Mil-
itary pcpulationa vaccinated with Influenza and/ or ade-
novirus vaccine experienced a lower Incidence of in-
fection than did control groups. The duty time lost by
vaccinated groups was significantly less than the duty
time lost by control groups. Military personnel were
not considered to be predisposed to respiratory infec-
tion by factors peculiar to the Arctic and associated
with environmental weather, protective clothing, type
of duty assignment, or living quarters. The problem
of upper respiratory disease in Alaska does not appear
to offer any unique features which would differentiate
It from the same disease occurring elsewhere in the
world. (Author).
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska.
A REPORT OF 103 AUTOPSIES ON ALASKAN NA-
TIVES, by Arthur W.- Gottmann. June 60, 2^ 16 refs.
Technical rept. 59-6.
Order from LC ml$2. 70, phH 80 TO 150 214
18
(^uallutlvely, the pathological findings within tlie na-
tive Alaskan population do not appear to be slgnificantiy
different from those found in the rest of the
United States. The problem of Infectious disease, as
might be expected, Is greater In this group where In-
•ufficient medical facilities and weather combine to
make adequate medical care difficult. The opportuni-
ties for clinical studies of these relatively isolated
people, and some of the specific questions which re-
main unanswered, are included in the discussion.
(Author)
Army Chemical Research and Development Labs.
Army Chemical Center, Md.
THE CULTURE OF CELLS FRC^ KIDNEY TISSUE
WOUNE«D BY HI(ai- VELOCITY MISSILES, by
Margaret W. Cavanaugh. Rept. for Nov 58-Oct 59 on
Wound Ballistics. July 60, 26p. 15 refs. Technical
rept. CRDLR 3016.
Order from LC ml$2.70, pfa$4.80 FB 152 003
Adult Angora goat kidney was shot with high-velocity
bullets and fragments of cortical tissue from the
margin of the permanent wound tract were cultured in
nutrient medium to test whether any viable cells sur-
vived the trauma caused by the formation of the tem-
porary cavity. (Author) i
Biomedical Lab. , Wright Air Development Dlv. ,
Wright -Patterson AFB, Ohio.
A NEW CHRONIC POLAROGRAPHIC IMPLANT UNIT
FOR MEASUREMENT OF CEREBRAL OXYGEN A-
VAILABILITY, by Lawrence R. Parton, Jay M. Lauer.
and Douglas L. Snith. Rept. for Dec 58- Aug 59 on
Health Hazards of Materials and Radiation. May 60,
I2p. 5 refs. WADD Technical rept. 60-388.
Order from OTS $0. 50 PB 171 073
1 I
This report describes the design and development of a
chronic brain polarographic Implant unit capable of de-
tecting small changes in cerebral oxygen availability
(a02). The design and fabrication of this unit: (a) pro-
ride for integral construction of both an anode and a
cathode In a single assembly ^e brain probe, cathode,
may be changed or replaced without removal of the
basic polarographic unit) and (b) improve surgical im:
plant methods resulting In a simple, rapid, and rela-
tively bloodless operation. Reproducible data can be
olitained within 5 days (often as soon as 2 days) follow-
iOR postsurgical recovery. (Author)
Brooklyn Coll. , N. Y.:
INCIDENCE OF ANIMAL PARASITES IN THE RESI-
DENTS OF THE EAST YUKON FLATS, ALASKA, by
George S. TUlloch. June 60, 40p. 16 refs. AAL Tech-
nical rept. 57-19.
Order from LC mi$3. 00, ph$6. 30 PB 150 561
A sampling was ma^e of the human population in seven
of the villages of the Bast Yukon Flats of Alaska to de-
termine the incidence cf animal parasites to provide a
basis for appraising their potential dangers to miliury
personnel operating In this area. Fifty- six or 22% of 251
residents were reactors to Triehlnglla spirally antigen
given intradermally. Seventy-four or 32% of 228 per-
sons harbored Intestinal protoooa. Diagnosis of the
pathogen, Endamoeba histolytica, was established in one
case and eig^t others were considered suspicious.
Glardia lamblla, a form of questionable pathogenicity,
was recovered from 16 Individuals. Sixty-one or 31%
of 198 persons, mostly in the age range of 1-10, were
positive for pinworm ova. Mites of the family Eupodidae
(Eupodes sp. ) were recovered on the pinworm swabs of
four children at Stevens Village. This is believed to be
the first record of an arachnid utilizing the perianal
» regloo of man as a site for a fixed association. Fifteen
or 21% of 70 persons were reactors to an experimental
antigen employed in testing for the presence of the
larval stages of Echinococcus granulosis.
Buffalo U. School (rf Medicine. N. Y.
PULMONARY EDEMA, EXPIRED AIR RESUSCTTA- [
TION. AND THE CHEMICAL CONTROL OF RESHRi^-
TION, by David G. Greene. Final rept. for 1 Sep 50- j
31 Aim 59 on Contract DA 49-007-MD-209. 8 refs.
AD-2^ 644.
Order fnxn LC ml$l. 80. ph$l. 80 PB 150 788
Pulmonary edema due to increased capillary perme-
ability has been produced with alpha -naphthyl thiourea,
and pulmonary edema due to increased pulmonary
venoua pressure has been produced with saline and
norepinephrine. Both types are better treated with in-
termittent positive pressure than with a resusciutor
with a negative phase in the pressure cycle. Pulmonary
compliance is reduced in both types in animals, and in
patients with pulmonary edema, in whom it is a quanti-
tative expression of the degree of pulmonary edema.
Expired air resusciution has been established on firm
physiological principles and applied to the integrated
plan for the ventilatory management of the nerve gas
casualty in the field, during transport, and in rear
insullations. The best techniques for general use and
teaching have been developed, and several training-aids
worked out. The chemical control of respiration In man
has been studied with trishydroxymethyUminomethane,
which has been given intravenously to volunteers while
various parameters have been measured, including
ventilation, alveolar and arterial CO2 tension, arterial
oxygen saturation and pH, urine flow, et al. The data
suggest a feedback mechanism based on CO2 tension.
(Author)
Kansas U. [Lawrence]
THE ROLE OF MAST CELLS AND HEPARIN IN
CERTAIN PATHOLOGICAL PROCESSES, by Tom R.
Hamilton. Final technical rept. for 1 Apr 53-31 Mar 58
on Contract Nonr-583(05). Nov 59, 6p. 12 refs.
Order from LC ml$l- 80, ph$l. 80 PB ISO 856
The object of this project is to study the role of heparin
and related polysaccharides in proliferative reactions
of mesenchymal tissues with special emphasis upon
skin, cardiac and synovial tissues as applied to funda-
mental changes in keloid formation and rheumatic di-
seases respectively; and to determine how components
and products of mesenchymal tissue are Involved tn
Streptococcic infectios and in tiie pathogenesis of ab-
normal respokises related to proliferative disease.
North Carolina State Coll. , Raleigh
FURTHER STUDY OF ALASKAN SCHISTOSOMES, by
Reinard Harkema and David A. Becker. June 60, 25p.
12 refs. AAL Technical rept, 57- 16.
Order from LC mi$2. 70. phK 80 FB ISO 560
19
!i
Ii-
Cercailae obcaliMd from luturally Infected siuUla,
Lymnawi BnigTUiHa. were used in experimental infec-
dOM of ducklings. The sdult form is described and
nsmetf TrtcbobUh^rzis alaskensis Harkema, McKeever.
and Becker. The fniracidium of this species is de-
scribed and limited studies on the sporocyst stages are
presented. Derel^ing metacercarlae were found In
the lungs al duckings 2 days after exposure. Three
new sources of itdi-prcductng schistosome cercariae
were found: Birch Lake, Smith Lake, and Chena Slough
(Badger Road). Mfctacercariae were recovered from
hemorrhagic lesions In the lungs of hamsters 1, 2 and
3 days after expo*jre to cercariae, (Author).
I I
Oklahoma U. Research Inst. . Norman.
EPIDEMIOLOGY OF TULAREMIA IN ALASKA, by
Cauff E. Hopla. Jitie 60, 44p. 45 refs. AAL Technical
repc. 59-1.
Order from LC ml$3. 30. pb$7. 80 PB 150 574
Skin test results iadicate diat tularemia is widespread
throughout central Alaska. The high number of positive
skin tests and serologies in certain villages below the
Arctic Circle implies tiiat the disease, when it does
occur, must be one at relatively low virulence. Studies
among the Indians at Canada showed that It is often mis-
taken for tuberculosis. As of now, the varying hare
has noc been found naturally infected with BacL tula-
rcp*c In Alaska. To date, the most important role that
can be ascribed to this hare is that at being die prin-
cipal host or the rabbit tick. The spleens from various
terrestrial rodents, totaling slightly over 1, 500 spec-
imens, were not found Infected with tularemia organ-
lams. All (rf the positive isolations of Bact. tularense
in Alaaka have coi^ from the rabbit tick, Haemaphy-
aalls let)orls-palusp-ls. This tick is of indirect impor-
tance to man inasmuch as It seldom, if ever, attempts
to obtain a blood meal from him. However, various
authorities believe that this tick is the most Inqxartant
reaervoir at tularemia in the wild. The possible role
<rf blood- sucking D^era is discussed. The possible
relationship of the muskrat- beaver, water and rn^KJ as-
sociation, is reviewed.
School of Aviation Medicine, Brooks AFB, Tex.
RAPID DECOMPRESSION: A PROTECTIVE SUB-
STANCE, by William G. Malette, John B. Fitzgerald,
. and Ben Elseman (Denver Veterans Administration
) Hospital). June 60, ^. 13 refs. Repc 60-62,
Order from LC mifl. 80. ph$l. 80 PB 149 246
Rats Injected with saline and methylslloxane were ex-
i P°«*d to a large do«e at gas emboli by means of rapid
I decompression. There was a significant reduction in
mortality rate in di* methylslloxane- treated group.
The possible mechanisms for such protection may be
I ^^ lowering at biterfacial tension or the prevention of
surface fUma. (Autkor),
School or Aviation Medicine, Brooks AFB. Tex.
A RAPID DECOMPRESSION CHAMBER FOR SMALL
ANIMALS, by William G. Malette, John B. Fitzgerald,
and Ben Elseman (Dtnver Veterans Administration
Hoepltal). Aug 60. Sg). Rept. 60-73.
Order from LC ml$|. 80. ph$l. 80 PB 150 207
Pharmacology and Toxicology
Army Chemical Research and Development Labs, ,
Army Chemical Center, Md.
THE INHALATION TOXICITY OF PERCHLORYL
FLUORIDE, by Earle A. Greene. Joseph L. Colbounj
and others. July 60, 23p, 27 rett. CRDLR-3010.
Order from LC ml$2. 70, phK 80 PB 150 665
The object at this Investigation was to itudy die toxic
effects at tingle 4-bour and repeated (6 bourt per day,
5 days per wedc) exposures to perchloryl fluoride gas
on rodents and dogs. Single exposures at rodents and
dogs to concentratioiu raaglng from 220 ppm to 885
ppm and repeated exposures at rodents to 185 ppm for
7 weeks caused pulmonary Irrlution, methemoglo-
binemia, and blood destruction. Urinary excretion
and bone deposition of fluoride occurred in rodents ex-
posed to 185 ppm and in rodents and dogs exposed re-
peatedly to 24 ppm or perchloryl fluoride for 26 weeks.
(Author) (See also PB 139 881)
Massachusens Inst. oTTecfa., Cambridge.
SYNTHESIS OF SCC«>OLAMINB AND RELATED
COMPOUNDS. THE TOTAL SYNTHESIS OF SCOPO-
UNE AND trans-6.7-DIHYDROXYTROPtNP.^ by John
C. Sbeehan, Arnold Vogel, and Ding-Djung H. Yang.
Pinal rent, for 15 Oct 52-14 Apr 56, Contract N5orl-
07877. [1959] 8p. 10 refs.
Order from LC mi) 1.80. ph$ 1.80 PB 152 096
Scopoline (oecine), a rearrangement product derived
from scopolamine fay sddic or basic hydrolysis, has
been synthesized toully via trsns-6. 7-dihydroxytro-
plne. AlkaUne hydrolysis oT 2. 3-epoKy-2, 5-dlmechaxy.
tetrshydrcTuran (derived from furan) produced trans-
3, 4-dlhydroxy-2. Stdlmethoxytetrahydrcruran, which
waa hydrolyzed to DL-tartar aldehyde. A RoMnaon
synthesis with methylamine and aoetonedlcar boxy lie
acid afforded trans -6,7 -dihydroxytroplnone. Catalytic
reduction gave trans-6. 7-difavdroxvtropine. which
cycllzed to scapoUne on successive treatment with
hydrogen bromide and dilute hydrochloric acid.
Mlcfalgvi U. . Ann Arbor.
ORGANO-TIN TOXICOLOGY, by T. M. fcody. Prog-
ress rept. 1 May-30 Nov 59, on Contract Nonr-
1224(27). 30 Nov .59. 5p. AD- 229 833.
OKder from LC ml|l, 60, ph$l. 80 PI 150 488
Vartous tissues were snalysed for content oT trlethyl
tin acetate (TET) after a<toiinlitratlon with the view oT
correlating in vivo concentration with that required to
produce a biochemical change jn vitro. A method was
used which is a modification from Cretner (Biochcm.
J. 67:87, 1957). In order to determine If the uncou-
pilngactlonorTETseentnla vitro systems might be
responsible for the actions oT this compound in the
whole animal, homogenates and mitochondria were pre-
pared from brains and livers or rats previously treated
with TET. Despite the imcoupllng potency oT TET in
vitro no effect was shown _ln vivo on oxidative phos-
pborylation or rat brain and liver mitochondria and
homogenates. The failure to see any effect here may
be the result oT excessive dilution or TET durli^ the
preparation oT the varioui tissues for assay, b an
Utanitt to determine whether the uncoupling action at
fBT was similar in mechanism to that cT 2, 4-dinitro-
Agnol. TET was compared with DM» on the acceptar-
S^ent system and on ATP-ase activation. In con-
trast to the work of Cremer and Aldrldge, TET did not
jccelerate respiration in an acceptor -deficient system.
Adogenous ATP-ase activity as well as magneslum-
Ktlvated and DNP- activated ATP-ase were studied.
ITiere appeared to be no stimulation of ATP-ase activ-
ity by TET; rather this compound Inhibited both the
04? and magnesium ATP-ases
Minnesoca U. School of Veterinary Medicine, St. Paul.
SrUDIBS OF SKIN. BLOOD, AND RECTAL TEMPER-
ATURES OF UNANESTHETIZED DOGS EXPOSED TO
EXTREME COLD. IL EFFECTS OF CARBON DIOX-
IDE. EPINEPHRINE AND ILIDAR. by A. L. Good and
A. F. Sellers. July 6a I7p. 22 refs. AAL Technical
Wt. 57-53.
Orter from LC ml$2. 40. ph$3. 30 PB 150 569
Wjethylene cannulaewere surgically placed in the
pulmonary artery and in the posterior vena cava at a
point where the hepatic veins enter (referred to as
"hepatic vein"). Thermistors mounted in polyethylene
tubing were passed through these cannulae and the tem-
perature changes of blood, skin (thorax, forearm, paw),
tad rectum were recorded photographically. The effects
of cattxxi dioxide, epinephrine, and Uidar were super-
imposed on extreme cold while continuously recording
blood, rectal, and skin temperatures. Carbon dioxide
inhalation was assocUted with a faU In blood and recwl
ttmperaturea and marked diminution erf shivering.
Little effect on skin temperatures was noeed. It was
thoi^ that the decrease In nnetaboliam contributed to
the fall in "core" temperature. Epinephrine, given in-
travenously in doses or 2. 5 mg. /kg was associated
wttb an Immediate cessation in shivering which per-
■isled for 1 to 2 minutes. Blood and rectal tempera-
tures fell slightly, skin temperature showed little
ctei^. The Intravenous administration oT Uidar in
doses or 4. 0 mg. /kg. was associated with rather
marked rises in blood and rectal temperature which
were additive to those resulting from exposure to cold.
Skin temperatures were only slightly affected. Appar-
ently the doses of Uidar were too snruU to block cut»-
neous vasoconstriction induced by sympathetic Im-
pulses reachii^ the cutaneous vessels. Vasodilation In
ibe viscera could result in shunting blood swsy from
the skin and in this wsy increase internal temperatures
(Author)
Rodiobiology
Baylor U. CoU. or Medicine, HouMon. Te«.
A STUDY OF THE EFFECTS OF TOTAL AND
PARTUL BODY- RADIATION CW IRON METABOLISM
AND HEMATOPOESIS, by Vincent P. Collins.
C. T. Teng, and Walton D. West. Rept. for 1 Dec 58-
31 Aug 59, on Contraa DA 49-007-md-428. [1959]
2lp. AD- 228 105.
Order from LC ml$2.70. pfa(4,80 PB 152 640
Ibis report released for eale to the public 7 Nov 60.
(1) Response of henuiiopoietic system following frac-
tionated doses oT total body radiaticxi is reported in
two patients; (2) Radiation effect on absorptive funcUon
of Intestinal mucosa has been studied by measuring ab-
sorption at radlolodine labeled serum albunun before
and after limited field or total body radiation; and (3)
The clinical and hematopoietic respcmse loUowing total
body radiation with shielding or critical areas has been
studied in a pilot experiment using laboratory animals.
The physical condition of the Irradiated animals, state
oT nutrition, and latent infection must be taken into ac-
count by carefuUy preparing animals to minimize the
Influence or these factors. (Author)
Food and Dri« Research Labs. . Inc. , New York .
THE EFFECT OF IRRADIATED FOODS ON SPECIFIC
ENZYME LEVELS IN BLOOD, by Alvin S. Ostashcver,
Kenneth Morgareldge and others. Final rept. on Con-
tract DA 49-007 -MD- 862. Sept. 59, 28p. 7 refs.
AD- 229 312. ^ .
Order from LC ml$2. 70, ph$4. 80 PB 150 671
A seriet oT studies performed for the purpose cT eval-
uating die possible effects at irradiated food on certain
or the blood enzyme lyKems are reported. Control and
Irradiated pork, bread, green beans, and shrimp were
fed to young rats for a period of approximately 12 wk.
The test samples of pork, green beans, and shrimp
were Irradiated at both the 2. 79 and 5.58 megarad levels
while the taead was exposed to 25 and 50 kilorads. On
a dry weight basis the pork was Incorporated into the
test diet at a 355^ level, the bread ar 80%, and the green
beans and shrimp at both 35 and 80% levels. These
foods were formulated into diets conuining, in addition,
adequate amounts or other essential nutrients (viwmlns,
minerals, and In some cases, casein as a supplementary
protein). Tbe blood enzyme systems assayed in the
rats on these experimental diets were: (1) serum ala-
nlne-a-ketogluMrate transaminase: (2) erythrocyte tran-
iketolaie: (3) erothrocyte glycolysis; (4) erythrocyte
aerobic oxidation oT glucose In the presence of methyl-
ene blue: (5) erythrocyte glutathione reductase. The
results or these studies demonstrated that the rats fed
diets containing these levels of highly Irradiated foods
displayed normal growth responses and normal activity
or the 5 blood enzyme systems Investigated. (Author)
Physics. Engineering, Chemistry Corp. , Boulder,
Colo,
BIOMEDICAL EFFECTS OF EXPOSURE TO ELEC-
TROMAGNETIC RADIATION. PART I: ULTRAVIOLET,
by Archibald R. Buchanan, Harold C. Helm, and Donald
W, StUson. Rept, on Physiology Research. Contract
AF 33(616)6305, May 60, 187p. 657 reft. WADD Tech-
nical rept, 60-376,
Order from OTS $3,00 « 171 072
Literature oooceming the biomedical effeas at ultra-
violet radUtlon it reviewed. Ultraviolet absorption re-
sults In mitotic alterations and abnormal cell division^
regressive changes In the somatic structures or some
lower antmalt, and ikln and eye tumors in mammals.
Damage to the eye from hl^ intensity ultraviolet is
probabily limited to the cornea and, to a slight extent,
the leas. The effecti elicited by ultraviolet irradiation
or certain proteint, nucleotides, enzymes, hormones,
and am tax) acids are reviewed. Literature pertinent
to the vltlbUity and hue of ultraviolet, the effects oT
21
ultrivlolet wavelength! on scotopic and photopfc visual
•enittlvlty and on ifie "reactivity" at the organism if
surveyed. (Author]
Public Health Serrlce, Washington, D. C.
RADIOUXaCAL HEALTH DATA. VOLUME I, NO. 7.
Quarterly repi. Cot 60, 68p, 6 refa.
Order from GTS $I.0(i$9.00/yr. PB 161 371-7
Contents:
Sect. 1. Milk: Public HeaJth Service milk monitoring
program; data on radioactivity In milk at Honolulu,
Hawaii (Jan-Mar to)
Sect. 2. Air: Public Health Service radiation surveil-
lance network: Public Health Service national air
sampling network
Sect. 3. Water: Public HeaJtb Service oadciial water
quality network
Sect. 4. Other data: external gamma activity; dally
intake at calcium and 8trontlum-90 from environ-
mental aources; concentration at stroiitlum-90 in
whole wheat and white bread purchased in New York
City in 1958-1960; estimated dally per caplu intake
erf wheat milling ptoducta and the relative contribu-
tion d strontium -90 from such products to the total
diet; RrGntlum-90 in milk and agricultural materials
in the United Kingdom (1958-1959); estimate at
Krontlum-90 In the diet at New York City intent*
nurtured on commercially processed baby foods and
milk; food con8um|iclon of households In the
United Slates, Southern and Western Regions (1955);
the cesium-pocasslum trend in humans at Chicago
aa a function at tlr»e; Delaware River surveillance .
aummary report; radioactive fallout from nuclear
detonations d Feb and Apr 60; fallout studies. (See
alaoPB 161 371-6)
Public Health Service. Washington, D. C
RAD10L(XJICAL HEALTH DATA. VOLUME I, NO. 8.
Monthly rept. Nov 60, 55p.
Order from GTS $1.00, $9.00/yr. PB 161 371-8
(Contents:
Sect. 1. Milk: Public Health Service milk monitoring
program; dau on radioactivity In milk (Apr -June 60);
aecretion o^ dietary Btrontlum-90 and calduin in
human milk
Sect. 2. Air: Public Health Service radiation aurveil-
lance network; Public Health Service national air
aampUng network; U. S. Naval Research Laboratory
radioactivity measurements (June 60)
Sect. 3. Water: Public Health Service national water
quality network; mooltarlng water supplies around the
Nevada Teat Site (M«y-June 60)
Sea. 4. Other data: External ganuna activity Qune 60);
summary c* research results related to environmemal
radioactivity; envlroomentaj levela erf radioactivity at
Atomic Energy Commission installations; strontium-90
in wheat and wheat products; Montefiare HcMpitaJ
metaboUc studies; short term training in radloloalcal
health. ^^
(See also PB 161 371- ')
. ■- I
Radiobiological Lab. . U. at Texas, Au^n.
A NEW CHR(»nC LOW-DOSE COBALT-60 FAaLITf
OF THE RADIOBIOLOGICAL LABORATORY, by Hugh
L. Perry. Jan 60. 6p. 2 refa. APSAM rept. 60-22;
AD- 233 168.
Order from LCmlSl, 80, ph$ 1.80 PB 152 353
Tbla report released for sale to the public 28 Oct 60.
Dertgn alibi* mew chronic low-doM CoteIt-60 facility
provide* a safe, reliable operation meeting the require-
menta aet forth by the Radiobiological laboratory. An
accepuble range at flux variation throughout the cage
was found. However, a rotaHotf <rf animal placement is
the cagea and the randomized movementa at the animals
in the cages ahould minimize the difference at radlatloa
dose delivered to each animal. (Author)
Zoology
University <rf Southern California, Los Angeles.
OBSERVATIONS ON THE REPRODUCTIVE CYCLE
OF THE MALE ARCTIC GROUND SQUIRREL
(SPERMOmiLUS UNDULATUa by Ormond G. Mitchell
June 60, 21p. 11 refs. AAL Technical rept. 57-26.
Order from LC ml92. 70. phH 80 PB 150 562
The study was undertaken In an effort to correlate the
histological changes observed in the testea with the re-
latively abort activity cycle. ,
Virginia U. School of Medicine, Charlottesville.
A STUDY" OF GROSS BODY COMPOSITION OF
SMALL ALASKAN MAMMALS AS COMPARED WITH
THOSE FR(»4 THE TEMPERATE ZONE, by Graver
C. Pitta. June 60, 31p. 20 refa. AAL Technical rept.
59-3. ^
Order from LC ml|3.00, ph|6. 30 PB 150 575
Gross comfXMltlon of the body with respect to fat,
water, specific gravity and 1 1 tissue componenta was
studied in 1 16 adult wild mammals of 29 species and
13 families. Body weight ranged from 3 to 130. 000, 000
grams, in a aerlea ranging from the shrew to the blue
whale Body fatneaa « 1. 50 (FFBW)0. 195 where FFBW
is the fat- free body weight. In all species studied adi-
pose tissue adapts itself to increasing body fatneaa by
two mechanisms: (1) die fat fraction of existing sdl-
poae tissue increaaea to a limiting value of about 80
percent and (2) as this limiting value is approached,
fat-free weight al the total adipose tissue present be-
gins to increase indicating a hypertrophy of exiating
l^Kxytea, a proliferation of new lipocyiea or both.
CHEMISTRY
National Inatitutea at Health, Betheada, Md.
PIPETTING APPARATUS, by Harry Philip Marshall.
Invention rept. [1958J 2p.
Order from LC mi$1.80, pb$1.80 PB 152 855
I
A siBBtcfa is presented of an apparatus consisting
tsannriilly of a vacuum line connected to a bell- shaped
ptofldc tube into which any size pipette may be
Inserted.
Inorganic Chemistry
Office of Technical Servicea, Dept. at Commerce,
Washington. D. C. '
ALKAU METALS: LITHIUM. SODIUM. POTASSIUM,
RUBIDIUM. AND CESIUM. July 60. 37p. 672 refa.
OTS Selective Bibliography 421 .
Order from OTS $0. 10 OTS SB-4ZI
A bibliography of reports listed In the two OTS monthly
■bstraa Journals: U. S. Government Research Reports
tod Technical Tranalationa. Reports listed cover the
metals, alloys, and compounds of lithium, sodium,
potaasium. rubidium and cesium, as well aa research
OB their toxicity, hazards, and safety in handling.
These reports were added to the OTS collection during
the period 1950 to July 1960.
Office of Technical Servicea, Dept. of Commerco,
Washington. D. C
ALKAUNE EARTH ELEMENTS (BARIUM, CALCIUM.
AND STRONTIUM). July 60, 21p. 335 refa. OTS
Selective BibUography SB-422.
Order from OTS $0. 10 OTS SB-422
A bibUography at reports listed in the two (TTS monthly
akifraa Joumala: U. S. Government Research Reports
and Technical Tranalationa. Reports listed cover the
ineuls and compounds of barium, calcium, and stron-
tium, as well as research on their toxicity, hazards,
and safety in handling. Tbeae reporta were added to
the OTS collection during the .period 1950 to Auguac |
1960.
Organic Chemistry
Oonoectlcut U. , Storrt.
TRANSANNULAR REACTIONS OF FREE RADICALS,
bjr Roy J. Critter, Edward Sabatlno, and Stanley
Suharow. Final rept. for 3 Mar 59-15 Jirae 60 on Con-
tract DA 19-020-ORD-4828. 50p. 21 refi. COR rept.
no. 2304. 1-C
Order from LC mi$3. 30. ph$7. 80 PB 150 407
The first phase at this inveatlgatkn was concerned with
Ihs possibility and extent at transAonular reactions of
free radlcklt in the substituted blcycllc ring system.
The second phase concerned the ptkotoisomerizatlon at
btcyclohepu-2, 5-dlene derivatives to form the corre-
sponding quadrlcyclic compounds. Anodier object of
this Investigation was to study the free radical chemistry
of some compounds containing a medium -sized ring to
teermine whether or not a transannular free radical re
action could occur.
Edinburgh U. (Gt. Brit.)
REACTIONS RELATED TO OXIDATION, by
T. Bercea, W. E. Falconer and others. Final ledi-
nlcal rept. oo. 1, Sep 59-Sep 60, on Contraa DA 91-
591-EUC-1184. 28 Sep 60, 34p. 40 refs.
Order from OTS $1.00 PB 171 122
This report falls into four parts, each of which de-
scribes the application of a simple competitive method
to the determination of the relative rates at which
alkanes are attacked by oxygen -containing radicals
that are involved in oxidations. Part 1. reports the
completion of the key study in this series. The rela-
tive rates of consumption of mixed alkanes oxidized in
sutic vessels with molecular oxygen have been meas-
ured. Hence the relative reactivities of the alkanea
have been found. The nature of the anactdng radlcala,
X, la not known but certain deductions can be made.
The next suge is to compare the reactivities ob-
served for X with thoee cf known radlcala. Part 2.
reports the completion of a study of the reactions of
methoxyl radicals generated by the pyrolysis of
methyl nitrite and dimethyl peroxide. From thla it
can be seen diat methoxyls do not play a aignlficant
part In oxidations. Some evidence of the absolute
ratea of methoxyl radical reactions has been obtained.
Part 3. reports the relative rates of consumption of
alkanes by the atuck of radlcala, presumed to be
alkylperoxy generated by the photolysis of ketones in
an excess cf oxygen. The radicals reaa very simi-
larly to X, which may therefore be a peroxy radical -
at any rate at low temperature. Pan 4. reports pre-
liminary reaulca in the reactions of hydroxyl radlcala,
which may be equivalent to X at hig^ temperaturea,
produced by the photolysis cf hydrogen peroxide in
solution. (Author)
Llnle, Arthur D., Inc., Cambridge, Mass.
A SURVEY OF THE LITERATURE ON THE USE OF
ORGANOMETALUC COMPOUNDS IN THE PREPARA-
TlOti OF ULTRA-PURE METALS, by W. A. G.
Graham. Scientific rept. no. 1 on Contract
AF 19(604)4975. 15 July 60. 42p. 122 refs. BRD-TN-
60-768.
Order from OTS $1.25 PB 171 097
A survey of the literature on methoda for recovering
metala from organometalllc compounds has been
carried out. Possible recovery methods are thermal
decompoaltion, photolysis, electrolysis, and hydro-
genolyaia. These have been appraiaed from the stand-
point of contamination of the product by organic rssl-
dues. Reaction of meuls with gaseous organic fi-ee
radicals haa also been reviewed, but does not appear
attractive as a means of purification. Reactiona of
organic free radicals in solution with metals are also
discussed. (Author)
Natloiiil Bureau of Standards, Washington, Di C.
VAPOR PRESSURES OF ORGANIC COMPOUNDS IN
THE RANGE BELOW CWE MILLIMETER OF MER-
CURY^ by E. E. Hi^ies and S. G. Lias. Oct 60. 26p.
115 refs. Technical note 70.
Order from OTS $0. 75 PB 161 571
22
fWJ|p,
23
Qua for vapor pressures less than one millimeter of
mercury for over three hiindred organic compounds
have been oollectcKL The values are presented to tabu-
lar form. No attempt has been made to evaluate the re-
liability of these data except where several Investigators
have studied the same con? pound over the same pres-
sure range. A brief discussion of the methods and In-
struments which l«ave been used to measure low vapor
pressures Is Inclitied. (Author)
Pennsylvania State U. ColL at Chemiatry and Phyalcs,
University Park. '^^
STUDIES ON THB MECHANISM OF OLEFIN-AL-
COHOL INTERCCKVERSION. THE EFFECT OF
AciDrry on thb o^^ exchange and dehydra-
tion RATES OF TERT- alcohols, by Robert A.
Boyd, Robert W. Taft, Jr. and others. Technical rept.
on Contract Nonr-656(03). Nov 59, 27p. 41 refa,
AD- 230 352.
Order from LC m||2. 70, phK 80 PB ISO 538
Evidence from the acidity and temperatxnre dependence
at the ratea at O^' exchange and dehydration al tert-
alcohols have been obtained which indicatea that these
two reactions proceed by common initial step* but In-
volve different rate determining steps. The results
appear to eliminate a mechanism In which a "free"
carbonium Ion Isoanerlzes to a Tf- complex In the rate
determining step al the alcohol-olefln interconverslon.
Present results are found to be consistent with mecha-
nisms which Involve either the free carbonium Ion or
the encumbered carbonlimi ion Intermediate, R -^ . . .
0H2- The latter classlflcatlan Is proposed for Inter-
mediates which poasess substantial carbonium Ion
character and invoive measurable interactions between
the catlonlc center and leaving or entering groups at
either neutral or various charge types. The mecha-
nism Involving the encumbered carbonium Ion Inter-
noediate Is favored by the weight of earlier Investiga-
tions. The Zucker-Hammen hypothesis is found to be
Invalid as a criterion of mechanism for the olefin-al-
cohol interconverston. The original basis for Tail's
mechanism has accordingly been shown to be Invalid.
However, all of the subsequent lines of evidence which
have been obtained are consistent with the modified
mechanism in which the rate determining step involves
the Isomerlzatlon of two intermedlaces.Tr -complex
sad the encumbered carbonium Ion. (Author).
Rutgers State U- School of Chemistry, New Bruna-
wlck, N. J.
^ABLE BORON POLYMERS, by Charles B. Erlckaon
and Edward G Melonl. Technical rept. no. 1 on Con-
tract NaBr-404(14), 17 Dec 59, 8p. 3 refs.
AD- 230 248. I
Order from LCmiil. 80. pii$ 1.80 PB 152 067
Ob:
Ob]ectl
w: To prepare a polymer containing B-O-B
ge having tetrtvaleot boron atoms, in the expecta-
tion 1^ the polymer will be noore resistant to oxygen
and molature than ^aom. other boron polymera. Mooo-
mer Deaired: 4-Di]|i0thylamloe- 1 -butanebaroalc add.
probably widi an Internal N — pB bood.
"2c — c"2
\
b"2
" "(0H)2
<P*3)2
Prepared Prom: 4-Chlaro-l-butaiieboronlc acid by
treatment with dimethylamlne . Present Status: The
monomer baa been made, but seems to be contami-
nated with a dl-boronlc acid, (H0)2BC4H8B(0H)2. The
polymer obtained by removing water from the monomat
la very viscous, partly because of cross-linking. It
reaas with water extremely slowly as expected if
boron la tecravalent. (Author)
University of Southern California, Loa Angeles.
CHEMICAL BEHAVIOR AND BONDING OF BORON
HYDRIDE DERIVATIVES, by Anton B. Burg. Technical
rept. no. 5 on Contract Nonr-228(13). 1 Nov 59. 3Sp.
58 refs. AD-228 177.
Ozxler from LC ml$3. Oa ph$6. 30 PB 150 519
Pkxyucai Chemistry
Caulyals Reaeardi Labs. , Alfred U. , N. Y.
FUEL CELL ELECTRODE PROCESSES. I. CATALY-
SIS AND CHEMISORFnON, by George J. Young and
Ralph B. Rooelle. Technical rept. no. 1 on Contraa
Nonr-656(19). Nov 59. 56p. 16 refs. AD- 232 641.
Order from LC ml)3. 60, ph$9. 30 PB 150 515
Chemisorptlon and caulysis were investigated with
respect to electrode processes in low -temperature fusl
gaa cells. Hydrogen on metal electrodes: The over-aU
electrode reaction in a fuel gas cell with H and O Is the
oxidation of H to form H2O. The cell potential la de-
pendent on the electrode catalyst. The implication Is
that measured equilibrium free energy change Is not be-
tween the gaseous reactants and the electrolyte but
rather between the cbemisorbed gases and the electro-
lyte. Measured values for hydrogen half- cell potentlali
were approximately a linear function of the heats of
chemisorptlon at that portion of the surface which is
active in the reaction. Hycfa-ogen on metal oxide elec-
trodes: Oxides of metals of the first transition series
were studied as catalysts at the hydrogen electrooe.
The oxide electrode catalysts appeared to follow the
same empirical correlation with the heata of cbemlsor^
tion. &nce the hydrogen electrode of the fuel cell csn
operate only by the reversible type chemisorptlon, the
beats of hydrogen chemisorptlon obtained from the half-
cell potentials contain no contribution from the Irre-
versible mechanism. Catalysis erf fuel cell electrode
reactions: The activity of various groups of metals for
both the fuel electrode and oxygen (air) electrode Is
discussed, giving a guide to the selection cf catalysts
for specific cell reactions.
Costing and Cheiiical L^. , Aberdeen Proving
Ground. Md.
TEMRRATURE DEPENDENCE OF SUSPENDING
POWER, by A. Mankowich. 15 Ai« 60, 19p. 8 refa.
CCL#96.
Order from LCnii$2. 40, pb|3. 30 FB 150 069
Temperature dependence studies of suspending power
were made at 28^ and 82. 2^ of three typea of sur-
factanta in built and unbuilt solution using a CrjOs
powder. The powder was suspended well by bothanionlo
and nonionlc surfactants. Temperature coefficients
wne smsU; snd, In unbuilt soludfan, were negative fbr
anionic SDBS and nonionlc PGNTC, and positive for
■odium oleate. Suspension isotherms in built and un-
built solution appeared typical; and could be explained
by the usual initial adsorption of detergent anions on the
Cr203 particles until maximum zeta potential and sus-
pendiblllty were attained, followed by sharp drops in
tuspendibillty due to the neutralizing effea on the zeu
potential of the increasing sodium ion concentrations. A
theory for the positive temperature_coefflclent of
sodium oleate was proposed. (Author)
Prick Oiemlcal Lab. , Princeton U. , N. J. «
INTER AND INTRAMOLECULAR POTENTIALS AND
THE SPECTRUM OF ICE. by C Haas and D. F. Homlg.
Technical rept. no. 3 on Contract Nrar- 1858(27).
25 Nov 59, 20p. 11 refs.
Onler from LC ml$2. 40. ph$3. 30 PB ISO 85S
Whereas the spectra of H2O and D2O Ice cannot yet be
explained unambiguously, the spectra of HDO In dilute
solution In either H2O or DjO may be Interpreted read-
ily, bi particular, since V q^ occurs at 3275 cm -1 and
2 if QH^t 63<X) cm-1, nearly the harmonic value, the
barrier to proton transfer lies well above the latter level
•ad must exceed 23 k. cal/mole. The width of i^nn *'
2416 cm'*^ Is only 20 cm'*, whereas tfiat of t'oH "
about 80 cm" land 2 t/ OH**""' ^^'^"'- Thesewidthi
can be explained by proton tunneling if the barrier
height is near 32 k. cal. , in which case the second mini-
mum must He below the level I^qm- ^ '""■^ therefore
be less than 14 k. cal/mole above me primary minimum
A doubling of l^oQ from OD . . OD pairs was also ob-
served and the magnitude of the splitting is consistent
with an effective charge cf 0. 6e on the protons. It is
clear from these results that the usual width of hydro-
gen bonded OH lines is not an Intrinsic characteristic
of die O-H. . . O bond but results largelyfrom intramolec-
ular coupling of the O-H motions. (Author)
Institute de (^Imica Pisica (Spain).
KINETICS OF THB SULPHU RATION OF METALLIC
SURFACES, by J. Llopls. J. M. Gamboa, and
L. Arizmendi. Final rept. on Contract AF 61(514)1329.
May 60, 82p. 13 refs. AFOSR-TR -60-73.
Order from LC mlM 80, ph|13. 80 PB ISO 334
A study has been made of the surface reaction of copper
and platinum with aqueous solutions of thiourea labelled
wldi S^S and C^^. The results suggest that a umlahlng
reaction takes place at die surface of the copper, prob-
ably forming a film of copper sulfide. The kinetics of
Ibis reaction may be expressed by the equstlon
kd *r
Ibe plot of log kr against 1 la linear, die alope corre-
iponds to an energy of actlvatloa A H* -10. 9 Kcal/mol;
the plot of log k^ against L gives two stral|^ linea.
The reaction with platinum finishes with the formstion
of a few monolsyers and the kinetics msy be slven by a
logarithmic law. Research has been extended to study
the surface reaction of copper with solutions of diphenjd -
ddourea in xylene; this reaction yields coherent films
showing interference colors. The surface reaction of
copper with aqueous solutions of methylthiourea and of
sodium polysulphide has been studied. The reactions of
copper and diver with benzene soluticms of sulfur have
also been studied. (See also PB 143 681)
Iowa State U. of Science and Tech. . Ames.
RESEARCH ON HEAT CAPAaTY LAG IN GASES, by
Sam Legvold and L. M. Valley. Final rept. on Contract
AF 18(600)1496. Aug 60. 6p. 6 refa. AFOSR TR-60-109
Order from LC mi$l. 80, ph$l. 80 PB 150 458
Laboratorl dl Elettrochlmica. Chlmica Piaica e
Meullurgla del Polltecnlco dl Mllano (Italy).
RESEARCHES ON HYDROCKN OVERVOLTAGE Oti
MBTALUC SINGLE CRYSTALS: TIN, by L. Peraldo
Bicelll and A. La Vecchia. Rept. for June-Dec 59 on
Surface and Interface Phenomena Matter. Contraa
AF 61(052)144. July 60, 19p. 15 refs. WADD Tech-
nical note 60-115.
Order from OTS $0.50 PB 171 079
Hydrogen overvoltage on tin alngle cryaul cathodea,
oriented following the (001). (100). (110). planes and
on polycrystalllne tin, haa been measured in perchlo-
ric acid solutions with two different concentrations and
In hydrochloric acid solutions. Tsfel law holds true;
whUe the parametera are different for the different
electrodea. (Author)
Laboratory cf Atomic and Solid State Physics,
ComeUU., Ithaca, N. Y.
SATURATION AND DOUBLE-FREQUENCY IRRADIA-
TICW ffTUDIES OF THE TWO-PROTON SYSTEM IN
CaS04*2H20, by D. F. Holcomb and T. R. Sliker.
Technical rept. no. 4 on Contract Naar-401(15).
29 Dec [59] 30p. 12 refa. AD- 234 160.
Order from LC mt$2. 70. ptS4. 80 PB 152 068
A number of experlmenta have been performed on the
proton spin system in CaS04- 2H20 with RF power level
iuffldent to appreciably satiorate the nuclear spin
resonance. Observations were made of the dispersion
and absorption modes in s standard CW experiment. la
the dispersion mode, st RF levels such thst the RF
msgnetlc field. Hi, was greater than 0. 1 gauss, a
third dispersion line appears in the center of the un-
iaturated two- line pattern. This extra line vMy arise
from a double-quantum process. Involving sbsorptlon
cf two "photons" from the RF oscillator field. In a
second set at experiments, two radio frequency
oscillators were employed. One oscillator, operating
at large Hi, produced a Urge power absorption at one
frequency while the other, low -level oscillator was
used to sample the absorption line shape in the pres-
ence of the large Hi by sweeping the frequency of the
low-level oscillator. Using crossed coils, the oecil-
latora could be operated with their frequencies dif -
ferity by as little as 5 kc/sec, st 12 mc/sec. without
interacting strongly. In these experiments, small
ctei^s in line shspe, and a surprising enhancement
of the absorption signal from one line while saturating
the other were observed. The presence of this en-
hancement demonstrates the existence of multiple spin
flip relaxation processes. (Audicr)
Louisiana State U. , Baton Rouge.
STRUCTURE OF THE DOUBLE LAYER AND ELEC-
TRODE PROCESSES IL EFFECT OF THE NATURE
OF TOE ELECTROC« AND APPLICATION OF THE
THALLIUM AMALGAM ELECTRON, by Paul Delahay
25
and Marcos Klelnerman. Technical rept. no. 40 on
Contraa Nonr-300|[00). Nov 59, 28p. 26 refs.
AD- 230 194.
Order from LC mljC. 70. phR 80 PB 150 870
The Influence at tht nature of the electrode In electro-
chemical kinetics |i the absence of specific electrode
effects. Is interpreted on the basis of a change in the
double layer structure. This double layer effect should
also be considered in kinetic correlations for processes
with specific electfode effects. Application is made o*
the dropping thallium -amalgam electrode (up to 31^5 Tl)
for which the point of zero charge can be shifted con-
tinuously by as much as -0. 4 v with respect to this
point for Hg. The tollowing reductions are studied:
bromate and iodace in alkaline solution, hexacyanochro
mate fill) In cyanide rreriji«n, c^xromate in alkalln*
solution, and tetracyano cadmium (II) in cyanide med-
ium, atfts of the Tafel line for bromate and variations
of the exchange current density for hexacyanochromate
(III) are interpreted quantitatively. Chromate waves
for tlie dropping thallium amalgam electrode in support-
ing electrolyte al {dm concentration exhibit a pro-
nounced minimum which is quantitatively discussed.
The maximum in the tetracyano cadmium (II) waves is
*^bscrlbed to a double layer effect in agreement with
other investigators , and a quantitative study is attempted
for the results obtained with the dropping »% electrode.
(Author)
Massachusetts Inst. c^Tech., Cambridge.
HYDROGEN PEROXtDE LABORATORIES, by
C. N. Sanerfield. Qiiarterly periodic status rept. on
Contraa Nonr-184lClI). 31 Dec 59, 12p. DSR 5-7476;
AD-231 415.
Order from LC ini$4.40, ph$3. 30 PB 152 095
Hydrogen perooti^e decomposition flame: Shadowgraphs
were made of H2O2 blames which were atabi 11 zed at
atmospheric pressure at the tip of a Pyrex burner.
Measurements were made al the flame velocities and
the energy d activation (E) of the H2O2 decomposition.
Calculations produced an E of 26. 7 kcal/mole which
was in excellent agfraement with experiment. Shadow-
graphs of H2O2 flamts at sub- atmospheric pressures
indicated a laminar (|ow in the burner tube. Parous
walled reactor studlas: Experiments in a porous stain-
less steel reactor were made by using N-H2O2-H2O
vapor mixtures with and without the injection <rf N
through the parous wail. The rate constants for firit-
order decompoeltlan pi H2O2 on porous stainless steel
varied from 5.4x10*'* to 7. 3x 10"^g-mole/(cm)^M)
(atm), depending on the temperature of the surface and
the flow rate of the g«s in the rea«tar. Decomposition
^ ^12^2 /^P"^ 9" catalytic surfaces: Decomposition 0^
0. 28 mole-% H2O2 was studied inside a Cu tube at
^0*^. The ratio of tlie measured reaction rate to that
predicted by as8umin| complete mass transfer control
increased from . 02 to . 06 with time. An Ag tube was
oxidized by being anodized in a NaOH solution, then
used as a caulyst tube. There was no decrease of
activity with time, even after washing with NH3 solu-
tion, and with H2O2 solution followed by NH3 solutiona
The reaction rate renMined about 0. 75 of the rate
predlaed by mass tr^nafer correlations. (Sec also
PB 146 281)
Metals Research Lab. , Carnegie Inat. of Tedi. ,
Pittsburgh. Pa.
MSSOLUnON KINETICS AT DISLOCATION ETCH
PITS IN SINGLE CRYSTALS OF LITHIUM FLUO-
RIDE, by M. B. Ives and J. P. Hirth. Technical rept.
no. 4 on Contraa Nonr-760(17). 1 Dec 59, 35p.
14 refs. AD- 232 562.
Order from LC miJ3. 00. pti$6. 30 PB 152 089
Dissolution at dislocation etch pits in lithium fluoride
dissolving in a dilute aqueous solution of ferric fluo-
ride did not follow the kinetic laws predicted by the
current topographical or mechanistic theories of crys-
tal dissolution. The results were conslstem with the
mechanistic theory involving dissociation of lithium
fluoride from monomolecular steps on a lithium fluo-
ride and subsequent diffusion into solution. If a time-
dependent adsorption of ferric fluoride "f>oisoa" at the
receding monomolecular steps was invoked. Deviations
from the topographical dissolution theory of Frank
[Growth and Perfeaion of Crysuls, p. 411, Wiley and
Sons. N. Y. . 1958] could also be explained by this
time -dependent model. The experimental results
could only be quallutlvely compared with theoretical
predialons because of the complexity of the time-
dependeot dissolution process. (Author)
Milan U. (Italy).
ELECTROCHEMICAL BEHAVIOUR OF OXYGEN AND
HYDROGEN PEROXIDE ON SILVER ELECTRODES,
by G. Bianchi. G. Caprloglio and others. Technical
(scientific) note no. 1 on Contract AF 61(052)260.
May 60. 41p. 21 refs. AFOSR-TN-60-299.
Order from LC mi$3. 30. ph$7. 80 PB 150 336
The electrochemical behaviour of oxygen and hydrogen
perootide on silver electrode was studied by means of
polarization curves. In acid and neutral solutions the
process Ag ^ Ag -»- interferes with chose of the system
H2O - H2O2 -O2. The reduction of O2 and that of H2O2
occur in the same way at 0. 15 V. The tension is inde-
pendent from the pH. In alkaline solutions the reduc-
tion of ©2 occurs at 0, 2 V and the oxide film covering
the electrode does not interfere. The reduction of
HjOo occurs through its decomposition in H2O and O2
and the successive reduction of oxygen according to the
process O2 + H20* 2e -^-HOj ♦OH." The anodic for-
mation of silver oxides is showed, but does not inter-
fere with the oxidation of H2O2 that occurs at a lower
tension (0, 18 V). (Author).
National Bureau of Standards, Washington, D. C.
SOME EXPERIMENTS ON THE DEPOSTTICM^ OF
GASES AT 4.20K, T. Baurer. Oa 60, 34p. 10 refs.
Technical note 73.
Order from GTS $100 PB 161 574
In order to develop some preliminary Information con-
cerning the very basic problems of gaseous deposition
at extremely low temperatures, samples (rf argon,
nitrogen, oxygen, and hydrogen were deposited at
4. 20K, and variations in some of the parameters as-
sociated with these depositions were observed. In addi-
tion, samples of the same gases were passed through
an excitation zone prior to deposition, and differences
26
In the depoaition behavior were recorded. The pres-
ture downstream of the deposition region and the tem-
perature within the deposited solids were found. In
general, to Increase with flow rate of the depositing
substances, and to vary with time In a mariner depend-
l|i^ on the density, flow rate, and statt of excitation of
the incoming gases. Arrhenius curves were plotted
using warmup data observed In these experiments and
•olid- phase transition data determined elsewhere.
Variations in the positions erf these plots were some-
times the result of differences in the conditions of
depoaition. and at other times an effea of the chemical
Mture of the gas studied. The experimental behavior
of hydrogen, relative to that of the other gases studied,
was observed to be strongly dependent upon its much
higher thermal conductivity. (Author)
Northwestern U. , Evanston, 111.
CATALYTICALLY ACTIVE SOUDS. byP W.Selwood.
FlMl rept. on Contraa Nonr- 1 228(08). 31 Dec 59, 3p.
9 refs.
Order from LCmiSl. 80, ph$l. 80 PB 152 126
Brief sumniary listing publlcadons prepared under the
contraa
Northwestern U. , Evancton. III.
CATALYTICALLY ACTIVE SOLIDS CHEMISORPTION
AND MAGNETIZATION, by Robert E. Dletz. Technical
r«pt. on Contract Nonr- 1228(08). 1 Nov 59, 156p.
78 refs. AD- 230 202.
Onler from LC ml$7. 50. ph$24. 30 PB 150 536
A study was made of unpaired electrons before and after
dwmisorptlon In order to gain a more complete descrlp
tkm of th« H-Nl chemlsorptlon bond. The Immediate ob-
jectives were to determine the effect of diemlsorbed H
on the saturation magnetization of fine Ni particles, and
to determine the Influence of particle size and mode of
preparation of the sample, conditions of adsorption, and
other physical factors on these changes. The following
measurements were made: (1) magnetizatioa-fleld in-
tensity measurements, (2) analysis of Ni in the samples,
and (3) pressure- volume measurements to determine the
volume of gas adsorbed by the samples. For sintered
samples containing particles of radius of the order of
60 A, the saturation, magnetization of the sample was
wllfaln l%of that of massive, polydomain NI. Hydrogen
dacreased the saturation magnetization by 0. 4 to 0. 7 by
■ad (L 6 to 0. 8 Bohr magnetrons for unsintered and
•tetered samples, respectively. Hydrogen was concluded
to be bound to the Ni surface by bonds of nattire Inter-
noedlate between the metallic-type bonds of the NI, and
purely ionic contributions as In the Pd-H system. A
phenomenological theory was developed which success-
fully related the changes In the low-field magnetization
to variables such as surface coverage, temperature,
magnetic field Intensity, and the nature of the distrlbu-
ttan of particle size. The saturation experiments were
tn approximate agreement with the low-fleld studies.
Office of Technical Services, Dept. of Commerce.
Waahington, D. C
MOLTEN AND FUSED SALTS. Aug 60, 9p. 135 refs.
(TTS Selective Bibliography SB-42S.
Order from OTS $0. 10 OTS SB-425
A bibliography of reports listed In the two OTS monthly
abstraa Journals: U. S. Government Research Reports
and Technical Translationa. This bibliography in-
cludes reports added to the (TTS collection during the
period 1950 to September 1960.
Olio State U. Research Foundation, Columbus.
A STUDY OF TIffi INFRARED SPECTRA OF FLAMES
USING PHASE- DISCRIMINATION METHODS OF DE-
TECTIC»^, by Fred P. Dickey. Norman Gailar and
others. Final rept. on Contract AF 19(604)2254.
July 60. 76p. 35 refs. AFCRL-TR-60-403.
Order from LC mlK 50. ph$12. 30 PB 150 755
"nils report is about the application of phase-discrim-
ination methods of detealon to overcome some of the
difficulties resulting trom the masking effects of the
Strang emission due to water vapor. These same meth-
ods could be extended to overcome masking effea s of
carbon dioxide or any other molecular radiation source
To date, two different methods of taking observations
have been used, and they accomplish essentially the
same end result, bi a given Individual study one method
may have some advantage over the other.
Included In the report Are:
Emission spectrum of the OH radical in an oxy
acetylene flame, pub. In The Jnl. of Chemical Physict
28:1253. June 58
28:1253. ^ine 58
Application of phase-discrimination method of detec-
tion to the study of the spectrum erf the OH radical In
an oxyacetylene flame, pub. in Seventh Symposium
(International) on Combustion, p. 938-941, 1959.
Bnlsslon spectrum of the CW radical In an oatyacety-
lene flame in the 1.5^ region, pub. in The Jnl. of
Chemical Physics, Aug 60.
Pennsylvania State U. Coll. of Chemistry and Physlca.
University Park.
SOLVENT EFFECTS ON MESOMERIC CHARGE SEP-
ARATION, by Robert W. Taft, Jr. . Richard E. Click
and others. Technical rept. no. 23 on Contraa Nonr-
656(05). Nov 59, 4p. 11 refs. AD- 230 353.
OrderfromLCml$l.80, ph$l. 80 PB 150 539
The contribution to the resonance hybrid of dipolar res-
onance structures as enhanced by solvents which sup-
port ionization was studied. The phenomena based upon
shielding parameters from the taiclear magnetic reso-
nance spectra of jn- and ^-substituted fluorob^enes.
Emphasis was placed on the quantity - (r - J^, die
mesomeric charge perturbation (m. c. p) at the F^' nu-
cleus. The m. c. p. 's were measured for a variety <rf
typical -R and -fR substituents in cyclo-C^i2. CCl4.
MeOH. ai»d 75% aqueous MeOH at infinite dilution. The
results indicated that to good approximation (± ~5 c),
the m. c. p. 's for most -R substituents are an intra-
molecular property independent of solute -solvent inter-
actions. In nonhydroxylic solvents, the m. c. p. 's for
OH and NH2 substituents had fixed values. In hydroxyllc
solvents, the m. c. p. 's were increased for the OH sub-
stituent and decreased for the NH2 aubstituent. The
m. c. p. 's for every -HI substituent substantially de-
creased with the increasing ability of the solvent to sup-
port ionization. These solvent effeas wer* ascribed to
the Increased contribution to the resonance hybrid of the
Isovalent dipolar resonance forms with increased (ioniz-
ing-supporting) solute -solvent interactions.
27
Royal Insc of Tec^. (Sweden).
THE FIRST STEP IN THE ACIDIFICATION OF WO?';
EQUILIBRIA IN 3 M NaC104 AT 250c, by Yukiyoehi
Sasaki. Technical noce no. 8 on Contract AF 61(052)162.
19>me60. 28p. 37 refs. AFOSR-TN-60-178.
Order from LC mitt. 70, pfaK 80 PB ISO 335
Tht reaction betweeti H'*" and the wolframate Ion,
WOJ' has been studied at 250C in 3 M NaClO^ medium
using a glass eleqtrode. The main reaction was found
to be: 7 H-^b WO^' ,j:?3 H,0 ♦ HWfiOjT wldi the equi-
librium conaumi log; K - 60. 68 ± 0. 03. On further
acidification, a range wltli slow reactions was encoun-
tered. The product HW. o5" , which is probably iden-
tical with the "para-wolfrarnaie A" o( Souchay and
others undergoes a slow reaction which does not seem
bemeter to disturb tlie present data, (Author).
^•ce Sciences Lab. , General Electric Co. ,
Philadelphia, Pa.
METHODS OF ANALYSIS OF NEARLY FREE MO-
LECULAR FLOW FOR A SATELLITE OR OTHER
SPACE VEHICLE, by D. Roger Willis. Rept. on Con-
tracts AF 49(638)465 and AF 04(647)269. Aug 60, 32p.
21 refs. Technical Information Series R60SD399.
Order from LC mlW. 00, ph$6. 30 PB 150 170
When a satellite or other space vehicle descends below
a certain altitude, s<yne Intermolecular collisions must
be considered. Various methods suggested for the
analysis of such nearly free molecular flow problems
are discussed. A formal iterative method at solving
Boltzmann's equation for the distribution function is
presented. It Is sho^fn that the first collision methods
represent an approxiinatlon to the calculation of the
first iterate In the proposed method, when the zeroth
iterate is taken as the free molecular solution. The
results of calculatione for a sphere In a high speed
raao floiw, with emergent molecules erf various ener-
!**•. »re presented. Tliese offer quantitative justifi-
cation ot some of the assumptions used in the methods
In the literature, which were limited to low energy
emergent molecules. However, It appears that the re-
sults d those methodA cannot be extrapolated to higher
energy emergent molecules, without paying due regard
to the molecular model employed. (Author).
Stanford Research Inst. , Menlo Park, Calif.
DIFFUSION AND HETEROC^NEOUS REACTION. "^ OL
ATOM RECOMBINATION AT CATALYTIC BOUNDARY,
by Han* Motz and Hetry Wise. Rept. on Project Squid,
Contract Nonr- 1858(25). Dec 59. 5p. 4 refs. Technical
rept. SR1-5-P
Order from LC mljl.,80. ph$l. 80 PB 152 152
See also PB 139 187
aanford Research Ust. , Menlo Pftrk, Calif.
PHOTOCHEMICAL SYSTB^IS FOR SOLAR ENERGY
CONVERSION: NTFROSYL CHLORIDE, by Rudolph J.
Marcus and Henry C Wohlers. Scientific rept. no. 1
on Contract AF 19(604)7302, continuation at Contract
AF 19(604)3477. 15 Aug 60. 52p. 66 refs. SRI ProJ.
SU-3223; AFCRL-TN«60-639.
Order from LC mi$3. 60, ph|9. 30 PB ISO 627
The deslraWe properties dt photochemical conversion
reactions are discussed and a number of possible reac-
tions are listed and rated. Studies of one al these,
the photolysis at nitrosyl chloride, are reported. The
solar furnace was used as a light source for these
studies. All available physical, photochemical, and
thermochemical data on nitrosyl chloride, chlorine,
and nitric oxide have been gathered and are reported
here. (Author)
Stanford Research Inst. , Menlo Park, Calif.
THEORETICAL ffTUDY OF HIGH TEMPERATURE
COMPOUNDS, by A. P. Brady, R. J. Marcus and
R. M. Sllverstein. Technical rept. no. 2 on Contract
Nonr- 2629(00). 9 Dec 59. 27p. 47 refs. SRI Project
no. SU- 2625; AD- 230 601.
Order from OTS J0.75 PB 171 103
Four genersl routes for decompoaition are considered:
homolysis. homolysis followed by radical chain reac-
tion (and a special case a< this, commonly termed
"unzipping"), four-ceAer mechanisms, and cleavage
by partner exchange. A compilation of Isoteniscope
"decompoaition points" is given and selected examples
are discussed in terms of possible decomposition
mechanisms. Four -center types of mechanisms of
decomposition, usually Involving formation of a new
double bond (as does unzipping), are fairly easily
avoided, and none of the more promising high tem-
perature compounds is susceptible to this mode of de-
composition. Cleavage by partner exchange can occur
when there are unused orbltala. It can be alleviated
to some extent by surrounding this atom with bulky
groups. Interpretation al most of the extant pyrolysls
data is hampered by lack of simultaneous information
on rates, activation energy, and initial produas at
decomposition. However, the dau that are available
are compatible with decomposition via radical chain
reactions. Two compounds, terphenyl and diphenyl-
methane, are discussed in some detail from this
standpoint, and a number of others discussed in gen-
eral. Three speculative lines at synthesis are dis-
cussed. One involves a boron -trlazine backbone, the
second a poly-perfluorocyclohexyl ether, and the third
a special P-O-Sl backbone for a "flexible glass."
(Author)
Texas U. [Austin]
ELECTRODE PROCESSES, by L. O. Morgan. Final
rept. on Contract Nonr-375(04). Dec 59, 12p. 10 refs.
AD- 232 403.
Order from LC ml$2.40, pti$3. 30 PB 152 097
Electrode potential changes were correlated with ad-
sorption of Cr (VI) anions on Cr metal surfaces. Ac-
tive and passive surfaces differed in the rate at ad-
sorption. Etched Cr was similar to aalve Cr with re-
spect to potential behavior but had a much larger ap-
parent surface area. Prolonged aging at aqueous solu-
tions of Cr2(S04)3 at 40^0 caused the formation of
species which prevented free precipitation of about 1/3
of the total sulfate present. Four fraaions were rec-
ognized in aged solutions of Cr2( 804)2 separated by
elution from Dowex-50 with NH4NO3 solution. A pro-
posal waa made for the electrolytic oxldaUon of chlo-
rate to perchlorate at a Pi anode. Pt03 forms st the
anode surface under conditions favorable for chlorate
oxldatioo, and an intermediate species is fornoed be-
(treen the oxide and chlorate ions. The internwdiate
gpedes then decomposes into Pt04 and CIO4 ions. A
gtudy was made of the sorption of (W) under conditions
varied as to pH. tungstaie concentration, and the
presence of other anions. Experln»ents were con-
(jucted to utilize proton relaxation measurements on
aqueous solutions of Cr 'III) salts.
Ultrasonics Research Lab. , Western Reserve U. ,
CleveUnd. Ohio.
A. C. STREAMING POTENTIALS, by Irving Galperin,
Ernest Ycager, and Frank Hovorka. Technical rept. 21
on Contraa Nonr- 1439(04). 1 Dec 58, 71p. 28 refs.
AD-229 511.
prder from LC ml$4.50, ph$12.30 PB 152 132
Streaming potential measurements, ac and dc, were
made with parous packings consisting of Ion exchange
resins. Pyrex glass wool, nylon, and cotton in a large
number of aqueous solutions. Special apparatus was
developed for the ac measuremerrts at frequencies from
0 to 30. Results by both methods are in substantially
complete agreement. No frequency dependence was
found over the limited range involved In the present
work. The dependence of the streaming potentials on
type and concentration of electrolytic solution is the
seme ss would be predicted on the basis of published
results obtained by conventional dc methods. Wltb ion
exchange resins such as Amber lite IR-120-Na, the
streaming potentials' were found to increase only 10%
when the particle diameter was reduced from 400 to
40>k This is in sgreement with theory. (Author)
Washington U. , Seattle.
SOLUBILITY OF HYDROGEN AND DEUTERIUM IN
LIQUID ARGON, by H. Volk and G. D. Halsey. Jr.
Rept. on Ckxitract AF 49(638)723. 15 July 60. 27p.
18 refs. AFOSR TN-59-12ia, AD- 242 750.
Order from LC ml$2. 70. phH 80 PB 150 461
The solubility of hydrogen and deuterium in liquid
argon at pressures from 10 to ICX) atm is reported.
Solubility Isotherms have been measured between 87°
and 140OK for hydrogen and between 87° and 120°K for
deuterium. The dependence of Henry's constant on tem-
perature, pressure and concentration, the heats of
solution, the partial molar volume of hj^rogen in
liquid argon and the second vlrial coefficients of hydro-
gen and deuterium in the liquid solution are reported.
The increase in the solubility of deuterium over hydro-
gen is 21. 3%, 20. 2% and 18. 5% respectively at 87, 100
and 120^ This isotope effect is discussed as a quan-
tum correction to the free volume. Comparison be-
tween theory and experiment indicates that the LJD free
volume is too Urge by approxlnutely a factor of five.
(Author).
EARTH SCIENCES
Aeronautical Chart and Informatlaa Cetfer,
St. Louis, Mo.
(SODETIC DI1?TANCE AND AZIMUTH COMPUTA-
TIONS FOR LINES UNCCR 500 MILES. Rev. ed.
Sep 60, 84p. 57 refs. ACIC Technical rept. no. 59.
Order from GTS |2. 25 PB 171 067
This report is a study of various methods of computing
geodetic distance and azimuth. Lines in various lati-
tudes at different azimuths were used for testing the
methods. Methods were evaluated for simplicity,
rapidity, and accuracy (within an allowable error of
ten feet in distance and one-tenth of a degree in azi-
muth). No lines longer than 500 miles were studied.
When positions are given in terms of geographic coor-
dinates, this rejxjrt recommends that the method de-
veloped by Colonel Swing be used for the computation
of the distance and azimuth of lines as long as 500
miles. When positions are given in terms of Universal
Transverse Mercator Grid Coordinates only, this re-
port recommends that the method devised 1^ Major
Hopkins and revised by ACIC be used for the compuu-
tion of distance and azimudi of lines as long as 500
miles. (Author)
Massachusetts Inst, of Tech.. Cambridge.
RESEARCH OH THE PHYSICAL PROPERTIES OF
MARINE SOILS. Sununary progress rept. for Aug 58-
July 59 on Contract Nonr-l841(29). Nov 59, lOp.
5 refs. AD- 229 369.
Order from LCmlSl. 80, ph$l. 80 PB 150 862
Research was conducted to develop knowledge on the
change of soil properties with time and environment.
Experiments indicate that the strength of a clay depends
upon pressure, time, water content, electrolyte concen-
tration, valence of exchangeable cation, sizeof hydrated
exchangeable cation, dielectric properties of the pore
fluid, cations in the pore fluid. pH, temperature and
disturbance. Decrease in temperature of a compacted
kaolinite resulted in loss of strength, while snnall
amounts of salt added to the pore fluid of a clay in-
crease the strength of the msterlal. The effect of time
(elapsed time and strain rate) on the shear strength of
kaolinite was Investigated with triaxlal equipment. The
effects of changes in pH, salt (NaCO concentrations,
and temperature were studied. The literature Indicates
that many fine-grained soils contain carbonates and/or
ferric oxides, and/or organic maaer which cement the
soil particles into aggregants. The effects of potassium
fixation by expandable clays (degraded illites, vermicu-
lite, and beidellite-type montmorlllonltes) was studied.
Fixation of potassium caused these clay minerals to
change to lllite. A clay containing 70% illite and 10 to
15% collapsible vermiculite decreased in void ratio up
to 10% when KCl was sdded to the permeating NaCl
solutions. Consolidation tests were performed on these
clays sediment ed in NaCl solutions at 2 to 1000 psf .
Upon completion of the consolidation tests, the clays
were tested In unconflned compression. They failed
like brittle materials with well-defined shear planes;
the strengths were extremely susceptible to small
moisture changes.
Climatology and Meteorology
Army Signal Research and Development Lab. .
Port Monmouth, N. J.
LAYER- CLOUD HEIGHT MEASUREMENT WITH
STORM- DETECTION RADARS, by Donald M Swingle
and Abraham Golden. 15 July 60. 21p. USASRDL Tech-
nical rept. 2135; AI>241 179.
Order from LC mi$2. 70, ph$4. 80 PB 152 193
29
u\
A theory Is developed for determining the elevation angle
at which a radar set can nxjst accurately measure the
heights of the tops «nd bases of layer clouds. A working
chart is provided wMch permits operators of AN/ MPS- 34
AN/CPS-9 and AN/APQ-13 weather radars to determine:
(1) cloud height (Including standard Corrections for earth
curvature) from range and elevation angle data. (2) op-
timum elevation angle for measuring layer cloud heights
and (3) corrections (o Indicated heights to account for
pulse- length and be^- width distortions. (Author).
Relation between Preclpiutlon Current, PotentUl Grad-
ient and Rate of Rainfall
Comparison of Open and Shielded Receivers
The Mirror -Image Effect
Transportable Apparatuf
Comparison of Preclpitat
Places
Point Discharge
Currents at DifTerent
bedm-
Army Signal Reseatrch and Development Lab. ,
Port Monmouth, nJ J.
PREFUGHT CONDrnONER FOR HUMIIDnT ELE-
MENTS, by C^ientin Prazler. 22 July 60, 28p. USASRDL
Technical rept. 21371; AD- 241 875.
Order from LC ml$21 70, phK 80 PB 152 195
DevelofMnent Is repotted of a device for field condition-
ing and calibrating ol resistance- type humidity ele-
ments such as those used in meteorologic*! sounding
equipmenL The principle requirement for this device
is u an audllary equipment to humidity- temperature
measuring set AN/AWQ-7 and vortex psychrometer set
AN/AMQ-13. This device is used to measure, control,
and maintain specific moisture and temperature envl- *
ronments aa obtained by exposure over supersaturated
•queous solutions of tarlous inorganic salts. Design
features of the chamber include a test section, a hu-
midity control systeni. a humidity ventilation system,
and a temperature coatrol system. The design of each
of the 4 systems <rf 2 experimental models is described
Problem areas, such |ts the elimination of temperature
stratification in the element test section and the
achievement of good Jiumidity measurement and control
are discussed. Design of a third experimental model
i* recommended as a basis for a production model.
Bureau of Shlpe. Wa^ngton, D. C.
MlCROMETEOROLOaCAL ffTUDIES AT SEA. by
PaulM. Wolff. Dec 58, 73p. 4 refs.
Order from LCml$4.k). ep$13.80 PB 152 273
The installation and oj^ratlon of a mlcrometeorologlcal
'*cill^abo«rd a coov«trted Liberty ship is described.
Th^ observations from three cruises off the California
coaat are listed. A brief analysis of temperature and
wlT«3 struaure in the lt)west one hundred feet of the
marine atmosphere is made. Some remarks are in-
cluded CO diffurton at 4ea and on the flow of air around
moving ships. i
Durham U. [Gt. Brit.
RESEARCH ON THE ELECTRICITY OF RAIN, by
J. Alan Chalmers, J. H. Maund and others. Final tech-
nical rept. for 1 Oct 5^-30 Sep 59. on Coniraa
AF 61(614)1072. Il959ll43p. 29 refs. AFCRC TR-
60-227. I
Order from LC mi$3. 3p, ph$7.80 PB 150 929
Contents:
Apparatus for Measuretnent of Precipitatioo Current
with Exposed Receive^
The Rainfall Recorder
The Shielded Receiver
1
ImperUl ColL of Science and Tech. . London (Gt. Briti
RADAR SCATTER BY LARGE HAIL, by It Atlas,
f^ H. Ludlam and others. Technical (scientific) note
no. 2 on Contract AF 61(052)254. tan 60. 38p. 11 refs
AFCRC- TN- 59 -663.
PB 150 420
Order from LC ml$3. 00. pbM). 30
Radars with wavelengths of 3. 3 and 4. 67 cm have been
used to measure the back- scatter cross- sections of In-
dividual artificial hailstones and their variations aa
melting occurs. The measurements confirm the cross-
sections computed theoretically. An ice sphere te a
better scatterer than a liquid water sphere of equal size
when its diameter exceeds 0. 8 wavelengUis; when the
dikmeter lies between 1. 2 and 2. 3 wavelengths it is
better by a factor of 10 or more. Thia behaviour of Ice
Is sifl^wrted by scatter measurements on a set of plexi-
glass (perspex) spheres with refracUve index close to
that of Ice, When melting begins, the 3. 3 cm cross-
sections drop snarply toward the all-Hquid values; those
at 4. 67 cm decrease gradually, and sometimes not at
all. The Implications are that: (1) a water coat of 0. 01
cm thickness has a major effect at 3. 3 cm and a minor
one at 4. 67 cm; (2) liquid continues to collect in sub-
surface cracks and cavities In the ice and causes a fur-
ther decrease In the cross- sections after the maximum
thickness of water coat has formed. The final cross-
sections are generally within 2 db of the all- liquid value
after 7 to 10 minutes of melting at 3. 3 cm and after 15
to 20 minutes at 4. 67 cm.
bitematlonal Inst, of Meteorology. U. of Stockholm
(Sweden).
ON VERTICAL MOTIONS AND TRANSVERSAL QR-
CULATIONS AT THE EASTERN AND WESTERN SIDE
OF LONG-WAVE DISTURBANCES IN TJffi SUMMER
ajBTROPICAL JETSTREAM, by Frledrich Defant.
[Ttechnical (scientific) note no. 7] on Contract
AF 61(514)963. [1959] 66p. 9 refs. AFCRC- TN-60-
226; AD-234 544.
Order from LC ml$3. 90, ph$10. 80 PB 148 262
■nils r^KJrt is part of Investigations on the General
Qrculation of the Atmosphere, with specUl empliasis
on upper atmospheric layers.
International Inst, of Meteorology, U. of Stockholm
(Sweden).
RESEARCH ON STRATOSPHERIC METEOROLOGY,
byFr. Defant. Technical (final) rept. on Contraa
AF 61(514)963. 31 Dec 59, 51p. 6 refs. AFCRC-
TR-60-229.
Order from LC mlJ3. 60, ph$9. 30 PB 150 930
30
International Inst, of Mecfeortflogy, U of Stockholm
(Sweden).
A SYNOPTIC INVESTIGATION OF TOE FLOW AND
MASS FIELD IN TOE CLOSE VICINITY OF THE
SUMMER SUBTROHCAL JET STREAM RELATIVE TO
THE JET-AXIS, by Frledrldi Defant. Technical (scien-
tific) note no. 6 on Contract AF 61(514)963. [1959] 71p.
8 refs. AFCRC TN -60-227; AD 234 373.
Order from LC mi$4. 50, ph$l2. 30 PB 148 263
This report is part of investigations on the General
Circulation of the Atmosphere, with special emphasis
on upper atmospheric layers.
Ionosphere Research Lab. , Pennsylvania State U. ,
University Park.
IONOSPHERIC ELECTRON DENSITIES FOR
WASHINGTON, D. C. , PANAMA, TALARA, AND
HUANCAYO, APRIL-JUNE, 1958, by E. R. Schmerllng.
Scientific rept. no. 128 on Ionospheric Research, Con-
tract AF 19(604)3875. 15 Jan 60, 295p. AFCRC TN-
60-267; AD-234 480.
Order from LC mi$ll. 10, ph$45.60 PB 148 256
See also PB 142 41 L
[Laboratory of Climatology, Centerton, N. J. ]
ANNOTATED BIBLIOGRAPHY ON PRECIPITATION
CHEMISTRY, by John R. Mather. Appendix no. 3 to
Final rept. , Technical note no. 2 on Contract
AF 49(638)409. [1960] 58p. 147 refs. AFOSR-TN-
60-876; AD- 24 1 893.
Order from LC mi$3. 60. ph$9. 30 PB 150 617
Types of precipiutors Involved include: rain water,
dew, fog, cloud, hoar-frost, rime and snow. The
bibliography includes an author Index, a subject outline,
and a geographical outline. (See also PB 150 614)
Naval Ordnance Test Sutlon, China Lake, Calif.
AN IMPROVED TIME- ALTITUDE METHOD FOR COM-
PUTING WINDS ALOFT USING RAWINSONDE DATA,
by Paul H. MiUer. 19 May 60, 15p. 3 refs. NOTS TP
2486; NAVWEPS rept. 7076.
Order from LC mi$2. 40, ph^Sw 30 PB ISO 867
A simplified and readily applicable technique was de-
veloped for rapidly obtaining more accurate winds-aloft
dau based on rawlnsonde information. The method em-
ploys either meters or feet and may be reduced as
levels either above the surface or above mean sea level
(Author).
New York U. Coll. of Engineering. N. Y.
DROPLET COLLISION EFFICIENCY, by
R. M. Schotland. Final rept. on Contract
AF 19(604)2135. July 60. 20p. 4 refs. GRD-TR-60-292.
Order from LC mi$2. 40. ph$3. 30 PB 150 437
An experimental study has been made of parameters
which Control the coalescence of drops in the diameter
range 200 to 800 microns withiarge liquid hemispheri-
cal targets. It is shown that the initiation of the coa-
lescence mechanism for electrically neuual drops in
equilibrium with their vapor is governed by two dimen-
slonless parameters: ""l " ^ V^D/>. •»2 ■ ^m/Pq
where p^ » drop density, p^ - medium density, y
surface tension, Vjj - normal component of impact ve-
locity, and D • drop diameter. (Author).
Quartermaster Research and Engineering Center.
Natick, Mass.
SGME OBSERVATIONS OF THE EFFECT OF DI-
RECT AND SNOW- REFLECTED SOLAR RACHATION
ON EXPOSED AND SHIELDED TH ERMOCOUPLeS, by
Femand de Perdn. Apr 58, 7p. 2 refs. Research
Study rept. RER-19.
Order from LC ml$l. 80. ph$l. 80 PB 152 070
This report released for sale to the public 7 Nov (60.
Tentative conclusions drawn from this brief stxxly are
as follows: (a) Well -shielded thermocouples of any
size will measure temperatures closely corresponding
to those recorded in the standard type instrument
shelter, (b) Exposed, bare thermocouples will be af-
fected by solar radiation, and temperatures recorded
will usually be higher than those obtained from shielded
thermocouples or by thermograph readings in an In-
strument shelter, (c) Exposed, white-coated thermo-
couples were affected by solar radiation almost as
much as the bare thermocouples, (d) Small gauge
shielded thermocouples (36-gauge or smaller) respond-
ing rapidly to changes in air temperature, are probably
more representative of the actual fluctuating air tem-
peratures, and differ from temperatures recorded by
larger size (20-gauge) thermocouples or those re-
corded by usual means (thermograph) in an instrument
shelter*.
Quartermaster Research and Engineering Center,
THE SIMMER CLIMATE OF THE LAKE PETERS
AREA, BROOKS RANGE, ALASCA, by Femand
de Perdn. Interim rept. Nov 58, Up. Research
Study rept. RER-2S.
Order from LC ml$2. 40, ph$3. 30 PB 150 765
This report released for sale to the public 26 Oct 60.
This report briefly describes the meteorological
measurements made during summer 1958 In a little-
known part c^ the Alaskan Arctic.
Travelers Insurance Co. , Hartford, Conn.
SELECTING VARIATES FOR MULTIPLE DISCRIM-
INANT ANALYSIS WITH AN APPLICATION TO SHORT
PERICX) FORECASTING OF* AIRFIELD CEILING
CCWDITICWS. by Robert G. Miller. Final rept. for
1 Apr 58-31 Mar 60 on Contract AF 19(604)3878.
July 60. 239p. 29 refs. AFCRC- TR- 60- 254.
Order from LC mi$10. 20. ph$36. 30 PB 152 050
A major portion of the work was devoted to the deriva-
tion of a statistical technique for selecting varlates in
discriminant analysis and the application of this tech-
nique to the problem of predlctli^ ceiling conditions
two hours in advance at McGuire Air Force Base. The
eittlre analysis i^s directed towards ultimate appllca-
31
tlon <rf the technique and the re«ult» to problems at
operational decision-making. A seml-technlcal sum-
mary erf the more Important concepts used In this study
and a summary of the results at the celllm experiment
U Included. (See 4Iso PB 143 579)
Geology
Heat TVanafer La|). , Mass. Inst, o* l^ch. .
Cambridge.
AN ANALYSIS OF METHODS AND EQUIPMENTS FOR
MEAajRINC HEAT PLOW THROUGH THE SOIL, by
Richard J. Nlckerson and Aydln Umur. Rept. on Ooo-
tr«:t DA 36-039-sc'78174. Feb 60, 22p. 10 refs
AD- 237 049. *^
Order from LC mi«. 70, phK 80 FB ISO 444
Consideration was given to measuring heat flow throv«h
•oil by means d a heat flow meter and by means o^ a
thermal condualvlty probe. The heat flow meter con-
sists d a thermal resistance across which the temper-
ature difference is oieasured and used (with calibration)
as an Indication at tbe rate at heat flow, b is a steady
state device and indications at heat flow are continuous
Objections to the heat meter were the Interference al
the meter with the normal moisture flow and the natural
beat flow, Temperature distributions obulned by the re-
Utttion method were used to describe several cases at
tbe distortion d heat How lines in a uniform medium
caused by the presence of the heat meter. Numerical
analysis indicated that distortion and OMSiderable error
occurred if too great *n unbalance exists between meter
«nd medium conductivity. The thermal conductivity
probe is a transient device consisting at a cylindrical
tube which contains a heater and temperature indicator.
The thermal response at this device when burled In a
large medium and siAjected to a consunt rate at heat-
ing can be used as an Indication at the thermal conduc-
tivity d the surrounding medium. An analysis by
Backwell (J. Appl. Phys. 25. No. 2. 137-144. 1954)
was given for a hollow probe burled in an faiflnlte, uni-
form medium when heat was generated at tbe outer
•uiface and temperaaire was measured at the toner
surface.
HeM Transfer Lab. i Mass. fast, d T^cb.
Cambridge.
METOODS AND EQUIPMENT FOR MEASURING TEM-
PERATURB AND HEAT FLOW THROUGH THE SOIL
by Richard J. Nickerion and Aydto Utnur. Final rept *
on Contract DA 36-03i9-sc-78174. tan 60. 2^ 6 nrfs
AD- 237 116. ^ ^ '
(Wer from LC ml|2,70. phR 80 PB 150 445
The design and construction o* a thermal conductivity
probe and a beat flow meter are discussed for measur-
big the heat flow and «ie temperature d soils. When
d^mnlniag hemt flow witii die tfiermal conductivity
prow, the probe is buried to the soil and measurements
Of sou conductivity are made simultaneously with tbe
local temperature gradient. The technique cannot be
made continuous by recording to a simple fashion. TTie
heat flow meter provides a heat flow resistance to the
•o'l-JWdi suitable calibration, a measurement d the
tmpmture drop across tbe faces d the meter, which
can be cootiiniausly racorded, provides a measurement
d the heat flow through the meter. The most importaa
requirement for the cylinder to be used for heat meter
tests is that die flow wlthto the cylinder be one-dlmen-
slonal at a distance from the heat meter. The thermal i
conductivity probe was used in experiments on a clear
plastic, a black silicone rubber tosuUtlijg materUl.
Kaylo (an tosulatlon board), and Santocel (a powder).
Serious discrepancies existed between the values of
thermal conductivity obtained with this device and those
determined by the Guarded Hot Plate tests for the plas-
tic and rubber specimens.
Navy Electronics Lab. , San Diego, Calif
PHYSICAL LIMNOLOGY OF LAKE MEAD, by
E. R. Anderson and D. W. Pritchard. Final rept. on
Lake Mead Sedimentation Sunrey. 11951) I52p. 12 refs
Rept. 258.
Order from LC mi$7. 50. ph$24. 30 , PB 152 643
This report released for sale to the public 7 Nov 60.
The general circulation and evaporation of Lake Mead.
Nevada, were determined from data gathered during
monthly survey cruises over the period February 1948
through February 1949. The circulations, based on
salinity patterns, did not materially differ In the win-
ters of 1948 and 1949. although the latter was much
colder, and It Is believed that the important features
d the circulation for all seasons sre repeated from
year to year. The total annual evaporation, computed
from a preliminary energy budget, was 161 cm, the
monthly average being 13. 4 cm as compared with a
monthly average of 8. 4 cm for the oceans. The work
was done to conjunction with the U. S. Geological Sur-
vey and other government agencies cooperating in a
Umnologlc and geologic survey d the lake. (Author)
Quartermaster Research and [Engineering] Center,
Natlck. Mass.
THREE MOUNTAIN AREAS IN SOUTHWESTERN
WYOMING, by Max E. Morris and William C. Robisoa
Sep 55, 37p. 27 refs. Research Study rept. RER-6.
Order from LC mlJ3. 00, ph$6. 30 PB 150 766
This report released for sale to the public 26 Oct 60.
The three mountain areas presented are: The Wind
River Range; The Wyoming'Salt River Range; and
The Ulnu Range. This report describes environ-
mental conditions affecting mibtary operations In the
■-~— 'tins.
inountai
'n
Oceanography
Hydraulic Bnglneerliig Lab. , U. of California,
Berkeley.
SILT TRANSPORT STUDIES UnuZING RADIOISO-
TOPES, by R. B. Krone. Annual prc^eaa rept. no. 1.
pa 56-Dec 57, on Contraa DA 04-203-CIVENG-57-61
(1958J 125p. 99 refa.
Order from LC mi$6. 30, ph$19. 80 PB 152 645
Thla report released for sale to the public 7 Nov 60.
32
Ttals research has been primarily concerned with the
development d a means d measuring the movement d
sediment. Conclusions regarding this method, as out-
lined in this report, can be summarized as follows: (1)
The movement d sands has been satlsfaaorlly traced
using g]:ound glass containing diasolved gamma emit-
dng radioisotopes. (2) The physical properties of
clayey sediments In salt water made inert particulate
tracers unsatlsfaaory for tracing these sediments.
(3) Simple sorption of gold- 198 or 8candium-46 on wet
clayey sediments provides an inexpensive and con-
renlent means of labeling these materials. (4) The
ultimate elutable label depends on suspension concen-
tration. (5) An underwater scintillation detector has
sstlsfactory sensitivity for detecting snull amounts of
labeled sediment. (6) Because of the shielding proper-
ties of water for gamma particles the resolution of the
detector for variations in tracer concentration is good.
(7) The problems of underwater detection associated
with unknown spatial distribution of radioactive mate-
rial can be resolved by a vertical traverse of the
sctlvlty, or for burled tracer, by core samples. (8)
Successful quantitative application of the method re-
quires foreknowledge of the qualitative sediment
regimen in the problem area.
Scrlpps Institution of Oceanography, U. of California,
San Diego.
MARINE MICROBIOLOGY, byCUudeE. ZoBeU. Final
rept. for 1 July 50-31 Jan 60 on Effects of High Hydro-
sutlc Pressure and Other Factors on the Distribution
tod Physiological Aalvlties of Marine Baaeria, Con-
traa Nonr- 221 6(00); Continuation of Contraa N6anr-
275(18). 31 Jan 60, lOp. 17 refs. SIO Ref. 60-14;
AD- 236 847.
Order from LCml$l. 80. pmi. 80 PB 147 175
Summary of reaults on: development of apparatus;
some effeas of high pressure on the viability of bac-
teria; effea of compression on baaerlal mcnrphology;
mutagenesis Induced by pressure; effect of compres-
sion CO phosphate aalvlty; pressure Inhibits nitrate
reduaion; effea of pressure on succinic defaydro-
Ipnase; effea of pressure on urea-urease system;
activity of an aspartase accelerated by pressure; stud-
ies on sulfate- reducing bacteria; denaturation of
glycosldase by compression; adaptation of marine
bacteria to increased pressures; heat of compression
of aqueous systems; oxygen tension In compressed
cultures; kinetics of baaerlal growth; partldpatian in
oceanographlc expeditiona. -
Texas A. and M. Coll. . College Stadon.
AN ANALYTICAL SYSTEM FOR INTERPOLATION
AND CALCULATION OF DYNAMIC HEIGHTS, by
R. B. Kilmer and A. C Duxbury. Technical rept. on
Contraa N7onr -487(02). Nov 59. 35p. 4 refs. Refer-
ence 59-24T; AD- 232 880.
Order from LC ml$3. 00. pb$6. 30 PB 150 487
A dau processing system was designed to provide a
rapid procedure for the computation and evaluation of
hydrographlc dau. This method Is funaional and accu-
rate. Although the final depth cards do not correspond
to the proposed totematlonal form (1. C E. S. ), (1958).
Ibey may easily be converted to this form for Incer-
aatlonal use. The compufl|^ calculations are completely
abjective and any varlatlona In the Interpolated curves
which do not meet the approval of the classical ocea-
Bographer may be changed at the discretion of the to-
vestlgator. (Author)
Washli^onU. . Seattle.
THE DYNAMICS OF A FIORD ESTUARY: SILVER
BAY. ALASKA, by William Bruce McAlister. Maurice
Rattray. Jr. and Clifford A. Barnes. Technical rept.
no. 62 on Contraas Nonr-477(10) and 477(01). Nov 59,
77p. 14 refs. Reference 59-28; AD-230 537.
Oixler from LC ml$4. 5a pfa$l2. 30 PB 150 497
Observationa of water properties aiid movements made
in July 1956 and March 1957, are used to describe the
dynamics involved in the circulation of .waters in Silver
Bay. Alaska. Thla is an estuary system of a type com-
monly found along the coasts of British Columbia snd
Alaska. The 2 seasons are representative of the ex-
treme of summer and winter oceanographlc conditions
which occur in this locality. In a tidal estuary, the
addition of fresh water by river rumff produces mass
and velocity fields to accordance with the principles of
fluid mechsnlcs. While the equations describing the
distribution of maas aixl velocity are not solved In gen-
eral, tbe individual terms In the equations are evaluated
for Silver Bay. With hi^ runoff, and consequent large
density gradients, results show thst the pressure gra-
dient, in the surface layerp la largely balanced by the
inertlal terms. With the low riinoff, the pressure gra-
dient balances the vertical stress gradient. The salt
balance of the estuary is maimatoed primarily by advec-
tive processes. (Author)
Washington U. . Seattle.
PHYSICAL AND CHEMIJAL DATA, NORTH PACIFIC
OCEAN, by Richard H. Fleming. Special rept. no. 30
on Brown Bear Cruise 1,99. July-August 1958 for the
totematlonal Geophysical Year of 1957-1958. Contraa
Nonr -477(10). National Science Foundation Grants
Y/9.7/79andY/9. 14/139. Mar 59. 21 Ip. 10 ref a.
Ref. no. 58-32.
Order from LC ml$9. 60. ph$33. 30 PB 148 267
The major objealves were: (a) To reoccupy CARNEGIE
Stations 1 26 through 1 32 to determine changes in the
properties of the deep water during the 29-year interval
sibce 1929 when these stations were last occupied, (b)
To study the transition zone between Sub -Arctic and
Subcroplc Water masses in the Northeastern Pacific
Ocean. In addition, a comprehensive program of ocean-
ographlc sampling was carried out along the cruise
track. (See also PB 139 858)
Woods Hole Oceanogri4)hlc tostltution, Mass.
OCEANOCaUPHIC DATA FROM CRAWFORD CRUISE
22: TRANSATLANTIC SECTIONS AT EQUATOR AND
24° SOUTH FOR THE INTERNATIONAL GEOPHYS-
ICAl^ YEAR OF 1957-1958. by W. G Meicalf. Rept.
on Contract Nonr-2 196(00). Jan 60. 149p. Reference
na 60-3; AI>237 815.
Order from LC ml$7- 20. ph$22. 80 PB 148 125
Temperature, aallnlty and oxygen profilea are pre -
sented on s base showing observstion potots and bottom
contours. The Depth of the observations haa been
^'
33
■a.
rounded off to the nearest five meters. Sal4nltle8 were
determined on the W^ods Hole sallnometer, K4odel 2,
*n Improved version of the instrument described by
Schleicher and Bradsliaw (1956). Dissolved oxygen de-
terminations were c«-rled out by the Winkler method.
The determinations at inorganic pho^onu, total
phosphorus and chloitjphyl were carried out. A detailed
sounding track is pre^nted.
Woods Hole Oceanographic Institution. Mass.
OCEANOGRAPHIC DATA FROM THE R. R. S. DIS-
COVERY IL INTERNATIONAL GEOPHYSICAL YEAR
CRUISE 3. 1958, by L. V. Wonhlngton. Rept. on Con-
tract Nonr-2196<00). Nov 59. 94p. 5 refs. Rcf no.
59-54; AD- 231 105. '
Order from LC ml$5. 40, ph$l5. 30 PB 150 529
Physics ol rhe Afmosphar*
Army Research and pevelopment Lab. , Fort
Monmouth, N. J.
ON THE STRUCTURE OP THE UPPER KDNO-
SPHERE. by Slegfriedi J. Bauer. 1 July 60, 27p. 24 refs.
USASRDL Technical rept. 2131; AD- 240 12«.
Order from LC miJ2. 70. phK 80 PB 150 452
Properties of ionosphetic models are discussed with
emphasis on the regio«> above the F2 peak and iono-
spheric parameters otxainable from moon radar,
rocket, and satellite observations. Examples of elec-
tron-density profiles for ionospheric models assuming
a scale- height gradienf and height- dependent electron
loss are presented iir graphical form. The basic
model for the electron density distribution in the iono-
sphere is the Chapman distribution, which was de-
rived on the basis of equilibrium between electron- ion
production by solar radiation and decay by height- in-
dependent recombination in an isothermal atmosphere.
The scale- height strucfure of the i^jper atmosphere
based on satellite data 48 briefly discussed. A modi-
fied Chapman distribution with a positive scale- height
gradient is shown to bei consistent with the electron-
density profile above tHe F2 peak obtained from re-
cent rocket measurements.
Army Signal Research and EXevelopment Lab. .
Fort Monmouth. N. J.'
PRELIMINARY ESTIMATES OP VARIABILITY OF
WINDS IN THE LOWE$T 500 FEET, by Raymond L
Bellucci. 15 June 60, l^p. 2 refs. USASRDL Technical
rept. 2122; AD- 241 176,
Order from LC ml$2. 40, ph$3. 30 PB 152 189
This report describes m experiment which was de-
signed for the purpose of determining the time varia-
tion of the wind in the lowest 500 feet, using the double
theodolite wind set for obtaining winds. The results of
the experiment led to ec|uatioos describing the surface
wind variability with ttnle and wind speed at Belmar,
New Jersey. (Author)
Ballistic R#»search Labs . . Aberdeen Proving Ground.
aJMMARY REPORT ON BRL-IGY ACTIVITIES, by
SpenceT. Marks. Apr 60. 174p. 61 refs. Rept.
no. 1104.
Order from LC ml|8.10. ph$27.30 PB 150 417
The historical badtground of the IGY Is reviewed
briefly. Activities in which BRL participated are
described. A number of studies peninent to IGY re-
search are presented. BRL-IGY program summarie*.
and research results are given. These include: The
Rocket Tracking Program, the Rocket Research Pro-
gram, the Balloon Research Program, the Electron
Density Program, and the Satellite Tracking Program.
A bibllography.of BRL-IGY reports , publications , and
presented papers Is also included . (Author)
'^ Electronics Research Lab. , Northeastern U. .
Boston, Mass.
RESEARCH DIRECTED TOWARD THE DEVELOP-
.MENT OF PHOTO- OPTICAL. ELECTRONIC. AND
CALIBRATION APPARATUS, by Louis J. Nardone.
Final technical rept. on Contract AF 19(604)1749.
31 Mar 60, 56p. AFCRC TR-60-234; AD- 234 043
Order from LC ml$3. 60, ph$9. 30 PB 148 257
In si^jport of the upper-air research program, activi-
ties conducted were primarily concerned with direct
and indirect support of projects dealing with micro-
meteorite detection, measurement of day air-glow, and
the installation of a data- reduction facility. A micro-
meteorite detection experiment launched from Holloman
Air Force Base, New Mexico, failed to yield the de-
sired information, because the nose-cone tip failed to
eject. An experiment was launched from White Sands
Missile Range, New Mexico to obtain measurements
perulnlng to sky brightness and the theoretical en-
hancement of the 6300A oxygen line. Preliminary re-
sults hxllcated a sky brightness of less than 1. 08 x
10-'*cd/ft2 above 175,000 feet. Since no indication of
the 6300A line was recorded, it was concluded that
this line must have a strength of less d;an 0. 5 kilo-
raylelghs, the maximum sensitivity of the recording
instnmientation. A data- reduction facility was estab-
lished to handle data obuined primarily from fm-fm
telemetry systems. An equipment development pro-
gram to support the major activities include a mag-
netic beam- switching tube counter and an Improved
facsimile recorder to assist in data reduction. De-
scribed also are a telemetry subcarrler separator used
with the five lowest standard telemetry channels, and
a preliminary investigation conducted to determine the
feasibility of constructing a rocket-borne, low-fre-
quency, solar-noise receiver. (Author).
Lichtkllmatisches Obeervatorlum Arosa (Switzerland)
VERTICAL OZONE DISTRIBUTION OVER AROSA
FROM THREE YEARS' ROUTINE OBSERVATION OF
THE UMJCEHR EFFECT, by Hans Ulrich Dfitsch. Final
rept. on Ozone and General Circulation In the Strato-
sphere. Contract AF 61(514)905. Sep 59, 57p. 8 refs
AFCRC-TR-59-290; AD-230 332.
Order from LC ml^. 60, phJ9. 30 PB 152 056
Contents:
Obeenrations
Extension of observations to very low sun heights
Calibration
Observations on cloudy sky
Evaluation of the vertical orone distribution from
Vmkehr observations on wavelength pair C
Secondary scattering
Influence of temperature on absorption coefficients
Comparison with other methods
Ramilta on vertical distribution
Seasonal variations oi ozone concentration at different
helots
Influence of large scale deviations from the normal
circulation pattern
Some single ozone distributions connected with special
VBStber situations
Vertical ozone distribution, single cases
Oklahoma SUte U. Research Foundation, Stillwater.
PROVIDE SERVICES TOWARD INSTRUMENTING
AEROBEE ROCKETS, by RJchard F. Buck. Final rept.
on Contract AF 19(604)2029' 31 July 60. 63p. AFCRL
TR-60-401 '
Order from LC mi$3. 90. ph$10. 80
PB 150 873
A wide variety of support activities have been conducted
vbich may be separated Into two broad classes: (1) di-
rect support In the form of man-power and equipment
lor bunch missions at the firing sites, where upper
air research experimentation has been conducted
through the use of rocket sounding vehicles and (2) in-
direct support activities, which have been concerned
with activities in the Stillwater laboratory. These have
provided the necessary equipment and facilities for
these research instrumentation vehicles. (Author)
Sunford Research Inst. , Menlo Park, Calif.
ATMOSPHERIC RADIATIVE HEATING AND COOLING,
bjr K. L. Coulson. Scientific repc. no. 1 on Contract
AF 19(604)5965. Mar 60, 40p. 44 refs. SRI Proj. 2994;
ARPA Order no. 26-59; AFCRC TN -60-273; AD-234 972.
Order from LC mi$3. 00, ph$6. 30 PB 148 255
Is an effon to develop a iwn-adiabatlc atmospheric heat-
ing model for use in dynamical -numerical investigations,
the various sources and sinks of radiative energy in the
atmosphere are discussed. For this study, the atmos-
pbere is divided vertically into 4 regions, each of which
has a radiation regime peculiar to Itself. The tropo-
spherlc radiation balance is controlled principally by
wster, either as vapor or as the liquid water of cloud
droplets. Processes In the troposphere combine to
cause a net radiative cooling of 1 or 29C per day. The
stratosphere, taken as the region from the tropopause
upward to the base of the ozonosphere, Is characterized
by small radiative effects which combine to produce
radiative quasi -equilibrium. The ozonosphere Is heated
by ozone absorption of solar radiation and cooled bv
long-wave emission from carbon dioxide and ozone. The
maxima of both heating and cooling occur at a height of
45-50 km, and the magmtudes are both of the order of
5-lOPc per day. Thus there is much cancelling of
sources and sinks. The mesosphere, consisting of the
region from about 55-60 km to the height of the temper-
nure minimum at about 80 km. Is generally considered
to have only minor radiative temperature changes. It is
Wggested that if the probable increase of ozone concen-
tration at night is taken into account, considerable cool-
ing could result from the long -wave emission by ozone.
Rapid photodissoclation of the ozone after sunrise pre-
vents much solar energy absorption during the day.
(Author)
Upper Air Lab. , U. of Colorado, Boulder.
RADIOMETER FOR HIGH ALTITUDE RAMATION
MEASUREMENTS, by Edward P. Todd and Frank E.
Stuart. Final rept. on Contract AF 19(604)1899. [1960]
84p. 16 refs. GRD TR-60-286.
Order from LC ml$4. 80, ph$13. 80 PB ISO 753
A history of the development of the miniature radiom-
eter for satellite use Is given with a more detailed de-
scription of the units. The solar consunt radiometer
is also discussed. Prior to the development of these
radiometers three radiometers, incorporating various
design features vdiose performance It was desired to
test, were built and flown in a series of four balloon
flights. These flights are described.
Willow Run Labs. . U. of Michigan. Ann Arbor.
ANALYSIS OT A FALLING- SPHERE EXPERIMENT
FOR MEASUREMENT OF UPPER-ATMOSPHERE DES-
SITY AND WIND VELOCITY, by J. Otterman,
I. J. Sattinger and D. F. Sniih. Rept. on Contract
AF 19(604)5205. Apr 60, 58p. 18 refs. Rept. no. 2873-
5-F; AFCRC-TR-60-218.
Order from LC mi$3. 60, ph|9. 30 PB 150 421
A method Is described by which upper-air density and
wind velocity can be determined by measuring th6 drag
acceleration of a falling sphere by means of accelerome-
ters mounted on an Inertial platform carried within the
sphere. An Investigation was made to determine the
size, weight, and accuracy cf available inertial plat-
forms. An analysis based on this information shows
that air density and wind velocity can be jneasured by
this method up to altitudes of at least 150 km and 120 knv
respectively. The error In air-density measurement
would be 20% or less, and the wind- velocity error
would be 10 m/sec or less. Some at tbe major consid-
erations In the design of the system are discussed,
particularly those Involved in the selection or design of
the rocket. Inflatable sphere, and Inertial -platform sys-
tem. (Author) (See also PB 147 762)
ENGINEERING
Aeronautical Engineering
Aeronautical Engine Lab. . Naval Air Material Ceoter.
Philadelphia, Pa.
DEVELOPMENT OF TURBO-JET ENGINE THRUST
DESTROYING AND REVERSING NOZZLE NO. ABL
102, by I. P. Polak. Rept. oa Pro). TED no. NAM-PP-
375 and TED no. NAM-04614. [13 Jan 50] lOlp. 9 refs.
AEL-1106.
Order from LC mi$5.70. pb$l6. 80 FB 152 641
This report released for sale to tbe public 10 Nov 60.
The results of ground and flight tests cfibducted with
tbe nozzle Insulled on FR-I airplane* indicate that the
use of tbe nozzle to provide rapid variation of thrust la
a substantial improvement over control by throttle.
Tbe improvement Is especially iKXiceable in operationa
such ^s: (a) reducing speed immediately after a cut on
a carrier -landing approach (b) reducing the landing run
of non-carrier airplanes (c) Increasing speed Immedl*
ately after a wave-off on a carrier landing approach.
Tbe results cf flight tests with the nozzle inscalled on
35
« PR-1 airplane alio Indicated that thla aircraft'*
stability and trim were critically altered by partial
and reverse thrust nozzle operatloo. Nozzle InstaUa-
lloo effects on the tircraft'a lift and drag were
negligible. (Author^
Aerospace Medical Mv. , Wright Air Development
Div. , Wright- Patterson AFB, Ohio.
USAGE RATES OF AIRCRAFT OXYCTN, by Margaret
M. Jackson. Rept. 9n Physiology of Flight ProJ. May 60
20p. 13 refs. WADO Technical rept. 60-106
Order from OTS |0. 50 PB 171 087
An Investigaaoo wa4 conducted to evaluate aircrew oxy-
gen requlrennents for current and ftmire aircraft. A
Uierature review of studies on die rate of oxygen use in
flight is presented. JData from actual flights, alUtude
chamber studies, and simulated missions on a jet
trainer and F- 102 simulator with subjects wearing full-
head pressure helm«s or oxygen masks is presented
and discussed. Results of the investigation indicate
that aircraft oxygen Installation figures, when baaed on
a pulmonary ventilation rate of 25 I. /mln. BTPS, will
provide an adequate caygen supply for 99 percent of the
Air Force personnel performing duties equivalent to
light work at cabin altitudes up to 35,000 feet. Loaa
of cabin pressure with subsequent exposure to hloher
altitudes increases tl»e requirement for oxygen. (Author)
Air Force Flight Tfcst Center, Edwards AFB, Calif
SA-16B LIMITED PHASE IV STABILITY CONTROL
AND PERFORMANCE, by Charles C. Crawford and
TommleD. Benefleli Oct 57, 90p. AFFTC-TR-57-16;
Order from LC mlH 80. ph|13. 80 PB 152 296
This report released for sale to the public 27 Oct 60.
For comparable fuel Aoads, the SA-16B overall per-
formance la sig>erlor to that of die SA-16A. The single
engine capability of tke B nvxlel indicates a consider-
able improvement over the A model. The single engine
service ceiling of the SA-16A for a gross weight of
32.000 pounds is sea level while the SA-16Bs single
engine service ceUlng is 4, 300 feet for a climb sttrt
gross weight of 33. SOD pounds. Comparison of the basic
radius mlssloq erf theae aircraft shows the SA-16B has
a radius of 805 nautical miles as compared to a radius
of 699 nautical miles for the SA-16A, based on equal
fuel loadings of 7425 founds of ftieL The stability con-
trol and handling characteristics of the SA- 168 are ac-
ceptable. (Author).
Army TransportatiaiRMearchCaairaand. Port
Eustls, Va. I
PROCEEDINGS OF A NATIONAL AERONAUTIGS
AND SPACE ADMINISTRATION (NASA) BRIEFING
ON AIRCRAFT RESEARCH. Rept. aa a Technical
Review of VTOL/STOL Principles That May Be Applied
to U. S. Army Requlranents. 15 Dec 59, 102p.
475 refs.
Order from LC ml$5. 70. ep$18. 30 PB 152 752
I
Thl* report released ior sale tb the public 17 Nor 60.
Contents:
General performance characteristics of VTOL/STOL
aircraft, by Richard E. Kuhn and Marlon O.
McKlnney, Jr.
Stability and control of VTOL/STOL aircraft, by
Robert O. Schade, Robert J. Tapscott, and Woodrow
L. Cook
Limited fligte experience with several types of VTOL
aircraft, by John P. Reeder and Fred J. i
Drlnkwaier, III.
Arnold Engineering Development Center [Tlillaboma
Tbnn].
AN INVESTIGATION OF EJECTORS WITHOUT IN-
DUCED FLOW. PHASE I. by D L. Barton and
D Taylor. Rept. on ARO, hic. , Oontraa AF
40(600)800. Dec 59, 42p. 4 refs. AEDC TN-59-145.
Order from LC ml$3. 30. ph$7. 80 PB 152 647
This report released for sale to the public 10 Nov 60.
An Investigation was conducted to determhie the effects
c* nozzle are* ratio and nosale throat to dtffuser area
ratio on performance of ejectors without induced flow.
Five nozzles having constant exit diameters and differ-
ent throat diameters were tested in three dlffusers
having different diameters. All nozzles had conical
contours wltfj a 36-deg total efflux angle, and all dlf-
fusers had length to diameter ratios of 3. 0. Test cell
pressure ejector nozzle driving pressure, exhaust
pressure, aid dtffuser sutlc pressure profiles were
measured Data from all configurations were analyzed
to determine the effects of ejector geometry on per-
'omianc* /Author^ j e i t^
Arnold Engineering Development Center (Tullahoma.
Tenn].
PRESSURE DISTRIBUTION TESTS OF SEVERAL
SHARP LEADING EDGE WINGS. BODIES AND BODY-
WING COMBINATIONS AT MACH 5 AND 8 by
R. E. Randall, D. R. Bell, and J. L. Burk. Rept. on
ARO. Inc. Contraa AF 40(600)800 S/A 11(60-110).
Sep60. 60p. 2 refs. AEDC-TN -60-173.
Order from LC ml$3. 60, ph$9. 30 PB 150 985
Pressure distribution data were obtained on several
sharp leading edge wings, conical bodies, and body-
wing combinations at Mach 5 and 8. The unit Reynolds
number was varied from 0, 8 x 10* to 6 x 10^ per foot
to determine the effect on the pressure distribution.
The angje-of -attack range was from -10 to +20 deg.
aadowgraphs of shock wave and boundary layer phe-
nomena were obtained at various aisles of attack.
Vapor screen photographs were taken with liquefied Oow
condidans in die test section to visualize the crocs -
sectlooai shape of the shock wave. (Author)
Naval Air De-
Avlation Medical Acceleration Lab.
- velopment Center. JohnsvUle, Pa.
CENTRIFUGE SIMULATION OF THE X- 15 RE-
SEARCH AIRCRAFT, by Carl C. Clark and
C. H. Woodllng (National Aeronautics and Space Ad-
ministration). Rept. no. 9 on Proj. MR OOS. 12-0005 4
and Proj. NM 11 02 12. 4. 10 Dec 59, 36p. 17 refs
NADC-MA-5916; AD- 233 340.
Order from LC ml$3. 00. ph|6. 30 PB 148 274
36
Three X- 15 centrifuge programs were conducted. The
first program Involved 168 runs under cam control,
with the subject receiving accelerations predicted for
the X- 15 as if he were a passenger. For the other two
programs, the newly developed technique of pilot-com-
puter "closed- loop" control of the centrifuge, or cen-
trifuge dynamic control flight simulation, was utilized
with the pilot receiving accelerations computed for the
X-15 under his own control while he carried out the
assigned flight mission, involvlnjt re-entries at vari-
ous angles of attack and peak normal loads with and
without speed brakes, and with or without control aug-
mentation (dampers). During these two programs,
991 "static" flights (centrifuge at rest) and 433 "dy-
namic" flights (centrifuge in motion) were made on the
centrifuge simulator. Pilots who were properly fitted
Into the seat and restraints; had at least 10 hours of
static simulator practice; and had previous high ac-
celeration experience could control the X-15 centrifuge
simulator through parts of the design missions (com-
puted aircraft speeds greater than Mach 2) while re-
ceiving the accelerations greater than 1 G continuously
conoputed in magnitude and direction as a consequence
of their control and used as centrifuge drive signals.
Pllqts who did not meet these specifications did notably
less well dynamically than statically, a consequence
attributed to their incorrect control responses whUe
under acceleration or to their leas rapid detection of
and correction for the involunury pilot inputs produced
by the flight loads. (Author).
Bolt, Beranek and Newman, Inc. , Cambridge, Mass.
FIELD MEASUREMENT OF COMMUNITY NOISE
EXPOSURE NEAR HANSCGM AIR FORCE BASE,
MASSw , by A. C. Pletrasanu. Rept. on Investigation
and Control of the Acoustic Charaaerlsrlcs cf
Air Force Noise Sources, Contract AF 33(616)3938.
Ai« 58, 28p. 1 rcf WADC Technical note 58- 163;
AD- 155 879.
Onler frtwn OTS 10.75 i PB 171 076
T
The noise e^tposure at a location near Hanscom Field
was measured for an eight-hour period by recording
the noise levels from all aircraft flyovers during this
period. The measured noise exposure, In terms of the
equivalent continuous sound pressure level In the 300-
600 cps band (Leq) ^^' found to be 74 db. It is com-
pared with several calculated values of Leq which
differ depending on whether assumed or actual flight
paths, flight profiles, or activity dau were used. For
assumed values for each of these three items, the cal-
culated Leo 's 79 db. Fpr the observed fliitht path,
flight profile, and aircraft activity, the calculated and
measured. Leq s sre In agreement. (Author)
Diamond Ordnance Fuze Labs. . Washington, D. C
BALLOON FOR SOFT IMPACT LANDING, by
H. D. Curchack and R. E. Van Der Linden. 29 Au« 60,
I9p. TR-863.
Order from LC mi$2.40, ph$3.30 PB 152 315
The top of a balloon striking a flat rigid surface would
be cushioned by the gas within the balloon, and the
feasibility at using this effea to cushion a load in high-
velocity impacts was investigated. A one-dimensional ,
analysis of the impact was made assuming that the
balloon la of moderate dimensions (from 3 to 30 ft in
diameter), that the Impact velocity Is either the nraon
escape velocity or 500 fpe, and that the otily force de-
celerating the top of the balloon Is supplied by gas
within It. Results indicate the system Is not feasible
for Impaa velocities as hl^ as the moon escape ve-
locity, but that the system may be feasible If the Im-
pact velocity la reduced through use of retrograde
rockets to about 500 fpe. (Author)
Diamond Ordnance Fuze Labs. , Waahlngton. D. C.
PRELIMINARY STUDY OF POWER SUPPLIES FOR
PNEUMATIC SYSTEMS, by D. J. Grant, A. Krasnlck,
andS. Katz. 30 June 60, 50p. 10 refs. TR-847.
Order from LC ml$3.30, ph(7.80 PB 152 313
A preliminary study was made of power supplies for
pure pneumatic systems Including a survey of several
representative methods of supplying gas for pneunwtlc
system elements; consideration of the thermodynamic
relationships pertinent to their design; and a compari-
son of representative power supplies on the basis of
wei^t, size, and estimated cost for specific pressure
and mass flow requirements. Other factors considered
in the study are handling problems, reliability, safety,
and container shape. Packaged power supplies, such as
gas generators and compressed gas battles, are rec-
ommended for further study. (Author)
Federal Aviation Agency, Atlantic City, N. J,
A STUDY OF HEUCOFTER PILOT* S EYE MOVE-
MENTS DURING VISUAL FUOIT CONDITIONS, by
James A. Sunkes and Eugene E. Pazera. Final rept.
Nov 59, llOp. 5 refs.
Order from OTS $2.50 FB 171 094
Tests were conducted using three different types of
Army helicopters, the Bell H-13, the Vertol H-21, and
the Sikorsky H-34, to determine tboae areas of the
windshield which the pilot actually uses most often
during various maneuvers encountered in fli^. The
results were then used to further establish minimum
cockpit visibility requlremencs for belicc^ers.
(Author)
Flight Control Lab. , Wright Air Developntent Div. ,
Wright -Patterson AFB. Ohio.
PROBABILITY OF ATTAINING A GIVEN FLIGHT
PATH AS A FUNCTION OF THE TURN RADIUS,
TURN INITIATION ERROR, AND HEADING CHANGE,
by Eugene M. Romer. Aug 60, 13p. WADD Tecduilcal
note 60-200.
Order from OTS $a 50 PB 171 116
The problem of changing aircraft heading to coincide
with a particular graixad track is considered. A prob-
ability function is derived which gives the probability
of arriving within a corridor erf specified width to
eldier side of the ctesired flig^ path. This probability
function is assumed to be a function only of the error
in asceruining the correct point at whldi to initiate
die turn, the error in attaining a specified radius of
curvature and the change In heading. Two forms of
the probability function are obtained and an lllustzmtive
example for a particular case is worked out. (Author)
37
Flight Sifety Foundation, Inc. , Phecnlx. Ariz.
AVIATION CRASi INJURY RESEARCH, by Ruth M.
P««ry. Final rept. for 1 Oct 55-15 Sep 59 on Contraas
Noor-401(21) and Ndnr-2883(00). 11 Un 6a 15d
44rrfs; AD-23403a
Order from LC mi«.4a ph^. 30 PB 148 870
A brief summary of Lork to provide data which can be
used to Improve cranh survival design at aircraft
thereby Increasing tie survival rare in many aircraft
accldeats.
Hlller Aircraft CosV- . Palo Alto. Calif.
COMPARATIVE PERFORMANCE CHARTS FOR
Si^°.^°*^^^*^^- ^^- « Contraa DA 44-
i?^£;*^^- '^ ^' ^OOP- 3« refa. Rept. no.
ARD-257; AD- 241 376. >* •«.
Order from LC ml$5^ 40. ph$15. 30 PB 150 783
The purpoM d this rfcport la (1) to prepare general
conparatlve charts Usotar as poesible from available
experimental and theoretical informaUon, (2) to coo-
dua two-dimensionaJ water experiments to obtain
visual data o€ the dueled propeDer wake, and (3) to
Moduct a Um|»ed theoretical study of the duct and wake
shape in the katlc cotdltion. The study is divided into
three types d flow: sikitlc operation, noo-axlal flow
and axial flow. The d*ta are reduced to coefficient
fcjrm and combfn*d with appropriate correlation
parameters and^«ed. Several useful performance
charts are C0D8iAdb4 Ai the different flow regimes
The water test resuJta are shown photographically but
are net conclusive due to test limitations. The theo-
retical duct shape and wake results are presented
jpraphlcally. The wak« shape from the water test and
theory are essentially In agreement, but due to the
water test limitations cannot be considered a valid
check. (Aitthor)
Institute of Tranaportttlon and Traffic Bngineerimr
U. of California, Berkeley.
A MATHEMATICAL 14DDEL FOR LOCATING EXIT
TAXIWAYS, by R. Hor#ojeff, R. Q Qraasi and others.
R^t. or Contract FAA/BRD-4. Dec 59, 52p. 4 refs
Order from OTS $1. 50 r 171 (»8
The purpose of the present project was to formulate and
test a mathematical mo4el for determining the exit lo-
cations that win enable ^e runway to accept the great-
eat number of aircraft per hour within specified limits
of percent wave-offs. Tlie model can also be used to
compute, for an existing airport where runways are al-
re«ly fixed, the average acceptance rates and percent
wave-offs for various cctidltlons. A mathematical
model waa developed for a single runway used exclu-
sively for landing. The model makes it possible to de-
termine the taxiway locations that will yield the hlohest
runway acceptance rates, and corresponding wave-off
rates, caking into account: (1) number of exits, (2) exit
speed. (3) aircraft arrival rates at runway direshold.
(4) aircraft population (I.e. , a speciiled mixture of
l^cafaT'^' (5) pilot variability, and (6) mete^ro-
opcal and geographical conditions. The results show
^t the optimum locatioi^ *nd the corresponding a^r-
age acceptance rates are quite senslUve t^alrcraft
population, exit speed, and number of exits. Furtber-
nwre, If the number of exits and intervals of time be-
tween airqraft arriving oyer threshold are fixed dJT
38
optimum io<uaons of the exits vary considerably tor
each aircraft popuUtloa (See alao PB 151 16?).
Minnesota U. , Minneapolis. * '
^ffLUENCE OF NATURAL FREQUENCIES AND
SOURCE CORRELATION FIELDS ON RANDOM RB-
aONSE OF PANELS, by R. F. U^be^C^ ^
D. H. Tack. Rept for Sep 58-Oct 59 on Meulllc Mate-
W^I^^'k'^ ^^ 33(616)6828. JUly 60. 74p. 7 refs.
WADD Technical rept. 60-188
Order from OTS $2. 00 FB 171 090
"Hieoretlcal and experimental analysis at random re-
sponse d panels with a view toward problems of de-
sign are presented. TTje Influence of source correU-
tion fields, damping, and boundary Impedance are In-
tegrated Into the analysis. Modal response Is viewed
from the complex frequency plane in the form of a pole
diagram. The concepts developed from this point of
view have dlrea application in design for spectfleu
m«in square response. The sutlstlcal independence of
modes and Its relationship to properties of the source
and panel are discussed and taterpreted for several
situations. (Author) ••^^r.i
li
i.t vi
MotoroU, Inc. , Riverside. Calif
^Si???^^'^' °^ ATMOSPHERIC TRANSMISSION
V!?^*^^*^^^^'^ PJ^OM A PULSED LIGHT SEP-
ARATED SYSTEM. byMelvlnH. Herman. Final r«»t
psrt 1. on Contract [AF] 19(604)2213. June 59. 112p
AD-I'lVeiT' "^ '*^^-3«28-3; AFCRC-TR-59-255;
Order from LC fni|6. 00. ph|18. 30 PB 152 350
Thla report released for sale to the public 1 Nov 60.
A pulsed light transmissometer has been tested by com-
?!i^i".'"**.'"^^'"""' **^ ^<>"« o* * telephotometer
and with visual range taken from an ak-craft. The re-
sultslndicate that the pulsed light transmissometer is
a uaeftil lnstrun»ent for determining the transmission
loss up a slant path, such as the glide path at an airport
This measurement can be made without affecting land-
ing aircraft. A logarlthnUc amplifier, diacussed in a
separate repon. was developed to simplify and decrease
the time of the data reducing technique. The theory pf
the separated pulsed light transmissometer hasbfii
ftirther developed and a nomogram drawn to faclllute
data reduction. TTie brocesaea of dau reduction have
be«i almplifled to the point at which automatic computa-
tion la feasible. System limitations, secondary scatter,
and ambient light level are discussed. A method for
simpler data reduction la diacusaed. (Audior)
National Aviation Facilities Experimental Center
Atlantic City. N. J.
EVALUATION OF A FLAME SURVEILLANCE -TYPE
reTECTOR. by Marvin F. Rammelaburg and Paul R
Dlefdorf. Apr 60. 28p.
Order from OTS %0. 75 pe m 028
A aurvelllance-type flame deteaor system of the
^7«ector design waa evaluated in laboratory bench -
tvpe testa and by exposing the units to more than 250
*mall-magnltude JP-4 test firea in a modified KC-135
nacelle which had a,comparaavely low internal airflow
li| I
Laboratory bench testing showed the detector's sensi-
tivity decreased as the ambient light increased. In the
ICC-135 powerplant tests, the system detected 93 per
cent of all the fires to which it was exposed. It func-
tloaed satisfactorily under several engine power con-
ditions and had a consistently short response time.
(Author)
National Aviation Facilities Experimenul Center.
Atlantic Qty. N. J.
PROGRAMMING IBM 650 RAMAC COMPUTER FOR
DATA PROCESSING IN AN AIR ROUTE TRAFFIC
CCWTROL CENTER, by Harold R. Johnson, Jr. Juel E.
Erlckson and others. Oct 59, 105p. 2 refs.
Order from OTS $2. 50 PB 171 040
This report describes the development and preparation
of a detailed ATC program for an IIW-650/RAMAC com
puter system. Many portions of this program are pre-
dicated on the ability of this system to process all of the
many types of flight plan Information, to produce flight
progress strips, and furnish other information needed
for the control of air traffic at the Indianapolis Air
Route Ti-affic Control Center. A description is given of
the types and quantities of flight plans which must be
processed. A general discussion of the program l<^c
used for processing airway and/or direct route flight
plans is included and Is illustrated by charts, flow-
diagrams, and pictures.'
Naval Ordnance Test Station. China Lake, Calif.
ON HARMONIC MOTION OF WIDE DELTA AIRFOILS
AT SUPERS(»I1C SPEEDS, by John W. Miles. 13 JuneSQ
47p. 8 refs. NAVORDrept. 1234; NOTS 294.
Order from LC nU$3.30. pfa$7.80 PB 152 352
This report released for sf le to the public 28 Oct 60.
The forces and moments acting on a generalized,
oscillating, delta wing, bounded by two supersonic
leading edges and a strslght tracing edge perpendicular
to the free stream, are formulated In such a way as to
reduce their calculation to an equivalent, two-dimen-
sional problem. Explicit results are given for the lift
and pitching moments on a delu wing due to plunging
and pitching, the damping moment In roll, and the lift,
pitching, and rolling moments due to control -surface
deflections. Numerical results are fiyeti in the form of
curves. (Author)
Fhyaica Lab. . Wright Air Development Dlv. ,
Wright- Patterson AFB, Ohio.
ANALYSIS OF RELATIVE PERFORMANCE OF ABLAT
ING MATERIALS COMPARED TO A HEAT SINK MA-
TERIAL, by R. E. Otto. Rept. for Aug 58-Sep 59 orf
Materials Analysis and Evaluation I'echniques. June 60.
13p. 2 refs. WADD Technical note 60-88.
Order from OTS $0. 50 PB 171 0$4
Dita are preaented comparing relative performance of
ablating materials with Heat sink materials in ternu of
inside surface temperature rise and on a weight per
unit area basis. Structural characteristics of available
nuterlals and analysis of re-entry deceleration loads
are indicated. (Author).
Chemical Engineering
Army Chemical Research and Development Labi. .
Army Oiemical Center, Md.
A PRELIMINARY THEORETICAL STUDY OF THE
CLOUD TRAVEL OF AEROSOL PARTICLES HAVING
DIAMETERS BETWEEN 20 AND 180 MICRONS, by
Donald O. Egner. Donald Cam|^ll and others. JUly 60,
88p. 7fefs. CRDLR-3002.
Order from LC mlK 80. ph$13. 80 PB 150 663
Several aerosol models have been reviewed for their
ability to predict Qie travel of an aerosol cloud. The
model of Baron. Gerhard, and Johnstone appears to be the
most promising since it allows treatment of cases where
settling velocities are aifpreclable. This model is eval-
uated for various conditions of wind speed, dissemina-
tion height, atmospheric stability, and terrain roughness.
Several relationships are derived that facilitate the eval-
uation and application of the model. Basic curves and
tables are established for use in describing cootamina-
tion-denslty fields and corresponding density-area re-
lationships. (Author)
Army Chemical Research and Development Labs. ,
Army Chemical Center, Md.
SHOPAIR (SHORT-PATH INFRARED^ TOXIC-AGENT
DETECTION AND CONCENTRATION- MEASURING DE-
VICE, by Hugh R. Carlon, Robert E. Hagman and
Harvey Tannenbaum. July 60. 20p. 2 refs. Technical
rept. CRDLR 3006. ^
Order from LC ml$2. 4a ph$3. 30 PB ISO lOl
A SHOPAIR (Short- Path Infrared) Instrument has been
constructed and evaluated in the detection and monitor-
ing of nerve- gas concentrations. Sensitivities of 2^/ liter
(20- in. path) or better are obuined, with alarm occur-
ing within a few seconds. The Instrument has one mov-
ing part. Applications are suggested. (Author)
Battelle Memorial Inst. , Columbus. Ohio.
A STUDY AND ENVELOPMENT OF THE HICKMAN
SEA-WATER STILL, by W. L. Buckel. W. D- Beck
andahers. Rept. on Contraa no. 14-01-001-104.
Sep 60. 152p. 9 refs. SaUne Water Research and
Development Progress rept. no. 43.
Order from OTS $3. 00 PB 171 030
The fundamental studies were especially necessary
because evaporation and condensation on a rotating
heat -transfer surface is a new art; It was particularly
desirable to determine (1) the conditions under which
rotating disks could be wetted with the thinnest possi-
ble films, and (2) the nuximum heat-transfer coeffi-
cients that could be obtained with rotating disks. As
a corollary of this study, the faaors governing the
economic potential of the distillation process have
been reasonably well defined.
Marine Lab. , U. of Miami [Coral Gables] Fla.
ANTIFOULING PROPERTIES OF PESTICIDAL MA-
TERIALS, by Sigmund Miller. Monthly progress rqjt.
for 1-30 June 59. on Contract NOa(s) 59-6182-c.
June 59, 8p. ML 59160.
Order from LC mijl. 80, phjl. 80 PB 150 769
39
Panels Impregnated <rlth the chemlc*!* are exposed In
the sea In racks which hold 18 test panels and one noo-
tojclc control panel (all of porous carbon). The group
<rf 19 panels are inspected three times, after Intervals
ct approximately ten days each, depending upon the In-
tensity (rf fouling at 9ie time of test. Fouling present
is recorded, and eacti group of panels is phocographed
at the time of the second inspection. The effectiveness
d the chemicals is listed in descending order at ef-
fectiveness. (See also PB 150 768).
Syracuse U Research Inst. , N. Y
Tfffi PROPERTIES OP GAS HYDRATES AND THEIR
USE W DEMINERAUZING SEA WATER, by Allen J
Barduhn, Howard E. Towlson. and Yee-Chlen Hu.
^pt. onCootraano. 14-01-001-177. Sep 60, 74p
39 refs. SaUne Water Research and Development
Progreas rept. no. 44.
Order from GTS %2. 00 PB I7i 031
TTils research was un«tertaken to study the properties
or hydrates systems fagr collecting dau from the
literature and our own experimental work on pres-
sures and temperatures at which various hydrates
formand by determining the other thermodynamic
properties of these systems such as heats of forma-
tion, composltioo. and effeas at dissolved salt. The
purpose was to get infcrmatlon neceasary for process
calculations snd design, so that a choice of hydraiing
agent and an accurate evaluation of the hydrate proc-
ess for demineralizatloo could be made. (Author)
Gvil Eiiioin««ring
I
V
Army Engineer Waterways Experiment Station.
Vlcksburg, Miss.
SOIL STABIUZATION: INVESTIGATIONS OP A
CHEMICALLY MODIFIED CEMENT AS A STABl-
LCINC MATERML, by G. R. Koian. Rept. for Peb-
Sep58 00 Solidifying or StablUzing Soils for Military
Operations. July 60, 6<^. Technical rept. no. 3-455
rept. 3; AD- 241 536.
Order from GTS $1.50i ^. PB 171 098
■V-
Ub«-atory and field tetts were made to (a) determine
olectlTeness d chemically modlfled cement as a su-
bUlilng material for a lean clay sdl. and (b) estabUah
nii<axy Of strength requirements proposed for a su-
blllZBd soil surface to be used for short-term military
operations. Initial laboratory tests revealed that 5*
Portland cement -1% sottion sulfste was as effective
aftw 24-hr curing as lOjJ portland cement (unmodi-
neaj. However, suppleanentary laboratory teats con-
ducted concurrently wlt» field tests indicated suUkte
2^2^?*!!'* essemlally ineffective for the t»ai
•f^**^ because the soil difteied in chemical
charaowisdcs from the soil used in the, initial testa.
A soil surface stabilized with 5% cement- It sodium
au^e. oastructed on a 4 CSR subgrade. developed
aufficlem strength wlthis one day to meet specified
traffic requirements, primarily due to stabilizing
aaion at the ceraeot. (Author)
Army Baglneer Waterways Experiment Station.
Vlckaburg. Miss.
VALIDATION OF SOIL- STRENGTH CRITERIA FOR
AIRCRAFT OPERATIONS ON UNPREPARED LANDING
STRIPS, by C. a ftims. Rept. on CrlterU for Design-
ing Runways &u<aced with Landing Mat and Membrane-
Type MaierUls. July 60, 43p. 3 refs. Technical rept.
BO. 3-554; AD-241 546.
Order from LC ml$3. 30, phf7. 80 PB 150 436
lb validate Corps at Engineers tentative soil -strength
criteria for aircraft operations on unsurfaced soils
afhlch are based on CBR values, WES participated In
aircraft operational tests on unprepared sandy soil sites
The C-123B, a single- wheel transport, and the C-130A
a multiple -wheel transport, with gross loads of 38, 000-
48,000 Iband 80.000-116.000 lb. andTnaln gear pres-
sures of 41-90 psl and from 55-60 psl, respectively,
were used. Soil-strength messurements were obtained
before and during the tests. Conclusions were that:
(a) both planes can operate successfully on sand surfaces
having 4- to 6-in. -deep ruts; (b) the average soil
strength of the 6- through 12-ln. depths can be used to
evaluate load-carrying capacity of sand subgrades;
(c) Increasing wheel loads at constant tire pressures
has little effect on rut depths, but increasing tire pres-
sure at constant or hicreasing wheel loads causes more
severe rutting; (d) minimum subgrade strei^;th require-
ments determined hi these tests agreed with those hidl-
cated by previously developed CBR design curves; snd
(e) the CE tentative strength criteria are as good as can
be established from available data. (Author)
Michigan U. [Research but. J Ann Arbor.
STRUCTURAL STEEL CONNECTIONS, by Leo
Schenker, Charles G. Salmon and Bruce G. Johnston
Rept. on Contract NOy- 74521. June 54, 227p. 112 refs.
2065- 1 -F ; AFSWP rept. no. 352.
Order from LC ml$9.90, pb$34.80 FB 152 355
This report released for sale to the public 28 Oct 60.
The report covers only one aspect of the problem of
structursl behsvlor, bulla an attempt to provide a
reasonably thorough and uaable evaluation and smmwry
Of available inforoatlon in the field of structural con-
nections. The properties of the aaual connectors
(rivets, bolts, welds, etc.) are discussed in Chspter I
Chspter II deals with tension connections. In Chapters
lUaad IV the characteristics of rigid and nourlgld con-
necdons as used in continuous frames and der buildings
are studied snd their efftea on the snalysis and design
procedures for building frames is investigated. The
influence of column anchorages on the resistance of
buildings to lateral loads la discussed in Chapter V.
Very little experimental Information on this problem Is
svallable so that the discussion here is primarily on a
theoretical basis. Chapter VI presents some examples
lUuArstlng the procedures that would make use of the
Information In the previous chapters.
#
Ei«etrical and Electronic EnginMring
Airborne Instruments Lab. , Mlneola, R Y.
DEVELOIMENT OP A MICROWAVE PRESELECTOR,
by R. Sleven. Pinal rept. on Contract DA 36-099-ac-
73160. Jtoe 58, 57p. 12 refs. Rept bo. 4600-1; |
AD- 208 579.
Order from LC ml$3. 60. ph$9. 30 PB 150 681
TNw microwave preselectors have been designed and
fibrlcated for operation over the 7125 to 8500 Mc band,
bch unit consists of a gang-tuned four-element filter,
« STRIPLINB balanced mixer, and an 1-f preamplifier*
Xmi 1-f amplifiers were provided to permit evaluation
rf the systems. The overall performance of the system
U best evaliMted by measuring the noise figures at
tsveral frequencies In the 7125 to 8500 Mc band. The
vise figures for system 1 varied from less dian 14 db
at the band edges to a minimum of 9. f db. The noise
fifuies for system 2 varied from less than 12 db at the
bsnd edges to a minimum oT 9. 6 db. The si^jerlor per-
fbrrrance d system 2 was atulned because of the ex-
pvlence gained In the development and fabrication of •"
nttam 1. (Audxn-)
Airborne Iiwtnnients Lab. , Melville, N. Y.
BVALUATICW OT AIR TRAFFIC CONTROL RADAR-
BEACON SYSTEMS (ATCRBS), by M. NatcWpolsky,
J. S. Perry and others. Final engineering rept. Phase 2,
Oa 58-July 59, on Contracts FAA/BRD 119 and 84;
formerhy CI 3 ca 606 and 68^. Oct 59, 28Sp. 2 refs.
Rept. no. 7356-1, Vols. 1 aad 2.
(Jrder from OTS $4.00 'I PB 171 095
To evaluate ths operational and tedudcal diaractar-
latlcs of the ATCRBS. an in-aervlce teat program was
conducted In the New York terminal area. The pro-
gram tested and evaluated the ATCRBS Installations at
the New York Air Route Trsfflc Control Center,
Idlewlld Tower, LaGuardla Tower, and Newark Tower.
During these tests, ATCRBS performance proved su-
perior to that of the primary radar. Several ATCRBS
operational procedures were tested and evaluated to
determine their cootribution ot the immediate Im-
provement and future automation of air traffic control.
Military- dvll high-density ground and air envlron-
nents were usedto determine system behavior for the
planned ATCRBS Installation in the New York terminal
area. The pulse Interference geoersted by the system
waa reduced by the fix-equipments (remedial equip-
ment) tested. Single defrulting effecUvely cleaned the
displays of fruit under all test conditions. A side-
lobe- suppression system was tested; It proved effec-
tive In preventing side- lobe interrogations and thus in
reducing transponder reply duty cycle. ATCRBS op-
erstlons procedures were tested snd found to Improve
the effeaiveaeaa of the present ATC system. The
immediate implementation of the ATCRBS and the
simultaneous development of a test program to achieve
maximum operational usefulness of the system ta
recommendml. (Author)
American Inst, for Researcrh, Pittsburgh. Pa.
SIMULTANEOUS VS. SUCCESSIVE PRESENTATION
OF RELATIVE MOTION PROBLEMS, by M. Paul
Willis and Frank Siroky. Rept. on Contract N61339-
348. 26 Aug 60, 77p. 11 refs. Technical rept.
NAVTRADEVCEN 348-2.
Order from LCmiJ4. 50, pl*12. 30 PB 150 160
Thla acudly tested tbm hypotfaeala that the darekpinem
dt understaadliv of relative motion concepts will be
facilitated by slmukaneous preseotatioo of three rele-
vant reference systems. Twenty-one high school
gratbjates attending an electronic technical Institjjte
were randomly assljaed to three experlmenul condi-
tions baaed on tbe simultaneity variable, namely, suc-
ceaalve, lotermediate simultaneity and maximum
simultaneity of preseoutlon of reference systems.
The spparatua consisted of two movable, transpsrent
polar coordinatea and one fixed rectangular grid,
which permitted subjects to superimpose sU three
■olutiona. Printed Instructions and self -teaching pro-
cedures were used exclusively. An analysis of vari-
ance statistical technique was Used on the data. The
findings showed tbat'slmultaneous methods of refer-
ence system presentation are not superior to succes-
sive presentation over all problem types and all refer-
ence systems. However, the slmultsneous methods
are superior on certain specific combinations of 1
factora, particularly for doaeat point of approach
and Intercept problema. (Author)
' Antenna Lab. . Ohio State U. Research Poundatloii.
Columbus.
ECHO AREA OP COMBINATIONS OP CONES, SPHE-
ROIDS, AND HEMISPHERES AS A FUNCTION OF
BISTATIC AN<H^ AND TAR^T ASPECT, by
J. W. Eberle and R. W. St. Clair. Rept. on Contract
AP 19(604)6157. 30 June 60, 39p. 1 rsf . Repc 1073-1;
ERD-TN-60-795.
Order from LC mi$3.00, ph$6. 30. PB 150 740
Tbe scanerlng croas section of various combinations of
cones, qiherolds, and hemispheres is presented as s
function of bistatic angle and target aspect. All mees-
urenients were taken at a frequency of 9375 mc (3. 2 cm
wavelei^{th). A desertion of the eq^pment used for
the meaaurenoents la given along with the method used
to calibrate the pattema. A technique is described
which permits the phase of a scanered signal to be de-
termined with respect to a fixed reference slgnaL A
typical anq>lltude and phaae pattern for a blhemlsphere
comblnatlop ia abown. (Audior).
Armour Research Foundation, Chicago, DL
HKH POWER TRANSDUCERS, BY H. B. Karplus and
R. R. Whymark. Quarterly rept. na 2 on Contract
[Nonr] 2900(00). 22 Dec 59, 4^. ARP 1149-2.
Order from LC ml|l. 80, ph$l. 80 FB 152 140
SeealaoFB 149 877.
Army Signal Research and Development Lab. ,
Fort Monmouth, N. J.
THE DESIGN AND FABRICATION OF HP AND VHP
LOW PASS FILTERS FOR A HIGH POWER TRANS-
MITTER, by Wslter Grudus and Alan Budner. 1 July 60,
58p. 2 refs. USASRDL Technical repc 2132; AD-240615.
Order from LC ml$3. 60, ph$9. 30 PB 152 191
The report presents die development of s series of 11
low-paas filters cqwble of handling at leaat 500 watts,
where the cut-off frequency varied from 8. 33 mc to
267 mc. Maximum insertions loss was 0. 5 db up to 0. 85
fc and the minimum attenuation waa 50 4b above L 25 f^.
41
The Impectonce lereliwas 50 ohms with a VSWR <rf 1. 5
to 1 up to 0. 9 f • THe conatructlon of thes* filters is
completely explained wtth all dau reqxilred for fabrica-
tion furnished. CliarBcterlstlcs erf the first set appear
In the Appendix. (AuUiorV
Army Slgna] Research and Development Lab.
Fort Monmouth, NJ J.
MULTIPLE BEAM ANTENNA SYSTEM, by William
Fishbeln. 15 Apr 60j I6p. USASRDL Technical rent
2112; AD- 238 426. '
Order from LC ml$2i 40. ph$3. 30 PB 152 188
An antenna aperture tiust be many wavelengths lot^ to
obtain high angular r^solulloo. In conventional anten-
nas, radiators are spaced about one-half wavelength
apart of avoid mulilpte lobes. USASRDL engineers
oooatructed an antenna consisting at 10 radiators
■pMed 30 wave length! apart. Two techniques Inyead -
gated circumvent the tnultlple lobe problem caused by
the large radUtor spacing. These Mchnlques are
based on the use of separate anKfOMS for transmitting
and receiving. The first technique involves the uae of
a receiving ancenna wfth a single beam narrow enough
to select only one at tke multiple lobes at the trans-
mitting antenna. The second technique uses 2 multiple
beam antennas with sUghtly different lobe spacings for
both transmission and reception. The first technique
was successfully evalwted wlthaRadar Set AN/MPQ-4
A multiple beam anieitui has the advantage o< requiring
relatively few radi«ta«a. Thus the antenna is light-
weight, easy to constrUa, and not difficult to scan
(Author)
Army Signal Researti) and Development Lab. , Fort
Monmouth, N. J.
THE SUPER REGENERATIVE PARAMETRIC AMPU-
FIER. by Bernard B. Bossard, William Fishbeln and
Emerson Fro«. 15 July 60, 24p. I ref . USASRDL
Technical rept. 2136.
Order from LC mi$2.^, ph$4.80 PB 152 194
Recent experiment* conducted at USASRDL have shown
the feasibility d combihing the low noise capability of
the parametric amplifier with the hi^ gain obtainable
from use of superregenerative techniques. Superre-
iBoerative parametric amplifiers were bulk to operate
« 1450 megacycles (L-pand) and 8500 megacycles
(X-Band). The L-Band ^plifier exhibited a gdn o* 70
decibels, a 3-megacycle bandwidth, and a minimum
detectable signal of -104 dbm. The X-band amplifier
exhibited a 52- decibel gain aid a 3- megacycle band-
width when utlUzing a v>ractor with a cutcrff frequency
ai 41 kllomegacycles. the superregenerative para-
metric amplifier has simplicity, high gain, a lownoiae
figure, and insensiti^ity to certain types at inter-
ference. The size and weight are small and power
consumption is low. M4ny elements oT the technique
may be utilized in low-«o« communication systenu
(Author)
Army Signal Research and Development Lab. ,
Fort Monmouth, N. J.
TEST SET. RADIOSONDE TA-1348 (XE-l)/GMM-f A
^ ^-T-- 9*^bone and A^ J. Mootedoro. 15 July 60. 26p.
This report covers the development., design, and evalua-
tion of Teat Set. Radiosonde TS- 1348(XE- 1) /GMM- lA
which aatiafactorily detects deficiencies in Battery Pack
BA-259/AM and Radiosonde AN/AMT-4 or AN/AMT-12
( ) during preflight testing. (Author).
USASRDL Technical rep(
Order from LC ml$2. 40
;
2134; AI>241 178.
ph$3. 30 PB 152 192
Balllatic Research Labs. . Aberdeen Proving Ground.
THE SHROUD ANTENNA, by Victor W. Richard.
June 60. 22p. 6 refs. Mema rq)t. na 1283.
Order from LC mlJ2. 70. phK 80 PB 150 958
The Shroud antenna waa designed for VHP telemetering
and Oappler tracking Instrumenutlon use on high ve-
locity rockets which require a small, light-weight an-
tenna with an omnidirectional radiation amplitude, con-
stant phase, pattern. A unique method of Insullatlon
of the Shroud antenna system is used which does not re
quire rocket body modification, mounting holes or
bolts. The antenna elements are held fast to the rocket
body with metal straps. facUltathig convenient, secure
mounting. The Shroud antenna has withstood success-
fully the high acceleration and temperature environ-
ment o€ the Nike-Cajun rocket which has a peak accel-
eration of 80 g's and attains a speed of Mach 6 as low
as 50, 000 feet. The flat plate area of the antenna is
small, presenting low drag. High tenqjcrature resis-
tant materials are used to withstand the extreme heat
generated by air friction. Properties of the Shroud
antenna discussed include: the basic theory of opera-
tion, radiation amplitude and phase patterns, gain,
efficiency, voltage breakdown, radiation efficiency,
Impedance matching, construction. Installation, ad-
justment and flight performance. (Author)
Bartol Research Foundation. Franklin Inst .
Swarthmore. Pa.
RESEARCH INVESTIGATION OF CATHODE EMISSIVE
MATERIALS, by W. E. Danforth. Scientific rept. no 9
on Contract AF 19(604)3904. 15 July 60. 25p. 5 refs
AFCRL-TN-60-798. J J > P ers.
Order from LC ml$2. 70, phf4. 80 PB 152 040
Existing data reUtlve to the evaporation rate al a tho-
rium monolayer as a function of coverage and tempera-
ture, taken at Barto' and from other sources, is com-
pared with a theory of Reiss suggested by Moore and
Allison. Aldiough the spread of the data la greater than
desired, the theory deacrlbes satisfactorily the form of
the curves when reasonable values are used for binding
energy and repulsive energy between nearest neighbors
We have measured previously the thorium coverage on
poljcrystal tungsten corresponding to maximum emis-
sion. Studies are now being made with a tube In which
thorium is depoelted In equal amounts on polycrystal
and single crystal tungaten. Activation of the single
crystal ribbon is qualitatively very similar to that with
polycrystal specimen. Quantitative difference* exiat
but have not yet been defined. X-ray determination of
the orientation of the single crystal specimen Is In pro-
gress. Oie tube has been processed in which a ZrC
specimen la heated by electron bombardment for ther-
mionic measurements. Richardson constants In rough
agreement with those by R. W. Pldd et al., are obtained.
Life tests at thorium impregnated matrix cathodes have
run to 12, 000 hours at 2. 3 umps/cm^. A life of n-eater
than 4500 hours have been obuined at 3 ampa/cn?'.
Studies are in progreas relative to the role played by
carbon in Inhibiting evaporation at thorium, (Audior)
(See also PB 148 517).
42
Bell Telephone Labs. ,^ Inc. , New York.
CRYSTAL RECTIFIERS. Interim tedmical repc.
00. 8, 1 Apr-30 June 56, on Bn^neerlng Services on
Transistors, Cootraa DA 36-099 -•c-5589. 15 July 56.
36p-
Order frcm LC ml$2. 70. ph|4. 80 FB 152 657
tUs report released for sale to the public 16 Nov 60.
Improved performance In microwave transmitting
oodulatora has been demonstrated with gold-hooded
diodes. This result is attributed to minority carrier
■torage. Theory Indicates that diodes which maximize
iMs effect can also lead to Improved harmonic genera-
tors and more reliable microwave receivera. Fabri-
cation of such devices by solid-state diffusion Is being
tttempted. (Author)
Bright Sur Industries, Clifton, N. J.
rOcr CELL MAGNESIUM DRY CELL BATTERIES
bf P. A. Keller. Semi-annual progress rept. no. 2,
I Apr 59-1 Apr 60, on Contraa DA 36-039-BC-78231.
tl«0ll3p. AD- 240 503.
Order from LCmi$2. 40. p(43. 90 FB 150 804
22 1/2 vok stacks submitted for tests failed due to
serious trouble with the dupJex electrode. (Autbor)
(See also PB 145 803) I
Cite Inst, at Tech. . Qeveland, Ohio.
STUDY OF CONTRCX- OF APERTURE PIELD6L
Srieattflc rept. no. 15, 30 Nov-59-30 May 60, oo Ooo-
trsct AF 19(604)3887. 1960. 39p. 29 reft. ERD 1N-
60-777.
Order ftom LC ml$3. 00, ph$6. 30 FB ISO 648
Progrett It reported on work Is the following areas:
Anltocroplc Propertlet at Artificial DIelectrlct.
(a) Dltc Medium, (b) Hi(^r Order Approothnatlont for
the Pblarlzabllltlet ofthta Circular DIsct, (c) Two
Dtanentional Strip Medium, Probe-Obstacle fateracticn
in a I^rallel- Plane Medium, Solid Angle Reflector Sjm-
tbetli. Meaiurement at Surface Currentt, Netwocfc
Sfiuhetli. (See alto PB 146 918)
Centre de Phjrsique Blectroi|lq|ue et Corpusculalr*
(Prance).
WIDE DYNAMIC RANCK BARRIER GRID STORAGE
TOtt T. C. M. 16, by G. Wendt. Quarterly rept.
■0. 2 on Contraa N62558-2275. 1 Dec 59, 26p. :
WR. 473. AD- 230 552. J
Order from LC mi$2. 70. pK4. 10 FB 152 092
Arevlously the reproducibility of the 06 SMD electron
guns seemed to be good, including good linearity be-
tween the beam current and the collector -aperture
current. It appears now. after having assembled a
larfcr number at TCM 16 tubes, that the percentafe d
fUBs with a linear characteristic is rather low. The
possible causes for these failures are discussed. The
Faraday cage which waa set up bad to be replaced by
t larger one. The good resolution obtained on TCM 14
tubes ot the j type led to a periodic irregularity on die
output signal due to the grid structure. It was possible
to manufacture grids of twice smaller pitch: 40 wires
fu millimeter, and to stretch them on the frame and
insulator. Sudi a targst assembly is being introduced
in a TCM 14 tube. In the gun using deflection as a
means for modulation, the two pairs at plates used for
beam current modulatiao and beam recentering had
different sensitivity. The modulation voltage had to
be divided before being applied to one of them. This
inconvenience was corrected. (Author) (See also
PB 148 868) .
Cornell U. School of Electrical Engineering,
Ithaca, N. Y.
INVESTIGATION OF NOISE CXNBRATION IN ELEC-
TRICALLY TUNABLE MICROWAVE OSCILLATORS
Quarterly progress repc no. 3, 23 Dec-23 Mar 60, oa.
Contract DA- 36-039- sc- 84524. [1960] 57p. 7 refs. Re-
search rept. EE 466; AD- 240 097.
Orxler from LC mi$3. 60. ph|9. 90 PB 150 817
Local oscillator noise of 6 backward-wave oscillators,
type VA- 161 Varian was measured over a range of 8. 2
to 10. 0 kmc. The order of magnitude of the measured
S/N per inc bandwidth 30 mc away from the curler waa
0. 1 X 10"'to 2. 0 X 10^^. From the normal noode anal-
ysis of periodic transmiaalon systems with nonuniform
current excitation, an equivalent circuit suitable for
use in BWO (backward- wave oscillator) analysis waa de-
rived. This equivalent circuit utilizes the special sym-
metry properties of helices. Certain of the important
parameters of the tape helices are presented. A de-
scription of the amplitudea. phaae^ and frequency re-
lationshlpa is made for a reflex klystron oscillator m
the locked rqion of oscillation as determined by a-sy»-
chronizliv slgnaL The general nature of the results
apply to all seU-exclted oscillators, and these resultt
are not limited to small synchronizing signals. The
technique uaed may be applied to any oaclllator whoae
nonlinear characteristic is known, either from snaly-
sis or from experiment. It is interesting to observe
that a finite region at locking always exists for a finite
synchronizing slgnaL (Author).
Cruft Lsb. , Harvard U. , Cambridge. Mass.
RADIATION PATTERNS OF ANTENNA ARRAYS CON-
SISTING OF DDPOLES COUPLED TO A TWO-WlRB
LINE, by Kun-Mu Chen. Scientific repc no. 8,sc<Ues2,
on Contract AF 19(604)4118. 20 May 60, 22p. 4 refa.
ERD-TN-60-764 «..^„.
Order from LC nil|2. 70. ph$4 80 F» 190 552
The radiation pattern of a pair of tilted dlpoles coupled
electromagnetlcally to a two- wire transmission line Is
found. Six antenna arrays consisting of dlpoles coiq>led
to two-wire lines for different purposes are suggested
snd the radiation pattern for each array is obtained.
(Autbor).
Ikvid Su-ooff Research Oatmr, Prtncetoii. R J.
ELECTRON EMISSION STUHES, by G. A. Morton.
A. R Sommer and others. (Quarterly rept. no. 5,
1 Oct-31 Dec 59, on Contraa DA 36-039- tc-78155.
ri959l 35p. 6 refi. AD-234 230.
Order from LCml$3. 00, ph|6. 30 PB 150 815
Profxvst ti iwpoited for work accomplished on the
fnUowti^ (1) piMJtoemistton Induced by an httemal
49
field In Cs-treate(l silicon and germanium, (2) scan-
ning of surface to ^tudy origin of phot oemiss Jon induced
by an internal fiel*. (3) theoretical considerations con-
cerning photoemispion induced by internal field,
(4) surface studie^oT cleaved silicon crystals. (5) hot
electron emission from Cs-treated germanium, (6) in-
vestigations of hottelectron emission in image tubes,
(7) luminescence associated with hot electron emission
(8) chemistryofth4 silicon-cesium system, and(9)evap-
oratlon d MgO by electron bombardment. (Author)
(See also PB ISO 8 4)
David Sarnoff Research Center, Princeton. N J
HIGH TEMPERATtJRE SEMICONDUCTOR RESEARCH,
by J. Blanc, R. Bui^ and others. Scientific rept. no. 2
1 Feb- 31 May 60, ton Contract AF 19(604)6152.
30>ine60. 67p. 2dref8. ERD TN-60-759.
Order from LC mlis. 90. ph$10. 80 PB 150 963
Contents: j
GaP and GaAs-GaPlalloys
Pf «P»ratlon at purq material
Impurity behavior j
Evaluation o( Material properties
Device studies
(See also PB 147 29>)
David Sarnoff Research Center, Princeton N J
RESEARCH IN ELHCTRON EMISSION FRCM SEMI-
CONDUCTORS. byA. R Sommer. W. E. Splcer and
others. C^jarterly i ept. no. 6. I ;an-3I Mar 60. on
Contract DA 36-039 -8C-78155. [1960] 23p. 5 refs.
AD- 238 923.
Order from LC mi J J. 70. phH 80 PB 150 816
The luminescence a|:companying hot electron emission
due to avalanche breakdown was measured and the
voltage dependence W the emission was compared with
that d the field induced photoemission to establish the
voltage at which avajanche breakdown begins in Si and
Ge. Experiments with different doping concentrations
in the n- and p- typ^ regions were carried out to deter-
mine the nature and (place of the breakdown. Hot elec-
tron emission and rectification were studied on crystals
which were outgassad at lower temperatures than pre-
vious samples before being exposed to cesium. With
the help of an image; tube a preliminary experiment
was made to establish whether a larger emitting area
can be obtained by suitable geometrical configuration.
The nature of the re4ctlons at Cs with Ge and Si was
further investigated, in particular to find out whether,
at the temperature u^ed for hot electron emission
activation. Cs forms' a compound with Ge and St
(Author) (Se. "'so PB 150 815)
Divid Sarnoff Research Ce«er. Princeton. N I
THERMIONIC EMISaON STUDIES, by G. A. Morton.
A. H. Soriimer and others. Quarterly rept. no. 2.
1 Jan -31 Mar 59. on Contract DA 36-039-»c-78155
[1959] 23p. 2 refs. j
Order from LC mi$2i70, pliK 80 PB 150 813
The tungsten bronzes of Na. Rb and Cs have been syn-
thesized and their thqrmiooic emission has been
studied. First result* are not promising. The secon-
dary emission of Cs-timgsten bronze has been measured;
its low value is In agreement with the low thermionic
emission. Work has been started on an investigation d
rare earth oxides. Progress has been made in develop-
ing an optimum surface treatment of Si with Cs. "nie
pulse equipment for measuring HEE has been com-
pleted and successfully used. Efficiencies larger than
those previously reported in the literature and pulsed
currents greater than 1 ma have been obtained from
junctions. Indications have been found that photocath-
odes cf the Ag-O-Cs type are "hot elearon" emitters
under suitable conditions. An ultra-high vacuum sys-
tem is nearing completion in which surfaces of vac-
uum -cleaved a crystals are to be investigated. A
modified image orthlcon tube has been designed to
study contact potential differences on Si p-n Junctions
(Author) (See also PB 145 236)
David Sarnoff Research Center. Princeton, N I
THERMIONIC EMISSION STUDIES, by G. A. Morton.
A. H. Sommer and others. Quarterly rept. no. 4,
1 >ily-30 Sep 59, on Contract DA 36-039- sc-78155.
[1959] 30p. 3 refs. AD- 231 405.
Order from LC mi$2. 70. phH 80 PB 150 814
The thermionic emission from the rare earth oxides
Y2O0, l^2^3 ""^^ *^2^ *^' measured and the corre-
sponding ^ and A values have been derived. Work on
these materials will be discontinued, at least for the
time being. Contact potential differences between vac-
uum-cleaved silicon crystals and a tungsten ribbon was
measured. Work function values were obtained for
three crystals containing different amounts of impuri-
ties. By cleaving each type of crystal at least twice,
it could be shown that die method leads to reproducible
values for each sample. A grown n-p-n Si junction was
used as a target In a low velocity beam scanning tube.
For the first time, the p-n Junctions were observed on
the display tube without using a blasii^ potential across
the crystal. Current -voltage characteristics were
measured in a new Cs activated tube. Measurements
on this and earlier tubes were correlated and a pro-
visional interpretation of the results obtained to date
is suggested. (Author) (See also PB 147 272)
Diamond Ordnance Fuze Labs. , Washington, D. C.
ADAPTIVE SERVO TRACKING, by A. I. Talldn.
20 Sep 60, 22p. 6 refs. TR-860.
Order from LC ml$2.70. ph$4.80 PB 152 311
This report describes a self-adapted sampled-data
tracking loop. The tracking loop may be considered to
be a low-pass filter with a variable bandwidth. The
loop is designed to adapt rapidly to changes in the Input
signal by monitoring both the apparent error and the
loop output. Results show a tracking accuracy of 25 to
34 percent higher than that of a comparable linear sys-
tem at a receiver S/N ratio (rf 10 db. In other terms,
to attain the fame accuracy the comparable linear sys-
tem requires an S/N ratio of 13 db. This improvement
In performance is obtained with relatively little addi-
tional circuitry. In general, the degree of improve-
ment obtained by adaptive tracking will depend on the
compromises made in the design of the unadapted loop
to track the most difficult type of target. ^Author)
44
Diamond Ordnance Fu^ Labs. , Washington, D. C
DOFL HIGH-G TELEMETRY SYSTEM, by Gilbert M.
Koaenberg. John C. Tomasello, and Walter L.
Gieseler. Interim rept. no. 1, 27 May 60. 28p. |
9 refs. TR-841.
Order from LC ml$2. 70, phj4. 80 PB 150 318
Preliminary design and evaluation dau are presented
OB a 200, 000-g telemetering system, capable of meas-
uring temperature and other parameters from missiles
during high-speed flight. Design considerations, com-
ponents shock-test results at hi^^ g, illustrative re-
sults of missile-firing tests, and an outline for future
dsslgD investigations are included. This system in-
corporates an rf oscillator operating at a frequency of
approximately 65 Mc and freqiiency modulated by a
fixed- frequency subcarrler osclllatar. Missile firing
of the present system has beerl made from powder
guns. With the final design, the high speeds snd set-
back will be produced by firing from ligbt gas guns.
(Author)
Diamond Ordnance Fuze Labs. , Washington, D. C.
UGHTWEIGHT HIGH-DRAIN ZINC-SILVER OXIDE
BATTERY, by Gilbert R. Snyder. 22 Aug 60, 25p.
5re«a. TR-859.
Order from LC nil|2. 70, pl44. 80 PB 152 314
The PS-503 reserve-type power supply has been de-
signed for use in a coriipact electronic device. The
electrically initialed, zinc- silver oxide power supply
will function over the temperanire range erf -40 to
^160^ with a current density of approximately 0. 5
amp/in. 2 of projected elearode area. This minia-
' turlzed power supply was made possible by earlier
work described in DOFL Repcart TR-560. The battery
consists of two voluge sections: a 1 . 4-v section and
a 6.7-v section. It is activated by a pressure -vacuum
system without auxiliary beat hr heating devices.
(Author)
Diamond Ordnance Fuze Labs. , Washington, D. C.
MAGNETRON GUNS. AN EXACT THEORETICAL
TREATMENT, by William E. Waters. 27 Apr 60, 77p
10 refs. TR-843.
Order from LCmi$4. 50, ph$l2. 30 PB 152 309
The properties of an electron optical system in which
a space -charge -limited current is emitted from a
conical cathode, immersed in a uniform axial magnetic
field, are discussed. All oecessary equations perti-
nent to a static space -charge flow are combined into a
system of four ordinary, nonsingular differential
equations; these have been solved simultaneously on a
hi^- speed dlgiul computer, and pertinent computer
calculations are presented In graphical form. An exact
solution is given for the properties of an annular ro-
tating electron beam, in which each electron moves In
a helical path of constant pitch, the magnetic field is
uniform and axial, and all electrons possess the sante
angular velocity about the axis. A numerical example
is presented for a particular gun design, together with
a few briefstatements concerkiing the actual per for m-
aace of the experimental gun that was built from this
design. The characteristics of the theoretical flow
patterns are interpreted, and mathenutical relstions
are presented. (Author)
Diamond Ordnance Fuze Labs. , Washington, D. C.
A STUDY OF ELECmiCAL PROPULSION OF ORD-
NANCE LAND VEHICLES, by H. Di Gather. 30 Sep 60.
33p. 22 refs. Technical rept. TR-777.
Order from OTS $1. 00 PB 171 026
A study cf future Ordnance vriilcle diaracterlstlci,
their power requirements, and of known sources of
electrical energy leads to the conclusion tfiat an elec-
trical propulsion system can provide marked, new
capabilities in mobility and that the fuel cell system
offers the best possibility of providing the required
power plant. A fuel cell/electric motor system can
provide many of the desired characteristics of a pro-
pulsion system, such as (1) utilization of a variety of
fuels at a new level of efficiency (2) freedom In vehicle
design (3) low field maintenance, and (4) lessened field
detectabillty. Major technical advances are required
both In terms of fuel cells and motors before a practi-
cal objective can be met. (Author)
Dielectrics Lab., Johns Hopkins U., Baltimore, Md.
DIELBCrRICS FOR OUTER SPACE, by Louis J.
Frisco. Interim rept. no. 1. 1 Mar 59-30 Apr 60, on
Cootraa DA 36-039- sc-78321. 31 May 60, 66p.
16 refs. AD- 240 028.
Order from LC mi$3.90, ph$10.80 PB 150 806
The results of the first phase of s study of the effeas
of simulated hig^ altitude* environment on the electrical
properties of electrical insulating materials are re-
ported. Tests have been made for periods up to 96-
bours In high vacuum, in the presence of ultraviolet
and 50-kv x-ray radiation. Measurements of flashover
strength from 60-cps to 18-mc, dieftctrlc consuntand
diesipatlon factor from 60-cp8 to 100-mc, and d-c
surface and volume resistivity have been made on
Alathon 4 BK 30, Aloot (aluminum oxide), glass poly-
ester laminate, and Formica FF-95 printed wiring
board. Observed changes in elearical properties sre
associated mainly with thermal effects, except in the
case of flashover. Electrode effeas prove to be
important in high vacuum flashover phenomena,
causing minimum values in high vscuum to be com-
parable to the low values obtained at atmospheric
m-essure. (Author)
Digital Computer Lab. . Mass. Inst, of Tech. ,
Cambridge. ^
*RELAY AND CONTACT LIFE TEST, by Robert
E. Hunt. 3 Mar 52. 8p. Engineering note E-452;
AD- 71 333.
Order from LC mljl. 80. ph$l. 80.. PB 150 754
This repon released for sale to the public 25 Oct 60.
A relay life test rack was set up and operated for 18
million cycles. Clare type J and Allied type BO relays
were used. Relay performance was excellent, but the
results of the test show that the most Important single
factor in applying relays is arc- suppression. The
second and most important factor is cleanliness.
Electric Storage Battery Co. , West Orange, N: J.
HIGH CAPACITY VENTED NICKEL- CADMIUM CELLS,
by Arthur Fleischer, Edward C. Kopper and others.
(Quarterly rept. na 2, 1 Mar- 31 May 60, on Contract
DA 36-039- sc-84555. [1960] 83p. 7 refs.
Order from LC mlU- 80, ph$l3. 80 PB 152 187
45
Six addltlooaL 23-pl«te Type SC4 ceU« were assembled
•fter sintering and Impregnating master plaques. The
capacity testing propam en the 39 Type SC4 cells as-
sembled with 23-. If- , 15- and U-pIate elements havln|
positive plates Impregnated In nickel nitrate soludoo
containing 0, 5, and 10%. cobalt and Edison process posl
tire plates was completed with the determination of cs-
pacltles at the 5- hour discharge rate at room cenq>ers-
ture and -40^ and at the 15- minute rate at room tem-
perature. The results at the capacity test were analyzec
and a nuroerlcsl ana^sls appUed to evaluate the effects
at the variables. It was found that there was an alter-
nadon in die relative capacities considered in relation
to the number ai plaoes. All cells having 15-plate and
ll-pl«ie elements failed to meet die capacity require-
ment for the Type SG4 cell at the 5- hour rate at -400.
All cells met the capacity requirement for die Type SC4
cell on discharge at ihe 15- minute (3C) rate at room
temperature. There was an indication that the fV>lypor
separator tended to shed the mlcroporous coatli^ The
analysis c* the test results led to the selection at the
plate dilcJmesses of the 19-plKe Type SC4 cell as the
opdmum combination for the production cells at the six
types. The Edison psocess positive platee were tested
in the 15-plate SC4 cells which did noc meet die low tem
pcrature requirement (See also FB 149 118).
ering
Electrical Engineering Research Lab. , U. of
Illinois. Urbans.
BEARING AVERAGING USING TWO OR MORE SPIN-
NING GONIOMETER RDF SYSTEMS, by Fred John
Wymer. Thesis. Technlcsl repc na 15 on Contracts
Nonr- 1834(02) and DA 36-039- sc- 74898. 24 Dec 59.
98p. 13 refs. AD- 231 860.
Order from LC ml|5. 40. phJlS. 30 PB 152 131
By using two or more Adcock Antenna arrays, and av-
eraging the todlcadons from each one. an "Instantane-
ous'* average bearing can be obtained. The equiptnent
used In dUs Investigation was designed to perform the
algebraic manipulatioas determining die bearing indica-
tion, and was used to show die validity of the ansJysia.
It was tested In die lahoratory using rwo channels to
represent two RDF systems. The problem, then, was
to develop equipment which would average die bearing
indications from two Adcock antenna arrays. The pur-
pose was to show that this system could be used to re-
*>ce^arroTa in bearing indicatione.due to Interler-
liig components at the carrier frequency. The develop-
ment d an optimum dlscrlbutioo of arrays was slso de-
sired, and for this purpose, the effects at varloua pa-
rameters on die sveraged bearing indication was de-
sirable (Author).
Electrortc Tech. Lah. , Wright Air Development
rav. , Wright-Patterson AFB, Ohio.
ABRASION RBSETTANCE OF HIGH -TEMPERATURE
COAXIAL CABLE JAOOST MATERIALS, by Bard
Suvorkrop. Rept. on Tliennionlc and SoUd Sute Blec-
troolc Technology. Apr 60, 8p. WADD Technical
note 60-75.
CWer trora OTS $0.S0| pb 171 118
Three dlffereat jacket aiaterlals for flexible, coaxial
cables that will be used at temperatiires of 2000C are
evaluated for their abrasion resistance. These mate-
n»iM *n (1) sUlcoos-vixalsh-impregnated Fiberglas
braids, (2) extruded fluorlnsted ethylene propylene
resin, snd (3) sllicone-rubber polyester fiber braids
Results indicate that Jackets (2) and (3) Iwve approxi-
mately 14 times the abrasion reaiatance of Jacket -<1)
(Author) '■
Electronic Tech. Lab. , Wright Air Development Dlv.
Wright-Patterson AFB, Ohio. t '
PROCEEDINGS OF THE WADC SYMPOSIUM ON J
METAL FILM RESISTOR PROCESSES, TECHNIQUES.
AND CAPABILITIES, by Robert E. Conklln. Rept. on
Improved Electronic Components. Feb 60, 203p.
11 refs. WADC Technical rept. 58-468: AD- 235 996.
Order fromLCmi$9.30, ph$31.80 PB 152 360
TWa report released for sale to the pubUc 28 Oct 60.
The objectives at this symposium were threefold: (1) to
provide an organized survey at the research and devel-
opment effort at film reaistors of the metallic film type,
and to provide a basis for the assessment of effeaive-
■<i»v^ progress of the total research and develop-
ment effort aa well as the present state-of-the-art; (2)
w serve as an incentive to investigators in the metal
film resistor field and to reduce the.reaults of their ef-
forts to writing for the benefit of all; (3) to further the
work being done by Industry of meul film resistors by
providing them wltii the Istest information available to
the governmem on the subjea asd thereby expedite the
commercial availability of more reliable Itema for
military use. The symposium pspers cover a wide
Istltude of subjects snd deal with the following general
areaa of interest: (1) physics of thin meullic films, (2)
Isborstory techniques for manufacturing thin film re-
sistors, (3) techniques for evaluating the capability of
naetal fllma, (4) the problems encountered in developing
production cspablllty, (5) problems encountered in the
research and development of meul film reaistors, and
(6) capabllltiea of metal film resistors. (Author)
Electronics Research Lab. , Northeastern U. ,
Bvanston, 111.
STUDIES OF COMMUNICATION CHANNELS, by
S»e-Uou Chang. Robert D. Klein and othera. Scien-
tific rept. no. 3, Pi. n. on Contraa AF 19(604)3053.
17 May 60, 43p. 9 refs. AFCRC-TN-60-574<II).
Order from LC ni43.30, ph$7.80 PB 150 645
This report is a brief summary of the progress to date
in miscellaneous studies of communlcstion channels.
The following topics are discussed: (1) The cspsdty of
a symmetrical binary channel with uniform digit apac-
ing, exponentially decaying memory, and additive
Gaussian noise Is approximated by a numerical method.
(2) Discrete chBanels sre combined to form cascaded,
sum, product, or other networks in order to achieve
such objectives as increaaing range, capacity, or
reliability. (3) Feedback systems for the reduction of
muMpath distortion have been evaluated. (4) A study
haa been carried <xM. at mathematical techniques sp-
plicsble to the combinstion of fallible formal neurons
as proposed by McCulloch. (Author)
f
46
Electronics Research Lab., U. of Olifomia,
Berkeley.
FERROMAGNETIC CORE FUNCTIONS IN THE
ANALYSIS AND DESIGN OF SELF- SATURATING
MAGNETIC AMPLIFIERS, by H- C. Bourne and
Di Nitzan. Rq>t. on [Contract Viaar- 222(7 A)] 1 Dec 5%
122p. 13 refs. Series no. 60, inue no. 261;
AD- 233 509.
Order from LC mi$6. 30, ph$19. 80 PB 146 750
Ihe object in this study is to analyze the three types erf
idf-saturating magnetic amplifier circuit in a general
form, appliable for design purposes. Based on ferro-
magnetic domain walls theory, a general core function
ia terms of mmf F, flux ^ and ^ is derived.
Electronics Research Lab. , U. of California, Berkeley.
RECENERATIVE MODES OF ACTIVE NETWORKS, by
E. S. Kuh. Rept. on Contract N7onr- 295(29). 3 Nov 59,
8p. 5 refs. Rept. no. 97; lER series no. 60, issue no.
258; AD- 230 482.
Order from LC mi$l. 80, ph$l. 80 PB ISO 511
An active device with passive imbedding csn produce
natural frequencies in the right half plane. In the design
(rf regenerative circuits, It is important to find the per-
missible location of regenerative modes. The maximum
real part of the natural frequency of an active device
under arbitrary passive imbedding was determined. It
ia shown that this regenerative mode can actually be re-
alized. For the case of s pentode, the required passive
network is a gjrrator. (Author).
Electronics Research Lab. , U. of California,
Berkeley.
VARIABLE-CAPACITANCE PARAMETRIC AMPU-
PIERS. by N. Kumagal. Rcpc on Contract N7onr-
29529. 17 Dec 59. 17p. 7 refs. Repc no. 98; Series
na 60, issue no. 263; AD- 233 477.
Order from LC ml$2. 40, ph$3. 30 FB 152 115
Variable- capacitance parametric amplifiers have been
constructed and operated satisfactorily at S-band. Two
resonant modes in the rectangular cavity have been
used as the aignal and idling tank circuits. The pump
power has been fed directly into the variable- capaci-
tance diode through a coaxial feeder making use of no
resonant circuit at the pun^ frequency. The dual -mode
cavity circuit has the (ollowlng advantages: (1) the di-
mensions and weight of the amplifier can be reduced
since only one cavity supporting two resonant modes is
used. (2) Since no resonant circuit for the pump power
is required, the practical difficulties of the frequency
adjustment are reduced. (3) The pump power is reduced
CO some extent because the diode is driven directly
through the pump feeder. (Authoz).
Essex Electronics, Berkeley Heights, N. J.
CHARACTERIZATKW OF I-F TRANSFORMERS, by
Charles V. Longa Final rept. for 1 Nov 54-30 June 57
on Contract DA 36-039- sc- 64522. [1957] 235p. 15 refs.
AD- 202 838.
Order from LC ml$10. 20. ph$36. 30 FB ISO 679
Sjpeclfication and characterization procedures in com-
aon usage in the industry as of the beginning of proj-
ect activity are described. The sbortcoraing9 of these
procedures are pinpointed and the requirements of a
satisfactory characterization procedure are delineated.
The important literature items which were consulted
during the background study are cited and two proposals
for solution evolved from this study are described in
broad outline. The two proposed methods are consid-
ered in turn. The detailed ^iplication is described and
test results presented. It is shown that Method I, which
relies upon parameter measurement, cannot satisfy
the essential accuracy requirements in the present
state of the measurement art. The successful applica-
tion of Method II, which relies upon direct measure-
ment of gain- bandwidth performance, is related chrono-
logically in conjunction with the presentation of numer-
ical test data. The development of ideas, techniques
and equipment pertaining to each phase of the opera-
tional procedure is described under appropriate sub-
headings. A summary evaluation of the method in -
eludes a listing of the variables requiring control and
the degree of control required for successful results.
(Author).
General Electric Co. , Owensboro, Ky.
ELECTRON TUBE EMISSION STABILITY, by John D.
Jordan. Rept. on Thermionic and Solid State Elec-
tronic Technology, Contraa AF 33(600)32562. Feb 60,
I03p. WADD Technical rept. 60-286.
Order from GTS $2. 50 PB 171 117
Previous work has Indicated that tubea are unstable to
some degree during the first few hours of life. An
investigation was made as to the magnitude and time
duration of this instability and what factors affea the
stability. (Author)
General Electric Co. , Schenectady, N. Y.
ELECTRIC DISCHARGE IN RF CABLES, by
W. T. Starr. E. G. Bianco, and J. Godfrey. Quarterly
rept. no. 1 on ContrBa DA 36-039-8C-78147.
16 Oct 58. 80p. 3 refa. AD- 207 809.
Order from LC mi$4. 50. ph|12. 30 PB 152 667
This report released for sale to the public 16 Nov 60.
The Interrelationships between life and electrical dis-
charge characteristics will be determined over a
range of temperatures, voltages, and frequencies.
Preliminary planning of the life test experiment, in-
cluding the choice of variables together with the "sur-
face fitting" technique of Dr. G. E. P. Box is described
The development of a cost -saving cable termination
which makes use of available alinninum funnels and
RTV silicone rubber is included iJA statistical com-
mentary on life testing is supplied which includes
mathematical concepts Useful for interpretation of re-
sults and for shartening the time requirements of the
life test. A computer pn-ogram was developed fra-
estimsting Weibull parameters on the life test data
with maximum accuracy. A survey of the literature ia
Included on the mechanism of electric discharge,
internal and surface discharges, effects of discharges
on polyethylene and butyl rubber, cable discharges,
and discharge measurement. (Author)
47
General Electric Co. . Syracuae, N. Y.
70-AMPERE HIGH POWER SILICON CONTROLLED
RECTIFIER, by R. M. Hunter. G. N. Hall and
R. P. Lyon. Final rept. for 19 Jan 59-18 Jan 60 on Con-
tract DA 36-039 -sc- 78278. [i960] I34p. 7 refs.
Order from LC mi|6. 90. p*42l. 30 PB 150 805
Tbe reaulta of studiea and Inveatlgatlona to optimize de-
vice propertlea vs. emitter and base resistivities, dif-
fusion parameters, junction areas, layer thiclmesses,
gate and cathode geometries as well as studies in the
theory at operation ot the three terminal PNPN structure
are presented. Fabrication techniques, equipment de-
scriptions and parts drawings to duplicate the devices
delivered are fumiahed and data or sample devices is
included. Conclusions and recommendations are also
presented. (Author) (See also PB 145 815)
ITTLabs. , Nutler, N. J.
RESEARCH INVESTIGATIWi OF RECTIFIBRS FOR
MAGNETIC AMPLIFIERS IN MISSILES, by G. R. Leef.
Final rept. for June 54- May 58 or Contract DA 36-039-
sc-64492. Oct 58, 179p. 3 refs. AD-211 953.
Order from LC mitt. 10. ph|27. 30 PB 150 678
The development <rf two diffused- Junction silicon recti-
fier models, basically raced at 50 noa and 2 amperes
and intended for use In printed circuit applications, is
described. Test data show that these rectifiers are
capable at meeting most of the target specifications. Ex-
perimental data showing the performance ot rectifiers
in a magnetic ampllfiler circuit and also measurements
at reverse recovery current effects in rectifiers are
presented. (Author)]
I
* Lincoln Lab. . Mais. Inst, at Tech. , Lexington.
THE ACM-52 AUTOMATIC CLUTTER MAPPER AND
PRELIMINARY EXTCRIMENTAL RESULTS, by
J. N. Harris and E. J. Madle. Rq)t. on Contract
AF 19(604)5200. 30 My 59, 52p. 19 refs. Technical
rept. no. 206; AD- 230 025.
Order from LC mi$$. 60. pb$9. 30 FB ISO 594
The ACM-52 Automatic Clutter Mapper la a stteclal-
purpoee, digital-data processing system. The ACM-52
accepts, stored and processes up to eight complete
scans (frames) of slowed- down video (SDV) data. A
fixed, but readily adjustable, program causes the
stored information to be processed so aa to yield a
mapping function. This function can then be used to
blank out portions of a display where returns occur too
frequently - a characteristic of certain types of clutter.
Preliminary experimental results Indicate the useful-
ness and flexibility at ACM-52 as a research tool in
investigating the natare of SDV cluttey . Jia current use
at a test site may indicate the possibility of using dils
technique to replace a similar task now performed by
a human operator. (Author)
Lincoln Lab. , Masi. Intt. of Tech. . Lexli^;too.
ADDITIONAL TEST^ ON THE AN/FRC-47 (XD-I)
MOdC-UP SYSTEM, by a E. NlchoU. Rept. for Apr -
Oct 59 on Contraa Ap 19(604)5200. 11 Mar 60, lOp.
Group rept. 36-44.
Order from LC ml$L 80, phSl. 80
PB 152 041
Several series of testa and measurements were made
over the Millstone Hill — Sauratown Mountain system
using the AN/FRC-47(XD-1) mock-up equipment to
measure both system performance and propagation ef-
fects. The equipment operates in the 400-Mcps region
over the 640-mile path. As a communicaticm system,
single- sideband modulation Is employed with 4th-order
diversity, but the equipment may also be used in other
manners for specific tests.
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
ANALYSIS OF SOME DETECTION CRITERIA FOR
PULSE RADAR, by E. J. Kelly, D. H. Lyons and
others. Rept. on Contract AF 19(122)458. 24 Jan 58.
1^. 4 refs. Technical rept. na 172; AD- 110 039.
Order from OTS $2. 40, ph$3. 30 PB 150 608
Th6 detector input is assumed to consist of a sequenct
of samples erf the IF modulation taken at regular inter-
vals of tln^e t^ ■*■ (n- 1)T, n - 1, 2, . , . . N and T is die
time interval Between transmitter pulses. The se-
quence of samples of the IF modulation taken is z(to),
^to •».T> z[to -^(n-lT], where z(t) is the complex
video process z(t) ■*iy(t). The discrete signal process,
without noise, is assumed to be of the form Sn ■ Sft^*
(n-l)TL » A exp [i(n V--6J\. where the Doppler phase la
y . Q-T andd - *>D(tQ^. 1) + ij^. This process ap-
plies exactly to a fixed-antenna radar and approxi-
mately to a scanning radar if the number of pulses la
siOficiently small. The method of maximum likelihood
la uaed, and formulas relating to sensitivities and
false-alarm rates are obtained.
Lincoln Lab. , Mass. Inst, of Ttech, . Lexii^^too.
THE CHARACTEREIATION OF CHANNELS WITH
RAPID MULTIPLICATIVE PERTURBATIONS, by
Herbert Sierman. Rept. on Contract AF 19(604)5200.
26 Aug 60, 4Pp. 20 refs. 25 G-0004.
Order fran LC mi$3. 30. ph|7. 80 PB ISO 796
Lincoln Lab. , Mass. InsL of Tech. , Lexington.
DESIGNING FOR RELIABILITY, by N. H. Tk^or.
Rept. for 1948-1956 on Contract AF 19(122)458.
9 Dec 56, 59p. Technical repc no. 102; AD- 93 756,
Order from LC ml$3. 60, ph|9. 30 PB 152 295
This report relessed for sale to the public 25 Oct 60.
The achievement of reliability is a goal that must be
pursued from the very beginning of the system design
project. The first step Is to consider each individual
component to be used in the system and to critically
analyze its capabilities and limiutlons. The second
step In the design project is to determine the applica-
tions of these components that tend to take advantage
of the best capabilities of these components and avoid
their worst limitations. This report lists analyses of
components and the resulting component applications
that have been made over a period of several years.
The third and final phaae of the design project is the
actual electronic circuit design, based on the compo-
nent i|nalyses and applications notes derived earlier
and predicated on the achievement of high reliability.
The thorough deaign method is described In detail.
This method provides reasonable component tolerancea
and adequate safety margins, and incorporates mar-
ginal checking throughout the design proceaa. (Author^
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
A METHOD OF PULSE COMPRESSI(»J EMPLOYING
NONLINEAR FREQUENCY MODULATION, by
B. L. Key, E. N. Fowle, and R. D. Haggarty. Rept.
on Contract AF 19(604)5200. 13 Aug 59, declassified
Mar 60. Up. 3 refs. Technical rept. no. 207.
Order from LC mi)2. 40, ph$3. 30 PB 150 595
Ib many of the pulse compression systems that have
been recently built or proposed, the receiver has been
deliberately mismatched to achieve a more desirable
receiver output waveform. In particular, most linear
FM pulse compression systems employ, in the re-
ceiver, some sort of weighting network designed to sup-
press the side lobes of the signal autocorrelation func-
tion. The deviation of the receiver from a matched
filter results in a loss in detection capability. We pre-
ssBt here a pulse compression method that achieves a
desirable receiver output waveform and, at the same
time, requires the receiver be an exact matched filter
to the sUmal transmitted; in addition, the transmitted
waveform is made to have an approximately rectangular
envelope. The method permits the receiver output or
autocorrelation function and the time duration and en-
fslope shape of the signal to be transmitted to be inde-
pendently specified at the outset. The method hinges
upon one's ability to specify the phase characteristic erf
• dispersive all -pass network. An approximate expres-
sloa for the phase characteristic is derived in terms of
die envelope shape desired and the signal energy density
spectrum. The quality of the approximate relation im-
proves as the signal bandwidth -time product increases.
The method is illustrated by an example. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
A METHOD OF SIDE- LOBE SUPPRESSION IN PHASE-
CODED PULSE COMPRESSION SYSTEMS, by
E. L. Key, E. N. Fowle, and R. D. Haggarty. Rept.
on Contract AF 19(604)5200. 28 Aug 59, 8p. Technical
rept. no. 209; AD- 229 403.
Order from LC mi$l. 80, ph$l. 80 PB 150 597
This report presents a method whereby the side- lobe
level of a phase-coded pulse autocorrelation function
may be suppressed, in principle, to any de^ed level.
Tbe side lobes are suppressed by mismatching the re-
ceiver; consequently, the detection capability is re-
duced. The method is explained by an example wherein
a weighting network is designed to suppress the side
k)bes of a particular phase-coded pulse autocorrela-
tion function. A bound is placed upon the loss in detec-
tion chat is caused by this weigbcing. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
PARABOLOIDAL REFLECTOR PATTERNS, by
R. L. Pease. Rept. on Contract AF 19(122)458.
S Aug 58, I'H). 7 refs. Technical rept. na 1841,
AD- 133 862.
Order from LC mi$2. 40, ph$3. » PB 150 592
Principal E- and H-plane radiation patterns are ob-
tained analytically for a finite paraboloidal reflector
widi an axlally symmetric feed at the focus. The effect
of a quadratic phJase term resulting from the use of the
current- distribution method is included, without re-
course to the usual plane- aperturp approximation. Re-
■ulta are expressed in a series of Lommel functions.
with coefficients pr<qx>rtlonal to the coefficients of ex-
pansion of the primary pattern in a series of orthogonal
polynomiala. For uniform illumination, the amplitude
of the first minimum in either principal plane is i^-
proximately l/5ka times that of the main lobe, where
k > 2if/^ and a is the focal lensth. For arbiury il-
lumination, ceruln general relationships between pri-
mary and secondary patterns are deduced for very
small and very large angles. (Author).
Lincoln Lab., Mass. Inst, of Tech., Cambridge.
PARABOLOIDAL REFLECTOR PATTERNS FOR OFF-
AXIS FEED, by S. S. Sandler. Rept. on Contract
AF 19(604)5200. 14 July 59. 25p. 12 refs. Technical
rept. no. 205: AD- 226 245.
Order from LC ml$2.70. ph$4.80 PB 148 368
The problem of predicting the radiation {>anern for an
asymmetrically illuminated paraboloid is covered in
some deull. The current distribution method is given
in a final form suitable for machine computation. An
approximate analytical solution using scalar diffraction
methods is compared with the experimental results and
the machine solution. (Author)
Lincoln Lab., Mass. Inst, of Tech., Lexington.
A PROBABILITY MODEL FOR COHERENT PHAffi-
ONLY MTI SYSTEMS, by.J. W. McGinn, Jr. Rept. on
Contraa AF 19(604)5200. 4 June 59. 17p. 4 refs.
Technical rept. no. 204; AD- 220 812.
Order from LCml$2. 40, pli$3. 30 PB 150 593
An approximate probability model is described for the
output of a phase-only, single video-delay line coher-
ent MTI system when the input to the system is the
radar return from a moving target in sea clutter .
Specific allowance has been made In the model far the
inclusion of radar receiver noise effects. The model
may be scaled In most of its major parameters and
thus can serve as a comparative measure of perform-
ance between specific MTI systems. (Author)
Lincoln Lab. , Mass. bist. of Tech. . Lexington.
RELIABILITY MODIFICATIONS TO THE ADC«R AND
KINEPLEX CONVERTER,. by P. L. Grant. E. J. Hof-
mann and others. Rept. on Contract AF 19(604)5200.
25 At« 60, 13p. 1 ref. Rept. 25G-0017.
^ Order from LC mi$2. 40. ph$3. 30 PB ISO 438
As part of the Group 25 effort in the testing of digital
data systems designed to function over voice -bandwidth
telepl^pne circuits, the Kineplex converter had been
built and used in conjunction with the ADDER for the
testing of the Collins TE 206 Kineplex. After several
weeks of testing it became obvious that pulses of exter-
nal origin were causing spurious errors to be added.
This report describes the methods which were used to
combat this unwanted noise and the modifications in tbe
ADDER and Kineplex converter vrhich resulted.
(Author)
Lincoln Lab. , Mass. bist. of Tech. , Lexington.
SEMICONDUCTOR DELAY LINES, by J. J. G. McCue.
Rept. on Contract AF 19(122)458. 15 Apr 58, 8p.
13 refs. Technical rept. no. 179; AD- 110 050.
Order from LCnU$l. 80, ph$l. 80 PB 150 609 '
the drift of minoJity carriers in an electric field in a
semiconductor provides a mechanism tor delaying a
video signal. Equfttioos are developed for the delays
and rise times that may be expected. At room temper^
ature, one can ex^t delays of tens of microseconds
with rise times of; the order of aie microsecond. At
lower temperatures, the delays irtld rise times are both
' shorter. It is shoim that the ratio of delay to rise time
depends only on the temperature and on the potential
. difference through! which the carriers drift. Apart
from theae factors, the delay- to- rise- time ratio does
not depend on the ^hoice of semiconducting material.
(Author). ;
Lincoln Lab. . Miss. Inst, of Tech. , Cambridge.
STUDIES IN PARTIAL SWITCHING OF PERRITE
CORES, by R. H. Tancrell and R. E. McMahon. Rept.
on Contract AP 19^604)5200. 21 Sep 59, 19p. 9 refs.
Technical rept. noi 210; AD- 227 928.
Order from LC inl$2. 40. ph$3. 30 PB 149 773
inll2.'
Under the influenc* of a narrow pulse of high -amplitude
current (an impulst of current), only a portion at a fer-
rlte core is switched and the core remains In a partially
switched state at tl»e end of the pulse. Partially switched
states can also be Achieved with low-amplitude currents
that do not produce fields strong enough to switch every
portion of the core., The characteristics of Mg Mn fer-
rite cores in various partially switched states are stud-
ied. The switching! characteristics of cores uixler drlv
ing conditions of hi|h- and low -amplitude currents (rf
different widths ar^ presented. A detailed discussion
is given of the uhpulse switching mode of core operation
to achieve increased memory speed. Additional results
are presented for stoecial cores fabricated with different
geometries. It is f^und that the amplitude and width at
the partial -switchiite current has a pronouncecf effect
on the core's behavior to subsequent drive pulses. Only
an inner ring of a qore is switched by a low -amplitude
current. With a hi^ narrow current, flux is switched
in a varying degree ifrom the inside to the outside diam
eters. Models are proposed to describe the speed of
switching in various regions of a core so that the per-
centage of flux switched in the different regions can be
predicted. The model is based on the nonuniformity of
the driving field actoss the dimensions of the core.
While the information gained from this investigation,
other computer applications of partially switched cores
are proposed. (Autk>r)
Lfcicoln Lab. , Ma^s. Inst, of Tech. , Lexington.
TRANSISTOR LIFE[iN THE TX-0 COMPUTER
AFTER 10,000 HO^RS OF OPERATION, by D. J. Eckl
and R. L. Burke Rtpt. on Contract AF 19(604)5200.
14 ^r 60, 47p. Technical rept. no. 221; AD- 239 227.
Order from LC ml$fi. 30. phJ7. 80 PB 150 601
The TX-0 computer^ began operating in April 1956.
This computer is a $-Mcps machine employing 2600
type L-5122 surfaced- barrier transistors in its high-
speed central sectic^i. During Its Initial period of opcr
ation at Lincoln Laboratory, the computer had a
256 X 256 word magnetic -core memory driven by
vacuum tubes. Aftef some 6000 hours of operation,
678 surface- barrier I transistors, 58 microalloy tran-
sistors, and 102 grrtwn- junction transistors were re-
moved for retest. Tpe results of this examination were
50
presented in Technical Report No. 199 and are re-
peated In this report. During the Summer of 1958,
TX-0 was moved from Lincoln Laboratory to M. L T
and a 64 X 64 word transistor-driven cSre memory wai
substituted for the larger one. After one year of oper-
ation at M. I. T. , the transistors had reached a total cf
about 10,000 operating hours. In July 1959, the 58
microalloy transistors and 800 surface- barrier tran-
sistors were again removed for retest, the results of
which are presented in this report. During the entire
period of operation, only one transistor-a light-pen-
ampllfler-waa removed as an "uncaused" failure. No
data are available on "personnel- induced" failures.
Approximately 10 per cent of the transistors tested fdl
below original acceptance specifications, but they were
returned to service and have operated normally. Cer-
tain of the parameter variations were unexjjected and
appear to be characteristic of surface changes in the
surface- barrier transistor. The results of the tran-
sistor tests so far are excellent and surpass those
originally anticipated. (Author).
Lockheed Aircraft Orp. , Sunnyvale, Calif.
CATHODE RAY STORAGE TUBES, by A. A. Beltran.
Spptial bibliography for 1947-1959. 20 Apr 60, 34p.
lis refs. S8-60-1.
6rder from OTS$ 1.00 PB 171 127
This survey covers the work on storage tubes from
late 1947 through 1959 and represents the report, peri-
odical, and technical society literature on this subject.
The sources consulted include the card catalog of the
Armed Forces Technical Information Agency, the vari-
ous catalogs of LMSD's Technical Information Center,
Science Abstracts - Sections A 8i B, U. S. Government
Research Reports. Engineering Index, Doctoral Dis-
sertations, and the Abstracts and References of the
Electronic and Radio Engineer (London). Russian,
French, and (jerman articles have been Included only
when similar material was not available iii English.
Storage tube fabrication processes and problems are
nor included.
Lockheed Aircraft Corp. , Sunnyvale, Calif.
A NONUNEAR CAPACITOR HARMONIC GENERATOR
SUITABLE FOR SPACE-VEHICLE APfUCATIONS. by
P. M. Fitzgerald, T. H. Lee and others. Technical
rept. 00 Physical Electronics. July 60, 41p. 8 refs.
LMSD- 703043.
Order irom LC ml$3.30, ph$7.80 PB 152 026
This paper descrlbea a small, compact, efflcleni, 9ih-
harmonic generator which consists of two cascaded
triplers. This device was designed to operate in the
environment normally encountered during the launch of
a satellite and its subsequent sustained orbital flight.
The results of environmental tests of shock, vibration,
acceleration, and temperature are presented. In addi-
tion, the results of an analysis made on two basic
harmonic generator's circuits are presented. Curves
of conversion efficiency as a function of the harmonic
generator's circuit parameters are presented for each
circuit (for harmonic numbers 2 through 10, inclusive).
This work Is an extension of Chang's wcM-k and allows
one to take into account the effect of lossy nonlinear
elements on conversion efficiency. (Author)
Ifallory, P. R. , and Ca , Indianapolis, Ind.
PACKAGING AND INTEGRATION OF TRANSISTOR
ASSEMBLIES, by R. Albon, D. N. Llghtboume and
%, L. Meek. Final repc for 1 July 56-31 >n 58 oo
Oontract DA 36-039- sc- 72834. [1958] 17^ 82 refa;
AI>-208 937.
Older from LC mi$8. IQ, ph$27. 30 PB ISO 810
XUm IB the final rqwrt of a research and development
■(ofram for the establishment of practical and effective
laDfhodn of packaging and integrating transistorized
^ited circuit assemblies. Package analyses pertain-
to integration, size and weight, therroal adequacy,
dlmatic protection, ruggedlzatlon, and maintenance
have been Included. The five representative systems
of integration and packaging which were developed and
Ibt work which led to their development are dlacuaaed.
S^octfic principles and techniques compatible with tran-
■iRorized printed circuit board are presented in the
DMign Guide"(FB ISO 809). (Author).
Mallory, P. R. , and Ca , Inc. , Indlanapolla,
tad.
PACKAGING AND INTEGRATION OF TRANSISTOR
ASSEMBLIES. DESIO^i GUIDE, by R. Albon,
D. N. Llghtboume and R. L. Meek. Rept for 1 July 56-
SIJan58 on Contract DA 36-039- ac- 72834. [1958] 105p.
77 refs; AD- 208 936.
Order from LC mi$5. 70, ph$16. 80 PB 150 809
Tlda design guide provides the design engineer with in-
tomatlon to guide him in circuit packaging and Integra
dOB of prlnted-wire subassemblies of minimum size
md weight for transistor applications. Other factors
such aa thermal adequacy, maintenance, ruggedlzatlon,
Md climatic protection are conaidered and designs sug-
|Mted compatible with such requirements. (Author).
MeUbs, Palo Alto, CaUf.
INVESTIGATION OF MICROWAVE NON- LINEAR
EFFECTS UnUZING FERROMAGNETIC MATERIALS
by Roy W. Roberts. Quarterly progress rept. no. 12,
1 Peb-30 Apr 60, on Contraa DA 36-039-8C-73278.
1960, 35p. 4 refs. AD- 239 869-
Order from LCml$3. 00, ph»6. 30 PB 150 683
Two expressions for second harmonic conversion effi-
ciency are developed in terms of a normalized sample
volume, the ferrite material properties, and the im-'
pedances of the test section. The conversion efficiency
can also be expressed in terms of external and unloaded
Q's. It is not certain at this time whether the ferrite
loss parameter which should be used in the conversion
expressions should be a surface limited linewidth or a
surface Independent spin- lattice relaxation time. Three
verslona of a K-band ferrite parametric amplifier have
been built and considerable teata have been carried out.
Two approaches have been carried out using TEqi and
TMoi signal modes. So far, no pump interaction or
oscillation have been found. The third version, which
has only received preliminary tetta, makes uae of
kagitudlnal pumping and a large single cryital garnet
qtere. (Author) (See also PB 147 994)
Melabs, Inc. , Palo Alto. CaUl
RESEARCH AND DEVELOPMENT OF A SOLID STATE
PARAMA04ETIC MASER, by Roy W. Roberts and
Harold D. Tenney. Final rept. for 10 June 59-9 June 60
on Contract AF 19(604)4071. 30 June 60. 130p. 24 rcCa.
AFCRL-TR-60-173.
Order from LC mi$6. 30, ph$19. 80 FB ISO 736
Methods of broadbanding the CW solid state maser have
been investigated, the most promising approach being
through the use of slow-wave atructures utilized in a
traveling- wave maaer (TW^^. Several types of alow-
wave structures were investigated experimentally. Best
results were obtained from an "ungrounded comb" con-
figuration. Methods of achieving non- reciprocal atten-
uation were investigated resulting in development of a
short-circuit stable amplifier. During the TWM exper-
imental phase cross relaxation effects were noticed.
Theoretical analyses were carried out on several types of
cross relaxation mechanisms and their effect on maaer
performance analyzed, b waa shown that these effecta
can either enhance or d^rade maaer performance, de-
pending on the type of mechanism involved, thejxra.-
oiagnetic ion concentration, the lattice temperature and
other related parameters. A survey of methods and
problema associated with high frequency masers was
carried out. It appears that rutile is the moat promising
material for millimeter masers as the present time.
(Author) (See alao FB 146 323)
Midxigan U. Research Inat. , Aim Arbor.
THEORETICAL AND EXPERIMENTAL INVBSTKJA-
TION OF RADIOACTIVE IONIZATION GAUCXS. by
Mohammad A. El-Moallmany. Doctoral tbeaia. Scien-
tific rept. DO. HS-1 on Contracts AF 19(604)545, 1511.
1948 and 6162. May 60. 199p. 52 refs. 2096; 2406;
2597: 03554-1-S; AFCRL-TN-60-658.
Order from OTS $3.00 PB 171 106
This dissertation la iotended to be a ooatrlbutioa to-
warda a systematic study of the properties and behav-
ior of radioactive ionization gauges. The chief ionic
and electronic processes encountered are briefly re-
viewed. Then a relationahip between the collected Ion
current and the gas pressure is analytically developed
for a planar configuration, conaldering the probability
of electron attachmem as a function of the electric
field incenaity and the gas pressure. In calculating the
theoretical current-pressure curves, the numerical
values used for ionic mobilities and the recombinatloa
coefficient are those derived from kinetic theory;
Bloch and Bradbury's theoretical values of electron
attachment are used for differeix mixtures ot nitrogen
and oxygen. E]q>erimental current -pressure curves
are found to be In fair agreement with the theoretical
reauhs. It Is indicated that the hysteresis phenome-
non, sometimes exhibited by ionization gauges, may
be caused by: (1) Temperature dependence of the main
electronic proceaaes Inside the gauge. (2) Varlatioa
in the environmental condltiooa which may result In a
change In the composition of one or more of the prea-
ent electro- negative gaaes. It is shown that the pri-
mary ionization by alpha particles, in a gas of con-
stant density, increases as the temperature decreases.
The results led to the design of two radioactive iooi-
zatlon gauges: one uses alpha particles emitted from
a radium source as the ionizing afent and the other
emplo^a beu particles from a tritium source.
51
Microwave Assotiates, bic. , Burlington, Mass.
HIGH POWER C-BAND BEACON MAGNETRON RE-
SEARCH AND reVELOPMENT PROGRAM. Quarterly
progress rept. no. 1, Appendix 1, on Contract
DA 36-039- SC-789H 25 Feb 60. 9p. AD- 237 957.
Order from LC nii|l. 80. ph$l. 80 PB 150 448
Additional informaiion on anode and output design, in-
put assembly, and kuner assembly and mechanism.
(See also PB 147 9i5).
Microwave Reaea^cb Inst. , Polytechnic Inst, of
Brooklyn, N. Y. '
THREE-PHASE MAGNETIC MODULATORS, by Edward
J. Smith. Repc. on Contract AF 30(602)1619. 7 July 60,
42p. 11 refs. Research rept. R-778-59; PIB-70o;
RADC-TN-60-168.
Order from LC mi4|3. 30, ph$7. 80 PB 150 875
The polyphase modfiator provides a means for obtaining
an output pulse -repetition rate which is greater than that
of the input a-c fre<iuency by an integral factor. Core
iron volume re<^irtments are determined by analysis,
and it is found chat the size of a three-phase modulator
need not be appreci^ly greater than that at a single-
phase line with an a-c source of three times the fre-
quency of the three-phase source. Experimental re-
sults on four basic ihree-phase connections show that
all circuits can be ifiade to operate in a stable and bal-
anced manner, yielding three output pulses per cycle
having equal amplit^ides and interpulse spacii^. The
effecu erf phase interaction on required modulator size,
staUlity. and ease pf balance are investigated. (Author)
MinneapoUs-Honeywell Regulator Co. , St. Petersburg
Fla
A CCSIGN STUDY FOR A MAGNETOMETER STABl-
UZATION SYSTEM, by W. J. Beirne. Final rept.
Phase 2. 15 Oct 59-^ Feb 60, on Contraa
AF 19(604)5216. 7 Mar 60. 81p. 2 refs. MH Aero
Document R-ED 28030; AFCRC TR-60-263.
Order from LC mi$4 80. ph$13.80 PB ISO 931
This report describes the preliminary design Of a mag-
netometer stabilization system. The primary use ct the
system is to maintain the axes at three Earth magnetic
field sensors In a preset azimuth and level orientation
during a ten-minute vertical flight of an Aerobee-Hl
sounding rocket. Included are a preliminary speclflca-
Uon, stating the design aims; a description d the de-
sign; the ofjeratlng procedures, and the design studies
which established the mechanical and electrical prop-
erties of the hardware (Author)
National Bureau of Standards. Boulder, Colo.
VHP AND UHF POMyER GENERATORS FOR RF IN-
STRUMENT ATIO^. by A. H. Morgan and P. A. Hudson.
Sep 60. 24p. 2 refs. Technical note no. 77.
Order from OTS $0. 75 PB 161 578
The work described Jn this report was undertaken to
provide certain projects with a series at fixed fre-
ycy rf generators having good stability with re-
•pect to both frequency and power output level aixl
continuously adjustable in power output from I to 100
watts. Prior to the oompletloo at the generators the
work at some at the standards projects was seriously
hampered because the rf generators available were
lacking In either sufficient power output, frequency
stability, or power output stability. For example,
bolometer bridges used for rf voltage and power meas-
uremems are sensitive to power Input variations as
small as a few parts In 10*. Power stability of at lease
one part In 10^ Is considered an absolute necessity to
obtain measurement accuracies of from 0.5% to 1%.
(Author)
Naval Research Lab. , Washington, D. C.
THE RELATIONSHIP OF A RETINAL-GAIN INDEX
TO SYSTEM PERFORMANCE, by S. Seldensteln,
R. Chernikoff, and F. V. Taylor. Interim rept.
26 Sep 60, 8p. NRLrept. 5548.
Order from LC mill. 80, pfa$1.80 PB 149 849
In a closed- loop man-machine control system, the re-
lationship between a given system error and the error
signal as Imaged on the retina of a tracker's eye Is
determined by (a) the display gain and (b) the viewing
distance. The reciprocal at viewing distance can be
termed optical gain. Display and optical gains of vari-
ous values can be convened to yield a single index,
namely retinal gain, which indicates the ratio between
the error as Imaged on the retina and system error.
This study investigated the relationship at optical,
display, and retinal gain to tracking {ireclsion, using
a compensatory tracking system. The following re-
sults were obtained: Increasing either optical or dis-
play gain reduced ferrcr . For each value of retinal
gain, there was no significant change in error over
the range al display and optical gains used. It is con-
cluded that display and optical gains can be combined
into a single Index, retinal gain, and that this index
is systematically related to tracking error. (Author)
Naval Research Lab. , Washington, D. C.
A a>IRAL-GRATING ARRAY, byj. R. Donnellan and
R. T. Close. 23 Aug 60, 18p. 2 refs. NRL rept. 5499.
Order from LC ml$2.40, ph$3.30 PB 146 395
A problem associated with a two-dimensional spiral
doublet array is concerned with the faa that use of the
spiral doublet (i.e. , two equally excited spirals al op-
posite sense placed side by side) as an element to ob-
tain linear polarization leads to spacing difficulties,
since the disunce between elements is always twice as
much in one dimension as it is in the other dimension.
Thus, the allowable scan is seriously limited In one
principal plane. A method is proposed for obtaining
linear polarization from a single two-wire spiral an-
tenna (thus eliminating the spacing problem) by using It
in combination with a polarization grating and a ground
plane. Experimental results were obtained by combin-
ing eight al these elements in a one -dimensional array.
For the broadside position at the main beam, the field
was found to be linear, with the cross -polarized com-
ponent al the main beam being 40 db down from the
principal polarization. As the beam was scanned out to
±45 degrees, the Unearity decreased quite rapidly (to
approximately 10 db at 45 degrees) and the plane of the
linear polarization was routed: sidelobes were much
higher than predicted. Use o* this array (rather than an
array c^ doubletti) would Involve a compromise concern-
ing specifications, dependent upon the particular appli-
cation of the array. (Author)
52
jilavy Electronics Lab. , San Diego, Calif.
BROAEBAND SLEEVE ANTENNA FOR OMNIDIREC-
TIONAL SHORE STATION USE, by W. E. Gustafson,
T. E. Devaney, and N. H. Balll. [1954] 12p. 4 refs.
Rept. 478.
Order from LC mi)2. 40, ph$3. 30 FB 152 615
llilB report released for sale to the public 15 Nov 60.
lUa report deals with the development of omnidlrec-
tioaal transnUtting and receiving antennas for 2. 5 to
7. 5 Mc, 5. 0 to 15. 0 Mc, and 7. 3 to 22. 0 Mc. It also
Ttpans the testing of a 2. 5-to-7. 5 Mc transmitting
prototype antenna. It was concluded that omnidirec-
tional antennas at the type developed can reduce the
total number of vertical antennas required and/ or in-
crease the efficiency of naval shore stations. (Authdr)
New York U. Coll. at Engineering, N. Y.
AN OPTIMUM SELF- SYNCHRONIZED SYSTEM, by
S. & L. Chang and B. Harris. Scientific rept. no. 1
oo Contract AF 19(604)6168. 8 >uie 60, 52p. 5 refs.
AFCRC TN-60-586.
Or6n from LC ml$3. 60, ph$9. 30 PB ISO 764
Sjnchronous detection has been often used as the model
for the modulation scheme al feedback systems. This
report considers the synchronization problem then
present. One optimum sdieme for transmission In the
pretence at additive noise is binary PSK using a modi-
flsd equal -weight Reed Code and synchronous detection.
Hiis technique also permits the synchronizing carrier
•t the receiver to be generated from the message
itgnal itself, so that phase drifts due to multlpath and
doppler can be automatically and correctly compensated
for.
Office c4 Naval Research, Washington, D. C.
CNR STUDY GROUP ON MICROELECTRONICS. Final
rept. June 60, 18p. ONR-7. AD-239 826.
Order from GTS $0.50 PB 161 890
This report released for sale to the public 2 Nov 60.
This report presents the results of a survey and study
of the state-of-the-art In microelectronics with particu-
lar reference to its implications and impact on the Navy.
Tbe Navy has need for Improved functional performance;
increased reliability, better power efficiency, and de-
creased size, weight, and cost of electronic equipment
lad components. Microelectronic techniques and de-
<rices are capable al contributing to the satisfaction of
tU at these needs. The methods al approach to the field
can be subdivided into three groqps: packaging tech-
alques, integprated circuits, and functional blocks.
There is fairly wide-spread developmental activity in
the first category, with some actual production of pro-
totype and regular-usage units. Research and develop-
ment in the second category is being conducted by many
industrial concerns and government laboratories, while
vork in the third category is confined to a small num-
ber of research laboratories. The development and
•doption of microelectronic devices and techniques is
likely to have a profound and wide 'spread effect on the
electronics Industry itself and on electronic equipment
•nd functions. It will make possible functions which are
■ct now capable of being performed, will offer the
potential of large Increases in reliability, and can
achieve reduaions of size, weight, and power con-
sumption of very large proportions.
Office of Technical Services, Dept. of Commerce,
Washington, D. C.
TRANSDUCERS. Aug 60, 7p. 92 refs. OTS Selealve
Bibliography SB-428.
Order from OTS $0. 10 OTS SB-428
A bibliography of reports listed in the two OTS monthly
abstract Journals: U. S. Government Research Reports
and Technical Translations. This bibliography includes
repents added to the OTS collection during the period
1945 to September 1960.
Patterson Moos [Div. Universal Winding Co. ]
Jamlca, N. Y.
RESEARCH STUDY OF THE PHYSICAL AND CHEMI-
CAL REACTIONS Oi> PRIMARY AND SECONDARY
CELLS UTIUZING RADIOACTIVE TRACER ELE-
MENTS, by John A. DeRosa and Harry C. Ueb. Quar-
terly progress rept. no. 4 (Final) 16 Jan- 15 Mar 53, on
Contract DA 36-039-sc-15507. 15 Mar 53, declasBificd
24 June 58. 51p. AD-10 037.
Order from LC ml$3.60, ph$9.30 PB 150 843
This report released for sale to the public 1 Nov 60.
t
Radioactive tracer studies of the Zn/KOH/Ag202 sys-
tem were conducted with a type-C-1 battery assembly.
Electrolytic additives (Versene, zlncate) had specific
actions on the Zn electrode and increased the corrosion
rate at Zn with a consequent shortening of battery life.
The presence trf appreciable amounts of sulfite lowered
battery performance; small amounts of the additive may
be beneficial. Deoxygenated electrolyte improved the
battery. At high KOH concentrations and low discharge-
rates and in early stages of stand, the reaction
2Zn -t-tOH' - 2e— »2Zn022" -f2H20 ♦H2 prevailed at
the Zn electrode; otherwise the reaction 2Zn •*■
40H* - 2e — »2HZn02' ■♦•H2 predominated. The reac-
tion at the Ag202 electrode was Ag202 ■♦• 4e — >2Ag *■ 20
with Ag20 as the intermediate product. EMssolution of
Zn was enhanced by higher KOH concentrations up to an
optimum value, by a greater volume of electrolyte, and
by a greater distance from the Ag202 electrode. Ca-
pacity and storageability were functions of the arr^ount
of Zn dissolved, provided that no side reactions oc-
curred at both electrodes. Suggestions for improving
the battery include: reducing the KOH concentration to
20 to 25%, increasing the ratio of electrolyte volume
to weight of Zn, employing a small amount of antioxi-
dant or a deaerated electrolyte, and using inert, less
permeable separators.
Pennsylvania State U., University Park.
PROPAGATION DISTORTION OF BANDS OF LARGE -
AMPUTUEE ACOUSTIC NOISE. II. AN EXPERI-
MENTAL INVESTlGATICW OF CERTAIN PLANE
Wave cases, by FuJIo Oda and Eugene Ackerman.
Rept. on the Generation, Propagation, Action and Con-
trol of Acoustic Energy, Contract AF 33(616)2772.
May 60, 31p. 5 refs. WADD Technical rept. 60-233.
Order from OTS $1.00 FB 171 059
53
TTie equipment requirements for experimental studies
at finite amplitude dlgtortlon at bands at noiae is com-
pared with almllAr requirements for pure tone studies.
Based on this cooiparlsoo, the equipment waa aasem-
bted for noise-band studies including a specially coo-
Btructed iooophoae (corona-type loudspeaker^ Fre-
quencies used at the looophooe were In the 15 to 50 kc
range. The over- all sound pressure levels were varied
from 110 to 135 db re 0.0002 bars. It waa possible to
verify theoretical predictions for two o* the regions
described In a previous report. (Author) (See also
PB 171 021)
Radio Corp. of America, Camden, N. J.
MICRO MODULB PRODUCTICW PROGRAM Quarterly
rept. na 8, 1 Ja«-I Apr 60, on Cootraa DA 36-039-
sc-75968. (1960J 169p. 4 refa. AD-241 358.
Order from OTS |3. 00 n 171 126
Prococype tests oq microelements and nwdulea and sub-
sssemhlies were completed. Results of the prototype
B testa on a total of 1 16 capacitor microelements at all
required types indicate 10% failures, with 6% failures
attrllwted to high dissipation factors. At the end at the
2000-hr operating life test, 168 capacitor elements in-
cluding all types had 14% faUures of whic± 8^ had Ugh
dissipation factors, both before and after ttm test. The
dissipation factors of capacitors increased after as-
sembly into test modules and encapsulation by a pre-
dictable amount wfclch la calculable from module de-
sign. A cc)nsidentt>le number of failures at prototype
mockiles were due to troubles with the termlnsdons
rather than the capacitor elements. This problem waa
resolved in the prtxtiction erf final -grade capacitor
elements. A total at 36 wafers each comainlng 144
resistors showed oo failures at the end c* the 2O0O-hr
load life prototype test. Resistor performance durli^
B-2 tests waa generally good. A revised standard for
leads and wafer laoda for microelen)ent reaiators
yielded Improved resistors. A kwrer viscosity encsp-
sulant, Stycast 2691-40, together with new mokUi^
techniques and flxoires brought about considerable Im-
provement. In view of these changes and with more
rigid quality inspection in effect before aasemhly and
encapsulation, flnsl -grade Inductor mlcroelementa
will exhibit improved quality. (See also PB 161 911)
Radio Corp. of America, Harrison, N. J.
A STUDY OF ELBCTRON TUBE DETERIORATICW
UTILIZING KINETIC THEORY, byE. R. Schrader.
Quarterly rept. no. 3 for 1 Jan-1 Apr 60 on Contraa
NObar-77637. [1960] 94p. 38 refa. AD- 235 319.
Ctder from LC m45.40, ep(16.80 PB 152 753
Thla report released for sale to the public 16 Nov 60.
The final results at a 2000 hr life test oo factory pro-
duced 581 4- A electron tubes are given in terms at the
klnedc deterioration scheme. The resulting aalvatlon
energy compares favorably with those found in similar
tests. A descriptlce ia given of the life test conditions
for a set c< specially prepared tubes of this type. The
tests on gas evolution from 3 plate materlala give
activation constants consistent with the values found In
the literature when the former are computed on a sta-
tistical basis. However, tests on individual samples
give scattered results. An improved processing
schedule is discussed. Prellininary and background
S4
information It given on the sublimation and proceste
phsses. The results at the first determination of ^^
electrode, mica, and bulb deposits by use oT the x-rn
fluorescence technique Is tshulated. (Author)
Radio Corp. of America, Lancaster, Pa.
ELECTRON TUBE MATERIALS, GASES. AND
GETTERS, bjr J. C. Turnbull and G. P. Kirkpatrlck.
Quarterly progress rept. no. 3, 15 Apr- 15 July 59 on
Contract DA 36 - 039 -sc- 78226. 15 Aim 59. 56p. 3 re^
AD- 227 616. -• . "K r^o.
Order from LCml$3. 60. pii$9. 30 FB 149 707
Methods hsve been standarlzed for the determinatlas
ai thermal outgaaalng at tube nuterlals. (1) durli^
Initial outgaaalng In which the sample is heated in
ateps to lOOOOC and (2) during extended heating at a
lownr temperature of 400<>C. InitUl outgaaalng meas-
urements are given for nickel, cold rolled low carbos
steel, nickel plated steel, nickel coated gas carbonisii
steel, and tantalum. A method is described for deter*
mining getter performance under tube operating coo-
ditlans at very lo«r preasures and for extended time
perloda. Results at metallurgical examination o* the
metal samples being uaed in the prea^nt contract work
are preaented. (Author)
Ray-O-Vac Co. , Madison, Wis.
PAPERUNED MAGNESIUM DRY CELLS AND BAT-
TERIES, by P. F. Albert. IHnal technical rept. for
2 Apr 57-31 Mar 60 on Contract DA 36-039- sc-73241.
1960, 35p. AD- 240 194.
Order from OTS II. 00 FB 171 102
500 Individual cells escfa at the sizes N, AA. A, B, 0
aitd F as weU as 300 each of the batteries BA-63.
BA-408/U, BA-409AJ, BA-414AJ, BA-416/U. BA-418/U
and BA -422/U types were assembled. 150 Batteries of
each type were in-plant tested and performances are
reported. The performance figures obuined on the
BA-408/U and BA-409AJ batteries were genairally
aatlsfaaory. In the other 5 types of banerles tested
the performance was poor with s high incidence of
failurea. The reaaons for this are discussed. (Author)
Raytheon Co. . Waltham. Maas.
STUDY OF PLATINOTRON DEVICES. Quarterly rept.
no. 4, 1 Aug-1 Nov 59, on QICS779. Contract DA 36-
039-8C-78229. (1959J 21p; AD- 235 637.
Order from LC ml$2. 70. pfa$4. 80 PB 150 44(
The mechanical problem with respect to the cathode
support was resolved and one additional tube waa con-
structed for evaluation. Additional dau on thla tube
with reapect to coolant flow and cathode emiaaioo con-
firmed the findings in the first tube that these were
adequate for the objectlvea of the uak. Some informa-
tion was obtained on the amount of leakage current
is-esent in the tube, and It was determined that at a
value of njagnetlc field one-third that of the operating
level leakage current was very low. Additional datawsi
wx obtained because of destruction of the tube by an In-
ternal arc. Some arching may be expected in processln
the tube, and the protector circuit which normally pre-
venta such arching from destroying the tube was not
working properly. (Author) (See also PB 147 427)
RCA Defense Electronic Products, Camden, N. J.
MICRO-MODULE PRODUCTION PROGRAM. Quar-
terly rept. no. 5, 1 Apr-1 July 59 on Contract DA 36-
099-SC-75968. [1959] 265p. AD-228 166.
Older from OTS $4. 00 PB 171 125
Amang the main achievements of the quarter was the
receipt of the great majority of prototype mlcrp-
elements required for the prototype grade of modules
and the initiation of the authorized testing program on
these parts. Other accomplishments include the per-
fecting of multilayer thin film ceramic capacitors of
sizable capacitancea in wafer form, the design of a
hermetic solder-seal for micro-element quartz crys-
tals, completion of the micro-module and modular
■uteasembly heat transfer study relating permissible
aticro-module power dissipation to the elevation at
module temperature above that of the surroundings.
tad the completion of a number of prototype modules.
(Author)
Research Lab. of Electronics. Mass. Inst, of
Tech., Cambridge.
ON JAMMING SPEECH COMMUNICATION WTTH
COHERENTLY AMPLITUDE -MODULATED INTER-
FERENCE, by J. C. R. Lickllder, Raymond J.
Chrlstman. and Newman Guttman. Rept. on Ccvitraa
AF 18(600)1219. 13 Oct 57. declassified 23 Jan 59,
23p. 6 refs. AFCRC-TN-57-58; AD-110 090.
Order firom LC ml$2.70. ph|4.80 PB 148 972
The problem is to make speech communication unin-
telligible to an enemy and at the same time intelligible
to a friend. This report describes experiments on '
two possible ways of achieving that goial. (Author)
Sonotone Corp. . Elmsford, N. Y.
DESIGN AND MANUFAtTTURE OF SEALED NICKEL-
CAEMIUM CELLS OF CYLINDRICAL DESIGN, by
Francis J. Alllegro and Herbert Bllsky. Quarterly
progress rept. no. 1, 1 Dec 59-29 Feb 60, on Contract
DA 36-039-$c-84496. [1960] 58p. 3 refs. AD- 239 280.
Order from LC ml$3. 60. ph$9. 30 PB 150 449
The purpose of this contract is the design and manufac-
ture of 60 engineering test models of each of three sizes
of sealed nickel-cadmium cells, viz. 10 A. a . 50 A. H.
«nd 100 A. H. capacity, measured at the five hour dis-
charge rate. Six cells of each of the sizes (10 A. H. ,
50 A. H. . 100 A. H. ) are under construction as proto-
types. All are of the colled design, containing paper
separator and utilizing flat end-plates. The length to
(hameter ratio has been determbied analytically to pro-
vide minimum cell case weight. Positive plates contain
cobalt. Exploratory tests show promising results on
lubstitutes for paper separator. Material for construc-
tion of cell cycling equiiwnent has been ordered. De-
(igns have been established for domed end plates for
cells, and for a 100 A. H. cell incorporating rectangulai
stack-ups. (Author)
Stanford Electronics Labs. , Stanford U. , Calif.
THE ANALYSIS AND SYNTHESIS OF NONLINEAR
COITINUOUS AND SAMPLED- DATA SYSTEMS IN^ '
V(X,VING SATURATION, by F. Kurzweil. Jr. Rept.
ai Contract Nonr- 225(24). 30 Nov 59, 103p. 16 refa.
Technical rqx. no. 2101-1; AD- 231 411.
Order from LC ml$5. 70. ph$l6. 80 PB 150 493
This study has been concerned with the analysis and
synthesis of saturating systems which are either con-
tinuous or discrete. Initially these saturating systems
are broken into classes in which the representative
member is the physical plant in Jordan normal form.
The equations describing the plant are written in terms
of its impulse response matrix G(t) and the forcing
function m(t)f. The constraint on the forcing function,
i ni(t) 1^1, cat^orizes the system as a saturating
system. The optimum saturating system is defined to
be that system which returns to equilibrium in mini-
mum time subject to the constraint on the forcing func-
tion. The synthesis problem is that of construction of
the optimum switching surfaces in n-dimenslonal space.
The method proposed here consists in the construption
of a linear region by means of a subspace generator,
then the placement of the point x(0) on a boundary of
the linear region. Analysis in the sampled-dau realm
is considerably simpler than in the continuous case
slnct a given sampling period T automatically fixes
the lag- time between the physical plant and the track-
ing subspace generator and places bounds on the quan-
tity (Dev)^^^. (Author).
StanfcH-d Electronics Lab^. , Stanford U. , Calif.
INVESTIGATIONS OF THE HELTTRON OSaLLATOR.
by B. P. Israelsen Rept. on Contract Nonr- 225(24).
23 Nov 59, 225p 13 refs. Technical rept. no. 404-1;
AD- 232 289.
Order from LC ml$9. 90.^tM34. 80 PB 150 492
This report describes investigations aimed at providing
a better understanding of the helitron. The resuks of
experiments dealing with spurious oscillations are pre-
sented. Measurements of backward-wave gain by two
different methods are described. A second experi-
mental helitron was constructed, the r-f circuit in this
case consisting of two, rather than four, segments, with
an internal termination. The beam was injected from a
alalom focusing structure. Performance was not as
good as obtained with the first helitron. A small-signal
field theory based on expansion in normal modes is pre-
sented. This theory shows that azlmuthal beam bundl-
ing, i.e. , bunching in the direction of electron motion,
is the primary interaction mechaniam. A study of space
charge effects indicates that one of the two space
charge waves grows exponentially, even in the absence
of circuit fields. An equation for backward- wave gain
is given in which two circuit waves and two beana
waves are considered. (Author)
Stanford Electronics Labs. , Stanford U. , Calif.
A METHOD FCMR SOLUTICW OF NONLINEAR NET-
WORK PROBLEMS BY DIGITAL COMPUTERS, by
W. F. Gilhnore. Jr. Rept. on Contraa Nonr -225(24).
30 Dec 59. 183p. 25 refs. Technical rept. no. 2051-1;
AD- 233 022.
Order from LC ml$8. 40, ph$28. 80 PB 152 183
Contents:
The evolution of die approximatian method
Prony's method
'I\ittle's method^
Al^mate procedures
Calculation by continued fractions ^
Expansion of a series in a continued fraction
Converting continued fractions to ordinary fractions
55
SbBplc •pproodivacions
A cxxnplete table al approzimatlaDa
Questkmi d coqvergence
RelAtloa to Hllbert space theory
'Two special continued fractions
A related Itoear operator
Blgenfunctions ^ the linear operator
Inversioo d. the Stleltjes transform
Approodmate soliclon d nonlinear differential equations
Nature at the approximation
Oalculatlon at dK Initial derivatives
Other application* and examples
Digital computer programming
Network synthesis from time responsa
Analog computer fxmctlon generators
Approximations from discrete data
Stanford Electronics Labs. , Stanford (J. . Calif.
A MODIFIEO FORM OF THE MELLDM TRANSFORM
AND ITS APPLICATION TO THE OPTIMUM FINAL
VALUE CONTROL PROBLEM, by J. Peachon. Rqpt.
on Contract No«-«225<24). 3 Nov 59, 152p. 13 refa.
Technical rept. no. 2102-1.
Order from LC aU$7. SO, ph|24. 30 PB ISO 823
A conunon property d the class of control- ayatema de-
scribed by linear constant coefficient differential equa-
tions Is that tranoienta take an infinitely long time to
vaniah. It la therefore not possible to demand that the
output and output derivatives - called the atates - d the
device to be concnoUed - called the plant - accurately
assume specified vaiuea at a specified finite positive
time. The class d systems investigated in this report
Is characterized by the requirement that all the plant
sutes assume a prescribed value at some normalized
time 'one'. The linear, time-varying systems investi-
gated In this report have the property of moving the
plant to the desirod final atate in aplte of most disturb-
ances and parameter changes. A naodifled form of the
Mellin Transform providea a convenient tool to analyze
and ayntheslze such final-value systems; this tranafbrm
is applied to time-varying systems In a noanner quite
aimiiar to the Laplace Transform In linear constant-
coefficient systems. In addition to the final- value re-
quirement, it la often desired to make the plant output
follow a trajectory which la optimum In aome sense.
If this optimum trajectory Is described by a linear dif-
ferential equation, for Instance an Euler equation, the
modified form of die Mellin Transform can be used to
synthesize a control- system In which the plant-out ap-
proximately follows this optimum trajectory, regard-
less d the values d the given initial and the dealred
final atates. (Autlior).
r^
Susfbrd Resear«) Inst. , Menlo Park, Calif.
CORNER -REFLECTOR ANTENNA STUCHES, by
W. E. Scfaarfman. Technical memo. no. 1 on Contract
DA 04-200-ORI>-674. Sep 59, 39p. 7 refa. SRI ProJ.
2231: AD- 230 813.
Order from LC mi$3.00. p(46. 30 FB 152 614
Thia report released for sale to the public 16 Nov 60.
The results d various stixUes on corner -reflector
antennaa designed to fulfill specific antenna requlre-
menca d the Balliatlc Research Laboratory are sum-
marized. The theory of ideal corner -reflector an-
tennas is daacrlbeil and Ita ap^cadon to practical
antenna designs Is discussed. Both linearly polarized
and circularly polarized antennaa are conaidered.
(Audior)
Stevens Inst, of Tech., Hoboken, N. J.
LITERATURE SURVEY ON THE EFFECTS OF
NUCLEAR RADIATICW TO ELECTRON TUBE MA-
TERIALS, by E. R. Johnson. Rept. no. 9, 1 June-
31 Aug 59 on Contract DA 36-039-8C-73146. [1959]
I6p. 12 refa.
Order from LC i$l$2.40, Ffa$3.30 FB 149 713
ExperlmeKal tedudquea In studying rsdiatlon damagi
la critically reviewed and the effecta of experimental
conditiona discussed. It is concluded that subminis-
tiB-e tubes will be more susceptible to radiation damsfe
than ordinary tubea. Radiation damage to thin films
and field emlaaion catboda Is discussed. (Author)
Union Swltdi and Signal Div. , Westinghouse Air
Brake Co. , Swlaavale, Pa.
i»Y aRCurr tests and test equipment for
ACCBFTANCE TESTING OF RELAYS FOR LOW
LEVEL APPUCATICM, by Earl R. Dubas. Interim
engineering rept. no. 7, 1 Apr-30 June 59 on Contrso
AF 33(600)33403. (1959) 53p. 7 refa. AD- 219 750.
Order from LC ml$3. 60, pl49. 30 PB 152 79«
Thia report releaaed for aale to the public 17 Nov 60.
Miaa-teat result pattern: It is questionable that satis-
factory reliability predictlona can be noade based on
either relay performance during the flrat 5400 opera-
tiona or on a contact resistance charge after a miss-
test . Miss-test resistance rejection limita: Of the
varioua miaa-teat resisunce rejection limits used, none
provad to be the beat for predicting future reliability.
At the loweat level, or one ohm, the number of con-
tacta and consequently the number d relays connected
in series had to be reduced since the interconnecting
wiring became an Important factor. Environmental
Influences: 1250C - At elevated temperaturea the num-
ber of misses appeared to be slightly less than the num-
ber at room temperature. -b5°C - No change in the
number of contact failures was evident at lowered tem-
peratures. Vibration - Due to weight restrictions of
the vibration machine, only one relay at a time could
be mlaa-tested, thus the total quantity of information
gained was less snd the results less evident . They did,
however, Indicate that the number of miases should be
leaa particularly at the resonant frequencies of the
contact spring numbers. Contact current pulae wave-
form: The contact current waveforma uaed were saw-
tooth, alne and aquare waves. No significant differ-
ence between tests using various waveforms waa
evident Mechanical Investigation: The mechanical
inrescigstion disclosed the probable cause of all con-
tact failures to be particle conumination. (Author)
Varlan Associates, Palo Alto, Calif.
LOW NOESE BACKWARD- WAVE AMPLIFIER (VA-I91)
OBVBLOPMENT, by Kenneth R. Evana. Rept. for
May 56-Oa 59 on Tbermionlca and Solid Sute Elec-
tronic Technology, Contract AF 33(616)3521 . Mar 60,
64p. 7 refa. WADD Technical rept. 60-199.
Order from OTS $1.75 FB 171 069
56
ThlB report deacrlbes a development program for an
X-band, backward- wave amplifier. The history of
work Is outlined and successes and failures are noted.
Deaign changes during this period are mentioned. The
dua presented in the form of graphs are taken from
(hs final tube meeting the specifications and developed
jy<wr ihia program. Reamunendatioos for further
work or investigation are discussed. (Author)
Waahington U. [Seattle], Coll.. of Engineering.
TRAVELING WAVE ANTENNA WITH BROAD BAND-
WIDTH, by Rubens A. Sigelmann and Donald K.
Reynolds. Technical rept. no. 42 on Contract
AF 19(604)4098. June 60, 65p. 12 refa. AFCRC TN-6p-
S81'
Ordier from LC ml$3. 90, ph$l0. 80 FB ISO 4»7
A non- uniform linear array supponing a traveling wave
can provide a radiation pattern \rhich la substantially
conatant in thxpc over a large frequency band. It would
be possible to realize this constant pattern if the part
of the antenna that supports the surface wave remaina
Invariable with the frequency, 1. e. . the dimensiona erf
the operating part of the antenna are constant when
meaaured in wavelengths. In order to excite such an
antenna, a continuous excitation is required. The prob-
lems of coimllng the exciter to the array have been
studied analytically, and are presented in this report.
Experimental results have been conducted on a model.
The radiation pattern waa substantially constant, how-
ever some anomalies were noted. (Author).
Ordnance, Missiles, and Satellite Vehicles
Air Force Cambridge Researdi Center, Bedford,
Mass.
ATMOSPHERIC PHENOMENA NOTED IN SWUL-
TANEOUS OBSERVATIONS OF 1958 ^2 (SPUTNIK III),
by J. Aaroos and H. E. Whitney, eds. Aug 60, 33p.
5refs. ERD-TR-60-174.
Order from LC ml$3. 00, ph$6. 30 PB 152 200
Amplitude and doppler records of the 20-Mcps trans -
mlssiCMi of 195862 (Spumlk III) were simultaneously
made at six radio observatories in Europe. Several .
distinct phenomena were noted. A sharp decrease In
amplitude, which lasted from one-half to one and one-
half minutes and was followed by an abrupt return of
the signal, occurred at the same time at all stations,
l^is phenomenon has been termed "dropout, " although
indications of low -level signals were usually present,
and is explained as a sudden decrease in transmitter
power of the satellite when the satellite passes through
a region of high electron flux. Another type of decrease
In tibe signal was anributed to highly localized absorb-
ing or scattering regions. A third phenomeiKxi, re-
corded by techniques of simultaneous measurements,
was observed in the concurrence cf scintillating signals
at some sutions and Faraday routions at others. The
overlap of the propagation path to each station record-
ing the scintillations defines a vertical slab of iono-
spheric region responsible for the scintillations. The
region is about 400 to 600 km in the horizontal plane
but Includes scale irregularities of less than 1 km.
(Author)
Air Proving Ground Center, Eglin AFB, Fla.
OPERATIONAL SUTTABIUTY TEST OF THE TYPE
A-3 FIXED GUNSIGHT SIGHT LINE LEVEL INDICA-
TOR. Final rept. on ProJ. APG/TAT/60-A-1.
15 May 52, declassified 5 Nov 53. 21p. AD- 16 351.
Order from LC m42.70, pbM.80 FB 152 361
This report released for sale to the public 2 Nov 60.
The Indicator was tested on F-84E and F-86E aircraft
and in the climatic hangar at temperatures down to
-60^^. The Indicator waa concluded to be operationally
suitable with a filter setting of approximately 6. 0 in
temperatures down to -20°F. It has an elevation error
of 1/5 mil as compared to sn elevation error of 3 mils
for the A-2 sight line level indicator. It was recom-
mended that (1) a polaroid filter with a U^ contrast
comparable to the 6. 0 aening be Incorporated as an in-
tegral part of the instrument, and (2) the level vial
and/or ita mounting be redesigned so that accurate
readinga may be obtained at temperatures below -2[pv .
Allied Research Associates. Inc. , Boston, Mass.
LAUNCHING OF AIRBORNE MISSILES UNDER-
WATER. PART V. RESTRAINING AN UNSTABLE
MISSILE'S RESPONSE TO WAVES, by Theodore R.
Goodman. Rept. on Contract Nonr- 2343(00). 15Dec59,
14p. 4 refs. Document no, ARA-708; AD- 229 733.
PB 152 122
Order from LC mi$2.40, ph$3.30
It Is shown that the response at the tree surface of an
unstable missile undergoing a vertical underwater
launch does not increase with increasing launch depth,
but is restrained for waves whose frequency is above a
certain critical value. It is then pointed out that there
is s cut-off frequency in s fully -devek^>ed confused
ses below which no waves exist. Finally there Is ob-
tained the degpree of inatabillty of the miaslle such that
all frequency components in a fully -developed sea be
greater than the critical. Thus, if the design sea
state is specified it becomes possible to calculate the
degree of Instability which can be tolerated in cn-der
that the Complete response be restrained. By dealgn-
ing according to this criterion, the response to waves
may be reduced far below the unrestraii»ed response
to other disturbances induced by the sea. (Author)
(See also PB 149 510)
Army Chemical Research and Development Labs. ,
, Army Chemical Center, Md.
EVALUATION OF MONONITROPOLYSTYRENE AND
DINITROPOLYSTYRENE AS EXPLOSIVES, by George
D. Clift and Konstantinos Ablas. July 60, 17p. 6 refs.
CRDLR-3009.
Order from LC mi$2. 40. ph|3. 30 PB 150 664
This report describes the tests conducted in the inves-
tigation of mononltropolystyrene and dinitropolystyrene
as explosives con4>ounds. The results obtained indi-
cate that nwnonitropolystyrene can be detonated at ap-
proximately 1000 m/sec and that dinitropolystyrene
can be detonated at approximately 2000 m/sec.
(Author).
Army Ordnance Human Engineering Laba. , Aberdeen
Proving Ground. Md. >
MUZZLE BLAST MEASUREMENTS ON HOWITZER,
105mm, M2A2E2 WITH MUZZLE BRAKE NO. 8, by
Howard H. Hollantl jr. Aug 60, 28p. 5 refa. Technical
memo. 12-60.
Order from LC ml|2. 70, phH 80 PB 150 733
Measurements of rtuzzle blAsc were made primarily to
determine the peak overpressures produced. Measures
of positive impKiise and duration at posirlve phase were
also made. The hoWritzer was fired at ( evations ot
1°14'. 35<^', and ^D^'O" wlth-2 propelling charges:
Charge Zone No. 10 (7. 22 02. of T34 and 3. 75 Iba. oT
Ml 7) and 115% of maximum rated pressure (7. 22 oz. of
T34 and 4. 00 lbs. of Ml 7). Some of the overpressures
measured were hlgfe enough to nipture unprotected
human eardrums. It is recommended that attempts be
made to lower the peak overpressure below 4 pal. If
this criterion is nof met, ear protection should be nuui-
datory. (Autlrar).
Army Signal [Res«arcfa and Development Lab] Port
Mcnmouth. N. J. i
A NOMOGRAM FOR THE SOLUTION OP THE
RAPID SURVEY PROBLEM, by Riillp Marsh. 11 Mar 57,
25p. 1 re*. Technical mema no. M-1870.
OrdoriEeinLC mi$e.70. ph$4.80. FB ISO 684
An alignment chart or nomogram has been developed by
means al which the computations necessary to the solu-
tion d the Rapid Radar Survey Problem can be per-
formed easily and Meil within the accuracy require-
ments d the systems Widi the use r* this nomogram,
orientation angle can be determined to within three mils
and parallax to within twenty yards. Rand-McNally sod
Conqjany has prepared the nomogram. (Author)
Ballistic Research Labs. , Aberdeen Provliw Ground.
Md.
ATTENUATION OF AIR SHOCK WAVES IN TUNNELS.
by Robert 0. Qark »nd George A. Coulter. June 60.
19p. 11 refs.. Memo rept. no. 1278; DASA rept.
00. 1176: AD- 241 876.
CJrder from LC ml|t 40. ph$3. 30 PB 150 957
The attenuation ct peaked shock waves as a function at
travel distance along straight, smooth-walled tunnels
at conataot cross-secUon Is discussed. A theory Is
presented describing the attenuation as a function at the
rarefaction overtaking the shock front. A theoretical
attenuation curve and experimental dau are presented
for a pressure ratio at 5. (AuthcHr)
'Ub...
Aberdeen Proving Ground.
Ballistic Research
Md.
CHANGES IN DRAG CAUSED BY AIR H.AST SHIELD-
ING, by George A. Oouiter and William T. Matthews.
June 60, 31 p. 6 refs. Memo. repc. na 1279; DASA
rept. no. 1157; AD- 041 504.
Order from LC mi$3. 00, ph$6. 30 PB 150 454
An unshielded rectangular target model was exposed to
air blast loading in tl)e BRL 24-lnch Shock Tube In an
overpressure range of 5 to 30 pel. Average pressure
loadings over each at the front aod rear surfaces cf the
target nwdel were measured. These values were com-
pared with tht)se obtained when two- and three-dimen-
sional recungular shields were placed upstream from
the target model. Chains in air blast loading on tar-
gets caused by the presence of shields are presented ••
a function of the dimensions of the shields and their dls-
unces upstream from the target model. (Author)
Aberdeen Proving Ground,
Ballistic Research Labs.
Md.
STATIC ACCURACY TESTS OF THE RBL SHAFT
ANGLE DIGITIZER, by Charles W. Lyle. July 60,
13p. Technical note. no. 1313.
Order from LCml$2. 40. ph»3. 30 PB 150 329
Static fleW tests at the BRL Shaft Angle Dlgltlzr were
carried out with the Instrument mounted on tl azimuth
axlsof a tracking telescope (RT-1). A wild T-3
theodolite was used as the standard for calibration.
The S. A. D. was found to be accurate to Its least count
of 00. 001. (Author)
Aberdeen Proving Ground,
Ballistic Research Labs.
Md.
STUDY OF HYPBRVELOCTTY MICRO- PARTICLE
CRATERING, by L. G. Richards and L. S. HoUoway.
>me 60. 28p. 12 refs. Mema rept. no. 1286.
Order from LC ml$2. 70. phK 8p PB 150 959
A ballistic projection technique capable ai accelerating
clusters of 10- to 100-micron particles to velocities ot
12. 0 Km/ sec Is described. The problem of associat-
ing discrete particles from these clusters with the cor-
responding craters resulting from target impact Is coo-
sldered. For cast Iron particles a prevalence of cer-
tain sizes In the fragments recovered is related to a
corresponding size distribution of the craters In a
specific target material A particle mass responsible
for a definite size of crater la thus obtained. The re-
sulting values are correlated with similar data for
larger particles at lower velocities. Scaling laws are
found to bold over a size range of seven orders of mag-
nitude. (Author).
Cryogenic Engineering Lab. . B^der, Colo.
CRYOGENIC MATERIALS DATA HANDBOOK.
Quarterly rept. no. 6 on Contract AF 04(647)59-3.
15 Sep^, 87p.
Order from OHTS $2. 25 PB 161 093-5
See also PB 161 093-4
Diamond Ordnance Fuze Laba. , Washington, D. C.
MEASURING THE ELECTRIC CHARGE ON A
MISSILE IN FUGHT. by Philip Krupen. 1 Aug 60,
15p. 2 refs. TR-856.
Order from LC ml$2. 40, ph$3. 30 PB 149 547
There Is considerable interest in the electric charge
resident on missiles and satellites in flight. An elec-
trosutlc field meter is described for measuring the
charge. It consists of stationary pickups over which
a sectored disk rotates. An alternating voltage la
generated at the pickups aa they are alternately
58
covered and exposed at a uniform rate. The magni-
tude erf the voltage is proportional to the electric
charge. The sensitivity of the meter and the relation-
ship among the various «>lectrostatlc quantities are
developed. When the meter Is mounted on a vehicle,
the charge information can be telemetered to the
ground. Some test results are given. (Author)
Peltman Research Labs. , Plcatinny Arsenal, Dover,
N. J. _
DEVELOPMENT OF A THIRTV -SECOND DELAY
SWITCH, by Martin Gilford and Burton Werbel. Oct 60,
9p. 5 refs. Technical notes no. FRL-TN-12.
Order from LCmi> 1.80, ph$ 1.80 PB 148 662
A prototype item has been developed which makes use
of the Atlas Powder Company delay squib switch mech-
anism and a delay gas-generator assembly. This com-
bination provides a nominal 30- second interval between
squib initiatioa and aaivation of the switch mechanism.
Tlie delay composition used conulned 58% barium
diromate. 32% pousslum perchlorate, and 10% tung-
sten. The switch proper was operated by pressure
developed upon Ignition of a gas -generating composi-
tion (lead nKMKxiitro-resorcinate 95%, potassium chlo-
rate 5%). No relay material was found necessary be-
tween the delay column and the gas -generating compo-
sition. The parts used In the prototype Item were a
modified 4 -second Ml 12 fuze housing with relay cup
and an experimental squib holder. (Author)
Peltman Research Labs. , Plcatinny Arsenal, Dover,
N. J.
DEVELOPMENT OF COATED CLOTH FOR MORTAR
PROPELLANT INCREMENT BAGS, by Sydney Axelrod.
Aug 60. Up. 2 refs. Technical rept. 2703.
Order from LC ml$2. 40, ph$3. 30 PB 148 914
Acrylic cJjjth waa coated with a polyethylene latex con-
taining ammonium perchlorate. The coated cloth could
not be heat sealed. It is believed that the salt pre-
vented the plastic from farming a strong bond. With
kxally available equipment, a satisfactory combustible
coating could not be deposited on mortar increment "
bag cloth. Work was discontinued because of lack of
funds. (Author)
Feknwn Research L«bs. , Plcatinny Arsenal, Dover,
N. J.
ELECTROSTATIC SENSITIVITY OF BARIUM
CHROMATE /BORON COMPOSITICWS, by Anthony F.
Taachler and Edward E. Jones. Oct 60, 9p. Technical
notes no. FRL TN-3.
Order from LCml$l. 80, phjl. 80 PB 149 960
Electrostatic sensitivity tests were conducted on 90/10
aod 95/5 barium chromate/boron mlxturea, both with
and without 1% added VAAR. The following Joule level
results were obtained: 90/10 barium chromate/boron,
0.0023; 90/10/1 barium chromate/boron/VAAR,
0.0315; 95/5 barium chromate/boron, 0.0270; and
95/5/1 barium chromate/boron/VAAR, more than
14. 850. The 95/5/1 mixture did not ignite even at the
highest Joule level obtainable with the equipment used.
(Author) I
Peltman Research Labs. , PIcslteny Arsenal. Dover,
N. J.
EVALUATION OF 1.5 INCH CANADIAN PLASTIC
5IGNAL CARTRIDGE CASE, by Bossle Jackson,
Seymour M. Kaye, and Garry Weingarten. Aug 60, 2lp.
2 refs. Technical notes no. FRL-TN-2.
Order from LC mi$2. 70, phV*. 80 PB 150 825
Static and ballistic perfbrmsnce tests were conducted on
1. 5- inch plastic signal cartridges which had been aub-
jected to a group of conditioning tests. The cartridgea
were supplied by T. W. Hand Fireworks Co. , Ltd,
Ottawa, Canada. The tests included JAN cycling, vibra-
tloe-transportation, rough handling, water Immersion,
and high- and low- temperature conditioning. Test re-
sults Indicated that the plastic signal cartridges had
failed to withstand the JAN cycling, water Immersion, »
and high temperature (1670F) conditioning tests.
(Author)
Peltman Research Labs. , Plcatinny Arsenal, Dover,
N I
INFLUENCE OF WATER ON THERMAL DECOMPO-
SITION OF ALPHA LEAD AZIEK. by Bruno Reitzner.
Sep 60. I7p. 14 refs. Technical rept. FRL-TR-5.
Order from LC ml$2. 40, ph»3. 30 PB 148 916
Thermal decomposition of alpha -Pb(N3)2 at 240°C
under moist nitrogen is charaaerized by pronounced
induction periods. The reduction of the aqueous ten-
sion, either by reaction with Pb(N3)2 or by adsorption
in hygroscopic liquids, accelerates the decomposition,
yielding lead as the final product. The acceleration
BUge can be suppressed by an aqueous tension greater
jhan 8.9 mm Hg; a hydrolysis reaction then predomi-
nates. HN3, which la fOTmed during hydrolysis, is
partially decomposed to give N2 and NH3, which react
with excess HN3 to form NH4N3. An explanation for
dw long induction perioda found with alkali and alka-
line earth azidea la proposed. (Author)
Peltman Research Labs. , Plcatinny Arsenal,
Dover, N. J. _. ■, ,
SILVER ACETYLIDES, by Virginia D. Hogan and Saul
Gordon. Aug 60, 12p. 34 refs. Technical rept. FRL-
Ordo^ from LC ini$2. 40, ph»3. 30 PB 150 970
The history of research on the three compounds that can
be prepared from silver nitrate and acetylene- -Ag2C2.
Ag2C2. AgN03, and Ag2C2.6 AgN03--is traced in de-
tail in this report, on the basis of a comprehensive
literature survey compiled by the authors. Experi-
mental work was also done, In which the three com-
pounds were subjected to differential thcrnaal analyals
both at ambient pressures and at reduced pressures
simulating high altitudes of i^) to 150, 000 feet. The
explosion temperaturea of the feebly eroloslve com-
pounds Ag2C2 and Ag2C2.6 AgN03 (138°C and 300^
respectively) were found to be substantially unaffected
by reduced pressures. However, Ag2C2. AgN03 ""
ploded violently at 245°C under ambient pressure, and
at 195°C at a pressure of one millimecer of noercury.
(Author) -v,
Pekman Research L«>8. , Picatiniiy Arsenal, Dorer,
N J
USE OF RAWOACnVATED METAL DISCS FOR
HYPERVELOCITY TRACER STUDIES, by Samuel Helf,
Eric N. Clark and cxhera. Aug 60, I2p. 4 refs. Tech-
nical rept. FRL-TR-U.
Order from LC mi$2. 40, pi43. 30 FB 148 22S
The use at radHoactivatBd discs at aluminum and steel
to estimate fragment erosion In solid targets for the
determination of hypenrelocltles was found feasible.
Activation was accomplished with a slow-netitron flux
at 6x 10^2 Qvt, in 3 da^s for the aluminum discs used
(4 grams, 1 Inch diamater x 1/8 inch thick), and in 4
houTB for the steel discs (5 grams, 1 inch diameter
X Vl6 Inch thick). Gaitima ray spectrometry indicued
the presence of both Fa^^ (half life 46 days) and Cr^^
(half life 28 days) in ratios otO. 5 for the aluminum
and 1 . 3 for the steel. The radloaaivities in the alumi-
num arose solely from impurities, whereas in the
steel they were contributed by the major component,
iron, and only supplemented by the chromium im-*
purity. The radioactivity was found by successive
acid solution determinations to be distributed evenly
in both metals. Experimental firings erf the tagged
discs with Comp B into polyurethane indicated that the
mass d a fragment can be estimated by measuring the
tocal radioactivity at th* eroded portico oTlt left In the
target material. Aluminum friagments were found to
erode 105^ and steel 2%. A narrow pipe filled with
foamed polyurethane was found to be the best method
erf minimizing th^ dispersion o* radioactivity. The
ablation erf the discs In idr was measured by firing
them through a pipe and catching the eroded radio-
active material on absorbing material lining the pipe.
(Audior)
Illinois U. , Urbana.
HYDR0BALLI5TIC CAliCULATH»<S OF THE RISE
AND WATER EXIT OP BUOYANT BOWES, by
J. M. Robertson. Rept. on Contract Nonr- 1834(10).
Nov 59, 71p. 20 refs. t. fc A. M. rept. no. 153;
AD-230 259.
Order from LC ml$4- 5<^ pfa$ 12. 30 PB ISO 831
Problems associated with the vertical rise and passage
through a water-air interface of small buoyancy-pro-
pelled bodies are considered. In general the methods o*
analysis are approximaie. Calculations are limited to
consideration at prolate ellipsoids and usually to those
<rf fineness ratio equal to 4. The terminal velocity and
length at rise distance required to approach the velocity
closely are calculated. Comparison with experiment
indicates fair agreement. Above a diameter at 2 in. ,
the Proude number no longer increases appreciably
with body size. A rough analysis of the added -mass
variation erf ellipsoidal bexlies ^a they pass through the
the free surface is developed. This estimate is used to
indicate the expected velocity and acceleration chaises
d exiting bodies, and ia shown to divetge somewhat
from those found experimentally. Besides the effect of
added-mass variaticm, buoyancy and drag changes as
the body exits are also shown to have an important ef -
fea on the velocity-distance and ftfceleration-dlswnce
profiles. Threffect of antrainod Mter is considered.
Calculations at the dlspJ|M»meijt volume of the boundary
layer on the body are shown to be tn fair agreement
with the measured entrained-wfcer volumes. (Author)
i I fl
Illinois U., Urbana.
TRANSITION STIMULATION FOR TERMINAL VE-
LOCITY REDUCTION IN WATER -EXIT STUDIES, by
J. M. Robertson. J. C P. Chow, and M. E. Clark.
Rept. on Contract Ncnr- 1834(10). Nov 59, 31p. 12 refs.
T. k A. M. rept. no. 152; AD-230 258.
Order from LC ml$3. Oa ph$6. 30 PB ISO 830
A technique for reducing the terminal velocities erf small
buoyant bodies rising threxigh water is described and its
exper^nental verification indicated. Sand-grain patches
to indKe premature transition erf the flow in the bound-
ary layer from laminar to turbulent were used in the
(length) Reynolds -number range at 105 to 106. A method
at designing the sand patches In terms of known infor-
mation em transitiexi, roughness effects, and laminar
boundary-layer growth is deuiled. Experlmenul evi-
dence of the achievement of transition stimulation in an
air tunnel, via hot-wire anemometer boundary-layer
studies and drag tests, Is presented. Finally, it is
shown that an appreciable reduction in terminal velcx:ity
was obtained in the actual water -exit tests. (Author)
Institute of Metals and Explosives Research, U. of
Utah, Salt Lake City.
FUNDAMENTAL INVESTIGATIONS OF HIOI EXPLO-
SIVES AND HIGH EXPLOSIVES PHENOMENA, by
T. K. Collins. Final rq)t. on Contract N7onr-451(07).
30 Sq) 59, 32p. 99 refs.
Order from LC ml$3. QO. ph|6. 30 PB 150 747
General subheadings erf subject matter covered by the
investigations are (1) chemical reaction rates in deto-
nation, (2) thermo- chemistry of high ejq)losive8, (3)
curvature of the detonation wave front, (4) instrumen-
tation for high explosives testing, (5) wave shaping tech-
niques and applications, (6) eepiations of state in deto-
nation, (7) meulized explosives systems, (8) explo-
sives with inert additives, (9) Isexhermal decomposi-
tion of explosives, (10) adiabatic deconqwsition of ex-
plosives, (11) theory of detonation, (12) shaped charged
studies, (13) time lag for inltiatiem erf detewiatlon
through air, glass, and steel, (14) detonation velocity
transients, (15) interaction of detexiation waves with
metal burdens, and (16) X-ray technique for measuring
density vs distance relationships in detemating
explosives.
Lincoln Lab. . Mass. Inst, of Tech. , Lexington.
ON THE LINEAR SMOOTHING OF REDUNDANT
RADAR DATA FROM SATELLTTES. by Fred G
Schweppe. Rept. on Contract AF 19(604)5200.
25 Aug 60, 58p. 22 G-0021.
Order from LC mi$3. 60, ph$9. 30 PB ISO 799
Linear smoothing prexredures for prcxressing redundant
satellite raelar returns with a digital cejmputer are dis-
cussed. Procedures based on polynexnial approxima-
tions to the orUt In the presence of noise are analyzed
and the optimum degree of polynomial Is considered.
Ccjmputer Implementatiem procedures for the actual
smexrfhing are outlined. A few Impllcatiexis of the
change in the noise character which results from a
transformaticn from radar cxiordinates to cartesian co-
ordinates are discussed. Advanced linear filters whidi
do not use a polynomial approfxlmation are presented in
general terras, and an upper bound on their capabllitief
is given. (Author)
h
fockheed Aircraft Corp. , Sunnyvale. Calif.
TRAJECTORY OP A VEHICLE DEPARTING PROM A
ORCULAR ORBIT, by Ralph B. Bower sox and David
Csrter July 60, 41p. 10 refs. LMSD-703049.
Orter from LC mi$3. 30, ph$7. 80 PB 150 886
jiiumerlcsl solutions for the two-body et^tions of mo-
tiao have been obtained by means of s digkal computer
for the case of a rocket departing from an initial clrcu-
Isr orbit with constant thrust and flow rate. Thirty so-
ludoas have been obtained in a wide range of thrust
m^tudes, specific impulses, and thrust directions.
One solution was obuined for an initial elliptical orbit
and another for a small negative thrust as n\lght be used
la • landii^ maneuver. The elata have been compared
widi solutions for other thrust programs. An appraxi-
mstlon has been derived to describe the trajectories in
terms of the variations in the orblul paranteters. At
either high or low specific thrust values, s circum-
ferential thrust gives as high a mass ratio at escape
(nifAno) •■ **** ■ tangential thrust progrsm. At inter-
mediate specific thrust values, the tangential thrust is
more effective. For sll the positive low thrust ex-
tmples, the eccentricity of the osenilating ellipse tends
to remain near zero (and actually decreases to zero
fran the initial elliptical orbit) until the vehicle is near
escape. Thus, the circular orbit appears to possess a
special stability when it is being expanded, but the op- |
posite is true for negative thrust, in which case the
trajectory becomes very eccentric. (Author)
McCrone, Walter C., Associates, Chicago, 111.
THE CRYSTALLOGRAPHY OF EXPLOSIVES. PHASE
I. CRYSTAL STRAIN IN LEAD AZIDE. PHASE II.
CRYSTAL STRUCTURE OP EXPLOSIVES, by
W. C. McCrone, John A. Reffner and L. V. Azaroff.
Quarterly rept. no. 1, 12 May- 31 July 60, on Contract
QA 11-022-ORD-3412. 12Ai«60, 21p.
Order from LC miJ2. 70, ph$4. 80 PB 152 062
i ' I -
A method for the continuous Isothermal crystallization
cf well formed clear crystals erf alpha lead azide is
described. Crystals grown wiith this apparatus are to
be used as seed crystals in a series of experiments
designed to test the hypothesis that strain in beu lead
•zide can cause spexitaneous dete>natie>n. The expert- ;
mental arrangement for carrying exit these experi- 1
meiKS has been constructed and preliminary expert* |
mems have begun. The crystal structure of normal
lead azide will have to be tackled in an indirect manner
because the scattering by tha lead atexns completely >
blankets the cexitribution erf the individual carbem, I
hydrogen, oxygen and nitrogen atexns. Thus far no
other styphnate isostruaural with lead styphnate has
been found. However, two i^pstructural styphnates, |
those of potassium and of anunexiium, have been pre'
pared in suitable crystals and structures erf these two
crystals Is well under way. (Author)
Melpar, Inc. , Watertown, Mass.
RECOGNmON OF (5BJECTS IN SPACE PRCM DY-
NAMIC TRAJECTORY DATA, by Arthur L. Levin*. I
Scientific rept. no. I on Contract AF 19(604)5996. j
A»«60. 134p. .1 ref. AFCRL-TN-60-966. !
XMtT from LC ml|6. 90, ph$2I. 30 PB 150 989
tacluded are the equations of motion of a space object
moving in a central force field as observed from a point
on a routing spherical earth, equations necessary to
calculate a set of orbital parameters for two different
minimum sufficient sets of observed data, equations
describing the sensitivity of orbital parameters to var-
iations in observed data, and equations describing the
variations in orbital parameters due to variations in
the force field on the body. (Aitthor)
Naval Ordnance Lab., Corona. Calif.
FUSED SALT VOLTAIC CELLS. AN ANNOTATED
BBUOGRAPHY OP THE TECHNICAL LITERATURE
CONCERNING CELL POTTENnALS, comp;. by
W. C. Spindler and R. E. Panzer. 31 July 59, 4lp.
85 refs. NOLC rept. 457; NAVORD rept. 5957;
AD- 225 203.
Order from OTS $1.25 PB 171 114
An annotated bibliography Is presented of 85 articles
pertaining to electrochemical cells utilizing fused salt
electrolytes, with particular application to energy -
producing voltaic cells. The literature cited Includes
material or electroele potentials and electrode reac-
tions in both voltaic and electrolytic cells; it does nerf
include references to the physical and chemical prop-
erties of fused saks. (Author)
Naval Ordnance Test Station, China Lake, Calif.
MICROSCOPICAL INVESTIGATION OF PLASTISOL
NITROCELLULOSE, by John W. French. 5 Apr 60.
19p. NOTS TP 2497; NAVWEPS rept. 7086.
Order from LC ml$2, 40, ph$3. 30 PB 150 456
A description of plastisol nitrocellulose (PNC) is
given for both the macroscopic and microse»pic appear^
ances and is supplemented by several optical- andelec-
tror-micro8ct)pe photomicrographs. Also, a brief
descrption is given of the materials and techniques used t
in this investigation. The average particle size cf dif-
ferent PNC lots is determined by various means, and
the results are tabulated and discussed. The methods
and results obuined on curing the solution of PNC in
pentaerythritol trinitrate (petrln^a plastlcizer, at ele-
vated temperatures are described and illustrated with
suitable charts and photon-, icrographs . (Author)
Naval Weapons Lab. , Dahlgren, Va.
TERRIER BOOSTER WATER QUENCH VALVE FOR
STOWAGE SAFETY, by H. V. Yams. 15 S^ 60. 20p.
6 refs. NWLrept. no. 1722.
Order from LC ml$2. 40. phJ3. 30 PB 150 626
The booster quench valve, developed by the Naval
Weapons LaborattJry for Terrier ready- service maga-
zines, is an automatic, mechanically emerated valve
which allows water to be Injected into An accidenully
ignited b<x)8ter at the beginning of burning. The design
makes use of experience gained in developing a similai
valve ftjr the Tartar systems. The design also con-
siders the initial burning characteristics of the
Terrier booster, and the original contraa specifica-
tions for Terrier quench valves. The valve consists of
25 separate parts including seals, screws and mount.
An analysis of the Terrier valve design indicates that
It is several times more sensitive than the Tartar
valve, and that it functions extremely rapidly in the
exhaust envlrooft^nt of a Terrier booster. Analysis
61
•Jao Indicates that the Terrier valve will meet the
spedfldktion and envlronmenul requirements.
(Author ]r i
f-JLkL
Piris U. (France).
DOPPLER MEASUREMENTS ON ARTIFICIAL SATEL-
LITES, by Etiennt J. Vassy. Technical note for
1 Apr 59-31 Mar 60 on Contract AF 61(052)155. (i960]
32p. 30 refs. ERI>-TN-60-773.
Order from LC irl$3. 00, ph$6. 30 PB 150 647
A device for meaajuring the Doppler shift at the artifldaJ
satellites has bees realized. For this purpose, the
time pips and the signals of the satellite, wtwse fre-
quency varies as *ie Doppler effect, are, both, recorded
on a double track magnetic tape. This frequency is then
measured by comparing it with an independent LF oscil-
lator by means at Llssajous ellipses. The position of
the inflection point of the curve and the gradient of the
tangent at this poi^t are determined by a grapho-analyti-
cal method. (Autb6r)
tb6i
Temple U. , Philadelphia, Fk.
mCH VELOCITY IMPACT STUDIES DIRECTED TO-
WARDS THE DETERMINATION OF THE SPATIAL
reNSTTT. MASS AND VELOCITY OF MICRCHclETE-
ORITES AT HIGH ALTTTUDES, by J. Uoyd Bohn and
Otto P. Fuchs. Scientific rept. #1 on Contract
AF 19(604)18^. 31 Jan 58, 53p. 8 refs. AFCRC-
TN-58-243; AD-112 478.
Order from LC m|$3. 60. phl|9. 30 PB 150 925
Since no measuring instruments are available whose
Indications represent a known function of the mass (m)
and the velocity (v) pertaining to impacts, the paper
discusses the particular problem d the development of
analytical expressions describing the Impaa
'processes.
Watertown Arsen$l Labs. , Mass.
METALLURGICAL OBSERVATIONS OF HIGH VELOC
ITY IMPACT, by Id. H. AbfaoR. Sep 60. 23p. 8 refs.
■I\K:hnical rept. noi WAL TR 161. 85/1.
Order from OTS If . 75 PB 161 800
I
Annealed 1020 steel, hardened FXS-318 steel, and
2024- T4 aluminum lalloy pellets with length -to-dlameter
ratios at 1. 25 were fired at standard steel armor,
aluminum armor, «nd 301 stainless steel plates at
velocities from 2. 000 to 13, 000 fps. Plate sections con-
taining crater half-]secticnt were subjected to hard-
ness, macrostructure and microstructure measure-
ments to determine metallurgical phenomena which in-
fluence crater formation. Dynamic insubilities re-
sultfaig in slip with ^e formation erf transformed un-
tempered nnartensi|e on maximum shear planet were
observed in the standard steel armor. The number of
these shear bands with associated cracking increased
with increasing pellet velocity. Slip without transfor-
mation was observed in both the aluminum alloy and
sulnless steel platfs. No local transformation from
austenite to martenlite was observed in the stainless
steel. Extensive hardening in the vicinity of the crater
was measured in all plate materials. (Author)
62
Ship Building
David Taylor Model Basin. Washington. D. C.
DYNAMIC LOADING OF A MOTOR TORPEDO BOAT
(YP 110) DURING HICW-SPEEt) OPERATION IN
ROUGH WATER, by Norman H. Jasper. Sep 49. 3tf.
10 refs. Rept. C-175.
Order from LC mi$3. 00, ph$6. 30 PB 152 797
This report released for sale to the public 18 Nov (0.
Pressures and strains were measured on the hull of t
motor torpedo boat (YPUO, Ex PT8) during rough-
water operation in order to establish design criteria
for hull plating and local structure. The most severe
loading due to wave farces occurred between the for-
ward quarterpoint and the midship section. The high-
est maximum effective pressure for this boat was 36
psi. In order to determine the effective pressures tla
solution is given for the damped response at a singk-
degree-oT-freedom systehi to a modified blast pulse.
Failure of portions at the hull structure during these
tests indicated that previous design specifications
were inadequate. In this report are proposed criteria
for designing structures of sufficient local and over-
all strength to withstand severe dynamic loading of thi
tjrpe encountered in rough water. Recommendations
for further research are made. (Author)
David Taylor Model Basin, Washington, D C.
A PROCEDURE FOR COMPUTING STRESSES IN A
CONICAL SHELL NEAR RING STIFFENERS OR
REINFORCED INTERSECTICWS, by Richard V. Raea
and John G. Puloe. Apr 58. 36p. 8 refs. Rept. 1015.
Order from LC mi$3. 00. pfa$6. 30 PB 152 807
This report released for sale to the public 18 Nov 60.
A second approximation to the complete theory for the
axisymmetrlc deformations of thin elastic conical
shells, as derived by E. Meissner and F. Dubois, is
presented. This simplification at the exaa differen-
tial equation leads to a so-called Geckeler-type ap-
proximation for conical shells. From this approxinu-
tlon, a step-by- step numerical procedure is developed
for calculating stresses and strains throughout the
conical elements of shell structures. The methods
include computation of the edge shearing forces and
bending monnents which arise from discontinuity
effects at cone -cone and cone -cylinder Junctures,
either with or without transverse reinforcing rings.
The range of applicability of the approximation Is
also discussed. (Author)
David Taylor Model Basin. Washington, D. C.
A SURFACE- ROUGHNESS PROFILOMETER, by
F. B. Miller. Sep 60. 9p, Repc no. 1347.
Order from LC mi$l. 80. ph$l. 80 PB 150 459
This report. describes a surface- roughness prof ilometa
device capable of recording the outline of a section of •
surface (rf structures such as ships' hulls. The full-
scale range of the system is ±f). 015 inch around a
chosen zero level. The recording is made on magnetic
tape, and upon playback, is available in electrical ana-
log form; thus conventional wave analyzers may be used
for analysis. The recording system is designed around
a vehicular -type tape recorder, and is small and com-
pact for field use. (Author)
FCX)D, HANDLING, AND PACKAGIhkS
EQUIPMENT j
i I
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
ARCTIC SURVIVAL RATIONS V. EFFECT OF PRO-
LONGED CONSUMPTION OF PEMMICAN SURVIVAL
RATION ON SOME ASPECTS OF THE INTERMEDI-
ARY METABOLISM OF RAT LIVER TISSUE, by
John P. Hannon and David A Vaughan. ^y 60, 26p.
22 refs. Technical fept. 57-55.
Order from LC mi$2. 70, ph$4. 80 PB 150 571
The effect of prolonged feeding (3 to 5 months) of pem-
mlcan meat bar on some aspects of the in vitro metab-
olism of liver tissue was investigated. The endoge-
nous metabolism of liver slices and homogenates was
significantly increased by pemmican. This increase
was very probably due to an Increase in the amount of
easily metabollzable substrate within the tissue of
these animals. Utilizing mitochondrial preparations, it
was found in the absence of added cytochrome- c and
diphosphopyrldine nucleotide that with all substrates
studied except gjlutamate, X'-ketoglutarate, and suc-
cinate, the respiratory rate was not affected by the
previous diet. The three subsfates mentioned were
oxidized at significantly lower r:ites in the pemmican
group. Upon the addition of cytochrome -c and diphos-
phopyrldine nucleotide, the q02 of glutanute, «<•-
ketoglutarate, and succinate was returned to the nor-
mal value. It was concluded on the basis of the {res-
ent measurements that prolonged feeding of a hlgh-
fat protein diet such as that found in the pemmican
meat bar results In no obvious deleterious effects In-
sofar as the Intermediary metabolism of rat liver
tissue is concerned. (Author) (See also PB 144 850)
MACHINERY. FABRICATION, AND
ACCESSORY EQUIPMENT j
Brown U. Dlv. of Engineering, Providence. R. L
A TENSION- TORSION MACHINE FOR BI- AXIAL
CREEP TESTING, by A. Shelton. Technical rept. na 1
on Contract Nonr-562(20). Nov 59, 14p. 1 ref. AD- 229 94
Order from LC ml$2. 40, ph$3. 30 PB 150 868
A tension- torsion machine is described which was de-
signed for both short- and long-term creep tests at rooir
and at elevated temperatures. The nnachlne. constructeci
almost entirely of Al, is essentially a constant- load de-
vice which relies on the application of dead weights at
die ends of levers to Induce a tensile load and/ or torque
on the test specimen: The loads and torques are deter-
mined from resistance strain-gages applied tocallbrated
bars. The maximum capacity of the machine is 6 tons
tension and 2 ton- in. torque. A sin:^)le muffle furnace
was designed for tests at elevated temperaturea.
Sundstrand Turbo Div. . Sundstrand Corp. [Pacolma.
Calif.]
STUDY OF TURBINE AND TURBOPUMP IKSIGN PA-
RAMETERa VOLUME IV. LOW SPECIFIC SPEED
TURBOPUMP STUDY, by Kenneth E. Nichols, Donald
G. Mcpherson, and O. Eric Balje. Final rept. for
6 Oct 58-31 Oct 59 on Contract Nonr- 2292(00). Nov 59,
241p. 27 refs. S/TD-1735; AD- 232 638.
Order fronr LC miJlL lb. ph$37. 80 PB 150 834
An investigation of maximum efficiencies of low specific
speed turbopumps obtainable with the present state of
the art is covered. Optimum suction specific speed and
optimum efficiency are analyzed and a theoretical
method of determining the deulled design criteria for
each optimum design performed. Experimental evidence
was accumulated to substantiate the analysis and the
final design parameters are presented as functions of
pump specific speed and specific diameter. (Author).
Engines and Propulsion Systems
Aerojet -General Corp. , Azusa, Calif.
UTILIZATION OF UPPER -ATMOSPHERE ATOMIC-
OXYGEN RECCAIBINATION FOR PROPULSION, by
A, Zukerman and C. B. Kretschmer. Rept. oo (Con-
tract AF 49(638)111. 10 Apr 59, 91p. 15 refa.
Aerojet-General TN-28; AF06R TN-59-517;
AD- 216 292. ,.,«cc
Order from LCml$5. 40. ph$l5. 30 PB 152 055
The report presents a preliminary Investlgatlan of
several methods for the utilization of the upper -atmos-
phere atomic-oxygen recombination energy for propul-
sion purpoaes. The following systems were studied:
(1) the fueUess ramjet. (2) a ramjet with fuel addition,
and (3) a catalytic ram rocket (a power plant of the
ramjet type in which the chemical reaction takes place
primarily on the catalytic surfaces of the reaction
chamber). The fuelless ramjet cycl was previously
Investigated using ideal conditions. In this investiga-
tion, losses were taken into account and the latest
available values for the reaction-rate constant were
used. This investigation shows that the fuelless ram-
Jet cannot provide enough thrust to sustain a satellite
In the atomic-oxygen layer. The Investigation of the
ramjet with mass addition shows that with fuels simi-
lar to NO2 ( in molecular weight and heat release)
enough thrust can be derived to overcome the external
drag, but not the total drag. Certain configurations of
the catalytic ram rocket show promise for sustaining
a satellite for a considerable length of time at a high
expense of coolant fluid. (Author)
Avco- Everett Research Lab. , Mass.
ANALYSIS OF CONSTANT VELOCITY PULSED
PLASMA ACCELERATOR, by 7L J. J. Stekly. Repi. on
Contract AF 49(638)659. July 60, 21p. 5 refs. Re-
search rept. no. 89. AFOSR-TN-60-935.
Order from LC nU$2. 70, phK 80 PB 150 %4
The equations are set down In a dlmenslonlei^s form
for a constant velocity pulsed plasma accelerator,
treating the accelerator as a circuit element. The
equations are solved in closed form and plots of volt-
age, current, gas energy and required mass distribu-
tion are obtained. It is shown that circuit inductance
both reduces and delays the energy transfer from the
c^>ac{tors to the gas. A typical dealgn for a constant
velocity pulsed plasma accelerator is obuined making
use of the dlmenslonless plots obuined as a result of
the analysis. (Author).
63
Avco-Everen Resetarch Lab. , Mas*.
MAGNETOHYDRODYNAMIC PROPULSION, by
G. Sargent janes. Rept. on Cooiraa AF 49(638)659.
Aug 60, 71p. 9ref8. Research rept. no. 90; AFOSR
TN 60-955: AD- 243 ll7.
Order from LCml$4. 50, pij$12. 30 PB 150 777
The morphology of plasnM propulsion devices ^s pre-
sented following a bnef diacussloo d the requirements
for mission objectives. The two criteria employed for
this classification are field-current configurations and
comainmem. Cootalement is essential for efficiency
and probably represents the primary area requiring
further research. Both aerodynamic and magnetic con-
tainment are considered. The various categories of
electrical motors art completely analogous to the
categories at field- current configurations. Three
specific examples of devices being studied at AERL
are presented together with a qualiutive discussion of
the basic physical principles necessary for their
understanding. (Aut^v)
I
Bell Aerosystema C0. , Buffalo, N. Y.
OBSERVATION OF PtOPELLANTS INJECTED INTO A
FIRING ROCKET CHAMBER, by Theodor G. Rossmann.
Rept. or Contract AF 49(638)260. 1 July 60,58p. ISrefs.
Rept. no. 8007-981-0ll; AFOSR -TR- 60- 98;
AD- 243 514. '
Order from LC ml$3. 60, ph$9. 30 PB 152 039
Various liquids were Injected Into a firing windowed
rocket chamber to ch^k and, if necessary, to supple-
ment existing theories dealing^ with evaporation rates of
droplets, as to their applicability to conditions exlsrtng
in rocket combustion chambers. The resulting droplet*
were photographed by means of an experimental tech-
nique especially developed for this purpose, which pro-
vides a succession of magnified shadow pictures of the
liquid core of. the droplets traveling In the combustion
gjases. The ptlesent rqwrt describes experiments with
liquids heated Before injection in an attempt to obtain
measurable evaporation rates of droplets larger than
100 microns. The windowed motor technique has been
utilized for investigations concerning the effect exercised
on the Injection pattern by disturbances introduced into
the feed system, such pis transient or periodical pres-
sure pulses.
I
Steves Inst. oTTech., Hoboken,
Davidson Lab.
SURVEY OF CYCLpIDAL PROPULSION, by
Cajarles J. Henry. Rept. on Contract Nonr- 263(27).
Dec 59, 30p. 13 refs. Rept. no. 728; AD- 230 866.
Order from LC inl$2.T0, pfa$4.80 PB 152 130
A brief hiacory is pre«eiited at cyclcidal propulsion and
a description d the kltematics of the flow through a
cycloldal propeller. The various types d cycloidal
propellers are discusaed and a description d several
Inatallationa is presented. A survey la presented d
the literature pertainiag to theoretical design proce-
dures used for cycloidal propellers. A comparison d
cycloidal and screw propulsion shows that cycloidal
{s-opeller efficiency is in the range 0.45 to 0.58 as
compared to 0. 66 to 0.76 for screw propellers. Some
advantages d cycloidal propulsion are discussed. In
order to insure optimum efficiency in designs of the
fiKure, it is recommended that research be carried
CKt to find the influence d: ICramer's effect, a lifting
surface passing through a vortex sheet, wake contrac-
tion, blade motion, wake adaption and blade
proportions. (Author)
> -■ , 1.
Jsmes Forrestal Research Center, Princeton, N. J.
BIBLIOGRAPHY OF UNCLASSIFIED SQUID PUBLICA-
TIONS, Supplement B, 1 July 57- 1 June 59, to Ten Yeari
of Project SQUID -- a Bibliography, Contract Nonr-
1858(25). Dec 59, 2lp. 68 refs. Proj. Squid Technical
rept. no. PR-67-P-B, Svppl. to Technical rqx. nos.
PR-67-P and PR-67-P-A; AD- 236 164.
Order from LC mi$2. 70, ph$4. 80 PB 152 153
Contents:
Properties of materials (Transpon, Structural)
Gases, liquids, and solids
Physical processes
Heat transfer | . '•
Mass transfer ancf mixing
Fluid flow
Mathematical physics
Chemical processes
Reaction kinetics
Thermodynamics and thermochemistry ' . '
Combustion phenomena
Ignition r
Flame propagation rate -
Laminar
Turbulent
Flame structure and stability
Flame spectrs and radiation
Miscellaneous
Engines and propulsive systems
Instrumentation
Temperature measurement .,
Pressure measurement j
Miscellaneous ! * - > .
(See also PB 136 669)
Junes Forrestal Research Center. Princeton, N. J
PROJECT SQUID Semi-annual progress rept. for
1 Apr- 30 Sep 59 on Contract Nonr -1858(25). 1 Oa 59,
105p. 50 refi. AD- 228 128.
Order from LC ml$S. 70, ph$16. 80 • PB 152 155
Contents:
Fluid mechanics
Fundamemal Investigation d nonsteady flow
Investigation of turbulence
Structure of a detonation wave '
Investigations in magnetohydrodynamlci
Transpon and transfer processes
Thermal conductivity and the viscosity of ammonia
and hydrazine
Thermal conductivity of gases and liquids over a
range of temperatures and pressures
Statistical properties of two-phase flow
Chemical kinetics
Elementary reactions in combustion
High temperature reactions
&irface- catalyzed atom and free radical reactions
Investigatloa of rftaaion kinetics in high -temperature
gases
Combustion phenomena
ftructure and burning mechanism of laininT flames
Research on high pressure comhustiaa
64
feivestlgatlon of gaseous combustion and transport
properties of gases at high temperature
knlzation in flames
Ionization In detonation waves
•Rxal radiation from burning solid propellant strand
Rapid response temperatiu-e probe
Rasmsflow in nozzles
(See also PB 145 886) •
Lockheed Aircraft Co. , Sunnyvale, C^alif .
GENERAL RESEARCH IN MATERIALS AND PRO-
PULSION, JANUARY 1959-jANUARY I960. VOLUME
I PROPULSION CHEMISTRY AND PROPULSICW
PHYSICS. Jan 60, 193p. 114 refs. LMSD- 228140.
Order from LC mii8. 70, ph$30. 30 PB 150 613-1
Contents:
pirt 1 ■ Propulsion Physics
IVrmionic theory and technique (LMSD- 31 1695)
Ionic propulsion - an assessment (LMSD-48456)
A nuclear -ionic system for space flight
Optimum proportioning of two propellants to obtain
maximum burnt velocity (Pub. in ARS Jnl. Aug 59)
A thermal -electronic convenor (LMSC-5106)
MeulUc carbides as emitter materials in thermsl-
electronic convenors i
Part 2. Propulsion chemistry
Aosphorus- fluorine oxidizers (LMSD- 49771)
liveatigatlon of nitro compounds as oxidants for hlg^-
easrgy chemical systems. I. Lithium dfnitroethane
(LMSD-48407). II. Methylenedinitr amine
(LMSD-4840e)
Lockheed Aircraft Corp. , Sunnyvale, Calif.
GENERAL RESEARCH IN MATERIALS AND PRO-
PULSION. JANUARY 1959-JANUARY 1960. VOLUME
n. METALLURGY AND CHEMISTRY. Jan 60, 275p.
63 refs. LMSD-288140
Order from LC mill 1.10^ ph$42. 60 PB 150 613-2
Contents:
Electronic structure of beryllium (LMSD- 288003)
Blearlcal resistivity of beryllium
Plastic deformation in befyllium '
Beryllium analyzed for trace impurities by gamma-ray
activation
High- temperature corrosion of beryllium in air
Stress corrosion cracking of beryllium (LMSD-49735)
Grain reflnenient in beryllium by alloying
Specific heats of beryllium and an alloy at room and
elevated temperatures (LMSD- 2702)
Studies of the gas carburizatlon of niobium
8tiidy of hallde- containing oxide films on columblum
(SeealaoPB 150 613-1)
Naval Weapons Lab. , Dahlgren, Va.
DYNAMIC TESTING OF THE 0. 7-ES-6400 (MK 29
MODO) RCXZKET MOTOR, by D. W. Culbertson. »
30 Aug 60, 22p. 2 refs. NWL Rept. 1715. \
Order from LC ml$2. 70, phH 80 PB 150 972
Results bf eight track tests conducted to determine the
dynamic performance of the 0. 7-ES-6400 (Mk29Mod0)
Rocket Motor under service conditions of acceleration
and temperature are presented. As s result of these
teau It is concluded that the 0. 7-ES-6400 (hfc29 ModO)
Rocket Motor will perform sstlsfactorlly under serv-
ice conditions of 15-18 ff's acceleration at tempera-
tures of -65^ to ♦145°F. The nnotor is considered
capable of withstanding the transverse and lateral vi-
bration loadings Imposed during track firings. Bssic
motor properties of shon burning time, medium thrust
level, and a high ratio of propellant weight to total
weight are desirable features of s propulsion system
for use on shon, medium speed tracks such as the
NAVWPNLAB 520 ft. facility. (Author).
Physical Research Lab. , Space Tech. Labs. , Inc. ,
Los Angeles, Calif.
THE MAGNETIC INDUCTION PLASMA ENGINE, by
Milton U. Clauser. 19 Aug 60, 40p. 14 refs. STL/TR-
60-0000-00263.
Order from LC ml$3. 00. phJ6. 30 PB 150 882
A comparison of conventional electric motors and plasms
propulsion engines shows that the categories of series,
shunt, and induction nuxors are also of value when ap-
plied to the plasnna engines. The only engine which al-
lows the plasma to magnetically insulated from the walls,
and thereby eliminates the unacceptably large heat
transfer to the walls, is the magnetic Induction plasma
engine. In comparing the ion engine and the plasma en-
gine, it is seen that the ion engine is seemingly simple
in concept but is proving to be, complex in its design;
the plasma engine, on the other hand, is complex in
theory, yet like the induction motor it holds the hope of
being simple in design and operation. It further appears
that while the ion engine may have difficulty in achieving
1 pound of thrust, this tends to be the lower limit for
the plasma engine, which can be easily extended to
larger thrusts. The use of different prc^jellants in tlie
MIP engine makes it possible to efficiently achieve dif-
ferent values of specific impulse. Deuterium Is appro*
prlate above 5000 seconds and will be used on those en-
gines which are con:q)etItive with the ion engines. Lith-
ium is appropriate In the 2500- 3500 second range which
is two low to be achieved by the ion engine and too high
to be achieved by the arc jet- Design parameters are
given for a deuterium engine and a lithium engine, llie
calculated weights and efficiencies are encouraging.
(Author).
Rocketdyne [Canoga Park, Calif. ]
EXPERIMENTAL ELECTRICAL PROPULSION, by
C. R. Dulgeroff and G. D. Seele. Final rept. for
1 May 58-31 May 60 on Contraa AF 49(638)351.
July 60, 74p. 12 refs. R-2565; AFOSR-TR-60-112.
Order£romLCmi$4.50, ph$l2.30 PB 150 861
The investigation of ion thrust cbaniber geometry,
using both an accelerate-decelerate electrode geometry
and a modified Pierce two-electrode geometry design,
showed the latter design to be superior inasmuch as it
showed improved focusing propenies, i.e., s decrease
of beam interception by the acceleration electrode. The
perveance of the latter system was experimenwlly de-
termined to be 3. 45 X lO"' amp/volt3/2. Current
densities for plane ionizer surfaces up to about
12 ma/cm2 for either tungsten, tsnatlum, or titanium
carbide ionizers were measured by*using a calorimet-
ric collector . Thrust mea*uren»ents of 40 to 50 micro-
pounds were made by a pendulum -type collector. Other
perfornMnce tests showed a sputtering rate of about
65
22 gm/amp hr for 9*kev cealum Idhs on nickel and an
ionization efficiency c€ greater than 90 percent over a
30- hr period. Tungaten, molybdenom, nickel, and
321 atalnlesa eteel are generally compatible with
cealum at 700 C but at 1000 C, Intergranular attack oT
nickel and moderate to aevere pitting at stainleaa ateel
by cealum occura over reaction periods of 100 hr
(Author)
Sundstrand Turbo IJiv. , SuodKrand Corp. fPacolma
Calif. ] r I .
ANALYSIS AND MEASUREMENT OT CHEMICAL CON-
VERSION TIME IN A LIQUID FUEL ROCKET EN-
GINE WITH DISTRIBUTED COMBUSTION, by
L. L. Bixson. Technical note no. 8 on Contract
AP 18(603)107 26 July 60. 23p. 2 refa. S/TD na 1855-
APOSR-TN-60-886; AD-243 095.
Order from LC m42, 7a ph$4- 80 PB 150 835
A major goal o^ the rocket scaling program is to de-
velop a valid method of measuring chemical conversion
time (Tau). The need for such fundamental measure-
ments is supported by the concept of chemi -acoustic
coupling and ita imponance to high frequency combus-
tion instabUity. Concise analytical models were pre-
viously developed which describe the combusUon clim-
ber pressure decay curves for boch the cases of coocen-
trated and distributed combustion. The models were
based on the aasumption of instantaneous propellant
shut -off during steady- sute combustion. In this note
die previous analysis is extended for the case of dis-
tributed combustion to permit direct, reasonably accu
rate compuutioo of Ttu from experlmentaUy obtained
pressure decay hiatorlea. Data are presented which
strongly support use of the distributed ccmbusticJn
model for the LOX. Rp-l propellant system which la
presently under investSgatloo. (Author)
&mdstrand TUrbo Dli. , Sundstrand Machine Tool Co.
[Pacoima, Calif. ]
THE EXPERIMENTAL DETERMINATION OF CHEMI-
CAL CONVERSION TIMES IN LIQUID FUEL ROCKET
ENGINES, by J. W. Bjerklle. Technical note no. 5 on
Contract AP 18(603)107. 15 Mar 58, 22p. 2 rrft.
S/TDna 1232; APOSR TN-58-415; AD- 158 218.
Order from LC ml|2. TO, ph$4. 80 PB 148 264
The experimental determination of effective tlmedelays
in rocket eaglnea accogdlng to Barrere: Two alternate
methods erf interpretation are described mathematically
baaed on the assumptions of concentrated and dis-
tributed combustion. Analysis of pressure deca^ at the
time erf propellant shut9ff *"<^ *" relation to chemical '
convCTsion tlme.-r. in rocket thrust ch^rr^y^■ -n,e
case Of distributed combustion is analyzed by startli^
with a law of burning s[»ray8 which has been shown to
be in good agreement with experiments. The results
for both analyses of distributed combustion are shown
to be identlcaL j
Technlache Hochachule, Wien (Austria)
CONDUCT THEORETICAL AND EXPERIMENTAL IN-
VESTIGATIONS OF THE MD(ING OF COOLING AIR
WITH COMBUSTION PRODUCTS IN A COMBUSTION
CHAMBER, by Herbert Melan. Technical (final) rept.
on Research on Combustion Chambers. Contract AF
61(052)93. 31 Oct 59, 36p. AFOSR-TR-59-197
Order from LC ml>3. 00^ pfa^. 30 PB 150 332
The purpose Was to test a new type of a combuatlon
chamber for gaaturblnea without a special flametube but
having a awlrl (vortex-) chamber at the Inlet and at the
exhaust of the combustion chamber. The tests with hot
gases with the tests of cold and warm air show that
with the new form of the combuatlon chamber a good
bit of die hypodieaes are fulfilled. It Is posslbls tobulld
a chamber without a flametube and by application of two
specially formed swirl chambers at the Inlet and at the
«th«u« , die wall temperatures can be diminished. At
die exhaust it is possible to get a more or leaa aimllar
dlatiibutlon of the outlet lenveraturea. The efficiency
ia not satisfying.
Manufacturing Equipment and Processes
Brush Beryllium Co. , Cleveland. Ohio.
FABRICATION OF BERYLLIUM WIRE, by A. G.
Groea, Jr. , R. G. O'Rourke and W. "W. Beaver. Prog-
ress rept. no. 3, 16 Feb- 16 Apr 59. on Contract
NOaa-59-6030-C. [1959J 48p. 7 refa. Technical rept.
no. 150; AD- 21 7 515. .
Order from LC inl$3.30, ph»7.80 PB 152 197
Thla report releaaed for aale to the pubUc 28 Oct 60.
Tn«-stress - true-strain tensile properties below
800°P were Investigated. The results Indicsted re-
producible ductile behavior aa low as 750OF. allowing
the use of lower working temperatures which should
favor more efficient lubrication in the drawing die.
Several flxturlng Improvements were made for use on
the draw-bench. Drawing experiments to data have
produced rod at 0. 144-inch diameter (drawn from
0. 252-Inch diameter), a quantiutlve evaluation of
molybdenum disulfide plus powdered graphite for lubrl-
catlon, pointing techniquea, and a cleaning technique.
These experiments, further, have proved certain pro-
cedures unscceptable. Tensile testing of drawn stock
substantiated the basic applicability of the Power Law of
Strain Hardening. Metallographlc and X-ray studies
have ahown the development of crysul arrangements
quite similar to those found in extruded beryllium.
Initial heat-treating experiments have provided an
optimistic suggestion of control of mechanical proper-
ties through thermal treatment after drawina. (Author)
(See also PB 149 617) ^^'
Defense Meuls Information Center. Battelle
Memorial Inst . , Columbus, Ohio.
STATISTICAL ANALYSIS OF TENSIUB PROPERTIES
CM' HEAT-TREATED Tl-4Al-3Mo-lV SHEET, by
H. R. Ofden, G. H. Bcatty and A. E. Mace. Rept. on
Contract AF 19(600)1375. 16 Sep 60. 45p. DMIC
repi. 461.
Order from OTS $1.25 FB 151 095
Some of the dau developed through Phase I of the
Titanium -Alley Sheet-Rolling Program have been
analysed statistically to determine the magnitude of the
variation in the tenalle propertlea and the relation be-
tween these properties and same of the proceaaina
variables. (Author)
66
Haval Engineering ExperimeA Sution, Ahnapolls,
Md.
A STUDY OF METALLIZING AND CHROME PLAT-
ING PROCEDURES FOR RECONDITIONING OF
WORN CRANKSHAFTS, by W. Lee Williams. Prog-
ress rept. no. 2. 10 Jan 56, 26p. 4 refs. Research
and Development rept. 040040F.
Order from LC mi$2.70, ph$4.80 PB 152 642
This report released for sale to the public 10 Nov 60.
The object la to determine the best procedures for re-
conditioning of worn crankabafts on the basis of mlnl-
fflum loss in fatigue resistsnce. The experiments In
dils report deal with: determining the optimum fillet
form for undercut areas in the way of chrome plating;
determining the relative effects of cut-wire peenlng
and shot peenlng as procedures to Induce residual com-
preaslve stresses in the way of plating; and determln-
1^ whether fatigue resistance Is lowered by tempering
of induction hardened journal surfaces to s machinable
level prior to reconditioning. (Author)
TransporVlfaction and Hoist Facilities
Army Engineer Waterways Experiment Sution,
Vicksburg, Miss.
STRESSES UNDER MOVING VEHICLES: TRACKED
VEHICLES (M29C. D4 AND D7) ON FAT CLAY,
1956. by J. E. Green and D R. Frelug. Rept. on
Trafflcability cA Soils as Related to the Mobility of
Military Vehiclea. July 60, 50p. 3 refa. Technical
rept. DO. 3-545, rept. 3; AD- 241 537.
Order from LCml»3. 30. ph$7. 80 PB 152 073
The results of s test program coixlucted to measure
■tresses induced In fairly soft soils by moving trscked
vehicles are presented. Three types of pressure-
sensing devices were installed in prepared areaa of
te clay, and these areas were trafficked by the M29C
weasel and the D4 or D7 engineer tractor. Speed, load,
■ad direction (forward or In reve^^se) of the moving
vehicle were varied during the testing, and the stresses
at various depths and offsets were measured by means
cf three types of pressure cella. It is believed that
such faaors as inadequate vehlcle-alignmem control
aad cell movement during the tests may have caused
the meaaured stresses to vary considerably from pass
to pass. It was found that stresses in the soil under s
tracked vehicle are not uniformly distributed. It wss
concluded that stresses under a loaded track system
dicrease with depth and offset, but not as rapidly as
Indicated by elastic theory. It is recommended that
the firogram to study the stress distribution beneath
dw traction and supporting elements of vehicles be
coatlitued and that the program be expanded to include:
(a) studies of vehicles towing loads; (2) studiea of the
lafluence of soil properties on stress magnltudea and
■reaa pattern; and (c) meaauremetus of static
■tresses. (Author) i
Land Locomotion Lab. . Ordnance Tank -Automotive
Command, Center Line, Mich.
DETERMINATION OF kc, k^, n-VALUES BY MEANS
OP CIRCULAR FOOTINGS. MODIFIED PROCEDURE,
by B. Hanamoto and Z. Janosi. Nov 59, 15p. 4 refs.
Rept. no. 57.
Order from LC ml$2. 40. ph$3. 30 PB 150 999
It hss been^hown by mesns of theoretlcsl and experi-
mental methods that the size effect of a circular footing
penetrating vertically into soil has to be considered by
applyii^ to equation p« (-^ +k^° the radius of the
plate instead of the diameter. Slight discrepancies
formerly noted between soil values established by
meana of recut^;ular and circular plates can be thus
eliminated. (Author)
Michigan U. , Ann Arbor.
OPERATIONAL DEFINITION OF MECHANICAL MO-
BILITY. SUPPLEMENT [NO. 1] by Thomas A. Davis.
Rept. on Contract DA 20-018 -ORD- 14620. Nov 59, 49p.
2 refs. CTAC rept. no. ILL] 55.
Order from LC ml|3. Sa ph$7. 80 PB 150 998
Transportation of a payload made up of a number of dif-
ferent types of commodities can be optimized in off-the-
road locomotion when using physical soil -vehicle re-
lationship defined in terms of speed time, snd fuel con-
sumption. This had been demonstrated by the ofXimiza-
tion of types of motor vehicles and their numbers se-
lected from the available pool. Terrain conditions and
distances to be traveled have been included in overall
consideration. Linear programming methods have been
applied when terrain was "passable". Other methods
were dlacussed in the case of impassable obsucles.
(Author)
Sunford ^. Graduate School of Business, Calif.
AN IMPROVED TRANSPORTATION MOVEMENT
SYSTEM OVERSEAS, by H. J. Canty, J. O. Carter
and others. Final Rept. on Phase 2, Contract DA 44-
177-TC-496. July 60. 244p.
Order from LC ml$ll. 10, ph$37. 80 PB 150 612
This report presents a proposed improved system for
transportation movements of personnel snd cargo in an
overseas area, highway traffic regulation and control,
and budgeting and accounting for transportation move-
ments. One portion of the report describes a con:q>lete
manual system, while s subsequent section deals with
the application of Automatic Data Processing (ADP) to
such s system. Annexes to the report include a com-
prehensive glossary of terms, requirements of the
contract, a description of the Study Task Groiq>, and
other siqjplementary materiaL (Author). (See also
PB 150 611).
Stanford U. Graduate School of Business, Calif.
THE TRANSPORTATION MOVEMENT SYSTEM W
USAREUR- 1958. Final rept. on Phase 1, Contract
DA 44-177-TC-496. [1958] 257p.
Order from LC ml|ll. 10, ph$39. 60 PB 150 611
This report summarizes the Army Transportation Move-
ments (T- Movements) system In effect In the European
Theater during the fourth quarter of 1958. It consists of
the material gathered and produced during a detailed
study of the system in effect in those countries of Europe
in which US Forces are stationed. The report includes a
definition of the system and study, and a summary of the
present sjrstem.
67
MATERIALS
Air Force Cambrilge Research Center. Bedford.
Masg.
MEASUREMENT TECHNIQUB FOR NARROW LINB-
WIDTH FERROMACNETS, by J. I. Muter*.
B. R. Capooe. and P D. Gianlno. May 6a lOp. 4 re£«.
AFCRC-TN-60-388.
Order from LC mi$|l. 80, ph$l. 80 FB ISO 412
Measurement of the line width d a ferromagnetic reso-
nance curve using tbe cavity perturt>ation method offers
some difficulty in tlie case erf fractional oersted line
widths. A new techiUque is described which utilizes
reradUtloo of the incident power by the magnetic sam-
ple Into an induction loop in the waveguide system. Data
are given showing how line widths measured by both
methods compare. (Author)
Feltman Research iLths. , Plcatlmiy ArscMil, Dover,
N. J.
ADHESIVE BONDINC OF METALS FOR ADVANCED
ORDNANCE APPLICATIONS, by John J. Veliky, Ray-
mond P. Wegman and other*. Sep 60, 21p. 2 reft
Technical rept. FRL-TR-8
Order from OTS |0.[75 PB 161 863
This Investlgarlon was conducted to determine die
practicability of bonding to various unusual metals such
as beryllium, chromium, gold, illver, and uranium
238. Ttn commonly used thermosetting adhesive!, a
polyester and a poly-sulfide- modified epooty, were se-
lected for evaluation on the basis of their ability to
•dhere to a variety of surfaces and their good cohesive
•trength chartcterHtica. A modified epoxylated novo-
lac was also evaluated for bonding some at the metals.
Two additional adheslves. a polyurethane and an epoxy
polyamlde, were selected for use with the uranium be-
cause erf difficulties ancountered in bonding to this
metaL (Autiior)
Marine Lab. , U. d Miami, Coral Gables, FU
MARINE BORER INVESTIGATIONS. Final rept. on
Contraa NOy-81879. May 60, 33p. 5 refa. Rept. 60-1;
ML 60106.
Order from LCmi$3, 00. pli$6. 30 PB1S0 9S4
The Marine Laboratory's marine borer control pro-
gram constitutes an erffort to combine knowledge at the
biology d marine wood boring organisms, the chemla-
xry d wood and wood preaervatlveB, and the properties
Of sea water, la an attempt to improve the perform-
ance of conventional wood preservatives by modifica-
tion, or to develop new preservatlvea bavins improved
performance, (See alBo PB 140 S41)
Snell, FoKer D., Ii^., New York.
NAVAL AIRCRAFT DE-ICER AND ANTI-ICER, by
W. RoaenbJatt. E. L.Jung, and J. Mitchell Fain. Final
rept. on Contract NO«s 54-167-c. «) July 54. 56p.
AI>46 281.
tt-der from LC ml$3.60. ph$9. 30 PB ISO 876
The develofxnent Is described oi a de-iang and antl-
Icing material for use on naval aircraft. A new com-
pound. 291 IF -94, whi(± Is recommended for use, con-
tains ethylene glycol and potassium acetate with auitable
corrosion inhibitors, s thickening agent, and a wetting
agent. In addition to good ice- melting and- inhibiting
propertlea, the componenta of 2911F-94 are available
and relatively Inexpensive. The previously recom-
mended compound 2911B-820I was redesignated 291 IF-
820 and revised to meet the requirement of not freezing
•oUd at -650F; the proportion of UCI was reduced to
37%. An Investigation was made of the effec: of the de-
icing fluid B-820I on the lubricating greases Intended
for general use on aircraft; results showed that B-8201
has no more deleterious effea than water alone. The
use of LlCl in the de-icing solution is more efficient if
the UCI Is applied as a concentrated solution than if
the same amount is applied in a more dilute solution.
The efficiency of ethyleneglycol-potaaslum acetate
formulations as de-icers waa evaluated. Studies of the
effea of waxed wing surfsces on the application and
effectiveness of various de-idng compounds Indicated
that the wetting agents performed satlsfaaorily; no
contraction of the compounds was noticed for 24 hr.
Structural Mechanics Research Lab. , U. of Texas,
Austin.
HIGH-VELOCITY IMPACT CUSHICWING. PART V
ENERGY -ABSORFnON CHARACTERISTICS OF PAPER
HONEYCOMB, by Charles H. Karnes, James W. Turn-
bow and others. Rept. on Contract DA 19-l29-<m-817.
25 May 59. 119p. 11 refs. AD-22S 216.
Order from LC ml$6. 00. ph$18. 30 PB 150 631
A review is presented of the enei^y -absorption charac-
teristics of paper honeycomb. For a given set cf test
conditions, a unique stress-strain curve for a particu-
lar grade of honeycomb exists and Is that curve ob-
tained when the cushion is completely cnished. The
average crushing stress for any paper honeycomb cuah-
lon may vary t \.C% from the mean value for that grade
of material. The stress and enei^-absorptlon values
are about 44^ Urger under dynamic losdii^ than for
static loading, while the strain values at bottomii^ are ;
pearly equal. Except for an initial peak, stress levels
are about constant up to 7€% strain under both dynamic
*nd sutlc conditions; a rapid Increase in stress occurs
about 805^ strain. For practical cushion design no
appreciable difference in stress -strain characteristics
occurs for impact velocities from 20 to 90 fps. Mois-
ture contents of less dian 10 to 12% have little effect on
the dynamic cushioning characteristics (rf paper honey-
comb. Increases in moisture content cause the denser
materials to lose energy-absorbing capacity more
rapidly than the lighter honeycomba. The effect <rf
moisture is less significant in dynamic loadii^ than in
static loading. The dynamic stress and ener^gy-absorp-
tkm TSlues of honeycomb material Increase rapidly with
lacraaae in density. The resUlence of paper honeycomb
Is nearly constant until the strain exceeds 70^ and Is
higher for the more dense materials.
This report released lor sale to the puhUc 31 Oct 60.
68
Ceramics and Refractories
Armour Reaearch Foundation, Chicago, 111.
ULTRASONIC AND CERAMIC COATINGS, by
R. R. Whymark and W. E- Lawrle. Rept. for 1 Apr 59-
39 Feb 60 on Materiala Analysis and Evaluation Tech-
niques, Contract AF 33(616)6396. May 60, 52p. 1 ref.
WADD Technical rept. 60-157.
Order from OnrS$ 1.50 PB 171 057
This r«port describes investigations into the use of
ultrasonic techniques to determine strength of ceramic -
meul bonds and to locate defects in the bonds. The
techniques evaluated have Involved the use of both high
frequencies (1-10 mc/s), low frequencies (14 kc/8)and
the simultaneoua use of high and low frequencies. Ex-
periments at low signal frequencies indicate the aver-
age bond strength of flame- sprayed zirconium oxide to
be about 1500 psl. Promising results have been ob-
tained using hl^ frequency transmitted energy and a
Schlleren detection system. Apparatus is designed to
generate surface acoustic waves. The applicadoo of
surface waves to defect detection is considered. An
experimental method has been developed to utilize
intermodulatlon between high and low frequency sound
waves to Indicate bond continuity. Intermodulatlon
techniques obviate the need for repeatable coupling of
transducers which is required In direct high frequency
transmission methods. Consideration is given to
ultrasonic Image converter systems. (Author)
Army Signal [Research and Development] Lab.
Fort Monmouth, N. J.
STUDY OF AGING EFFECTS ON DIELECTRIC
ELECTROMECHANICAL PROPERTIES OF FERRO-
ELECTRIC CERAMICS, by N. A. Terhune and
J. J. Charlton. [1956] 7p.
Order from LCmi$ 1.80, ph$ 1.80 PB 152 805
This report released for sale to the public 18 Nov 60.
Brush Beryllium Co. , Cleveland, Ohio.
AN INVESTIGATION OF INTERMETALLIC COM-
POUNDS FOR VERY HIGH TEMPERATURE APPLI-
CATIONS, by Robert M. Paine, A. James Stonehouse,
and Wallace W. Beaver. Rept. for 13 Mar 57-
31 Oct 58 on AEC-ANP Materials Research, Contracts
AF 83(616)56-12 and AT( 30- 1)541. July 60, 130p.
9 refs. WADC Technical rept. 59-29. Part II; un-
cUssified version cf WADC TR 57-240, Part U.
Order from OTS $3.00 PB 171 081
The preparation, fabrication, and properties of loter-
meulllc compounds under development for service In
die temperature range of 2300° to 3OO0PP are de-
scribed. The compounds have exhibited strength as
measured by the modulus-or-rupture test of up to
40, 000 pel at 2700°F and resisunce to oxidation for
100 hours to 2800°F and have indicated good thermal
conductivity. The compounds were prepared by solid-
state reactions and fabricated chiefly by hot-pressing
techniques. Oxidation rests were tnade in dry air to
3000OF and In moist air to 2500OF. TransvelSe-
rupture tests were carried out at 2300°. 2500°, and
2750<^. Room-temperature hardness data and melting
points are reported for some compounds. Thermal-
expansion and thermal-conductivity data for selected
compounds are also presented. (Author)
Carborundum Co. , Niagara Falls, N. Y.
CONTINUOUS FILAMENT CERAMIC FIBERS, by
W. A. Lambertson. D. R Aiken and E. H. Glrard.
Rept. for Jan 59- Feb 60 on Air Force Textile Materials,
Contract AF 33(616)6246. >ine 60, 8^. 45 refs.
WADD Technical rept. 60-244.
Order from OTS $2. 25 PB 171 061
* r
Melting and fining of refractory glass compositions and
drawing of ccMttinuous filament ceramic fibers have
been carried out in a dry. Inert-atmosphere glovebox.
which permitted the use of refractory metals, graphite,
and boron nitride as crucible and heater materials,
and prevented the adsorption of moisture by the fila-
ments. Several refractory glasses in the baria-alum-
ina- silica, calda-alumina- silica, and magnesia-alum-
ina-silica systems were successfully drawn into con-
tinuous fllamets. Tensile strengths of filaments drawn
were determined at room and elevated temperatures.
Values as high as 138, 000 pounds per square inch at
room temperature and 132, 000 pounds per square inch
at 1500°F. (815°C. ) were obulned. (Author)
Lockheed Aircraft Corp. , Sunnyvale, Calif.
PROPERTIES OF REFRACTORY MATERIALS: COL-
LECTED DATA AND REFERENCES, by Wanda G.
Bradshaw and Clayton O. Matthews. 2nd ed. 3rd
printing, 15 June 60. 114p. 114 refs. LMSD-2466.
Order from OTS $2. 50 PB 171 IM
., I
A survey of the elevated-temperature characteristics
of refraaory materials melting above 2500°F was
nude. Data have been tabulated for evaluation of these
materials for use in elevated-temperature nuclear re-
actors, and in high-temperature missile applications.
Data on the melting points, ductility, and elevated-
temperature stability <^|>fbe refraaory meuls, car-
hides, nitrides, oxideaxj^ilicides, sulfides, beryl-
lldes, alumlnides, other Intermetallics, phosphates,
and uranates are presented. The thermal shock re-
sistances, thermal conductivities, thermal expansion^
and emlsslvltles reported for these materials are
given. The effea of nuclear radiation on ceramics Is
reported. The mechanical properties (rf refraaory
materials are briefly reviewed. Sources of thermo-
dynamic data for these materiala are presented. The
effeas of various gas coolants, helium and its major
likely contaminants, oxygen and water vapor, hydro-
gen, nitrogen, and other gases on refraaory materials
are also reported. Where confllaing or variable data
exist, the original authors are cited. (Author)
Olin Mathieson Chemical Corp. , New Haven, Conn.
INVESTIGATION OF GLASS FLAKE LAMINATES, by
J. J. Aclin and T. A. Cocca. Final rept. on Contraa
DA 19-020-ORD-4751. 2 Feb 60, 52p. 8 refs.
AD- 233 969.
Order from OTS $1.50 PB 171 039
Three methods of preparing glass lamellates have been
developed. Each method appears to be commerlcally
69
feasible. The techniques differ In the method of com-
bining the resin and ilass flakes and may be summar-
ized as follows: (1) spraying free falling glass flakes
with resin in a plenum chamber and "B" staging prior
to molding; (2) coatir^g the glass flakes with resin by
mixing in a centrifuge; and (3) dry blending of powdered
"B" suge resin and glass flakes. The lamellates pro-
duced by these processes have excellent physical prop-
erties, except for impaa and tensile strength whichare
somewhat low. The low values may be due to the ex-
cessive quantity of fl^ particles at glass in commer-
cial glass flakes. Two practical applications for glass
flake laminates have been suggested by this work- (1)
rocket exhaust nozzles and (2y rocket cases. (Author)
Utah U. . Salt Lake tlty.
SURFACE AND ENVIRONMENTAL EFFECTS ON
CERAMIC MA.TERIALS. by P. Glbbs. G. S. Baker and
others. Rept. for June 58- May 60 on Ceramic and Cer-
met Materials, Contract AF 33(616)5«76. Aug 60 29d
11 refs. WADD Technical rept. 60-473. '
Order from OTS SO. 7j pg m 074
Creep and recovery phenomena in sintered polycrystaj-
llne alumina have been studied. Effects of temperature
and impurity content oti creep behavior and the results
of observation of polished and etched surfaces are dis-
cussed. The results are analyzed in terms of a tenta-
Uve conventional mechanical analog. An electrical
study of the behavior cT sUver tons on a corundum sur-
face is described. Current flow between evaporated
silver films on AI2O3 (Crystals Is investigated as a
function of geometry, cemperature. atmosphere, his-
tory, and applied voltage. The initial stages of creep
insingle crystals of aAl203 (synthetic sapphire) have
been investigated as a function of stress and tempera-
ture. Creep rates were measured in die temperamre
^' ^?^^ "^ ^^°^ *™^ 1" *« ««" '"te^«l of
500 to 1000 Kg per cm. ^ resolved shear stress on the
outermost fiber of the apecimen. The stresses covered
«e region from too little stress to Initiate creep op to
the fracture stress. A plot of log. creep rate versus
reciprocal temperature gives an activation energy of
85 Kcal/mole. ^)eclm«is oriented so that (ll20) (lIOO)
slip system wai^-operatJve but the (0001) (ll20) slip
system had zero resolved shear stress gave no signif-
icant creq> at these temperatures. (Author).
I
Fod«, LobficanN, and Hydraulic Fluids
Air Force Flight Test Center, Edwards AFB. Calif
DECONTAMINATION or LARGE UQUID FLUORINE
SPILLS, by Ronald P. Rickey. Oct 59. 31p. AFFTC-
TR-59-31; AD-228 033.
Order from LC nil$3. 00, ph|6. 30 FB 152 297
The main objecUve of th« tests was the development of
an effective neutralization of liquid fluorine spills.
The minimum requirement would be the reducuon of
fluorine- concentration oq the ground ar the edge of the
reservation at Highway 395 (6 miles downwind) to a
level below one part per million. Preliminary test at
General Chemical's plant at Baton Rouge indicated that
water spray and/ or sodii»n carbonate (soda ash) would
be effective materials fof testing. Using these as the
neutraliters. a total of 5^)00 P9und8 of fluorine was
i 70
' "I
•pUled at the Haystack Butte area. A third apiU was not
neutralized and was used for comparison with the two
methods. The water ^ray waa the nrKjst effective; the
carbonate neutralization was moderately effective The
unneutralized fluorine was detectable 6 miles downwind
from the spill. A combination of water fog and/or so-
dium carbonate should give acceptable neutralization of
liquid fluorine in the case of a Urge spill. (Author).
Army Ordnance Corps. Washington. D. C.
SAFETY REQUIREMENTS FOR THE MANUFACTURE
AND LOADING OF CASTABLE COMPOSITE PROPEL-
LANTS. 1 Mar 60. I3p. ORDM 7-230.
Order from LC ml$2. 40. ph$3. 30 PB 152 354
This report released for sale to the public 25 Oct 60.
r
Defense Meuls Inforjnatioo Center. Battelle
Memorial Inst.. Columbus, Ohio
COMPATIBILITY OF ROCKET PROPELLANTS WITH
MATERIALS OF CONSTRUCTION, by W. K. Boyd and
E. L. White. Rept. on (Contraa AF 18(600)13751.
1^ Sep 60. 65p. 200refs. DMIC memo. 65.
Order from OTS $0.50 pb 16I 215
This report summarizes the available Information on
the compatibility of Uquid rocket propellants with
I«-omlnent materiala of construction. It is pointed out
that compatibiUty data for materials not ordinarily
covered by the Defense Metals Information Center are
ncluded. These data were found during the search for
InfOTmation on materials that are within the scope of
'_!-.■ '"^ "* Included for convenience. Fuels and
oxidlzera of current Interest are discussed. The cor-
rosion data which are presented will apply to storing
handling, and control equipment outside of missiles
and to missile components up to the combustion cham-
tier. The compatibility of materials with reaaion
K^'<!Sn'sffe?°°"^"^"' "°"^"' «-• »»-
[Feltman Research] Laba. , Picadnny Araenal.
Dover, N. J.
ANALOG COMPUTER COMPUTATION OF PROPEL-
LANT UNEAR BURNING RATE, by Arthur 1. Rubin.
Mar 5<J, 33p. 3 refs. Technical rept. 2237
Order from LC ml$3. 00. ph$6. 30 PB 152 351
This report released for sale to the public 28 Oct 60.
Unique circuitry was developed to compute Unear
burning rate from closed bomb data with the Ease analog
compwer. Results of this computation are permanentl/
recorded as a continuous curve representing linear
burning rate as a function of pressure. Significant
savings in computing time are achieved by the analog
computer. The desk -calculator method computes only
Ave or six points 00 the burning rate pressure graph
To lllu«rate the method, details of the analog computer
computation are shown for a representative problem.
(Author)
L^ockheed Aircraft Corp. , Sunnyvale, Calif.
DEFLAGRATION LIMITS IN THE STEADY LINEAR
HJRNING OF A MONOPROPELLANT WITH APPLI-
CATION TO AMMONIUM PERCHLORATE, by
V E. Johnson and W. Nachbar. Technical note on
Contract AF 49(638)412. Aug 60, 42p. 17 reft.
LMSD- 703060; AFOSR-TN-60-700; AD- 243 489.
ORlerfrom LCmt$3. 30, ph$7. 80 PB 152 027
Aa analytical model lor tjie steady, linear burning of a
mcoopropellant it employed to describe the results of
experiments done elsewhere on the burning of pressed,
pure ammonium perchlorate pellets. Upper and lower
bounds for the eigenvalue of the mathematical problem
are derived. These bounds are convenient to use for
Bumerlcal compuutlons, and they afford a rigorous
Mttaate of the approximation error. In following the
liypothesis that the low-pressure deflagration limit
(p_- ) observed In these experiments Is due to radiant
mSStti loss from the burning surface of the pellet, it
Is first demonstrated analytically that the'model will
also display a similar p[^ upon Introduction of a term
representing this loss, tt is shown that, with reason-
able numerical values, a good fit can be obulned from
this theory to the experimental burning rate vs. pres-
sure curve for pressures well above Vn,- However,
the calculated value of Pq^ due to surface radiant loss
Is much less than the observed value, and agreement
vllh experiments is obtained only when an energy loss
greater than that which can be presently accounted for
is assumed. (Author)
Naval Ordnance Test Station, China Lake, Calif.
SCREW EXTRUSION OF SOLVENTLESS DOUBLE -BASE
PROPELLANT IN ECCENTRIC SHAPES, by James R.
Sima. 1 Mar 60, 3lp. NOTS TP 2041; NAVORD rept.
5894. '
Order from LC ml$3. 00, ph$6. 30 PB 150 390^
Development work was performed on the extrusion of
eccentric shapes of solventless double- base propellant
for possible Inclusion in a segmented grain. The 1-
inch screw extruder was used as a processing tooL
Equipment design and test extrusions for each of three
segment designs are described and the results are dls-
cuaaed. The propellant flow and expansion character-
istics are shown to be significantly different in concen-
tric and eccenrric extrusions. Methods of compensa-
tion for these differences were investigated. The fea-
sibility of extruding eccentric shapes with a screw ex-
truder was demonstrated. (Author).
Naval Research Lab. , Washington, D. C.
MICROBIAL INHIBITORS FOR SYSTEMS OF JfiT
FUEL AND WATER, by Dorothea E. Klemme and
John M. Leonard. Interim rept. 31 Aug 60, lip.
9 refs. NRLrept. 5501.
Order from LC ml$2.40. ph$3.3(> FB 146 402
Certain bacteria and fungi developing in water phases
in conjunction with Jet fuels are indicated as sources
of trouble in these hydrocarbon nruterlals. Growth of
the microorganisms apparently decreases filterabllity
of the fuel and otherwise causes nulfunctionlng of fuel
systems. The biological tissue can clog filters. One
poaslbiUty for controlling such microbial cootamina-
tlooa in fuel-water aystema ia the addition of a toadc
agent that would prevent the development of the organ -
lams. With this purpose in mind, twenty substances
known to be toxic to microorganisms have been studied
for inhibition in an environment of JP-5 fuel and aque-
ous salts solution, the fuel serving as the sole source
of carbon. Four n-alkyl quaternary ammonium chlo-
rides and an n-alkyl laoquinolinium chloride prevented
bacterial growth when incorporated in the solution at
50 or 100 ppm, but not at lower concentrations. Only
the isoqulnolinlum substance caused no turbidity in
either the fuel or the water p>hase. Silver metal, toxic
at exceedingly low concentrations, proved to be
bactericidal in smaller amounts than required for
fungicidal action. Tetraethyllead and ethylene dibro-
mlde, when incorporated individually in |P-5 at roughly
0. 13 and 0. 5 ml per gallon, respectively, were .
inhibitory to baaeria. In comWnatlon in the tetra-
ethyllead antiknock preparation, however, these com-
pounds exhibited a lesser degree of toxicity. Although
none of the quaternaries were Inhibitory at coocentra-
tlons as low as desired, some of them may be useful
in keeping microbial contaminations to a minimum in
such trouble areas as storage tanks. But addition oi
inhibitors to Jet fuels poses many complications, and
for this reason, other approaches to the solution of
the problems are under investigation. (Author)
Naval Research Lab. , Washington, D. C.
A STUDY BY UGHT SCATTERING OF THE
EFFECT OF WHM TEMPERATURE ON THE FOR-
4, MATION OF INSOLUBLES IN JET FUELS, by
R. L. Shuler, J. A. Krynitsky, andH. W. Carhart.
Interim rept. 4 Oct 60, 19p. 21 refs. NRL rept. 5553.
Order from OTS $0.50 PB 161 921
An Investigation of the chemical behavior of JP-4 and
JP-5 fuels and pure Hydrocarbon solutions heated to
high temperatures (300° to 700OF) has been undertakea
using light scattering and gas chromatography as the
primary research tool*. The extent of degradation of
the hydrocarbon systems in this temperature range
was evaluated on the basis of particulate matter
formed. This quantity was estimated by the Intensity
of the light scattered at 45 degrees measured in a
backward direction from the Incident light. The ex-
perimental evidence obtained in this manner has
clearly indicated that, in the temperature range
studied, the oxidation of small amounts of nonhydro-
carbon substances present In the fuel, e.g., sulfur
and nitrogen compounds, gives rise to Insoluble mate-
rials. The possibility of pyrolysis as a major decom-
position process has apparently been eliminated by (a)
the absence of pjartlcle formation in a fuel heated in
an oxygen-free atmosphere and (b) an infrared spec-
tral analysis which shows no gross changes in hydro-
carbon structure after heating the fuel. The possi-
bility of using the light- scattering technique to gain an
i .sight into particle size by measuring the dissjrmme-
try of scattering was explored.
Nonmetallic Materials Lab. , Wright Air Development
Div. , Wright -Patter son AFB, Ohio.
LOAD SUPPC»T AND ANTI-SCUFFING PROPERTIES
OP LUBRICANTS. PART II. WADC UNIVERSAL
GEAR AND SPLINE LUBRICANT TESTER, by Leslie
R. Drane, Jr. Rept. for Jan 59-Jan 60 on Aviation
Lubricants. May 60, 21p. 15 refs. WADC Technical
rept. 59-736, Part 2.
Order from OTS $0.75 PB 171 055
71
n
The design and cipei^ting characteristics of a gear and
spline lubricant tesQer are described. Results of
sriidles to determine the effect erf lubricant flow rate,
gear speed, and inert atmosphere on gear scuff load
are presented. Lubricant load carrying ability de-
creased sharply in (tie 5000 Co 10, 000 rpm range, but
leveled off in the 15, 000 to 20, 000 rpm range. A
slight increase in scuff load with increasing speed was
noced in some casea The use of an inert atmosphere
caused a decrease in scuff load rating with a mineral
oil, a sebacaie, and a silicon-ester blend. Two slU-
cooe fluids showed no significant change In scuff load
when tested in an in^rt atmosphere. (Author)
Nonmetallic Materjlals Lab. , Wright Air Development
Div. , Wright -Pattar son AFB, Ohio.
PERFORMANCE OP PETROLEUM BASED HYDRAU-
UC FLUIDS IN A PUMP LOOP AT 3000 PSI AND
275OF, by Robert E, Johnson. Rept. for Jan 56- July 59
on Power Transmission Technology. June 60, 87p.
WADD Technical reft. 60-352.
Order from OTS > 2. 25 R 171 063
Fluid breakdown and pump wear were investigated in
f. pump loop at Z75°t and 3000 pM on five petroleum
. based hydraulic fluids. The mechanical shearing erf
these fluids resulted In excessive loss of viscosity,
although their resistance to oaddatlon was not appreci-
ably changed. The wide variations in the wear data at
these fluids indicated their difference In lubrication
characteristics In the particular system employed.
Bench wear data did not correlate with the pump wear
results. (Author)
t
[Office erf Defense llesearch and Engineering!
Washington, D. C
SYMPOSIUM ON ANALYSIS OF NITRIC ACIDS
SPONSORED BY THE PANEL ON FUELS REQUIR-
ING OXIDIZERS. 3L Dec 51, 87p. 20refs. Commit-
tee on Fuels and Lubricants rept. FRO 200/10.
Order from OTS $2. 25 PB 171 115
Contents:
Wet methods of analfsls
- Determination at nirlc add in metal contaminated
solutions I
Analysis at fuming kiitrlc acids
Wet methods of analysis at nitric acids and mixed
adds
Volumetric analysil at white and red fuming nitric
add if.
The determination ^ nitric add by reduction with
ferrous sulfate
Methods of analysis for fuming nitric adds
Instruments, method* of analysis, and direct deter-
mination at water
Determinatioa erf w^ter in fuming nitric add by
Infrared absorption
The determination of water in white fuming nitric
add with a few co(nments oo instrument methods
for other componeus
A field aasay for witite fuming nitric add
Parker Aircraft Co. , Los Angeles, Calif.
HYDROGEN HANDBOOK. A COMPILATICW OF
PROPERTIES, HANDLING AND TESTING PROCE-
DURES, COMPATTOILITY WITH MATERIALS AND
BEHAVIOR AT LOW TEMPERATURES. Arthur D.
Little, Inc., rept. on Contract AF 33(616)6710.
Apr 60, 257p. 157 refs. APFTC TR-60-19.
Order from LCmi$l 1.10, ph$39. 60 PB 150 282
This report released for sale to the public 14 Nov 60.
This report summarizes (1) experience with and avail-
able technical information on the development of rwo
prototype valves, one for a cryogenic gas service and
the other for a cryogenic liquid service; (2) biblio-
graphical information on the physical and mechanical
properties of specific construction materials for a
temperature range of -420°F to +200*^ (these mate-
rials include some austenitic stainless steels and
Teflon plastics); (3) the thermodynamic properties erf
helium, hydrogen, and nitrogen fluids with which the
valves may be used or tested: (4) the hazards asso-
ciated with the transportation and storage erf hydrogen
and with its use for testing the pn-ototype valves for
leakage across the seats; and (5) the sources and
availability of hydrogen, and the Los Angeles regula-
tions that apply to its transportation and use. (Author)
Shell Development Co. , Emeryville, Calif.
FUNDAMENTALS OF GEAR LUBRICATION, by
V. N. BOTSoff. Final rept. for June 54- June 55 on Con-
traa [NOas] 53-356-c. [1955] 128p. 11 refs. Rept.
no. S-13649. AD-87 968.
Order from LC mi$6. 30, ep$21 .30 PB 152 755
This report reltsased for sale to the public IS Nov 60.
Research was conducted to explain the mechanism of
gear lubrication and to determine the effeas of gear
geometry, operational, and lubricant faaors. The in-
vestigation showed that unreactive minerals and syn-
thetic oils operate in gears through the formation of a
thick lubricating film. Such films deform viscously In
slow-speed operations, bu at high speeds, the oils be-
have as semi -elastic solids. With unreactive oils,
breakage of the thick film results In scoring. Extreme
pressure (EP) compounded oils operate by the forma-
tion of strongly attached films which are the produa
of the reaction between the metal and the aaive agent.
Wear of gears was subdivided into: (1) wear by scor-
ing; (2) wear by abrasion; and (3) wear by chemical
corrosion before reaching the score load. The im-
portance erf viscosity as a lubricumt factor was demon-
strated with various synthetic oils. Changes in the
viscosity effect with speed suggested the involvement
erf relaxation phenomena. The results of long-term
wear tests agreed with those of the short-term tests.
The long-term wear tests revealed that in operations
at loads above the score load of the lubricant, the
conditions are unstable and any sh<x:k or vibration may
cause the recurrence of severe s<x>ring. Gear geome-
try factors appreciably affected the load-carrying
capacity. Tests with radioactive EP lubricants con-
firmed the theory of the action of EP agents through
the fornuulon of strongly attached EP films. The
thickness erf the EP films increased with tempersture;
for each set erf operating conditions, an appropriate
steady-state thickness of EP film is established. (See
also PB 137 817)
i 4
' t
Leather and Textiles
72
(Varternuster Research and Engineering Center,
ftetlck, Mass.
nevELOFMENT OF SHADE STANDARDS AND TOL-
ERANCES FOR USAF BLUE 84 AND BLUE 584 SERV
ICE AND OPTIONAL WEAR UNIFORMS, by Frank J.
lUno, Constaatlne J. Megas and others. Rept. for
26 ^n 53-1 Oct 58 on Air Force Textile MaterUli,
Oootttcts AF 33(616X53-221, 54-2. 55-72. and 54-107V
Uav60. 247p. 55 refs. WADD Technical rept. 60-150.
SrdLrfTomOTS$3.50 PB 171 089
An extensive study erf dye formulations was accom-
plished from which new highly colorfast formulations
lere developed. These formulations have application
cteracterlstlcs suitable for both large and small In-
daitry. The formulation selected represents somewhat
of a compromise between, colorfastness properties,
i^lcatlon characteristics, availability factors and
«k1 use requirements. The complete program was
monitored by application of both standard visual tech-
niques and color imetrlc analysis based on spectro-
Bhotometrlc data transposed in accordance wldi the
cristlmulus functions erf the QE standard obso-ver for
colorlmetry. The tolerance ranges are visually well
spaced, although the colorimetric spacing of the in-
strumental technique does not coincide with visual
Judgment. The reasons for dils situation are analyzed,
and it Is concluded that a further review of the theory
of color mixtures must be made for dils type of blend-
ti^ operatiexi. (Author)
(Quartermaster Research and Engineering Cet«er
[Natick, Mass.]
DEVELOPMENT OF SHAC« STANDARDS AND
TOLERANCES FOR USAF TAN 505, by Frank J.
Rlzzo, Constantine J. Megas and others. Rept. for
Jan 53-Jan 57 on Air Force Textile Materials, Con-
iraas AF 33(616)53-221 and AF 33^616)55-72. May 60,
63p. 49 refs. WADD Technical rept . 60-294.
Order from OTS $1 . 75 PB 171 062
Shade standards and tolerances for USAF Tan 505 used
In hot weather clothing have been developed in three
fabric constructions ualng a formulatltm which has had
considerable industrial appUcatlon for a number of
related shades. This program was monitored by visual
as well as colorimetric procedures. The tolerance
■padng visually should provide for a reasonable ap-
proach to a monotone a{>pearance in uniftMrms made
from two different pieces of fabric in the same con-
struction. The shade charaaeristics of the three fab-
rics are such as to provide for use of any erf the fab-
rics In a single ensemble. Whatever differences
occur are ihore related to fabric texture than to
•pecific differences In color. The colorimetric spac-
ing obtained instrumentally does not coincide with the
visual evaluation. The report discusses the reasons ,
for this in deuU. The degree of colorfastness I
achieved is optimum for the depth of shade. (Author)
(JuarternMister Research and Engineering Center,
Natick, Mass.
WOOL-TYPE 16-OUNCE SHIRTING FABRICS
BLENDED WITH THREE FIBERS, by Constantl
J Monego and Lyman Fourt (Harris Research Labs. ).
Rept. no. 29 (Final) for 18 Sep 58 on Contract DA
l9-129-qm-l073. May 60, 44p. 11 refs. Textile
Series rept. no. 112.
Order from LC mi$3. 30. ph$7. 80 PB 150 548
Studies of the effects of fiber, yarn, weaving, and full-
ing variations have led to principles of design and fin-
ishing for promoting thickness and wool-type charac-
teristics. Man-made fibers should be matched In diam
eter. length, and crlny with the wool; yam twist should
be relatively low; direction of twist she>uld be opposite
In warp and filling; float length should be relatively
long, and fulling^ould be extensive, with up to 25 per-
cent shrinkage ijP>oth width and length. Thickness
should be devel#ed by fulling alone, without n^>plng,
to conserve strength and obtain a wool-plated surface.
Fabric thickness in the range of the standard shirt- ^
Ing can be obtained without napping, using 35 per-
cent non-wool fiber nude up by 15 to 20 percent of
pairs selected from acrylic, modacryllc, viscose
rayon, cotton, or nylon fiber. The results indicate
that nylon is advantageous for strength, and viscose
rayon for strength, ecexiomy. fulling, and some as-
pects of resistance to flame and heat. Trials of differ-
ential shrinkage as an alternate or supplement to full-
ing indicate that much more development work will be
required before this principle can be i^jplied in this
type of heavy woven fabric.
National Research Coundl. Washington, D. C
FABRICS FOR COATING: MILITARY APPUCATIONS:
PROCEEDINGS OF A CONFERENCE AT THE
QUARTERMASTER RESEARCH AND ENGINEERING
CENTER. NATICK, MASSACHUSETTS, OCTOBER
16-17, 1958, ty Frank R. Fisher and Stanley Backer.
1959. 227p. 22 refa.
Order from LCmi$9. 90. ph$34. 80 PB 150 962
This report released for sale to the public 17 Nor 60.
Contents:
Army applications of fabrics for coating
Naval applications for coated fabrics
The role of coated fabrics in today's air force
Design for climatic extremes
Interactlcms of fabrics and coatings
Fabrie^s for coating— design and e^existructloo
New fibers and fabrics for coating
Technical advances In coating nruierlals for fabrics
Technical problems of the coater
Evaluation of end item performance
Supplementary presentatiexis
Characteristics of vinyl and nitrile coating nuterlals
as well as a lcx)k at some newer produas
Butyl rubber In proofed goods applications
The laminate structure
Comments on fibers
73
Wyandotte caiemlcals Corp. . Mich.
DEVELOPMENT Of A FABRIC TO PROVIDE PER-
SONAL PROTECTION FROM TOXIC MATERULS. by
Raymond G. SpUn and Alexander V. Sanger. Rept. for
I May 59-30 Apr 60 on Air Force Textile Materlala
Comraa AF 33(616)6501. June 60, 45p. WADD Tech-
nical rept. 60-198.! \
Order from OTS $125 PB 171 058
This report describes research directed to the devel-
ojment of a coated fabric to resist the chemical effeas
o€ and be Impermeable to high energy fuela (HEF).
This program Included the dealgn and fahrlcadon of
special test equipment and of a laboratory fabric coat-
ing apparatus. A base fabric (Dacron) was selected oo
the basis d resistance to HEF. and the majority at
the effort was direcped toward the coating o* this fabric
with nuoroeUstomer based compoaltlons and the
necessary subsequent testing. (Author)
Poirits and FinishM
irits
Marine Lab. . U. of Miami [Coral Gables] Fla
ANTIPOULING PROfERTIES OF PESTICTDAL 'MATE-
RIALS, by Sigmund Miller. Monthly progress rept fbr
1 May-15 June 59. of Contraa NOa<s) 59-6182-c
15 June 59. 7p. ML S9137.
Order from LC mi$L 80, ph$l. 80 PB 150 768
The purpose d this program is to evaluate the effec-
tiveness d various etcperlmental and proprietary pesti-
cides as antifoullng toxicants. The screenli^ test tech-
niques which Is employed wlU^iualltatlvely classify the
effectiveness of the pesticides for control of the various
forms of fouliTg organisms. The first rack at 19 panels
was exposed on 19 M$y 1959. When the panels were in-
apected after 10 days, fouling organisms were present
oo the control panel and on 15 test panels. Three pan-
els were completely free of fouling. This group has not
yet completed a full thirty day test period. Six addi-
tional racks d 19 panels each have since been exposed
, U. or Mi.
Marine Lab. , U. d iMiami [Coral Gables] Fla
ANTIFCULING PROPERTIES OF PESTICTDAL 'MATE-
RIALS, by Slgraund Miller. Monthly progress rept for
1-31 July 59. on Cootjact N0b(8) 59 -61 82 -t. July 59, 8p
ML 59182. •^
Order from LC ml$l. 80. ph$l. 80 PB 150 770
The effectiveness of tl^ chemicals In preventii« attach-
ment of the various fouling organisms Is listed in de-
scending order of effectiveness. 84 of the 144 chemi-
cals tested were completely Ineffective, and have not
been Included In the table. (See also PB 150 769)
Marine Lab. . U. d Miami [Coral Gables] Fla
ANTIPOULING PROPERTIES OP PESTiaDAL MATE- '
RL^LS, by Sigmund Miller. Monthly progress rept for
1-31 Aug 59. on Contract N0b(8) 59-6182-c. Auc 59
7p. ML 59211. ^
Order from LCmI$l.iO. ph$1.80 PB 150 771
The effectiveness of the chemicals in preventli^ atuch -
mem of the various fouling organisms Is listed in de-
scending order d effectiveness. 94 d ttv 144 chemi-
cals tested were completely ineffective, and have not
been included in the table. (See also PB 150 770)
Marine Lab. . U. d Miami [Coral Gablesi PU
ANTIPOULING PROPERTIES OF PESTiaDAL MATE-
RIALS, by Sigmund Miller. Monthly progress rept for
1 -30 Sep 59, on Contract NOa<s) 59-6182-q, Sep 59. 9p.
Order from LCmUl. 8a phll. 80 ,.PB 150 772
The effectiveness d the chemicals In preventli^ at^d|.
ment of the various fouling organlsma is listed in de-
Bcendlng order of effectiveness. 25 of the 36 chemicals
tested were completely ineffective, and have not been
Included in the table. Confirmatory tests have been
conducted on 36 chemicals; results of the confirmatory
test tn shown immediately below results o* the test d
each chemical. (See also PB 150 771)
Marine Lab. , U. d Miami [Oorml Gables] PU
ANTIPOULING PROPERTIES OF PESTICIDAL MATB-
RL\LS. by Sigmund Miller. Monthly progress rept for
iii^^cS*o''' <* Contract NOb<s) 59-6182-c. Oa 59, 8p.
Order from LC ml$l. 80. phjl. 80 PB 150 773
The effectiveness of the chemicals In preventliM atuch-
mcni d the varloui fouling organisms is listed In de-
acendlng order d effectiveness. Six of the 18 chemicals
tested were completely Ineffective, and have not been
included in the table. Confirmatory tests have been
cooAicted on 72 chemicals. (See also PB 150 772)
Marine Lab. . U. d Miami [Coral Gables] PU.
ANTIPOULING PROPERTIES OF PESTIODAL MATE-
RIALS, by Sigmund Miller. Progress rept. for 1 Nov-
31 Dec 59. on Contract NOa(s) 59-6182-c. [1960] 13d.
ML 60020. ^
Order from LC ml$2. 4a pfa$3. 30 PB 150 774
The effectiveness of the chemicals In preventing attach-
ment d the various fouling organlams is listed in de-
scending order of effectiveness. Thirty-six of the
chemicals tested were completely Ineffective, and have
not been Included in the table. Confirmatory tests were
conducted on 90 chemicals. (See also PB 150 773)
Marine Lab. , U. of Miami [Coral Gables] FU.
ANTIPOULING PROPERTIES OP PESTICIDAL MATE-
RIALS, by Sigmund MiUer. Progress rept. 1 Jan-
29 Feb 60, on Contraa NOa(s) 59-6182-c. [1960] lOp.
Order from LC mill. 80. ph$ 1. 80 PB 150 775
The effealveness of 36 chemicals In preventing atuch-
ment of the various fouling -vganlsms is listed in
descending order of effectiveness. Twenty-two of the
. chemicals tested were completely ineffective, and have
not been Included In the table. The first evaluation of
36 new chemicals was conduaed during the present
repwrt period. Descriptions of the chemicals and re-
sults of the test follow. Nine of the chemicals were
completely Ineffective, and have not been included in
the table of results. Confirmatory tests were coo-
ducted on 18 chemlcaU. (See alao PB 150 774)
i_
lock UUnd Arsenal Lab. , HI
T»ffi EFFECT OF IONIC NICKEL IN HOT ZINC PHOS
IHATIZING SOLUTIONS, by Paul G. Chamberlain.
iQFeb 59. I3p. 4 refs. Rept. no. 59-492; AD-210 922.
Order from LC ml$2. 40. ph$3. 30 PB 152 294
TWs report released for sale to the public 1 Nov 60.
jh« effect of nickel Ion additions to hot zinc phosphatlz-
M baths on coating weight, corrosion resistance and
tenure of coating was determined. It was found that as
BMCfa as 20% increase in coating weight resulted. A
riWK Improvement in darr^slon resistance was noted.
TIjs texture erf the coating n^s somewhat coarser than
(fce control without nickel. (Author).
!"
PlofHcs
Falrchild Kinetics Div. , ^airchild Engine and
AirpUne Corp. [New York].
DBflGN MANUAL FOR GCASS REINFORCED
PLASnCS IN NAVAL APPUCATIONS. Rept. oo Coo-
tract NOb8-66373. Jan 58, ;7I6p. 31 refs. NAVSHIPS
350-346-3.
Order from OTS $8. 00 PB 171 096
Stniaural pUstics are prenently being used in the
coostrualoo of a variety o# naval ships, boats and
•qulpment . Successful use of these materials depends
\^oa proper design, fabrication and insulUtion. This
manual is provided for general guidance in the design
of gUss reinforced pUstlc structures. The design
■tress curves are not applicable to all struaures.
Tliey will need to be modified in many Instances to
■ait the particular need of the structure.
PUatica Technical Evaluation Center, Picatinny
Arsenal, Dover, N. J.
FLAKE-GLASS LAMINATES, by Allen M. Shlbley.
State of the Art, Oa 60, 130p. 8 refs. PLASTEC
rept. 1.
Order from OTS $2. 75 PB 161 947
An evaluation of flake-glass Umlnates for structural,
electrical, and other uses. Methods of manufaauring
and testing gUss flake are described and illustrated.
Compositions d various types of suitable glasses are
Indicated. Resin coatings and methods of applying
these coatings are also described and illustrated.
Optimum resin systems are detailed. Methods used
fcr the manufaaure of fUke-gUss Umlnates are given
la detail. Tests of tensile and flexural strengths, and
flf modulus, are described. Comprehensive dau oo a
vide variety of physical charaaerlstics. ss measured
t^ standard and milltfi-y speciflcatioos. are given.
(Author)
Rubber and Elastomers
Institute of Rubber Research, U. of Akron, Ohio.
STRESS RELAXATION AND STRUCTURE OP HIOI
TEMPERATURE ELASTOMERS, by Maurice Morton,
V. R. AUen. and R. D. Gates. Technical rept. no. 6,
1 Sep-30 Nov 59, on Contract Nonr-2573(00). [1959]
Sip. 13 refs. AD-231 153.
Order from LC mi$3. 60. ph$9. 30 PB 150 491
The sol -gel reUtions were determined for different pri-
mary molecular weights of natural rubber. A low-
temperature, modified dlthio-carbomate -sulfur curing
system was used to reduce the uncertainty In the ob-
tained reUtions caused by degradation during the cure
period. It was found that no apprecuble degradation
occurs during the cure aitd extraaioo periods. Pair
agreement was obtained between the sol -gel reUtiooa
for the two types of vulcanizates, i. e. peroxide and
accelerated -sulfur. Based on these reUtions. the ratio
of the number of physical to chemical network chains
was determined as a funaioo of the printary molecuUr
weight. Excellent agreement was found between these
results and the ratio predicted from the sol versus
degradation study. It was propoeed that the presence
In the network of physical dwins due to entanglements
may have an effea on stress relaxation. Further, It
was considered how these enunglements could affea
both the rates and shape of the stress relaxation curves
To check for possible effects, measurements were
carried out with a very sensitive relaxometer. It was
found that no appreciable effea was observable, prob-
ably because of the more pronounced Influence of other
variables. Aging of Viton-A vulcanizates at 275°C indi-
cates that the degradative scission process which pre-
dominates during the first two hours of aging is later
overshadowed by a crosslinklng reaaion. 4-6-Butyi
thiophenol was used successfully to Inhibit this cross-
linking reaction. The latter reaction also occurs (as
would normally be expeaed) in the aging (at 200^0 of
samples of unvulcanized Viton A. (Autiior) (See also
PB 148 600)
Rock laUnd Arsenal Lab. ,111.
OZONE AGING OF POLYMERS, by Z. T. Otsefort.
Rept no. 3 on Aging of Vulcanized Rubbers. 5 Oa 49,
29p. 3 refs. RIA Lab. no. 49-1236; ATI-65 612.
Order from LC mi$2. 70, ph$4 . 80 PB 152 590
This report released for sale to the public 10 Nor 60.
An apparatus consisting of ozone generator, testing
chamber and measuring device for the ozone coocen-
tratioo, is described. Measurement of the effea of
ozooatioo on the various rubber specimens Is effeaed
by a decrease in modulus test. The cracking produced
by ooooe reduces the modulus of the test specimens
and thls.is used as a measure of the degree of ozona-
tion and, hence, can be used to measure the reaiatance
to ozone afforded by various protective coatinga. Pro-
tective coatings of neopreoe, polyisobutylene, pUollte
S* and Vanderbih BUckout BUck were found to be the
moat resistant to attack by ootone. Rubber compooenta
which are prepared for long term storage should be
stored, if possible, in an unstreased condition.
(Author)
MATHEMATICS *
Applied Mathematics and Statiatica Laba. , Stanford
A CLASS OF DYNAMIC GAMES, by WlllUm E. Trultt.
Technical rept. no. 19 oo C«»tract Nonr- 225(28)
4 Dec 59, 47p. 5 refa.
Order from LC mi$3. 30. ph$7. 80 PB 152 175
There U a large daas of business and military situa-
tions in which declaioos must be made oo the basis of
75
certain observed Irandom variables. When these situa-
tions are described as games they often bear a striking
resemblance to poker. A fixed- point method for the
solutions of games of this tvDC was proposed by Karlln
and Restrepo in [Annals of Mathematics Study no. 39
(1957). p 337-3631 ] One of their examples, knowii as
"le Her", indicated the applicability of the method to
games in which there is more than one relevant random
variable observed by each player. It is the purpose of
this paper to examine some further games In which mori
than one random variable is observed by each player ant
some of the randdn variables may be observed by both
players. Since the primary interest is in the method of
solution, poker models have been chosen to illustrate
the method becau«e at their familiarity.
athem^t
Applied Mathematics and Statistics Labs. , Sunford
A GENERAUZEd VOTING-GAME, by Marcel F.
Neuts. Technical rept. no. 21 on Cootraa Nonr-
225(28). 30Dec5>. 30p. 3 refs. AD- 230 318.
Order tr<xn LC m|$2.70, pi44.80 PB 152 177
A discussion is presented d a simple game over the
square, which serves as a model for many comDetltive
situatlaoa. ,
Applied Mathematics and Sutistics Lab. . Stanforxl U
Calif.
MEASUREMENT, EMHRICAL MBANINGFULNESS ANE
THREE -VALUED LOGIC, by Patrick Suppes. Technical
repc. DO. 20on Cottract Nonr-225(17). 29 Dec 58, 26p
13 refs.
Order from LC mll2. 70. ph$4. 80 PB 152 0S3
Applied Mathematics and Statistics Labs. . Stanford
U. . Calif.
THE SOLUTION C^ QUEUE ING AND INVENTORY
MODELS, by Augustus J. Fabens. Technical rqjt
na 20 on Omtract Nonr-225(28). 7Dec59, 33 p. 13ref8;
AD- 230 328. ^
Order from LC ml|3. 00. ph|6. 30 FB 152 176
An approach is investigated for queueing and Inventory
models which is baled on the theory of semi- Markov
processes. The nujthod Is applicable to a wide variety
of models in continuous pr discrete time. After 2 basic
theorems are developed, the Umiting distributions for
the models are determined by showing them all equiva-
lent to a batch service queue with Poisson Input and then
the latter is solved. Waiting time distributions and ex-
pected length <rf busy periods are shown for the queues
The application of tke mediod to finite queues Is indi-
cated. (Author).
Behavioral Sclencas Lab. . Wright Air Development
DIv. , Wrlgla-Flitterson AFa Ohio.
TABLES FOR MOODS DISTRIBUTION: FREE IWTBR-
VAL ESTIMATION TECHNIQUE FOR DIFFERENCES
BETWEEN TWO MEDIANS, by John H. Btjwen and Earl
D. Siarp. Repc. on Psychological Research on Human
Performance. May *), 23p. 4 refs. WADD Ifechnical
note 60-89.
Order from OTS |0,75 PB 171 078
The report presents tables which can be used to ofatah
fiducial probabilities and confidence Intervals for dif-
ferences between the medians of rwo populations. Alio
included are the formulae, as originally derived by
Mood, and an illustrative application of the technique
to experimental data which had been obtained by the
writers. (Author)
Colorado U. , Boulder.
CONVERGENCE REGIONS FOR CONTINU^D>RAC-
TIONS AND CERTAIN OTHER INFINITE PROCESSES,
by W. J. Thron. Rept. on Contract AF 49(638)100.
(I960] 34p. 34 refs. AFOSR-TN-60-1091; AD- 243 470
Order from LCml$3. 00, ph$6. 30 PB 152(^71*
Columbia U. , New York. ' '
EXTENSIONS OF SHEAVES OF ASSOCIATIVE
ALGEBRAS, by John W. Gray. Technical rept. no. 3
on Contraa Nonr- 266(57). Jan 60, 14p. 2 refs. CU-3-
60-ONR-266(57)-M; AD- 238 205.
Order from LC ml$2. 40. ph$3. 30 PB 148 063
Let X be a topological space. A a sheaf of associative
algebras over X, and A a sheaf of two-sided A-moduks
considered as a sheaf of algebras with trivial multipli-
cation. The group F(A A) of equivalence classes of
algebra extensions of 7\ with A as kernel has been
shown to occur naturally in an exact sequence
--►Hl(X. A)— F(A. A)-*Ext2(A A)— H^X. A)-»"
where H^X, A) denotes the Cech cohomology of X with
coefficients in A. The case in which A has a non-
trlvlal multiplication is discussed. Under appropriate
hypotheses P(A,A) is shown to occur in a similar exaa
sequence, except that in the other terms of the se-
quence, A must be replaced by the blcenter KiA) at A.
(Author) ^
Columbia U. (New York)
FIRST EMPTINESS OF TWO DAMS IN PARALLEL, bf
Joeeph M. Ganl. Rept. on Contract Nonr-266(59). 11959]
2lp. 5 refs. CU- 12-59 -Nonr- 266(59) MS; AD-228 114.
Order from LC mi$2. 70, phM- 80 PB 150 522
The probabilities are considered of first emptiness of
2 dams in parallel; both are subject to a steady release
at constant unit rate, and fed by a discrete additive in-
put process such that unit inputs are always directed to
the dam with lesser content. The problem is equivalent
to that of the single dam fed by 2 ordered inputs. A re-
currence relation for the probabilities of first emptiness
in this process is obtained. Equations for the generat-
ing functions of the probabilities ate derived, and a
formal solution to these is given. A more convenient
method of evaluating probabilities of first emptiness is
found by reducing the process to an associated occu-
pancy problem. The probabilities of first emptiness for
Poisson Inputs are then ahown to be dxalned by a rapk)
computational procedure. A general formulation is con-
cluded of the problem when the times of arrival for 2
ordered non -negative inputs of random sire form a
Poisson process. (Author)
76
-Nonr-
PB 150 521
OdumbU U. (New York]
UARKOV RENEWAL PROCESSES WITH FINITELY
MANY STATES, by Ron#ld Pyke. Rept. on Contract
Nonr-266(59). [1959] 43p. 11 refs. aJ-Il-59-Nonr-
266(59) MS; AD-228 117.
Order from LC mi$3. 30. ph$7. 80
Markov renewal processes having a finite number of
autes are studied. Explicit expressions are derived for
die distribution function^ of first passage times, as well
as for the marginal distribution function of the corre-
apoadli« semi -Markov process. Double generating func
tfonssre obtained for the distribution functions of the N,
processes. The limiting behaviour of a Markov renewal
process Is discussed; the sutionary probabilities being
derived completely. General Markov renewal processes
are introduced, and a related stationary process Is de-
termined. Several illustrative examples are given.
(Author)
Columbia U. , New York.
A NOTE ON SUFFICIENCY IN REGULAR MARKOV
CHAINS, by J. Ganl and B. R. Bhai(U. of California)
Rept. on Contract Nonr- 266(59). [1959] 13p. 4 refa.
CU- 14- 59- Nonr- 266(59JMS.
Order from LC mlJ2. ^. ph$3. 30 PB 152 106
The initial suie Eoc 1« random, and a slightly more gen-
eral result Is obtained for positively regular chains with
InitUl probabilities ^^(^) and transition probabilities
Pij(f^) (<.i,J-1.2 •). . ,
Columbia U. [New York]
ON THE NUMERICAL EVALUATION OF A CLASS
OF MULTIVARIATE NORMAL INTEGRALS, by
Harold Ruben. Rept. on Contraa Nonr -266(59). [1959]
14p. 10 refs. CU-13-59-Nonr-266(59)MS; AD-229 528.
Oitler from LC mi$2. 40, ph$3. 30 PB 152 100
An explicit formula is obulned for the probability that
each of n normally distributed and equally correlated
random variables with zero expectations and unit vari-
ances does not fall short of a given value h. The ratio
of the required probability to the density at the cut-off
point (h, h, . . ■ h) is expressed as a power series ex-
pansion ln>'[n/(l+(n-l)/>)l h, where /^ Is the common
correlation. The coefficients in the expansion involve
the geometrical nuxneots relative to the plane of sym-
metry A . of a regular (n-1) -dimensional spherical
simplex, with dihedral angles arc cos; ^,A being de-
fined as that plane through the centre of the hyperaphere
(on whose surface the simplex is located) which is
orthogonal to tlie line Joining the Utter point and the
centroid of the simplex. (Author)
Digital Computer Lab. . U. of Illinois. Urbana.
NUMERICAL QUADRATURE OVER A RECTANGULAR
DOMAIN IN TWO OR MORE DIMENSIONS IIL QUAD-
RATURE OF A HARMONIC INTEGRAND, by
J, C. P. Miller. Rept. on Contract Nonr- 1834(27).
11 Dec 59, 12p. Rept. na 95; AD-230 863.
Order from LC ml$2. 40, ph$3. 30 PB 152 109
Previoua notes have ahown that the error term la very
much reduced If the integrand f(x. y) Is a harmonic func-
tion, that l8,lf v^ - 0. In this note the case in which
high accuracy is attainable with few points is dlscusskd.
Expansions for n variables, and more extensive one*
for 2 variables are obtained. Special quadrature for-
mulae are obtained and considered, (Author)
DukeU. [Durham, N. C]
NUMERICAL VALUES OF SOME INTEGRALS IN-
VOLVING BESSEL FUNCTIONS, by D. L. George.
Rept. on Contract AF 18(600)1341. July 60. 29p. /
4 refs. AFOSR-TN-60-982: AD-243 143. (
Order from LC ml»2.70, p»i$4.80 PB 152 066
The object of the present paper is to make available
tablea of numerical values of the integrals S(v, n),
C(v,n) for the values: -
v*0, n»0,l;
v« 1, n • -l,0,l.
Analytical expressions for these integrals are derived.
DukeU. [Durham, N. C]
THE PERTURBATION OF GROUP REPRESENTATIONS
by R. T. Harris, Jr. Rept. on Contract AF 18(600)1341.
July 60, 17p. 10 refs. AFOSR-TN-60-983; AD-243 144.
Order from LC ml$2. 40. ph$3. 30 PB 152 067
An explicit method is given for the construction of uni-
tary equivalences for unitary rq)resenutlon8 of
abelian groupa having scalar spectral measures abso-
lutely continuous with respect to the Haar measure
over the dual grouf).
niinols U. , Urbana- .v^^».
THE ZEROS OF ENTIRE FUNCTIONS OF EXPONEN-
TIAL TYPE, by Paul Malliavln (Caen U. ) and
L A. Rubel. Rept. on Contract AF 49(638)517. 5 Aug 6a
44p. 25 refs. AFOSR-TN-60-910; AD-243 162.
Order from LC mi$3. 30, ph$7. 80 PB 150 883
In order that there exist a non- null entire function f(z)
of exponential type that vanishes on a given sequence
AQ' Al' Ao. . . • of poslUve real numbers and satisfies
|f<Iy)l ^ exp (nblyj) for all real y. It is necessary and
sufficient that there exist a constant K such that If x ^y
thei9»<y) - X(x) ilog (y/x)-»-K. where K(x) Is the sum of
the reciprocals of those ),„ **t ^° "** exceed x.
(Author). ^
Institute for Fluid Dynamics and Applied Mathe-
matics. U. of Maryland, College Park.
ON EXISTENCE, UNIQUENESS, AND NUMERICAL
EVALUATION OF SOLUTIONS OF ORDINARY AND
HYPERBOLIC DIFFERENTIAL EQUATIONS, by
J & Diaz. Rept. on Contract AF 49(638)228. Sep 60,
31p. 22 refs. Technical note BN-216; AFOSR-TN-60-
TN-60-1059; AD- 242 860.
Order fix>m LC ml$3. 00, ph$6. 30 PB 150 641
This is a detailed account of an invited lecture delivered
at die Sixth Conference of Arsenal Mathematicians,
held at Duke University, Durham, North Carolina,
June 1, 2. 1960. The general uniqueness theorem for
the hyperbolic partial differential equation Ujy-f(x,y,ii
proved in sectiwi 5, Is an exact analogue of die general
uniqueness theorem for the ordinary differential equa-
tion d^ -f (x.y) which is proved In section 4. (Author)
dx
77
Institute of Plight Structures, Columbia- U , New York
NUMERICAL EVALUATION OP CERTAIN INFINITE
INTEGRALS, by Sara R Boley. Technical rept. no 14
on Contract Nonr- 266(20). Oct 59. 9p. 4 refs. CU-14-
59-C»4R-266(20)-CE
Order from LC mlJliSO. ph$L 80 PB 150 993
It is the purpose of this note to present a modification
for the usual asymptcxic series ''*p«"TtCTi
Johns Hopkins U. , Bf itlmore, Md.
ON STABILITY IN THE LARGE FOR SYSTEMS OF
ORDINARY DIFFERgNTIAL EQUATIONS, by
Philip Hartmen. Technical note no. 17 on Contract
AF 18(603)41. June 60^ 20p. 10 refs. AFOSR-TN-60-
656.
Order from LC ml$2. |I0. phf3. 30 PB 150 646
■h
This paper is concern^ with questions of stability o*
systems of real dlfferfential equations x* « f(x) or
x' - f(t, x), where t 4 O and x is a point of a complete
Rlemannian manifold M". The central assumption is
that the Hermitian part |) ei^_|| " of the tensor e.L. -
m' 'u is negative dtfinitfe. If M" • E" Is Euclidean
ice, fhis means tha< the Hermitian part J" of the
Jacobian matrix J . ( A f/ ^ x) is negative definite.
g
Lincoln Ub. , Mass.! Inst, of Tech. . Lexliwton
COSET LEADERS, by, Everett C. Dftde. Rept. on Con-
tract AF 19(604)5200. ^4 Aw 60. lOp. 1 ref
55G-0027.
Order from LC ml^. $p, ph$I. 80 PB 150 509
Lincoln Lab. , Mass. j Inst, of Tech. . Lexington.
GALOIS OOHOMOLOGV OF CERTAIN MODULES
OVER FORMAL SERIES FIELDS, by Stephen S Shatz
Rept. on Contract AF 19(604)5200. 8 Sep 60. 33p.
9 refs. 3^-0013. '
Order frop* LC ml$3. ob. ph$6. 30
PB 150 951
The problem of finding jail cyclic p extensions of a field
k of characteristic p > 0 was essentially solved by E.
Witt in 1937 when he published his fundamental paper
en what are now knowfi as Witt Vectors. This re-
port gives a cohomological treatment of the problem,
and then uses some ne^ results of Tate (unpublished)
to obtain the chomology of a certain Galois Group
with coefficients in finite modules of p power order.
"f
Lincoln Lab. . Mass. In|f. of Tech. , Cambridge
STOCHASTIC APPROXIMATION AND "MINIMAX"
PROBLEMS, by L. A. Gardner, Jr. Rept. on Contract-
AF 19(604)5200. 11 Apr 60. 44p. 7 refs. Technical
rept. no. 219; AD-238 226.
Order from LC mi$3. 30, ph$7. 80 PB ISO 600
Feedback techniques are studied which automatically
adjust system parameters to achieve an ideal system
performance. The response of a system to unpredict-
able inputs is a statistical quantity whose behavior var-
ies with the values of the controllable parameters. A
criterion for optimum performance is formulated in
statistical terms. Minimum mean- square deviation of
output from zero and maximum average Output are con-
sidered. A procedure that makes system parameter
adiustments in accordance with responses at its cur-
rent parameter settings is called an adaptive process.
Such a procedure generates increasingly accurate es-
timates of the optimum parameter values as system
operation continues. A stochastic approximation pro-
cedure is investigated for estimating the minimum or
maximum of an extreme value function (and not a mean
value function). Probability one convergence of the
approximation is proved.
Minnesota U. [Minneapolis]. ,
SUMS ARISING IN THE THEORY OF MARKOV
CHAINS, by Steven Orey. Rept. on Contract
AF 49(638)617. 9 Aug 60, 16p. 6 refs. AFOSR-TN-60-
1067; AD- 243 767. . ,
Order from LCmi$2. 40, ph$3. 30 PB 152 289
A recurrent irreducible Markov chain with stationary
tranaitloo probabilities is considered. Questions of
convergence, absolute convergence and summabllity
are investigated.
Minnesota U. , Minneapolis.
THE WIENER HOPF EQUATION WHOSE KERNEL IS
A PROBABILITY DENSITY (II), by Frank Spltzer.
Technical rept. no. 1 on Contract Nonr-710(28). [195^
19p. 4 refs. AD- 229 646.
Order from LCml$2. 40, ph$3. 30 PB 152 106
StxMfy is continuing on the integral equation F(x) «
)^ Mx - y)F(y)dy, x > 0, where the known kernel
function k(x) is assumed to be an even pirobabillty den-
F(x) rr
sity. Tbe result of the equation lim
X-»QO
where
Uncoln Lab. , Mass. Inst, of Tech. , Cambridge. " J Ji^x)(ix may be infinite or finite, is strength-
ON-^iaJLsA^LU^ U^ THE CASE OF NON-BAND-
LIMITED FUNCTIONS, i by K. R. Johnson. Rept. on
Contraa AF 19(604)5200. 16 Feb 59. 25p. 2 refs.
Technical rept. no. 195J AD- 211 215.
Order from LC mi$2. 7(1 ph$4. 80 PB 147 588
A theoretical investigation is presenteJ trf the use erf
(sin x)/x sampling to represent a function f(t) having a
Fourier transform g^) such that for large |w| , Igj
and |dg/di*| tend to zeroes |AJ^al and |<u|-'»2, respec-
tively, when oj > 2. 02 >2. The uniformity of the con-
vergence of the representation as the number of sample
points increases is investigated. A rigorous proof of
the (sin x)/x sampling theorem for band-Umited con-
tinuous functions in Li ife presented. (Author)
ened concerning the asymptotic behavior of F(x).
Tauberian theorems are employed in a form which is
familiar in renewal theory.
NorthweatemTechnologlcal Inst.. Evanston, 111:
CHANCE CONSTRAINED PROGRAMS WITH NORMAL
DEVUTES AND UNEAR DECISION RULES, by
A. Charnes and W. W. Cooper (Carnegie Inst, of Tech. X
ONR Research memo. no. 28 on Temporal Planning and
Management Decision under Risk and Uncertainty, Con-
traa Nonr -1228(10) and Planning and Control of Indus-
trial Operations, Contraa Nonr-760(01). Nov 59. 20d
4 refs. AD-2ai 475.
Order from LC ml$2. 40, ph$3. 30 PB 150 482
78
A class of chance-constrained programming problems,
« f., those Involvlr^ linear decision rules in Indepeod-
eac normal varlates is discussed, and their direct I
equlralence to certain mathematical progranunlng prob-
lems is developed. The procedure elides, for this
class of problems, the 2- stage faaorization of Charnes,
A and Cooper, WW. ("Chance-constrained Program-
alng." Management Sd. 6, no. I. Oct. 1959). Pre-
ltinli«ry to the development of extensions of this pro-
cedure to other classes of varlates (or decision rules),
a ctaracterlratlon of distributions is obtained in terms
of their charaaerlstic (or moment -generating) func-
tioos. A simple way of evaluating alterations In quaUty
or risk faaors that enter into managerial decisions can
be effected for this class of problems. Analytical aids
•re suppU^ to management by tightening or relaxing
those parts of tie constraints while avoiding the twin
dUficulties that are associated with the ex ante ap-
oroacbes to these problems, e.g. , via subjective
probability or utiUty analyses. This either shifts the
burden of analysis onto management or requires
management to make preliminary Judgements in artifi-
dtlly simplified situations without being able to assess
Ihelr consequences for the problems that are aaually
cf Interest. (AiAhor)
Northwestern Technological Inst. . Evanston. 111.
THE DISTRIBUTION OF LINEAR COMBINATIONS OF
RANDOM DIVISIONS OF AN INTERVAL, by M. Dwass.
ONR Research memo. no. 21 on Temporal Planning and
Management Decisions under Risk and Uncertainty,
Cijntraa Nonr- 1228(10). Nov 59. 9p. 6 refs. AD-230351.
Onter from LCmi$l. 80. ph$ 1.80 PB 150481
Onsider n - 1 Independent random variables, each uni-
formly distributed over the interval {0, 1). The ordered
values. x.ix2i... .s^Xq. of these random variables
partition the unit interval Into n intervals of lengths Ui-
U2. . . . , Un The (Uil are dependent random variables
whowsumlsl. LetU(i)iU(2)i--^U(n)bethe
onlered values of the lengths Ui- In explicit form, the
probability laws are obtained of the random variables,
fa*l"l- ivi»>i"(i) <A"^'>
Northwestern Technological Inst. , Evanston, QL
RANDOM CROSSING OF CDF'S, by M. Dwass. ONR
Research memo, na 29 on Temporal Planning and
Management Decisions under Risk and Uncertainty,
Contract Nonr- 1228(10). Jan 60, 12p. 6 refs. i
AD- 237 865. ^
Order from LC mi$2. 40, ph$3. 30 PB 146 199
The following is proved: let Xj and Yj 1 ■ 1 n, be
2b independent random ▼arlables, each with the same
continuous c, d. f. . F(x). Let F. and Gi, J -n, denote
(be empirical c. d. f. "s ol the Xj" s andT/s, respec-
tlrely. Let P(n) be the number of times Fj equals F and
let (Xn) be the number of times F, equals G.. Then, as
■ -»•>. 11m PlP(n)/(2n)P <t] - Iftn P((J(n)/(4n)P <t] -
l-(l/lni2), where p - 1/2.
Northwestern U. , Evanstin. 111.
FLUCTUATION THEOR^POR INTEGER -VALUED
RANDOM VARIABLES, by Meyer Dwass. Rept. on
Contract AF 49(638)877. I Sep 60. 15p. 3 refs. AFOSR-
[TN)-60-1036; AD-243 194. ,„^-
Order from LC mi$2. 40. ph$3. 30 PB 150 652
If Xi Xn «re non-negative. Integer-valued and
Interchangeable random variables, then P(Sm< m, m«
1 N) » E(N-Sn)"*: This theorem is used to derive
the distributions of max (m - Sm) *nd max (Sm - nt).
m "^
(So - 0) where die maximum Is uken over 0, 1, . . . , N
or over 0. 1 ad inf. . Some of the results re<jiire
independence. Some applications are made to suprema
of Infinitely divisible processes. (Author)
Remington Rand Univac Div. , Sperry Rand Corp.
Philadelphia, Pa.
MINIMIZATION OF BOOLEAN FUNCTlONa Final rept.
on Contract AF [19X604)5228. Apr 60, 47p. 6 refs.
AFGRC-TR-60-156. _ .«,«.„
Order from LC ml$3. 30, ph^. 80 PB 152 049
This paper describes and compares two methods of re-
ducing a Boolean function to simplest normal form by a
computer. The two methods examined are (1) Celine's
method for obtaining the 'prime implicants. " followed by
Petrick's procedure for finding all Irredundant normal
equivalents, and (H) Urbano and Mueller's topological
method for determining the "essential stars, " followed
by Petrick's procedure for finding all irredundant normal
equivalents. The feasibility of programming die above
methods for the Air Force Cambridge computer is in-
vestigated, and several possible programs evaluated.
Five programs were developed which handle both method*
and extensions of these programs to handle more terms
or more variables, or both were evaluated. Thfe running
times of the two naethods were compared, and the possi-
bility of using criterU for comparison other dian running
time was investigated. (Author). .,
Syracuse U., N. Y.
INVERSE THEOREMS OF APPROXIMATION, by
G. G. Lorcnti. Technical rept. on Contraa
AF 49(638)619. 25 Sep 60, 17p. 8 refs. AFOSR-TR-
60-21. „ .c, -o-
Order from LC mi$2. 40, pl43. 30 PB 152 292
This paper contains several theorems which give a
lower estimate for the degree of apprradmation of
functions f of a given class by means of linear combl-
natloos P - ai gi^. . . . *. *n gn- The distance from f
to P Is measured in the C- and the L*- norm. (AKbor)
Therm Advanced Research. Ithaca, N. Y.
EXPRESSION AS A LEGENDRE FUNCTION, OF AN
ELLIPTIC INTEGRAL OCCURRING IN WING THEORY,
by B. O. U. Sonnerup. Rept on Contract Nonr-
2859(00). Nov 59. 18p. 6 refs. TAR-TN-59-1,
AD- 231 252. ..«.^
Order from LCml$2. 40, pl43. 30 PB 150466
79
■^
m.
An Integral that arises in potential theory is shown to be
related to half order Legeixlre funaions of the second
kind, including a special form at the integral studied by
Rlegels (Arch. Math. 2;117, 1949-59). Series expan-
sions of these Legendre function* for values of the argu
ment in the neighborhood at unify and much greater than
unity are also presented. Recursion formulas and ex-
presaioos in terma of elliptic integrals are noted.
(Author)
U. . cttroit,
Wayne State U. . Cbtroit. Mich.
DESCRIPTIVE CHAHACTERISnCS AND ORDER STA
TISnCS INFERENCE FOR A MODEL WITH REUA
HIUTY FUNCTION S»(t) - exp [1 - t
Andre G. Laurent. Technical rept. no,
Nbor-2575<00). 24 Mov 59, 26p. 3 r«f«
CWer from LC mitt. 70, phK 80-
- exp (- t )] by
6 on Contract
AI>^231 937.
PB 150 477
L*t 2? be a system vhose respoose to the cumulative
e«rea or the Increasing intensity X of a stimulus can be
described by the X-to-fallture probability distribution at
C; 1. e. the probability distribution F(X) al that Inten-
sity x of the stimulus which causes Cto fall. The sur-
vival function S»(X) • 1-F(X) is assumed to have, in
terms oT the reduced variable t, the analytical expres-
sion S*(X) -exp(l-fexp<-t)] where t-X/B*. The stim-
ulus X is called time or age; t or T is the reduced age;
S*(X) denotes the survival function; m*(XX the mortality
rate or fallture; e*(X) dw mortality density; E*. die
expectancy ofllfe at «»e X; and r»(X), the potential al
life at age X. (AuthokT
Wayne State U. , OQtrolt. Mich.
MINIMLM VARIANCE UNBIASED ESTIMl«rEa GEN-
ERALIZATION OF TTiCMPSON'S DISTRfiJUTION,
RANDOM ORTHONOFMAL BASES, by Andre G.
Laurent. Technical »ept. no. 5 on Contrapt Nbnr-
2575(00). 10 Nov 59, 34p. 1 ref. AD- 231 936.
Order from LC ml$3, 00. pfa|6. 30 PB 150 476
Wayne State U. , Datrolt. Mich.
ORDER STATISTICS AND STATISTICAL INFERENCE
FOR A MODEL WITH RELlABn^nT FUNCTION S(l)-
expfl* t-cxp(t)], by Andre G. Laurent. Technical rept.
no. 4 on Contract Now-2575<00). 1 Nov 59, 71p.
AD- 231 641.
CMmr frora LC mlK 50. ph$12. 30 PB 150 496
The present paper is devoted to the use of order sta-
tistics In problems of statistical inference that arise
under the assumption that the phencmem under study are
correctly represented by the RellaWllty Function S(t)-
«xp(l ♦ t - exp t], where t is a "reduced variable",
Wooda Hole Oceanographlc Inatltutlon, Mass.
ON THE THEORY OF CHARACTERICTICS, by
Robert McKelvey. Rept. on Contraa Nonr- 891(00).
Nov 59, 28p. 3ref8. Ref. no. 59-58; AD- 230 599.
a-der from LCmU2.70, p*44.80 PB ISO 514
In the theory of the profMigatlan of linear wavea. Im-
portance is attached to thoee surfacea In space-time
which can carry disccntlnultlea of the wavea. These
•urfacea are sublect to a flrat order non-linear partial
dlfterendal equation. The theory of this latter equatlca
is equivalent to a space-time geomfetrlcal optics for
the wave equation. Singularities of solution surfacea
are directly related to the geometrical concepta of
caustics and shadow zones. The theory of characteris-
tics for quasi- linear and non-linear first order paniti
differential equations is given, with special emphasis
upon the singularities of solution surfacea. (Author)
Computing Devices
Army Chemical Corps Engineering Command,
Army Chemical Center. Md.
PERT: PROGRAM EVALUATION AND REVIEW TECH-
NIQUE FOR THE ROYAL McBEE LGP-30 COMPUTEIL
>ily 60, 90p. Engineering Command rept. ENCR no. 45.
Order from LC mlK 80, ph$13. 80 PB 150 992
Thle report contains the results of a study undertaken
to convert the Booz- Allen- Hamilton Program Evalua-
tion and Review Technique (PERT) for small scale ap-
plications to the Royal Mcfiee LGP-30 compter. The
report contalna presentations on the program function
and capabilities, operating instructions, LGP-30 flow
chart, symbolic and ftiachlne langiuge codes, data in-
put error check list, dau tablea and LGP-30 sub- rou-
tine and dau table aaaembly. (Author).
Computation Lab. , Harvard U. , Cambridge. Mass.
DESIGN AND OPERATION OF DiGITAL CALCULAT-
ING MACHINERY, by Howard Aiken. Pinal rept. on
Contraa AF 19(604)4947. 1 Dec 59, 123p. AFCRC
TTl-60-119; AD- 234 295.
Order from LC ml$6. 30. ph$19. 80 PB 148 259
■!
Contents:
httem recognition using correlation
Some aids to the evaluation of a certain Integral
Beam sweep matrix computations
Aerodynamic origin of magnus moment '^
(See also PB 143 026)
Cornell Aeronautical Lab. . Inc. , Buffalo, N. Y.
CONTRIBUnONS TO PERCEPTRON TOEORY. by
R. Dsvld jMeph. Rept. on Pro]. Plara. Contract Nonr-
2381(00). 15>ine60, 108p. 6 refs. Rept. no. VG-1196'
0-7.
Order frona OTS $2. SO PB 171 093
Farcepcrons are a class of faratai models which have
bsen faitroduced in previous reports. There are several
ways hi which an analysis of a perceptron's ability to
associate responses with stimuli may proceed. One ap-
proach Is to place a distribution over die members of
a subclass (In a specific manner) and then to analyze
statistically the ability of a randomly chosen manber of
the subclass to perform a given task. A second approach
considers the "aptlmum" characteristics for the com-
pooents for perceptnns subject to a given set of con -
stralncc, and "optimum" operating procedures for
flvea subclasses of perceptrons. Until this past year,
almost all the analytic wort done on perceptnns has
foUowed the first approach. Quite recently, some
poiwerful results for the second approach have been ob-
igjaed Ibr a subclass of perceptrons called simple
o^fceptrons. The purpose of this report is to present
^ rigorous analyses of tl*e first type which have been
gtosined, to display the techniques which have thus far
proyed useful, and to give some additional results of
the second type.
Cornell Aeronautical Lab. , Inc. , Buffalo, N. Y.
TABLES OF Q- FUNCTIONS FOR TWO PERCEFTRON
IIOOeLS. by Frank RoeenbUa. Rept. on Pro] . Para,
Oootract Nonr- 2381(00). May 60. 144p. 4 refs. Rept.
BO. VG-1196-G-6.
Order from OTS $2.75
PB 171 092
]
80
^l
This volume contalna four sets of tablea for Q-func-
tioas. These functions have been found to be easentlal
la many quantitative analyaea of perceptrona, and naay
also be of more general Interest, since they Include
oanulatlve probability distributions for differences of
Itoomial and Polsson distributed random variablea.
David Samoff Research Center, Princeton. N. J.
AN INTEGRATED BINARY ADC«R, by M. E. Szekely.
S. M. Marcus and J. T. Wallmark. Scientific rept.
so. 3 on Integrated Semiconductor Device Studies,
Oniraa AF 19(604)5561. 15 Aug 60, 20p. 4 refs.
APCRL-TN-60-955.
Order from LC ml$2. 40. ph$3. 30 PB 152 045
Thli article describes an integrated binary full adder
which uses as its aalve and passive elements unipolar
field-effect transistors. A binary full adder is a com-
puter circuit that adds three binary numbers, X, Y and
a carry from a previous stage, C, giving two outputs,
one for the sum and one for the carry to the next stage
Bach one of these binary numbers may be 0 or 1 cor-
responding to eight posaible combinations as shown by
die eight columns of the truth-table in Fig. 1. The de-
sign will be developed in terms of conventional cir-
cuitry, and then extended to an integrated module. The
active element used throughout the adder Is the uni-
polar field-effea transistor (UT) the operation of
wUch la described. Tlie only passive elements used
are resistOTS which are also in the form of unipolar
traaalstors. The logic concept used is direct -coupled
tmlpolar transistor logic (DCUTL) which is also
dsscribed. (Author)
Electrical Engineering Research Lab. , U. of Texas,
Austin.
AN ANALOG CORRELATION COMPUTER, by
C B. McCullough. Rept. on Contract AF 19(604)2249.
1 Aug 60, 57p. 12 refs. Rept. no. 6-37; ERD-TN-
60-783.
Order fnjm LC ml$3. 60, ph$9. 30 PB 150 649
This study describes a correlation computer designed
to be compatible with the equipment which Is presently
being used for data handling. The computer otxalns its
input from magnetic tape, and since the time functions
to be analyzed »re recorded directly on magnetic tape,
correlation analyses may be performed using a mini-
mum of manual or automatic transcription processes.
■Rme functions from a few seconds to several hours In
Ifliytfa may be analyzed. Included also is a discussion
I
at the dieory Involved In correlation analysis, a de-
scription of the operation of the computer, and several
examples of auto-correlation and cross -correlation
analyses which have been performed with this computer.
(Author)
Hermes Electronics Co. , Cambridge, Mass.
DEVELOPMENT OF A MAJORITY GATE FOR IM-
PROVING DIGITAL SYSTEM RELIABILITY, by
R. Waaserman. Rept. on Contraa Nonr -21 33(00).
2 Nov 59, 51p. PubUcation no. M-809; AD- 229 364.
Order from LCmi$3. 60. ph$9. 30 PB 150 484
Efforta were made to develop logical design procedure
for the efficient use of redundancy In improving the re-
Uablllty of digital systems. This called for the develop-
ment of a highly reliable, aimple constructed, majority
gate. Requirements and design considerations are pre-
sented for the majority gate using magnetic cores aa
logical building blocka. Logical deaign principlea are
presented for the shift register, dynamic flip-flop, logi-
cal gate functions, binary counter, comparator, and two
input full adder. The 6- core majority gate module and
the 9-core majority gate module are diacussod.
Institute for Systems Research, U. of Chicago. HI. .
TESTING CONTINUOUS OpMPUTERS, ed. by
R. C. Mikullch. Rept. on Analysis of Continuous Com-
puters for Flight Simulation, Contraa AF 33(616)2797.
Fd> 58, 208p. 18 ref a. WADC Technical rept. 57-622.
Ortler from OTS $3.50 PB 171 080
A program was Initiated to deaign and develop perform-
ance tests for continuous computers. Such tests neces-
sitated investigation of actual operations of continuous
computers and previously developed error theories. A
mathematical theory of testing continuous computers
is given and the differencea between component and
aystem testing are delineated. An appropriate compo-
nent test program, with Interprewtion and analysis, is
proposed. The use and application of system testing la
then discussed and criteria for the selection of test
proWems, their running, and subsequent analysis are
established. One chapter Is devoted to the operational
aspects of a computer. Including quantlMtive measures
of repeatability and reliability and qualitative dlacua-
slons of recordablllty. adaptability, and convenience.
(Author)
Laboratory for Electronics, Inc. , Boston, Mass.
RESEARCH IN FERR0MAC2«(ETICS. Annual rept. for
1 Sep 58-31 Aug 59 on Contract Nonr-26 76(00). [1959]
89p. 20 refs. Rept. no. 570- Al; AD- 240 322.
Order from LC mlH », ph$l3. 80 PB 149 593
Eaqierlments performed on two films of different Iron-
nlckel composition showed diat a do^hi wall can be
moved controlledly in a film made from a melt whoae
composition Is In the vicinity of 80-20 Nl-Fe. The field
required for domain waU nucleatlon is 25% greater than
die field to move a wall in a permalloy film. Equipment
for making measurements of the properties of interest
in the investigation of thin magnetic films is described.
Simple Bloch and N^el walls are treated by a metiiod
utilizing charged aheeta. For a permalloy film It Is
ahowji that a Bloch to Nfel tranaiilon occdrs at about
81
250 A. Independent at the fllni's •nlaocrapy and dMt the
w»ll energies are piimarlly by exchange and magneto-
natlc effects. The theory of these walls la applied to a
coercive force calculation. The complex croas-tie wall
la analyzed. Three niodela introduced for calculation
purpoaes are traated. The chain of ellipaoida model in-
dicates that the •rlgln at the wall lies in magnetoatatlc
Inieractlona. The other two models attempt to show how
the magnetic Interaction produces the cross tie. Utiliz-
ing these interactions the cross- tie dlmensioaa are de-
termined. Sevenal Bitter pattern experlmenta are exam-
inad. (Author).
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
APPLICATIONS OF BOOLEAN MATRICES TO THE
ANALYSIS OF FLOW DIAGRAMS, by R. T. Proaaer
Rept. on Contra<it AF 19(604)5200. 22 Jan 60. lip.
15 refa. Technical rept. no. 217; AD-234 081.
Order from LC r$ii$2. 40. ph$3, 30 PB 150 599
^ analysla at th^ stnicture at flow diagrams such as
those associated Mfith computing machine programa.
can be given in tfrms of Boolean matrices. A pair at
Boolean matricea is associated with each diagram. The
first of these, called the connectivity matrix, contains
die topological sQructure of the diagram, and the
second, called the precedence matrix, conuins its pre-
cedence relations. Elementary computations on these
njatriccs are ahcmm to yield detailed information con-
cerning the Internal logical consistency of the flow dia-
gram. Possible applications to autbmatic compiling and
debugging proc Mures are suggested. (Autlior)
Lincoln Lab. , Mass Inst, of Tech. , Lexington.
THE CALL ISCOPE: A VERSATILE ALPHANUMERIC
DISPLAY. byK. E. Perry and E. J. Aho. Rept. on Con-
tract AP 19(604)1200. 43 Nov 59, 18p. I ref. Technical
rept. no. 212; AO-232 164.
Order from LC mi$2. 40, ph$3. 30 PB 150 598
The calliscope is a digitally controlled alphanumeric
and graph display intended for preaenutlon of output
dau from a digital computer. Tills display employs a
magnetically focused and deflected cathode-ray tube.
Spot positioning is accomplished by digital switching of
high currents thrtiugh a low -Inductance yoke. Settling
time is 20 ^sec. Alphanumeric symbols are generated
by a calligraphic or spot writing method which synthe-
sizes the X and Y current waveforma necessary to con-
trol the motion of the spot. (Author)
major periodicals In the computing field. Detailed
training courses in the use of particular machines an
offered by various universities and also by the
manufacturers.
Lincoln Lab. , Mass. Inst, of Tech., Lexington.
AN INTRODUCTION TO DIGITAL COMPUTING, by
Bert F. Green, Jr. Rept. on Contract AF 19(604)5200.
18 Aug 60, 46p. Ul refa. 58 G- 0011.
Order from OTS $1.25 PB 171 100
Thla article {s-ovldea an introductory description of
electronic digital computers and a preliminary guide
to programming. It also briefly surveys the uses
psychologists have found for computers, and lists
some of the praalcal Issues involved in using digital
computers. For those wishing additional information,
the bibUograpfay Usts several texts, and notes the
Lincoln Lab. , Mass. Inst, of Ttech. , Lexington.
A 6- SYMBOL 7 -STATE UNIVERSAL TURING MA-
CHINE, by Marvin Minsky. Rept. on Contract
AF 19(604)5200. 17 Aug 60. 8p. 4 refs. 54G-0027.
Order from LC mill. 80, pfa$l. 80 PB 150 508
Moore School of Electrical Engineering, U. of
Pennsylvania, Philadelphia.
JiSFRUCnON BOOK. TYPHOON RESOLVERS, 1, 2,
3. 4. Rept. on Contract N383s-80094(02). 1 Apr S3.
47p. Research Dlv. rept. no. 53-33.
Order from LC ail$3. 30. pfa$7. 80 PB 152 651
TUs reoort relessed for sale to the public 9 Nov 60.
National Bureau of Standarda [Waahlngton. D. C. )
DESIGN AND C»ERATICW OF THE CElLCMwIETBR
COMPUTER, by Paul Meissner. Oct 60, 77p. Tech-
nical note 64.
Order from OTS $2.00 PB 161 Stf
The ceilometer computer has been developed to pro-
vide a diaplay and electrical readout of cloud-height
information for use with an automatic weather statioi.
The computer receives an analog signal from the
dMector of a rotating- beam ceilometer, and deter -
nunea the height at which cloud indicatlona occur. A
small magnetic storage drum conuins ten minutes of
cloud- height information which is continuously up-
dated, and these dau are analyzed for the following
factors: (1) Predominant cloud height over the past ta
minutes, (2) Maximum and minimum height at which
significant cloud occurrences were observed, (3) Num-
ber of cloud observations up to a selected critical
altitude. The computer is a wired-program machine
constructed of transistorized plug-in packages. Sev-
eral modea of manual operation have been incorpo-
rated for testing and maintenance purposea. (Author)
Remington Rand Unlvac Dlv. , S|;>erry Rand Corp. .
RiiladelphU. Pa.
COMPUTER- C« VICE APPLICATIONS OF THIN FER-
ROMAGNETIC PILMSl Final engineerii^ rept. for
15 Mar 59-15 May 60. on Contract AF 19(604)5506.
May 60, 30p. AFCRC TR-60-160.
Order from LC ml$2. 70. phK 80 PB 150 767
Thia report describes the results of a study of the
application of thin ferromagnetic films to computers.
Anisotropic, 'double threshold. " and "rotating anlsot-
ropfay" films were considered for use as logic and
memory devices. A plausible explanation of the unique
properties of double threshold and routing anisotropby
films It given in terms of domain walls and impurity
atom diffusion. Two NDRO memory devices using
double threshold and rotating anlsotropy films are de-
scribed. An "and" gate, an "exclusive or" gate, and
three types of full adder using thin films are described
82
An "and" gate, an "exclusive or" gate, and a NDRO
memory element using double threshold films were
ccnstructed and evaluated. (Author)
Rome Air Development Center. Griffiss AFB, N. Y.»
PRELIMINARY STUDY OF THE PROBABILISTIC BE-
HAVIOR OF A DIGITAL NETWORK MAPRITT DE-
QSKXi ELEMENTS, by Saburo Muroga. Aug 60, 15p.
Iref. RADCTN-60-146.
Order from LC ml$2. 40. ph$3. 30 PB 150 973
A maiorlty decision element is an element in which a
finite number of inputs are coupled with one output.
The output value is one or zero, depending on the in-
put values. An advantage of elements of this sort is
that a single element can represent a fairly complex
function. Consequently, the network for a given func-
don can be represented with few elements-. In addition,
a highly reliable network can be constructed with un-
reliable elements. This rqx>rt discusses the probabi-
listic behavior of a network of elements characterized
by a majority decision principle. (Author).
I
MECHANICS
j Fritz Engineering Lab. , Lehigh U. , Bethlehem, Pa.
IJTERATURE SURVEY ON THE ANALYSIS AND
DESIGN OF RESTRAINED COLUMNS, by Morris
Ojalvo. Rept. on Welded Continuous Frames and
Their Components, Contraa Nonr-610(03). Dec 59,
34p. 38 refs. Fritz Lab. rept. no. 278.1; AD- 233 729.
Order from LC ml$3.00. pfa$6.30 F6 152 143
The present report will concern Itself only with refer-
ences that consider failure by excessive bending about
one of the principal axes of the column section. It also
will be assumed that the column ends do not translate
and that the columns are not loaded or restrained ex-
cept at their ends. In spite of these restrictions on the
scope of the investigation, the type of column consid-
ered often occurs in tier building design when the col-
umns are clad in a manner that precludes failure by
lateral-tor sional buckling or when columns are of a cross
section having a high torsional rigidity (box and annular
ssctlonB). This investigation is concerned with the be-
havior of columns up to the ultimate carrying capacity in-
cluding effects of partial plastification. (Author)
Institute of Engineering Research. U. of California.
Berkeley.
AXISYMMETRIC VIBRATIONS OF SHALLOW
ELASTIC SPHERICAL SHELLS, by A. Kalnins and
P. M. Naghdi. Technical rept. no. 6 on Contract
Nonr-222(69). Nov 59, I8p. 8 refs. Series no. 131.
laaue no. 6; AD-230 120.
Order from LC ml$2. 40. ph$3. 30 PB 150 524
An exact solution within the scope of the bending theory
ctf shells is given for axisymmetric vibrations of thin
shallow elaatlc spherical ahells. ^>eclfically, the
solution is applied to an investigation of the natural
frequencies of the free axisymmetric vibrations of
spherical shell segments with various edge conditions.
Comparison is drawn with previously known results
(or transverse vibrations of shallow spherical shells,
where the effect of longitudinal Inertia is ^eglected.
(Author). , ,
Mlnnesou U. , Mlnneapolla.
EFFECT OF VISCOELASTIC FOUNDATION ON
FORCED VIBRATION OF LOADED RECTANGULAR
PLATES, by C. T. Hsu, C. W. Chu, and C. C. Chang.
Rept. for May 58- June 59 on Meullic Materials, Con-
tract AF 33(616)6828. July 60. 23p. 8 refs. WADD
Technical rept.t60-360.
Order from OTS $0. 75 PB 171 071
Farced vibration of a loaded rectangular plate with
visco-elastic foundation is treated. Two types of
viaco-elastic material are considered, Kelvin-Vcrfgt
solid and Boltzmann model. Analytic solutions are
given for the plate subject to compression and a
periodic transverse pressure. A numerical example
is worked out for the case of Kelvin-Voigt solid. Some
features revealed by the example are (a) With visco-
elastic effect, the natural vibration damps out rapidly,
(b) There exists a critical damping factor U/^ . For
Vf ^ ^.tbe damping is oscillatory; otherwlae the
damping Is monotonic. (c) The closer ^ is to H ^n
ma^tude, the faster the dam^irihg. (d) The time re-
quired for damping is almost independent ctf the fre-
quency of the periodic loading, (e) The greater the
viscosity coefficient/^, the smaller the anplitude of
vibration. The above statement is obtained from pre-
liminary compuutions. Further work haa to be done
before conclusive summary can be made. (Author)
Mlnnesou U., Mlnneapolla.
QUASI-ORTHOGONAL MOOTS OF DYNAMICAL SYS-
TEMS, by Lawrence E. Goodman and Yellappa C. Das.
Rept. for Jan-July 59 on Metallic Materials, Contraa
AF 33(616)6828. Aug 60, 58p. 6 refa. WADD Tech-
nical rept. 60-306.
Order from OTS $1.50 PB 171 070
When energy dissipating devices are inserted at the
boundaries the analysis of structural vibration firob-
lems becomes difficult. The usual classical methods
in such cases yield an infinite set of equations for the
coefficients of a modal expansion of the solution. The
method developed In this report, gives a finite equation
for each coefficient of the modal expansion and thus
makes it possible to obtain solutions for structural
vibration problems with boundary conditions involving
the time derivatives. The structural vibration problem
treated is identicsl with that of the tranaient analysis
of electrical circuits having distributed capacity and
inductance and terminated by a lumped resisunce.
Certain problems in heat conduction also fall within
the scope of the method developed. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
ON THE CREEP- STRESS ANALYSIS OF SCHVffi STRUC
TURES, by Sharad A. Patel and B. Venkatraman. Rept.
on Conyracta AF 49(638)302 and [Nonr- 839(23)]. June 60.
40p. 8 refs. PIBAL rept. no. 560; AFOSR-TN-60-836;
AD-242 414.
Order from LC ml$3. 00, pb$6. 30 PB 150 416
The present paper considers the analyaia of aome struc-
tures in which the deformations are caused exclusively
by ci'eep. The paper begins with a discussion of a uni-
axial cre^ law and its generalizations for the analyaes
of problems in a trlaxlal sute of stress. Moment-curva-
ture relationa are then develnoed from these Uws for
83
problema in bending: and an elementary device for the
Inclusion of compretsihillty effects in creep is briefly
discussed. With these as basis, the particular problems
considered are, the bending at thin- walled beams, the
bending of annular plates, and the stress distribution in
a compreaslble sphere. In analysing these problems,
use has been made of the elastic analogue. Further, in
some cases , the similarity of creep to plasticity has
also been used. In all cases, closed form solutions have
been presented. (AiftK>r)
Watertown Arsenal Labs. , Mass.
ON THE BASIC THEORY OF THW CYLINDRICAL
SHELLS, by Oscar L- Bowie. Rept. on Materials for
Ughnreight Conatruaion. Sep 60. 25p. 3 refa. Tech-
nics! rept. no. WAL TR 893. 3/3.
Order from LC ml$2.70, pli$4.80 PB 149 295
A three-dimensioaal solution for cyllndrlcsl sbella is
considered and sets at solutions satisfying the exact
equilibrium equations are generated. Systematic pro-
cedures for effectively apprcadmating the boundary
conditions are derived. Thus, using this approach,
conventional thin shell solutions can be extended to
moderately thick shells. The solution is carried out
numerically for the ease at bending monnents acting on
the ends at a cylinder. (Author)
Awodynamtp and Pneumatics
Air Force Missile DevelopoMnt Center. HoUoawn
AFB, N. Mex.
DEVELOPMENT OF THE NATION'S LEADING
TEST-TRACK FACTUTY 1956-1960. VOLUME U.
HISTORY OF TRACKS AND TRACK TESTING 1949-
1960 AT THE AIR FORCE MISSILE DEVELOP-
MENT CENTER, HOLLOMAN AIR FORCE BASE,
NEW KfOSXICO, by David BushneU. [1960] 171p.
241 refs. AD- 240 889
Order from LC mi^A. 10, pfa$27. 30 FB 152 802-2
This report released for sale to tbe public 18 Nov 60.
The present volume, the second at the pianrwrf three-
volume series on tracks and track testing. Is prlma-
rliy a documented account d the developnient at
HoUoman's major tr$ck fadUty. although It includes
informatlan related to advances In the state at the art.
In addition to covering the physical evolution at the
track itself, the volume discusses the parallel prob-
lems and accomplishments since 1956 of AFMDC's
track organization. 1» sled design sad development,
Inatrumeixation and Related fields.
Air Force Miaalle Oevelopment Center, HoUoman
AFB, N. Ilex.
ORIGIN AND OPERATION OF THE FIRST HOLLO-
MAN TRACK. VOLUME I. HISTORY CP TRACKS
AND TRACK TESTING AT THE AIR FORCE MIS-
SELS DEVELOPMENT CENTER, HOLLOMAN AIR
PORCE BASE, NEW MEXICO, 1949-1956, by David
Buahnell. [1959} 134p. 195 refa. AD- 231 907.
Order from LC ml$6.90, pfa$21. 30 FB 152 802-1
Ttala report released for aale to the pubUc 18 Nov 60.
Contents:
Origin at the Holloman high-speed track
Beginnings of track testing
Planning and construction of the original Holloman
track
Military hardware on the 3550 ft track. 1950-1956
The Snark program on the HoUoman track (June 1950-
Marcb 1952)
Project Sleighrldc (March 1952- February 1954)
Q-2 acceleration tests (September -October 1952)
0Q-I9 launchings (December 1952-February 1955)
MX- 1601, Jet vane control tests (February 1953-
September 1954)
Matador recovery system tests Ouly 1953-March
1956)
B-58 flutter model testing Ouly 1954-March 1955)
Acceleration tests, flight control components
Ouuary-March 1955)
Aeromedlcal experiments on the Holioman track:
1953-1956
Track administration and development
Admlnistratloo of the Holloman high- speed track
The development of Sleran
Projea 6876, track facility development
Allied Research Associates, Boston, Mass.
NONSTEADY INCOMPRESSIBLE HEAT TRANSFER
FOR ARBITRATY BODIES AND ALL PRANDTL NUM-
BERS, by Theorore R. Goodman. Rept. on Contract
A F 49(638)839. 1 Sep 60, 27p. 14 refs. APOSR-
TN-60-843. AD- 242 475.
Order from LC ml$2, 70, phH 80 PB 150 634
The title problem is solved using an Integral method,
and Ignoring viscous dissipation. A partial differential
equation is derived which yields as special cases Llght-
hlll's non-unfform heat transfer formula and the non-
steady heat conduction In a slab. The differential equa-
tion Is then specialized to the nonsteady but imiform heal
transfer on a flat plate. Comparisons with other solu-
tions are made when available, and it is shown that the
integral method produces accuracy of a few percent In
these limiting cases. Finally, the heat transfer formula
which has been derived is used to calculate the temper-
atures in a thin skin subject to a Jump In external veloc-
ity. (Author)
Army Chemical Research and Developraem Labs. ,
Army Chemical Center, Md.
GENERAL EQUATION FOR TERMINAL VELOCITY
OF FREE -FALLING SPHERICAL C»OPS FOR SOLU-
TIOH ON AN ELECTRONIC COMPUTER, by Fritz A.
Hedman and Richard L. Campbell. July 60, 14p.
5 refs. Technical rept. CRDLR 3000; AD- 240 483.
Order from LCm42.40| pb|3. 30 FB 150 100
An empirical equation, easily differentiated and suita-
ble for use with electronic computers, has been de-
rived that gives the terminal velocities of spherical
dropa having diameters in the rsnge of 3fLto more
than SSOOu. The derivation of the equation made use
of equatloas by Stokea and Newton. (Author)
84
Arnold Engineering Development Center (Tullahoma,
Tenn.)
A MINIATURE WAf'ER- STYLE PRESSURE TRANS-
DUCER, by W. Ei. Smotherman. Rept. on ARO, Inc.
Contract AF 40(000)800 S/A 11(60-110). Oct 60, 34p.
2refs. AEDC-TR-60-11.
Order from OTS J 1.00 PB 171 104
Design, operating theory, and performance character-
istics of a newly developed variable reluctance differ-
encial pressure transducer, the wafer gage, are de-
icrlbed. This transducer wss designed for use prima-
rily in the arc-heated, Hotshot type, hyperveloclty
wind tunnels at the Arnold Engineering Development
Center. The wafer gage provides a series of pressure
ranges from 0-0. 5 to 0-5. 0 psid by means of Inter-
changeable diaphragms. Although 0-0. 5 psld is the
kwest range specified for the wsfer gage. It Is fre-
quently calibrated for full scale output at 0. 01 psid,
and pressure differentials of 30 microns of mercury
can be resolved. Because of the convenient wafer
riiape and the miniature size of this transducer, it may
be used in nrumy sppllcations where larger transducers
are not feasible. (Author)
Cornell Aeronauticsl Lab. , Inc. , Buffalo, NY.
ON THE UNIQUENESS OF SOLUTIONS FOR PAS-
SAGE OF SHOCK WAVES THROUGH DUCTS OF
VARIABLE CROSS SECTION, by George Rudinger.
Rept. on Project Squid, Contract Nonr* 1858(25).
Nov 59, 30p. 10 refs. Technical rept. CAL-79-P.
Order from LCmi$ 2.70, ph$4. 80 PB 150 531
If shock waves strong enough to produce supersonic
fkw psss through a duct of variable cross section, the
shape of which Is approximated by a single discontinu-
ous area change, s variety of wave patterns may be
found. These are unique for particular conditions ex-
cept for a range of area convergence for which it was
recently shown that three solutions exist. Examination
of the transient processes that precede the establish-
ment of the final flow suggests, and a general proof
confirms, that only one of these solutions can actually
be reaUzed if the duct converges monotonically. For
mere general duct configurations, the other solutions
mty also he found, but the correct wave pattern nruty
have to be established with the aid of a wave diagram
in which area changes are proper lyTiken into account.
For configurations with a throat, additional wave
patterns may appear both within and outside of the
region of ambiguity which then loses its significance.
(Author) ,
}■
Cornell U. Graduate School of Aeronautical Engi-
neering, Ithaca, NY. ,
ANALYTIC SOLUTICWS FOR THE SURFACE TEM-
PERATURES DUE TO AERODYNAMIC HEATING, by
Alvln L. KaskeK Rept. on Contraa AF 49(638)544.
June 59, 68p. 22 refs. [AFOSR] TN-60-643.
Order tram LC mi$3. 90, ph$10. 80 PB 150 621
The transform procedures of operstional calculus are
used to obtain analytical solutions for the surface tem-
peratures of a solid- symmetric airfcdl at zero angle of
tttack, when the heat transfer coefficient and the re-
covery temperature of the fluid through which the wing
is moving can be expressed by polynomials, exponen-
tials, the product of polynomials and exponentiala or
the sum of polynomials and exponentials. The solution
for the surface temperature of a hollow wing in which
the inner surface of the wing is insulated is also in-
cluded, along with an approximate solution for the sur-
fsce temperatures of the solid wing at small angles of
attack. The transform procedures are applied to a set
of simultaneous Integral equations for the upper and
lower surface temperatures of the wing. These equa-
tions sre obtained by making a heat balance between
the heat inflow to the wing from aerodynamic heating
and the internal temperature gradients at the upper and
lower surfaces of the wing. The temperature gradients
are obtained from Fourier's one dimensional heat flow
equation by using the principle of superposition and
Duhamel's integral to find the temperature distribution
inside the wing due to the application of an arbitrary
upper and lower surface temperature. For conven-
ience, a special approximation Is made to the exact
solution for the hollow wing and an example is worked
out to show the results that can be expected by using
this approximation. The results sre compared with an
existing exact solution for the hollow wing with the
inner surface Insulated. (Author)
Cornell U. Graduate School of Aeronautical Engineer-
ing, Ithaca, fl. Y.
UNSTEADY MAGNETOHYDRODYNAMIC FLOW ABOUT
THIN AIRFOILS, by Leon E. Ring. Rept. on Contract
AF 49(638)544. June 60. 152p. 24 refs. [AFOSR] TN-
60-638; AD-243 016.
Order from LC mi$7. Sa ph$24. 30 PB 150 620
The theory is developed for the magneiohydrodynamic
flow erf an incompressible fluid about thin airfoils in non -
uniform motion. A uniform nnagnetic field Is applied
parallel to the free stream and solutions are obuined sub-
ject to the restriction of small perturbations. The ef-
fects of viscosity are included, for the most part, only
through the application of the usual Kutta condition for
lifting airfoils. The general character of the flow is
discussed at lei^:th. The validity and range of applica-
bility of the infinite -ccHiductivity and moderate -conduc-
tivity theories are determined on the basis of an order-
of -magnitude analysis. The flow -field for infinite con-
ductivity is changed from the non -magnetic case only
through the new transport speed <rf vorticlty; the forces
on the airfoil are changed due to surface currents, ior
the case of the Alfven speed less than the free-stream
speed, the airfoil lift and pitching moment are given in
integi«l form for general unsteady-airfoil motion and
are given in closed form for harmonic oscillations. The
forces St moderste frequencies are found to be larger
than the corresponding non-magnetic case. The re-
sponse to a unit step -function change in the downwash
is studied and the asymptotic form of the lift is c^-
tained for small and large time. Using the Oseen ap-
proximation, a set of singular solutions with arbitrary
conductivity and pnagnetic field strength are obuined
for harmonic oscillations. Limiting forms of these
sii^iar solutions are given for low conductivity and
for low frequencies. Using these solutions, integral
equations are formulated for the case of an oscillating
airfoil, which may be a conductor or an Insulator.
(Author^
85
Diamond Ordnance Fuze Laba. , Washlngtod, D. C
A HKjH-ALTmjrm ALTIMETER, by Arthur O.
Morse and Harvey M. Nilson. 15 June 60, 34p. 5 refa.
TR-623.
Order from LC ml$3. 00. ph$6. 30 PB 152 312
An altimeter systfm capable of providing accurate re-
entry altitude dat4 in multiples of 5000 ft has been
deslgneAand developed. It is for use on ballistic nose
conea a%ltitudes between 190, 000 and 5000 ft and
velocities up to l5, 000 fps. The system operates on
UHF pul6^ radar. A preliminary evaluation of flight
teats conducted with this equipment indicates perform-
ance in close agreement with experimental results and
theoretical calculations. Functional, mechanical, and
circuitry details of this development are described and
illuatrated. (Author)
General Applied iScience Labs. , Inc. , Westbury, N. Y.
ON THE AERODtNAMlC NOISE OF A JET, by Sin- 1
Cheng. Rept. on Contraa AF 49(638)194. Apr 59, 59p.
8 refs. GASL Technical rept. no. 148; AFOSR TN-
59-1308: AD-233 |64.
Order from LC mi$3.60, ph$9. 30 PB 148 689
A new model is advanced for analyzing the broad
spectrum noise cf a turbulent Jet. The shear layer
bounding the turbulent Jet is assumed to play an im-
portant role in modifying the quadrupole sound radia-
tion from the intefior. To the sound emitting small
scale turbulent edciies (with frequencies much larger
than those large scale ones, responsible for the inter-
mittent phenomena near the edge at a turbulent Jet),
the ahear layer is laminar and la of an irregular con-
tour, as If the lar^ scale turbulent motions were
frozen. The linearized analysis is then applied to the
laminar ahear laytr to relate the acoustic oscillations
acroaa It. The co^ceft of geometrical acoustics is
generalized to repreaent the passage of an acoustic
ray through a lainlnar shear layer.
Institute fox Fluiid Dynamics and Applied Mathe-
matics, U. of Maryland, College Fkrk.
ON THE ROLLINC-UP OF A VORTEX SHEET, by
Francis R. Hama iuid E^lward R. Burke. Rept. on
Contraa AF 49(638)645. Sep 60, 32p. 5 refs. Tech-
nical note. BN-220; AFOSR -TN- 60- 1069; AD-243f 734.
Order from LC mj$3.00, ph$6.30 PB 152 047
Validity at the classical result obtained by Rdisenhead
on the rolUng-up Of a vortex sheet is examined. His
computation is foitid to be doubtful and does not
actually result In fhe rolling up of the vortex sheet In
a simple way. Fli^st, smaller time intervals must be
uaed for the step- by -step integration of the nonlinear
development erf tha vortex sheet . Second, redistribu-
tion ot the vortldty along the sheet, as it undergoes a
sine-wave dlstortlDn, has to be taken into account. It
is then shown that the vortex sheet rolls up In a more
regular manner. Strong concentration of the vorricity,
however, does not result. Effect of positive or nega-
tive background v<jrtlcity on the rolling- up formation
is also considered!. (Author)
Institute for Flul4 Dynamics and Applied Mathe-
matics, U. at Maryland, College Park.
ROUGHNESS EFFfCT AND CORRELATION OF
TWO-DIMENSIONAL WIRE ROUGHNESS IN TURBU-
LENT SHEAR FL^W, by Matthew Stevenson. Tech-
nlcal rept. no. 2 on Effect of Surface Roughness on
Turbulent Shear Flow, Contraa Nonr- 595(07). DecSJ
33p. 8 refs. Technical note BN-181; AD- 231 182.
Order from LC ml$3.00, ph$6.30 PB 152 17)
The roughness effea on 2-dimensional tiorbulent ahear
flow at wires at various spacing ratio is measured.
Except for the largest spacing ratio, the results are
restricted to the fully rough region of the roughness
effea. By keeping the roughness height constant and
varying only the spacing ratio, a simple correlation i»
found in terms of a power funalon wtidch agrees cloae^
with Schlichting's equivalent (NACA TM 823, 1937)
sand-grain correlation. (Author)
Iowa Inst, d Hydraulic Research, Iowa City.
POTEhmAL FLOW ABOUT BODIES OF REVOLUnCK
AND SYMMETRIC TWO-DIMENSIONAL FORMS, tqr
L. Landweber. Rept. on Contract Nonr- 161 1(01).
Dec 59, 68p. 13 refs. AD- 234 703..
Order from LCmi$3.90, ph$10.80 PB 152099
A procedure is presented for computing the potential
flow about bodies of revolution and symmetric two-
dimensional forms In arbitrary states at motion. Sdu-
tion for general motion is obtained by superlmpoaing
the solutions of the boundary-value problems for the
different components. Technique consists of formulat-
ing each problem as a Fredholm integral equation of
the first kind which can be closely approximated, bf
means at a quadrature formula of moderate order, bf
a set of linear equations with a matrix having a strooi
principal diagonal, suitable f ~r solution either by
elimination or iteration. For the general motion of
bodies at revolution, three such integral equations
need to be solved; for the two-dimensional forms,
solutions for four potential- flow problems are re-
quired, two at which are obtained from integral equa-
tions, the remaining two being obtained from the
integral equation solution for longitudinal flow by cca-
formal mapping. Method was programmed for the IBM
650. The separate programs for the body at revolutia
and two-dimensional forms are jjresented and the ap-
plication at computer-obtained results is Illustrated
with several examples. A considerably shortened and
somewhat less accurate procedure, suggested for use
when an automatic computer is not available, is alao
Illustrated in detail and compared with computer-
obtained results. (Author)
L^aboratorio dl Meccanlca Applicata del PoUtecnlco
dl Torino (Italy).
ON THE INTERACTION BETWEEN STREAM AND
BODY IN A FREE-MOLECULE FLOW. PART I:
ENERGY EXCHANGES, by Silvio Nocilla. Technical
note 15 on Contract AF 61(052)208. June 66, 33p.
11 refs. AFOSR-TN-60-914.
Order from LC nUS3. 00, ph$6. 30 ' PB 150 346
The study of the energy exchanges is usually faced by
eliminating .the unknown energies by the introduction of
convenient accommodation coefficients, and then giving
to these, In a more or less arbitrary way, certain
constant values. The object of this research is to over
come this arbitrariness by defining a precise energy
balance on the surface between body and flow, and dis-
cussing the derived equations in the three cases of
phenomena(l)adlab«tic, (U) with radiation and (lii) with
heat tranafer. This study, from which also appears
86
(be need of introducing Interaction parameters new
with respect to the usual accommodation coefficients,
tOams one the calculation at the re- emission temper-
,ture, to obtain a new physical Interpreutlon of the
local accommodation coefficient a. to calculate the
fflofaal accommodation coefficient "a, and to recognize, on
the baaia of icnown experimental results, that In the
case (HI) the latter assumes values somewhat different
from those usually assigned. (Author).
Laboratorio dl Meccanica ^>pllcafa del
ftolltecnlco di Torino (Italy).
SIMULTANEOUS TRANSFER OF MOMENTUM, HEAT
AND MASS. PART I: HOMOGENEOUS GASES, by
Gianni Jarre. Technical note 16 on Contract
AF61(0'^2)208.July 60. I4p. 11 refs.AFOSR-TN-60-915.
OrderfiomLCnU$2.40, ph$3.30 PB 150 347
Ihe aim of this paper is to stixly the analogies of mo-
mentum, heat and mass transfer for high speed
streams of moist gases over surfaces on which the va-
por may undergo a change of state. The known results
for homogeneous gases subjected to momentum and
beat transfer only are referred to. Such results are
elaborated and interpreted In a suitable form for the
further extenaion to nnolst gases. (Author).
Uncohi Lab., Mass. Inst, of Tech.. Lexington.
REENTRY PHYSICS PROGRAM. Semiannual technical
iianmary rept. no. 3. 1 Jan-30 June 60, on Contraa
AF 19(604)4559. 5 Aug 60, 56p. 5 refs; AD- 241 226.
Order from LC ml$3. 60, ph$9. 30 PB 150 606
A major portion of the effort in reentry physics Is con-
cerned with field experiments utilizing a apedal test
rsaotry vehicle. LaJxiratory and theoretical studies in
Hpport of the field experiments are carried on to
eatablish a model for predlaing the events that are ex-
peaed to be observed in the field and to assist In
analyzing and interpreting the reaults that are obtained.
These efforts include the study of (a) the How field abou
hypervelocity objeas, (b) the elearonic properties of
(dasmas, (c) the interaaion at elearomagnetic radla-
don with plasmas, (d) emission from plasmas, and (e)
microwave and optical meaaurements on the flow field
•asoda^ with amaller- diameter objeas fired in
kjrperbal^istlc rangea.
Massachusens Inst, of Tech., Cambridge.
MOMENTUM AND MASS TRANSFER IN COAXIAL
GAS JETS, by Walton Forstall, Jr. and Aacher H.
Shapiro. Rept. onProJ. Meteor, Contraa NOr(l-9661 .
)Hly49, 21p. 89 refa. Meteor rept. no. 39.
Order from LC ml$2. 70. ph$4. 80 PB 152 357
This report released for sale to the public 1 Nov 61 .
The mixing at constant pressure of a circular Jet with
aa annular coaxial stream haa been stiidied for condl-
tlons of nearly common denaity and temperature, bm
ttforli^ initial velocities. By using 10 per cent by
rahme of helium as a tracer In the Inner stream, the
mixing region was mapped with respect to both noateiial
•od momentum transfer . It is concluded that naaterial
dtffusea more rapidly than momentum; (hat the princi-
pal Independent variable determining the ahape ot the
V
mixing region is the velocity ratio of the streams; and
that the integpral method of Squire and Trouncer, using
experimentally determined constants, Is adequate for
predicting approximate values of concentration and
velocity in the mixing region of a Jet flowing into a mov-
ing medium of the same density. Dau for widely dif-
ferent experiments of various investigators show that
the turbulent Prandtl and Schmidt numbers are both
within dlO per cent of 0. 70, independent at the natui^e
of the experiment and the magnitude at the laminar
Prandtl and Schmidt numbers. (Author)
Polytechnic Inst, at Brooklyn, N. Y.
FREQUENCIES OF AN INFINTTBLY L(»KJ NON-
QRCULAR CYLINDRICAL SHELL. PART II. PLANE
STRAIN, TORSI(»lAL AND FLEXURAL MODES, by
Jerome M. Klosner. Rept. on Cootr set Nonr -839(1 7).
Dec 59, 42p. 5 refs. PIBAL rept. no. 552; AD- 231 234
Order from LC mi$3. 30, ph$7. 80 PB 152 139
A set of frequencies and modes for an infinitely long
nondrcular cylindrical shell are decermlned. The non-
circular shell is formed so that it has the same cir-
cumference as a circular shell of radius rQ; the radius
of curvature of the shell is given by r» ro/(l'*- • cos 28)
where the parameter c is a measure of the noDCi,rcu-
larity of the shell and a is the nondimenalonal circum-
ferential-distance. The perturbation technique was
used to obtain the frequencies, and terms ot order
€*[0(4 ^)I were retained for the plane strain vibrations.
Expressions for the frequencies of the torsional and
flexural modes were determined retaining terms of
0(f ^. The modes presented are non-orthogonal and
are related to the normal modes of the circular shell
only to the extent that the major portion of their dia-
placementa are attributed to these original circular
modes. This new set of nuxles can be used to obtain
the response of the noncircular shell to an arbitrary
forcing function . Numerical examples of the fre-
quencies are Included for the plane strain modes and
for the primarily torsional and zeroch circumferential
flexural modes. The calculations were made for a
mean radius to thickness ratio of 91 . 7 and for ratios
of major to minor axis of the shell e^ual to 1 . 1 and
1 . 40, correspoDding to an « equal to 0. 1427 and 0. 5.
(Author)
Space Sciencea Lab. , General Electric Co. .
Philadelphia, Pa.
F0RBIQ4 GAS INJECnCW INTO A COMPRESSIBLE
TURBULENT BOUNDARY LAYER ON A FLAT PLATE,
by Nathan Ness. Rept. on Contraa AF 04(647^269.
Aug 60, 68p. 12 refs. Technical Infornuttlon
Series R60SD410.
Order from LC ml$3. 90, ph$10. 80 PB 150 802
The distributed Injection of a foreign gas Into a com-
pressible, turbulent boundary layer in the absence of a
pressure gradient is considered. The analysis is pier-
farmed within the framework of the binary mixture
concept, that is, the primary fluid flowing over the
surface represents one compoDent while the Injeaed
species represents the second. Calculations have been
performed for the Injeaion of helium into undiasodated
air. The results Indicate the effea of Mach number cm
aurface shear and energy transfer when distributed
light gas Injea^ normal to the aurface exlsta. A com-
pariaon with experimental data Indicatea reasonable
agreement over a range of Mach Number. (Author)
87
Stanford U., Calif.
THERMAL BENDING STRESSES IN SHELLS, by
W. FlOgge. Final re*t. on Contract Nonr-225(l6).
10 Nov 59, 28p. 10 r^fs. Div. at Engineering Me-
chanics. Technical rfcpt. no. 124; AD- 229 109.
Order from LC n:ii$2^70, ph$4. 80 PB 150 853
The research deacrll^ed briefly in this report was con-
cerned with thermal pending stresses in shells. Such
stresses may be attributed to two distinctly different
causes: Temperature differences within the shell and
temperature differences between the shell and other
structural elements to which it is connected (e. g. rings
or bulkheads). The solutions at these two parts at the
thermal stress problem correspond to particular and
complementary solutions at the differential equations.
Work has been done along both lines, and where it
appeared that the thetmal stress problem could best be
appreciated at a part at the general stress problem,
due anaitian has beef paid to die latter.
Hydrodynamics, Wydraullcs, and Hydro«tatic«
t
Brown U. I>iv. at Applied Mathematics, Providence,
R. I.
THE EFFECTS OF SURFACE TENSION AND VIS-
COSITY ON THE St ABILITY OF TWO SUPERPOSED
FLUIDS, by W. H. ieid. Technical repc. no. 29 on
Contract Nonr-562(0p), Nov 59. 31p. 10 refa. Repc.
562(07)/29. J
Order from LC ml$^ 00, ph$6. 30 PB 150 528
The effea of surface tension on the stability of two
superposed fluids can be described in a universal way
by a nondimensional /'surface tension number" S which
provides a measure pf the relative importanqe at sur-
face tension and visoosity. When both fluids extend to
infinity, the problem can be reduced to the finding d
the roots at a quarti^ equation. The character of these ,
roots is first analyzed so as to obuin all possible
modes of stabiUty oy instability. Two illustrative cases
are then considered in further deull: an unstable case
for which the density of the lower fluid is zero and a
stable case for whicli the density of the upper fluid is
zero, the latter cas4 corresponding to gravity waves.
Finally, the variatioiial principle derived by Chandra-
■•khar for problems, of this type is critically discussed
and it is shown to be of less usefulness than had been
thought, especially i^ those cases where periodic
modes exist. (Authot) "
Compagnie de Reckerchea et d'Etudes Aerooautiquea
(France). '^ [
CONTROL Of aRCULATTON AROUND A ORCULAR
CYLINDER, by Jean Brocard. Technical status rept.
no. 2 on Contraa AF 61(052)333. 20 May 60. 28p.
AFOSR-TN-60-1015(.
Order from LC mill. 70. pt44. 80 FB 150 368
For this particular »tudy Mr. Qruaon has developed
an original method which oiakes it possible to obtain
in the water tank, not only quaUtaclve results such as
those usually obtained, but alao quaotltatlve results
such as, in particular, the estimated C^^. This method
Is described In the jr*
David Taylor Model Basin, Washington, D. C.
BOUNDARY- LAYER INVESTIGATION ON USS
TIMMERMAN (EAG 152) (EX-DD 828) by Clifford L.
Sayre. Jr. and Ralph J. Duerr. Aug 60, 24p. 10 refa.
Rept. 1170.
Order from LC ml|2. 70, ph|4. 80 PB 150 737
Results of velocity measurements in the boundary layer
of USS TIMMERMAN (EAG 152) are presented in this
report. Measurementa of velocities In the throat of the
condenser scoop and the pressure drops across the coo-
denser are also given. A generalized form of Prandtl's
equation for the growth of the turbulent boundary layer
on a flat plate is derived for use in estimating the bound-
ary layer thickness at large Reynolds numbers. (Auduv).
Dynamic Developments, Inc. , Babylon, N. Y.
PENDULUM FACILITY REPORT, by T. Andrews and
R. Smith. Rept. on Contract Nonr- 2852(00). Nov 59, ^
4 refa. Rept. no. 115.
Order from LC ml$3. 30. ph$7. 80 PB 150 478
The Pendulum Facility has been designed and constructed
to Inveatlgate the loading characteristics of various hy-
drofoil designs. In addition to a facility description, diit
report presents Pendulum test data obtained on hydro-
foila and struts which have been previously tested at the
towing tanks of either the Stevens Institute of Technology
at Hoboken, New Jersey or of NASA at Langley Field,
Virginia. The comparison of such data establishes Pen-
dulum a'^curacy. , .
y--..
Dynamic Developments, Inc. . Babylon, N. Y.
PENDULUM TESTS OF SPECIFIC HYDROFOIL DE-
SIGNS, by T. Andrews and R. Smidi. Rept. on Contraa
Nonr- 2852(00). Nov 59. 45p. 2 refs. Rept. no. 116;
AD- 233 433.
Order from LC ml$3. 30, ph$7. 80 PB 150 479
Teat data are presented on two basic types of hydrofoil
One type is of low thickness ratio, low aspect ratio and
of a modified delta plan -form with high sweepback at
the leading edge. It Incorporates a shalp leading edge
and a blunt trailing edge. The second type incorporates
a larger thickness ratio and larger aspect ratio, and
embodies less sweepback at the leading edge. It employs
a streamwise cross section with a parabolic thickness
distribution and a blunt trailing edge. Camber is intro-
duced into both types of foil designs. The supporting
struts used with the modified delta foils employ a cross
section with a parabolic forebody and a tapered after-
body. Forcbody and afterbody are separated by a step.
The second type of tested foil was supported by a atrut
which employs a cross section of parabolic thickness
distribution over its entire chord and which has a blunt
trailing edge. The tests described represent an initial
study directed toward the development of fully sub-
merged hydrofoils for operation at crulae speeds be-
tween 80 and 100 knots. -As such, the tested configura-
tions have employed realistic structural geometries.
The blunt trailing edges of struts and foils are vented
to the atmosphere aa a meana of baae-drag reduction.
These tests have been very useful in determining gr
ometry characteristics necessary to obtain sn^ooth losd
tranaltlon between conditions of wetted and ventilated
flow on foil upper surfaces.
88
.1.-..I i.\
Glbbs and Cox, Inc. . New York.
A LINEARIZED THEORY FOR THE HYDROFOIL OF
FINITE SPAN IN A FLUID OF INFINITE DEPTH, by
J P. Breslin. Technical rept. no. 16 on Hydrofoil Re-
search Proj. , Contract Nonr-507(00). Jan 54, 67p.
14 refs. AD- 24 418.
Order from LC mi$3.90. ph$10.80 PB 152 416
This report released for sale to the public 1 Nov 60.
The fluid motion produced by a foil of finite span is ob-
tained from the free surface theory of Havelock (Proc.
Roy. Soc. 118:24-23, 1927). Formulas for the velocity
potential are obtained for points at some distance aft of
the foil, and formulas which are der^ed from these ex-
pressions for the wave profile, wake velocities, and
drag are considered sufficiently simple for engineering
uae. The analysis showed that the total lift -dependent
drag comprises an Induced drag and a wave drag. The
induced drag is essentially that of a foil moving close tc
a rigid wall. The wave drag lb represented by an
Integral which expresses the sum of the transverse and
lateral wave drag. The Integral is a funalon only of
■pan- and submergence- Froude numbers and approaches
a limit which is independent of gravity. The limit is
equal to twice the drag Increment resulting from a
blgplane image. A comparison with total lift -dependent
drag from model tests showed reasonable agreement
irlih theoretical results. ;
Institute of Engineering Research, U. of California,
Berkeley.
ON THE MEASUREMENT OF TURBUUENT PRESSURE
FLUCTUATIONS WITH A TRANSDUCER OF FINITE
SEE, by G. M. Corcos, J. W. Cuthbert, and W. A.
Von Winkle. Rept. on Contract Nonr -222(30). Nov 59,
30p. 10 refs. Series no. 82, Issue no. 12.
Order from LC mi$2. 70. ph$4. 80 PB" 150 540
The general problem of the mapping of random fields by
a linear operator has been treated, in particular by
H. W. Liepmann and Uberoi and Kovasnay. The use of
transducers of finite size for the measurement of pres-
sure fluctuations within turbulent flows Involves a sys-
tematic error which is an example of this mapping. The
new feature at the problem Is the coupling of the time
and of the space donwin caused by the apparent down-
stream conveaion of the pressure field which has been
observed in turbulent shear flows. The problem is
formulated for a field which la homogenous (but not
Isotropic) in the relevant coordinate axes and stationary.
A model of the downstream convection is introduced and
used to derive formulae for the distortion of the three-
dimensional sp)ectrum and of the frequency spectrum.
For the three-dimensional spectrum, the formalism is
Chat of Uberoi and Kovasnay. For the frequency spec-
trum, a somewhat more direct approach is presented
although the results of Uberoi and Kovasnay are again
useful in generalizing the convection model. The results
confirm recent measurements which indicate that the
frequency spectrum may be considerably in error for
the higher frequencies even when the mean square
pressure measurements are only slightly affected by
the finite size of the transducer. (Author)
Massachusetts Inst, of Tech., Cambridge.
AN APPRAISAL OF THE HYDRAUUC ANALOGUE TO
GAS DYNAMICS, by Ascher H. Shapiro. Rept. on Proj.
Meteor, Contraa NOrd-9661. Apr 49, 21p. 18 refs.
Meteor rept. no. 34.
Order from LC mi$2. 70, ph$4. 80 PB 152 356
This report released for sale to the public 1 Nov 61.
The assumptions of the hydraulic analogue to gas dy-
namics are reviewed in the light of recent experience,
with the aim of assessing the analogue as a practical
tool. Some experimental techniques are discussed, and
some typical results obulned with a "supersonic water
channel" are presented, k is concluded that the water
channel is a valuable instrument for making qualiutive
studies and for making quantitative studies of a com-
parative nature but does not lend Itself to obtaining di-
rect design data. (Author)
Naval Ordnance Lab. , White Oak, Md.
STABILITY CRITERIA FOR NUMERICAL SOLUTIONS
OF THE NORMAL AND SHOCK REGIONS IN UN-
STEADY TWO-DIMENSIONAL CYLINDRICAL
LAGRANGIAN FLOW, by Julius W. Enig. 15 Mar 60,
I7p. 4 refs. NAVORD rept. 6726; AD-237 718.
Order from LC mi$2. 40, ph$3. 30 PB 148 178
An application of a method given by von Neumann and
Richtmyer (J. Appl. Phy. 21: 1950) is used to derive the
stability criteria for numerical solutions of the normal
and shock regions In unsteady two-dimensional cylindri-
cal Lagrangian flo'v. The shocks are computed by the
psuedo -viscosity method for one -dimensional flow; this
method has been applied to the computation of unsteady
shock propagaticwi In two -dimensions. By introducing a
small perturbation into the hydrodynamlc differential
equations, the set of equations of first variation are ob-
tained. The stability criteria are obtained by perform-
ing a stability analysis on the finite difference repre-
senution of the dcxninant equation of the set of equations
of first variation. Utilization In compnitttional pro-
grams shows that the derived criteria lead to stable
solutions. (Author)
Rensselaer Polytechnic Inst. , Troy, N. Y.
SOME VARIATIONAL PRINCIPLES FOR PROBLEMS
IN HYDRODYNAMIC AND HYDRODYMAGNETIC STA-
BILITY, by R. C. DiPrlma. Rept. on Contract Nonr-
591(08). 13 Nov 59. 25p. 17 refs. RPI MathRep no. 28;
AD-229 361.
Order from LC mi$2. 7a ph$4. 80 PB 150 871
Contents:
The Taylor problem
The inhibition of convection by a magnetic field
The Taylor problem with an axial magnetic field
Direct series solution
Royal Inst, of Tech. (Sweden).
TRANSITION IN BIREFRINGEMENT FLUID FLOWS,
by E. Rune Lindgren. Final rept. for 1 Jan 57-
31 Mar 59 on Contract AF 61(514)120. 23 June 59, 5p.
4 refs. AFOSR-TR-59-135.
Order from LC mi$l. 80, ph$l. 80 PB 150 331
89
The aim at the present study has been to try to remove
apparent discrepancies between findings «^ various
authors and also If possible co add facts about the tran-
sition process which may have escaped previous inves-
tigators. Only a getierai survey of the experimental
t^hniqiiff and the fitxllngs are presented here.
Woods Hole Oceanographlc Institution, Mass.
AN EXPERIMENTAL STUDY OF SHIP MOTIONS, by
Wilbur Marks. Tfectinical rept. on Contract Nonr-
1168(00). Nov 59, I2p. 16 refs. Reference oo. S9-S9;
AD- 228 212.
Order from LC mi)^. 40, ph$3. 30 PB ISO 842
A Ilnesr theory at ship motion prediction was presented.
An ezperlmenul verification at the theory was described
for pitch and heave and in head and following seas. Im-
provements at certain coupling terms in the equations ol
morion are presentad. The pitch and heave at the launch
Risk (36- ft long) were recorded for a specific set of test
conditions and analyzed in terms of the oiergy spectra 4,
at these motions. From the physical and geometrical
properties at the vessel, the particular amplitude re-
sponse operators in these degrees of freedom were com-
puted with and without the assumption of coupling. The
observed spectra w4re compared to the 2 computed sets
of spectra. Results show that: (1) the linear prediction
scheme agrees reasonably well with observation,' atid
(2) the linear prediction sdieme yields motion statistics
which in general agree more nearly with observatloo.
(Author)
Statics, Kinematics, and Kinetics
Brown U. Dlv. of Engineering, Providence, R. I.
ON ANOMALIES IN THE MEASUREMENT OF THE
COMPLEX MODULUS, by S. R. Bodner. Technical
rept. no. 16 on Contract Nonr-S62(20). Dec 59, 32p.
9 refs; AD- 230 329.
Order from LC inl$8. 00, ph$6. 30 PB 152 170
Resonance tests on aluminum and lead specimens re-
veal multiple resonance peaks, i.e. resonances In
sddltlon to the natural frequencies of the system, when
the specimens are subjected to uniform static stress or
contain residual strssses. The multiple resonance
peaks can be interpretated in the same manner as the
resonance dispersions observed by B. R. Pltzgersld
(Phys. Rev. 108:3, Nov 1957). Experiments were con-
ducted which show that the phenomenon is directly re-
lated to the presence of either residual or applied static
stresses . A tentative explanation of the phenomenon Is
presented which is based upon the mathematical repre-
seiKatlon of the experiments by Mathieu type equations .
The sddttlODsl resonances are interpreted as instabilities
of the solution of the Mathieu equation. (Author)
I I
Bureau of Ships, WSshlngton, D. C
PROCEDURE FOR TORSIONAL VTBRATI(»I ANALY-
SIS OF MULTIMASS SYSTEMS, by Richard J. Gsrl-
bokli. Research and development rept. 15 Dec 53,
93p. 7refa. Rept. no. 371-V-19.
Order from LC mi$5. 40. ph$15. 30 PB 152 681
The object of this report is to present a general pro-
cedure for analysis of the torsional vibration charac-
teristics of multi-mass systems. Technical texts,
papers, sod reports were drawn upon for dau and In-
formation. No attempt has been msde to present all
possible methods of calculation or to derive all equa-
tions. Rather, the steps are explained as briefly as
possible with references to the literature given for a
more thorough study. The only original work in this
presenutlon is the compilation of a systematic proce-
dure of analysis. Procedure is presented In the se-
quence ordinarily followed in analyzing the torslonsl
characteristics of a system. (Author)
f« G. Engineering Research Associates, Baltimore,
Md.
VIBRATIONS OF THICK SHELLS IN A VACUUM AND
IN AN ACOUynC MEDIUM. PART II. AXIALLY
SYMMETRIC VIBRATIONS OF A THICK CYLINDRI-
CAL SHELL IN AN ACOUSTIC MEDIUM, byJoshuaE
Greenspon. Technlcsl rept. no. 3 on Contract Nonr-
2733(00). Nov 59, 25p. 6 refs. AD- 231 422.
Order from LC ml$2. 70, ph$4. 80 PB 150 480
The dynsmlc behavior of infinitely long thick cylindrical
snells surrounded by water is investi^ted. The shell
is excited by axially symmetric forces. Curves Sre
presented which give the forced vibrstion smplitude sad
scoustlc pressure In the water aa a function of fre-
quency for various modes of vibration of the cylinder.
The application of the analysis to deep sea sound
sources and transducers is discussed. (Author) (See
slso PB 145 249)
Rensselaer Polytechnic Inst., Troy, N. Y.
WELDING ASPECT OF SLIDING FRlCnC»i BE-
TWEEN UNLUBRICATED SURFACES, by F. F. Ung.
Final rept. on Contract AF 49(638)67. 30 June 60,
44p. 30 refs. AFOSR-TR-60-117.
Order from LC ml$3. 30. pti$7. 80 PB 150 952
This report abscraas materials from five previous
technical notes written for the project on the welding
sspect of friction for unlubricated metallic surfaces.
It also shows in detail s theoretical and experlmenul
Investlgstion of sdheslon in which the coefficient of
adhesion Is related to two important parameters:
salvation energy of the process sod s time exponent,
both of which are dependent on the degree of cleaoli-
ness of the surfaces. (Author)
This report released for sale to the public 16 Nov 60.
METALLURGY
Curllss- Wright Corp. , Caldwell, N. J.
RESEARCH ON PRC»»ERTIES OF HIGH STRENGTH
MATERIALS SUITABLE FOR HIGH THvlPERATURE
APPUCATIONS, by Harold N. Cummli^s, Foster B
Stulen, and William C. Schulte. Rept. for May 59-
Juoe 60 on Msterisls Applications, Contract
AF 33(616)6552. ^jly 60, 61p. 7 refs. WADD T^Jchnl-
cal rept. 60-240.
Order from OTS $1. 75 PB 171 060
90
0US of Iron-nwlybdenum alloys, intended for study
IS to suitability for ball bearings at temperatures up to
I000°F, were found to be So non- homogeneous and
brittle that specimens could not be machined from /
them High temperature tnrslon tests of relaxation^
were made to study the suitability of two alloys. Mjl
tool steel and Inconel X, for springs at lOOOOF, and of
two alloys. Was pa Hoy and Udlmet 500, for springs/at
150^. Alternating torsion of ±10 k«l, superimpt^sed
OB an Inltlsl steady stress of 25 ksl. was applied lb
jpeclmens of each alloy. Inconel X lost shout 10 to 15
percent of the steady load in about 100 hours. The
Ihiee other alloys relaxed two to three times as much
«tien tested at the respective temperatures mentioned
above. (Author)
Naval Research Lab. . Washington, D. C.
ELEVATED TQ^PERATURE DIFFUSION IN THE
SYSTEMS Nb-Pt, Nb-Se. Nb-Zn, Nb-Co, Nl-T^, AND
Fe-Mo, by R. E. Seebold and L. S Blrks. Interim
rept. 19 Sep 60, I3p. 6 refs. NRL rept. 5520.
(>?ter from OTS $0. 50 PB 161 767
The electron probe microanalyzer has been used to de-
termine the composition and extent of phases occurring
In bimetal diffusion couples st 1100°C. A total of eigh-
teen phases were determined in six binary systems:
Nb-Pt. Nb-Se. Nb-Zn, Nb-Co, Nl-T», and Fe-Mo. In
all cases the phases are stoichiometric and expressible
to tmall whole numbers. The Nb-Se and Nb-Zn sys-
tems are somewhat alike in their phase formations in
that Nb-Se exhibits Nb-Se, Nb2Se3, and Nb-Se2 while
Nb-Zn produces Nb-Zn, Nb2Znp, NbZns, Diffusion be-
tween niobium and platinum to torm Nb3Pt, NbPt,
NhPt2' ^"^ NbPta would seem to preclude prolonged
use of platinum Uiermocouples In oonuct with niobium
at llOCrC. The only phases produced in the Nb-Co sys-
tem are previously unreported in the literature ano are
NbaCoo and NbCo4. This system also exhibited an ex-
tended region containing about 5 weight percent nio-
bium in cobalt in agreement with the solubility limit
shown in existing phase diagrams. Ni-TS diffusion
prxxluced ronds whlclfthowed strong cracking and
grain formation. The phases TiNis, 'ftNlj. TTsNi, and
ThoNio comprised the zones, with pure tanuluniOTe-
clpltatlng In the TaNl2 phase on cooling from 1100"C
Pe-Mo produced only one phase: Mo2Fe3. (Author)
Naval Research Lab. , Washington, D. C.
HIGH TEMPERATURE OXIDATION OF IRON-CHRO-
MRJM BINARY ALLOYS IN WATER VAPOR. PART 1:
A PRELIMINARY STUDY OF THE MECHANISM OF
OXIDATION OF IRON-CHROMRJM BINARY ALLOYS
IN WATER VAPOR, by C. T. FuJU and R. A, Meussner
Final rept. on phase 1. 21 S«P 60, 27p. 22 refs. NRL
rept. 5506.
Orter from OTS ». 75 PB 161 696
The oxidation of a series of iron-chromium binary al-
loys In a water vapor- argon atmosphere at high temper-
stures wss investigated. The chromium contents of the
alloys were 5. 10, 15, 20 and 25 percent and the oxida-
tion temperstures were 700o. 900°. snd 1100°C. Pow-
der x-rsy diffraction methods and metallographlc tech-
niques were used to Identify the oxides that were pres-
snt In the scales formed on the alloy. Generally, the
scales that formed on each specimen could be conven-
iently divided into three parts. There is v> outer layer
of wQstlte. s two-phase inner layer composed of w-^s-
tite and a mixed Fe-Cr oxide, and a subscale. Corre-
lations between chromium concentration of the alloy,
temperature of oxidation, weight gain, oxide composi- "
tlon, and the mlcroetructure of the oxide layers are
presented. Weight gain versus tlnae plots bidicate that
at 700° and 900°C the oxidation follows a parabolic
curve, whereas the rate at I lOQOC is linear. A pos-
sible mechanism for the oxidation process is suggested
In the form <rf wiistite decomposition at the outer- inner
scale layer boundary, giving rise to Fe *2 diffusion to
the outer layer and O" ^diffusion to the alloy-oxide in-
terface. (Author).
Office of Technical ^rvlces, Dept. of Commerce,
Washington, D. C
UQUID METAUS. A^ 60, lOp. 179 refs. OTS Selec-
tive Bibliography 86-424.
Order from OTS $0. 10 OTS SB-424
A bibliography of reports listed in the two OTS monthly
abstract Journals: U. S. Government Research Reports
and Technical TranslsHons . This bibliography includes
reports added to the OTS collection during the period
1950 to September 1960.
Watertown Arsenal Labs. , Mass.
A COMPARISON OF SHEAR STRENGTH VALUES
OBTAINED FROM THREE TYPES OF SHEAR TESTS
7075-T6 ALUMINUM, by Armsndo A. Isnnelll.
Oa 60, 15p. Technical rept. no. WAL TR lW/1.
Order from OTS $0. 50 PB 161 989
Sheet, punch and double shear tests hsve been carried
out to establish a comparison of shear strength values
(Atained by the three methods. The material used in
the investigation is 7075-T6 aluminum. For each type
of shear test the specimen sizes have been varied.
The effea of size on shear strength values is
presented. (Author)
Watertown Arsenal Labs. , Mass.
ETCH PITS IN PYROLYTIC GRAPHITE, by Aram
Tarpinlan and George E. Gazza. Rept. on Materials
for High Temperature Uses. Oct 60, Up. 6 refs.
Technical rept. no. WAL TR 130.5/1.
Order from LC ml%2. 40, ph$3. 30 PB 150 917
The observation of pits In pyrolytlc grsphic after Ion
bombardment etching is described snd their similarity
to dislocation etch pits is speculated. Evldetice of etch
pit multiplication ln:{he form of slip line segments and
low angle tilt boundail^ is presented. (Author)
Ferrous Metals
American Brske Shoe Co. , Mahwsh, N. J.
DEVELOPMENT OF LOW ALLOY STEEL COMPOSI-
TIONS SUITABLE FOR HIGH STRENGTH STEEL
CASTINGS, by Hugo R. Larson, Ronald C Campbell,
and Herbert W. Uoyd. Rept. for May 59- May 60 on
Metallic Materials, Contract AF 33(616)6485. July 60.
75p. WADC Technical rept. 59-63, Part IL
Order from OTS $2. 00 PB 171 065
n
A snidy waj made of beat treatments and compositions
for optiinum properties In heavy sections ctf low alloy
heat treatable steels and a 5% Cr air hardening steel.
The influence of high purity melting stock was investi-
gated. Fatigue testing was also performed. Alloy var-
latioas of the 5% Cr steel were sttidled, and elevated
temperature proper^es determined. The effect of feed-
ing distance and aoitadness on properties of the 5% Cr
steel was investigated. Production heat data was ana-
lyzed and exhibited good reproducibility as well as su-
perior properties iq high purity heats. (Author).
Armour Research IPoundation, Chicago, DL
STUDY OF FATIGUE PROPERTIES OF ULTRA-HIGH
STRENGTH STEEL, by Harvey B. Nudelman and John
P. Sheehan. Rept. tor Mar 59- Feb 60 on Metallic
Materials, Contract AP 33(616)6290. June 60, 65p.
3 refs. ARF 2172-6t WADD Technical rept. 60-120.
Order from OTS $ll 75 PB 171 056
A temper- resistant, high- strength steel was investi-
gated with reference to fatigue strength. This alloy
was prepared by two different melting techniques. The
first method consisaed at induction melting In air using
standard deoxidation techniques. The second method
involved the application d a special deoxidation prac-
tice to induction melting; silicon-free steel was deoxi-
dized with carbon and aluminum to minimize the pres-
ence at silicate inclusions. These alloys were tested
in fatigue using the Prot accelerated method. The re-
sults at the samples melted with standard practice in-
dicated ttiat fatigue strength is improved slightly by
tempering at elevated temperature. The application at
a special melting pnx:ess showed that a very sign if Icaitf
Increase in the Prot fracture stress to ultimate tensile
strength ratio (En/UTS) can be olxained by eliminating
the presence d siliqon and deoxidizing with carbon and
aluminum. (Author);
Defense Metals Infbrmation Center, Battelle
Memorial tfist., Columbus, Ohio.
DESIGN INFORMATION ON 17-7 PH STAINLESS
STEEL FOR AIRCilAFT AND MISSILES, by
R. J. Favor, O. L. Deel, and W. P. Achbach. Rept. on
Contract AF 18(600)1375. 23 Sep 60. 37p. 7 refs.
DMIC rept. 137.
Order from OTS »i.00 .. PB 151 096
E levated- temper ataTe design curves for short-tinie
ultimate tensile strength, tensile yield strength, com-
pressive yield strength, ultimate shear strength,
bearing ultimate strength, and bearing yield strength
are presemed. Thete curves have been based on a
number of published and unpublished reports and
papers. Data are sifrunarized in Appendix A in a
format recommended for MIL-HDBK-5 (Superseding
ANC-5), Strength o< Metal Aircraft Elements. Appen-
dix B contains sumnmry plots ot substantiating data
from which design allowable strengths were derived.
(Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
SCME PHYSICAL PROPERTES OF MARTENSITIC
STAINLESS STEELa by J. G. Hoag and D. B. Roach.
[Rept. on Contract AF 18(600)1375]. 28 Sep 60, Sip.
24 refs. CMIC memp. 68.
Order from OTS $0. 50 PB 161 218
I
Metals and Ceramics Lab. , Wright Air Developraev
Dlv. , Wright -Paner son AFB, Ohio.
THE STATUS OF RESEARCH AND DEVELOPMENT
FOR HIGH STRENGTH AIRCRAFT STEELS, by
E. M. Kennedy. Jr. Rept. for 1956-1959 on Metallic
Materials. July 60, 36p. IS refs. WADC Technical
note 59-326.
Order from OTS $1.00 PB 171 077
New aircraft and missile developments have required
the development and use at structursl steels having
optimum strength and ductility over a wide range of
temperatures. In this survey an attempt is made to
point up to some of the significant areas of investiga-
tion in which efforts are being expended toward devel-
oping and improving steels having tensile strengths in
excess erf 260, 000 psi . In order to complete the
survey of the field of Interest, the sources Imown to
have research and development interest in this area
were contacted either by personal visitation or througb
official carrespondence. fbe results of the conucts
nude were gratifying and the many Investigations and
studies being carried on are commented upon in the
text erf this report. (Author)
Naval Research Lab. , Washington, D. C
VACUUM INDUCTION MELTING: OXYGEN AND
CARBON IN IRON, by J. E. Srawley. Final rept. on
phase 1. 21 Sep 60, 20p. 5 refs. NRL isept. 5516.
Order from OTS |0. 50 \PB 161 764
Oxygen was removed from vacuum Induction melts of
electrolytic Iron to a limiting level of the order of 20
parts per million (ppm) by means of carbon additions.
The initial oxygen contents were about 200 to 300 ppm;
a minimum of about 450 ppm of carbon was required to
lower the oxygen contents to 20 ppm. Excess carbon
reacted with the crucible materials, which resulted In
a lost of about 10 percent of the carbon added during
heats of 4 to 5 hours duration. Of the three crucible
materials used, alumina appeared to be distinctly less
reactive to carbon addition than zirconia or magnesia.
In the absence of carbon the oxygen contents of dip
samples taken from the melts remained substantially
constant throughtout the heats. The usefulness of leiik-
up rate measurements for process control is discussed
and the features of leak- up rate charts are described.
(Author)
Rutgers [State U. ] New Brunswick, N. J.
INHBITICW OF HYDROGEN EMBRtTTLEMENT
DURING PICKLING, by Robert H. Anderson. Quart-
erly progress rept. no. 5, I Jan-31 Mar 57, on Coo-
traa DA 30-069-ORD-[16891. [1957] 17p. AD- 136 254
Order from LCmi$2. 40. pi43. 30 PB 152 680
Tfaia report released for sale to the public 16 Nov 60.
Hydrogen evolution and concomitant dissolved iron
have been determined for the reaction of 1095 steel
with 4. 8 N HCl inhibited with DHQ (IX bexamlne, and
a combination of these two inhibitors. For 0. 5%
hexamine the number of mlllimoles of hydrogen evolved
is from 10 to 15% less than the number of millimoles
of iron dissolved. The rate of hydrogen evolution does
not vary markedly with time in the solutions containing
0. 15% DHQ; but in 0. 5% hexamine solution the rate de-
creases by a faaor of 5 over a period Of 15 hours. A
•olidon made by immediately diluting 5 g each of
rtoSildine and hexamine to 1 Uter with 4. 8 N HCl was
^own to be no better as an embrittlement inhibitor
thu the Inhibited acid of U. S. Army Specification
Ito 4-105. F-4a(2). Also the embrlnlement inhibition
did not improve over a 58 day period of standing. The
aew compound, EtDHQ (II), was tested for embrittle-
Bient and metal attack inhibition in combination with
Kexamine. No significant differences were found be-
tMso it and the combination of DHQ and hexamine in
lliBSe two properties. When tested in combination
with DHQ, Moore Fatigue tests indicated that acetal-
dehyde was not as good as hexamine, in its embrittle-
juett inhibition properties. (Author) (See also
FB 145 503)
Jght Metals
r I J
92
Lockheed Aircraft Corp. , Sunnyvale, Calif.
BERYLLIUM CRACK PROPAGATION AND EFFECTS
OF SURFACE CONDITION, by C. O. Matthws
M. L lacobaon and others. Rept. for 1 July 58- 31 Dec 59
on Meuilllc Materials, Contract AF 33(616)5978. July 60
I97p. 13 refs. WADD Technical rept. 60-116.
Order from OTS 13.00 « 171 088
The mechanical properties of beryllium sheet with var-
ious surface finished were investigated. The best prop-
erties were obtained on sheet which had been etched to
remove surface defects caused by machining. Ductility
was low in aU cases, being Umited by the presence of
notches and by preferred orientation in the sheet. Duc-
tiUty was Increased by heating to 400° to 600°F. The
fatigue endurance limit was as high as the static tensile
Btrengjh, and was Improved by etching. Impact tests
were found to be most suitable for distinguishing be-
tween various surfaces. Theoretical analyses were
made of the effect of including residual stress in di«
Griffith crack theory, and of the dynamic stress at the
leading edge of a crack Ih a unlaxlally stressed plate.
(Author)
New York U. . N. Y. ' : „ ^„ ^^
INVESTIGATION OF CREEP BUCKLING OF COL-
UMNS AND PLATES. PART II. CREEP BUCKLING
EXPERIMENTS AND COLUMNS OF Ti-7Al-4Mo
TITANIUM ALLOY, by Ralph Papimo and George
(Jerard. Rept. for May 59 -Feb 60 on Ceraniic and
Cermet Materials. Contract AF 33(616)5807. July 60,
54p. 3 refs. SM 60-6; WADC Technical rept. 59-416,
Order from OTS |1. 50 » 171 082
Creep bucklli^ and short time buckling experiments
have been performed on columns of Tiunium Alloy
Ti-7Al-4Mo with simulated simple support and fixed
etxl boundary coiKlitlons. Both end shortening and cen-
tral deflection were recorded autographicaUy during
loading and durli« creep. Elevated temperature prop-
erties of the test material had previously been deter-
mined from specimens taken from 3/16 inch thick
stock and these were augmented by tests on 3/8 Inch
thick stock since the mechanical properties and struc-
ture were significantly different for the two thick-
nesses. The excellent creep properties of the test ma-
terial Indicate that creep buckling tests must be con-
ducted at 950Pf or higher for creep buckling to occur
in reasonable times at stress levels below the short
time compressive yield strength. Since only a narrow
range of test conditions is svailable for creep buckling
experinents with this material, colunui tests were
conducted L'//> at approximately 40 at 95(fiP. (Author)
(See also FB 161 488)
Nonferroos (except light) Metals
Defense Meuls Information Center, Battelle
Memorial ln»t., Columbus, Ohio.
PHYSICAL AND MECHANICAL PROPERTIES OF
THE COBALT-CHROMIUM-TUNGSTEN ALLOY
WI-52, by F. R. Morral and H. J. Wagner. [Rept. on
Contract AF 18(600)13751. 22 Sep 60. 20p. 2 refs.
DMIC memo. 66. « ,^, o,it
Order from OTS $0. 50 « 161 216
WI-52 was designed for gas-turWne components re-
quiring high- strength properties in the 1000 to 2000 F
temperature range. It has been used primarily as a
first- stage turbine vane, supplanting the older X-40
(HS 31) alloy. Above 1800 F it may be useful in appli-
cations requiring resistance to thermal shock, fatigue.
and oxidation, but with lower strength requirements.
It Is available only in the form of castings.
IlUnols Inst, of Tech. , Chicago.
ENERGY CHANGES AND ISOTHERMAL KINETICS OF
ORDERING IN AuaCu, by Francois d'Heurle and Paul
Gordon. Technical rept. no. 4 on Contraa Norir-
1406(03). Nov 59, 40p. 24 refs; AD- 229 7^.
Cfrder from LC ini$3. 00, ph$6. 30 PB 150 470
The order -disorder transformation in AU3CU is s re-
versible transformation with a critical temperature of
212 •♦• l*t for 72. 5 atomic per cent cold alloy. Long-
range order formation below the critical temperature
has been observed to have three- stage isothermal ki-
netics and short-range order formation above the criti-
cal temperature two-stage kinetics. The first stage of
long-range ordering appear to have kinetics similar to
the first stage of long-range ordering, indicating that
Initially the mechanism of the reactions are alike. A
gradual transition from three -stage to two- stage ki-
netics takes place as the temperature of isothermal
ordering is raised through the critical temperature.
Contrary to theoretical expectations for A^3 type alloys
no Istent heat was found at the critical temperature.
The apparent lack of agreement with theory, together
with the degree of the transition has been discussed.
From the experinventally measured changes in internal
energy during ordeil ng, a total internal energy change
of approximately 390 calories per mole between a com-
pletely disordered and completely ordered sample has
been estimated. In quenched samples the rates of
ordering at low temperatures have been revealed to be
surprisingly fast. The rates found in such samples at
about 100°C were more than ten thousand times
greater than woi*ld be expected from the rates observed
near 19(J°C. It appears safe to conclude that this
phenomenon is due to the quenching- in of Uttice defect^
presumably vacancies as suggested by a measure of the
energy of motion of these defects. (Author)
98
Jotm Carroll U.
Cleveland, Ohio.
PHYSICAL PROPERTIES OF GALUUM, by H^-oId J.
Murphy Technical rept. no. 2 on Contract NonV-
2S77<01). 15Dec|59, 49p. 60 refs. AD-230 598\
Order from LC n^$3.30, ph$7.80 PB 15^ 151
I
The report contaihs tables of available data on me-
chanical, thermal, electrical, magnetic, optical, \
atomic, and cry«)allographlc properties of this ele-
ment. In addition, brief qualitative descriptions 0^ ^
various characteristics of gallium of special interest -
to the experimeni^Ust are included. (Author)
ilcals,
Research Chemlbals, Inc. , Burbank, Calif.
THE METALLURGY OF YTTRIUM AND THE RARE
EARTH METALS, PART I. PHASE RELAT1(»1SHIPS,
by Bernard Love. Rept. for Oct 58-Oct 59 on Metallic
Materials. Contraw AF 33(616)5905. May 60, 246p.
28 refs. WADD Technical rept. 60-74, Part I.
Order from OTS $.3. 50 PB 171 085
Partial constitutio<ial diagrams were established for
the systems Er-TJ, Y-Ti, Er-Cu, Y-Cu, Br-Sn,
Y-Sn, Er-Co, Y-Co, Er-Zr, Gd-Zr, V-Er. V-Yv
Cr-Er and Cr-Y. Compounds are formed in the cop-
per, tin and cobalt systems. Vanadium forms exten-
sive (and chromium forms limited) liquid immisci-
UUty regions vithi erbium and yttrium. Euteaics
are formed at the rare earth ends of all systems.
Terminal solubility otf all elements (except zirconium)
in the rare earths, and at the rare earths in vanadium
and chromium is low. Zirconium is appreciably solu-
ble In both alpha atid beta zitcanium. Tbe zirconium-
yttrium and -gadolinium systems are similar except
for lower solubilities. Ytterbium forms a compound
with beryllium. No eutectic is observed at the beryl-
lium end, and the ^lability is low. (Author)
Research Chemidals. Inc., Burbank, Calif.
THE METALLUR(JY OF YTTRIUM AND THE RARE
EARTH METALS. PART U. MECHANICAL PROPER-^
TIES, by Bernard Love. Rept. for Oa 58-Oct 59 on
Metallic Materials, Contraa AF 33(616)5905. June 60,
73p. 8 refs. WADO Technical rept. 60-74; Part II.
Order from OTS$ J. 00 PB 171 086
Tensile, compression, fadgue, and impact properties
were determined f<Jr rare earth metals and alloy sys-
tems. Cast )rttriuit, eribum and dysprosium can be
cold worked to impk-ove mechanical properties. All
are easily swaged at 980°C. The resulting structures
are uniform and dense. Strength and duaility proper-
ties are improved Over the cast condition. The cast
rare earth metals »re notch sensitive. Fatigue endur-
ance limits are approximately 40-50% of the corre-
sponding ultimate tensile strengths. Zirconium enters
into solid solution in erbium and results in marked
tensile strengthening. Dispersed, second phase Hr-
conium also contrlliuies to hardening. Recrystalllza-
tlon cjt erbium, cold worked ()0%, occurs at approxi-
mately llOOOC; yttrium at approximately 900OC. Dy«-
prosium and scandium were purified by vacuum dis-
tlllatlan. Attempts to purify yttrium, erbium, and
dysprosium by electron beam melting were not suc-
cessful. Carbon deoxidation procedures decreased
oxygen content slightly. (Aishor) (See also
PB 171 085)
•■. •■ ■. I ' ... •
Sylvania Research Labs. , Bayside, N. Y.
STUDY OF THE PROPERTIES OF ULTRAPURE
NICKEL, byC. W. Hees, L. Castleman, and
G. H. Morrison. Final rept. for 1 Oct- 31 Dec 59, en
Contract AF 19(604)5213. 30 Jan 60, 30p.
TR59- 104-205- 704. 3; AFCRC-TR-60-144.
Order from LC mi$2. 70, ph$4. 80 I PB f 50 280
1 Dec 59.
. 11 r^fs.
Principal reliance is being placed on zone refining for
the meullurglcal preparation of the ultrapure nickel
required for the program. A zone melting apparatus
has been designed and is under construction. Pending
delivery of the apparatus, a number of preliminary
experiments have been undertaken to determine the
feasibility of reducing the impurity level of the nickel
prior to melting, and to altering the distribution coef-
ficients of the impurities during melting. A detailed
investigation has been made of solvent extraction frora
chloride solution as a method of removiDg trace iron
from nickel and the method appears promising. Suit-
able cleaning procedures have been established and
'sfhe necessary equipment and facilities are either
available or on order. Steps are being taken to secuie
emission carborates erf the necessary high purity. The
charcoal absorption trap, while cumbersome to proc-
ess, functions satisfactorily as a booster pump., The
use of thernruil titanium devices is under investiga-
tion. A temperature servo has been designed and is
being constructed. (Author) (See also PB 144 972).
Sfructural Metallurgy and Corrosion
Aeronautical Materials [Lab] Naval [Air Material
Center] Philadelphia, Pa.
ENDURANCE TESTS OF METALS; EFFECT OF
CHROMIUM PLATING, by F. S, Williams. 28 July 42,
52p. 1 ref. Rept. no. AML(M)-595.
Order from LC mi$3. 60. pli»9. 30 PB 150 877
This report released for sale to the public 2 Nov 60.
Applied Mechanics Lab. , Mass. Inst, of Tech. ,
Cambridge.
DETECTION OF FATIGUE DAMAGE WITH
RAYLEIGH WAVES, by Pierre J. Broaens, Nader A. G
Hakimi, and Ghassan R. Khabbaz. Rept. on Contract
AF 33(616)6469. Aug 60, 57p. 28 refs. ARL Tech-
nical rept. 60-307.
Order from CTTSJ 1.50 PB 171 099
94
Some aspeas of the fatigue process in metals are
presented which indicate that the detection of fatigue
dunage by ultrasonic means must be based on concen-
traHoo at ultrasonic energy at the surface of the ex-
amined metal. Rayleigh waves appear to be those d
BKMt interest. They offer the posslWUty d detecting
both fatigue damage prior to crack formation and the
fitigue cracks present after crack formation. These
ultrasonic waves are, therefore, studied theoretically
and experimentally. In the experiments, only low fre-
(Hiency waves (2 megacycles) were used hence crack
detealon was achieved but detection of fatigue damage
prior to crack fornrution was not. (Author)
Oiitli «- Wright Corp. . Caldwell, N. J.
SCME QUANTITATIVE ASPECTS OF FATIGUE OF
MATERIALS, by Harold N. Cummlngs. Rept. for
liay 59-Apr 60 on Materials Applications, Contract
AF 33(616)6552. July 60, 292p. 85 refs. WADD Tech-
nical rept. 60-42. \
Order from OTS H 00 PB 17I\084
b this report are given not only the fatigue properties
of n«ny structural materials but also the "static" prop
ertles and such other supplementtry information as
was given In the references consulted. The dau are
In general from room temperature tests, but a few data
are given on tests at higher temperatures. The data
are presented in tables and on curves, supplemented
by brief discussions In the text. (Author) (See also
FB 161 145)
Institute for the Study of Meuls, U. of Oilcago, 111.
CRYSTAL DISTORTION IN MAGNETICJ COMPOUNDS,
by Junjlro Kanamorl. Technical rept. no. 2 on Con-
tract Nonr-2121(13). Nov 59, 39p. 21 refs.
Order from LC mi$3. 00, ph$6. 30 PB 150 468
The crystal distortion which arises from the Jahn-
Teller effect is discussed in several examDles. In the
case of cotnpounds containing Cu2+ or Mn^* at octa-
hedral sites, the lowest orbital level of these Ions Is
doubly degenerate in the undlstorted structure, and
diere Is no spln-orblt coupling in this leveL It is shown
d>at. Introducing a.fictltious spin to specify the degen-
erate orbital states, we can discuss the problem by
analogy with die magnetic problems. The "ferromag-
netic" and "antlferromagnetlc" distortions are dls -
cussed In detail. The transition from the distorted to
the undistorted structure Is of the first kind for the
former and of the second kind for the latter. Higher
approximations are discussed briefly. In compounds
like FeO, CoO and Cucr204. the lowest oroual level
la triply degenerate, and the spln-orblt coupling is
present In this level. In this case the distortion is de-
peiktent on the magnitude of the spln-orblt coupling ire-
lailVeto the strength of the Jahn- Teller effect term.
The distortion at absolute zero temperature and Its
temperature dependence are discussed. (Audior).
Institute for the Study of Metals, U. of Chicago. HI.
MAGNETIC TRANSITIONS AT LOW TEMPERATURES,
by J. W. Stout. Technical rept. no. 1 on Contract
Nonr-21 21(13). Nov 59. 20p. 31 refs.
Order from LC ml$2. 40. ph$3. 30 PB 150 467
Some examples of magnetic transitions in salts of di-
valent ions oif manganese. Iron, cobalt and nickel are
discussed.
Manufaauring Labs., Inc., Cambridge, Mass.
MARTENETRON MATERIALS FOR USE IN BINARY
RESISTANCE DEVICES, by Paul J. Foplano. Rept. on
Electronic Concepts of Information Handling, Contract
AF 33(616)6414. Jan 60, 48p. 11 refs. WADD Tech-
nical rept. 60-273. _^
Order from OTS U. 25 PB 171 066
Certain metallic systems which exhibit a comjjuier-
type hysteresis loop, wherein a discontinuous change
in resistance occurs at different temperatures depend^
ing on whether the temperature is being increased or
decreased, are referred to as martenetron materials.
The present Investigation is concerned with the practi-
cability of employing such materials In nonlinear re-
sistance devices. The type of solid- sute transforma-
tion in metallic systems upon which this device Is
based is known as a martensitic or diffusionless reac-
tion. The selection of a wide range of potential mar-
tenetron materials with martensitic reactions has been
carried ou by surveying the literature. From this
list, those systems felt to be of particular interest
were investigated. In at least one system (iron-nickel^
several compositions have been studied in considerable
detail to correlate the effect of composition on the
martensitic reaction. In each system, the resistance
change, the critical temperature range, and the
hysteresis effects (if any) have been determined. With
typical high and low temperature materials, the
BtabiUty after repeated cycling has been measured
and metallurgical observations such as microhardness
and metallography have been made. The effea of
quenching media on switching rate, the heat require-
ments, and some possible methods of packaging have
been investigated. (Author)
Massachusetts Inst, of Tech., Cambridge
EXPERIMENTAL EVIDENCE FOR MARTENSITIC
EMBRYOS, by M. H. Richman (Doctoral thesis),
M. Cohen, and H. G. F. Wilsdorf (Franklin Inst. Labs.).
Technical rept. no. 3 on Contract Nonr-l841(35) and
rept. on Contraa N5orl-78, Task XIV. 2 Nov 59, 6p.
7 refs
OrderfromLCmiJl.SO. phSl.SO PB 150 850
Massachusetts Inst, of Tech. . Cambridge.
THE TRANSFORMATION CHARACTERISnCS OF A
BETA-PHASE TITANIUM ALLOY, by R. A. Rawe,
J. M. Dupouy, and M. B. Bever. Technical rept. no. 3
on Phyaical Metallurgy of Titanium Alloys, Contract
Nonr- 184 1(02). 20 Nov 59, 21p. 8 refs. DSR-7433;
AD- 229 740. »..«««.
Order from LC mi$2.70, phM.SG PB 150 855
The transformatlot behavior of a titanium alloy con-
taining 11% chromium, 13% vanadium and 4% aluminum
ha#been investigaoed by hardnesa n^easurements,
x-ray diffraction and metallography. The solution
treated alloy consisted entirely of beta phase. Aging at
temperatures between 1(XP and IISO^F increased the
hardness; the rate« of hardening suggested that beta
decomposed by dif|erent modes upon aging above
105(W and below ^OCP? and by a combination of these
modes between these temperatures. X-ray diffraction
analysis indicated that in the upper -temperature range
the reactions P-»Pr,"^ »-»Pu ♦ a-*TiCr2 occurred, while
in the low- temper alture range, the transition phase
omega appeared aitl the reactions were p-»Pr*<^-»P^*a
■Two modes of decomposition were also suggested by
the microstructuras. A TTT diagram is proposed on
the basis of these results. The hardening is attributed
to the predfritatioq of omega and alpha and to solid
solution hardening of the remaining beu. An increase
in solution time did not change che hardness at the
solution treated specimens but decreased the rate of
subsequent hardening. Cold working of solution treated
specimens accelerated hardening and raised the
^hardness level attained. (Author) (See alao
PB 144 956)
Michigan U. Coil^ of Engineering, Ann Arbor.
THE EFFECT OF SURFACE TENSION OF A LIQUID
METAL ENVIRONMENT ON THE FRACTURE
STRENGTH OF SOLID METALS, by D. A. Kraal,
S Floreen and othdrs. Technical rept. on Contract
AF 49(638)422. Jul* 60. 301p. 8 refs. 2782- I-F;
APOSR-TR-60-116:
Order from LC nil|ll. 10, ph$47. 10 PB 150 637
This report Is divided Into three sections. Each section
covers a specific aspect of the relationship of surface
and environments akiid their effects on the mechanical
properties of solids: (1) effects of some liquid metal
environments on the fracture of copper. (2) the effect
of strain on the surface energy of solids. (3) the effect
of tensile stress on dihedral angles in leaded copper.
U. . Miir
Minnesou U. , Mfcineapolls.
FATIGUE AND ffTKESS RUPTURE PROPERTIES OF
INCC»ffiL 71 3C, V-57C AND TITANIUM ALLOYS
7A1-3MO-T1 AND ICST 821 (8Al-2Cb-Ta-Tl). by
A. E. Cera and A. ▲. Blatherwick. Repc. for Jan 58-
Dec 59 on Materials Analysis and Evaluation Tech-
niques, Contraa Ap 33(606)6828. July 60, 92p.
17 refa. WADD Technical rept. 66-426.
Order from OTS JX 25 PB 171 064
I
Fatigue, rupture and creep data at various tempera-
tures obtained at various alternating and mean stress
combinations are presented for the alloys Incooel 71 SQ
V-57C (modified Si^jer A-286), 7Al-3Mo-Tl and MST
821 (8Al-2Cb-lTa-Ti). The tests were performed on
unnctched specimens and for Inconel 71 3C also on
nocched specimens ^vlng a theoretical stress concen-
tration factor of 2.f . The data are presented as S-N
curves and streM-tange diagrams to ahow the effea
of temperature, ratio of alter nating-to- mean stress,
stress magnitude and specimen notch on the fatigue and '
rupture properties. (Author)
Naval Research Lab. , Washington, D C.
CORROSION OF METALS IN TROHCAL ENVIRON-
MENTS. PART 5: STAINLESS STEELS, by
B. W. Forgeson. C. R. Southwell, and A. L. Alex-
ander. Interim rept. 19 Sep 60, 24p. 15 refs. NRL
rept. 5517.
Order from OTS $0. 75 PB 161 749
Over a period of eight years, six stainless steels have
been exposed to underwater and atmospheric environ-
ments in the Panama Canal Zone. Stainless steels are
severely pitted during sea water Immersion; the meta
tide immersion produced one-fourth to one-tenth the
pitting of continuous Immersion, and the metals were
practically unattacked when submerged in fresh water.
Greater pitting attack in tropical than temperate seas
may be the result of heavy marine fouling. The type
and extent of pitting attack of stainless steels is com-
pared with phosphor "bronze and several structural
steels. Stainless steel is not recpmmended for sea
water service where perforation of structure Is a con-
sideration; it was inferior to phosphor bronze and to
the structural steels. In fresh water, stainless steels
are superior to ordinary steels and equal to phosphor
bronze which is noncorroslve in this environment.
Tropical atmospheres appear to be no more corrosive
to suinlets steel than temperate climates; the marine
effects are slightly greater than the inland. However,
precautions should be taken to eliminate cracks where
passivity-destroying «gents could accelerate pitting
atuck. (Author)
Nuclear Metals, Inc. , Concord, Mass.
BERYLLIUM RESEARCH AND DEVELOPMENT IN
THE AREA Q? COMPOSITE MATERIALS, by
Jacob Greenspan, Gerald A. Henrikson, and Albert R.
Kaufmann. Rept. for 15 June 58-14 June 59 on Metallic
Materials, Contract AF 33(616)5912. July 60, 121p.
33 refs. lNMl-9404] WADD Technical rept. 60-32.
Order from OTS $2. 75 PB 171 083
CXictillty of some beryllium composite materlala is
compared to the ductility of beryllium itself. Bend duc-
tility in sheet beryllium as a fuiK:tlon of sample width
and thickness revealed that grain orientation also played
a part. Strip composites consisting of alternate strips
of beryllium and aluminum or silver filler metal were
investigated. Clad composites did not institute unusual
changes in the composites' ductility. However, clad-
ding appeared significant as a "failwafe" and surface-
protection medium. Beryllium may be cladded by roll-
ing or extrusion when a thin silver Interlayer is pre-
sent between core and cladding. Silver or alumlniun
coating did not change unusually the tensile strength
or ductility of beryllium composites. Methods for pol-
ishing beryllium surfaces are described. (Author).
NUCLEAR PHYSICS AND
NUCLEAR CHEMISTRY
■urvsu of Naval Peraotmel, Waahlngton, D. C.
lASIC NUCLEAR PHYSICS. 1958, 270p. NAVPERS
10786.
Order from LC mllU. 10, ph$41. 10 PB 152 233
This report releAsed for sale to tbe public 15 Nov 60.
TlUa publication. Principles of Nuclear Physics, has
^0ffn issued as a source of background information for
students attending the nuclear courses of tbe Special
WMfwns Training Group, AFSWP. Students whose
training in physics is incomplete, or who lack an un-
derstanding of the unclassified aspects of nuclear phe-
nomena as revealed by modem research, will find the
information in this publication of value In comprehend-
{afi course material.
((Juantum, Inc.. Walllngford, Conn.)
THE FORMATION OF NEW POLYMERS USING
IONIZING RADIATION. Quarterly technical rept.
BO. 1, 12 Sep-12 Dec 58, on Contraa DA 44-009-eng-
S723. (1959] lip. AD-226 148.
Order from LC ml$2. 40, pli$3. 30 PB 152 648
This report released for sale to the pobllc 7 Nov 60.
The objectives are: (1) the formation of new and
structurally useful polymeric materials, and (2) the
formation of Uquid or resinous coating materials.
Quantum, Inc., Walllngford. Conn.
THE FORMATION OP NEW POLYMERS USING
IWIZING RADIATION, by R. F. Horan. (Quarterly
technical rept. no. 2, 12 Dec 58-12 Mar 59, on Con-
traa DA 44-009-eng-3723. [1959) 37p. 17 refs.
Order from LC ml$3. 00, ph$6. 30 PB 152 649
This report released for sale to the public 7 Nov 60.
Radiation Induced polymerization involves only the
pure starting compounds and should therefore produce
materials of intrinsically higher thermal charaaeris-
tics and dielectric strength properties. Eight of the
thirty-five reactions reported to date have produced
polymers of some promise. Melting points of these
polymers are generally on the order of 300°C. Pro-
posed struaures for these produas involve the highly
stable P-N cyclic struaures as in the trlallycyanu -
rate - phosphonltrilllc chloride copolymer; phenyl-
So-C- chains as in polymers formed with triallylcy-
aaurate-dlphenyldichlorofitannane. Analysis of reac-
don mechanisms has been arrived at both through a
study of reports in the literature concerning radiation
effea s on analogous chemical compound and through
a correlation of the known fundamental aspects of
radiation interaaion with matter. Infra-red absorp-
Upn spectra of control aod irradiated samples are
supplied by ERDL. Dau from these curves has sup-
ported the proposed reaction mechanisms. (Author)
(See alw) PB 152 648)
Cosmic Rays
Air Force Missile Development Center. Holloman
AFB N Mex.
AIRBORNE DETECTION AND ANALYSIS OF PRIMARY
COSMIC PARTICLES WITH A SCINTILLATION DE-
VICE, by dePaul J. Corkhlll and Rudolf A. Hcrffman.
July 60. 17p. AFMDC-TN-60-12.
Order from LC ml$2. 40. ph$3. 30 PB 150 371
This paper presents data derived from telemetered in-
formation from a primary cosmic particle detecting
device. The data are preliminary in nature in that com-
parison between the cosmic particle spectrum (as
shown by the mechanical detector) has not as yet been
made with similar information provided by nuclear
emulsions exposed to regions of primary cosmic par-
ticles simultaneously with the mechanical device.
(Author).
Iowa State U. , Iowa City.
OBSERVATIONS PERTAINING TO COSMIC RAY
ORIGIN, by IClnsey A. Anderson. [1959] 19p. 14 refs.
Rept. SUI-59-23.
Order from LC ml$2. 40. ph$3. 30 PB 150 518
Assuming the other stars in the galaxy supply ener-
getic particles in the same manner as the sui;! the high
energy cosmic radiation might be maintained^if the
Fermi acceleration process provided a high rate of
energy gain per gas cloud collision. However calcu-
lations show that a high rate of energy gain does not
lead to the flat energy spectrum exhibited by the ga-
lactic cosmic rays. Also, the absence of fast solar-
accelerated helium Indicates that if the sun Is to be a
typical injector of cosmic radiation the energy gain in
the galaxy would have to be rapid, a requirement
again Inconsistent with the spectral shape calculation.
It therefore t^ipears that using the sun as a model cos-
mic ray injector together with the Fermi acceleration
process is not a suitable means of {nroducing the ga-
lactic cosmic radiation. (Author).
Elementary Particles
Army Chemical [Research and Development] Labs. .
Army Chemlc*l Center. Md.
THE FEASIBILITY OF USING A REACTOR AS A NU-
CLEAR-WEAPONS SIMULATOR FOR SOIL-ACTIVA-
TION STUDIES, by John H. McNellly and Edward F.
Wilsey. Rept. for Apr 58 on Protection Against Radio-
logical Hazards. June 60, 28p. 10 refs. Radiological
Lab. Technical rept. CWLR 2380; AI>238 %1.
Order from LC mi$2. 70. phM- 80 PB 152 000
The experiment described uses a nuclear reactor as a
neutron source to simulate a nuclear weapon for study-
ing the residual gamma activity induced In soils. The
results obtained are then compared with results obtained
from a nuclear detonation. The reactor- irradiation and
nuclear- detonation dau are in good agreement for so-
dium; however, the results with manganese are between
35% and 50% higher for the reactor Irradiation than for
the nuclear detonation. The behavior of the diernul-
96
neutron flux with reUtloo to depth was very ^milar at
depths greater than 15 cm. The nuclear- detonation neu
tron-flux dau showed a peaking <rf the thernnal flux at
about 8 cm, but the$e peaks were not seen in die nuclear
reactor data. This traa explained by the neutron- spec-
trum differences and the lack of optimum experimental
conditions because (jf a rainstorm during irradiation by
the reactor. Although the feasibility df using a reactor
in place of a nuclear detonation for studying neutron-
induced activities ini soU looks promising it cannoc be
definitely established by the results of this study.
(Author).
Durham U. (Ot. Bx^).
VARIATIC»IS OF THB SEA LEVEL MUON FLUX, by
P. V. O'Connor and A. W. Wolfendale. Technical noce
na 1 on Ckwtract Af 61(052)27. 26 Ian 60, 2*>. 5 refs
AFCRC TN-60-283.
Order from LC ml$t 70, phK 80 PB 150 937
The characteristics are described ol a cosmic ray spec-
trograph which uses • solid iron nuignet with Gelger
counters as detecting elements. The instrument is be-
ing used to study the variations of the ^- meson flux at
sea level, with direction and time, as a function ot mo-
mentum. Preliminary results are reported ol the meas-
urement at the pressure coefficient at the ^- meson flux
for three bands o^ momenta having median values 2. 9
GeV/c, 4. 5 GeV/c aad 8. 6 GeV/c. Ualng a simple one-
term regression formula the corresponding pressure co
efficients are 0. 25% mb" ^ 0. 15% mb'^ and 0. 11% rab^.
These values bear a constant ratio to the expected co-
efficients, as would l>e expected- from an analysis based
on the known mechanism of the propagation of cosmic
rays and the propertiies of the atmosphere. (Author).
Maryland U. , College Park.
STRANGE PARTICLB DECAYS AND THE NATURE
OF WEAX INTERACTIONS VOLUME I, by Jbgesh C
Psil. Rept. on Contract AF 49<638)2'^. Sep 60, 152p.
146 refs. Physics Dept. Technical repc no. 193;
fAFOSR] TN-60-105U.
Order from LC mi$7. 50. ph$24. 30 PB 152 058-1
Chap. L bttroductlon: Nature of interactions at ele-
mentary particles; axp>erimenul foundation ot univer-
sal four fermion interactions between nucleoas and
leptons; theoretical frame -work of universal four
fermion interaction; the strange particles; general
features at strange particle decays.
Oiap. 11. The decay of the A-lwperon: Scheme at
interaction; preliminaries on A -decay; prevluus
work (Tbe CMS- Analysis) and success; needs for new
look; a new class of diagrams; evaluation at the
matrix element of the new diagram
C3wp. III. The decay frf the K- me son: The leptonlc de-
cay modes at K-mescm; the asymmetry In the energy
distribution of K * — ^ ir *♦ »^* ir*^-decay.
Maryland U. , Oollegt Park.
STRANGE PARTICLE DECAYS AND THB NATURE
OP WEAK INTERACTIONS VOLUME II. by Jbgesh
C. Pati. Rept. on Contract AF 49(638)24. Sep 60,
143p. 43 refs. Physics Dept. Technical rept. no. 193;
fAFOSR] TN-60-1051h -
Order from LC mir. *). ph$22. 80 PB 152 058-2
98
CJiap. IV. The possible existence at an hitermedlate
vector bosoa: S^ieculatloa; general effects at the noo-
locallty in four fermion Interactions; absence ot
^— •« ♦ "y -decay; the assignment of Lepton Numbers
and the nature of the neutrino; effects of non- locality
on the energy spectra in lCe3 (Km3) -decays; effects
of non-locality on the decay of the A -hyperon
Appendix: Notations; The anguUr dlatrlbutioo of ploos
and kngltudlnal polarization of nucleoo in the decay
of A -hyperon; Matrix elements of various K- meson
decay modes; Decay rates of various K-me8oo-mode«
Energy spectra in ICm3 and ICe3- decays for local and
non local four fermion interaction; Matrix element cf
rhe-sinsle. neutron- intenn^iate state dUoram for
/^ — ♦N-f'T-decay with intermediate vector boson. (See
alsoPB 152 058-1)
Fhytical Research Ub. , Space Itech. Labe. . Inc. .
Los Angeles, Caltf.
THE NEUTRON PRODUCING MECHANia* IN TRANS-
VERSE PINCHES by V. Jotephson, M. H. Dfczey, and
R. F. Wuerker. Rept. on Contract AF 04(647)309.
9 Aug 60. 14p. 12 ref». STL/TR-60-0000- 19258.
Order from LC ml|2. 40. ph$3. 30 PB 150 776
Bxperlntentt performed on a transvel-se pinch assem-
bly show that the presence of a longitudinal magnetic
field Inside cf a conducting plasntu and in the reverse
direction to that cf the external pinching field results
in the generation of the m « 0 (sausage) instability
mechanism. This inttablliry mechanism can generate
high electrical fields which will accelerate deuterons
to energies sufficient for, neutron production in deute-
rium plasnus. Subsequent to the blow-up of the insu-
blllty, the plasma -fielil configuration ii such ttat the
accelerated deuterons can continue to circulate in sta-
ble orbits until lost by neutron producing collisions or
by dtffusion out of the ends of the geometry. (Author)
UppsaUU. (Sweden).
AKHPROTON ANNIHILATIONS IN COMPLEX NU-
CLEI, by A. G. Ekspong. A. Frisk and others . Tech-
nical noce no. 1 on Contract AF 61(052)13, phase G.
[1960] 83p. 44 refs. AFOSR-[TR]-60-937.
Order from LC nai$4.80. ph|13.80 PB 150 351
356 antlproton annihilations in nuclear emulsion have
been investigated . The average pion multiplicity and
total energy in the primary process were found to be:
atrest<Ny> -4.68t0.12. <BV> -39l±10MeV
in flight <N«>-5. 11 ±0.12, <Eir> •390±9 MeV at
<rp> -166 MeV. The results for KK -production are:
percentage at KK - pair* <Njg^ "3-2% average
ehergy <Ejj^> -33 ± 22 MeV/iur .
Virginia U. , Charlottesville. Vs.
RESEARCH STUDIES WITH A I -MEV VAN OT
GRAAFF MACHINE, by Frank L. Herefoni Annual
rept. on Contracts AT (40-1)- 1754 and DA 36-034-ORD-
2046. June 60, 16p. 7 refs. OOR rept. 1510. 8-P;
AD-239 923.
Order from LC ml$2. 40, ph$3. 30 PB 150 406
Instruments and Installations
Army Chemical Research and Development Labs. ,
Army Chemical Center, Md.
A SURVEY OF SOLTO-STTATE GAMMA/NEUTRON
CBTECnON SYSTEMS, by RusseU Gmlnder, John W.
Kinch and others. July 60, 64p. 197 refs. CRDLR
3020; AD- 241 399.
^ from OTS $1.75 PB 171 124
This analysis, which is based on ah extensive llters-
ture search and on personal contacts with some of the
leading researchers in solid-state radiation detection,
presents the major advantages and linUtations of many
loUd-sute detection systems. Some recently pro-
posed and partially studied systems are also dls-
cuesed. The systems were classified according to the
radiation -induced effea utilized for measuremeiK.
(Author)
Kellogg Radiation Lab. . Calif. Inst, of Tech. ,
Pasadena. fi
PRESENT STATUS OF SEMICONDUCTOR PARTICL^
COUNTERS, by C. A. Barnes. Technical rept. on
Contract Nonr-220(18). 23 Nov 59. 8p. 9 refs.
AD- 229 706. _ ,^^ ^^,
Order from LC mi$l. 80, ph$l. 80 PB 150 473
U
Naval Radiological Defense Lab. , San Francisco,
CaUf.
A STUDY OF THE REPRODUCffilLITY OF IONIZA-
TION READINGS OBTAINED WITH LANDSVERK
MODEL L-65 200-mr POCKET CHAMBERS, by
B. W. Shumway, H. H. Hechter, and W. G. MiUer.
4 Ian 60. 18p. 5 refs. Research and Development
technical rept. USNRDL-TR-399; AD- 233 424.
Order from LC ml$2.40. ph$3. 30 PB 152 677
Thla report released for sale to the public 16 Nov 60.
A study was made of the reproducibility of ionization
readings obtained wHh Landsverk 200-mr chambers
used in conjunction with modified Model L-62 charger -
readers. The errors considered were the differences
between radiation trials, between 2 charger -readers,
between chambers, and between 2 methods of reading.
These were measured at levels of exposure of 33, 100,
and 167 mr. Estimates of the errors assoclsted with
the degree of exposure indicated that the variance of
the readings was proportional to the scale reading. It
was observed that eonae chambers did not maintain a
given calibration though others were excelleiB. The
modified charger -readers were found to be inter-
changeable, and readings could be reproduced at full
scale with an error of about 2-1/2%. A systenutlc
error was observed when the meter of the charger-
reader was set at zero prior to Introducing a chamber
to be read. A method of reading in which an offset
from zero was made prior to introducing a chamber
resulted in nearly eliminating the error. There was a
variation in the readings obtained with different
radiation trials. (Author)
Texas Nuclear Corp. , Austin.
A PROTON -RECOIL ORGANIC SCINTILLATION
SPECTROMETER AND WVECTIGATION INTO A
VARIABLE THRESHOLD SPARK COUNTER, by John
B. Ashe, WllUam E. Tucker and others. Rept. for
18 Feb 59-17 May 60 on The Chemistry and Physics of
Materials, Contraa AF 33(616)6362. Jiily 60, 35p.
31 refs. WADD Technical rept. 60-293.
Order from OTS $1.00 PB 171 120
A scintillation detector is described which has the
ability to differentiate between neutrons and gamma
rays by means of the different decay times of recoil
proton and Compton elearon scintillations. This de-
tector has been Incorporated into a neutron spectrom-
eter which is highly insensitive to gamma rays over a
deteaable neutron energy region of approximately 0. 8
Mev to greater than 17 Mev. Dau obuined with the
spectrometer are presented. In addition to the scin-
tillation deteaor, investigations into the feasibility al
using a spark counter as an energy sensitive neutron
detector are also described. The results of these in-
vestigations are discussed and representative dau
are presented. (Author)
Nuclear Engineering and Power
Ballistic Research Labs. , Aberdeen Proving Ground,
Md
BLACT EFFECTS TESTS OF A ONE -QUARTER
SCALE MODEL OF THE AIR FORCE NUCLEAR
ENGINEERING TEST REACTOR, by Wilfred E. Baker
and James D. Patterson, II. Ke^. on Contracts
AF 33(616)3471 and AF 33(616)56-83. Mar 57, I87p.
1 ref. Rept. no. 1011; AD-129 167.
Order from LC ral$8.40, ph$28.80 PB 148 647
TUs report released for sale to the public 17 Nov 60.
This report presents the results of a series of ten
simulated nuclear power excursions conducted within a
one-quarter scale model of the Air Force Nuclear
Engineering Test Reaaor. The objective of the tests
was to simulate, as closfcly as possible, large nuclear
power excursions of die potential predicted by the
"Borax" test dau and to experimentally evaluate the ^
effects of the resulting blasts on the reactor structure
and safety shell. Explosives and propellants were
used to simulate the power excursions. Measurements
were made of the time histories of pressures, strains,
displacements and accelerations at various locations
within the model. It is concluded that the reactor de-
sign will, with minor modifications, safely contain an
explosively- released energy at 1000 n»egawatt-
seconds. This is approximately three times the
maximum energy release In the maximum credible
power excursion for the AF NETF reactor. The
accuracy of simulation of an excuraion by explosives
and propellants and the applicability and Umlutions of
scaling of blast loading and structural response are
discussed. (Author)
Coovilr, Fort Worth. Tex.
REACTOR POWER CALCULATOR, by J. R. Gardner.
Rapt, on Contract AF 33(600)32054. 30 Apr 58, 24p.
NARF-58-18T; MR-N-136; AD-159 902.
Order from LC T$i$2.70. pb$4.80 FB 152 358
This report released for sale to the pubUc 28 Oa 60.
An electromechaaical power calculator waa developed
for use with the aircraft shield teat reaaor and the
ground test reactor. The computer solves the equation,
P •QAT, by means at a flow rate amplifier which aup-
plles a voltage that is hnear with flow rate, and a null
balance servo syatem which produces a potentiometer
shaft position that Is linear with the temperature dif-
ferential existing between the coolant water flowing Into
and o« of the reactor. The computer contains its own
power supply and reference supplies as well as a self-
contained low-flow alarm system. One version uses
60 cycle power, while another waa constructed for
400 cycle power. (Author)
J.
Coorair, Fort \torth, Tex.
REMOTE INSPECmON OF AIRCRAFT WITH TELE-
VISION, by W. A. Baird. Kept, on Cootraa
AF 33(600)32054. 12 May 58, 51p. 9 refs. NARF-
58-19T; MR-N-20P.
Order from LCm|$3. 60, pli$9. 30 FB 152 359
This report released for sale to the public 28 Oct 60.
A preliminary experiment was performed in tbe^uae of
cloaed circuit black and white televiaion to inspect air-
craft. Television equipment waa used to evaluate the
effea d lighting, camera position, and lenses on the
inspection problem. An industrial closed circuit televi-
sion system was set up at a B-47 airplane. The time
required and the accuracies obulned were compared be-
tween normal (dlrta visual) Inspectiona of certain
items and remote Inspections made with television
equipment . The effectiveness of televiaion inspection
was studied in a series of experimental set-upa. For
each set-up, the iaterrelatlonahlpe of the factora which
influence picture quality were atudied. A detail analy-
sis is presented of optical phenomena and televiaion
equipment characterlsucs. Subjects treated include
depth of field, resolution, video bandwidth, lens aya-
tema, and lighting, The experiment ahows that remote
inapectlon of aircraft with televiaion is feaalble. Re-
sults indicate that off-the-shelf type televiaion compo-
nents can be obtained which are satiafactory for this
application. Only auch items aa die lighting equipment
and the camera boom and dolly will have to be of ape-
daldeaign. (Authdr]i
I
Nuclear Reactions
Facult^ dct Scienbea , Onay (France).
RBLATIVISnC DBUTBRON WAVE FUNCTION. H. by
Gourdin and J . Tran Thanh Van. Technical note
no. 19 on Contract AF 61(052)173. [1960] 22p. 4 r«fs .
AFOSR-TN-60-917L
Order from LC mil?. 70, ph$4. 80 FB 150 349
M
Carrying on research on the deuteron relartvistic wave
function, Bethe and Salpeter's relativlsclc wave equa-
tion has been applied to the bound system of two
particles with spin 1/2. After some very slight ap-
proximations , the s<}lution of the Infinite system of
coupled integral equations enables one to find the
explicit structure of the wave matrices correspondliw
to the S and D sutes . The percenuge of D sute ob-
tained is in good agreement with the experimental
result. (Author)
Institute of Mathematical Sciences, New York U. .
N. Y.
A HARTREE SELF CCWSISTENT METHOD FOR THE
SCATTERING OF POSITRONS BY HYDROGEN ATQMJ
Richard S. Rufflne. Rept. on Contracts AF 19(604)4555
and DA 30-069- ORD- 2581. Apr 60, 69p. 14 refs. Re
search rept. no. CX-48; AFCRC TN-60-441.
Order from LC nUj3. 90, phJlO. 80 PB 150 944
We have developed a method for generalizing the Har-
tree self consistent scheme used for atomic structure
problems so that it may be used for problems of the
scattering of electrons or positrons by atomic systems.
This method has been used to calculate the scattering
of poaltrona by hydrogen atoms. -For this problem, we
have three coiqiled differential equations. The effec-
tive Interaction is made up of a sum of induced multi-
poles. We have confined ourselves to the dipole in-
teraction and then integrated the aystem of equations
for s-wave scattering self consistently on a high speed
computing machine. The system of equations reduces
to the adlabatic approximation if we assume that there
Is negligible penetration of the atom by the incident
particle. The results at the calculation show that diere
la a large attractive potential between the positron and
the atom for very low incident energies, in agreement
with the recent results of ^ruch and Rosenberg. In
fact our results lie somewhat between the static ap-
proximation and die lower bounds published by these
last authors. It la encouraging that the correlations
responsible for the attractive potential do show up.
Presumably if spherical distortion and higher induced
multipoles of the atoms were included the results
would improve. The method is ^jpllcable in principle
to the problem of the acatterlng of electrons by hydro-
gen and by more complicated atoms. (Audior).
Pittsburgh U. , Pa.
ELECTRON CAPTURE AND LOSS BY HYDROGEN
ATCArfS IN MOLECULAR HYDROGEN, by R. Curran
(Doctoral tbeaia) and T. M. Donahue. Technical rept.
no. 9 on Captive- loaa and Ionization Cross -Sections of
lona and Neutral Partidea, Coatract Noor- 624(06).
Nor 59. 20p. 11 refa.
Order from LC mi$2. 40, pfa|3. 30 FB ISO 523
Meaaurementa of the alngle electron capture and loaa
crosa sectiona for atomic hydrogen in molecular by-
drogen are reported for atoma of energlea 4 to 35 Ker.
Pealca in the loaa croaa aection are found which appear
to be aaaodated with the formation of negative iooa is
the target gaa. (Author)
100
.f^p.--^
-'■ -'.-^^
Sarah Mellon Scalfe Radiation Lab. , U. of Pittsburgh.
AN ANALYSIS OF (d. t) PICK-UP REACTIONS, by
Wlia Imp^rio Hamburger (Master's thesis) land)
FINITE RANGE CORRECTION IN DISTORTED WAVES
CALCULATIONS, by Norman Austem. Technical rept.
BO 2 on Precision Scattering ot Nuclear S^rtlcles. Con-
tract Nonr-624(10). Nov 59. 52p. 26 refs. ^^B.230 172.
Onler from LC mi$3. 60, ph$9. 30 PB 150 516
A comparison is made between (p. d) (or (d. p)] and (d.l)
pick-up reactions involving transitions between the same
nuclear levels. Cases are studied for nuclei from A«6
to 25 (also A«l 17). for orbital angular momentum trans
ler 1-0. 1 and 2, and for incident enei^es of the order
of 15 Mev. It is found that if the differdniial cross sec-
tions of the corresponding (d. p) and (d. t) reactions are
plotted as functions of momentum transfer the curves
differ by a factor independent of angle. Because of the
proportionality between the curves in the.forward direc-
tion, it is possible to obtain an expression for extract-
ing the stripping reduced width of (d, t) reactions. This
reduced width corresponds to the reduced width of the
same transition when studied by a (d. p) process. No
emphasis is placed on the interpretation of the results
in terms of the structure of the trition. A general and
unified approach for estimating finite range corrections
In reaaions such as (n. n), (n. p). (d. p) is also pre-
sented, and the use of distorted wave functions en-
hances these corrections. The method is suiuble for
incorporation into machine calculations of these re-
actions. (Author)
Radioactivity
Army Engineer Research and Development Labs. .
Fort Belvoir, Va.
SOLUBILITY CHARACTERISTICS OF RADtOACHVE
BOMB DEBRIS IN WATER AND EVALUATION OF
SELECTED DECONTAMINATION PROCEDURES, by
Harry N. Lowe, Jr. , Don C Lindsten and others.
12 Feb 59, 85p. 2 refa. Technical rept. 1569 -TR;
AD-212 440. -• . _ ^^^^^
Order from LC mi$4^»0. phjl3. 80 PB 152 65C
This report released for sale to the public 7 Nov 60.
The more important results of these experiments are
summarized as follows: (a) The radioactive debris re-
sulting from a nuclear detonation was only sparingly
soluble in water, (b) The solubUity of the radioactive
debris increased as the pH of the solvent was lowered,
(c) Filtration through dense filter pads or through
bonded ceramic elements effectively removed sus-
pended radioactive debris from water. Such filtration
followed by deminerallzation with a column of mixed
bed ion exchange resins removed both suspended and
dissolved contaminants, (d) Coagulation foUowed by
fHfration was effective in removing suspended contam-
htants from water but was relatively ineffective in re-
moving the dissolved components of the radioactive
debris, (e) Lime and lime-soda softening were rela-
tively ineffective in removing the dissolved compo-
nents of radioactive debris from water. (0 Clay was
not effedtive in removing the dissolved conuminants
from water although earlier research had indicated
that significant removals of many radioisotopes can be
thus achieved, (g) Coagulation followed by filtration
followed by deminerallzation by ion exchange resins
removed all of the contaminants, suspended and dis-
solved components alike. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
THE USE OF PLASTIC SHIELDS TO REDUCE
PERMANENT NUCLEAR RADIATION DAMAGE, by
Edwin T. Hunter. 15 June 60. 18p. 5 refs. USASRDL
Technical rept. 2123. «...«^o.
Order from LC ml$2. 40, ph$3. 30 PB 150 687
Permanent alteration in DC electrical charaaeristics
of germanium, homogeneous base, pnp, power transis-
tors was determined as a function of the thickness of
epoxy-type shielding nwterlal surrounding the device.
Exposures were made on the Godlva reactor at Loa
Alamos Scientific Laboratory, Los Alamos, N. Mex.
Results indicate that most of the permanent damage is
caused by fast neutrons, with a smaller pert of the
damage being caused by some other component of the
radiation, apd that the epoxy shields thermalize many
of the fast neutrons, thereby reducing the permanent
damage suffered by the transistors. The subsequent in-
crease in thermal neutrons and gamma -rays inside the
shields will probably have an effea on the transient
alterations in electrical (Characteristics of the devices,
but this facet of the investigation was not studied at
this time. (Author)
Bureau of Yards and Docks, Washington, D. C.
RADIOACTIVITY IN WATER SUPPLY AND WASTE
WATER SYSTEMS: PEACETIME DETECTION AND
CONTROL. June 60, 88p. 68 refa. Technical pub.
NAVDOCKS TP-Te-6.
Order frikn OTS $2. 25 PB 171 091
This pid>Iication presents the latest Information on the
detection, handling, and disposal of such peacetime
radioactive contamination in water supplies and wastea
These data have been prepared for the guidance of
management personnel who are concerned with the de-
algn, control, and operation of water siqjply and waste
water systems where radioactivity Is involved.
Convair, Fort Worth, Tex.
FISSION PRODUCTS FIELD RELEASE TEST. 1.
Rept. on Contraa AF 33(600)32054. Sep 59, 477p.
17 refa. NARF-59-32T; FZK-9-140: AFSWC TR-|
59-44; AD- 228 267.
Order from LC ml$ll . 10, ph$72. 60 PB 152 806
This report released for aale to the public 17 Nov 60.
A test was performed to check and resolve uncertain-
ties in the currently used methods of safety analysia
for nuclear aircraft. The test was made to evaluate
release percentages, airborne radioactivity, and dif-
fusion and deposition characteristics of fission prod-
ucts from melted aircraft reaaor fuel elements. A
COTollaf y objealve waa to determine the r«entlon and
distribution of the released fission produas in animals
located within the release network. A highly instru-
mented fan- shaped grid having 7 concentric arcs with
101
a maxlinum radiua at about 5 miles was used to collect
cloud diffusion, meteorological, radiological, radio-
biological and radioactivity deposition data. Release
percentages, size U aerosols, deposition velocities,
external and internal dose, fluorescent tracer behav-
ior, and atmospheric diffusion parameters were
determined. (Autb^) v
National Bureau of Standards, Washington, D. C
SCATTERING OF (COBALT-60 GAMMA RADIATION
IN AIR DUCTS, Okarles Eisenhauer. Oct 60, 25p.
9 refs. Technical iote 74.
Order from GTS %Q. 75 PB 161 575
M1.75
The exposure dose rates due to Cobalt -60 gamma
radiation scattered in small air ducts in concerte has
been measured for iduas with one and two right angle
bends. The inside ^rner of a right angle bend has
been found to be an! important source of scanered
radiation. Results are analyzed in terms of solid angle
relationships and attempts are made to extrapolate
experimental resulls to other duct configurations.
(Author)
Naval Radlologlcajl Defense Lab. , San Francisco,
Calif.
COMFUTATIWJ OP EARLY -TIME FISSION PRODUCT
DOSE -RATE SPECTRA AND GAMMA -RAY AIR
ATTENUATION, bj^ C. F. Ksanda and E. Laumets.
Rept. on Effects of Atomic Weapons. 14 Sep 59, 39p.
16 refs. Research |ind Development technical rept.
USNRDL-TR-361; AD- 232 225.
Order from LC miS3. 00, ph$6. 30 PB 152 644
This report released for sale to the public 7 Nov 60.
On the basis o^ recent measurement df photon spectra
for short-time irradiations of U^^. fission-product
dose- rate spectra are computed for times from 1.7 to
1550 sec after fiasicm. Air-anenuatlon curves that
would result from pblnt -isotropic sources having such
spectral dlstrlbutiots are then computed. The fact
that the attenuation curves are nearly straight lines
when plotted agalnsf distance from the source on a
semilogarithmic scale indicates that an effealve atten-
uation coefficient, H, can be used in computing the
gamma-ray air attenuation. The attenuation is given
by an expression of the form F ■ exp (-Ax), where the
value liis an effective attenuation coefficient, varying
with time after flssjon, that takes into account ab-
sorption and buildup of the ganmia rays over the
entire radiation spectrum. (Author)
Naval Radiological Defense Lab. , San Francisco,
CaUf. 1
IDENTIFICATION OP MICRON -SIZED, INSOLUBLE -
SOLIDS FALLOUT PARTICLES COLLECTED DUR-
ING OPERATION REDWING, by W. R. Schell. Rept.
on Effects of Atomic Weapons. 24 Sep 59, 20p. 5 refs.
Research and Development technical rept. USNRDL-
TR-364; AD- 229 280.
Order from LC mi$2.40, phJS.SO PB 152 646
This report released for sole to the public IC Nov 60.
Fallout from Redwing shots Flathead and Navajo, deto-
nated on barges anchored in shallow water, is de-
scribed. The Insoluble solids formed by the vaporlza'
tion and subs^uent condensation of the barge, coral
ballast, fission products, and evnironmental sea salts
were analyzed through electron diffraction, electron
'jBicroscofjy, emiaalon spectrograpby, phocomlcrogra-
-,^?^> '"'^ X-ray diffraction. These insoluble solids
were found to consist primarily of spherical particlea
less than 1 jxln diameter and to be composed to com-
pounds and elements consistent with the environmental
materials. (Author)
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Aerospace Medical [Dlv. ] Wrigtat Air Development
Div. . Wright -Patterson AFB, Ohio.
GUIDE TO AIRCREW PERSONAL AND AIRCRAFT
INSTALLED EQUIPMENT, by Paul F. Klehl. Sep 60,
156p. WADD Technical note 60-230, supersedes
WADC TN-58-259, Aug58.
Order from OTS $3. 00 PB 171 119
A catalog format has been used In thl« technical note
to describe and illustrate both personal equipment for
aircrews and the equi[»nent insulled in aircraft that is
of special interest to aircrews. The document includes
information on special high altitude and long range
flight clothing, personal and aircraft -installed oxygen
equipment, aurvival kits, life rafts and preservers,
parachutes, in-flight feeding systems, survival food
packets, and aircraft -insulled food service equipment.
Brief descriptions of 128 items are included along with
photographs illustrating the items. (Author)
California U. , Los Angeles.
PREDICTION OF THERMAL TOLERANCE WHEN
USING AN MA -2 VENTILATING GARMENT WITH A
MODIFIED MK-IV ANTI-EXPOSURE SUIT, by John W.
McCutchan and John D Isherwood. Rept. for June 58-
Mar 59 on Human Thermal Tolerance, Contraa
AF 33(616)5402. June 59, 32p. 11 refs. WADC Tech-
nical rept. 59-326; AD- 226 520.
Order from LC mi$3.00. ph$6. 30 PB 152 299
This report released for sale to the public 25 Oct 60.
The' physiological responses of human aubjects have
been investigated in the thermal envlrofunents ranging
from 120O to 240«'F while wearing the MA -2 ventilating
garment, and MK-IV exposure suit, and other garments
comprising 2.15 clo of thermal resistance. The venti-
lating garment was given air inputs ranging from 2 to
14 ft3 per minute in volume, and from 50° to 90OF in
temperature The thermal responses of the subjects
are shown graphically In terms of heat storage, heart
rates, sweat rates, aod composite Indices of these
variables. The results of these experiments have been
prepared In terms of an equation which is presented
graphically as a nomograph. This nomograph predicts
the cooling power of the MA -2 ventilating garment and
is to be used in conjunction with the tolerance chart
available in the HIAD. The tolerance data, which we-e
determined on steady exposures In a preheated cham-
ber, are used to predict human tolerance for conditions
where the air and wall temperatures are not constant.
(Author)
rolumbia U. School of Engineering, New York.
nRCBRING AND DISPOSAL OF INVENTORY WITH
pffO OR LIFO ISSUING AND KNOWN DEMAND, by
Arthur F. Veinott, Jr. Technical rept. no. 5 on Coo-
troa Nonr- 266(55). 5 Dec 59. 98p. 18 refa.
SS^froI^LC ml$5.40. ph$15.30 PB 152 124
gfBdent ordering and disposal policies ore studied
wben the utility at oiock depends upon its age at
iMuing and where an Issuing poUcy is specified. The
tosionptlon is made that the stock is issued on a lasc-
la-flrst-out (UFO) or a first-ln-first-out (FIFO)basis.
The problems considered are(l) find an optimal order -
iM policy when no dispooal is allowed and where the
issuing policy is given, and (2) find both an optimal
. ordering and an optimal disposal poUcy where the
Issuing policy'^s given. The demands are assumed to
be known with certainty la both problems. The prob-
lam <rf inventory control may also be viewed as a prob-
' km in quality control because the methods of ordering
and issuing affea the quality of product issued.
Engineering Dlv. , Air Materiel Command, Wri^t-
Patterson AFB, Ohio.'
THE BIOPHYSICAL RE(5UlREMEm"S FOR VENTI-
UTED CLOTHING, by E. S. Fletcher, Samuel I.
Rapapon, and John F. Hall. 5 May 48. 66p. 24 refs.
Rept. no. 5702; ATI -23 309.
Order from LCmi$3. 90, ph$10. 80 PB. 152 298
This report released Iot sale to the public 25 Oct 60.
The purposes of this report are to establish the prlncl-
pkes for engineering development of ventilated clothing
and define the ventilation requirements for a wide tem-
perature range; to record new observations upon tem-
perature regulation of the extremities and relate these
findings to ventilated and electrically heated clothing.
The following conclusions are reached: (1) Forced, in-
ternal ventilation of clothing offers a praaical and
economical means of thermal proteaion in hot enviroo-
inenta. In environnients which vary between hot and
cold, and In environmenta which require impermeable
(Personnel Supplies and Personal Equipment, 13 Jan 61)
outer clothing, provided that an air supply hose nwV be
attached to the Wearer. (2) Ventilated clothing permits
choice of protective and/or Insulative garmenta on the
baais of functional suitability alone, since no thermal
•tresa is Imposed on the wearer. (3) Orderly engl-
■serlng development is feasible on the basis of the
principles and requirements set forth herein. (4) The
handa and feet require no artificial heating or cooling
in the range between -30OF. and + lSOOP. , if prolonged
coouct with good conductors is avoided With venti-
lated clothing, it is better to err on the side of over-
beating, rather than of over -cooling the body to insure
protection of the extremities at very high or low tem-
peratures. (5) The power distribution of the present
Kondard elearically heated clothing requires re-
examination. (Author)
Naval Supply Research and Development Facility,
Bayonne, N. J.
LABORATORY EVALUATION OF IMPERMEABLE
PRCTECnVK CLCrmiNG. by Sidney A. Schwartz.
Nov 59, 28p. 11 refs. Clothing and Textile Division
rept. no. 45.
Or<»erfromLCml$2.70, ph$4.80 PB 150 778
Two series of tests were conduaed with Impermeable
protective clahing. The first was to determine the
ambient temperature at which the heat load began to
cause intolerable physiological stress. The second
evaluated garments designed to reduce or relieve this
stress. It was found, under test chamber conditions,
that temperatures below 80°F caused Uttle heat stress
under moderate activity for two hours. AnJjient tem-
peratures from 80° to 90°F caused varying degrees of
stress with the intolerable condition being reached at
90OF . Ambient humidity appeared to be erf minor im-
portance for those wearing impermeable garments. At
90PP temperature, filtered ventilation slits depending
upon body motion or "pumping" action ottered Uttle
relief. Forced air circulation through the use erf a
mechanical air circulator offered sufficient relief to
make work at 90°F practical. The relief from the
circulator was directly proportional to the volume of
air moved by the fan. (Author)
Psychometric Lab. ,,U. of North Carolina. Chapel Hill.
DEVELOPMEKT OF SUITABLE PSYCHOMETRIC
TECHNIQUES FOR VALID. RELIABLE AND EFFl-
QENT MEASUREMENT OF SUBJECTIVE REACTIONS
OF TROOPS USING QM ITEMS IN FIELD TEST CON-
rariONS. by L^e V. Jones and Thomas B. Jeffrey.
Rept. on Measurement of Relative Importance of Vari-
ous Clodilng Characteristics and Item Accepunce. Con-
tract DA 19-129-qm-1492. Sep 60. 96p. Technical rept.
R-7; FEA MRS 6002. .c^ono
Order from LC ml$5. 40, ph$15. 30 PB 150 892
Ratings of feature importance and feature aOetfiAcy as
separate and as Joint predictors of oser acceptance of
selected clothing items are examined by regression *
analysis. Item features are classified in terms of rela-
tive importance ana adequacy by scale value computed
by the means of ratlins assigned to the various features
' by 266 soldier subjects. (Author)
(^rtermaster Reseordi and Engineering Center,
Natlck, Matt. ^
A TECHNIQUE FOR MEASURING CLOTHING INSILA-
nON UNDER DYNAMIC CONDITIONS, by Alan H.
Woodcock and Ralph F. Goldman. July 60, 9p. 2 reft.
Technical rept. EP-137. .e«,^o
Order from LC ml$l. 80, ph$l. 80 PB 150 748
Tbe uie or a Beckmon & Whitley Heat- Flow Transducer
for measurli^ fluctuations in heat loss from die human
•kin through clothing to the environment has been ex-
amined using two different types of clothing. The
method has been found satisfactory as a technique for
obtaining local effects due to ventiUtion caused by body
movement. Of the two hot weather uniforms examined,
the experimenttl seemed to have little or no advanuge
with regard to coolness. ' (Author)
PHYSICS
AppUed Phyaica Lab. . |ohns Hopkins U. , Silver Spring.
Md.
TECHNICAL PAPERS FROM THE QUARTERLY RE-
VIEW OF BUMBLEBEE ACTIVmES JANUARY-
DECEMBER 1959. RepL on Contract NOrd 7386. [1960J
69p. 24 refs. Bumblebee rept. no. 291. ,,^ ^^
cSd*r from LC mi$3. 90, ph$10. 80 PB 150 872
102
103
Contents:
Radiation Patterns <if Microwave Stepped- Index Luneberg
Lenses. |
Measurement of Laininar Flame Speeds of Ethylene- Air
and Propane- Air Mixtures by the Double-Kernel Method.
Torsional Analysis bf Thin- Walled Shells with Closely
Spaced Spars. '
Honeycomb Sandwich Panels.
Combustion Instability: Acoustic Interaction with a Burn-
ing Propellant Sur<ace.
Stability Tests on a Bleed Simulator at Mach 2. 43.
Hydraulic (Olstllledl Water) Servo- Operated Hot Gas Con-
trol Valve. I
Insulation for Hypei^sonic Engines and Airframes.
Water Injection: A New Protective System for Missile
Magazines.
^ Analysis of Blstabld Control Systems.
Acquisition Search problem.
Nutation Damping o^ Satellites by the Drag of Internal
Fluid Motions.
(SeealaoPB 145 094).
ivfcn,
Yale U. , New Havfcn, Conn.
THE THICK- WALLED HOLIjOW SPHERE OF AN
ELASTIC- LOCKINa MATERIAL, by Aris Phillips and
Asim YAldiz. Tech^cal rept. no. 8 on Contraa Nonr-
609(12). Dec 59, a%j. 3 refa. AD- 232 402.
Order from LC mi$8.00, ph$6.30 FB 152 134
The purpose at this study is the exploration at the
rheological concept of the locking material which was
Introduced by Prager (Trans, of the Soc. d Rheolog>,
V. I (1957) p. 169-175). In anocher paper (Proc. DC
Intematlanal Congress at Applied Mechanics, ▼. 5
(1957) p. 206-211) n-ager Introduced the concept at the
elastic solid d limited compresslblUty. By a synthesis
d the two concepts, Phillips (Trans, of the Soc. of
Rbeology, v. ID) ingroduced the concept ot the ideal
locking material re]|resemed by means at two curves.
It Is seen that such # material may lock either by com-
pression or by shear. In this study the work at Prager
and Phillips is extended by introducing the elastic-
locking material as an extension at the Ideal locking
material.
Acoustics
Naval Research Lab , Washington, D. C
THE MUTUAL MEqHANICAL RADIATION RESIST-
ANCE FOR ALL VALUES OF ka OF AN UNBAF-
FLED QRCULAR RIGID nSTON WITH PRESSURE
RELEASED BACK, by S. Hanish. Interim rept.
22 Sep 60, 14p. 12 refs. NRLrept. 5513.
Order from LC ml$^. 40, ph$3. 30 PB 147 832
The theory -of the radiation at sound from one face at
an unljaffled rlgfld piston whose second face is pressure
released is reviewed in detail. Two such unbaffled
pistons located in a ^lane with their centers separated
by a distance d are clriven with identical amplMu^ps of
velocity Vq. Formulas are derived fca- the real acous-
tic power developed, the mechanical radiation ^elf
resistance and xhe mechanical radiation mutual realat-
ance at all values ctf frequency and piston radius, and
for all distances d. procedures and equations that
/
simplify numerical computauon are discussed and
amplified. Numerical calculations, however, are not
included, these being reserved for a companion report
(Author)
Speech Research Lab. , U. of Michigan, Ann Arbor.
LINGUISTIC CC»<SIDERATIC»4S IN THE STTUDY OF
SPEECH INTELUGIBIUTY (PART I); VOWEL, AM-
PLITUDE, AND PHONEMIC STRESS IN AMERICAN
ENGUSH (PART II); [and] THE IDENTIFICATION OF
FILTERED VOWELS (PART UI) by Use Lehiste and
Gordon E. Peterson. Rept. no. 3 on Studies of Syllable
Nuclei, Contract Nonr- 1224(22). Nov 59, 135p. 5 refsj
AD- 231 102.
Order from LC mi$6. 90, ph$21 .30 PB 150 494
Intelligibility Is defined as a property at spee^ com-
munication involving meaning. Since only meaningful
units have normal linguistic distrlinitional properties,
only meaningful units have the phonetic properties o^
actual speech. An analysis is presented of the Harvard
PB (phonetically balanced) lists, and a set of 10 lists of
50 monosyllables each is presented having an almost
exact first order phonemic balancing. There is as yet
no satisfactory method of calculating the loudness of the
various types of complex quasi -periodic sounds that
appear as time functions in speech, and it is suggested
that any such method would be Inadequate for deriving
physical correlates of accent or stress Judgments about
speech. Volume indicator and insuntaneous amplitude
observations are reported on sustained vowels produced
under various conditions of speech effort, and on vowels
produced in CNC syllables in a carrier phrase with
stress held constant. The untested theory is proposed
that the perception of Unguistic stress is based upon
judgments of the physiological effort involved in pro-
ducing vowels. A filtering technique was employed in
order to determine the relative influence of the various
formant frequencies upon vowel identification. When
the high-pass filter admitted only formants above the
third, vowel identification dropped below 5%. It was
feh that vowel substitutions are predictable under
certain conditions at filtering, and particular aspects
0* each vowel pattern are primary, or may be consid-
ered as essential information -bearing vowel
parameters.
Electricity and Magnetism
Army Signal Research and Development Lab. ,
Fon Monmouth, N. J.
A RADIOSONDE FOR MEASURING THE AIR- EARTH
CURRENT DENSITY, by Heinz Kasemlr. 15 June 60.
31p. 16 refs. USASROL Technical rept. 2125.
Order from LC ml^. 00, ph$6. 30 PB 152 190
An instrument is described which, in connection with an
ordinary meteorological radiosonde, measures the air-
earth current density as a function of altitude. The in-
strument is provided with three separate channela of
high input impedance which make it possible to measure
three atmospheric electric elements during the same
flight. A detailed analysis of the measuring technique
is given, and the results of 40 test flights are discussed
(Author).
SuSSaCE^^AVK W^ER A LOSSY CONDUCTOR, by
Bernard Friedman. Technical rept. no. 3 on Mathemat
teal Aspects of Electromagnetic Theory H, Contract
Sor- 222(60). Nov 59. I6p. 2 refs. AD-229 040.
SSr from LC ml$2. 40. ph$3. 30 PB 150 880
The electromagnetic field produced by a magnetic line
Murce on an Imperfectly conducting plane was the sub-
lect ot many papers (H. Bremmer, Encyclopedia of
PhyslcB. XVI). The question of whether this field con-
tttas surface waves or not renulns a matter of dlscua-
lioo. An effort is made In the present discusaloo to
tvold such essentially semantic notions as the existence
of a surface wave. Instead, the well- known (B. Friedman
and W. Elwyn Wllllama. Proc. Int. Elec. Eng, . P*" C.
kn 58) integral representation for the field produced
by the line source is studied, the Integrals Involved are
evaluated as carefully as possible, and, most intportant,
estimates of the error naade in evaluating tlw Integral
are obuined. (Author), l \
Carnegie Inst, of Tech., Pittsburgh, Pa. ,^^„,^^
BlS^TRIC FIELD DISTRIBUTIONS IN AN IONIZED
GAS. n. by Bernard Mozer (Doctoral thesis) and
Michel Baranger. Technical rept. no. 2 on Contraa
Nonr-760(15). [1959] 23p. 8 refs. AD- 227 317
Sder from LC ml$2.70, ph$4.80 PB 150 526
A method is used to calculate the probabiUty distrlbu-
tloB of the low-frequency component of the electric
field at a neittral point, the distribution of the low-
frequency component at an Ion. and that of the high-
frequency component at an electron. (Author) (See also
PB 144 897)
104
ttectro-Mechanics Co. . Austin, Tex.
VARIABLE MY -MAGNETOMETER. Interim engineering
rept. on Contract AF 19(604)1742. 9 Apr 57, 37p.'
AFCRC-TN-58-409; AD-152 552. „ ,^ or?
Order from LC ml$3. Oa ph$6. 30 PB 150 927
The Variable -Mu Magnetometer utilizes the principle
ttet a variation exists in the permeability of a magnetic
core when the core is subjected to a varying magnetic
field, such as the earth* field. The variation in perme-
aWlity of the core serves to change the inducunce of a
coil that is wound on it. The coil and core are used as a
variable inductance in an osclUatlng circuit causing the
dicult's frequency to follow changes in the permeability
of the core. A counter records the frequency of the
oscillator Consequently, the variation in a nnagnetlc
field may be indicated by the readings of the frequency
counter. A nuhiber of possible core materials were
tested for suitability and the Magnetic Ceramic, Cera-
mag 27. was found to be the most promising one. Core
shapes were tested and it was determined that the
double dumbbell shape produced the best results. The
sampling of the earth's magnetic field taken with die
variable -Mu Magnetometer (using various cores) are
ibown as graphs on 25 figures. (AuAor) (See also
PB 145 570)
Geophysical Uist. , U. of Alaska. College.
A STUDY OF THE MORPHOLOGY OF MAGNETIC
STORMS: GREAT MAGNETIC STORMS, by Masahisa
Suglura and Sydney Chapman. Final rept. on Contract
AF 19(604)2163. 31 Aug 58, 74p. 8 reCs. AFCRC TR-
Order from LC mi$4. 50,,ph$l2. 30 PB 150 932
Average characteristics are determined for 74 great
magnetic storms with sudden commencements that oc-
curred In 1902-1945. The storm field is resolved for dif-
ferent epochs of storm time into two parts: (i) Dst,
which is lndq)cndent of local time, that is, of longitude
i , relative to the sun, and (11) DS, which depends on A-
They are obtained, for each o< the three magnetic ele-
ments. decUnatlon. horizontal force, and vertical force.-
at eight geomapietlc Utitudes ranging from 80^ to 1^.
DS is harmonically analyzed; the first harmonic compo-
nent is shown to be the main component of DS. The
storm-time course at this component is compared with
thst of Dst; DS attains Its nriaximum earlier and decays
more rapidly. The results of the analysis of great
storms are compared with those for weak and moderate
storms that were reported previously. Some character-
istics of Dstrhsnge with intensity. Except in magnitude,
main characteristics o< DS are independent of intensity.
(Author).
Metals Research, Ltd. (Gt. Brit. )
RESEARCH ON IMPROVED MATERIALS FOR HYS-
TERESIS MOTORS. Final technical repc for 15 Mar-
14 June 60 on Contract DA 91-591-EUC-1157. Aug 60.
Sder fr^om*LC ml$3. OO, ph|6. 30 PB 150 644
An extensive Uterature search showed that the main re-
quirements of materials for the rotors of hysteresis
motors are (i) maximum Induction, (11) a coerclvity of
60-100 oersteds, (111) a very square B-H loop, and that
suitably sintered connpacts of equiatomic iron cobalt
alloy powders should have the desired properties. The
particle size of the powders must be such that each
particle contains only a few domains and the particles
should be aclcular; for optimum magnetic properties
diey should be aligned before compacting and finally an-
nealed In a magnetic field. Techniques have been devel-
oped for the production of compacts of fine Iron cobalt
alloy powders; in this preliminary work, however, the
powders were produced by decomposition of organic
metal salts and were larger and more spherical than
ideal and no attempt was made to align them before
conyacttng.
Electronics
Battelle Memorial Inst.. Columbus, Ohio.
INVESTIGATIONS OF RARE-EARTH OXIDE CATH-
ODES by J. B. Baker and G. B. Gaines. Scientific rept.
no. 3 'on Contraa AF 19(604)5691. 1 May 60. 9p.
ERD-TN-60-774. « .c/, ^o.
Order from ^mljl. 80, ph$1.80 PB 150 424
The thermionic emission from a mixture of 75 per cent
neodymlum oxide and 25 per cent gadolinium oxide is
being studied. The oxide mixture was applied to
105
rhenium and to unckiped tungsten electrophoretically.
Heating the oxides on undoped tungsten wires to tem-
peratures or about 1300°C (brightness) or above re-
sulted In permanent redualon at the emission capabili-
ties. On the other hand, heating the oxides on rhenium
wires to temperatures up to 1540°C temporarily Im-
proved the emission. Emission from both types (tf
cathodes was erratic, and true values for the emission
constants probably have not been obtained. In future
work, other oxides and base metals will be used.
(Author) (See also,FB 145 734)
Case Inst, at Tech. , Cleveland, Ohio.
HIGHER ORDER 8VALUAT10N OT THE WFFRAC-
TIC*! OF A PLANE WAVE BY A SMALL CIRCULAR
DISK, by Wllhelm H Eggimann. Sclenti^c rept.
no. 14 on Contract AF 19(604)3887. 7 July 60, 50p.
17 refs. ERD-TN-60-767.
Order from LC ml$3. », ph$7. 80 PB 152 077
The current dlstrlDution on a small circular disk due
to an incident plane wave has been obtained as a power
series in (ka). This representation lends Itself easily
to the calculation cf the scanered field In terms at
elemenury functiots. Expressions for higher order
mulilpole moments can be computed; for that purpoee
some elementary integrals are given In table III and
IV in the appendix. Recently Lure has cteained a
solution at this pro|>lem by reducing it to a pair at
Predholm Integral equations of the first kind. He ob-
tained an expression for the scattering cross- section
which agrees with the result in this paper. This Im-
plies therefore the correctness erf the coefficients for
the current distribMtion. (Author)
General Electric Co. . Schaiectady, N. Y.
INVESTIGATION OF VARIOUS ACTIVATOR -
REFRACTORY SUBSTRATE COMBINATIONS, by
J. H. Affleck. Scientific rept. no. 7 on Contract
AP 19(604)4093. 15 Mar 60, 13p. 3 refs. AFCRC-TN-
60-183; AD- 234 797.
Order from LC ml$2. 40, ph$3. 30 PB 148 254
A ninnber at dispenser cathodes have been prepared,
composed at a rtfractory matrix containing barium
slllcide. The tungsten carbide system has the lowest
work function erf tho«e examined. In addition to thermi-
onic data, tubes are being designed which will permit
the determination at the barium evaporation rate.
(Author) (See also PB 145 364)
Marine Physical Lab. , Scrlpps Institution al
Oceanography. San Diego, Calif.
THE HORIZONTAL ELECTRIC MPOLE IN A CON-
DUCTING HALF-SPACE, by Alfred Banoe, Jr. and
Jamea Paul Wesley. Rept. on Cootraa NObar -43356.
Sep 53, 238p. 49 ref». SIO Reference 53-33.
Order from LC mi$10. 20, ph$36. 30 re 152 676
This report releasee^ for aale to the public 16 Nov 60.
a ih
This report gives a iharou^ and complete account at
the mathematical problems involved in the determina-
tion of the electromagnetic field components generated
by a horizontal electric dipole embedded In a condua-
ing half- space whose plane boundary la also horizontal.
The problem ru formulated by introducing the Hertziaa
veaors or polarization potentials and employing the
technique at triple Fourier transforms in Cartesian
coordinatea. In configuration apace as well ss in
transform space. Suitable integral representations
are oticained for the conjpooenta o* the Hertzian vec-
tors. It Is shown that thia formulation Is fundamental
in the sense that it cootalns "per ae all other known
formulationa of the problem. By correctly apecifyliw
tbe original path at integration in Sommerfeld s fcr-
mulatibn at the problem and by carefully analyzing the
class at permissible deformations of the original path,
the whole moot question at poles aitd residues is
clarified In a straightforward manner. The repon
also presents the complete Independent solution of the
SUtic problem and It Is shown thst all solutions for
tbe alternating caae converge uniformly to the static
■dutions as the frequency Is made to vaniah.
National Bureau of Standards, Washington. Dl C.
SOVIET RESEARCH IN FIELD ELECTRON AND ION
EMtSSKSti. 1955-1959; AN ANNOTATED BIBLIOGRA-
PHY, by Tlbor W. Marton and Ralph Klein, Oct 60.
41p. 122 refs. Ttechntcal note. 75.
CVder from OTS |1. 25 PB 161 576
Soviet field emission research, as refleaed in the
technical literature from 1955 through 1959, is the sub-
ject matter of this annouted blbUbgraphy. Ibplcs In-
clude experimental and theoretical work on field elec-
trtjn emissioo from meuls and semiconductors, work
functions, phase transformations, adsorptic^, diffusion,
evaporation, surface ionization, and field Ion emission.
Over one hundred complete references to original pub-
lications in Russian and Ukrainian and to a few in
Mish. Hungarian, and Czech were selected after an
extensive search of tbe literature. Full references are
given to English translations of the entries whenever
available. A list of relevant scientific meetings, refer-
ences, and a brief subject index are appended to the
compilation. (Author)
Rome U. (Italy).
MODES IN RECTANGULAR GUIDES PARTIALLY
FILLED WITH TRANSVERSELY MAGNETIZED FER-
RITE. by Giorgio Barzilal aixl Giorgio Gerosa. Scien-
tific note MX 1 on Contract AF 61(052)101. 3 June 59.
19p. 4 refs. AFCRC- IN- 59-785.
Order from LC ml$2. 40. ph$3. 30 PB 150 413
A general model solution for a rectangular guide par-
tially fUled with a slab of ferrite transversely magne-
tized and situated against one side wall Is considered.
The relative characteristic equation, which has been
obtained In a previous work, Is numerically solved for
some typical cases and for modes of zero, first and
second order with respect to the dependence slong the
direction of the d, c. magnetic field. The results are
summarized In twentyone diagrams giving the propaga-
tion constant versus the ferrite slab thickness. From
the preceding analysis It can be concluded that: (a)prop
agatlng modes of any order may exist; (b) modes of
zero order may not be the lowest propagating modes In
the sense that higher order modes can propagate when
zero order modes are attenuated; (c) cases can exist
when all the unanenuated propagating modes travel in
the same aense. (Author)
106
Sunford Electronics Labs. . Stanford U. . Calif.
cBRIES SOLUTIONS FOR PERTURBATIONS ON
CROSSED- FIELD BEAMS, by B. A. Wlghtman and
n Chen. Rept. on Contract Nonr-225(24). 9 Nov 59,
So 5 refs. Technical rept. no. 207-2; AD-229 950.
oJder from LC ml$2. 70. pbH 80 PB 150 822
The differential equation of perturbations on the
grlllouln state of a rectilinear beam In crossed fields
is presented. The solutions of this differential equation
have limited value for cong)utational purposes. Series
developments are given of these soluticms, and the nu-
merical values of the coefficients are tabulated in a
torm adapted to high-speed digiul compuution. The
aame Infornvatlon Is given for a determinantal function
formed from these solutions and applicable to boundary -
value problems Involving such a beam. An example
problem Is solved uaing this determinantal function.
(Author).
aanford Electronics Labs. , Stanford U. , Calif.
TRAVELING- WAVE AMPLIFICATION OF WHISTLERS
byN. M. Brlce. Technical rept. no. 7 on Contract
AF 18(603)126. 16 Aug 60, 8p. 5 refs. AFOSR-TN-
60-931; AD-243 601.
Order from LC ml$l. 80. ph$l. 80 PB 150 820
Assuming that the traveling wave amplification mech-
anism is operative in the outer Ionosphere, It Is shown
diat amplification and absorption of audio frequency
waves depend on their rate cf change of frequency with
time. For a descending gliding tone, as In a whistler,
there Is inherent In Its propagation a bias In favor of
amplification of the wave. (Author)
Tung- Sol Electric. Inc. , Bloomfleld, N.J.
RESEARCH AND DEVELOPMENT IN UTILIZATION
OF SELF -SUSTAINED ELECTRON EMISSION IN-
VESTIGATION, by B. G. Firth, Warren C.Johnson,
and Donald W . Mayer. Quarterly repc. no. 1.1 Jan-
31 Mar 60. on Contract DA 36-039-8C- 85120. [1960]
SOp. 2 refs. AD- 237 920.
Older from LCmi$3. 30. ph$7. 80 PB 150 450
The characteristic physical . chemical . and electrical
properties of the N^lO cold cathode and lu preparation
ire reviewed . Development of 499 "AUoy" nickel
sleeve preparation (or such cathodes was very satis -
hctortly and finally completed. A method of stereo-
scopic photomlcrographic analysis of cathode coating
structures was dfrrelopei for use as a tool for correlat
li^ said structures with cathode preparation and sub-
sequent electrical test results . A careful study of
"pop-out" (sudden emission failure) shows this phe-
•omenon to be caused by reduction of coating surface
chaige due to rapid rise of MgO conductivity with rise
la temperature as a result of power dissipation In the
coating. Research established the fact that nMterials
other than MgO, such as AI2O3 and BeO, can be made
to give the same type of self- sustained electron
emission. (Author)
t
Molacolar Phy»ic« and Spectroscopy
Columbia U. . New York,
ANOMALOUS RELAXATION OF HYPERFINE COM-
PONENTS IN ELECTRON SPIN RESONANCE. U. by
Jan W. H. Schreurs and George K Fraenkel. Technical
note rept. no. 5 on Research In Electron Spin Reso-
nance. Contract AF 49(638)520. 1 Aug 60. 47p.28 ref»-
CU-5-60-AF-520-Chem. ; AFOSR-TN-60-863. ♦
Order from LC ini$3. 30, ph$7. 80 re 150 430
A detailed atudy haa been made erf the line width and
peak height of each of the five components iij^the elec-
tron spin resonance spectrun of the p-benzosemlqui-
none Ion as a function of microwave power at X-band
fr|squencles. Studies were also made of the spectrum
of the peroxylamine dl sulfonate ion as s function of
power. A 20 percent variation ih the line widths from
one hyperflne component to another was found in the
p-benzosemiquinone ion spectrum, and a 13 percent
varUtlon in the saturation parameters (T,). The aver-
age value for the line- width parameter at low power
for the p-benzosein^qulnone Ion was found to be
(l/T,) ■ 1. 11 x 10^ sec'^ and the reciprocal of the
average value erf the saturation oarameter was found
to be about (l/T^) - 0. 74 x 10^ sec'l. (See also
re 146 749),
Columbia U. , New York,
ELECTRON SPIN RESONANCE SPECTRUM OF THE
CYCLOOCTATETRAENYL RADICAL ANION, by
Thomas J. Katz and Herbert L. Strauss. Technical note
rept. no. 4 on Research In Electron Spin Resonance,
Contract AF 49(638)520. 1 Apr 60, 6p. 15 refa. CU-4-
60-AF-520-Chem; AFOSR-TN-60-589. AD- 242 503.
Order from LC nil$l. 80. ph$l. 80 TO 150 429
ColumbU U. . New York,
MOLECULAR ORBTTAL THEORY AND HYPERFINE
SPLITTING IN ELECTRON SPIN RESONANCE
SPECTRA OF SEMIQUINONES, by Gershon Vlncow
and George JC Fraenkel. Technical note rept. no. 6 on
Research In Electron ^In Resonance, Contract
AF 49(638)520. 15 Aug 60, 36p. 24 refs. CU-6-60-
AF-520-Chem. ; AFOSR-TN-60-920. AI>242 505.
Order from LC mi$3. 00. phJ6. 30 W 150 431
Molecular orbital calculations of the unpaired electron
density in a number of semiquinone ions have been
made as a function of a range of values of the Coulomb
integral, cq, for the oxygen atom and the resonance
integral. PcO- between the oxygen atom and the carbon
atom. The unpaired- electron densities, P^, were com-
pared with the experimental hyperfine splitting con-
stants sj arising from the proton bonded to carbon
atom 1 by the use of McConnell's relation ^^ - Q Pi,
Excellent agreement is obtained for the proper choice
of «o ■«' PCO.
107
Columbia U. . Hew York.
NOTE ON THE CALCULATION OF SATURATION
EFFECTS IN MAGNETIC RESONANCE, by
M. J. Stephen. Technical noce rept. na 7 on Research
in Electron ^in Resonance, Contract AF 49(638)520.
15 Aug 60. 19p. 6 refs. CU- 7-60- AF - 520- Chem. ;
AFOSR-TN-60-919. AE>-242 506.
Order from LC «nl$2. 40. ph$3. 30 PB 150 432
A simple method using diagrams Is described for cal-
culating saturation parameters in spin systems. Re-
sults are derive^ for tl»e multiresonance case. The
lattice is regard|ed as inducing transitions amongst
the various spin llevelg and the transition probabilities
are assumed knoWn. The method is particularly use-
ful in con^licated spin systems as are found in or-
ganic free radicals. For a free radical in solution
with one odd eledtron and N equivalent nuclei under
conditions where the intramolecular electron nuclear
dlpole-dlpole interaction and g factor anisotropy con-
tribute to the relaxation, the dependence of the satura-
tion parameters erf the electron resonance spectrum
on the nuclear qi^tum nmnber mj is given by an ex-
pression (rf the fdrm Amj* ^ Bmi -tC. Such behav-
ior has been founil experTmentally. (Author).
Reje
Electronics Research Lab. . U. at Califamla, ^
Berkeley.
ELECTRON SPIN RESONANCE IN NEUTRON-
IRRADIATED C^LCITE, by J. C. Kemp. Rept. on
Contract AF 49(688)102. 5 July 60, 6p. 5 refs. lER
series no. 60, is$ue no, 293; AFOSR TN-60-601;
AD- 242 247.
Order from LC n|l$l. 80, ph$l. 80 PB 150 374
Institute of MatHenrutlcal Sciences, New York U. .
N. Y.
BOUNDS ON SCATTERING PHASE SHIFTS: STATIC
CENTRAL POTENTIALS, by Leonard Rosenberg and
Larry ^nich. Ran. on Contracts AF 19(604)4555 and
DA 30-069- ORD- ass 1. June 60. 35p. 21 refs. Research
repc no. CX-49; AFCRC TN-60-464 [sic].
Order from LC m|i$3. 00. phS6. 30 PB 150 945
It has recently befn shown that rigorous upper bounds
on scattering lengths can be obtained by adding to the
Kohn variational ^ression certain integrals involving
approximate wave functions for each of the negative
energy states. Pen- potentials which vanish Identically
beyond a certain ploint, it is possible to extend the
method to poaitiva energy scattering; one obtains upper
bounds on (- k cot 7^)"\ where 7^ is the phase shift.
In addition to the negative energy states one must now
take into account a finite number of states with posi-
tive energies lying below the scattering energy. The
sutes In this associated energy eigenvalue problem
are defined by the imposition erf certain boundary con-
ditions on the wavt functions. A second approach. In-
volving an associated potential strength eigenvalue
problem, is also used. The second method includes
the first as a special case and, more significantly,
can be extended to scattering by compound systems.
If some states are not accounted for, a bound on cot 77
is not obuined; nefertheless It is still possible to ob-
tain a rigorous lovier bound on 77. Upper bounds on 77
may also be obtained, but In a way which is probably
not too useful for many body scattering problems.
(Author).
Kansas State U. , Manhattan.
THE SPECTRA OF NITROGEN OXIE«S, by
I. C. Hisatsune. Final rept. for 1 May 57-31 Aug 60
on Contracts AF 19(604)2255 and AF 19(604)6622
Aug 60. 23p. 52 refs. GRD-rTR]-60-2%.
Order from LC mi$2. 70, ph$4. 80 PB 150 09*
Infrared absorption bands of some oxides of nitrogen
in the one to thirty micron region and in the gas. liquid
and/ or solid phases have been investigated using a
medium resolution infrared spectrometer. Normal
coordinate analyse using the Urey- Bradley potential
field have also been carried out on several of these
nitrogen oxides. The results of these experimental
and theoretical work are briefly summarized in this
report. The following papers are included: Existence
of N2O4 isomers, by I C. Hisatsuneand J. P.DevIin.Pub.
in Jnl. of Chemical Physics 31:1130-1131. Oct 5S^ the
Raman spectrum and the structure of N20"» by
I. C. Hisatsune and J. P. Devlin pub. in ^pectrochim-
ica Acta 16:401-406, 16 Nov 59. Urey-flradley poten-^
tial constants in nitn^feen dioxide, nitrate ion and di-
nitrogen tetroxideyfcy I. C. Hisatsune, J. P. Devlin
and S. Califano. JlU). in Spectrochimica Acta 16 450-
458. 1960. (SeeyfelsoPB 143 667).
ki . -
Space Sciences Lab. , General Electric Co. ,
Philadelphia. Pa.
DE- IONIZATION CROSS SECTION FOR OXYGEN, by
R. G. Breene. jr. Rept. on Contract AF 04(647)269.
20 July 60, 24p. 10 refs. Technical Informatian Seriet
R60SD409.
Order from LCmi$2. 70, pta$4. 80 PB 150 949
Out atomic and free electron wave functions are
applied to the calculation at the de-ionization croes
■ection for OD. Our a- and d-wave numerical aolu-
tions to the free electron wave equation Is fitted to
Coulomb functions for normalization. This result is
used to determine the cross- section for the transitloos
s-wave to 2p orbital and d-wave to 2p orblul. We
carried out an approximate calculation for the tranal-
tion to the 3p orblul with the resulting indication that
the hydrogen result may reasonably be used. For the
contributions from transitions to 3d and higher orbiuls
the hydrogen cross- sections have been adopted. Our
final result Is 198 x 10" 21 cm. 2 leading to a rate cnn-
aum for radiative de-lonl2atlono# 218x10-1*. (Author)
Stanford U. . Calif.
PROTON RESONANCE SHIFTS IN PYRENE MONO-
NEGATIVE ION AT 4. 2**K. by M. E. Anderson,
P. J. Zandstra, and T. R. Tuttle, Jr. Rept. on Con-
tracts AF 49(638)482 and AF 18(603)131. [I960] 4p.
4 refs. AFOSR- TN-60-904: AD-242 738.
Order from LC ml$l. 80, ph$l. 80 PB 150 378
Optics
Centro di Studio per la Fialca delle Mlcroonde (Italy).
STEPPED CYLINDRICAL MIRRORS CORRECTED FOil
APERTURE AND FIELD ABERRATIONS, by Uura
Ronchl Abbozzo, Vera Ruaao and Gluliano Toraldi
I>1 Prancia. Technical note no. 1 on Contract
AF 61(052)234. Feb 60, 22p. 5 refa. AFCRC-TN- '
60-565.
Order from LC ini$2. 70. ph(4- 80 PB 150 415
108
IB tMa paper a stepped zone cylindrical mirror la de-
aoibed which satisfies the following requlrementa: (1)
It is free from spherical aberration for a point source
at infinity on the axis, (2) both off-axis spherical
tberraUon and ctaroa vanlah for fixed values at the field
,njte. /i , and of the aperture, -ff . The analyais has
been carried out, in the approximation of parageomet-
rlcal optica, by considering a dlffraaion grating of the
•encrallzed type, equivalent to the stepped zone mirror.
T^ee Interesting results are obtained: Independently of
the values of jTand ff, the equivalent diffraction grating
baa a quasi -parabolic cross -section; the off-axla
■iberical aberration turns out to be negligible over the
vbote aperture 0- ^, for field angles up to at least
Kr?; and the residual coma turns out to be well cor-
rected, too. (Author) ,
I I
Laboratory of Astrophysics and Physical Meteorology,
Johns Hopkins U. . Baltimore. Md.
SCATTERING BY IMPERFECT GRATINGS, by
II Bottcma. Final rept. on Contract AF 19(604)3491.
31 Dec 59, 31p. 6 refa. AFCRC- TR-60- 265.
OrJer from LC ml$3. 00. ph$6. 30 PB 150 628
The Irreducible erratic errors of groove spacing In a
diffraction grating, although relatively small in gratings
vtth a ipacug suitable for use in the visible sp>ectrum.
may be seriously large when gratings will be made with
smaller spacing, ruled for the vacuum ultraviolet or X-
ray spectrum. This report gives a thfeoretical analysis
of the effect of erratic groove spacings and observations
with experimental gratings with built-in erratic spacing
errors. Observations and theory are compared. A
similar investigation, on gratings with erratic errors
in groove depth, is also described. (Author)
Solid State Physics
Army Signal [Researclj^and Development Lab. ]
Fon Monnvxith, N. J.
SHORT CARRIER LIFETIMES AND THE PHOTO-
MAGNETOELECTRIC EFFECT, by Frank A. Brand.
15 Aug 57, 49p. 61 refs. Technical memo.no. M-1918;
AD-156 260.
Ordei from LC mi^. 30, ph$7. 80 PB 150 686
The PME effect, which Is based on the diffusion of op-
tically excited carriers in the presence of a trans-
verse magnetic field, was utilized to study carrier
lifetimes in germanium. The effect is analyzed assum
Ing electron- hole generation la confined to one surface
of an infinite slab, and expressions for the relative
conductance change, PME short circuit current, Dem-
ber voltage, and Dember field are develcjped on an
amblpolar basis. Equations for carrier lifetime vnder
dilck or thin sample conditions are derived Independ-
ant of light Intensity by considering the ration of re-
lative conductance change to short circuit PME cur-
rent Methods for measuring the relative conduCtaiice
change and PME response are presented in some de-
tail, and the experimental limits encountered for the
various measaremenis are indicated. Dau obtained on
20 germanium slabs are presented in tabular form
showing measured lifetime values ranging from 5 *•
KT* to 2 y W^ sec. Comparisons between long life-
tline specimens measured by the PME effect and other
more conventional technique* such as photoconductlve
decay or Morton- Haynea method are made showing
very good agreement In all cases. The effects of add-
ing recombination centers such as nickel or copper by
solid state diffusion show how carrier lifetime can be
effectively d^raded In germanium by orders of mag-
nitude. In addition, increasing the density of disloca-
tion centers by heat- quench cycling Is also observed
to reduce lifetime, though not as drastically as Is
possible by chemically adding recombination centera.
Bell Telephone Labs. , Inc. [New York].
FUNDAMENTAL STUDIES OF THE PROPERTIES OF
NATURAL AND SYNTHETIC QUARTZ CRYSTALS, by
J. C. King. Final rept. for 1 Feb 55-10 June 60 on Con-
trao DA 36-039-ac-64586. 10 June 60, 95p. 50 refa.
Rept. no. 27424-0; AD- 238 614.
Order from LC miJ5.40. ph»15.30 PB 150 680
Starting with the results of measurements of the steady-
state electrical conduaivlty in quartz from SOO^C down
to room temperature, a review is made of the resonator
behavior of synthetic quartz derived from various seed
plate orientations from -60° to 100°C. Without any
attempt at preserving the chronological order of the
work, the report proceeds with a description of defor-
mation and diffusion-type mechanical relaxation phe-
nomena found in quartz. These absorption proceaaea
are found to have direct Bearing on the behavior of
thickness shear resonators over the temperature range
-600 to 1(K)°C. Thus studies of methods by which the
amplitude of these relaxation absorptions can be altered
lead not only to further knowledge of the underlying
defect but also to techniques for improving the elastic
properties of synthetic quartz resonators. The acoustic
absorption commonly found near 20°K In 5-mc thick-
ness shear resonators is described and compared with
analytical treatments of dislocation relaxation in
crystals. (Author) (See also PB 149 724)
California U. . Los Angeles.
THE ATTENUATION OF SOUND IN ALUMINUM AND
SILVER AT LOW TEMPERATURES, by Edward Lax.
Technical rept. no. 17 on Contract [Nonr]-233(48).
Dec 59, 93p. 55 refa; AD-230 867.
Order from LC ml$5. 40. ph$15. 30 PB 152 144
The present study examined die attenuation of sound due
to the electron- lattice interaction in the normal conduct-
ing 8»te of ntietals. A comparison widi theory was
made by measuring both the ultrasonic attenuation and
the electrical conductivity of the same or similar sam-
ples over a wide temperature range. Except for copper,
which yielded curious results, only metals with com-
plicated electronic or crystalline structures were meas-
ured In the past. All prevloua meaaurements were
made above 9 mc by pulse techniques, usually in single
crystals to avoid grain boundary scattering. In the
experiments described here, Al and Ag, both face cen-
tered cubic metals with almost spherical Fermi sur-
faces, were studied. Aside frommeasurements in su-
perconducting Al. the effect was not previously exam-
ined in these single metals. The acoustic measure-
ments were made in high purity polycrystalllne speci-
mens at low frequencies by the reverberation decay
method. (Audior).
109
Cornell U. , Itha<^, N. Y.
INVESTIGATIONS ON THE DEPOSITION OF CAD-
MIUM (W MICA 3URFACES. by Gregory Soh-Yu Yeh.
Technical rept. no« 17 on Theoretical and Experimental
Investigations of tl^ Atomic Phenomena Occurring on
and Near the Surfates of Solids, Contract AP 18(600)674
15 June 60. 49p. li refs. AFOSR-TN -60-755.
Order from LC mi^3. 30, ph$7. 80 FB 152 036
I
The nucleation and{ growth of cadmium crystallites dur-
ing deposition front the vapor phase on mica has been
investigated using the electron microscope. In the
range of incident vtpor ^nslties studied, the mica must
be cooled to temperature^ below -700C before critical
nuclei will form, it temperatures above -120^ to
-130PC nucleation appears to be very rapid and subse-
quent deposition causes only growth ol the crystallites.
When the mica substrate is cooled below -136^ the
number of nuclei fcjrmed per unit area is proportional
to the time of deposition and the activation energy o( the
process is much la(wer (1, 400 cal/mol) than the process
occurring on the w^rm substrates (S, 900 cal/mol). By
direct observation iof these deposits with the electron
microscope, dau ub obtained on the number and rate ot
crystallite nucleatibn, as well as the size and rate of
growth of the crystals during deposition. (Author)
t
Diamond Ordnanc^ Fuze Labs. , Washington, D. C.
DETECTION OF l^GH- POWER MICROWAVES BY
FERRITES AND GARNETS, by D. Jaffe, J. C Cache-
ris, and N. Karayl^nis. 5 Oct 60, I5p. 4 refs.
TR-867. I
Order from LC miil.iO. pfa$3.30 PB 152 310
Measurements of tie low-frequency (detection) compo-
nent ol mz in ferrilfe and garnet as a function c^ micro-
wave power are priseoted. Most of the measurements
were made on rodsjof garnet having line widths on the
order d tens of oersteds. The detected output is
obtained by a coil df wire wrapped around the garnet
rod, critically loacled by a resistor. The efficiency,
defined as the ratioj ol the power In the resistor to the
microwave power, Is only on the order of 10"^ even
at high rf power levels. (Author)
niinois U. , Urbai^
COLOR CENTERS jlN KCl AND KBr, by John Cape and
Gilbert Jacobs. Technical rept. na 2 on Physics ot the
Solid State, Contract Nonr- 1834(19). Nov 59, 17p.
10 refs. I
Order from LC mil2. 40, ph$3. 30
FB 150 543
Potassium chloride land potassium bromide crystals
were exposed to X fays at lO^lC The optical absorp-
tion produced by thj^ irradiation and the changes in
optical absorption plroduced by subsequent annealing at
higher temperature^ were measured. The tempera-
cures at which changes in optical absorption occurred
were correlated wiqfi the temperatures at which free
electricaj charge appeared, and thermoluminescence
was observed. The absorption band at 345 mu, in KCl,
which has been namled the H band, was shown to pos-
sess a component caused ^y self- trapped holes. In
KCl, the self- trapped hole band bleaches thermally at
430K with a releasel of free electrical charge. H cen-
ters disappear at 56^ with a release of free charge.
The optical absorption band of the H center was shown
CO have its maximum at 335 m^ In KBr, the thermal
release of free charge at 30OK Is attributed to the dis-
appearance ot H centers. No charge burst was ob-
served in KBr which may be attributed to the destruc-
tion of self- trapped holes. (Author).
^ I . i . i . Y
Illinois U. , Urbana. • ' *'
TRANSPORT NUMBER IN SOLID CESIUM BROMIDE,
by Neal Laurance. Technical rept. no. 3 on Physics of
the Solid State, Contract Noor- 1834(19). Nov 59, 9p.
7 refs. AD- 229 494.
Order from LC mill. 80, ph$ 1.80 PB 150 544
The transport number of CsBr single crystals was
measured over the temperature range 350^ to iSCPC by
the method of Tubandt. No temperature dependence is
observed, and the average value of t^e cation cransport
nun\ber is . 49i. 06. A preferential growth phenomenon
is described, and Its possible interference with the
measurement is discussed. It is estimated that the true
cation transport number may be as low as 0. 3 because
of this phenomenon. (Author)
Institute of Tech. , U. of Minnesota. Minneapolis.
ON THE KINETICS AND MECHANISM OF PRECTPI-
TATION OF LITHIUM PROM GERMANIUM, by
J. R. Carter, Jr. and R. A. Swalin. Technical repc.
no. 1 on Contract Nonr-710(27). 25 Nov 59, 40p.
23 refs. AD-233 797.
Order from LC mi$3. 00, ph$6. 30 ^ PB 150 501
The investigation ot the precipitation of Li from Ge was
undertaken to determine (1) precipitation rates in crys-
tals supplied from various sources, (2) the effect of
thermal history prior to introduction of Li, and (3) the
influence of selective impurity additions (O and Cu) on
the kinetics of the precipitation of Li. The basic tech-
nique involved the saturation of a sample of Ge with Ll
at a high temperature and the subsequent quenching to a
lower temperature where precipitation ot the Li oc-
curred. The progress of precipiution was followed by
using electrical resistivity techniques. The precipita-
tion kinetic data followed Ham's theory qualitatively
(J. Phys. Chem. Solids 6:335, 1958) if the Ll were In-
troduced at a high temperature. The crystals which
were, obtained from different sources yielded drastically
differing values ol pie apparent nuclei number density.
A 2-hr 900^^ anneal of the Ge prior to saturation with Li
increased the number of nuclei for all samples. Doping
the Li with O and Cu tended to increase aitd decrease,
respectively, the nuclei number density.
ITT Labs., Nutley, N. J.
STUDY OF THE INFLUENCE OF ATMOSPHERE AND
ANNEAUNG ON CRYSTAL GROWTH PERFORMED
WITH ELECTRICALLY SUSTAINED HEAT SOURCE,
by A. J. Marino and W. L. Harries . Final engineering
rept. on Contract AF 19(604)2261 . July 60. 16^.
295 refs. AFCRC-TR-60-149.
Order from LC mi$7.80. ph$25.80 PB ISO 547
This study was undertaken to investigate the various
parameters of the flame fusion technique, the effects of
110
Unpufltlef , techniques for further treating the crystals
ifter growth, and to engineer and design a process
ftilch will produce more perfect crystals .
I^Oludcy Research Foundation, Lexington.
SO^E SEMICONDUCTING PROPERTIES OF BISMUTO
TMSULFIDE AND Bia^UTH TRIOXIDE. by
IX M. Mattcat. Technical note on Electrical. Optical
^ Thermal Properties ot the M JD N y*> Semlcon-
(juctors. Contract AF 49(638)90. 31 July 60, 47p.
VJrttt. AFOSR-TN-60-ia28.
Order from LC ml$3. 30, ph|7. 80 PB 150 784
Gootann: Ptrt I Sample Preparation; Bi2S3, tulk,
dandrltes, films, polycrysulllne; BI2O3 bulk, films;
psrt II Measurements; Thermal energy gaps, ^2^' '■
BI2O3, electrical resistivity, BI2S3. single cry stall,
pdycrystalline; BI2O3, films, thermal conductivity,
II2S3, single crystal; polycrysulllne; Seebeck coeffl-
:lent for BI2S3, optical transmission, BI2S3, BI2O3,
trfrared transmissloo, H»ll measurements.
Laboratory for Insulation Research, Mass. Inst, at
TWi. . Cambridge.
CRYSTAL PHYSICSl Annual summary rept. na 1,
lS>Be 58-15 Nov 59. on Contraa Nonr- 1841(50).
Nov 59, 38p. 18 refs. Technical rept. no. 144;
AD-229 196.
Order from LC ml$3. (X), ph$6. 30 PB 150 541
Contents:
Pnparatioo at solid striutlons of ammonium aluminum
chromium alum from (NH4) Cr(S04)2 •12H2O and
(NH.)A1(S0J, •I2H2O
hirtflcatlon orilkall Ralldes by zone-meltlng technique
(Irowth of cesium chloride crystals
hrfluencc of the growing direction on the tonic
condualvlty of KBr single crysuli
kxilc conductivity of TIQ, TlBr, and mixed crystal of
Tia/TlBr
brestigation of crystal defects by thermal etching
(}rysal growth by flame fusion
hvMtlgatlan of color centers in cesium hallde crystals
hfluaice of mono- and trlvalent impurities on color
centers In CaF2
Color centers In alkaline earth halides
liacoln Lab., Mass. Inst, of Tech. . Lexington.
THE CHEMICAL ANALYSIS OF MANGANESE-
MAGNESIUM FERRITE (MEMORY -CORE MATERIAL)
by D. G. Wlckham. Repi. on Contraa AF 19(122)458.
23 Aug 57. 6p. 1 ref. Technical rept. no. 164;
AD-150 870.
Order from LC mill. 80. pbll. 80 PB 150 673
Procedures are given for the determination of iron,
manganese and magnesium in nunganese-nMgneslum
ferrite. A procedure Is also described for the deter-
mination of the value Mil* ♦"♦■- Fe** present In the
solid ferrite. These four determinations make it poa-
itble to compute the ratio of divalent metal to trlvalent
■Bttl. M'*'"^"*"%M*-^.The complete chemical
•BtlyBls is applied to an examinatian ot memory cores
btfcre and after a retiring treatment carried out at
VXiOPC in an atmosphere of nitrogen. The ratio
M"*"7M* ■^♦M**"*wa8,found to remain unchanged and
equal to the theoretical value for a perfea 2-3 spinel
(M**Mi*'**04). (Author)
LlDColnLab. , Mass. Inat. of Tech. ; Lexington.
SOLID yrATE RESEARCH. (Quarter ty progreas rept. ,
Dlv. 8, on Contract AF 19(604)5200. 15 Apr 60. 99p.
74 refs. AFCRC-TN-60-1007: AD- 239 537.
Order from LC mi$5. 40, pl4l5. 30 FB 150 603
Contents:
Semiconductor device design
Chemistry
Materials research
Band structiore of groupa
Microwave and magnetic properties of solids
Magnetic materials ^
Magnetic films
Semiconducting con^poneKs
Display techniques
\
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
STRUCTURE AND MAGNETIC PROPERTIES O*' PER-
OVSKITES, by Aaron Wold. Rept. on Contract
AF 19(604)5200. 29 Aug 60. Up. 20 refs. 53 G-0040.
Order from LC mlR 40. ph». 30 FB 150 757
The principal effects responsible for the crystal 8tr)icc
ture of rare-esrth transition metal perovskites (ABO3),
ionic size and electronic ordering, are discussed. The
further relationship between these two effects and the
magnetic prtjperties of several perovaklte systems is
described. Extreme purity of the rare earth constituents
Is found to have in^x>rtant effects on the phenomenon of
^psraaltic ferromagnetlsm In perovskites, which Indi-
cates the desirability of re- examination of previous in-
vestigationa. (Authoi^.
Lockheed Aircraft Corp. , Sunnyvale, Calif.
ELECTRON SPIN RESONANCE IN SINGLE CRYS-
TALS OF SrTlOj. by W. 1. Dobrov. M. E. Browne,
and R. F. Vleth. Technical m«no. Sep 59. 49p.
16 refs . LMSD-49730; AD-226 691 .
Order from LCmi$3. 30. ph$7. 80 FB 150 666
The Intensities of paramagnetic resonance lines in
SrTi03 were correlated to the Fe coocentrationi . Evi-
dence for attributing the origin of the resonance in
ticanates to Pe3 + impurities rather than to the domain
structure was obuined. In SrTlOs resonance experi-
ments over the range 300OK to 1 .90K show a sltiw con-
tinuing increase of the tetragcmal component of the
cryswlline field down to the ferroelectric region. Ap-
plications of an electric field in this region revealed
little effect on crystalline splittings , thus showing that
the ferroelectric state of SrTlOa is not an Induced one.
[>lscrepancles between experimental results and con-
ventional Hamlltonlan were reinterpreted as originating
from residual stress in the crys»l. From Intensity
cunsideratioos the transitioas were identified by their
quantum numbers . (Author)
111
Materials Research Lab. , Watertown Arsenal, Mass.
CRYSTALLINE FIELD AND SPIN POLARIZATION
EFFECTS ON ELECTRON DENSITIES AND MAG-
NETIC FORM FACTORS, by A. J. Freeman and
R. E. War son (Mass. Inst, of Tech. )• June 60, I9p.
22 refs. MRLrept. bo. 79.
Order from LC tnl$2. 40. pii$3. 30 FB 148 918
The combined effects of spin (or exchange) polarization
and an external crystalline field on charge densities,
X-ray and magnetic form factors, and hyperflne param-
eters are Investigated following the analytic Hartree-
Fock self consistenc field approach. The crysuUlne
field was represented by a crude cubic field arising
from an oaahedral array o< point charges surrounding
the central ion - in this case Ni*2. The loo's spin den
sity leads to a Peru)! coacaa hyperflne term In bener
agreement with experiment than the value reported In
an earlier spin polafizcd calculation for the free Nl ^^
ion and a magnetic florm factor whose Fourier trans-
form resembles none at the individual 3d charge dis-
tributions. (Author!
Materials Research Lab. , Watertown Arsenal, Mass.
ON 'SCREENED IMPURITY POTENTIALS IN
METALS ", by Ralpti J. Harrison and Arthur Paskin.
July 60. 5p. 5 refs. MRL repc no. 81.
Order from LC mi$l. 80, ph$l. 80 PB 148 830
Mclrvine recently eitamined the spatial form at the
screened potential ot>tained from the work of Takimota
The present note points out some llmiutions In
Mclrvine's approactv In particular, the authors re-
en^asize the importance of the screening arising from
elect rona at the Fermi surface; This contributioo, neg-
lected by Mclrvine, was shown earlier by Langer and
Voflko to be dominant at large distances. (Author).
Materials Research Lab. , Watertown Arsenal, Mass.
ON THE CALCULATION OF THE CRYSTALLINE
FIELD STRENGTH, by A'. J. Freeman and R. E. Watson
(Mas*. Inac. alTeci^.). Jane 60, 18p. 44 refs. MRL
rept. no. 80.
Order from LC ml$j.40. pb$3.30 PB 148 919
A calculation ol the Crystalline field 8tr«ngth, Dq, la
reported for the cas# d chrome alum, using the same
model and crystal fltld potential employed by Kleiner
and recently determined Hartree-Fock wave functions
for the Cr"*'-' Ion. Particular emphasis is placed on a
consideratioa at reported point charge calculations and
Phillips' method at including the effects at orthogonall-
latlon at ligand to metal ion wave functions. Our results
Indicate that the point charge model estimates for Dq
gave good results mostly because they were baaed on
the use of improper 8d wave functions. Kleiner's re-
sult Is significantly improved - his wrong algn for Dq is
reversed and a small positive Dq is obtained - but In
such a way as to contradia Phillips conclualona.
(Author)
'Materials Research Lab. , Watertown Arsenal, Mass.
THE UNRESTRICTZD HARTREE-FOCK METHOD:
ELECTRON DENSITIES AND MAGNETIC FORM
FACTORS FOR SPIN POLARIZED Nl*t by A. J. Free-
man and R. E Watson (Mass. Inst, of Tech.). June 60,
23p. 46 refs. MRL rept no. 78.
Order from LC ml$2.70, ph$4.«0 PB 148 917
The effect (rf relaxing the restrictions sssoclated with
the Hartree-Pock method are discussed with particular
emphasis on that constraint which requires common
radial behavior for wave functions with all quantum
numbers except m^ (spin direction) in common. Result!
at such a "spin polarized" Hartree-Fock self consistem
field calculation are reported for the Nl'''^ ion and re-
lated to earlier calculatlona of Wood and Pran. and
Heine. Emphasis is placed on a consideration of the
effects on electron density and on X-ray and magnetic
form factors. The calculation suggests that one would
obtain a nwgnetlc form factqr,::Whlch is measurably ex-
panded (hence a contracted charge distribution) in com-
parison ¥fith that appropriate for any single 3d electron.
Also presented are results at calculations at several
hyperflne parameters. (Author)
Minnesota U. , Minneapolis.
STUDY OF TOE NATURAL AND INDUCED MAG-
NETIC SPECTRA OF SOME FERRITES, by
A. H. Mcrrlsh. Final rept. on Contract AF 18(603)113.
July 60, 53p. 9 refs. AFOSR-TR-60-90.
Order from LC mi$3. 60. ph|9. 30 PB 150 633
The first part at the report sumtnarizes the aims and
accomplishm^ts of the research' carried out over the
entire period at the contract. The last part of this re-
port outlines the research progress made since Tech-
nical Note TN 60-61. This latter material is covered
under the following four headings: (a) natural spectra
at ferrlte powders, (b) ferrlmagnetlc resonance In
magnetite spheres with either domain struaure or with
twinning, (c) induced spectra o< -Y-Fe203 powders and
(d) ferromagnetic resonance in thin permalloy films.
National Bureau of Standards, Washington. D. C.
ON THE NATURE OF THE CRYSTAL FIELD AP-
PROXIMATIOJ, by Henry Goldberg (Doaoral thesis,
U. at Maryland) and Charles Herzfeld. Oa 60, lOOp.
22 refs. Technical note 67.
Order from GTS $2. 25 PB 161 568
A new method Is developed for the treatment of
molecular interactions, and is applied to a system
consisting of a hydrogen atom in a 2p state and a hy-
drogen molecule in the ground state. The Interaction
of theae two species is calculated using ordinary
crystal field theory and also the new method. A com-
parison of the resuhs shows some of the shortcomings
of the conventional crystal field theory, and provides
correaions to it. The new method consists of (1) ex-
panding all electron terms of the total Hamlltonian for
the system which Involveslnteractlons between the
atom and the molecule, thus transforming the interac-
tion Hamlltonian into sums of products of one-electron
operators, and (2) of using properly antisymmetrized
wave functions made up of products of atom and
molecule elgenfunctions . The calculations show the
effect of the neglect of overlap and exchange in
ordinary crystal field theory. All calculations and
results are presented in full detail. Transformations
of three- center to two-center integrals are given
explicitly. (Author)
112
. ifl.
I II
New York Sute Coll. of Ceramics, Alfred U.
SEMICONDUCTING MATERIALS, byT. J. Gray.
Annual rept. Dec S8-Nov 59, on Contraa Nonr-I503(01)
[I960)70p. 60 refs. AD- 229 943.
Order from LC mi)3. 90. pb$10. 80 PB 150 537
A number of single crystal and polycrystalllne samples
refused to respond in the test unit during photocon-
ductivity. When the minority carrier concentration in
an extrinsic material is increased temporarily above its
equilibrium value, Ita return will be by first order
Unetlc decay. The recombination rate in an illuminated
tample Increases above the norm as the hole and elec-
tron concentrations increase. Recombinations usually
occur at centers deep in the forbidden band. The decay
and the presence of centers can be studied by thermal
glo-curves and by pulse Illumination. Lifetimes are
particularly sensitive to number of surface states, the
•urface treatment, and sample history. The nwjor dif-
ficulty encountered in making d. c. Hall measurements
on hot -pressed specimens seem to be a lack of uni-
formity in the specimens. Preliminary magnetoreslst-
ance values indicate a very small contribution from a
bot-pressed sample. The addition of both d. c. and a. c.
amplifiers should help to solve the sensitivity problem.
The activation energy of a single crysul measured in a
thermoelectric rig was normal, but the hot- pressed
-flllK was distinctly low. The sU^t deviation from
Unearlty of this plot is possibly connected with the
channeling problem, as this is a duplicate sample to
tbfi one used for HAIl nteaaurements.
New York U.. N. Y.
PARAMAGNETIC RESONANCE IN THE SOUD STATE,
by Hartmut Kallmann. Quarterly rept. no. 7. Jan-
Mar 60, on Contraa DA 36-039-8C-78056. May 60, 8p.
I ref. AD- 238 346.
Order from LCmi$l. 80, ph(l. 80 PB 150 443
Measurements of the number of free radicals produced
by X-ray irradiation a( solutions containing various
percentages of benzene and carbontetrachloride are
described. The solutions contain 10*^ mole dlphenyl-
plcrylbydrazyl (DPPH) as scavenger. The disappearance
of the DPPH is measured in an EPR spectrometer. The
imount of DPI^ consumed is a measure of free radicals
produced. Measurements with varloua X-ray (iiobes
riiow that the DPPH consumed and thus the free radicals
formed are prpportlcxial to the doee. Measurements of
Q sod monitoring the power input to the sample cavity
ars planned to improve methods of comparing spin con-
oaatrations in different samples. (Author) (See also
PB 147 931)
Ohio State U. Research Foundation. Columbua.
PHOSPHORUS DIFFUSION INTO SIUC(»4 THROUGH
AN OXIDE LAYER, by Dawoo Kahng and M. O. Thurs-
ton. (Quarterly technical rept. no. 1, 1 Jan- 31 Mar 59,
on Research on Dlffuaion of Impurities into Siliooo
Through an Oxide Layer, Contraa DA 36-039- •c-83874.
May 59, 66p. 21 refi. Rept. 896-1; AO-218 842.
Order from LC mi$3.90. pfa$10.80 FB 152 185
Thla report released for sale to the public 10 No¥ 60.
The oaddatlon of sIIIcod and the solid-state diffusion at
phosphorus into silicon under oxidizing conditions have
been studied theoretlcaljy and experimentally. It is
shown that the mechanism of oxide growth on aillcao
depends upon the type of oxidizing atmosphere. In sir
the oxide grows at Its outer surface, while in steam
the growth occurs at the oxide -silicon interface. Solu-
tiona of the diffusion equation for various oxide- silicon
systems of Interest are presented, h is shown that for
a diffusion begun with an oxide-free sample, the sur-
face concentration of phosphorus on the silicon is in-
dependent of diffusion time. A simple formula is given
for predicting how long a preoxldized sample of p-type
sllloon may be diffused st a given temperature before
the surface will be converted. The experimental value
of the diffualvlty of phospborua in SIO2 is 10-^^ cm^
sec'^ at 1250°C; measured values at other tempera-
tures are also given. (Author)
Pictfic Semlconduaors, Inc. , Culver City. Calif.
STUDY OF SURFACES IN SHkllCOTOUCTOR DE-
VICES, by T. C Hall. Quarterly technical rept. no. 2,
15 Sep- 15 Dec 48, on Ccmtract DA 36-039- sc- 78049.
[1958] 23p. 1 ref. PSI rept. no. 3000:21 -2^Q.
Order from LC mi$2. 70. phK 80 PB 150 811
The results of a 1000 hour continuing reliability study
consisting of room temperature power aging on a group
of eight silicon diffused, J unction diode structures pro-
tected by a thick chemically bonded polysUoxane layer
are presented. Relative constancy of reverse break-
down and saturation current after initial stabilization
is reported. Varying degrees of passivation of silicon
diode crystal surfaces is produced by esterlflcation of
the surface oxide layer by exposure of the surface to
alcohol and moist triethoxysllane vapor in separate
experiments carried out In autoclave at elevated pres-
sures and temperatures. Sensitivity of electrical char-
acteristics on exposure to 0-100% relative humidity
varied with aucoclavlng cooditioas. (Author)
I^ciflc Semiconductors, be., Culver City, Caltf.
STUDY OF SURFACES IN SEMICaODUCTOR DE-
VICES, by T. C Hall. Quarterly tedinical rept. no. 3,
15 Dec 58-15 Mar 59, on Contract DA 36-039-8C-
78049. [1959] 20p. 1 ref. PSI rept. no. 3000:21-3-Q.
Order from LC mi$2. 40, ph$3. 30 PB ISO 812
Thickened oxide films generated by either chemical or
thermal methods on silicon p-n bar diodes have vari-
ous effeas on dibde electrical characteristics under
dry amblents. These effeas are dependent upon the
specific technique employed in the film formation.
Such films provide limited protection against high
humidity amblents over extended periods of time. Al-
cohol esterlflcation of such oxide films on diodes under
study causes no deterioration of electrical character-
istics beyond that which may have been produced by
the prior oxidation process itself. The ratenclon of
the initial Junction electrical clutracterl sties In ambient
humidity Is observed on esterihed-OKide-proteaed
Junction;. Application of this ioformation to the solu-
tion of problems of device reliability appears promis-
in«. (Author) (See also PB isa 8U)
113
ii
Pennsylvania dJ. School of Metallurgical Engineering,
Philadelphia.
THE FRICTION AL STRESS ACnNG ON A MOVING
DISLOCATION IN AN OTHERWISE PERFECT CRYS-
TAL, by Doris Kuhlmann-Wilsdorf. Kept, on Contract
AF 49(638H35. July 60. 33p. 16 refa. [AFOSR] TN-
60-978.
Order from LC mi$3. Oa ph^. 30 PB ISO 651
The problem of 'the frictional stress suffered by moving
dislocations in ^herwlse perfect crysuls Is Investi-
gated. This is 4one without calculating the core ener-
gies of dislocations, but by considering stresses and
strains on the slip plane. The level of frictional stresses
obtained is much higher than reported previously. Since
common glide dislocations in metals with close packed
structures apparently do not suffer significant frictional
stresses, mechanisms are discussed which tend to re-
duce their effect A new such mechanism is discovered.
It is based on the Idea that the positions of dislocation
axes are not defilned with precision, but only within one
to a few times the average displacement of the oscillat-
ing atoms. The expected results of this, is a depres-
sion of the frictional stress for close packed metals
even at very low temperatures, almost no effect on dis-
locations In cry»uls with diamond ftnictures, and a
temperature dependence proportional to e'Conat T/Tm
for hJaCl type salts and, probably, for b.c. c. metals.
(Author)
Rice U. , Houafeon, Tex.
STACKING FAULTS IN PLATINUM, by J. Taranto and
Franz R. Brocz«n. Technical repc na 3 on Contract
AF 49(638)78. JMy 60, 20p. 17 refa. AFOSR TN-60-88:
Order from LC ml|2. 40, ph$3. 30 PB ISO 749
The shift of X-r»y diffraction lines was observed at var
ious stages of recovery In filed powder specimens at
platinum. As the line shift is a criterion of the change
in stacking- fault probability, the disappearance of stack
faults during annealing could be followed In an approxi-
mate manner. The activation energy at the annlhll^Uon
process was estimated to be 28. 8 ± 5 kcal/mtrfT^^
(Author).
Stanford Blectfonics Labs. , Sunford U. , Calif.
STUDY OF SEM1C0N6uCT0R DEVICES BY ANA-
LOGUE TECHNICJUES, by R Bharat. Rept. on Con-
traa Nonr-225(a4). 16 Nov 59, 91p. 16 refa. Technical
rept. no. 1502-1|; AD- 229 532.
Order from LC $ii$5. 4a ph$15. 30 PB ISO 52S
Analogue techniques are applied to the study at seml-
conduaor devicas m pulse circuits, enabling one to
make a transient analysis of models which describe both
the internal and the terminal behavior al the devices.
Physical phenomena in semiconductor devices are de-
scribed in terms of lumped models and an analogue
computer is set up to simulate the equation* derived
from these modeis. Equations relating the variables in
the model of the device to the variables describing the
circuit In which the device Is. operating are alao simu-
lated on the computer, and transient solutions are ob-
tained for all the variables Computer and electric-
circuit analogues al several physical phenomena fre-
quently encountered in semiconductor devices anre
developed. Both linear and nonlinear phenomena are
considered and vtrlous nnethods at simulating them are
described. Analogue computer solutions are obulacd
for transistor pulse circuits in which interacting non-
linear phenomena influence the operation of the circv^
Solutions for a drift -transistor switching circuit aid
for an avalanche-transistor relaxation -oscillator cir*
cult are presented. (Author)
Uppsala U. (Sweden).
BORIDES AND SILICTDES OP THE TRANSITION
METALS, by Bertll Aronsson. Technical note no. 13
on Contract AF 61(062>4(X 1 July 60, 114p. 197 reft.
AFOSR -TN -60-683.
Order from OTS $2. 50 PB 171 12l
Contents:
A survey of interntediate phases In Me-B, Me -Si, airi
Me-Sl-B systems and their crystallographic cooscua
Borides
Silicldes
Silico-borides
Physical and chemical properties of borides and sill-
cides. Some general features of Mei -M2-X, Me-
B-X and Me-Sl-X ternary systems (X-B, Si, C, N)
Some features of the crystal chemistry of borides aad
silicldes
The solid solubility of boron and silicon in metals
Structures of phases comaining less than 33 atom
per cent non-metal
Structures of phases containing 33-40 atom per cea'
non-metal
Structures of phases containing 40-50 atom par cast
non-metal
Structures of phases containing 50-75 atom per cm
non-metal
Structures of phases oonrainlng more than 75 atom
per cent non-metal
Concluding remarks
A brief comment on the similarities between the prop-
erties of silicldes, borides, carbides and nitridies
and on the 'bonding' in theae phases
(See also PB 142 971)
T
Theoretical Physics
Avco-Everen Research Lab. , Mass.
AN ARC TUNNEL FOR MAGNETOHYDRODYNAMK
STUDIES, by Richard Rosa. Rept. on Contraa
AF 04(647)278. June 59, 13p. 12 refa. Research
note 132; AFBMD-TN-59-6; AD- 227 863.
Order from LCml$2. 40, pfa$3. 30 PB 152 671
This repotrt released for sale to the public 16 Nor 60.
An arc wind tunnel or plasma Jet can be used to pro-
duce s steady gas flow over a considerable range at
temperature, pressure, and gaa composition. In
particular. It can produce gas temperatures suffidetf
for appreciable thermal Ionization to occur, especlal]|f
if the gaa is seeded with a small amount (1^ or less)
or slkali metsl vapor. For this reason It should be •
useful tool for magnetohydrodynamic (MHD) studies.
A discussion Is presented of s t\innel developed fortiiU
purpose, specifically for studies related to MHD ac-
celeration of and power generation from a conductlnf
gas stream. The dealgn criteria for such a facility
114
are discussed. A magnet for use with this tunnel was
also built and some first results of efforts to generate
electric power from the interaaion of the hot gas
stream and the magnetic field are described. (Author)
Elearon Tube and Microwave Lab. , Calif. Inst, of
Tech. . Pasadena.
PUSMA INTERACTION RESEARCH PROJECT, by
R. W. Gould and D. G. Dow. Quarterly progress rept.
DO. 4 (Final) I Dec 58-30 Nov 59, on Contract DA 36-
039-SC-78230. [1959] 28p. 12 refs. AD- 239 994.
Order from LC mi$2. 70, ph$4. 80 PB 150 447
Detailed studies are under way concerning the feasi-
bility of the cyclotron orbit oscillator described in
previous reports. The effect of a non-uniform plasma,
and the degree of non- uniformity to be expected are
considered theoretically. A modification of the Phillips
Ion Gauge (PIG) discharge is being investigated for
possible generation of millimeter wavelength plasmas.
A partial explanation for the multiple scattering peaks
aeen in the reflection of an electromagnetic wave from
• plasma column was worked out, and the discrepan-
cies between the experiment snd theory may be ex-
plainable on the basis of density variations in the
plasma.
Maryland U. , College Park.
DEMONSTRATION OF QUANTUM MECHANICS IN
THE LARGE, by T. B. Day. Sep 60, 12p. 7 refs.
Dcpi. of Physics Technical rept. no. 195.
Order from LC mi$2.40, ph$3.30 PB 150 891
Maryland U. , College Park.
LIE EQUATIONS FOR A LEE MODEL, by E. R.
Calaniello and S. Okubo (U. of Naples). Rept. on Con-
tract AP 49(638)24 and Technical rept. no. 12 on Con-
traa DA 91-591 -EUC- 1096. July 60, 21p. 2 refs.
Physics Dept. Technical rept. no. 185a; [AFOSR] TN-
«>-898; AD- 242 656.
Order from LC mi$2. 70, ph$4- 80 PB 150 557
Ite renormalization in configuration space of a slight
fneralization of the Lee model is discussed, as an
nample of general procedures which seem to be appli-
cable also to more general cases than the present one.
The replacement of ordinary with finite -part Integrals
removes consistently all ultraviolet infinities and per-
mits to write the Lie equations of the renormalization
group, the solution of which yields the familiar rela-
dOM between unrenormalized and renormalized param-
flters. (Author)
1 II
Maryland U. , College Part.
A NEW REDUCTION TECHNIQUE IN QUANTUM
FIELD THEORY, by John S Toll. Rept. on Contract
AP 49(638)24. Aug 60, 24p. 12 refs. Riysics Dept.
"rtchnical rept. no. 194; [AFOSR] TN-60-1089;
AD- 243 376.
Order from LC mi$2. 70, ph$4. 80 PB 150 969
A new technique Is presented for reduction of the scat-
tering matrix or other physical quantities in quantum
field theory. These quantities are expressed as Inte-
frali involving vacuum expectation values of products
of field variables. The procedure is similar to that of
Lehmann, Symanzik and Zlmmermann but differs from
LSZ by the explicit Introduction of funaloos which
vanish outside the future li^t cone. The new techniques
is more cumbersome than the LSZ method and inferior
to It for many applications but has the advantage of
yielding a larger primitive domain of analyticity and of
not requiring local commutatlvity nor any other form
of causality assumption beyond those requirements diat
are implicit in the modified asymptotic condition. The
method Is illustrated for the case of two particle scat-
tering and for the vertex function. It has been checked
in simple cases of examples In perturbation theory in
lowest order. It is shown that, without additional
assumptions, the Reduction technique has only trivial
consequences, for it Is proved that any matrix element
can be chosen as an arbitrary invariant function of the
energies and momentum transfers involved and that it
can still be extended off the mass shell to satisfy the
analyticity and mass spectrum conditions. Thus, use-
ful restrictions Involving only quantities at points of
direct physical meaning have not yet been obtained; to
gain such restrictions, the unitarity condition or some
explicit form of causality assumption would be re-
quired. (Author)
Maryland U. , College Park. *
REGULARIZATION AND RENORMAHZATION
THROUGH FINITE -PART INTEGRALS, by E. R.
Calaniello and A. Campolattaro and B. Preziosl (U. of
Naples). Rept. on Contract AF 49(638)24 and Technical
rept. no. 11 on Contract DA 91 -591 -EUC- 1096. June 60,
33p. 11 refs. Physics Dept. Technical rept. no. 182.
[AFOSR] TN-60-762; AD- 242 655.
Order from LC mi$3. 00, ph$6. 30 PB 150 556
The replacement of ordinary with finite -part integrals,
which generalize the definition originally given by
J. Hadamard, was shown previously to yield ipso facto
correctly renormalized field equations independently of
perturbative techniques, provided due care is taken of
the symmetry properties of the theory and some quanti-
tative conditions (closely related to Epson's heuristic
conditions for retKirmalizabllity) are satisfied by the
theory itself. In this work we extend the class of finite-
part integrals considered before to cover all instances
which nvay practically occur and discuss several possi-
ble prescriptions in configuration space which exhibit
the wanted properties. It appears that sane prescrip-
tions are better suited to the study of general questions,
such as renormalizability of a theory and deduction of
the Lie equaticHis of its retiormalization group, while
others are more convenient for actual compuution, once
renormalizability is proved. This work will be followed
shortly by another in which this method will be shown
to yield the expected results in the case of the Lee
model. (Author)
Naval Supersonic Lab., Mass. Inst, of Tech..
Cambridge.
RESEARCH IN A CC^dPREHENSIVB THEORY OP
PLASMA STATES AND PHENOMENA. Final rept.
(Part 4) on Contract AF 33(616)5693. Mar 60. 80p.
6 refs. Technical rept. no. 441; WADD Technical
rept. 59-486; pt. 4; AD- 239 876.
Or^ from LC mlM-SO, pb$12.30 PB IA7 780-4
A
The analysis indicated that a plasma, except at very
high pressures, can be conaidered as a nearly perfect
115
^
gas. The depamirf may lead to a coiTecxloa which la
usually 10% or lea a. Further, the correction term
can be approximated to a good accuracy by meana d
the Debye-Huckel theory. The effects al magnetizing
the plasma are shcwwj to influence the transport prop-
erties by altering the effective collision frequency.
Finally, it is showa that the coupling between a moving
fluid and a magnetic field is reduced by the changes in
transport properties produced by the magnetic field.
The recommendation was made that one of the primary
research efforts in plasma physics be' that d meas-
uring the transport properties under a variety of
circumstances. (AiAbor) (See also PB 147 780-3)
(Aiitt
Office of Technlcil Services, [>ept. d Commerce,
Washington, D. d.
MAGNETOHYDRODVNAMICS. Aug 60, 8p. 122 refa.
OTS Selective BibUography SB-426.
Order from OTS $4 10 OTS SB-426
I
A bibliography of reports listed in the two OTS monthly
absrraa journals: \i. S. Government Research Reports
and Technical Tranplatioos. This bibliography includes
reports added to tht tTTS collection during the period
1950 to September I960
r
Physical Researcli Lab. , Space Tech. Labs. , Inc. ,
Los Angeles, Calif.
DYNAMIC STABILiZATKW OF A PLASMA COLUMN,
by Erich S. Welbel, 15 Aug 60. 63p. 21 refs. STL/TR-
60-0000- GR269.
Order from LC ml$3. 90. phJlO. 80 PB 152 113
A cylindrical plasnta columir is confined by a magnetic
field whose z- component is constant while the }f-
component oscillates sinusoidally. The skin depth is as
■umed to be negligible so that the boundary can be con-
sidered aa sharp and the Interior of the plaama aa field
free. The plasma itself is treated aa an assembly of
non-colliding (Mrtioles which are specularly reflected at
the plasma surface. The oscillating pressure of the
applied field causes the plasma surface to execute a
small periodic motion independent of Y "^ ^ ^^
other components df the displacement decay In time.
Thus, the plasma it positively stable against all defor-
matlona. For magnetostatic confinement this treatment
yields the usual instabilities, but in contrast to earlier
work, the growth r(tes are bounded as the deformation
wave length approathes zero. This appears to be In
better agreement wjth experiment. (Author).
Plasma Propulsion Lab. , Republic ATiation Corp. ,
Farmmgdale, N. Y.
PINCH DYNAMICS WITH NONUNIFORM INITIAL COH-
DITIONS, by Willian) J. Guman and Irving Qranet. Rept.
on Contraa Nonr- 2851(00). Jan 60, 24p. PPL-TR-60-6;
AD- 237 560.
Order from LC init2. 70. ph$4. 80 FB 147 838
The basic eqoBtloni of the ''snow plow" pinch analyils
are formulated in a constant area electrode geometry
for the case of a pinch occurrlog In a fluid having initial
velocity and density distributions. The geometry se-
lected readily converts radial pinch mocioo to an axial
motion. This new lormulatlon can be applied to the
case of uniform initial conditions and also to a different
approach to the slug model which accounts for the In-
ernal energy in thf fluid. (Author)
Sperry Gyroacope Co. , Great Neck, N. Y.
A BEAM- GENERATED BEAM- PLASMA SYSTEM, by
C. C Wang. J. E. Hopson and L. P. Lcvine. Final rept
for 1 Apt 59-31 Mar 60 on Contract AF 19(604)5555.
May 60, 40p. 2 refa. Sperry rept. no. NA-8210-8199:
AFCRC-TR-60-163.
Order from LC ml$3. 00, ph|6. 30 , PB 150 991
The minimum preaaure condition for plasma generatloa,
the result of directing an electron beam through a re-
sidual gas (hydrogen in this study) along magnetic field
linea, has been theoretically predicted and experimen-
tally verified. For pressures greater than the niinlmuin
preaaure, the equilibrium plaanui de nalty haa been ana-
lyzed. Plasma growth greater than that expected from
collisions of primary electrons with residual gas atoms
was found; diffusion-controlled breakdown cauaed by a
microwave generation process of the system explains
thla growth. Microwave Interaction of the beam- gener-
ated plaama circuit with the primary beam la exhibited
as a velocity modulation of the beanL Experlmenta
ahow a discrete bandwidth noise spectrum; theoretically,
discrete frequency oscillations over a prescribed band-
width abould be produced. Plaama circuit character-
istics are not independent of microwave power level aa
aasuroed in the theory; the microwave power generated
is apparently absorbed by the pl^ma. The plaama.
then, is unstable. Objectives have been attained In the
e]q>erimental and theoretical atttdiea of the generation
of a plaama by an electron beam, and the beam gener-
ated plaama aa an electromagnetic circuit for interac-
tion with the aame electron beam. (Author). (See also
FB 148 316).
Sperry Gyroscope Co. , Great Neck* N. Y.
ELECTROMAGNETIC WAVE PROPAGATION IN GYRO-
ELECTRIC PLASMAS, by C. C. Wang and J. E. Hopsoa.
Scientific rept. no. 2 on Contract AF 19(604)5555.
May 60. 79p. 10 refs. Sperry rept. no. NA-8210-
8191-2; AFCRC-TN -60-596.
Order from LC mi$4. 50, ph$l2. 30 PB 150 629
A detailed theoretical analjrsia at electromagnetic wave
propagation in a uniform plaama Immersed in a unlfonn.
externally-superimposed nugnetlc field is presented.
The assumed plasma model is a uniform distribution of
free, noocollidlng charged particles of zero temperature
and with an average net charge of zero. The poaatbillty
at interaction between electromagnetic waves in plasma
circuits and directed electron beams is of particular
intereat. The Maxwell equations and boundary condi-
tiona for the assumed plaama model are developed, and
the general phase characteristics of plane waves in an
infinite plaama are discussed. It Is shown, by solutloe
of the Maxwell equations, for general wave propagation
along an externally-superimposed magnetic field, that
it ia in general impossible to separate TE and TM
modea except at cutoff. The general, exaa theory de-
veloped is applied to the problem of a circular wave-
guide filled with a uniform plasma and having a magnetic
field directed along the symmetry axis. The method is
also applicable to other problems involving propagation
along the externally-superimposed magnetic field.
(Author)
116
Utalversity of Southern California. Engineering Center
Loj Angeles.
MICROWAVE MEASUREMENT OF ELECTRON DEN-
SnY DISTRIBUTIONS IN PLAa^A COLUMNS, by
Qoixlon E. Stewart and Zohrab A. Kaprlellan. Tfcduil-
csl note on Contract AF 49(638)522. 29 July 60, 45p.
USCEC rept. 79-201; AFOSR-TN-60-927; AD-243 530.
Older from LCm 1(3. 30, ph$7. 80 PB 150 9P8
Numerous applications of the arc discharge tube in the
itudy of plasmas require some knowledge of the elec-
tron density as a function of position in the tube. In
leneral, the region of the discharge called the "posi-
tive column" is used for studying the properties at this
plasma. In the positive column Sie electron density is
Independent of axial or longtitudlnal coordinates, but
does vary with the radius. It is the objective of this
psper to describe a method for explicitly representing
tbe radial dependence of the density in terms of a se-
ries of orthogonal polynomials of the radius, the co-
efficients of which are evaluated by the shift in fre-
quency of resonance of microwave cavity modes.
(A»tfhor)
University of Southern Calif ornia . Engineering
Center. Los Angeles.
RADIATION FROM A GAP-EXCITED CYLINDER
SURROUNIKD BY A UNIFORM PLASMA SHEATH, by
Hans H. Kuehl. Rept. on Contract AF 19(604)5722.
30 June 60, I9p. 2 refs. USCEC rept.* 71-202; ERD
TN-60-785.
Order from LC ml$2. 40. ph$3. 30 PB ISO 734
The far-zone electromagnetic radiation from a long,
pp-excited. perfectly conducting cylinder surrounded
bjra uniform plasma aheath, is derived. The gap la
taken to be very narrow In the axial direction and en-
circles the cylinder; the Impressed electric field in
the gap is in the axial direction. A general Integral
expression for the far-zone radiation is presented for
irbltrary cylinder lengths and the exciting gap not
necessarily in the midplane of the cylinder. For the
case of infinite cylinder length, the integral can be
easily evaluated; this result being the zero-order ap-
prodmation to the finite length cylinder. Radiation
panerns for the Infinite cylinder of small radius and
riieath thickness are presented for various values of
the plasma frequency . (Author)
Western Reserve U. , Cleveland, Ohio.
"niB INTERNAL STATE OF A GRAVITATING GAS,
tyC. E. Tauber and J. W. Weinberg. Technical rept.
lor 1 June 58-10 Dec 59 on Contract Noor- 1439(05).
10 Dec 59, 77p. 22 refs. AD- 237 969.
*der from LC mi$4.50, ph$12.30 PB 147 908
Tlie Blgnlflcance of a theory of gravitational equilib-
tkm of concentrated masses is discussed in connec-
tJoowlth possible general relatlvlstlc effeas in white
*»«rf stars. TTie covariant form of phase space and
Uourille's theorem is developed, using the canonical
«|uatlona for a particle under gravitational and elec-
tromagnetic farces. The dynamical isotropy of the
tdeal fluid is formulated, and the associated equations
<f state and allowed streaming patterns are found. A
owariant kinetic theory yields general relatlvlstlc
•«m» for the Maxwell and Fermi distributions in the
"^ae of thermal equilibrium, and limits their stream-
ing to rigid motion. Raating fluids are studied in
comovlng coordinatea, and the problem of determining
their gravitational equilibrium la reduced, in most
cases of physical l^erest, to a aimple standard form
with constant density and vortlcity. (Author)
Thermocl)rnamics
Avoo-Everett Research Lab. , Mast. i
CONTINUUM INFRARED SPECTROM OF HIGH '
TEMPERATURE AIR, by Raymond L. Taylor. Rept.
on Contract DA 19-020-ORD-4862. June 60, 19p.
14 refs. Research rept. 88.
Order fnxn LC mi$2. 40, ph(3. 30 PB ISO 955
It has been possible to measure the absolute intensity
erf Infrared radiation from air shock heated to an equi-
librium temperature of 8(XX)(>K and nearly atmospheric
density over tbe wavelength range of 2 - 6. 5 fj. The
continuum radiation is due primarily to free-free
scattering of electrons by atoms and molecules. The
general level of intensity, but not the wavelength de-
pendence. Is predicted by a calculation of the Kramer'i
radiation using a coulombic field of effective nuclear
charge, Z ■ 0. 15. The temperature dependence of
this radiation measured ab 2. 35 |Land 3. 88 ^.over the
range of 6000-8000°K is found to follow the tempera-
ture dependence curve appears around 3. 6 - 4. 0 jl
The origin of a band system in this region is not known,
although it would appear to Involve an electron collision
process. (Author)
Brown U. Dlv. of Engineering, Providente, R. I.
STEADY- STATE THERMAL STRESSES W AN
ELASTIC CONE, by Rokuro Muki and Eli Sternberg.
Technical rept. no. 14 on Contract Nonr- 562(20) and
Rept. on Contract Nonr-562(25). Nov 59. 41p. 21 refs.
Nonr 562(20)/ 14; AD- 229 493.
Order from LC ml$3. 30, ph$7. 80 > PB 150 474
A determination was made oi the steady- sute thermal
stresses generated in an elastic circular cone of semi-
infinite extent by a discontinuous distribution of the
prescribed surface temperature. Specifically, the
surface of the cone is exposed to a constant tempera-
tlire up to a given distance from the vertex, the re-
mainder of the boundary being maintained at a distinct
uniform temperature. A solution to the associated
thermoelastic problem is established in real integral
form. This solution, which is exact within the clas-
sical theory of elasticity, is deduced with the aid of
the MelUn transform. Ulustrative numerical results
are presented for the thermal stresses along the axis
and at the surface of the cone, corresponding to an
opening angle of 60°. The scheme erf analysis em-
ployed in connection with the current thermoelastic
investigation is adaptable to an explicit treatment of
ordinary elastostatic boundary- value problems for a
cone subjected to piecewise continuous surface loads.
(Author).
/
117
Convalr, Pomona, Calif.
THERMAL STRESSES IN A PERFORATED SQUARE
PLATE, by R. D* Sutherland and S. M. Manvllle. Rept.
on Contract AF 49<638)592. June 60, 39p. 5 refs.
TM-349-19; AFOBR TN-60-840; AD- 242 797.
Order from LC itil)3. 00, ph$6. 30 PB 150 738
1 The thermal streiBs problem in a square plate containing
a central circular hole is solved using the complex anal-
yais of Muskhellahvili and conformal mapping. A tem-
perature distribution for this configuration is observed
experimenully. tThis distribution is used in conjunction
with the results cif the analysis to calculate the thermal
stresses in the place. The stresses thus obuined are
presented as functions of radial and angular displace-
moit tiiroughout the plate. (Author).
DukeU. [Durham, N. C. )
A CLASS OF SOLUTIONS OF THE EQUATIONS OF
THERMOELASTIC EQUILIBRIUM, by Ian N. Sneddon.
Rept. on Contract AF 18(600)1341. Aug 60, lip.
9 refs. AFOSR-TN-60-1046; AD-243 176.
Order tram LCml$2. 40, ph$3. 30 FB 152 068
In this paper a wlIuclaD is given of the equations of
tbermoelasdc eq^llbrium appropriate to problems In
which the coodlti^s
are imposed. It 1 i not assumed that the normal com-
ponent cf stress i ^ is also zero.
Institute of Engilieering Research, U. at California.
Berkeley.
THE INFLUENCE OF HYDROGEN RECOMBINATION
ON TURBULENT FLOW HEAT TRANSFER TO A
FLAT PLATE, ta^ L. L. Cobb. Jr. Master's thesis.
Rept. on Contract DA 04-200-ORD-776. 1 June 60, 44p.
15 refs. Rept. na HE- 150- 183; Series oo. 128, issue
na 5.
Order from LC nti$3. 30, pbl?- SO FB ISO 762
A previous study 0l the heating characteristics of an
ovygao- acetylene iflame apparatus for surface ablation
WudiM showed a large difference between measured
heating rates and those predicted by convection heat
transfer theory. Since atomic hydrogen was present in
the flame, it was postulated that the exothermic recom-
bination at these 4toms waa responsible for the in-
creased energy cnansfer. The present investigation was
undertaken to stujy this possibility. A discussion of
convection heat tramsfer in dissociated gas systems is
presented. /.Experimental measuremenu were made to
verify the niagnitilde of the lotil heat flux and to estab-
lish the recombination mechanism. The experimental
measurements vefified the flux magnitudes predicted by
the theory; volum* recombination was established as
the procesa re«po(isible for the recombination reaction.
Massachusetts lAat. of Tech.. Cambridge.
AN EXPERIMENTAL APPROACH TO THE DETER-
MINATION OF GASEOUS TRANSPORT PROPERTIES
AT VERY HIGH TEMPERATURES, by I. Amdur.
Technical rept. no. 4 on Contraa Nonr- 1841(23).
30 Nov 59, 21p. 2f refa. AD- 230 116.
Order from LC ml$2.70. pfa(4.80 PB 150 486
Values of gaseOua transfx>rt properties at elevated
temperatures may be calculated from appropriate
kinetic theory relations (or from statistical mechanlci
if equilibrium properties are of Interest) provided that
the correa Intermolecular potential functions are
known. It Is pointed out that the potentials for this pur-
poee may not be exirapolationa of functions which are
valid only for relatively large distances of separation,
and therefore suitable only for calculation of low tem- •
perature properties, but must be ones which are valid
at the smaller distances at separation of importance «
elevated temperaturea. The experimental procedure ia
described for determining such potentials from elastic
scattering of neutral beam particles having kinetic
energies of the order of 1000 ev. It is shown that
meaningful potential energy information cannot be
deduced from such experiments unless the shape and
intensity distribution of the beam, as well as the
geometry of the beam-detector system are taken into
account. Results are tabulated for the potentials of a
number of atom-atom and atom-molecule systems and
a procedure for obtaining molecule -molecule Inter-
aalons for such results is indicated. (Author)
Massachusetts Inst, of Tech. , Cambridge.
IONIZATION IN SEEDED DETONATION WAVES, by
Satyaki Basu. Rept. on Project Squid, Contract Nonr-
1858(25). Nov 59, 30p. 18 refs. Technical rept.
MIT- 22- P; AD- 229 112.
Order from LCmi$2. 70, ph$4. 80 FB ISO 532
An investigation was made of equlmolal oxy-C2H2 det-
onations at 1/10 atm Initial pressure, which were
seeded with C2HK to obtain good conductivity. Finely
ground C2HK was injected into the initial mixture .
Conductivity was determined by a magnetohydrody-
namic interaction method developed by Lin (J. Appl.
Phys . 26:95, 1955). Measured conductivities were
compared with the results of thermodynamic equilib-
rium calculations , which included the cooling effect
due to the heat capacity of the additive. Theoretical
and measured conductivities agreed within a factor of
2, the agreen^ent Improving with Increasing mole
fraction of K. An electron-gas cross section of
2.5 X 10" 15 cm2 agreed with theory and experiment.
Physical Research Lab. , Space Tech. Laba. , Inc. ,
Los Angeles, Calif.
SUPERFAST PINCH STUDIES, by Lee O. Heflinger ud
Stanley L. Leonard. Rept. on Thermonuclear Propulitai
Research, Contract AF 04(647)309. Aug 60, 64p. 16 refi
STL/TR-6O-000O- 09226.
Order from LC mi$3. 90, ph$10. 80 PB 150 890
An apparatus dealgned to accelerate protons of a hydro-
gen plaama to energies of 1 kev or ntore by means of
the radially converging magnetic piston of a longltudlaal
pinch has been constructed. A capacitor charged to Td^
agea of up to 300 kv is discharged through the plasma,
producing currenta of up to 75 ka. The ringing f requencT
la 18mc, ao that the rate of current rise la about 0. 8 x
10^3 amp/ sec. Radially converging luminous fronts wit*
maximum velocities in excess of 50 cm/)iaec are ob-
aerved and are interpreted as shock waves driven by a
magnetic piston. Magnetic probe measurements and
meaaurementa of the electric flfeld at the wall of the dis-
charge tube ahow that much of the magnetic flux Inrro-
118
duced during the first half cycle Is trapped in the hot
plaama. The effecta of varying such parameters aa the
total current, the initial preaaure of the gas, the type of
pa, and the frequency of the discharge have been In-
restigated. The experimental results are Interpreted in
terms of the claaaical Roaenbluth-Garwin theory of the
ptnch, which seems to correlate well with the obaerva-
tiooa. (Author).
Wave Propagatiion
Air Force Cambridge Research Labs. , Cambridge,
BACK SCATTBRMG FROM CONDUCTING SUR-
FACES, by Roy (31 Spencer. Apr 51, 18p. 7 refs.
B5070.
Order from LC mi$2. 40, pb$3. 30 FB 152 616
This report releaaed for sale to the public 16 Nov 60.
Three methoda of analysis are diacusaed: (1) Geomet-
ric Optica. The mean back scattering cross section ^
far all orientations of a amooth, convex closed surface
It X ~S/4 where X is the mean ahadow area of die
surface and S is the total aurface. Any particular ^is
given by 7RxR2 where Ri and R2 *re the principal
radii of curvature at the point at Incidence. (2) Fhyai-
cal Optics. This neglects polarization and leads to
r"(4 '^g^/A^ where g la the effective flat-plate area
of the surface and ia usually approximated by l/f
times the area of the flrat Freanel zone (area cut by
the plane wave a distance A/4 beyond the point of
ioddence). (3) Elearomagnetic Theory. With certain
Umpllfying aaaumptlgna, there la no depolarization.
Again. «r - (4 irg^yA^ where g - [e^ikP dA. The
method is applied to (a) the inclined rectangular plate
and (b) surfacea of revolution observed end-on. In-
cluding spheres, elllpaoiclb and cooes. The upered
cone has a value of <r- ( .^/16/r )tan*d where 6 Is the
aagle between the axis and the conical elementa at the
Up. This value increaaea slowly aa the cone la tilted.
The validity cf the aaaumptlona ia to be questioned In
•uch caaea of extremely small values of <r. (Author)
Bolt Beranek and Newman. Inc. , Cambridge. Maas.
INPUT IMPEDANCES OF SIMPLE CYLINDRICAL
yiRUCTURES. by Peter A. Franken. Kept, on Contract
Nonr- 2322(00). 10 Nov 59. 22p. 3 refa. Repc na 690.
Order from LC ml$2. 70, phR 80 FB ISO 879
A thin cylindrical ahell driven in vacuimi below its ra-
dial resonance may be deacribed by membrane theory.
Each non-axis]minietric modal lixqwdance contalna a re-
•Istance and a maaa of equal magnitude, aa in the case
of an Infinite bar. The impedance decreases with in-
creaaing mode number up to a "cutoff" mode, and stiff-
Mss effects become important for modes above the cut-
off mode. The analysis include* finite ahella and rlnga.
(Audior).
Brown U. Dlv. of Engineering, Provldenoe, R. I.
WLSE DIFFRACTION BY AN IMPERFECTLY RB-
PUBCTING WEDGE, by V. M. Papadopouloe. Sden-
ttflc rept. no. 8 on Research Directed Toward the
Study of Radiation of Electromagnetic Waves, Con-
tracts AF 19(604)4561 and Nonr-562(24). June 60, 16p.
15 refs. Scientific rept. AF 4561/8; APCRC TN-
60-597.
Order from LC mi$2. 40, pb$3. 30 FB 152 069
A aimllarlty method la used to develop a aolutlon of
the wave equation within a sector with mixed boundary
condltlona. In this manner the field which results from
the diffraction of an incident pulse of step function
time dependence is found. (Author)
Centro Radloelettrlco Sperlmentale "G. Marconi",
Rome [Italy].
TROPOSPHERIC INFLUENCE ON R F. BACKSCATTER
NEAR THE SEA, by L Ranzl. Scientific note no. 2 on
Contract AF 61(052)139. 30 Mar 60. 7p. 1 ref. AFCRL-
TN-60-953.
Order from LC ml$l. 80. ph$l. 80 FB 160 650
Very Intense echoes backscattered from mountains near
the coastal boundary at distances i^ to 100 km and more
are observed on frequencies between 3 and 7 Mc/a. The
Intenalty of the echoea ahowa a diurnal variation with a
midday maximum and a day to day variation, apparently
connected with the meteorological conditions, lliis be-
havior and the high value of the backscatter crosa sec-
tions, resulting from the meaaurementa, ahow that the
backacatter mechaniam for R P. radio wavea la
atrongly influenced by the tropoqihe^c refraction.
(Author).
Ionosphere Research Lab. , Pennsylvania State U. .
University Park.
P0LARIZATIC»4 OF VERTICALLY INCIDENT RADIO
WAVES AT A FREQUENCY OF 300 KC/S, by
J. M. Greene. Scientific rept. no. 137 on Ionospheric
Research. Contract AF 19(604)4563 and National
Science Foundation Grant G 5939. IS Aug 60, 61p.
6 refa. AFCRL TN-60-645.
Order from LC mK3. 90, pttflO. 80 FB 150 669
Instrumentation la described for the recording of
polarization dau on a frequency of 300 kc/s. Incident
waves are resolved into their two circularly polarized
components, the amplitudes of which are directly
recorded by the equipment . Continuous polarization
data of the main (90 km) echo have been scaled for the
period November, 1959 to March, 1960 and averaged
resulta are preaented in tabular form. Samples of
"high-echo" dau (I.e. , echoes observed at a height
above the main echo) are presented and some of the
more conunon phenomena are discussed in terms of
the classic magneto-ionic theory. Thla theory is re-
viewed in some detail in one of the chaptera. (Author)
Lincoln Lab. , Mast. Inst, of Tech. . Lexington.
ATMOSPHERIC ABSORPTION OF 10-400 IA4cps RA-
EHATICW: SUMMARY AND BIBLIOGRAPHY TO 1960.
by E. & Rosenblum. Rept. on Contraa AF 19|i04S200.
IS Aug 60. 24p. 75 r«fs. 82G-0Q21.
Order from LC miC2. 70. ph$4. 80 FB 150 507
This report attempts to summarize the presently avail-
able dau on atmospheric absorption, and to explain the
limltationt at these dau. Onphaslt is placed herein on
119
^
absorption by norknal molecular oxygen and water vapor;
ocber contributing factors are considered only inciden-
tally, if at all.
I
Lincoln Lab. . K|ass. bist. at Tech. , Lexington.
THE STEWART AIR FORCE BASE TO NORTHTRURO
TROPOSPHERIC- SCATTER COMMUNICATION SYSTEM
by C. L. Mellen, D. H. Hamilton, Jr. and others.
Rept. on Contract AP 19<122HS8. 18 July 58, 24p.
7 refs. Technical rept. no. 183; AD- 133 863.
Order from LC nf i$2. 70, ph$4. 80 PB ISO 610
i '
The results of th^ operation at an experimental UHF
tropospheric- scatter communication system suitable
for Texas Tower to shore application are presented.
The system provided 72 voice- telephone channels be-
tween terminals separated t^ more than 200 statute
ailes. bicluded 4re conclusions and recommendation!
for new design anfl operating criteria in future tropos -
pheric- scatter syktems. (Author)
!ykt
^ples U. duly .
FURTHER EXPEtlMENTS OF IONOSPHERIC SEIJ--
MODULATION AT OBUQUE INaDENCE, by Mario
Cutolo, Maria Cioffi and other a. Scientific rept. no. 1
on Contraa AF 61(514)1229. 5 jan 60, 54p. 15 refa.
AFCRC-TN-60-210.
Order from LCn^3. 60, pb$9. 30 FB ISO 928
\
i
National Bureau n Standards, Boulder. Colo.
(QUARTERLY RADIO NOISE DATA, JUNE, JULY,
AUGUST 1959, bf W. Q. Crichlow, R. T. Disney, and
M. A. Jenkins. 9{Sep60, 65p. 11 refs. IVschnical note
no. 18-3,
Order from OTS 11.00 PB 151 377-3
See also PB 151
r
National Bureau of SUndards, Boulder, Colo.
(QUARTERLY RADIO NOISE DATA, SEPTHk4BER,
OCTOBER, NOV^BBR 1959, by W. Q. Crichlow,
R. T. Disneyj an4 M. A. Jenkins. 28 Sep 60, 64p.
11 refs. Technical note no. 18-4 .
Order from OTS ll. 50 PB 151 377-4
See also PB 151 3" 7-3
National Bureau of Standards, Boulder, Colo.
(QUARTERLY RADIO NOISE DATA, DECHb^BER,
JANUARY, FEBRUARY 1959-60, by W. Q. Crichlow,
R. T. Disney, ani M. A. Jenkink. 10 Oct 60, 66p.
II refs. Technical note no. 18-5.
Order from OTS ^1.75 PB 151 377-5
See also PB 151
t
'National Bureau of Standarda, Boulder, Colo.
TABLE OF MAGNITUDE OF REFLECTION COEF-
FICIENT VERSUS RETURN LOSS (Lr -20 log^o i.i
by R. W. Beatty and W. J. Anaon. 19 Sep 60, 47p. " '
3 refs. Technical txxe no. 72.
Order from OTS SI. 25 PB 161 573
The following table ylelda values of r for a given vahit
of R according to the relationahip R * 20 logio -t
The range and intervals al R are aa follows: 0.(j000
(0.0001)0.0100, andO 000(0 OOl) 20.000. One can
extend the use of the tables to higher yaluea of R
merely by shifting decimal points in an appropriate
manner. The intervals are sufficiently amall to per-
mit convenient and accurate inverse interpolation.
The seven significant figures given in the table are
estimated to be correa except for an occasional error
of one digit in the last place due to rounding.
Purdue Research Foundation. Lafayette, Ind.
THE SCATTERING OF A PLANE ELECTROMAG-
NETIC WAVE BY A FINITE CONE, by C. C. Rogers
and F. V. Schultz. Scientific rept. no. I on Contract
AF 19(604)4051. 1 Aug 60, 72p. 34 refs. ERD-TN-60-
765.
Order from LC mif4. 50. ph$l2. 30 PB 150 874
This paper treats the solution of the vector Helmholtz
equation for the case of a plane electromagnetic wave
at 'no«e-on' Incidence on a perfectly-conducting coaed
finite aize. The solution presented la exact and in the
form at an infinite series of spherical harmonics. The
ejqMmaion coefficients of the series are determined by
a set of an infinite number of eqviations involving an in-
finite number of unknowna. A dlacuaaion and numerical
.investigation oif the field singularitiea at the tip and ed|i
of the cone are included, aa well as graphs of the aaso>
elated Legendre functions of non- integral degree, P|^
(coa 9). and their firat derivatives. (Author). "
Technical Research Group, Syoaset, N. Y.
SURVEY OF THE LITERATURE ON MILLIMETER
AND SUBMILLIMETER WAVES, by Jerome Lurye.
Scientific rept. no. 2 on Contract AF 19(604)4574,
30 June 60. 103p. 213 refs. TRG-127-SR-2; ERI>TN-
60-762.
Order from LC mif5. 70, ph)l6. 80 PB 152 OSl
This report contains a survey of the literatuire on milli-
meter and aubmilllmeter waves with emphasis on their
application to the problem of conununlcatlon between
two high altitude hypersonic vehicles. The topics cov-
ered are sources and amplifiers, the effect of the ion-
ized sheath, propagation phenomena, and (briefly) de-
tectora. The survey is followed by a comprehensive
bibliography of the aubject. The bibliography covers
the decade from 1950 through 1959; however, some
earlier and some more recent references have been in-
cluded. (Author).
University of Soikhem Califomiay Engineering Center,
Los Angeles.
A STUDY OF THE TRANSMISSION OF RADIO SIG-
NALS FROM A HYPERSONIC VEHICLE, by Raymond
L. Chuan, Hans H. Kuehl, and Zohrab Kaprielian. Rept
on Contract AF 19(604)5722. 30 June 60. 32p. 9 refs.
USCEC rept. 71-101; ERD-TR-60-176.
Order from LC m43. Oa pb$6. 30 PB 150 735
In order to acquire some understanding of the mecha-
nisms whereby the propagation of an electromagnetic
signal is £^ected by the pressure of a partially ionized
gas layer (the "ion abeath") adjacent to a hypersonic
120
^chicle, a program of research conbining theoretical
aad experimental efforts was Initiated. The first year's
tUkB consisted of (1) the modification of a low density
liypersonlc wind tunnel to produce flows at Mach number
14 at an equivalent altitude of about 3001 000 ft. and a
teloclty of about 15. 000 ft. /sec. ; (2) a study of scaling
parameters to render possible the extension of model
ftudies to full-scale flight conditions; (3) theoretical
ttudles of the effects of a uniform plasma sheath on the
radiation of a finite cylinder; (4) determination of the
electronic and aerodynamic confi^rations for the wiixl
tunnel experiments; and (5) exploratory studies of the
use of 8 microwave interferometer for the determina-
tion of electron density. (Author)
Ballistic Research Labs . . Aberdeen Proving Ground,
Md.
INSTRUMENTATION FOR THE DETERMINATION OF
PHOTOOkAPHIC IMAGfe CORRELATION, by Donald F.
Menne. June 60, 18p. Technical note no. 1315.
Order from LC mi$2.40. ph$3.30 PB 150 418
A description of instrumentation for correlating photo-
graphs of selected subjects is presented. The tech-
lique employs a parallel light beam which is inter-
sected by a stationary photograph and a movable 1
photograph. A comparator has been modified and '
adapted to transport the movable photograph on its
stages and provide the facilities for measuring the dis-
placement between the two photographs . Correlation is
indicated by a photosensitive device which measures
the amount of light passing through the photographs .
Results from the correlation of a high contrast pattern
Illustrate the sensitivity and reproducibility of the
measuring system. Samples of auto-correlation and
cross -correlation of selected subjects are included.
(Author)
Human Sciences Research, Inc. , Arlington, Va.
METHODOLOGY FOR ANALYSIS OF MAN'S ROLE
IN AN ADVANCED SPACE FUGHT SYSTEM. A
CASE ^UDY IN SYSTEM RESEARCH METHODOL-
OGY, by Peter G. Nordlie. Rept. no. 5 on Contraa
Norr -2525(00). Nov 59, 17p. 1 ref. HSR-RM-
59/25-SM; AD-229 925.
Order from LC ml$2. 40. ph(3. 30 PB ,150 838
The tasks described represent the logical sequence of
steps taken to develop design requirements for the dis-
plays and controla of the apace vehicle cockpit. The
flhaae /function analysis resulted in a set of required
woctional activities, which were tentatively assigned to
human and equipment components. These functional
activities were translated into a set of required input
tad output {>arameters, which were in turn described on.
a time base in the SSOA (Second -by -second Operational
Analysis). Results of the SSOA were summariied to pro-
vide indices of work load, link frequency, and use/fre-
<)uency. These indices in turn helped to specify design
(Research Methods, Techniques and Equipment, 1 3 |an 60)
requirements for the cockpit and for the displays and
OODtrols it contained. (Author)
Human Sdencea Research. Inc. , Arlington, Va.
METHODOLOGY FOR EVALUATION OF A MAN-
MACHINE SURVEILLANCE SYSTEM, by John A.
Whittenburg. Rept. «6 on Contraa Nonr- 2525(00).
Dec 59, 23p. 7 refs. HSR-RM-59/26-8m; AD-234 464.
Order from LC ml$2.70, ph$4.80 PB 152 146
A case study at system research methodology.
Human Sciences Research, Inc. , AHlngton, Va.
MONTE CARLO METHODS AS TOOLS FOR SYSTEM
RESEARCH. A SPECIAL REPORT IN A PROGRAM
OF STUDY OF SYSTEM RESEARCH METHODS, by
Alvin L. Schreiber. Rept. no. 7 on Contraa Nonr -
2525(00). Nov 59, 23p. 13 refs. HSR-RM-59/27-SM;
AD- 229 926.
Order from LCml$2. 70, ph$4. 80 PB 150 839
A research program aimed at synthesis (A system re-
search methodology is continuing. Major features of
one important class d analysis techniques, Moiue
Carlo methods are summarized. Ways in which these
methods can be utilized in system research are pre-
sented. The mathematical iMses and the computational
procedures associated with Monte Carlo methods are
not treated except as they are essential to exposition.
The kinds of problems to which these method»can be
applied, the conditions necessary for their application,
and the kinds of solutions Which they can provide are
studied. (Author)
RESEARCH METHODS, TECHNIQUES
AND EQUIPMENT
Human Sciences Research, Inc. . Arlington, Va.
RESEARCH METHODOLOGY REQUIREMENT-
SETTING STUDIES, by Joseph E. McGrath and Peter G.
Nordlie. Rept. no. 3 on Ckmtraa Nonr -2525(00).
Nov 59, 43p. 49 refs. HSR-RM-59/23-SM; AD-229 924.
Order from LC ml$3. 30, ph$7. 80 PB 150 837
The methods which have been used in system research
studies designed to establish various types of require-
ments for manned aspects of a complex man -machine
system, principally weapon systems, were examined
with reference to the review oi approximately 50 perti-
nent research studies. Emphasis was placed on studies
dealing with requirements for those aspects of the sys-
tem relating to the human operator. Results of the
review were organized by classifying studies into types,
by dividing the total research task into phaaes, and by
compiling and comparing the research methods used
for studies of each type within each phase. Within these
requirement -setting studies, areas where a relatively
well articulated set of procedures exists, as well as
areas where systematic, explicit methodology has not
yet been fully developed, are indicated.
Human Sciences Research, Inc. , Arlington, Va.
A SYSTEMATIC FRAMEWORK FOR COMPARISCW OF
SYSTEM RESEARCH METHODS, by Joseph E. McGrath.
Peter G. Nordlie. and W. S. Vaughan, Jr. Rept. no. 1
on Contract Nonr-2525(00). Nov 59, 71p. 50 refs. HSR-
TN-59/7-SM; AD-229 923.
Order from LC mi$4. 50, ph$l2. 30 PB 150 836
121
i
Contents:
The problem and stutly approach
HistoricaKdevelopTfient of system research
Discussion of system research orientations
Phase I: Study apprt»ach
A descriptive framelrork for comparison at system re-
search methods
Structure of a system research problem
Descriptive classification of the system research
process
Development of models in system research
Collection of inforr^ation in system research
Synthesis of information in system research
Some concepts for a tljeory of method in system
research
A model at researbh information
Reformulation of the descriptive framework
Evaluation and program plans
Naval Ordnance L4b. , Corona. Calif
FOUNDATIONAL RESEARCH PROJECTS Quarterly
rept. for kpr-Juoe 6fi. Aug 60, 48p. 40 refs.
NAVWEPS rept. 6005; NOLC rept. 514.
Order from LC ml$$. 30. ph^. 80 PB 152 035
Contents: I
Ferroelectric phenomena
High temperature polymer program
Small antenna study
(See also PB 149 084|>
mation items into an integrated picture. Addressing
refers to the question at who needs certain categories
at informatian. (See also PB 143 465)
Uijti
Remington Rand Ui^v«c Dlv. . Sperry Rand C>3rp. ,
fPMladelphia, Pa]
DIRECTIONS IN THE RETRIEVAL OF SCIENTIFIC
INFORMATIOI. by C K. Schultz and C. A. Shepherd.
Rept. on Contraa Nonr- 2297(00). [1959] 32p. 15 refs.
AD- 228 389.
Order from LC ini$3|.00, pti)6.aO FB ISO 81 A
The role in scientific communication of s«CQiidary pub-
lications, such as abstracts and indexes, is traced
from the early days of science to the present time in
order to elucidate evolutionary trends. A brief evalu-
ation is then given of the current conununlcatloa net-
work with respect to Its evolutionary maturity for the
field of science as a whole, and for individual scien-
tific disciplines. (Author)
Institute for Applied ;Bxperimental Psychology, Tufts
U., MedfordMsss. I
RESEARCH INVOLVING COMMUNICATION PROC-
ESSES IN TASK 0RI8NTED GROUPS, by Thornton B.
Roby, Bernard W. Harleston. and Lorraine D. Eyde.
Technical rept. no. 2 on Contract N«jnr-494( 15).
IS Nov S9, I2p. 3 ref^. AD-230 421.
Order from LC ml$2. «0, ph$3. 30 PB 150 495
Five broadly defined aibfunaicns of group performance
were investigated. These were: vigilance; phasing:
storage; patterning; and addressing. The general notion
of vigilance refers to the probability of speed with which
persons detea ceruint critical environmental signals.
Phasing is concerned with temporal relationships amon^
the component actions performed by various group
members. Storage is defined as the extent to which In-
formation is retained (or direct use in guiding group
actions, nineming consists of grouping various infer -
Communication Theory
Ohio State U. Research Foundation, Columbus.
VOICE COMMUNICATION STUDIES, by John W. Black.
Final rept. for 1 Oct 49-30 Sep 59. Contract N6onr-225(25)
29 Dec 59, 17p. 109 refs. Rept. 398- Final; AD-232 565.
Order from LC mi$2. 40. ph$3. 30 PB 152 172
A bibliography is presented of research In voice com-
munications conducted by the Ohio State University
foundation between October 1, 1949 and September 30,
1959. The bibliography may be viewed as related to
these topics: (1) voice intelligibility; (2) dimensions of
voice; (3) problems in listening; (4) hearing oneself,
side tone; (5) the langfuage of voice communication; (6)
problems in hearing; and (7) the evaluation of equip-
ment. In addition, a brief report is presented on the
XI Congress of the International AssocUtlon of Logo-
pedlcs and Pbonlatrlcs.
SOCIAL SCIENCES
Northwestern Technological Inst. , Evanston, III.
INDUCTIVE INFERENCE AND BUSINESS BEHAVIOR,
by R. W. Glower. ONR Research memo. no. 25 on
Temporal Planning and Management Decision under Risk
and Uncertainty. Contract Nonr- 1228(10). Dec 59, 15p.
7 refs. AD- 237 866.
Order from LC ml$2. 40, ph$3. 30 PB 148 197
An attempt was made to remove the shortcomings of
traditional price theory as an instrument for describing
observed market behavior. The approach taken was one
which lies between the revolution of the foundations of
traditional price theory and the evolution of its super-
structures. To elaborate upon this dieme, a simplified
learning model of oligopoly was sketched which is
broadly consistent with traditional doctrine yet suffi-
ciently general to include both the established monopoly
theory and the accepted theory of pure competition as
special cases. The unifications of existing theories by
recognizing that all of them are equally indeterminate
in the absence of specific assumptions about the way in
which market participants learn from experience was
suggested.
Wisconsin U. . Madison.
HIGH LATITUDE FRINGES OF SETTLEMENT, by
Kirk K Sione. Annual rept. on Contract Nonr-1202(05
1 Dec 59, 18p. 6 refs. U. of Wis. no. 86:2439;
AD- 229 922.
Order from LC ml|2. 40. ph$3. 30 PB 152 110
The principal objective is to determine what settlement
experience in Scandinavia (countries of older settle-
ment) may be used in planning for pcesent and additional
settlement in northern North America (countries of
newer settlement). These data may be ofaulned by the
122
location, classification, and determination of the char-
acteristics of the fringe of settlement regions in
}jorway, Sweden. Finland, northern Canada, and
Alaska. Especial attention is given to the measure-
ment of the degree of permanence of settlement in
Itiese areas. (See also PB 143 859)
Documentation
Center for Documentation and Communication Re -
search. Western Reserve U. , Cleveland. Ohio.
CHEMICAL NOTATION STUDY: DYSON -WISWESSER
NOTATION SYSTEMS: ENCOEHNG OPERATIONS, by
Allan D. Pratt and James W. Perry. Phase rept. rev.
00 National Science Foundation Contract G 5754.
1 Aug 60, 53p. 2 refs. i ji
Older from OTS $1.50 ' '! PB 1^1 123
A comparison was made of the structural -formula
chemical -noution systems developed under the leader-
ship of G. M. Dyson (Proposed international chemical
nomioa- tenutive version. Prepared by the Connmis-
sioo on codification, ciphering, and punched card tech-
■iques of the lUPAC. Longmans, Green and Co. .
LoBdoo, 1958) and William J. Wiswesser (Llne-
{onauii chemical noution. Thomas Y. Crowell Co. .
N. Y , 1954). Three thousand structural formulas for
encoding, provided by the Chemical Abstracts edi-
torial office from Section 10 of that Journal, were di-
vided into 3 Jtroups of 1000 each. Each trroup of 1000
compounds was encoded by each of the 2 systems by
one each of 3 practicing chemists, 3 students working
Rward the doctorate in chemistry, and 3 undergraduate
students majoring in chemistry. The E>yBon ciphers
lere cprrect in 42. t% of the cases and the Wiswesser
codes in 46 6%. The 4. C% difference is not meaning-
Ad. Undergraduate students achieved higher accura-
cies (58. 3 and 56. 4%) than either graduate students
(41. S and 50. 2^) or tbe practicing chemists (28. 0 and
33. OJ^) in both the Dyson and the Wiswesser systems,
hrticipants thought ttiat both systems contalned'am-
liguities and unclear directions.
Remington Rand Univac Div. , Sperry Rand Corp.
[Philadelphia, Pa.]
A COMPUTER ANALYSIS OF THE MERCK SHARP
AND DOHME INDEXING SYSTEM, by Claire K. Schuli
tod Clayton A. Shepherd. Kepi, on Contract Nonr-
2297(00). [1959] 37p. AD- 229 380.
Order from LC ml$3. 00. ph$6. 30 PB 150 819
I'
"^ MISCELLANEOUS
Naval Research Lab. . Washington, D. C.
REPORT OF NRL PROGRESS. Dec 60.
Order from OTS $1. 25, (10. 00/year PB 161 288
Contents:
Articles:
The Shell Model of the Nucleus and Proton Capture, by
J. W. BuUer
A Six-Port Trimode Turnstile Waveguide Junction, by
R. S. Potter and C E. Jedrey. Jr.
Scientific program:
Atmosphere and Astrophysics: Atmospheric scattering
of aerosols in the visible and Infrared. Flights at im-
proved balloon-borne meteorological station (Transo-
sonde) yield data on the vertical motions of air
Chemistry: Filterability of distillate fuels. 1: develop-
ment of methods and effect of filter porosity. Kinetics
of hydrogen evolution at zero hydrogen partial pres-
sure. A dry chemical system for carbon dioxide re-
moval from submarine atmospheres
Mathematics: Functional electromagnetic constitutive
relations
Metallurgy and Ceramics: Cre^ rxipture data for
0. 250- and 0. 357 -inch diameter nickel specimens at
150(PF. Pile measurements of Hall coefficient and
conductivity of silicon. Bxperimenul assembly for
studying effect of elevated temperature upon neutron -
induced changes in steel. Kinetics of CbZn2 forma-
tion on columbium in zinc vapor. Effect of oxygen
solution on the oxidation of niobium. Effect of ikhj-
adherent corrosion products on localized attack of
steel exposed to aqueous media at elevated
temperature
Optics: An f/2. 8 low -dispersion time -resolving grating
spectrograph
Radia Experimental shipboard multicouplers (2 Mc to
9 Mc) with system isolation in excess of 40 db for 5%
frequency separation and transfer efficiency of 6C%
to 70^ Analjrsis of the relationship between collision-!
avoidance trajectory of an aircraft and its perform-
ance capability. Experimental tubes constructed and
tested under high vacuum yield additional data on
electrical breakdown in electron tubes. Electron gun
for a lumped -parameter, backward-wave amplifier
(225 Mc to 400 Mc)
Solid -State Physics: Solid-state analog of the Bragg -
Gray cavity ionization chamber. Vibrational contri-
bution to specific heat near phase change. Effect of
pressure on the absorption spectra of phosphors: III.
Ka:Tl
Sound Effect of hydrostatic pressure on three types of
resistors (the carbon composition type exhibits
adaptability for pressure transducer applications)
123
J
ATOMIC ENERGY COMMISSION REPORTS
ReoortB may be purchased In accordance with instructions on the inside front cover o< the U. S.
fiOVERNMENT RESEARCH REPORTS. As PB numbers are not indicated, order by series and number.
These reports may also be consulted at any ABC Depository Ubrary. A list of these libraries may be
flbttlned from the U. S. Department of Conunerce. Office of Technical Services. Washington 25. D. C.
Reproduction in whole or part of any report listed herein is encouraged by the U. S. Atomic Energy
Cominlssion subject to the approval of authors or originating sites. General inquiries from the indus-
ffUl press about ABC -developed information should be directed to the Industrial Information Branch,
Atomic Energy Commission, Washington 25, D. C.
Bio
f'l
ogy and Medicine
ttological. chemical studies of "^r^g planktMi.
Appendices to reference no. 60-6 cwKJucted
aurifij^ the pericxl May 15 through December 31,
l959 Woods Hole Oceanographic Institution.
li^iFa. Feb 60.
Order from LC.
Contract AT(30-l)- 1918. 159p.
Mi $7. 50. phJ24.30.
AECU-4703
Biological and medical research division semiannual
rnwrt from January through June. 1959, by W. H.
Taliaferro and others. Argonne National Labor-
atory. Argonne, III
l09-cng-38. 105p.
Aug 60. Contract W-31-
Order from GTS. $2.25.
ANL-6200
A avgylement to die LMFRB preliminary hazards
e^luatioo. The Babcock & Wilcox Company,
Lynchburg, Va. June 58. Contract AT(30-1)-
1940. 27p. Order from OTS. $1.00.
BAW- 1017-1
Research in radlobiology. Annual report of work in
progress on the chronic toxicity program, by
T. P. Dou^rty. University of Utah. College
of Medicine, Salt Lake City. Utah. Mar 60.
Contract AT(ll-l)- 119. 228p. Order from LC.
Mi $9. 90. ph $34. 80. . COO-220
Hanford biology research annual report for 1959,
by H. A. Komberg and others. Hanford Atomic
PnxluctB Operation. Richland. Wash. Jan 60.
Contract AT(45-1)-1350. 205p. Order from
ens. $3.00-. . HW-65500
An analogue computer for the generalized tfaree^
coiqpartmentjpodel erf transport in biological
systems, by B. C. Gregg. Western Reserve
lAdversity. Atoinic Energy Medical Researdi
project. Cleveland. Ohio
W-31-109-eng-78. 2^.
Ml $2.70, ph$4.80.
Dec 59. Contract
Order from LC.
NYO-2096
quantiative study erf the effects of radiation oo the
blood capillaries of normal animals . Final
scientific report. University of Miami. Coral
Ciiles. Pla. Ind. 1 8p. Order from LC.
Mi $1.80, ph $1.80. ORO-230
Final and comprehensive report on work accom-
— plished. by N. T. Werthessen. Southwest roun-
dadon for Research and Education. San Antonio,
Tex. Dec 59. Contract AT(40-1)- 1776. I6p.
Order from LC. Mi $2. 40, ph$3.30.
ORO-233
The effects erf radiation on root growth erf hi
plants. Final report, by R. T. Brumfiel
Loogwood Coll. , Farmville,
tract AT(40-1)- 1676.
Ml $2.70, ph$4.80.
Va. Jan 60. Con-
24p. Order from LC.
ORO-237
ElectrocardJom-aph naeasurements at ^ration
teapot, by H. H.
_ Sander and O. J. Birdsong.
Saiidia Corporation, Albuquerque. N. Mex.
Dec 55. 22p. Order from LC. Mi $2.70.
ph$4.80. SCTM-261-55-51
Marine Sciene^s ReseareJi. by C. L. Dunham and
others. University of Connecticut. Marine
Research Laboratory. Storrs. Conn. Jan 60.
40p. Order irom OTS. 50 cents. TID-4040
Tonicity and hazareis of beryllium and rocket pro-
pellants. A literature search, by W. E. Boat.
Office of Technical Information Extension, Oak
Ridge, Tenn. Oct 60. 20p. Order from OTS.
50 cents. TID-3531 (Ist Rev. )
Bffecta erf radiatit>n on pure procelna and nucleic
acids, by Virgil L. Koeiitg. Northwestern
! prote
!lUg. \
University. , Chicago. Medical School. [Mar 60].
Project No. 8. Contraa AT(ll-l)-89. 8p. Order
from LC. Mi. $1.80 Ph. $1.80.
TID-5692
125
Snidies on chamical protection against radUtioo-
induced intcatlnal injury. Period covered: June
1. 1959-M<rch 1. iW byE. E. Schwartz and
B. Shapiro. Mar GO. Contract AT(30-l)-2406.
7p. Order from LC. Ml $1 . 80, ph $ 1 . 80.
' ^ TID-5827
DlBtributloo of Injected l^^^L labeled antibody to do|
fibrin in tumorbea ring dogs, by I. L. Spar, a^
others. University of Rodiester, Atomic Energ*
Project, Rochester, N. Y. Mar 60. Contract
W-7401-eng-49. 13p. Order fnMn IX!.
Mi $2. 40, ph$3.30. UR-569
of pro^in synthesis in the gastrointestinal KtpUi determination erf citric add in biological
: o^notmal and irradiated mioe. Final re^ fluids, by K. Lane and P. S. Chen, Jr. The
Studies
tract _ ^ -
port. Coniell University, Medical College,
iSaca, N. 1Y. [i960). Contract AT(30-1)-2179
I6p. Ordef from LC. Mi $2. 40, ph $3. 30.
TID-5882
The use of calcium -47 in diagnostic studies of
patients wli^ bone lesionsr by K. R. Corey and
others. Sl()an- Kettering Inst, for Cancer Re-
search, New York, N. Y. [19601. Contract
AT(30-1)-910. 60p. Order from LC. Mi$3.60,
ph$9.30. TID-5954
Pr
ogress report for the period October 1, 1959 to
September ^, 1960, Marquette University,
Miiwaukee, Wis. I960. Contract AT(ll-l)-820.
12p. Orden from LC. Ml (2. 40, ph $3. 30.
TID-6043
The biologic etfects of radiation on tfayrold tisaue.
Annua fprogreas report for May 16, 1959 to
May 15._19to and renewal application, by O.
Cope. Central Hospital, Boeton, Mass. June 60.
Up. Ordei! from LC. Ml $2. 40, ph $3. 30.
TID-6063
Mechanisms o^ radiation -chemical reaction in blo-
chemical sytems, by W. M. Garrison. Univert
sity of CalUbmia, Lawrence Radiation Labors-'
tory, Berkeley, Calif. June 60. Contract W-
7405-eng-4«. lOp. Order from OTS. 50 cents.
UCRL-.9218
Progress repogt for period ending July 31, I960, by
R. S. Stone and cf. D. Adams" University of
California School of Medicine, Department of
Radiology. $an Francisco, Calif. Sep 60. Coo-
tract AT-ll-l-GEN-10, Project No. 2. 55p.
Order from OTS. $2.00. UCSF-20
Bale
Atomic
^Energy Project , Rochester, N. Y. Mar 60.
Contract W -7401 -eng-49. 2^. Order from LC.
Mi $2.70. dh $4.80. UR-567
University of Rochester, Atomic Energy Project,
Rochester, N. Y. Sep 60. Contract W -7401 -ei^
49. 7p. Order from OTS. 50 cents. UR-579
Chemistry — General
The electrochemical theory of smelting and related
reacdons. Technical report no. 36, by X. 3e
Hempdnne and others. University of Utah.
Institute for the Study of Rate Processes, Salt
Lake City, Uuh. Nov 59. Contract AT(1 1-1)-
82. 43p. Order from LC. Mi $3.30. ph $7.80.
AECU-4504
Anodic precipitation at tracer manganese as dioxide,
E. A. HeiJntz and L. B. Rogers. Massachusetta
Institute of Technology, Cambridge, Mass., and
Massachusetts Jjistitute of Technology, Labora-
tory, for Nuclear Science, Cambridge, Mass.
[19591. Contract AT(30-l)-905) 25p. Order
from LC. Mi $2.70, ph$4.80. AECU-4SM
Labora-
tories, Inc., CleveUnd, Ohio . Oct 58. Decl.
with deletions February 17, 1960. Contracts
AT(11-1)-171 andAF33(600)-38062. 77p. Order
fromLC. Mi $4.50. ph $12.30.
APEX-431(DeI.)
Diffusion at Xenon through aluminum and stainlesa
steel, by A. W. Castleman, F. E. Hoffmann,
and A. M. Eshaya. Brookhaven National Labon-
tory. Associated Universities, Inc. , Upton,
N.Y. July 60. 9p. Order from OTS. 50 cents.
BNL-624(T-190)
Process engineering report on revised process de-
sign transmitul" green aalt plant. Job no. 3dW
of die feed materials production center, Fernald,
Ohio, byC.V. Holby and F. James. Catalytic
Construction Co., Philadelphia, P«. June 52.
Decl. October 7, 1959. Contract AT(30-1)-
1060. 22p. Order from LC. Ml $2.70.
ph$4.80. CCCO-557
126
Chemistry — Radiation and Radiochemistry
The Radlochemtstry of Indium, by D. N. Sunderman
and C. W. Townley. Banelle Memorial Inst. ,
Columbus, Ohio. May 60. 46p. Order from OTS.
50 cents. NAS-NS 3014
Hatogen collector test program, Hsnford Atomic
~ rtt>ducts Operation, Richland, Wash., Div. of
General Electric. March 60. Contract AT(45-1)
-1350. 76p. Order from OTS. $2. 00.
HW- 65587
The Radiochemistry of Astatine, by Evan H.
Appelman, Argonne National Lab. , Lemont, 111.
March 60. 29p. Order from OTS. . 50 cents.
NAS-NS 3012
Ch^istry — Separation Processes for
Plutonium and Uranium
Design and Scaleup of Mixer -Settlers tor the P»pex
solvent extraction process, by A. D. Ryon, F. L.
Daley and R. 5. Lowrle. 6ak Ridge National Lab.
Oak Ridge, Tennessee, [ndl Contract W-7405-
eng-26. 74p. Order from OTS. $1.75.
ORNL-2951
A simple analysis of the tubular pinch discharge,
by Wulf B. Kunkel. University of California,
Lawrence Radiation Lab. , Berkeley, Calif.
Jul 60. Contract W-7405-eng-48. 15p. Order
from OTS. 50 cents. UCRL 9311
Criticality Stt>dies
Hazards summary report for the hanfbrd plutonlum
critical mass laboratory, by W. A. Reardon and
others. Hanford Atomic Products Operation,
Richland, Washington. Aug 60. Contraa
AT(45-1)-1350. 124p. Order from OTS. $2.50.
HW-66266
Multl -region reactor lattice studies, by Ira H. Coen,
Westlnghouse Electric Corp. , Atomic Power
Dept. Pittsburgh, Penna. Jul 60. Contract
AT(30-1)-2176. 3lp. Order from OTS. 75 cents.
WCAP-1419
Engineering and Equipment,
Leakage of water from gasketed Joints proposed for
the HWCTR, by Pr<5erlck C. AppU. B. 1. du
Pont de Nemours k Co. Savannah River Lab. ,
Jul 60. Contract AT(07-2)-l. lip. Order from
OTS. 50 cents. DP-487
Contag resistance and the effects of rhaterlals and
process variables on contact resistance and
Bibll
[lographT on nuclear reactor fuel reprocessing
ai5^«e disposal. Vol. 2, byTTP. Conoiiy" Oak
Ridge National Lab. , Oak Ridge, Tennessee.
[nd|. Contraa W-7405-eng-26. 152p. Order
from OTS. $2.75. ORNL-2971
Chemical technology division annual progress report
for period ending August 31, 1960, by F. L.
Culler and others. Oak Ridge National Lab. ,
Oak Ridge, Tenn. [ndj. Contract W-7405-eng-26.
228p. Order from OTS. $3. 50. ORNL-2993
contag reliability In switching devices, by L.
M. Berry and others. Sandla Corp. ,
Albuquerque, N. Mex. Aug 60. 50p. Oroer
from OTS. $1. 50. SCTM 73A-60(l6)
Controlled Thermonuclear Processes
^
i
Electron gun measurements In a stelUrator with
Helical stsblUzlng windings, by M. S. Jones. Jr. .
G. Hess and L. G. Smith" Office of Technical
Information Extension, Oak Ridge, Tenn. July
59. Contraa AT(30-l)-1238. 23p. Order from
GTS. 75 cams. MATT- 14
Bad-losses from mirror machines, by I. E. Roberts.
andM. L. Carr. University of California,
Lawrence Radiation Lab. , Llvermore, Calif.
Apr 60. Contraa W-7405-eng-48. 80p. Order
from' OTS. $2.00. UCRL 5651 -T
Steam Jet pump analysis and experiments, by R. P.
Rose, Bettis Atomic Power Lab. , Pittsburgh, ?»,
June 60. Contraa AT-ll-l-GEN-14. 12lp.
Order from OTS. $2. 75. WAPD-TM-227
Geology and Mineralogy
Reconnaissance tor uranium In the Salanrianca area.
Province of Coqulmbo, Chile, by P. H. Knowies,
and others. U. S. Atomic Energy Commission,
Geologlcas De Chile. July 58. 14p. Order from
OTS. 50 cents. RME-4526
Fossil fuels In the future, by M. F. Searl, Office
of Operations Analysis and Forecasting, United
States Atomic Energy Commission. Oct. 60.
63p. Order from OTS. 75 cents. TID-8209
Health and Safety
Fallout program. Quarterly summary report
E. P. Itardy, Jr. and others. United Ststes
hy
Atomic Energy Conunlsslon, New York
127
operations ofQce.
OTS. $3.00.
Oa 60. 210p. Order from
HASL-95
Rafttoacttve falky from nuclear detonations of
February and| April 1960, by A. W. Klement, Jr.
Pallout Studios Branch, U. S. Atomic Energy
Commission. Washington 25, D. C. Jun 60.
I3p. Order fnom OTS. 50 cents. TID-6235
Nuclear Explosions — Pen<*Aful Applications
Ground water In the oak spring formation and
hydrologlc effects of underground nuclear
eiq)losioiis at the nevada test site, by
A. Clebsch, Jr. U. S Geological Su rvey for
the U. S. Atomic Energy Commission. Apr 60.
29p. Order from OTS. 75 cents. TEI-759
Instrumentation of structures for air-blast and ground
shock effects ,i by J. J. Meszaros and others
. Ballistic Research Labs. , Aberdeen Proving
Ground, Md. Ian. '60. 75p. Order from OTS.
$1.75. WT-1452
Instrument*
The linear scaimy in clinical studies, by F. Plrcher,
Oak Ridge Institute of Nuclear Studies, Oak Ridge,
Pressure <^>6ervatlons In the crater vicinity during
the explosion of small charges In dry sand, by
lanoli
explosion of small charges
R. P. Reed and W. E. Taylor. Sancila Corp.^
Albuquerque, N. Mex. May 60. 33p. Order
from OTS. $1.00.
SC-4448(RR)
Tean. Aug 60. 37p.
Order from OTS. $1.00.
ORINS-36
A small wrist doaimeter for beta and ganuna
radiation, by U. H. Hubbell, Jr. a^d others.
Oak Ridge National Lab. , Oak Ridge, Tenn.
[nd). Contract W-7405-eng-26. Il6p. Order
from OTS. $2^50. ORNL-2730
Inline Instrumentation: Gamma monitor, Uranium
rolorimeter, pyj- W. Landry, Oak Ridge
National Lab. , Oak Ridge, T6nn. Sep 60.
Contract W-7405-eng-26. 25p. Order from OTS.
Plowshare series: Report No. 2, proceedings of the
second plowsha re' symposl um pa rt I . Univ. of
Calif. Lawrence Radiation Lab. , Overmore,
Calif. May 59. Contract W-7405-eng-48. I64p.
Order from OTS. $3. 00. UCRL-5675.
Particle Accelerators and Mlgh-
Voltoge Machines
The
SO cents.
ORNL-2978
Metalurgy and Ceramics
Thermal diffusion, of hydrogen in nonstoiciuonaetric
zirconium-di hydride, by A. W. Sommer.
Atomics Interiational t, Div. of North American
Aviation, Inc. , Canoga Park, Calif. Oct 60.
Contract AT(ll-l)-GEN-8. 27p. Order from
OTS. 75cents ' NAA-SR-5066
Carburlzaiion of austenltic stainless steel in liquid
sodium, by WJ J. Anderson and G. V. SneesbyT
Atomics Intemational, Dlv. , of North American
Aviation, Inc. , Canoga Park, Calif. Sept 60.
Contract AT(1 ,
75
-i)-GEN-8. 27p. Order from OTS.
KAA-SR-5282
Technical progrMJi leport to the ABC reactor division
Research Association, [nd] 35p. Order from
OTS. $1.00. MURA-569
Acceleration across transition et>ergy, by
G. Bronca. Midwestern Universities Research
Association, Madison. Wise. May 60. Contract
AT(ll-l)-384. 15p. Order from OTS. 50 cents.
MURA-575
Drift tube alignment for the AGS Ilnac, by A. Kevey.
Brookhaven National Lab, , Upton, N. Y. Mar 60.
9p. Order from LC Mi. $1.80 Ph. $1.80.
BNL-4689
Physics and AAathematics
I
Table of electron wave functions at the nuclear
surface, by C. P. Bhalla and M. B. Rose.
Oak Ridge National Lab. , Oak Ridge, Tenn.
[nd] Contract W-7405-eng-26. 203p. Order from
OTS. $3.00. ORNL-2954
Ml hie
for the period ending June 30, 1959. Nuclear
Metals, Inc. , Concord, Mass. Jul 60. Contract
AT(30-I)-1565i. 156p. Order from OTS. $2.75.
NMI-12i6
128
ae problem with capture, by S. N. Purohlt. Oak
Ridge National Lab. Oai Ridge, Tenn. [nd]
Contract W-7405-eng-26. 28p. Order from OTS.
75 cents. ORNL-3005
Total cross sections for negative pions on protona
« 230, 290. 370. WaSdiamey. by]. C. "
carls and others. Univ. of Calif. Lawrence
Radiation Lab. , Berkeley. Calif. Jun 60.
Contraa W-7405-eng-48. i9p. Order from OTS.
50 centa. UCRL-9278
Progress Reports
i—ial technical progress report AEC unclassified
^^^^^Qgrams fiscal year I960. Atomics Intemational,
HvT, North American Aviation, Inc. , Canoga
Park CaUf. Aug 60. Contraa AT(ll-l)-GEN-8.
3«7p. Order from OTS. $5.50. NAA-SR-5350
Articles published in technical Journals, reports
- — [Mued, papers preseiited at scientific meetlngB,
theses completed, and Inventlotis disclosed
aiHngT959 by ORNL staff nMimbers. Oak Ridge
National Lab. , Oak Ridge, Tenn. ind] 84p. Order
from OTS. $2. 25. ORNL 60-6-49
Pittsburgh 30, Penna. Jul 60. Contract AT -(30-3)
-500. 49p. Order from OTS. $1.25. WCAP-1596
Radiation EfFects on Materials
Mar. 60. Contract W-31-109-Eng-52. 50p.
Order from LC. Ml. $3.00 Ph. $6.30.
lCAPL-1305
Energy required for atomic displacements in graphite
detemrtlned by electron bonxpardment, by D. T. &
Bggen. North American Aviation, Inc. , Lod
Angeles, CaUf. Apr 50. Decl. Oct 59. 20p.
Order from LC. Ml. $2. 40 Ph. $3. 30.
NAA-SR-69
Three-minute irradiation at variable power density
of prototype cetr fuel pellets, by L. M. Ferris
and others. Oak Ridge National Lab. , Oak Ridge,
Tenn. [nd] Contract W-7405-eng-26. 9p. Order
from OTS. 50 cents. ORNL-2999
Radioactive Waste
■Wayte disposal in salt: I. the HNOS-NaCl reaction.
~ by H. Kubota and T. Tamura. Oak Ridge National
Lab. , Oak Ridge, Tenn. [nd] Contract W-7405-
eng-26. Order from OHTS. 50 cents.
ORNL-2984
Winchester laboratory quarterly rcpo^'^' April I, 1960,
June 30, 1960. National Lead Company. Inc. ,
H
The determination of teotoptc radium, by B. J.
Baratta and A. C. Harrington. National Lead
Co., Inc. Winchester, Mass. Sep 60. Contraa
AT(49-6)-924. 26p. Order from OTS. 50 cents.
WIN-118
Reactors — General
Reaaor Safety, A literature search, compiled by,
Richard J. Smith. Office of Technical Information
Information, Oak Ridge, Tenn. Sep 60. 70p.
Order from OTS. $1.75. TID-3525(Rev. 2)
Fast fuel test reactor -FFTR conceptual design
study, by R. Brubaker and others. Argoime
National Lab. , Argonne, IlUnols. Aug 60.
Contract W-31- 109 -eng-38. lOlp. Order from
OTS. $2.25 ANL-6194
HFIR preUminary physics report, by R. D.
Cheverton. (jiak Ridge National Lab. , Oak
Ridge, Tenn. [nd] Contraa W-7405-eng-26.
nop. Order from OTS. $2. 50 ORNL-3006
Reactors — Power
Heavy-water-moderated power reaaors engineering
and economic evaluations, volume 1 -summary
report, by E. 1. du Pont de Nemours Bl Co.
Bn^iieering Dept-Design Dlv. E. I. du font de
Nemours k Co. , Wilmington, Delaware. Jun 60.
Contraa AT(07-2)-l. 119p. Order from OTS.
$2.50. DP-510
Background information for selealon of beryllia as
moderator for the marltlnxe gas-cooled reaaor,
by MGCR Program Staff. General Dynamics
Corp. Apr 60. Contract AT(04-3)-l87. 27p.
Order from OTS. $1.00. GA-1280
Transportability studies, ML-1 nuclear power plant,
by J. W. Blakley and others. Aerojet -General
Nucleonics, San Ramon, Calif. Apr 60.
Contract AT( 10-1) -380. 266p. Order from OTS.
$3.50. IDO- 28555
Stable Isotope Separation
Development of krypton -85 static elimination
equipment. Quarterly progress report no. I for
jgPlSrPeceinber 1, 1^58 to February 28. 1959.
by P. Palmerl, Jr. , and others. United States
Radium Corp. , Bloomsburg, Pa. Apr 59. Contra
Contraa AT( 30-1) -2306. 30p. Order from LC.
Mi. $2. 70 Ph. $4. 80. AECU-4362
nchester, Mass. Aug 60. Contract AT(49-6)
-924. 35p. Order from OTS. 75 cents.
WIN-117
Recovery of degraded -heavy water at the savannan
river plant, by W. C. Scotten and others. E. J.
du Pom de Nemours k Co. Savannah River Lab. ,
129
Aiken, S. Car. Jul 60. Contraa ATX07-2)-l.
2^. Order from OTS. $1.75. DP-470
B.
Computer techniques tor radtoaCTlvtlon arulyla,
Annual report, by W. E. Kuykendall and R.
Waineridi. Texas Engineering Experiment
Station, College Station, Texas. May 60.
Contract AT -(40-1) -2565. 200p. Order tmm
OTS. $(2.50. ORO-307
fachnoiogy — Feed Materials
Process enjgineering report on production of tnorlum
M Iowa state coUem, by H. H. Bulkowski and o
others. Catalytic Construction Co. , Philadelphia,
Pa. Jan 52. Decl. Mar 60. 72p. Order from UZ.
Ml. $4.50 Ph. $12.30. CCCO-400
Conversion of UO
and electrolysis,
2 to UP4 by ion exc
rtcrly report- "
1953. 6ak
10. lW2-PAruary 10, 1953. 6ak Ridge
National Lab. , Oak Ridge, Tenn. Feb S
19p. Order from OTS.
53.
30 cents.
CP-53-2-255
The problems, nsture, and control of the orgmc
contamination of refinery liquors, by W.'CT^
Bradford and others. MaUlnckrodt Chemical
Works, St. Louis. Missouri. Mar 57. 32p.
Order from OTS. 75 cents.
MCW-1394
ISO
SOURCE INDEX
Source
Aerojet -General Corp.,
Azusa, Calif.
Page
Aeronautical Chart and Inform-
ation Center, St. Louis, Mo. 29
Aeronautical Engine Lab. ,
Naval Center, Philadelphia.
Pa. 1 'f
Aeronautical Materials Lab. ,
Iteval Air Material Center,
PhiUdelphia, Pa.
Aerospace Medical Div. ,
Wright Air Development Div. ,
Wright- Patterson AFB, Ohio
Air Force Cambridge Research
Center, Bedford, Mass.
Air Force Flight Test Center,
Edwards AFB. CaUf.
Air Force Missile Envelopment
Center. Holioman AFB,
N. Mex.
36
102
57
68
119
36
70
7
84
I
Air Proving Ground Center,
Elgin AFB, PU. , ;,
'I
Airborne Instruments Lab.
Melville, N. Y. 1 v
Mineola, N. Y. | jj
Allied Research Assoclues, Inc. ,
Boston, Mass.
97
41
57
84
American Brake Shoe Co. ,
Mahwah. N. J.
I '1,
American Inst, for Research.
Pittsburgh. Pa.
6
41
American Inst, for Research,
Washington. D. C. 6
Antenna Lab. . Ohio State U. Re-
search Foundation, Columbus 41
PB Number
152 055
171067
35 152 641
94 150 877
152 300
171 053
171 087
171 119
152 200
150 412
152 616
152 296
152 297
150 372
152 802-1
152 802-2
150 371
57 152 361
171 095
150 681
152 122
150 634
91 171 065
171 075
150 160
152 136
150 740
Source
P»ge
FB Number
pplied Mathematics and
Sutistics Labs.
, Stanford U.
,
Calif.
7
152 178
75
152 175
76
162 053
5t>> >•
152 176
152 177
Applied Mechanics Lab. , Mass.
Iftst. ol Tech. . Cambridgie 94
Applied Physics Lab. , Johns
Hopkins U. . Silver Spring.
Md. 103
Applied Psychological Services,
Wayne, Pa. 6
Arctic Aeromedical Lab. ,
LaddAFB, Alaska 12
13
16
18
63
Armed Services Technical
Information Agency, Arlington.
Armour Research Foundation.
Chicago, 111.
41
69
92
Army Chemical Corps Engineer-
ing Command, Army Chemical
Center. Md. 80
Army Chemical Research and
Development Labs., Army
Chemical Center, Md.
I-l
171099
150 872
152 142
152 028
152 029
152 030
150 218
152 031
152 033
147 745
150 577
150 578
147 476
150 214
150 229
150 566
150 576
152 032
150 571
171 106
152 140
171057
171056
150 992
13
152 001
152 002
19
152 003
20
150 665
39
150 101
150 663
57
150 664
84
150 100
97
152 000
99
171 124
Source
Fige PB Number ^ ,» Source
Page PB Number
Army Eaglneer Reseercfa and
Development Lab*., Port
Belvoir, V».
Army Engineer Waterways Ex-
periment Sitatioa. Vicksburg,
Mlas.
101 152 650
40
67
Army Ordbance Corps. ,
Waahingtoi^. D. C.
Army Ordnance Human Engineer-
ing Labs. , Aberdeen Proving
Army Tranasorution Research
Command. iPort Eustis. Va. 36
Arnold Engineering Development^
Center, Tullaboma, Tenn. 36
85
36
85
63
64
114
117
ARO. Inc.. Tullaboma. Tenn.
Avco-Bvereti Research Lab. ,
Mass.
iMecic
Aviation Kiedcal Acceleratioa
Lab. . Naval Air Development
Center, Johosville, Pit. 13
14
16
36
BalUatlc Research Labs. ,
Aberdeen Proviog Ground. Md. 34
42
150 436
171 098
152 073
70 152 354
Ground. Ki
d.
58
150 733
Army Research and Development
Lab. , Fort Monmouth. N. J.
34
150 452
Army Signal Research and
Developmei
lit Lab..
Fort
Monmouth,
N. J.
2
29
30
34
41
42
56
150 451
152 193
152 195
152 189
152 191
152 188
1S2 192
152 194
150 664
69
101
104
109
152 805
150 667
152 190
150 666
152 752
150 985
152 647
171 104
150 985
152 647
171 104
150 964
150 777
152 678
150 955
150 442
150 439
150 440
150 441
148 274
150 417
150 596
Ballistic Research Labs. ,
Aberdeen Proving Ground,
Md. (coo.)
I ■' T
Battelle Memorial Inst. ,
Columbus, Ohio '^
-it
Baylor U. Coll. at Medicine,
Houston. Tbx.
Behavioral Sciences Lab. ,
Wright Air Devel(^?ment Dlv.
Wright -Patterson AFB, Ohio
0
Bell Aerosystema Co. .
Buffalo. N. Y.
Bell Telephone Labs.. Inc..
New York ,
58
1
99
121
-.■^,
105
21
76
64
43
109
150 329
150 454
150 957
150 959
148 647
150 418
171 030
150 424
152 640
171078
152 039
152 657
150 660
Biomedical Lab. , Wright Air
Development Div. , W right -
Patterson AFB, Ohio
Bolt. Beranek and Newman, Inc. ,
Cambridge, Mass.
19 171 073
37
119
Boston U. , Mass. t
Bright Star Industries,
Clifton, N. J.
Brookhaven National Lab.,
171 076
150 879
152 103
43 150 804
Upton. N. Y.
24
150 538
Brooklyn Coll. , N. Y.
19
150 561
Brown U. , Providence, R. 1.
25
150 858
Brown U. Div. of Applied Mathe-
matics, Providence, R. I.
Brown U. Div. oi Engineering,
Providence, R. I.
Brush Beryllium Co. , Cleveland,
Ohio
BufEak) U. School of Medicine,
N. Y.
Bureau at Naval Personnel.
Washington. D. C.
88 150 528
63
90
117
119
150 866
152 170
150 474
152 059
66
69
152 197
171061
19
150 788
97
152 233
1-2
Source li*
Bureau at Ships, '
Washington, D. C.
lureau of Yards and Docks,
Waahington. D. C.
Cam 0. (France)
Olifomia Inat. of Tech. ,
Pfeaadena
California U. , Berkeley
Galifornla U. , Los Angeiet
California U. , Los Angelet.
School of Medicine
Page PB Number
30
90
101
77
Carborundum Co. , Niagara
Falls, N. Y.
'-Ill
Carnegie Inst, of Tech. ,
Pittsburgh, Pa.
Carnegie Inst, of Tech. .
Graduate School of Industrial
Administration, nttsburgh,
Pa.
Carter Observatory
(New Zealand)
77
105
7
6
102
109
li
69
105
78
2
Case Inst, of Tech. , Cleveland,
Ohio 1
43
106
Oualysis Research Labs. .
Alfred. U., N. Y.
Center for Documentation and
Communication Research,
Western Reserve U. , Cleve-
.land, Ohio
CMiter for Radiophysics and
Space Research, Cornell, U. ,
Ithaca, N. Y.
(Centre de Physique Electronique
St Corpusculaire (Prance) 43
Centro di Studio per la Pisica
delle Microonde (luly)
106
Centro Radioelettrico Speri-
menule "G. Marconi", Rome,
luly 119
Chicago Midway LAbs. , U. of
Chicago, III. 39
152 273
152 661
171091
ISO 863
14 150 854
152 106
150 880
150 498
152 104
152 299
152 144
150 216
171061
150 526
150 482
150 941
150 942
150 648
152 077
24 150 515
123 171 123
149 007
152 092
150 415
150 650
171054
Source
Coating and Chemical Lab. ,
Aberdeen Proving Ground,
Page FP Number
24 150 089
Colorado U.
BouUer
11
150 527
*^.
76
152 071
Colimihia U.
• -
, picw
York
76
148 063
150 522
77
150 521
152 100
152 106
107
150 429
150 430
•
A
106
150 431
150 432
CoIumbU U.
School of
Engineering, New York
lOS
152 124
Compagnie de Recfaerches et
d'Etudes AerooauHques
(Prance)
Compuution Lab. , Harvard U.
Cambridge, Maes.
Connecticut U. , Scorrs
Convalr, Fort Worth, Tex.
Convalr, Ponaona, Calif.
Cornell Aeronautical Lab. ,
Inc., Buffalo, N. Y.
Cornell U. , Idiaca. N. Y.
Cornell U. Graduate School of
Aeronautical Engineering.
Ithaca, N. Y.
Cornell U. School of Electrical
Engineering. Ithaca. N.Y. 43
Cruft Lab. , Harvard U. ,
Cambridge, Mass.
Cryogenic Engineering Lab. ,
Boulder, Colo.
i>
Curtis-Wright Corp. , Oaldwell,
N. J.
David SamoCf Research Center,
Princeton, N. J.
1-3
150 366
SO
148 259
23
150 407
100
1(U
152 356
152 359
152 806
118
150 738
80
81
85
171 093'
171 092
150 531
38
110
148 870
152 036
85
150 620
150 621
43
150 817
4S
150 552
56
161 093-5
90
95
171060
171064
43
44
150 815
150 813
150 814
Source
David SuTDolf Research Center.
Princeton. N. J. (con.)
David Taylor Model Beain.
Waahingtoi, D. C.
Davidson Lap. , Stevens Inst,
of Tech. ,
Hoboken, N. J.
Defense Meoals Iifonnation
Center, Banelle Memorial
Inst., Colilmbus. Ohio
m
n Number
Source 1
Page FBNumbtr
1
Electrical Engineering Re-
44
150 816
search Ub. , U. of Illinoia,
150 963
Urhana
46
152 131
81
152 045
Electrical Engineering Reaearcb
Lab., U. of Texaa, Austin
81
150 649
62
150 459
152 797
Electro-Mechanics Co. ,
I ^
152 807
Austin, Tex.
105
150 927
88
150 737
Electron Tube and Microwave
Lab.. Calif. Inst, of Tech..
64
152 130
Electronic Tech. Lab. , Wright
Air Development Div. , Wright-
115
150 447
■
66
151095
Patterson APB, Ohio
46
152 360
70
161 215
171 118
92
151096
■'■•'■ ,
161 218
Electronics Kesearch I^. ,
1
1 .
93
161 216
Nortlieastern U. , Boston,
1
\
Mass.
34
148 257
Denver Veterans Administration
Hosplul, Colo.
Daimond Ordnance Fuze Labs. ,
WashingtoQ, O. C.
20 150 207
Dielectrics \Mb. , Johns Hopidns
U., Baltimore, Md.
Digittl Computer Lab. , Mass.
Inst, of TecA. , Cambridge
Digiul Computer Lab. , U. of
Illinoia, Ufbana
Duke U. , Durham. N. C.
Durham
U. dSt. Brit.)
Dynamic Detelopments, lac ,
Babylon, N. Y.
Edinburgh U (Gt. Brit.)
Educational Research Corp. ,
Cambridge, Mass.
Electric Storage Battery Co. ,
West Oran^, N. J.
37
152 313
152 315
44
152 311
45
152 309
152 314
150 318
171026
58
149 547
86
152 312
110
152 310
45
150 806
45
150 754
77
152 109
77
152 066
152 067
118
152 066
30
150 929
96
150 937
88
150 478
150 479
23
171 122
5
171053
45
152 187
Electronics Research Lab. ,
Northeastern U. , Evaniaton,
Ui.
ElectrtMilcs Research Lab. ,
U. of California, Berkeley
46
47
108
Engineering Dlv., Air Material
Command, Wright -Patterson
APB, Ohio 103
Esses Electronics, Berkeley
Heights, N. J.
Faculte des Sciences,
Orsay, France
Pairchild Kinetics Dlv. ,
Pair child Engine and Airplane
Corp, New York
Federal Aviation Agpency,
Atlantic City. N. J.
Pels Group Dynamica Center,
U. of Delaware, Newark
Feltman Research Labs. ,
Picatixuiy Arsenal, Dover,
N. J.
47
100
75
37
8
59
60
66
70
150 645
146 750
150 511
152 115
150 374
152 298
150 679
150 349
171 096
171094 f
150 472
148 662
148 914
148 916
149 960
150 825
150 970
148 225
161 863
152 351
1-4
Source F
Plight Control Lab. , Wright
Air Development Div. , Wrl^-
PtoersoDAFB, Ohio
Plight Safety Foundation, Inc. ,
Rioenlx. Ariz.
Pood and Drug Research Labs. ,
inc.. New York
Pranklin Inst, for Research -
and Development, Philadelphia,
H.
Prick Chemical Lab. ,
Princeton U. . N. J.
Pritz Engineering Lab. ,
LofaigbU. , Bethlehem, Pa.
Qm Dynamics Lab., Princeton
U., N. J.
General Applied Science Labs. ,
Inc., Westbury, N. Y.
General Electric Co.,
Ovenaboro, Ky. I j
General Electric Co.
Schenectady, N. Y.
General Electric Co. ,
Syracuse, N. Y.
Geo|riiyaical Inst. . U. of
Alaska, College
tkrris Research Labs. , j
l^ahlngton, D. C |
HuvardColI. Observatory,
Cunbridge. Mass.
Hermea Electronics Co. ,
Cambridge. Mass.
Hl|h Altitude Observatory,
kukler, Colo.
ttUv Aircraft Corp. , Palo
Alio, Calif.
Page
FB Number
37
171 116
38
148 870
21
150 671
95
150 850
25
150 858^
83
152143
28
150 170
86
148 669
47
171 117
47
106
152 667
148 254
2
105
Glbfaa and Cox. Inc. , New York 89
73
2
Heat Transfer Lab. . Mass.
hat. of Tech. , Cambridge 32
81
105
^kiuon Sciences Rei
Arhsfton, V«.
eh. Inc.,
121
ISO 805
150 573
150 932
152 416
150 548
150 741
150 444
150 445
150 484
1S0 9S2
150 783
150 836
1S0 8S7
150 838
Source
Human Sciencea Research,
Inc., Arlington, Va. (con.)
Hydraulic Engineering Lab. , U.
at California, Berl^eley
UIlDols Inst, of Tech. , Chicago 93
Illinois U. . Urbana
Illinois U. Coll. of Medicine,
Chicago
Inqwrial Coll. of Science and
Tech. , London (Gt. Brit. )
Institute fbr Applied Experimen-
tal Psychology, Tufts U. ,
Medford, Mass.
Page
FB Number
121
150 839
152 146
32
152 645
93
150 470
8
60
77
110
150 490
150 830
150 831
150 883
150 543
150 544
16
17
150 565
150 570
30 150 420
8
14
122
Institute for Fluid Dynamics
and Applied Mathematics,
U. of Maryland. College Park 77
86
Institute for Systems Research.
U. of Chicago, Ul. 81
Institute for die Study of Metals,
U. of Chicago. UI. 95
Institute of Engineering Re-
search. U. of Califomla.
Berkeley
Institute of Flight Structures,
Colombia U. , New York
i83
89
118
Institute ofMarhematlcal
Sciences, Ne^i^YoclK^J. . N. Y. 100
Institute of Meuls and fi^qujo-
slves Research. U. of Utth»
Salt Lake Qty 60^
\
Inatltute of Rubber Research,
U. of Akron, Ohio 75
Institute of Tech. , U. of
Mlnnesou. Minneapolis 110
152 107
152 138
150 495
150 641
152 047
152 173
171080
150 467
150 466
150 524
150 540
150 762
78 150 993
150 944
150 945
150 747
tN491
ISO SOI
J
• I
1-5
Source
Institute df Transportation and
Traffic Engineering, U. of
California, Berkeley
Instituto (te Quimica Pisica
(Spain)
International Inat. , of Meteor-
ology. (J. at Stockholm
Sweden
Ionosphere Research Lab. ,
Pennsylvtaaia Sute U. . Univer-
sity Pari
Iowa Inst, of 'Hydraulic Re-
search, jlowa City
Iowa Stat^ U. , Iowa City
Page PB Number
Iowa Statei U. of Science and
Tech., Ames
Israel Ins^. at Applied Social
Researc|i
ITT Labs i, Nutley, N. J.
]. G. Engineering Research
Associates, BaltinKire, Md.
James Forrestal Research
Center, iPrinceton, N. ].
Jefferson Davis Hospital,
. Houston] Tex.
John CarxloII U. , Cleveland.
Olio I
Johns Hoficins U. , Baltimore,
Md.
Kansas Soate U. , Manhattan
Kansas (J., Lawrence
Kansas U, School of Pharmacy,
Lawrence
Karolinslqa Institutet,
Stockholm (Sweden)
Kellogg R3diation Lab. , Calif,
of Tech. , Pasadena
Kentucky Research Foundation,
Lexington
38
25
30
31
31
U9
2
3
97
48
110
1-
171068
150 334
148 262
150 930
148 263
148 256
150 669
86 152 099
150 517
152 057
150 518
25 150 458
8 150 361
150 678
150 547
90 150 480
64
152 153
152 155
21
152 640
94
152 151
78
150 646
108
150 096
19
150 856
8
152 098
12
148 269
99
150 473
111
150 784
Souros
Laboratorio di Elettrochimica,
Chimica Pisica e Metallurgla
del Politecnico di Milano
(Italy)
Laboratorio di Meccanica Ap-
plicau del Politecnico di
Torino (Italy)
Laboratory for Electronlcfi
Inc., Boston, Mass.
Laboratory for Insulation Re-
search, Mass. Inst, of Tech.,
Cambridge.
Laboratory of Astrophysics
and Physical Meteorology,
Johns Hopkins U. , Baltimore,
Md.
Laboratory of Atomic and
Solid Sute Physics, Cornell
U., Itfiaca, N. Y.
Laboratory of Climatology,
Centerton, N. J.
Land Locomotion Lab. , Ord-
nance Tank -Automotive Com-
mand, Center Line, Mich.
Lichtkllmadsdies Observatori-
um Aroea (Switzerland)
Liege U. (Belgium)
Page FBNunhi
25 171079
I
86 1%34«
87 150 347
81 149 S93
111 150 541
3 152054
109 150 628
25
1
31
34
3
Lincoln Lab., Mass. Inst, at
Tech., Lexington
48
49
50
60
1-6
152 OM
150 614
1S0 61S
150 616
150 617
67 150 999
152 056
150 931
150 939
150 940
150 943
150 926
150 369
150794
150 975
150 594
1S0 6GI
150796
152 041
152 295
148 361
150 431
ISO 592
150 593
150 515
150 597
150 60)
149 778
150 601
150 79*
Source
Lincoln Lab.. Mass. iQSt. of
fedi. , Lexington (con. )
>i
Uttfc, Arthur D., Inc.^
Canibrldge, Mass.
Lockheed Aircraft Corp. ,
Sunnyvale, Calif.
Page FB Number
Ti 147588
150 509
150 600
150 951
82 150 506
150 598
150 599
171 100
87 150 606
HI 150 603
150 673
150 757
119 150 507
120 150 610
K.':
«M
.H
Louisiana State U. , BatDO
Rouge
u .
McCrone, Walter C. , i
Associates, Chicago, DI.
•
Mallory, P. R. , and Co. , Inc.
Indianapolis, lad.
MancheaierU. (Gt. BrU.)
23
72
50
61
65
69
71
93
HI
9
26
Manufacturing Labs. , Inc. ,
Cambridge, Mass.
Marine Lab. , U. of Miami.
Coral Gables, Pla.
Marine Physical Lab. , Scripps
Institution of Oceanography,
San Diego. CfUf.
Source ?•
Maryland U. , College Park
^ ' • '"
ill
Page n Number
98 152 058-1
152 058-2
115 150 556
150 557
150 891
150 969
Massachus«jtts Inst, of Tech. ,
Cambridge
171 097
150 282
152 026
171 127
150 886
150 613-1
150 613-2
171 101
152 027
171 088
150 666
150 542
150 870
: .V Id :.v
20
26
29
87
89
9S
112
118
J.
Massadiusetts U. , Amherst
Materials Research Lab. ,
Watertown Arsenal. Mass.
Melobslnc, Palo Alto, Calif.
Melpar, Inc., Watertown,
Mass. I '*■ i
112
51
152 096
152 095
150 862
152 357
152 356
150 850
150 855
148 918
150 486
150 532
150 503
150 504
148 830
148 917
148 918
148 919
150 683
150 736
61 152 062
Metals and Ceramics Lab. ,
Wright Air Develq>ment Div. .
Wright- Patterson AFB, Ohio
61 150 989
92 : 171 077
Metals Research.
Ud.
51
150 809
(Gt. Brit.)
105
150 644
150 810
■■'
Meals Research Lab.,
-tG-x re
4
150 933
Carnegie Inst, of Tech. ,
150 934
Pittsburgh, Pa.
26
152 089
150 935
150 936
Michigan U. , Ann Arbor
20
150 488
■
67
150 998
95
171066
Michigan U. Coll. of Engineer-
ing. Ann Arbor
96
150 637
39
150 769
Michigan U. Research Inst.
66
150 954
Ann Aibor
40
152 355
74
150 768
51
171 105
"
150 770
150 771
Microwave Associatea, Inc. .
150 772
Burlington, Maas.
S2
150 448
150 773
150 774
Microwave Research Inst. ,
150 775
Polytechnic Inst
of Brooklyn,
N. y.
52
150 875
Milan U. (luly)
26
150 336
loe
152 676
1-7
Source ; Page FB Number
MianeapoUs-Htaeywell Regular-
tor Co., St. Ptetersburg. Fla. 52 150 931
MinneMXa U. , 'Minneapolis
Miaoesota U. ^cbool of Veterin-
ary Medicine] St. Paul 21 150 569
Moore School <k Electrical
Engineering \jf. at Pennsylvania
Philadelphia , 82 152 651
4
148 260
38
171 090
78
152 106
152 289
83
171070
171071
96
171064
112
150 633
Motorola. Inc., Riverside,
Calif.
Naples U. Cta
ronBL
38 152 350
115
120
National Aeronautics and Space
Administration, Washington,
D. C.
I
National Aviatibn Facilities ^
Experimental' Center, Atlantic
City, N. J.
38
39
National Bureaa of Standards,
Boulder, Cok .
National Burea i
Washington.
S2
120
of Standards,
I. C.
National Instiniws of Healdi,
Betfaesda, Md,
I
National Inst. ^ Oceanography
(Ct. Brit.) I
National Research Council,
Washington, ^.C.
Naval Engineering Experiment
Sution. Anna|)oIis, Md.
Naval Ordnanc4 Lab. ,
CoroM, Calii.
23
26
82
102
106
112
22
34
73
67
61
122
150 556
150 928
36 148 274
171 028
171 040
161 578
151 377-3
151 377-4
151 377-5
161 573
161 571
161 574
161 565
161 575
161 576
161 568
152 855
150 529
150 962
152 642
171 114
152 035
Source
Naval Ordnance Lab.,
White Oak, Md.
Page P6 Number
Naval Ordnance Test Sution,
China Lake, Calif.
Naval Radiological Defense Lab.
Sao Francisco, Calif.
Naval Research Lab. ,
Washington, D. C.
Ki-'ptH
(X
31
39
61
71
99
102
52
71
91
92
96
104
123
150 867
152 352
150 456
150 390
152 677
152 644
152 646
146 395
149 849
146 402
161 921
161 696
161 767
161764
161749
147 832
161 288
Naval Supersonic Lab., Mass.
Inst, of Tech. . Cambridge
Naval Supply Research and
Development Facility,
Bayonne, N. J.
Naval Weapons Lab. , Dahlgren,
Va.
Navy Electronics Lab. ,
San Diego. Calif.
New Yort State Coll. of
Ceramics, Alfred U.
New York U. , N. Y.
115 147 780-4
I
103
i
61
65
32
S3
150 778
150 626
150 972
152 643
152 615
113 150 537
10
93
113
New York U. Coll. of Engineer-
ing. N. .Y.
Nonmeullic Materials Lab. ,
Wright Air Development Dlv. ,
Wright-Patterson AFB, Ohio
North Carolina Sute Coll. .
Raleigh
Northwestern Technological
Inst., Evanston, 111. ^,^ ^^
31
53
150 639
171 082
150 443
150 437
ISO 764
•oviwu-it
71
72
171 055
171 063
19 150 560
78
79
122
150 482
148 199
150 481
148 197
1-8
Source
(jortfawestern U. , Evanston,
Itt.
Page PB Number
*•. it-:
liiactoar Meuls, Inc. .
Concord, Mass. .
ir^.
27
79
96
OIBoe of Defense Research and
Bagineering. Washington, D. C. 72
Office of Naval Research,
Washington, D. C.
Office of Technical Services,
Dqjit.d Commerce,
Washington, D. C.
53
23
27
53
91
116
CUo State U. Research Founda-
doo, Columbus i i.,, j
Oklahoma State U. Research
Foundation, Stillwater
Oklahoma U. Research Inst. ,
Norman
OUb Madiieson Chemical Coq;>.
Nmt Haven, Coon.
Orefon U. Medical School.
Portland
10
27
113
122
35
20
69
14
17
FiCiflc Science Board. National
RMeai-ch Council, Washington.
D. C. 12
Pldflc Semiconductors, Inc. ,
QdvcrCity, Calif. 113
hrlsU. (France) 62
Parker Aircraft Co. , Los
Angeles, CaUf. 72
Pfeasrson, MoosDiv., Universal
Winding Co. , Jamlca. N. Y. 53
fNasylvania State U. Coll.' of
QKmistry and Physics,
Uoiversiiy Park
I hi
taasylvania State U. .
Ihhwrsity Park
24
27
150 536
152 126
150 652
171 063
171 115
161890
OTS SB- 421
OTS SB-422
OTS SB-425
OTS SB -428
OTS SB-424
OTSSB-426
150 859
150 755
152 185
152 172
150 873
150 574
171 039
147 744
150 564
147 100
150 811
150 812
150 647
150 282
150 843
150 538
150 539
S3 171 059
Source
Pennsylvania U. School ai
Medicine, Philadelphia
Page fB Number
14
IS
Pennsylvania U. School of
MeuUurgical Engineering,
Philadelphia
Physical Research Lab. , Space
Tech. Labs., Inc., Los
Angeles, Calif.
Physics, Engineering, Chemistry
Corp., Boulder, Colo. 21
Physics Lab. , Wright Air Devel-
opment Div., Wright -Patterson
AFB, Ohio
Pittsburgh U. , Pa.
Plasma Propulsion Lab. ,
Republic Aviation Corp.,
Farmingdale, N. Y.
Plastics Technical Evaluation
Center, Picatinny Arsenal,
Dover, N. J.
39
100
Psychometric Lab. , U. of North
Carolina, Chapel Hill 103
Psychological Lab., U. of
Southern California, Los
Angeles 6
Psychological Labs. , Carnegie
Inst, of Tech. . Pittsburgh, Pa. 11
Psychological Research Associ-
ates, Inc. , Arlington. Va. 7
PubUc Healdi Service,
Washington, D. C. |
Purdue Research Foundation,
Lafayette, Ind.
Quantum, Inc. , Wallingford,
22
1-9
150 566
150 572
114 150 651
65
150 882
96
150 776
116
152 113
116
150 890
171 072
171 054
150 523
116 147 838
75 161 947
Polytechnic Inst, of Brooklyn,
N. Y.
83
150 416
. ..^ ^ ._
87
152 139
150 892
150 483
1S2 1U,
152 123
161 371-7
161 371-6
120 150 874
Conn.
97
152 646
1
152 649
Quartermaster Research and
Engineering Center, Natick,
Mass.
5
146 319
31
150 765
Ohio
•
-
152 070
N,
tl'l!
'i.B
/
,/
' Souro^
Quartemiiiflter Research and
Engineering Center, Natlck,
Mass.
o^
)
Radio Cotp. al America,
Camden, N. J.
Radio Corp. of America,
Harrison, N. J.
Radio Corp. of America,
Lancaster, Pa.
Radiobioitigical Lab. , U. of
Texaa, , Austin.
Ray-0-V«c Co., Madison, Wis.
Raytheon Co., Waltham, Mass.
RCA Defense Electronic
Product^, Camden, N. ].
Remingtoi Rand Univac Div. ,
Sperry Raod Corp. Philadel-
phia, Pa.
Rensselaer E*olytechnic Inst. ,
Troy. H Y.
Page
FBNimiber
*^ Source I
'age
^■H
Royal Inst, of Tech. (Sweden)
28
■
—
t9
32
150 766
73
150 548
Rutgers Sute U. , f4ew Bruns-
150 962
wick. N. J.
10
171062
*
92
171089
• •
•'■
103
150 748
Rutgers State U. School of .
Chemistry, hiew Brunswick.
N. J. • ^
24
54
171 126
'
St. Luke's Convalescent Hospital
1
Greenwich, Conn.
17
54
152 753
St. I.4ike's Hospital,
1
New York
17
54
149 707
i
Sanitary Engineering Research
<n
Lab. , U. of California.
22
152 353
f Berkeley • '
32
54
171 102
Sarah Mellon Scaife Radiation
;I«b,. U. of Pittsburgh, Pa.
101
54
150 446
55 171 125
1. H
Research Center for Group
DynamiQs, U. of Mich. ,
Aon Arbtn-
Research Chemicals. Inc..
Burbank. Calif.
79
82
122
123
89
90
10
94
R— esrcfa ^Lab. of Electronics,
Mms. list, of Tech. , Cam-
brl4ie 55
RioeU.. Houston. Tex. 114
Rock Island Arsenal Lab. , Ql. 75
ila^
Rockeidyiie. Caooga Park,
OtUf.
Rome Air Development Center,
Griffiss AFB, N. Y. 83
Rome U. (Italy)
106
152 049
150 767
150 818
150 819
150 871
150 952
\
150 638
171 085
171 066
148 972
150 749
152 294
152 590
65 150 861
School of Aviation Medicine,
Brooks AFB, Tex. 20
Scripps Institution of Oceanog-
raphy, U. of California, •<*
San Diego S3
Shell Development Co. ,
Emeryville, Calif.
Small Groups Research Center,
Washington U. . St. Louis, Mo. 10
Snell, Poster D. , Inc. .
New York It
Sonocooe Corp. , Blrosford, N. Y. 55
Space Sciences Lab. , Goieral
Electric Co. , Philadelphia, Pa. 5
28
87
108
Speech Research Lab. . U. of
j Michigw. Ann Arbor 104
»J . >-*-
Sperry Gyroscope. Co. .
Great Neck, N. Y.
116
:m«t
Stanford Electronics Labs. .
Stanford U.. Calif. , 55
150 973
ISO 413
? .D
MO in 9J,
56
107
114
MO
150 335
ISO 331
148 2(1
152 411
152 OW
150 471
150471
152 645
ISOSU
149 246
150 207
147 175
72 152 755
ISO 851
150 852
150 871
150 449
ISO 8a
150 179
ISO 802
150 949
150 494
150 629
150 99!
150 491
150 495
152 lis
ISO 823
ISO 820
150 822
ISO SB
Source
Stanford Research Inst.
MenloPark. Calif.
SiaaiiDrdU.. Calif.
Stanford U. Graduate School
of Business. Calif.
Stevens Inst, of Tech. .
Hoboken. N. J.
Seructural Mechanics Research
Ub.. U. of Texas. Austin
Suodstrand Turbo Div. .
Suodstrand Macfaloe Tool Co. ,
Picoima. Calif. |
Sylvania Research Labs. .
Bsyside, N. Y.
Syracuse U. , N. Y.
! I :-
Syracuse U. Researdi bat. .
N. Y.
Technical Research Group.
Syosset, N. Y.
Temple U. , Philadelphia. Pa.
Texaa A. andM. Coll..
College Station
Tnu Nuclear Corp. . Austin
Texas U. , Austin
Tbenn Advanced Research,
Ithaca, N. Y.
Travelers Inaurance Co. ,
Hartford, Conn.
'HAS U. School of Medicine.
Boston. Mass,
TUng-Sol Electric Inc..
Bkxanfield. N. J.
Uhruonics Research Lab. ,
Western Reserve U. .
Cleveland. Ohio
Union Switch and Signal Div. ,
Westinghouse Air Brake Co. ,
Swiasvale, Pie.
Page
PB Number
28
S5
56
150 627
152 152
171 103
148 255
152 614
•8
101
150 853
150 378
67
150 611
150 612
56
149 713
66
150 631
68
66
150 834
148 264
150 835
94
150 280
79
152 292
40 171 031
120
62
33
99
28
79
31
17
107
152 051
150 925
140 487
171 120
152 097
150 466
152 050
147 743
150 450
29 152 132
56 152 796
Source
University Kospiuls,
Iowa City, Iowa
Page PB Number
15 152 118
University of Southern Califor-
nia. Los Angeles 22
24
University of Southern California.
Engineering Center, Los
Angeles 117
*
120
University of Southern Califor-
nia. School of Medicine.
Los Angeles 15
17
Upper Air Lab. . U. of Colorado.
Boulder 35
96
114
11
70
UppsaU U. (Sweden)
Utah U. . Salt Lake Qty
1
Varian Associanes. Relo Alto.
Calif. 56
Veterans Administration Hospiul
Denver. Colo. 20
Virginia U.. Charlottesville. Va. 96
Virginia U. School of Medicine.
Chartocteaville 22
Washington U. St. Louis. Mo. II
Washington U. , St. Louis. Mo.
School of Medicine II
Waahington U. . Seattle
29
33
Washington U. Seattle. CoU. a(
Engineering 57
mshingtonU., Setttle. SdKX>l
of Medicine 17
Watertown Arsenal Labs. , Mass. 62
84
91
Wayne Sute U. . Detroit. Mich. 80
Western Reserve U. , Cleveland,
Ohio 117
Ml
150 562
150 519
150 734
150 968
150 735
150 219
150 563
150 567
150 753
150 351
171 121
150 475
171 074
171069
149 246
150 406
150 575
152 111
152 lOI
150 461
148 267
150 497
150 457
150 230
161800
149 295
150 917
161 989
150 476
150 477
ISO 496
147 906
Source
Wiltow Run liAbs., U. at
Michigan, knn Arbor.
Wisconsin U., Madison
Wisconsin U, School at
Medicine, Madison
Woods Hole Oceanographic
Institution, Mass.
Page
FB Number
Source
Page
PB Number
Woods Hole Oceanograi>hic
35
150 421
Institution. Mass. (con.)
80
90
150 514
150 842
122
152 110
Wyandotte Chemicals Corp. ,
Mich.
74
171058
15
150 215
Yale U. .
1
1
» ■
New Haven, Coon.
7
152 123
33
148 125
104
152 134
34
150 529
t- ^'
-.]
1-12
Subject
Atelian groups
--Theory
Ablation materials
Acceleration
— Fhysiologlcal*fetfects
—Testing equipment
Acceleradcxi tolerance |.
•-Physiological factors
Aa4-52 nMipper
Adrenal cortical extract
--Physiological effects
Adrenolytic drugs
--Physiological effects
Aerial reconnaissance
Aerobee
AerobeeHi
Aerodynamic heating
Aerodynamic noise
Aerosols
—Scattering T
Air
••Radiatioo I
—Radioactivity
— Spectrqgr^>hic analysis
Air blast
--Shielding
Air drop operadoos
•-Equipment j
Air traffic
••Scheduling
Air traffic control systems
--Coding
—Equipment
Aircraft
(.•Equipment
•-Inspection i
—Materials
—Safety measures
Aircraft fires
-•Detection
Aircraft steels
AirfoiU
"Theory
Airframes
•-Materials
Airplane landings
--Equipment
Airplane noise
— Analysis
--Measurement
AirplBie panels
-Vibratian {
Airplanes
--De-icing systems
Alcohols
--Oehydratlao
Algebra
ABcali metals
—Bibliography
SUBJECT IIMDEX
Page PB Number
77
39
14
36
13
48
15
121
35
52
85
86
117
22
117
SS
68
39
39
41
102
100
92
38
38
92
85
92
38
37
37
24
76
152 067
171 054
150 440
148 274
150 442
150 594
14 147 744
150 569
152 146
150 873
150 931
150 621
148 689
39 150 663
150 955
161 371-8
150 955
150 454
150 631
171 040
171040
171095
171 119
152 359
151096
148 870
171028
171 077
150 620
171077
152 350
171076
171076
38 171090
66 150 876
150 638
148 063
23 OTSSB-421
^
Subject
Alkaline batteries
--Design ^
--Production
Alkaline cells
--Design
Alkaline earth compounds
--Bibliography
Alkaline earth meuls
--Bibliography
Alkaloids
--Synthesis
Alpha counters
--Development
Alternating current
- -Detection
Altimeters ^ |
--Design
Aluminum
--Shear stresses
--Stresses
Aluminum oxides
--Mechanical properties
Alums
--Crystal structure
Amino axirids
- -Biochemical effects
Ammonia
--Spectra
Ammonium (wrchloraee
--Combustioo
Amphibian planes
--Control systems
--StablUty
Amplitude modulation
--Mathematical analysis
AnatcMnical nnodels
--Analysis
Anesthetics
--Physiological effecu
Annihiliation reactions
--Analysis
Antenna radiation patterns
--Analysis
- -Determination
•-Mathematical analysis
--Synthesis
--Theory
Antennas
--Design
--Reflectors
--Theory
Antibodies
--Biochemical effects
Antifbuling coatings
--Chemical analysis
--Test results
I-I3
Page FB Number
45
45
152 187
152 187
55 150 449
23 OTSSB-422
23 OTS SB-422
20 152 096
99 150 473
29 152 132
86 152 312
91
90
70
111
\7
3
71
36
36
53
15
15
96
43
106
49
41
43
56
122
52
49
56
106
39
74
161 989
152 170
171 074
150 541
150 471
152 054
152 027
152 296
152 296
171059
152 118
150 215
150 351
150 552
152 676
148 368
150 592
150 740
150 648
152 614
152 035
146 395
148 366
152 614
152 077
16 150 441
150 769
150 768
n
Subject
Aadfouliiig
--Test
co^tinga
resuJts
Page PB Number
(con.)
(con.)
74
Aotiprocona
--Nuclear rdactiona
Aperture fields
Approximate odmputation
--Theory
Area suctioa
--Test results
Argon (Liquid)
--Solvent properties
Arteries i
--Pathology |
Artifical resptratioo
- -Equipment
Astronomical Hata
--Tables
Astronomy
- -InstrumenQatioa
Atmosphere
- -Electromagnetic properties
--Heat transfer
--Light transmission
- -l^teorology *
--Northern hemisphere
Atmospheric electricity
--Measurement
--Meteorological effects
Atmospheric sounding
- - Instrumenoatioa
Atmospherics |
--Theory I
Atomic strucntre
--Matbemati^l analysis
Atoins
--Energy
- -Scattering
Attitudes
- -Measurement
--Psychological factors
- -Sociologic4l factors
--Sutistical fcnalyais
Aurorse
--Clsssificatioa
--RsdUtion '
--Southern hemisphere
i
Autopsies
Aviation accidents
- - Counte rmeas ures
Avlacion persoiioel
--Qothing I
- -Equipment
--Military raqulremenu
--Training devices
Avlatioo safety
96
43
77
79
88
29
15
19
119
35
38
30
30
104
30
35
107
108
112
108
108
10
8
10
10
6
8
2
2
18
102
102
6
5
38
150 770
150 771
150 772
150 773
150 774
150 775
ISO 351
150 648
150 641
152 292
150 366
150 461
150 563
150 788
150 938
150 940
150 507
148 255
152 350
150 930
150 930
152 190
150 929
150 753
150 820
150 945
161 566
150 945
150 945
150 859
152 104
150 851
150 852
152 142
150 361
150 941
150 942
150 517
150 941
150 942
150 214
148 870
171 119
171 119^
171075
171 053
148 870
Subject
Azlmudi
--Determination
Backward wave amplifiers
--Oevelc^nnent
Backward wave oscillators
--Signal -to- noise ratio
Bacteria
--Culture
Ball bearings
-- Materials
Balloons
- -Applications
Barium chromates
--Electrical factors
Barium titanate crysula
- -Electrical properties
Barrier grid tuibe
Batteries
--Design
--Electrodes
Beams
--Bibliography
Beryllium
--Mechanical properties
--Metallurgy
--Processing ^rvk
--Surface properties
Beryllium compounds
- - Production
Bessel functions
--Applications
Bibliography
--Air F^rce personnel
re<piir^ments
--Alkali metals
--Alkaline earth compounds
--Alksline earth metals
--Beams
--Cathode ray tubes
- -Construction
--Cycloidal propeller*
--Electrolytic cells
— Electromagnetic waves
--Explosives
- -Field emission
--Gallium
--Group dynamics
--International Geophysical
Year
--loo emission
--Jet propulsion
--Job analysis •
--Liquid metals
- -Magneto- hydrodynamic
waves
--Metalorganlc compounds
--Molten salts
--Predpltatioa
--Protective construction
--Radiation counters
--Radiation damage
Page PB Number
-Salts
29
56
43
12
90
37
59
69
43
45
45
V
66
93
96
65
66
93
69
77
83
6
23
23
23
83
SO
I
64
'61
119
120
60
106
94
7
34
106
64
6
91
116
23
27
31
1
99
S6
27
171 067
A71 069
150 817
148 269
171 060
152 315
149 960
152 805
152 092
152 314
152 314
83 152 143
152 197
171 088
171 083
ISO 613-2
152 197
171 068
171 061
152 066
150 524
171 075
OTS SB-421
OTS SB-422
OTS SB-422
152 143
171 127
171 106
152 130
171 114
150 507
152 051
150 747
161 576
152 151
150 498
ISO 417
161 576
152 153
171 075
OTS SB-424
OTSSB-426
171 097
OTSSB-425
150 617
171 106
171 124
149 713
OTSSB-425
1-14
Subject '
WbUography (con. )
--Transducers
••Voice communidation
systems
Bioinstnunenution
Biological laboratories
--Equipment
Bircfringement
Bismuth oxides i
--Conductivity i
Bismuth sulfides
-Conductivity
Blast effects
--Measurement
Blood chemistry
--Cllmstic factors
Bodies of revolution
--Boundary layer
••Heat transfer
--Hydrodynamic character-
istics
--Velocity
Body fats
--Determination
Body temperature
••Physiological factors
Bomb debris |
Bonding i
--Theory
Boolean functions i
Borides I
--Crystal structure
Boron
•-Electrical factors
Boron compounds (Organic)
--Bonding
•-CSiemical reactioim
"Polymerization
Boundary layer
--Measurement
•-Turbulence
Brain |
--Physiology
Broadband antennas
— Anslysis
"Design
Brown Bear Cruise
Bumblebee
lutyl rubber
--Applications
Ctdmium crystals
"Growth
Calcite
--Effects of rsdlstion
"Spectra
Calcium sulfate
--Resonance
GtlUscope
Carbohydrates {
--Metabolism
Carbon dioxide
--Physlologicsl effects
Page PB Number '
53 OTS SB-428
122
14
13
89
HI
HI
58
16
86
84
60
60
22
\i
22
101
28
79
114
59
24
24
24
88
89
57
53
33
108
47
110
106
106
25
82
17
21
152 172
150 440
152 033
150 331
150 784
150 784
150 733
150 578
152 099
150 634
150 830
150 831
150 830
150 575
171 103
152 049
171 121
149 960
150 519
150 519
152 087
150 737
150 540
19 171 073
150 457
152 615
148 267
150 872
152 667
152 036
150 374
150 374
152 088
150 598
150 564
150 569
Subject
Carbonium ions
--Exchange reactions
Carboxylic acids
--Synthesis
Cargo
--Transportation
#
Cartridge cases
--Materials
Catalysts
--Effectiveness
Csthode ray tubes
- -Applications
--Bibliography
Cathodes
- -Materials
Cathodes (Electron tubes)
--Materials
- -MeuUurglcal analysis
Ceilometer computer
Cells (Biology)
' --Biochemistry
-'Culture
--Magnetic properties
Cements
--Applications
Centrifugal pumps
- -Performance
Centrifuges
- -Applications
Ceramic coatings
--Ultrasonic analysis
Ceramic materials
--Electrical properties
- -Mechanical properties
Cesium
--Chemical reactions
Cesium bromides
--Conductivity
Chemicsl notatioo
Chemical reactions
--Analysis
- -Theory
Chemical warfare agents
- -Detection
Chemicals '
--Coding
Chemi sorption
Chromatographic analysis
-- Applies tlons
Chromium - coba It - tungs ten
allays
- -Mechanical properties
--Physical properties
Chromium- Iron alloys
- -Oxidation
Chromium -iron -nickel alloys
--Fatigue
-- Tempers ture factors
Chromium plating
- -Effectiveness
--Test results
Circulatory sysienns
- -Stresses
Page PB Number
24
23
67
59
27
3
105
106
54
82
12
19
11
40
63
36
69
69
70
110
123
25
28
123
27
71
93
93
96
90
94
67
150 538
150 407
150 611
150 612
150 825
152 126
150 598
171 127
42 152 040
150 424
148 254
149 707
161 565
148 269
152 003
150 527
171 098
150 834
148 274
171057
152 805
171 074
65 150 861
150 554
171 123
150 334
152 152
99 150 101
171 123
150 536
161 921
)
161 216
161 216
91 161 696
171 064
171 060
150 877
152 642
15 150 563
,>
1-15
Subject
Page FB Number
Clays
-TrafficJBbility
Climate
--Alaska
Clothing
--Acceptability
--Insulution
--MiUtar/ requirements
Cloud beigtit indicators
--Effectiveness
Clouds ;
--Radar analysis
Clutter mapper
Coaxial cables
--Thermal insulation
Cobalt- iro« alloys
--Magnetic properties
Cobalt isotopes (Radioactive)
- -Applications
--Radioactivity
Cockpits I
--Visual factors
Colloids I
--Temperature factors
Colors
--Standands
Combust ioit
--Mathenlatical analysis
--PhysicaJ factors
Combustioii chamber gases
--Analysiis
Combustloit chambers ^
--Design
Comets
--Spectra
--Tbeory
Commerce
--Economic aspects
Communic^lcn systems
--Theory
Complex io^s "^
- - Adsorpdion
--Hydrolysis
Composite materials
Concrete i V
--Reflecti|ve effects
Conical bodies
--Heat transfer
--Hypersonic characteristics
--Pressure distribution
"Reflective effects
--Stressed
Construct! cti
--Bibliography
Containers I
--Corrosion
Continued fractions
--Theory]
Controlled Systems
--Errors
67
31
lOS
\03
73
103
29
29
48
46
105
22
102
37
24
73
64
66
70
66
66
66
3
3
122
46
48
28
28
96
102
117
36
36
120
62
70
76
52
152 073 .
150765 .
•J
150 892
150 748 ..
171 062 ^'
171 089 ^
150 892 '
152 193 ^
152 193
150 594 ^
171 118 '
150 644 I
152 353
161 575
171 094
150 089 ^
171 062
171 089
152 155
148 264
152 351
150 835
150 332
150 332
150 943
150 938
150 940
148 197
150 645
150 796
152 097
150 335
171 083
161 575
150 474
150 985
150 985
150 874
152 807
171 106
161 215
152 071
149 849
Subject
Control systems (con.)
--Reliability i
' •-Synthesis
]■
Copper
--Chemical reactiooa
Copper crystals
--Electron transitions
--Impurities
C<^)per-gold alloys
--Phase studies
Copper wire
--Fracture
Correlation computer
Correlation functions
Corrosion
--Tropical regions
Corundum
--Surface properties
Coset leaders
Cosmic radiation ,
--Detection '■'
--Intensity
- -Measurement
--Physical effects
--Sources
Coupled antennas
--Electromagnetic effects
Crankshafts
--Plating
Cratering
Cryogenics
--Handbooks
Crystal field theory
Crystal rectifiers
--Development
Crystal structure
--Defomvatlon
--Magnetic effects
--Mathematical analysis
Crystals
--Deformation
--Elasticity
--Stresses
Culture
--Sociological factors
CX-48
Cyanogen
- -Spectrographlc analysis
Cycloidal propellers
--Bibliograpjhy
Cyclooctatetraene
--Spectra
Cylinders
--Hydrodynamic character-
istics
Cylinders (Stiffened)
--Stresses
Cylindrical shells
--Deformation
••itf-'ii-
Page
48
53
55
56
25
112
112
93
96
81
49
96
70
78
4
, 97
3
5
5
98
3
97
43
67
58
58
112
43
48
96
112
112
112
114
114
114
10
4
64
107
88
62
84
1-16
'
PBNunte
152 295
150 764
150 493
150 823
150 334
148 830
148 830
150 470
150 637
150 649
150 597
161749
171(J74
150 509
148 260
150 371
152 057
148 258
150 801
150 937
152 057
150 518
150 552
152 642
150 959
161 093-5
161 566
152 657
150 80S
150 468
148 917
148 918
148 919
161 568
150 651
150 651
150 651
150 851
150 944
150 926
152 130
150 429
150 368
152 807
149 295
Subject
Oyllndrical shells (con.)4»
• -Mathematical analysis
--Vibratioa
Page PB Number
Duta
--Processing
Data storage systems
--Development
--Equipment
Dau transmission systems
--Equipment
--Mathematical analysis
--Test methods
--Testing equipment
Decompression chambers
De-icing materials
--Development
De- ionization cross section
Delay elements
--Development
Delay powders
--Combustion
Deminerallzatlon
Denul research i
--Alaska |
Detectors (FM)
--Design
Detergents |
--Solubility
Detonation waves
--Physical effects
Deuterium
--Solubility
Deuterons
--Nuclear reactions
Dielectrics
--Development
Diesel engines
--Vibration
Diet
--Physiological effects
--Theory
Differential equations
--Applications
"Theory
Diffraction gratings
--Errors
Diffusion
--Temperature factors
--Theory
Digestive system
--Physiology
Diodes
--DeveloproeiU
—Theory j
Dipole antennas
--Electromagnetic effects
--Radiation
84
87
87
90
67
122
123
82
81
48
46
49
49
20
68
106
59
59
40
U
53
24
118
29
100
45
90
14
17
83
89
US
118
77
78
109
91
113
28
17
113
43
43
106
149 295
152 139
152 139
150 480
150 611
150 612
150 818
150 819
150 598
149 593
150 594
150 645
150 438
150 438
150 207
150 876
150 949
148 662
148 662
171 031
150 229
150 764
150 089
150 532
150 461
150 349
150 806
152 681
147 744
150 471
171 070
150 871
150 556
150 557
152 068
150 641
150 646
150 628
161 767
152 185
152 152
150 567
150 812
152 657
150 552
152 676
1-17
Subject
Direction finders (RF)
--Development
Documentation
--Coding I
- - Instrumentation
Doppler tracking systems
--Applications
Drag
- -Measurement
Dr(^-
--Velocity
Drugs
--Physiological effects
Dry batteries
--Development
--Test results ;
Dry cells '
--Test results
Ducts
--Aerodynamic character-
istics
Dyes
- -Specifications
Dyaamical systems
Ear
--Physiology
--Pressure distribution
Edema
--Therapy
Elastic shells
--Vibration
Elssticity
--Mathematical analysis
--Theory
Elastomers
--Stresses
--Temperature factors
Electric arcs
--Reduction
Electric batteries
- -Effectiveness
Electric discharge
- -Applications
--Physical factors
Electric fields
--Physical tectors
Electric motors
- -Materials
Electrical potential
--Measurement
Electric prt^Milsion
--Ai^llcations
--Effectiveness
--Equipment
Electric relays
--lAUt ejq>ectancy
Electrical conductance
--Measurement
Electrical double layer
--Theory
Electrical networks
--Mechanical analysis
-Mathematical analysis
Page PB Number
46
123
123
122
62
58
84
8
43
54
54
85
73
83
15
58
19
83
114
83
118
75
75
45
45
4l7
47
105
105
29
64
45
65
45
109
118
26
29
47
55
152 131
150 819
171 123
150 818
150 647
150 454
150 100
152 098
150 804
171 102
171 102
150 531
171 089
171 070
152 118
150 733
150 788
150 524
150 651
171 071
152 068
150 491
150 491
150 754
171 026
150 988
152 667
150 526
150 644
152 132
150 777
171 026
150 861
150 882
150 754
150 686
150 532
150 870
152 132
150 511
152 183
_•■ , -1 ' " . :'
Sublect
! ■
1
1'
Page
PB Number
Sublect
Page
PB Number
Subject
Page
PB Number
Subject •■"■
P«F
PB Number
Ferroelectric crysuls
Frontier settlement
122
152 110
Eleccrocbei
lis try
24
150 515
Electroeutic accelerators
-Aging
--Growth I
1 II 69
152 805
Frostbite
26
150 336
1 —Applications
98
150 406
I.|i 110
150 547
--Therapy
1
18
147 746
150 870
Encke
S
150 938
—Temperature factors
69
152 805
.
152 a32
$
28
152 097
150 940
Ferroelectric materials
122
152 035
Fuels
•
Electrodes
Enzymes
-Applications
1
1 <7
146 750
--Toxic effects
74
171058
--Axlaorpc
.ve properties
28
152 097
--Dietary factors
tL
150 671
' 81
149 593
Functions
--C3ieinic4I analysis
26
150 870
Epinephrine
1 1 ■
82
150 767
--Determination
79
152 292
--Elecrriaal propertiea
2S
171079
--Physlolog;ical effects
21
150 569
--Development
105
150 644
- -Theory
79
152 049
Electrolytic cells
.
Equations of sute
117
147 908
Ferromagnetic materials
Fused salts
27
OTSSB-425
- -Bibliogri
iphy
61
171 114
Broalon
h'Tf
--Electromagnetic properties 51
150 683
Gallium
.
- - Tempe r a ture factors
24
150 515
--Measurement
tt
148 225
-Magnetic properties
68
150 412
--Bibliography
94
152 151
Electromagnetic fielda
Erythrocytes
--Production
110
150 547
- -Physical properties
94
152 151
--Mathemt
Ideal analysis
106
152 077
j --Production
14
150 854
-•Resonance
66
150 412
Galois cohomology
78
150 951
1^676
Eskimos
110
152 310
Games theory
75
152 175
Electromag]
aetic theory
119
152 616
--Physiology
18
150 229
Field emission '
76
152 177
■-Mathematical analysis
106
150 880
Estuaries
^ mn^ •^» ^^ mm m^ ^^ ^» " -^ • • ^
•-Applications
107
150 450
121
150 839
Electromagnetic waves
--AUska
SS
150 497
--Bibliography
106
161 576
Ganuna radiation
V --Bibliography
119
150 507
--Hydrography
. 32
152 645
Fire detectors
- -Attenuation
102
^152 644
120
152 051
Etch pits
M
152 089
—Performance
38
171 028
--Detection
99
171 124
--Diffraction
106
152 077
91
150 917
Fission fragments
--Dosage determination
99
152 677
1
119
152 059
Ethylene polymers
•-Radioactivity
101
152 806
- -Scattering
102
161 575
•-Propagailon
116
150 629
--Applications
47
152 667
"Solubility
J 101
152 650
Garnets
120
152 051
Ethylenes ''
--Spectra
102
152 644
--Applications
110
152 310
-•Radiatioli
117
150 734
--Chemical reactions
24
150 538
•
Flake-glass
75
161 947
Gas embolism
--Scatters
kg
119
152 616
Evaporators *
Flake laminate
69
171 039
- -Countermeasures
20
149 246
120
150 874
--Development
91
171030
Flame surveillance detector 38
171028
Gas flow
ElectrcHnete
rs
Exit taxlways
38
171 068
Flame velocities
—Analysis
89
152 356
--ApplicaD
Ions
58
149 547
Explosive decompression
--Measurement
26
152 095
--Applications
114
152 678
Electron be4
ime
--Pathological effects
20
149 246
Flames
--Heat transfer
87
150 347
--Applicat
ions
116
150 629
150 207
--Radiation
27
150 755
118
150 762
150 991
Explosives
i
--Spectrographic analysis 27
150 755
- - Laminar boundary layer
87
150 347
--Focusing
55
150 492
--Bibliography 1
60
150 747
Flight paths
Gas flow
--MatfaesMtical analysis
107
150 822
--Blast '
1
171 106
--Matiiematical analys
Is 37
171 116
- -Mathematical analysis
28
150 170
Electron btMibtrdment
--Crysttl atructure
U
152 062
Fluid flow
--Physical factors j
26
161 574
- - Applieatlons
42
152 040
--Sensitivity
SO
149 960
--Analysis
89
152 356
--Temperature
86
150 346
Electron capture
f
—Test results
S7
150 664
--Mathematical analys
is 86
152 099
--Turbulence
87
150 802
--Measurement
100
150 523
Exposure
.
89
152 416
118
150 762
Electron giin
ts
--Pathological effects
18
147 476
"Subllity ,
88
150 528
--Velocity
87
152 357
--Design
45
152 309
--Physiological effects
14
150 568
1
89
148 178
Gas ionization
114
152 678
Electron mix:roacopes
IS
150 572
--Surface tension
88
150 528
118
150 532
--Applications
110
152 036
16
147 745
—Turbulence
89
150 331
--Applications
63
152 055
Electron tubes
150 213
—Velocity
88
150 737
--Electrical effects
105
150 526
--Development
54
150 446
150 577
--Viscosity
88
150 528
Gas masks
--Effects of radiation
56
149 713
•J-
150 578
Fluid mechanics
64
152 155
- -Effectiveness
13
152 002
- - Life expectancy
1 5*
152 753
17
147 743
89
152 356
Gas turbines
--Material
1
' 54
149 707
Uit^- .
150 230
Fluorescence
--Exhaust gases
66
150 332
56
149 713
150 564
--Excitation
3
150 943
--Materials
93
161 216
--Stability
47
171 117
18
150 576 .
Fluorine (Uquid)
Gases
y
--Test res
ults
47
171 117
21
150 569
--Chemical reactions
70
152 297
- -Acoustic properties
25 T50 458
Electronic e<
Huipment
Exposure suits
Fluorine isotopes
--Cxmdensation
26
161 574
--Design
54
171 126
--Physiological effects
102
152 299
—Nuclear reactions
101
150 516
- -Separation
92
161764
55
171 125
103
152 296
Fluorobenzenes
--Thermal properties
118
150 486
Electronic n
BJaya
Eye
«
*
"Resonance
27
150 539
Gears
--Circui^v.;
56
152 796
--Motion
1
(§8 as
Fond
--Lubrlcstion •
71
171055
--Quality ooDtrol
56
152 796
--Shielding
--Effects of radiation
21
150 671
72
152 755
--Testing «
equipment
56
152 796
F -centers
Free radicals
Generators
Electronic si
Rritchea
Factor analysis
77
152 100
--Chemical reactions
23
150 407
--Design
114
152 678
— Orcuita
48
150 805
Palling aphere
3S
150 421
•-Hyperfine structure
107
150 430
Geodetic data
Electrons
Fatigue (Mechanlca)
--Spectrographic analy
sis 113
150 443
--Analysis
29
171 067
- -Density
31
148 256
--Ultrasonic axui lysis
94
171 099
Frequency multipliers
Germanium
94
150 452
Feedback systems
S3
150 764
"Design
50
152 026
--Inqiurities
110
150 501
117
150 968
FerrltBS
--Test results
i 5^
150 683
Getters
54
149 707
Electrophor<
»sls
--Applications
Si
150 683
Friction i
Glass textiles
--Applications
12
148 269
•^ --CSiemical axxalysls
111
150 673
"Theory
1
90
150 952
--Properties
f^
69
171061
Blectroshocli
--Maoneric nrnnertl'M
106
112
150 413
150 633
. 75
171 096
--rtycholo
(leal effects
11
152 101
--Spectra
hl8
i
1
1-19
■
Subject
Glass textiles
--Tempe
Glucose
--Metabolisn
con.)
ratu -e factors
Glycines
--Physiological effects
Glycogen
--Synthesis
Goniometers
--Application^
Graphite
--Crystal striicture
Gravitating gaa
Group dynamic^
--Bibliograph i
--Psychological factors
--Sociological factors
--Test methods ,
--Theory
Groups (Mathe4iatic8)
--Theory
Gun sights
--Calibration
Hail
- -Meteorological factorsx
Harmonic analysis
--Application! I
-Theory
Hartree
--Fock method
Headgear
--Human engineering
Heart
--Physical fat^tors
--Physiology
Heat resistant Alloys
--Developmert
1
--Fatigue
--Profjerties
Heat resistant ttolymer^
--Decomposition
Heat sink
Heat tolerance
--Analysis
- -Eteierminatllon
Heat transfer
--Arctic regi<>ns
--Mathematical analysis
Height finding
Page
69
12
16
17
14
17
14
46
91
117
8
122
7
10
10
7
11
9
76
78
S7
30
105
77
112
5
13
12
13
15
90
93
96
92
28
39
103
102
64
2
84
85
4
PB Number
Subject
1
Page
PB Number
Height finding (con.) i '•*
4
150 935
171 061
Helicopters 1
150 936
152 028
--Human engineering
37
171 094
150 213
Helitron oscillator
55
150 492
147 743
Helium (Liquid)
--Thermodynamic properties
72
150 282
147 744
Hemoglobin
150 564
- - Production
Hemc^ilus pertussis
14
150 854
^ 147 744
--Culture
Hemopoiesis "'
12
148 269
152 131
--Effects of radiation
Heparin
21
152 640
150 917
--Physiological effects
19
150 856
147 908
Hickman still
39
171 030
150 361
High altitude
150 495
--Electrical effects
45
150 806
150 498
- - Instrumentation
- 35
150 753
148 268
High speed photography
150 859
--Applications
64
152 039
150 851
High temfjerature research
118
150 890
150 852
Holloman track
84
152 802-1
152 103
152 802-2
150 475
Honest John
34
152 189
150 542
Horizonul indicators
--Test results
57
152 361
148 063
Hormones
150 509
--Physiological effects
13
150 442
150 951
Hot shot tunnel
Howitzer
85
171 104
152 361
--105mm-M2A2E2
58
150 733
--Blast
58
150 733
150 420
Human engineering
14
152 138
121
150 836
150 932
• i
150 837
152 109
. iVli.
152 146
--Handbooks
5
148 319
148 917
Humidity cabinets
--Design "^
30
152 195
148 319
Humidity sensitive elements
--Calibration
30
152 195
150 218
Hydrates
152 028
--Applications
40
171 031
152 029
--Physical properties
40
171 031
152 030
- - Resonance
25
152 088
152 031
Hydraulic fluids
•
150 215
--Test results i
Hydrodynamics 1
72
171 063
171 060
--Mathematical analysis
89
150 871
161 216
Hydrofoils
171 064
--Design
88
150 478
151 096
--Hydrodynamic character-
150 479
171 103
istics
89
152 416
171 054
--Test facilities
88
150 478
--Test results
88
150 478
152 298
150 479
152 299
Hydrogen
152 155
--Adsorption
27
150 536
150 573
--Electron transitions
100
150 944
150 634
--Proton cross sections
100
150 523
150 621
--Solubility
29
150 461
150 933
--Thermodynamic properties
118
150 762
150 934
1-20
Subject
Hydrogen (Uquid)
"Handling
Hydrogen embrittlement
--Inhibition .
Hydrogen overvoltage I
Hydrogen peroxide
--Chemical reactions
--Decomposition
--Electrolysis
--Stability
Hydrography
Hydrology
Hydromagnetics
Hyperbolic equations
-Theory
Hyperfine structure
--Spectra \
Hypersonic lest vehicles
--HypersoiUc characteristics
--Perform* nee -
Hypervelocity prcfjectiles
••Erosion
•-Beoetratlao
Page PB Number
Hypervelocity vehicles
—Communication systems
--Materials
Hypothermia
•-Physiological effects
Hysteresis •! | lijl
--Temperature factors'
Ice
•-Molecular structure
•-Spectra
bnage correlation
Impact shock
••Physical effects
--Reduction
indexes
--Preparation ^
Inchistrial production
--Scheduling
Information theory
Infrared equipment
-'Design
Infrared spectra
--Analysis i
Instrument panels
"Coding
Insulation i ' I ii
•-Measurement ' I {'
--Physical factors
Insulin
••Physiological effects
Integral equations
"Tables
— Tbeory
72
92
25
26
26
26
26
33
33
89
77
107
120
87
60
19
58
62
120
39
13
15
105
95
25
25
121
58
62
37
123
76
9
78
3
27
117
103
46
77
77
150 282
152 680
171 079
152 095
152 095
150 336
152 095
150 487
150 497
150 871
150 641
150 430
150 735
150 606
148125
152 003
150 959
150 925
152 051
171 054
150 218
150 215
150 644
171 066
150 858
150 858
150 418
150 959
150 925
161 800
152 315
171 123
152 176
150 794
147 588
39 150 101
152 054
150 755
150 955
171053
150 748
171 118
15 ISO 219
152 066
152 100
152 109
^
Subject
Integral equations (con.)
--Theory (con.)
Integral functions
--Theory
Interior ballistics
--Mathematical analysis
Intermediate frequency
transformers
--Test methods
Intermetallic compounds
--Production
--Thermal properties
Internatioiial Geophysical Year
Ion beams
--Production
--Thrust
Ion exchange
--Physical factors
Ionization chambers
--Performance
Ionization gages
--Effectiveness
Ionosphere I
--Analysis |
--Electromagnetic properties
--Physical properties
Iono8i:^ere models
Ions
--Intensity
Iron
--Determination
--Metabolism
Iron -molybdenum alloys
--Temperature factors
Iron -nickel alloys
--Phase studies
Jahn-Teller effect
Jet engine fuels
- -Contamination
- - Impurities
--Temperature factors
Jet engine noise
--Analysis
Jet fighters
--Fire control systems
Jet mixing glow
--Turbulence
Jet propulsion
--Bibliography
--Theory
Jet streams (Meteorology)
--Analysis
Jets
--Turbulence
Job analysis
--Bibliography
Kineplex converter
Page
PB Number
78
150 993
152 108
79
150 466
78
147 588
77
150 883
70
47
69
69
33
34
65
65
29
99
51
31
107
120
57
34
111
21
1-21
95
95
71
71
71
86
87
64
65
64
63
30
31
6
49
152 351
150 679
171 061
171 061
148 267
150 417
150 861
150 861
152 132
152 677
171 105
148 256
150 820
150 928
152 200
150 452
150 943
150 673
152 640
90 171 060
150 850
150 468
146 402
161 921
161 921
148 689
57 152 361
152 357
152 155
150 613-
150 613-
152 153
150 964
148 262
148 263
86 148 689
171075
150 438
Subject
Laboratory jequipment
--Design
Laminated ^lass
--Development
--Mechanipal properties
Laminates
--Design
- -Development
--Handbooks
Language
--Intelligllility
Lead
--Stressea
Lead azide .
--Crystal structure
- -Decomposition
-Moisture factors
Leadership
"Analysis;
--Physiolotical factors
--Sociological factors
--Theory
Learning
--Measuretnent
" Physiological factors
--Statistical analysis
--Test nie^hods
Lee model
Legendre fuictions
Lenses |
--Test results
Lie equatiooa
Light
--Scattering
Light ranging systems
-- Design
Liquid metalB
--Bibliography
--Surface tension
Liquid rocicet propellants
--Combustion
--Conuinerts
- -Corrosive effects
--Handling,
Lithium I
--Precipitation
Lithium fluofide
--Solubility
Locking matsriala
Loop antennae
--Design i
Low temperntre research
Lubricants \
--Test resiilts
--Testing equipment
Page PB Number
20 150 2(77
75
69
75
75
75
104
61
59
59
6
11
11
9
7
11
7
7
9
115
79
13
115
71
109
38
91
96
64
66
70
TO
72
26
104
42
24
25
26
109
71
71
161 947
171 039
171 096
161 947
171 096
150 494
90 152 170
152 062
148 916
148 916
150 483
152 HI
152 111
150 542
150 372
152 101
150 178
152 103
150 503
150 504
150 557
150 466
152 001
150 556
150 557
161 921
150 628
152 350
OTS SB-424
150 637
<
152 039
148 264
150 835
161 215
161 215
150 282
110 ISO 501
152 069
152 134
150 958
150 515
150 858
161 574
152 144
171 055
171055
Subject
Magnesium
--Determination
Magnesium oxides
- - Applicafions
Magnetic amplifiers
--Circuits
--Equipment
Magnetic compounds
Magnetic cores
- -Applications
--Materials
Magnetic fields
--Theory
Magnetic materials
"Crysul structure
--Spectrographic analysis
Magnetic niodulators
--Circuits
--Performance
Magnetic piston
Magnetic resonance
--Analysis
- -Measurement
Magnetic storms
--Analysis
Magnetic susceptibility
--Measurement
Magnetite
--Crysul structure
--Temperature factors
Magneto-hydrodynamics waves
--Applications
--Bibliography
--Prc^Mgation
--Theory
Magnetometers
--Development •■"
--Stabilization
Magneto-optic roution
--Theory
Magnetostriction transducers
--Design
Magnetron guns
Magnetrons
— Development
--Electromagnetic properties
Maintenance personnel
--Performance
Majority gate
Majority principle
Mammals
--Alaska |
Manganese
--Determinatiaa
Marine biology
Marine borers
- -Countermeasures
Page PB Number
111
54
47
48
95
47
50
81
111
98'
112
HI
52
52
118
108
25
27
108
113
11
112
112
115
116
64
116
114
85
105
52
41
45
52
45
6
81
83
111
33
68
150 673
171 102
146 750
150 678
150 468
146 750
149 773
150 484
150 673
150 776
148 917
148 918
148 919
150 603
150 875
150 875
150 890
150 3^8
152 088
150 537
150 432
150 443
105 150 932
150 527
150 633
150 633
147 780-4
147 838
150 777
OTS SB -4»
152 678
150 620
150 927
150 931
149 007
152 140
152 309
150 448
152 309
152 142
150 484
150 973
22 150 575
150 673
147 175
150 954
1-22
Page PB Number
Markov chains
Markov processes
Mars
--Reflective effects
Marte natron
Martensite '
--Crysul structure
Maser
Masking reaction
Mass energy relation
Mast cells
Master slave manipulatoi:
Materials ,
I r
--Fatigue
• -Heat transfer
--Magnetic properties
--Physical properties
--Stresses
Mathematical computer dau
--Coding
Mathematical computers
--Applications
-Calibration
-Circuits
-Design
--Development
--Equipment
--Han<ttxx>ks
--Operation
--Performance
--Scheduling
- -Simulation
--Theory
Mathematical logic
--Theory
Matrix algebra
Medical research
--Alaska
Memory
--Analysis
--Test methods
77
78
7
77
2
95
95
51
13
117
19
5
65
95
99
95
58
104
78
80
82
33
53
55
60
82
84
100
70
81
80
81
82
82
95
50
82
82
81
83
39
79
80
82
82
80
76
82
9
9
9
■1
-2
152 106
152 289
152 178
150 521
150 741
171 066
150 850
150 736
152 002
147 908
150 856
152 300
150 613-
150 613-
171064
171054
171 066
161 093-5
152 134
150 509
150 992
150 599
150 487
150 764
152 183
150 799
171 100
150 100
152 358
152 351
152 045
149 259
150 649
150 598
161 565
150 767
171 066
150 601
152 651
161 565
150 484
171 080
150 973
171 040
152 049
148 259
150 506
150 599
171 100
150 506
171 093
152 053
150 599
18 ISO 214
150 369
150 975
150 503
150 504
Subject
Mesomertlc charge separation
Mesons
--Production
Meubollsm
-Climatic factors
Page PB Number
27
150 539
--Effects of radiation
Meul films
--Production
Metal ions
- -Hydrolysis
Meul plates
--Stresses
--Vibration
Meullic crysuls
- -Magnetic properties
--Purification
--Ultrasonic properties
Meullurgy
Meulorganlc compounds
- -Bibliography
- - Decompos itlon
Meul-plastic adhesives
--Materials
Meuls
- -Bonding
--Coatings
--Creep
- -Electrical properties
--Fatigue
--Physical prc^rties
--Friction
--Purification
--Recovery
--Testing equipment
Meteor
Meteorites
--Detection
Meteorological bsllons
- -Applications
Meteorological batteries
- - Tes ting equipment
Meteorological charts
--E*reparatlon
Meteorological dau
-- Analysis
--Northern hemisphere
- -Recording devices
--Sutistical analysis
--Switzerland
--Tables
Meteorological Instrumenu
--Arctic regions
--DevelojMnent
Meteorological radar
- -Applications '
98 150 937
14
IS
16
17
18
21
46
28
93
83
95
111
109
23
23
66
66
69
63
95
94
95
58
60
23
23
63
89
34
34
42
31
82
31
30
31
34
31
31
30
150 568
150 572
150 213
150 577
150 578
150 230
150 564
150 576 I
152 640
152 360
150 335
171062
171 071
150 467
150 468
150 541
152 144
150 613-2
171097
171 097
161 863
161 863
171057
150 866
171066
171099
171 064
161 093-5
150 952
171 097
171 097
150 868
152 356
148 257
152 169
152 192
150 867
161 565
148 263
152 273
152 050
152 056
148 256
152 070
152 195
30 150 420
1-23
Subject
Meteorological radar (Airborne)
--Appllcationp
Meteorology i «
Microelectronics'
Micrometeorology
- -lostrumentttion
Micro-module i
MicroorganiaiTKB
--Inhibition , .,
--Physiology
Microwave amDlifiers
--Design
--Development
Page PB Number
--Test resulti
Microwave optii »
--Theory
Microwave oecijllators
--Deaign
Microwave pre^ lector
Microwaves
--Detection
Military equipment
--Human engineering
--Preservation
Military facilities
--Construction
Military operatipos
--Geographical faaors
Military personsel
--SeleaioQ
Miliury research
Military training
--Effectiveness
MiUc .
--Radioactivity
Miniature electric equipment
--Circuits
--Developmeni
Minimax
Missile batteriei i
Missile launchens
--PerfornianceT
Missiles
--Electrical prjoperties
■-Equipment
29
31
53
30
34
54
55
71
33
47
42
51
54
51
lOt
41
110
5
73
32
6
121
'6
22
54
55
S3
78
61
57
58
48
--Hydrodynamlc charaaerlstics57
--Materials
--Safety device^
--Telemeter systems
--Test faciliti^
--Tracking
Mltochrome
Molecular associiation
--Energy
--Mathematical! analysis
Molecules
--Motion
58
92
61
45
84
58
16
86
112
.28
86
152 193
150 617
161 890
152 273
148 257
171 126
171 125
146 402
147 175
192 115
152 194
150 736
150 446
160 683
150 415
150 492
150 681
152 310
148 319
150 962
171 106
150 766
150 483
152 146
152 142
161 371-8
171 126
171 125
161 890
ISO 600
171 114
152 122
149 547
150 678
152 122
161 093-5
151096
150 626
150 318
152 802-1
152 802-2
150 329
150 441
150 346
161568
150 170
ISO 346
Sub|ect
Mood distribution
Moon
--Exploration
— nutopapby
--Reflective effects
--Surface properties
Moon rocket
Motor reactions
--Test methods
Page PB Nunabar
76
4.
2
2
37
Motor torpedo boats
--Hydrodynamlc cbaracteristics62
Mountains < .
--Wyoming 32
Moving target indicators
--Mathematical analysis 49
— Signal to noise ratio 49
Multipath transmission
--Mathematical analysis 48
Naval personnel
--Organization
l^raining
6
6
41
123
Naval research*
Needs
--Psychological faaors 10
Negative resistance circuits 48
Nervous system
--Physiology ii
--Stimulation V 8
Neutron detectors
--Design 99
Neutrons
--Physical effects 97
—Polarization 98
--Produaion 98
—Scattering 98
Nickel
--Adsorptive properties 27
--Magnetic properties J12
--Physical effects 75
--Properties 94
--Purification 94
Niobium alloys .
—Diffusion 91
--Phase studies 91
Nitric acid ^'
--Analysis f72
Nitro compounds (Organic)
--Detonation 57
Nitrocellulose
--Processing 61
Nitrogen
--Determination 17
Nitrogen (Liquid)
— Tbemaodynamic properties 72
Nitrogen oxides
--Spectra 108
1-24
171078
150 933
150 034
150 935
150 936
150 933
150 934
150 935
150 936
150 451
150 451
152 315
152 098
150 639
15^797
. 150 766
ISO 593
. ISO 593
150 796
152 136
152 142
ISO 160
161 288
150 852
150 805
150 216
152 098
171 120
171 124
152 000
ISO 406
150 776
150 406
150 536
148 917
148 918
152 294
150 280
150 280
161 767
161 767
171 115
150 664
150 456
150 567
150 282
150 096
Subject
Wtrofen oxychlorides
—Photolysis
)«,lse (Radar)
.-Analysis
Hoise (Radio)
.-Measurement
Page PB Nuntber
1'
— Reduaion
Hon -destructive testing
Huckar physics
"Study and teachingl ;
Huclear reactions I
• -Analysis I '
..Mathematical analysis
Huclear spins
—Resonance
"Theory
Ooeanographical datS
--Atlantic Ocean
"Processing
Oceanography
"Pacific Ocean
(XRcer personnel
. --Performance
Operations research
-Applications
28
60
lao
49
69
4
97
101
102
3
98
25
107
108
77
79
33
34
33
33
6
121
6
67
93
Order-disorder transformations
Or^nlc compounds
—Molecular structure 28
--Oxidation 23
--Vapor pressure 23
Organic solvents
--Effectiveness 27
Oxidat ion -reduaion reaalons
--Analysis ■. 23
Oxide cathodes I ! *
--Development 107
--Properties 105
Cocygen
--Blearochemlstrjr ; 26
"Elearon transitions 108
--Energy 63
—Metabolism 11
Oxygen consumption
--Measurement 19
36
Oxygen equipment
--Test results 36
150 627
150 799
151 377-3
151 377-4
151 377-5
150 438
171057
148 260
152 233
150 516
152 644
152 057
152 058-
152 058-
152 088
150 429
150 431
150 530
150 374
150 432
ISO 883
150 481
150 652
148 125
ISO 529
150 487
148 267
150 483
150 836
150 837
150 838
152 146
152 136
150 998
150 470
171 103
171 122
161 571
ISO 539
171 122
150 450
150 424
150 336
150 949
152 055
150 216
171073
171087
171087
Sub} eg
Oxygen isotopes
--Exchange reaalons
Oxone
—Chemical effects
— Measurement
Pacific Islands
--Ecology
Packaging
—Materials
--Shock resistance
Pantothenic acid
--Physiological effeas
Parabolic anteimas
--Radiation
Paramagnetic crystals
--Applications
Parasitic infections
--Alaska
Parasitology
--Alaska
Partial differetitial equations
--Theory
Particle accelerators
--Development
Particle trajeaories
--Mathematical analysis
Particles
--Decay
--Scattering
Particles (Airborne)
--Analysis
—Meteorological faaors
--Radioaalvlty
Pellets
--Penetration
Pemmlcan !
Penchilum
Perceptron
Perchloryl fluoride
--Toxic effects
Perovskites
--Crystal struaure
- -Magnetic properties
Pert
Perturbation theory
Phosphate coatings
--Effectiveness
Phosphorus
--Diffusion
Photochemical reaalons
- -Analysis
Photographic emulsions
- -Applications
Photographic Intelligence
- -Instrumentation
--Visual faaors
Photomagneto-elearic effea
Page PB Number
24
75
34
12
68
68
16
49
120
51
19
19
80
98
118
117
98
115
102
39
101
102
62
63
88
80
81
20
111
111
80
77
107
115
75
113
98
121
8
109
150 538
152 590
152 056
147 100
150 631
150 631
147 745
150 592
150 610
150 736
150 561
ISO 561
150 514
150 776
150 890
147 908
152 058-1
152 058-2
150 969
152 646
190 663
152 806
152 646
161 800
150 571
150 478
150 479
171093
171092
150 665
190 757
150 757
150 992
152 067
150 822
190 969
152 294
152 185
150 627
190 351
190 418
152 107
190 686
1-25
Subject
Photooa
--PoUrlMtIa
PlckllQg compoiinds
--Symheal* j
Pickup reactionp
Plkxs
—Training
--Visual tectort
PlDCli effect
Pinch experiment
Pipettes
"Developinetit
Pistons
--Acoustic properties
Plants
--Micronesia
Plasma (Physics)
Page PB Number
»Ap|dicatioai
— Blectromagsetic effects
--Blectromag^edc factors
i
—Magnetic favors
--Mathematical analysis
--StablUty
—Theory
Plasma acceleration
Plasnu engine i
Plasma Jets |
--Thrust
»1
Plasma procel
--Metabolism
Plastic coatings j
— Appilcationsj
Plasticity
--Theory
Plastics
- -Applications
- -Pi opei tls0
Platlnotron
Platinum
--Crysul structura
--X-ray analytis
Pneumatic systema (Airborne)
--Power supplies
Polarographlc aaalysis
--Appllcationat
Polymerization
--Bflects ct radiation
Polymers
--Aging
--Stability
--Synthesis
--Temperaturt fActors
Polynomials
--Applications
115
92
101
7
37
116
lU
22
104
12
64
87
98
116
117
118
115
120
lis
117
65
117
116
115
116
63
65
63
16
17
73
104
99
101
75
94
114
114
37
19
97
79
24
97
122
7f
150 891
152 680
190 516
152 123
171094
147 838
150 890
152 855
147 832^
147 100
150 777
150 606
150 776
147 838
150 988
150 890
150 447
150 735
150 447
150 734
150 882
147 908
152 113
147 780-
150 629
150 991
150 964
150 882
150 964
150 565
150 570
150 962
152 134
150 825
150 687
171096
150 446
190 749
150 749
152 313
171073
152 648
152 649
152 590
152 087
152 648
152 649
192 035
152 292
Subjeq
Population
--Geographical factors
Positrons
--Energy
--Scattering
Potassium bromide crysuls
--Crystal structure
Pousslum chloride crysuls
—Crysul structure
Potential theory
Powder bags
--Coatings
--Materials
Power fsnerators
Power series
Precipitation
--Bibliography
Preselector
Precico
Primates
--Testing equipment
Printed circulu
—Containers
Probability (Statistics)
--Applications
—Determination
-TUdes
—Theory
Page PB Number
Profllometer
Projectile fragmenu >
--Recovery
Propellant grains
—Design
—Extrusion
Propellanu
—Combustion
— MaterUls
Propulsion chemistry
Protectivs clothing
—Climatic tacton
—Materials
—Physiological effecu
—Ventilation
\
122
100
100
no
no
79
86
n
79
»1
41
St
7t
n
•
49
H
79
76
77
76
•0
9i
77
62
40
71
71
70
71
61
69
103
74
103
102
103
152 110
150 944
150 944
ISO 543
150 543
150 466
152 099
148 914
148 914
161578
150 951
148 199
150 617
150 681
150 835
150 372
150 809
150 810
150 482
152 108
148 199
150 361
150 593
152 176
150 600
150 522
152 100
171078
150 496
171092
150 521
152 106
152 289
150 481
150 652
150 476
150 477
150 496
150 459
148 225
150 390
150 390
152 351
152 027
150 456
ISO 613-1
150 613-2
150 778
171058
150 778
152 299
150 778
152 298
1-26
Subjgg
pjQisctive construaiott
frotelM
.-Biochemical effect^
..Metabolism
pitjion cross sections
■ •Measurement
fgycbomotor tests '
-Applications ,
-Physiological factdtf
ffjfchotherapy
.•Psychological factors
Public health
.•Periodicals
-Preservation
Pulse cables
-Blectrical properties
Pulse generators
-Design I;
Pulse modulation
.•Instrumentation
Fyrene
.-jVesonance
Q-fuDCtlons
00779
Qoncum mechsnics
—Theory
()MzO crysuls
-Physical propertlM
Qulnones
— Hyperfine structure
I;
••Spectra
Mdsr antennae
—Design
lUdir beacons
-Performance
Rsdar comer reflectors
-Design
Rtdsr eclio areas
--Geographical factors
--Measurement
Radar operators
--Training devices
Radar reflections
•-Measurement t
Radar scanning | '
—Equipment |
Radar signals 1
—Detection > :
Radar targets ' | ||
—Detection
Radar tracking sysums
—Design
Radar transmitters
—Equipment i
Radiation
—Biochemical effecu
—Ionizing effecu
-^ourcea
17
17
7
22
22
47
49
49
JOB
Bl
94
119
il9
109
107
108
107
42
41
96
21
97
113
5
PB Number
171 106
150 471
150 567
150 570
190 923
152 123
152 098
150 490
161371-7
161 371-8
152 667
150 595
150 595
150 378
171092
110 446
150 556
150 557
150 891
150 969
150 680
ISO 430
150 431
150 432
150 431
152 188
171095
152 614
Subject
Radiation counters
--Bibliography
Radiation damage
—Bibliography
— Countermeasures
Radio astronomy
Radio interference
--Physical effecu
Radio signals
--Transmission
Radio wave reflections
-Tables
Radio waves
--Electromagnetic properties
--Polarization
--Pn^g^ion
--Scattering
Radioactivity
--Detection
RadioMology
- -Instrumenution
Radlochemlstry laboratoriei
--Equipment
Radlofrequency cables
--Electrical properties
Radlofrequency filters
--Design
—Mathematical analysis
Radlofrequency generators
—Design
—Power siqjplies
—Stability
Radlofrequency pulses
--Detection
Radioisotopes
—Applications
Radiological contamination
- -Countermeasures
Page PB Number
119
150 650
f
41
150 740
—Mathematical analysis
41
150 160
—Measurement
2
190 451
—Tables
--Test resulu
52
146 395
Radiometers
-Design
48
150 608
Radiosondes
-Design
49
150 593
—Testing equipment
44
152 311
-Analysis
—Blectrical properties
49
190 595
--Growth
Random distributlM
150 671 Rare earths
152 648 — Api^cations
152 649 Rations (MiUury)
150 443 —Arctic regions
150 801 Rawinsonds dau
1-27 1
99
56
101
2
55
120
120
120
119
48
119
120
119
101
22
22
47
41
41
92
92
92
32
93
60
22
101
1
1
1
101
99
104
42
91
90
91
79
109
69
Si
171 124
149 713
150 687
149 007
148 972
150 735
161 579
150 928
150 669
152 041
150 669
150 610
ISO 928
150 650
171 091
152 353
152 353
152 667
152 191
152 191
161 578
161578
161 578
150 997
152 645
150 843
148 225
161 371-7
161 371-8
152 650
190 616
150 614
150 615
150 616
152 806
150 753
152 190
152 192
150 437
190 929
150 437
148 199
190 424
150 571
190 867
Sub}eq
Rayleigh wavei
Reaction (Psychology)
--Analysis
--Test methoiJs
--Theory
Reactors
--Blast effect^
--Calibration'
--Hazards i
Reading machines
--Development
Reasoning i
--Psychological factors
Recombination ramjet engines
- -Performance
Rectifiers
--Development
Redwing ^
Re-entry aerodynamlca
- -Instrumentation
--Test facilities
Reflection coefficients
Refractory mattrials
- -Applications
- -Development
--Properties
Reliability
--Statistical a
lalysis
--Theory I
Remote control Systems
--Human engineering
Resistance devices
Resistors
"Production
Resonance
--Mathematical aiutlysis
Respiration I
--Control I
Respiratory disdases
--Alaska
Respirometers
— Design
--Test results
Restrained colur^ns
Riboflavin
- -Physiological) effects
Rivets
--Stresses
Rocket fuels
--Materials
Rocket motor nozzles
--Test resulta
Rocket motors
--Design
--Fuel injectioi
--Mark 29
--Performance
--Test results
--Thrust
Rocket oxidizer*
--Hazards
--Materials
94
9
7
9
99
100
101
80
81
8
63
48
102
39
M
87
120
106
69
69
80
48
5
9S
46
90
19
18
14
13
83
18
40
72
36
(PB Number
171 099
150 503
150 504
150 372
150 794
148 647
152 358
152 806
171 093
171092
152 104
152 055
150 678
152 646
171054
152 312
150 606
161 573
148 254
171 061
171 081
171 101
150 477
150 496
152 295
152 300
171066
152 360
152 170
150 788
150 566
4
150 439
152 002
152 143 ^
150 576
152 355
171 115
152 647
Subjeq
fi
Page PB Number
69
150 882
66
148 264
65
150 972
66
150 835
65
150 972
61
ISO 886
?5 iff ?f5
Rocket propellants
--Corrosive effects
--Safety measures
Rocket propelled sleds
--Development
Rocket propulsion
--Theory
Rocket research
Rodents
--Arctic regions
Royal McBee
Rubber
—Oxidation
--Preservation
Runway lights
--Visibility
Runways
--Location
--Trafficabllity
Rural areas
—Arctic regions
SA-16B
Salts
- -Bibliography
Sampling (Statistics)
Satellite vehicle research i
Satellite vehicle trajectories
--Mathematical analysis
Satellite vehicles
--Applications
--Equipment
--Propulsion -j- I
"Tracking
Scheduling
--Theory
Schistosoma
--Alaska
Scientific reports
--Processing
Scientific research
--USSR
Scintillation counters
--Applications
--Design
Scopolamine
--Synthesis
Sea water
—Desalination
Search radar data
- -Nomographs
Search radar systems
--Signal to noise ratio
70
70
84
65
65
34
22
80
75
75
38
38
40
122
36
60
61
5
50
64
60
62
78
19
161 215
152 354
152 802-2
150 613-1
150 613-2
150 882
150 417
150 562
150 992
152 590
152 590
152 350
171068
150 436
152 110
152 296
27 OTS SB -425
80 150 476
57 152 200
150 799
150 989
148 258
152 026
150 777
150 799
150 647
150 482
150 560
122
150 818
123
171 123
103
150 872
121
150 836
150 837
150 838
150 839
122
152 035
123
161 288
106
161 576
2
150 517
7
150 371
99
171 120
20
152 096
39
171030
40
171031
Sli
150 684
m'
150 608
1-28
V
Sedlmenutioa
•-Analy«lB
.-Uke Mead
Semlcoodualng fllmfl
—Test results
jfgilooaductora
"kffUcMtiotm
.-Conductivity
— Dsvelopment
-Blectroa transltlooa
PafB PB Number
—Impurities
.-Haterlals
-Mathematical analyst
-Properties
-•Surface properties
-Temperature factors
Sensory perceptloo
-Analysis
Series expansions
—Applications
Servomechanlsms
-Applications
-Operation
aa^ digitizer
32
32
113
49
99
109
44
111
113
49
109
110
44
114
111
113
44
ID
77
78
79
44
5
58
-Hypersonic characterlatlca 87
—Materials
—Production
—Stresses
96
66
93
118
66
—Tensile properties
Shielding I I n
-Materials f' > fji 101
Ship hulls
—Struaural analyala 62
—Surfaces 62
Ships
-Hydrodynamlc characterlatlca88
-Motion 90
—Propulsion 64
Shivering
"Physiological effects U
Shock tubea
—Applications
Shock waves . . l.
--Attenuation | '{.
— Praaaure
—Reflection
Sbopalr
Shroud antetmas
Shrouded propellers
—Performance
-Wake
Side- lobe suppreaaloo
Slpala jj-
— Gonulnera '
$lllcldea
—Cryatal atnicture
SlUcon
-Oaldation
i
58
58
56
65
\»
42
36
36
49
59
114
113
152 645
152 643
150 812
150 609
150 473
150 686
150 963
150 603
150 537
150 609
150 686
150 501
150 963
150 525
150 784
150 811
150 812
150 963
150 638
152 100
150 993
150 466
152 311
152 300
150 329
150 347
171083
151095
171 088
150 738
151095
150 687
152 797
150 459
150 737
150 842
152 130
150 216
150 454
150 957
150 957
150 531
150 101
150 958
150 783
150 783
150 597
150 825
171 121
152 185
Subject
Silicon cryauls
--Surface properties
Silicon dioxide
--Surface properties
Silicones
--Applications
Silver acetylide i
--Detonation
Silver electrodes
- -Electrochemistry
Single crysuls
--Growth
"Surface propertlea
Single crysuls (Metallurgy)
- -Electrochemistry
—Electron transitions
--Resonance
Sky brlghtneas
- -Meaaurement
Slave manipulator j
Sleeve antennas
Social communication
--Psychological tectors
—Theory
--Visual factors
Social sciences
--Theory
Soils
^I'Cb^amlnatloa
—Heat tranafer
—Mechanical properties
—Moisture content
—Physical properties
—Radloaalvlty
-Stabilization
—Temperature
-TrafflcaWUty ,
Solar atmospbers \
--Radiation
--Spectra
— Spectrographlc analyals
Solar flares
--Meaaurement
Solar furnaces
--AppUcatlona
Sollda
--Catalytic properties
--Magnetic propertlea
--Surface propertlea
Sound
--Propagation
—Theory
— yekx:ity
Sounding rochets
--Equipment
1-29 I
113
20
m
26
111
113
26
25
111
111
34
5
56
6
10
122
6
122
31
32
67
1
29
97
40
32
40
67
2
3
3
4
5
28
27
HI
110
53
104
25
35
42
PB Number
150 811
152 185
149 246
150 970
150 336
ISO 541
ISO 537
152 089
171079
150 666
150 666
148 257
152 300
152 615
150 490
150 851
150 495
ISO 472
148 197
150 617
150 444
150 445
150 999
ISO 614
150 615
150 616
150 862
152 000
171098
150 444
150 445
ISO 436
171098
ISO 998
150 999
149 007
150 939
152 054
150 926
150 801
150 627
152 126
ISO 603
152 036
171099
147 832
150 458
150 873
150 958
Subject
Sounding rockets
--Equipment
--Meteorological factors
Space Charles
--Electrotnagnetic effects
Space flight ,
--Analysis
--Physiological effects
--Stimulai ion
Space medicine
--Instrumentation
Space objects
Spaceships I
--Design
--Flight paths
--Rocket vropulsion
Speech ;
--Intelligi^lUty
Speech transmission
- -Intelligl|}ilicy
Spheres
--Elasticity
Spiral antenpias
<;',
[uid
Stainless sti !el
— Corrosion
--N4echanical properties
- -Physical; properties
Stars
--Motion
--Spectra
Starvation
- -PhysioloWcal effeas
Statistical analysis
--Equipment
Steel
--Fatigue
--Mechaoldal pixyperties
--Melting
"Pickling
--Tensile properties
--Test results
Steel casting^
--Development
Stepped zone mirror
Stochastic approximation
Storage batteries
--Electrodes
Storage tube«
--Design
Storms
--Radar an* lysis
Strain flages
Page
S2
34
45
61
7
14
121
36
14
61
121
61
61
104
55
122
104
52
64
85
118
96
92
92
117
3
12
13
81
67
92
94
40
92
92
92
91
91
108
78
S3
43
3P
13
PB Number
150 931
152 189
152 309
150 886
150 372
150 439
150 440
150 838
148 274
ISO 440
150 989
150 838
ISO 886
150 886
150 494
148 972
152 172
152 134
146 395
152 153
152 155
150 531
ISO 532
161 749
151096
161 218
147 908
150 939
152 028
152 029
152 030
152 031
150 649
152 642
171056
150 877
152 355
161 764
152 680
171077
171065
171065
150 415
150 600
150 843
152 092
150 420
152 033
Subject
,0--
Page PB Number
Strontium isotopes (Radioactive)
--Precipitation
Strontium titanate crystals
--Resonance
Structural shells
--Deformation
Structures
— Creep
--Load distribution
--Stresses
--Vibration
Styrene polymers
--I>etonation
Submarine hulls
— Acoustic properties
--Stresses 1
--Wave trarismission
Submlnlature electronic
equipment
--Development
Sulfur
--Chemical reactions
Sun
--Radiation
Superconductors
--Acdustlc properties
Superregeneratlon
Supersonic nozzles
--Configuration
Supplies
—Disposal
--Quality control
— Scheduling
Surfaces
"Catalytic properties
--Coatings
--Friaion
— Recording devices
—Refleaive ef^ts
—Temperature
Survival
— Arctic regions
--Dleury factors
iV
Survival kits
Switching circuits
--Equipment
--Materials
Synthetic fibers
--Properties
System research
Tarur
Taylor series
--Applications
Teeth
--Chemical analysis
Telemeter systems
--Design
Television
--AppUcatloos
Teniperature
--Measurement
-30
HI
88
I 83
40
83
83
57
119
62
119
h-
53
25
2
109
42
36
103
103
103
28
25
90
62
119
85
63
12
13
102
SO
9S
73
121
61
77
18
4S
100
4S
iS0 6U
150 6U
150 6(1
1S0 8S
ISO 416
152 3SS
1S0 4U
171070
130 66(
1S0 879
152 807
150 879
161890
150 334
ISO 573
152 144
152 194
152 647
152 134
152 124
152 124
152 1S2
150 334
ISO 952
ISO 450
152 616
150 621
ISO 571
152 028
152 029
152 030
152 031
171 119
149 773
171066
150 548
150 836
150 839
150 626
152 109
ISO 29
1S0 31S
152 359
150 318
Subject
--Design
Terrier
Test sets
-Design
Testes |
--Physiology
Textiles
--Coatings
Tlieodolites
—Applications
Thermal radiation
--Analysis | ^!
Thermal stresses
—Mathematical analysis
Thermionic emission
Page PB Number
--Mathematical analysis
Thermocouples
-Shielding
Thin films
--Magnetic properties
Thyroid gland '
--Physiology
Tin compounds (Orginlc)
--Toxic effects
Tin crystals
c -Electrochemistry
Tissues (Biology)
--Pathology i
--Physiology
Titanium alloys .
—Creep , j \
--Fatigue ' ' '
--Heat treatment
—Mechanical properties
•-Phase studies
Topology
Torque
--Mathematical analysis
Tracked vehicles
--Pressure i
Tracking. i
--Control systems
"Psychological faaors
Tracking telecopes ■
--Development
Tracks (Aerodynamics)
--Development
--Operation
Training
--Test methods
Training devices
--Design
63
61
42
22
73
34
3S
88
117
118
42
43
44
105
106
31
81
82
IS
20
2S
19
13
93
96
66
66
95
76
77
78
90
67
14
52
7
58
\
84
84
10
10
150 868
150 626
152 192
150 562
150 962
152 189
148 255
150 853
150 474
150 738
152 068
152 040
150 815
150 813
ISO 814
150 816
150 424
148 254
152 07tj
I
149 593
150 767
150 219
150 488
171079
150 856
152 033
171082
171064
151 095
151095
150 855
148 063
152 067
150 951
152 681
152 073
152 138
148 849
152 123
150 329
152 802-2
152 802-1
150 639
150 639
Subject
-
Page
PB Number
Transducers
--AppllcatlonB
89
150 540
--Bibliography
53
GTS -SB -428
--Design
85
171 104
Transfor mat ions
(Mathematics)
78
147 588
Transistors
--Applications
35
150 753
81
152 045
--Containers
51
150 809
150 810
--Life expectancy
50
150 601
--Theory
43
152 657
Transmission lines
--Equipment
43
150 552
TransDort numbe
r
110
150 544
Transportation
--Analysis 67
Transverse pinches 98
Traveling wave tubes
--Design 115
--Theory 107
Triangular wings
--Supersonic characteristics 39
Trlodes
--Test results 54
Tropical deterioration 96
Tularemia
—Alaska 20
Turbojet exhaust tK)zzleu
- - De ve lopment 35
Turbulent boundary layer
- - Mat hemat i ca 1 ana lysl s 87
--Pressure 89
Turbulent flow
--Analysis 89
--Measurement 89
--Shear stresses 86
Typhoon resolve r 82
Ultra high frequency
communication systems
- -Performance 48
120
Ultrasonic radiation
--Applications 94
--Attenuation 109
--Thermal effects 18
Ultrasonics
--Applications 69
Ultraviolet radiation
--Pathological effects 21
--Physiological effects 21
Underground structures
--Blast elffects 58
Underwater ballistics 60
--Mathematical analysis 60
Underwater objects
--Fouling 39
Uniforms 73
Universal turing machine 82
Upper atmosphere
--Analysis 34
--Density 35
- -Instrumentlon 34
--Instrumentation 3S
150 611
ISO 612
150 776
ISO 447
150 820
152 352
152 753
161 749
150 574
152 641
ISO 802
150 540
150 331
150 540
152 173
152 651
152 041
150 610
171099
152 144
152 032
171 057
171072
171 072
150 957
150 830
150 831
150 7ov
171 089
150 508
150 452
150 421
148 257
150 873
1-31
Sutaect
Upper ctmoophei^ (con. )
--InstrumentAQlaa 42
--lonlzatloo 6S
--Meceorologjr 30
--Properties 34
Uranium laocopeB (Radiosctive)
--Spectra 102
V-particles
--Theory 98
Vacuum fumacef
- - Apphcatlooa
Vacuum metallurgy
Valves
--Design
Van Allen radiation
Vapor pressure
--Tables .
Vehicles
--M29C
--Propulsion
Verbal behavior
--Psychological factors
Vertical take -off planes
--Military requirements
--Perforrnance
Very low frequency
communication systems
Vibration
- -Mathematical analysis
-Theory
Video delay line^
--Materials |
Video mapping I
Video signals
--Tranamisrtoi
Visibility J
--Measurement
Visual acuity i
Visual perceptlo^ |
--Analysis
Visual range meoer
Voice communlc4tion systems
--Bibliography ,
—Coding
Voltage !
- - Measurement
Vortices \
--Mathematical analysis
Voting game
Water exit i
92
92
61
5
23
67
4S
104
9
36
96
83
90
38
83
49
48
48
38
8
S2
38
122
55
25
86
76
60
FB Number
150 598
152 055
148 262
150 417
152 644
152 058-1
152 058-2
161764
161764
150 626
150 801
161 571
152 073
171026
150 494
150 503
150 504
152 752
li2 752
148*258
171070
152 681
171090
171071
150 609
150 594
150 594
152 350
152 107
149 849
152 350
152 172
148 972
171079
152 047
152 177
150 830
150 831
Subtea
Water supplies
- -Comamlnatlon
--Radioactivity
Water vapor
— Chemical effects
--Heat transfer
—Spectra
Water waves
--Mathematical analysis
Wave equation
Waveguide filters
--Design
--Perfbrmance
Waveguides
--Mathematical analysis
Weather forecasting
--Statistical analysis
Welds
- -Stresses
Whistlers
Wiener Hopf equation
Wind
--Measurement
--Velocity
Wind tunnels
--Design
--Instrumentation
Windshields (Airborne)
- -Human engineering
Wings
--Hypersonic characteristics
--Pressure distribution
Wire
--Mechanical properties
Wood
--Preservation
Woolen textiles
--Test results
Wounds
--Analysis
X-15
X- radiation
--Physiological effects
- -Sources
X-ray diffraction analysis
--Applications
YP-110
Yttrium
--Mechanical properties
--Phase studies
Page PB Number
101
22
101
91
35
3
90
80
41
41
106
31
40
107
78
31
34
35
114
85
37
36
36
66
68
73
19
36
21
2
I
114
62
94
94
152 650
171091
161 371-1
171091
161696
148 255
152 054
150 842
ISO 514
150 681
ISO 681
150 413
152 050
152 355
150 820
152 108
ISO 867
152 189
150 421
152 678
171 104
171094
150 985
150 985
152 197
150 954
150 548
152 003
148 274
152 640
150 517
150 749
152 797
171086
171085
1-32
Number
AALTN-60-8
AALTN-60-9
AALTN-60-11
jUU-TN-eO-14
AALTR-57-I9
AALTR-57-26
AALTR-57-31
AALTR-57-33
ALLTR-57-34
AALTR-57-35
AALTR-57-38
AALTR-57-44
AALTR-57-47
AALTR-57-48
AALTR-57-51
AALTR-57-53
AALTR-57-54
AALTR-57-55
AALTR-58-I8
AALTR-58-21
AALTR-58-22
AALTR-58-23
AALTR-58-24
AALTR-58-27
AALTR-59-1
AALTR-59-3
AALTR-59-6
AALTR
AALTR
AALTR
AALTR
AALTR-59
AALTR-59
59-7
59-8
59-18
59-19
23
24
AALTR-eO-14
AALTR-60-15
AALTR-60-16
AALTR-75-16
ACICTR-59, rev.
AD- 10 037
AO-16 351
AO-24 418
AD-46 281
AD-71 333
AD-87 968
AD-93 756
AD- 110 039
AD-110 050
AD-110 090
AD- 124 114
AD- 129 167
AD-133 862
AD-133 863
AD-136 254
AD-ISO 870
AD-152 478
AD-152 552
AD-155 313
AD-155 879
AD- 156 260
AD-158 218 I
NUMBER INDEX
. P^
Number
12
AD- 159 902
13
AD-202 838
18
AD-207 809
13
AD- 208 579
19
AD-208 936
22
AD-208 937
17
AD-210 922
15
AD-211 215
17
AD-211 953
16
AD- 21 2 440
13
AD-216 292
18
AD-216 657
15
AD-217 515
17
AD-217 614
14
AD-218 842
21
AD-219 750
17
AD-220 812
63
AD-225 203
17
AD-225 216
15
AD-226 148
11
AD-226 245
14
AD-226 520
15
AD-226 691
2
AD-227 317
20
AD-227 616
22
AD-227 863
18
AD-227 928
18
AD-228 033
18
AD-228 105
12
AD-228 114
12
AD-228 117
16
AD-228 128
18
AD-228 166
16
AD-228 177
16
AD-228 212
16
AD-228 267
19
AD-228 389
29
AD-228 635
53
AD-228 638
57
AD-229 040
89
AD-229 109
68
AD-229 112
45
AD-229 196,
72
AD-229 280
48
AD-229 312
48
AD-229 361
49
AD-229 364
55
AD-229 368
36
AD-229 369
99
AD-229 372
49
AD-229 379
120
AD-229 380
92
AD-229 403
HI
AD-229 493
62
AD-229 494
105
AD-229 511
4
AD-229 528
37
AD-229 532
109
AD-229 624
66
AD-229 644
Page
Number
v*.
100
AD-229 646
47
AD-229 706
47
AD-229 733
41
AD-229 737
51
AD-229 740
51
AD-229 833
75
AD-229 922
78
AD-229 923
48
AD-229 924
101
AD-229 926
63
AD-229 941
3
AD-229 943
66
AD-229 950
38
AD-230 025
113
AD-230 116
56
AD-230 120
49
AD-230 172
61
AD-230 194
68
AD-230 202
97
AD-230 244
49
AD-230 246
102
AD-230 248
111
AD-230 258
105
AD-230 259
54
AD-230 318
114
AD-230 328
50
AD-230 329
70
AD-230 332
21
AD-230 351
76
AD-230 352
77
AD-230 353
64
AD-231 368
55
AD-230 421
24
AD-230 445
90
AD-230 482
101
AD-230 535
122
AD-230 536
10
AD-230 537
10
AD-230 538
105
AD-230 545
88
AD-230 552
118
AD-230 598
111
AD-230 599
102
AD-230 601
21
AD-230 813
89
AD-230 863
81
AD-230 866
7
AD-230 867
29
AD-231 102
10
AD-231 105
17
AD-231 153
123
AD-231 182
^9
AD-231 213
117
AD-231 234
lie
AD-231 252
29
AD-231 405
77
AD-231 401
114
AD-231 415
9
AD-231 422
19
AD-231 475
78
99
S7
93
95
20
122
121
121
121
63
113
107
48
118
83
101
26
27
6
8
24
56
fO
76
76
9Q
34
79
24
r
12
122
8
47
9
9
33
11
6
43
94
80
28
56
77
64
109
104
34
75
86
7
87
79
44
55
26
90
78
1-33
Number
AO-231 516
AO-231 641
AO-231 842
AD-231 860
AD-231 907
AD-231 936
AD-231 937
AD-232 164
AD-231 175
AD-232 225
AD-232 289
AD-232 402
AD-232 403
AD-232 562
AD-232 565
AD-232 638
'AD-232 641
AD-232 745
AD-232 880
AD-233 022
AD-233 164
AD-233 168
AD-233 340
AD-233 352
AD-233 424
AD-233 433
AD-233 457
AD-233 477
AD-233 509
AD-233 729
AD-233 797
AD-233 969
AD-234 030
AD-234 043
AD-234 081
AD-234 160
AD-234 230
AD-234 295
AD-235 319
AD-234 373
AD-234 464
AD-234 480
AD-234 544
AD-234 703
AD-234 797
AD-234 972
AD-234 974
AD-235 637
AD-235 996
AD-236 164
AD-236 461
AD-236 847
AD-237 049
AD-237 116
AD- 237 560
AD-237 718
AD-237 815
AD-237 865
AD-237 866
AD-237 920
AD-237 957
AD-237 969
AD-238 114
AD -238 205
AD-238 226
P*ge
Nionber
14
AD-238 346
80
AD-238 426
103
AD-238 614
46
AD-238 923
84
AD-238 961
80
AD-239 227
80
AD-239 280
82
AD-239 464
8
AD-239 537
102
AD-239 772
55
AD-239 826
104
AD-239 869
28
AD-239 876
26
AD-239 923
122
AD-239 976
63
AD-239 994
24
AD-240 028
11
AD-240 097
33
AD-240 128
55
AD-240 194
86
AD-240 322
22
AD-240 483-,
36
AD-240 503 f
8
AD-240 615
99
AD-240 887
88
AD-240 889
5
AD-241 176
47
AD- 241 178
47
AD-241 179
83
AD-241 226
110
AD-241 358
69
AD-241 376
38
AD-241 399
34
AO-241 504
82
AD-241 536
25
AD-241 537
43
AD-241 546
80
AD-241 713
54
AD-241 875
31
AD-241 878
121
AD-241 890
31
AD-241 891
30
AD-241 892
86
AD-241 893
106
AD-242 247
35
AD-242 414
5
AD-242 475
54
AD-242 503
46
AD-242504
64
AD-242 505
12
AD-242 506
33
AD-242 528
32
AD-242 653
32
AD-242 655
116
AD-242 656
89
AD-242 738
33
AD-242 750
79
AD-242 797
122
AD-242 859
107
AO-242 860
52
AD- 243 016
117
AD-243 017
15
AD- 243 095
76
AD-243 117
78
AD-243 143
1-34
X
Page
Number .1
hs.
1
1
Number
Pajp
113
AD-243 144
77
"""""""
42
^ AD-243 162
/ AD-243 176
77
AFCRL-TN -60-762
120
109
111
AFCRL -TN-60 -764
43
44
AD-243 376
US
AFCRL-TN-eO-765
Ml 120
97
AD-243 470
76
AFCRL-TN-60-767
5- 106
90
AD-243 489 ,
71
AFCRL-TN-60-768
23
55
AD-243 514
64
AFCRL -TN-60 -77 3
62
2
AD-243 530
- 117
AFCRL -TN-60 -774
105
111
AD-243 601
107
AFCRL-TN-60-777
43
2
AD-243 734
86
AFCRL -TN-60 -785
11-7
S3
AD-243 767
78
AFCRL -TN-60 -795
41
51
ARnC-TN-59-145
36
AFCRL -TN-60 -798
42
lis
AEDC-TN-60-173
36
AFCRL-TN-60-953
119
98
AEDC-TR-60-11
85
AFCRL -TN-60 -955
81
20
AERDL 1569-TR
101
AFCRL-TN- 60 -966
61
lis
AE WES TR- 3-455. R-3
«
AFCRL-TR-60-119 ,
80
45
AEWESTR-3-545. R-3
fi7
AFCRL -TR- 60 -149 ,
|; 110
43
AEWES TR-3-554
0
AFCRL-TR-60-156
1 79
34
AF TR-5702
103
AFCRL-TR-60-160
1 82
54
AFBMDTN-59-6
114
AFCRL -TR- 60 -163
U6
81
AFCRC-TN-57-58
55
AFCRL-TR-60-173
51
84
AFCRC-TN-58-409
105
AFCRL-TR-60-174
57
43
AFCRC-TN-59-270
4
AFCRL -TR- 60 -17 6
120
41
AFCRC-TN-59-663
30
AFCRL-TR-60-210
5
48
AFCRC-TN-59-785
106
AFCRL-TR-60-218
35
84
AFCRC-TN-60-441
100
AFCRL-TR-60-227
30
34
AFCRC-TN-60-1007
111
AFCRL -TR- 60 -229
30
42
AFCRC-TR-58-266
105
AFCRL -TR- 60 -234
34
29
AFCRC-TR-59-255
38
AFCRL-TR-60-254
31
87
AFCRC-TR-59-290
34
AFCRL -TR- 60 -263 ,
52
54
AFCRC-TR-eO-144
94
AFCRL-TR-60-265
109
38
AFCRL E5070
119
AFCRL-TR-60-286
35
99
AFCRL-TN-50-783
81
AFCRL -TR- 60 -292 |
31
58
AFCRL -TN-58 -243
62
AFCRL-TR-60-401 i
35
40
AFCRL -TN- 60 -183
106
AFCRL-TR-60-403 i
27
87
AFCRL -TN-60-210
120
AFFTC-TR-57-16
36
40
AFCRL-TN -60-226
30
AFFTC-TR-59-31 ^
70
31
AFCRL-TN-60-227
31
AFFIC-TR-60-19
72
»
AFCRL-TN -60 -267
31
AFMDC -TN-60 -12
97
58
AFCRL-TN-60-268
4
AFMDC-TR -60-20
7
. 1
AFCRL-TN- 60 -269
4
AFGSR-TN-58-415
66
1
AFCRL-TN -60 -270
4
AFCSR-TN-59-517
63
1
AFCRL -TN-60-271
4
AFOSR-TN-59-1210
29
31
AFCRL -TN-60-273
35
AFOSR-TN-59-1308
ll'. 86
108
AFCRL-TN-60-283
98
AF06R -TN-60- 97
•'■ 1
83
AFCRL -TN-60-296
3
AF06R-TN-60-178
28
84
AFCRL-TN-60-297
3
AFCSR-TN-60-299
M 26
107
AFCRL-TN-60-388
66
AFOSR-TN-60-589
! 107
107
AFCRL-TN-60-401
3
AFOSR -TN-60 -601
108
107
AFCRL -TN-60-414
2
AFGSR-TN-60-638
85
108
AFCRL -TN-60-439
3
AFOSR -TN-60 -64 3
85
78
AFCRL-TN -60 -464
UN
AFOSR -TN-60 -683
114
1
AFCRL-TN-60-565
UN
AFOSR -TN-60 -700
71
lis
AFCRL -TN-60-574(Il)
46
AFOSR -TN-60-755
110
115
AFCRL -TN-60-581
57
AFOSR -TN-60-762
115
108
AFCRL-TN-60-586
S3
AFOSR -TN-60 -836
83
?
AFCRL -TN-60-596
116
AFOSR -TN-60 -840
f 118
11
1
AFCRL -TN-60-597
119
AFOSR-TN-60-843
i 84
2
S
AFCRL -TN-60-616
2
AFOSR -TN-60 -863
107
7
r
AFCRL-TN-60-628
2
AFOSR -TN-60 -87 5
1
i
5
AFCRL-TN-60-639
28
AFOSR -TN- 60-876
31
85
AFCRL -TN-60-645
119
AFOSR -TN-60 -88 2
114
66
AFCSR-TN-60-656
78
AFOSR -TN-60 -886
66
64
AFCRL-TN -60 -658
51
AFOSR -TN-60 -898
115
77
AFCRL -TN-60 -759
44
AFOSR-TN-60-904
108
tfOSR-TN-60-910
77
Number
Number
Page
AFOSR-TN-60-914
86
ASRDL-2135
29
AFOSR-TN-60-915
87
ASRDL-2136
42
AFOSR-TN-60-917
100
ASRDL-2137
30
AFOSR-TN-60-919
108
ASRDL M-1870
58
AFOSR-TN-60-920
107
ASRDL M-1918
109
AFOSR -TN-60 -927
117
ASTR
100
AFOSR -TN -60-931
107
ATI 23 309
103
AFOSR-TN-60-935
63
ATI 65 612
75
AFOSR-TN-60-937
98
AvcoRN-132
114
AFOSR-TN-60-955
64
Avco RR-88
117
AFOSR-TN-60-978
114
Avco RR-89
63
AFOSR -TN-60 -982
77
Avco RR-90
64
AFOSR -TN-60 -983
77
B8C-150
66
AFOSR -TN-60 -1008
, 8
BBN-690
119
AFOSR -TN-60 -1015
88
Bell -8007 -981 -Oil
64
AFOSR-TN-60-1028
111
BN-181
86
AFOSR-TN-60-1036
79
BN-216
77
AFOSR-TN-60-1046
118
BN-220
86
AFOSR-TN-60-105la
98
BRL-lOU
99
AFOSR -TN-60 -105 lb
98
BRL'1104
34
AFOSR-TN-60-1054
10
BRL MR-1278
58
AFOSR -TN-60 -1059
77
BRLMR-1279
58
AFOSR-TN-60-1067
78
BRLMR-1283
42
AFOSR -TN-60 -1069
86
BRL MR -1286
58
AFOSR-TN-60-1089
115
BRL TN- 1313
58
AFOSR-TN-60-1091
76
BRL TN- 1315
121
AFCISR-TN-60-1161
28
BTL-27424-0
109
AFOSR-TR-59-61
3
BuMed MR005. 12-0005. 4,
AFOSR -TR- 59 -135
89
R-9
36
AFOSR-TR-59-197
66
BuMed MR005. 15-0002. 2
14
AFOSR-TR-60-21
79
BuMed MR005. 15-0002. 2,
AFOSR -TR- 60 -7 3
25
R-6
14
AFOSR -TR -60 -90
112
BuMed MR005. 15-0002. 7,
AFOSR-TR-60-98
64
R-2
13
AFOSR-TR-60-101
1
BuMed MR005. 15-0002. 7.
AFOSR-TR-60-109
25
R-10
16
AFOSR-TR-60-112
65
BuShip8-371-V-19
90
AFOSR-TR-60-116
96
CAL-VG-1196-G-6
81
AFOSR-TR-60-117
90
CAL-VG-1196-G-7
80
AFSAM-60-22
22
CCL-96
24
AFSAM-60-42
15
ConvalrTM-349-19
118
AFSAM-60-62
20
CRDLR-2380
97
AFSAM-60-73
20
CRDLR-3000
84
AFSWC-TR-59-44
101
CRDLR-3002
39
AGC TN-28
63
CRDLR-3006
39
AIL-4600-1
41
CRDLR-3007
13
AIL-7356-1,1.2
41
CRDLR-3009
57
AIR-33-59-FR-218
6
CRDLR-3010
20
AN/FRC-47(XD-1)
48
CRDLR-3013
13
ACHEL TM-12-60
58
CRDLR-3016
19
APG/TAT/60-A-1, FR
57
CRDLR-3020
99
APL/JHU BB-291
103
CU-3-60
76
ARA-708
57
CU-4-60
107
ARF-1149-2
41
CU-5-60
107
ARF-2172-6
92
<nJ-6-60
107
ARL-TR-60-307
94
CU-7-60
108
ARPA Order -26- 59
35
CU-11-59
77
ASRDL-2112
42
CU-12-59
76
ASRDL-2122
34'
CU-13-59
77
ASRDL-2123
101
CU-14-59
77
ASRDL-2125
104
CU-14-59
78
ASRDL-2129
2
CX-49
108
ASRDL-2131
34
DASA-352
40
ASRDL-2132
41
DASA-1157
58
ASRDL-2134
42
DASA-1176
58
1-35
Number
DCL E-452
DDI-115
Da-n6
DMIC-137
DMIC-46I .
DMIC M-65
DMIC M-66
DMIC M-68
IX)FL TR-613
DOFLTR-?:?
DOFL TR-8- 1
DOFL TR-8'3
DOFL TR-8>7
DOFL TR- 8; 6
DOFLTR-819
DOFLTR-Sdo
DOFLTR-843
DOFL TR-847
DSR-7433-3
DSR 5-7476
DTMBC-175
DTMB-1015
DTMB-1170
DTMB-1347
EE-466
EERL-6-37
EES-040-04(jF
ENCR-45
EP-133
EP-137
ERL-97
ERL-98
ETT-728
Fritz-278. 1
FRLTN-2
FRLTN-3
FRLTN-12
FRL-TR-3
FRL-TR-5
FRL-TR-8
FRL-TR-U
FRO-200/10
FZK-9-140
GASLTR
GRD-TR-eO-
GTR
HE-150-183
HEI M-809
HH ARD-257
HSR RM 59/
HSR RM 59/
HSR TM 59/
HSR RM 59/
HSR TN 59/7
IER-60-258
IER-60-26I
IER-60-263
lER -60-293
IER-82-12
IER-128-5
IER-131-6
ILU DCL -95
IRL-128 I
IRL-137
LFE-570-A1
14$
296
^3
SM
SM
6-SM
SM
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as
;7
45
88
88
92
66
70
93
92
86
45
45
45
37
58
45
44
37
110
95
26
6*
62
88
62
43
81
67
80
5
103
47
47
64
83
59
59
59
59
59
68
60
72
101
86
108
100
118
81
38
121
121
121
121
121
47
47
47
108
89
118
83
77
31
119
81
Number
LIRTR-144
LL-36-44
LL-54-19
LL-58-2
LL-22G-O021
LL-25G-0004
LL-25G-0017
LL-52G-0013
LL-53G-0040
LL-54G-0027
LL-55G-0027
LL-58G-0011
LL-58G-0013
LL-82G-0021 I
LLTR-102
LLTR-164
LLTR-172
LLTR-183
LLTR-184
LLTR-179
LLTR-195
LLTR-204
LLTR-205
LLTR-206
LLTR-207
LL TR-2D9
LLTR-210
LLTR-212
LLTR-217
LLTR-219
LL TR-221
LMSD-2466
LMSD-2702
LMSD-5106
LMSD-48 407-48 408
LMSD-48 456
LMSD-49 730
LMSD-49735
LMSD-49-771
LMSD 288 003
LMSD 228 140, v. 1
LMSD-288 140, v. 2
LMSD-311 695
LMSD-703 043
LMSD-703 049
LMSD-703 060
Lock SB-60-1
Meteor - 34
Meteor -39
MH Aero R-ED 28030
MIP engine
ML(UM)59 137
ML(UM)59-160
ML(UM) 59-182
ML(UM)59-211
ML(UM) 59-230
ML(UM) 59-242
ML(UM)60-1
ML(UM)60-020
ML(UM)60-106
MRN-136
MRN-209
MRI R-778-59
MRL(OMRO)-78
MRL(OMRO)-79
1-36
Page
111
48
9
9
60
48
49
78
HI
82
78
82
9
119
48
111
48
120
49
49
78
49
49
48
49
49
50
82
82
78
50
69
65
65
65
65
111
65
65
65
65
65
65
50
61
71
50
89
87
52
65
74
39
74
74
74
74
68
74
68
100
100
52
112
112
Number
MRL(OMJRO)-80
MRL(OMRO)-81
MSEE-53-33
MUPTR-182 .
MUPTR-185-a
MUPTR-193, vol.
MUPTR-193, VOL
Pai
MUPTR-194
MUPTR-195 ' .
NADA-MA-6020 .~
NADA-MA-6025 ' '
NADA-MA-L6018
NADA-MA-L6021 ,
NAMC AEL-1108
NAMC AML(M)-595
NARF-58-i8T
NARF-58-19T
NARF-59-32T
NAVDOCKS TP-Te-6
NAVORD-1234
NAVORD-5894
NAVORD-5957
NAVORD-6726
NAVPERS- 10786
NAVSHIPS-250-346-3
NAVTRADEVCEN 348-2
NAVTRADEVCEN 558-1
NAVWEPS-6005
NAVWEPS-7076
NAVWEPS-7086
NBSTN-18-3
NBSTN-18-4
NBSTN-18-5
NBSTN-64
NBS TN-67
NBSTN-70
NBS TN-72
NBSTN-73
NBSTN-74
NBS TN-77
NEL-258
NEL-478
NM 11 02 12.4. R-9
NMI-9404
NOLC-457
NOLC-514
NOTS-294
NOTS TP-2041
NOTS TP-2486
NOTS TP-2497
NRL-5499
NRL-5501
NRL-5506
NRL-5513
NRL-5516
NRL-5517
NRL-5520
NRL-5548
NRL-5553
NSF G-4951
NSF G-5754
NSF G-5939
NSF G-y/9. 7/79
NSF G-Y/9. 14/139
NSL-441
112
112
82
115
115
98
98
115
115
16
13
14
14
35
94
100
100
101
101
39
71
61
89
97
75
41
10
122
31
61
120
120
120
82
112
23
120
26
102
52
32
53
36
96
61
122
39
71
31
61
52
71
91
104
92
96
91
52
71
10
123
119
33
33
lis
8P
1-C
Number
NSRE«'-45
HWL-1715
I11IL-1722
<)NR-7
OORR-1510
OORR-2304
OORR-2360
OORR-2360
0RDM7-230
0SURF-398-F
OBURF-798-8
OSURF -896-1
0gURF-ia73-l
OSW RWR-43
06W RDPR-44
OTAC LL-55
OTAC LL-57
OfrS-SB-421
OrS-SB-422
OrS-S8-424
CrrS-SB-425
onrs-sB-426
OrS-SB-428
PA TR -22 37
PA TR- 2703
n 146 395
n 146 402
n 146 750
IB 147 100
ni47 175
ni47 588
n 147 743
11147 744
IB 147 745
IB 147 746
IB 146 780-4
IB 147 832
!-p.l^
IB
PB
IB
IB
IB
IB
IB
IB
147 838
147 908
148 063
148 125
148 178
148 197
148 199
148 225
18148 254
PB
IB
IB
IB
IB
IB
IB
PB
IB
IB
IB
IB
IB
IB
IB
148 255
148 256
148 257
148 258
148 259
148 260
148 262
148 263
148 264
148 267
148 268
148 269
148 274
148 319
148 368
IB 148 647
IB 148 662
IB 148 689
IB 148 830
Page
103
65
61
53
98
23
100
108
70
122
10
113
41
39
40
67
67
23
23
91
27
116
53
70
59
52
71
47
12
33
78
17
14
16
18
115
104
116
117
76
33
89
122
79
60
106
35
31
34
S
80
4
30
31
66
33
10
12
36
S
49
99
99
16
112
Number
PB 148 870
PB 148 914
PB 148 916
PB 148 917
PB 148 918
PB 148 919
PB 148 972
PB 149 007
PB 149 246
PB 149 295
PB 149 547
PB 149 593
PB 149 707
PB 149 713
PB 149 773
PB 149 849
PB 149 960
PB 150 089
PB 150 096
PB 150 100
PB 150 101
PB 150 160
PB 150 170
PB 150 207
PB ISO 213
PB 150 214
PB ISO 215
PB 150 216
PB 150 218
PB ISO 219
PB 150 229
PB 150 230
PB 150 280
PB 150 282
PB 150 318
PB 150 329
PB 150 331
PB ISO 332
PB 150 334
PB 150 335
PB 150 336
PB 150 346
PB ISO 347
PB 150 349
PB 150 351
PB 150 361
PB 150 368
PB 150 369
PB 150 371
PB 150 372
PB 150 374
PB 150 378
PB 150 390
PB 150 406
PB 150 407
PB 150 412
PB 150 413
PB ISO 415
PB 150 416
PB 150 417
PB 150 418
PB 150 420
PB 150 421
PB 150 424
PB 150 429
Page
Number
38
PB 150 430
59
PB 150 431
59
PB 150 432
112
PB 150 436
112
PB 150 437
112
PB 150 438
55
PB 150 439
.
2
PB 150 440
20
PB 150 441
84
PB 150 442
' 58
PB 150 443
81
PB 150 444
54
FB 150 445
: V 56
PB 150 446
1 ' 50
PB 150 447
'-
52
PB 150 448
l' 59
PB 150 449
24
PB 150 450
108
PB 150 451
84
PB 150 452
^
39
PB 150 454
41
PB 150 456
28
PB 150 457
20
PB ISO 458
16
PB 150 459
18
PB 150 461
15
PB 150 466
-
11
PB 150 467
13
PB ISO 468
15
PB 150 470
18
PB 150 471
17
PB 150 472
94
PB 150 473
72
PB 150 474
[
45
PB 150 475
58
PB 150 476
89
PB 150 477
66
PB ISO 478
25
!B 150 479
28
PB 150 480
1
26
PB 150 481
86
PB 150 482
87
PB 150 483
100
PB 150 484
98
PB 150 486
8
PB 150 487
88
PB 150 488
9
PB 150 490
97
PB 150 491
7
PB 150 492
108
PB 150 493
108
PB 150 494
.
71
PB 150 495
98
PB 150 496
23
PB 150 497
68
PB 150 498
106
PB 150 501
108
PB 150 503
-
83
PB ISO 504
34
PB 150 507
121
PB 150 508
30
PB 150 509
35
PB 150 511
1Q5
PB 150 514
107
PB ISO 515
107
107
108
40
31
49
14
14
16
13
113
32
32
54
115
52
55
107
2
34
58
61
57
25
62
29
79
95
95
93
17
8
99
117
11
80
80
88
88
90
79
78
6
81
118
33
20
8
75
55
55
104
122
80
33
7
110
9
9
119
82
78
47
80
24
1-37
Number
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
t»B 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB150
PB 150
PB 150
PB150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
SB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB 150
PB ISO
51*
517
518
519
521
522
523
524
525
526
527
528
529
531
532
536
537
538
539
540
541
542
543
544
547
548
552
556
557
560
561
562
563
564
565
566
567
568
569
570
571
572
573
574
575
576
577
578
592
593
594
595
597
598
599
600
601
603
606
608
609
610
til
612
613-1
^ge
Number
101
PB 150 613-2
2
PB 150 614
97
PB 150 615
24
PB 150 616
77
PB 150 617
76
PB 150 620
100
PB 150 621
83
PB 150 626
114
PB 150 627
105
PB 150 628
11
PB 150 629
88
PB 150 631
34
PB 150 633
85
PB 150 634
118
PB 150 637
27
PB 150 638
113
PB 150 639
24
PB 150 641
27
PB 150 644
89
PB 150 645
111
PB 150 646
9
PB 150 647
110
PB 150 648
110
PB ISO 649
110
PB 150 650
73
PB 150 651
43
PB 150 652
115
PB 150 663
115
PB 150 664
19
PB 150 665
19
PB 150 666
22
PB 150 669
15
PB 150 671
17
PB 150 673
16
PB 150 678
18
PB 150 679
17
PB 150 680
14
PB 150 681
21
PB 150 683
17
PB 150 684
63
PB 150 686
15
PB 150 687
2
PB 150 733
20
PB 150 734
22
PB 150 735
18
PB 150 736
16
PB 150 737
16
PB 150 738
49
PB 150 740
49
PB 150 741
48
PB 150 747
49
PB 150 748
49
PB 150 749
82
PB 150 753
82
PB 150 754
78
PB 150 755
SO
PB 150 757
111
PB 150 762
87
PB 150 764
48
PB 150 765
' 49
PB 150 766
120
PB 150 767
67
PB 150 768
67
PB 150 769
65
PB 150 770
sss.
Number
M
^^T-
65
PB 150 771
1
PB 150 772 ,
1
PB 150 773
1
PB 150 774
31
PB 150 775
85
PB 150 776 .
85
PB 150 777 ■'
61
PB 150 778
28
PB 150 783
109
PB 150 784 * ^
116
PB 150 788 . ,
68
PB 150 794 . •,
112
PB 150 796
84
PB 150 799
96
PB 150 801
10
PB 150 802
10
PB 150 804
77
PB 150 805
105
PB 150 806
46
PB 150 809
78
PB 150 810 ,
62
PB 150 811
43
PB 150 812
81
PB 150 813
119
PB 150 814
114
PB 150 815
79
PB 150 816
39
PB 150 817 r
57
PB 150 818
20
PB 150 819
HI
PB 150 820
119
PB 150 822
21
PB 150 823
HI
PB 150 825
48
PB 150 830
47
PB 150 831
109
PB 150 834
41
PB 150 835
51
PB 150 836
58
PB 150 837
109
PB 150 838
101
PB 150 839
58
PB 150 842
117
PB 150 843
120
PB 150 850
51
PB 150 851
88
PB 150 852
118
PB 150 853
41
PB ISO 854
2
PB 150 855
60
PB 150 856
103
PB 150 858 I
114
PB 150 859
35
PB 150 861
45
PB 150 862
27
PB 150 867
HI
PB150 868
118
PB 150 870
53
PB 150 871
31
PB 150 872
32
PB 150 873
82
PB 150 874
74
PB 150 875
39
PB 150 876
74
PB 150 877
Pay
74
74
74
74
74
9«
64
103
38
Ul
19
9
4«
60
5
87
43
48
45
51
51
113
113
44
44
43
44
43
122
123
107
107
56
59
60
60
63
66
121
121
121
121
90
53
95
10
10
88
14
95
19
25
10
65
29
31
63
26
89
103
35
IX
52
61
94
1-38
Number
PB 150 879
PB 150 880
PB ISO 882
PB ISO 883
PB 150 886
n ISO 890
PI 150 891
PB 150 892
PB 150 917
PB 150 925
PB ISO 926
PB ISO 927
PB ISO 928
PB 150 929
PB 150 930
PB ISO 931
PB 150 932
PB 150 933
PB ISO 934
FB ISO 935
PB ISO 936
IB ISO 937
n ISO 938
PB 150 939
PB ISO 940
PB ISO 941
PB 150 942
PB ISO 943
PB ISO 944
PB 150 945
PB 150 949
FB 150 951
FB ISO 952
PB 150 954
FB 150 955
FB ISO 957
FB 150 958
FB 150 959
FB 150 962
FB 150 963
FB ISO 964
FB 150 969
PB 150 970
PB 150 972
FB 150 973
FB 150 975
FB 150 985
FB 150 988
FB 150 989
FB ISO 991
11150 992
11150 993
FB 150 998
FB 150 999
PB 151095
PB 151 096
PB151 377-3
PB151 377-4
PB151 377-5
PB 152 000
PB 152 001
PB 152 002
PB 152 003
II 152 026
» 152 027
Page
Number
119
PB 152 028
t 105
PB 152 029
65
PB 152 030
77
PB 152 031
61
PB 152 032
118
PB 152 033
lis
PB 152 035
103
PB 152 036
91
PB 152 039
62
PB 152 040
11 4
PB 152 041
^ 105
PB 152 045
120
PB 152 047
30
PB 152 049
30
PB 152 050
I 52
PB 152 051
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PB 152 053
4
PB 152 054
4
PB 152 055
4
PB 152 056
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PB 152 057
98
PB 152 058-1
3
PB 152 058-2
3
PB 152 059
3
PB 152 062
2
PB 152 066
2
PB 152 067
3
PB 152 068
100
PB 152 070
108
PB 152 071
108
PB 152 073
78
PB 152 077
90
PB 152 087
68
PB 152 088
117
PB 152 089
58
PB 152 092
42
PB 152 095
58
PB 152 096
73
PB 152 097
44
PB 152 098
63
PB 152 099
115
FB 152 100
59
PB 152 101
65
PB 152 103
83
PB 152 104
9
PB 152 106
36
PB 152 107
117
PB 152 108
61
PB 152 109
' 116
FB 152 110
80
PB 152 111
78
PB 152 113
67
PB 152 115
67
PB 152 118
66
FB 152 122
92
PB 152 123
120
PB 152 124
120
FB 152 126
120
FB 152 130
97
FB 152 131
13
PB 152 132
13
PB 152 134 .
19
FB 152 136
50
FB 152 138
71
PB 152 139
Number
12
12
12
13
18
13
122
110
64
42
48
81
86
79
31
120
76
3
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34
3
98
98
119
61
77
77
118
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24
25
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77
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77
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77
122
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116
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57
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103
27
64
46
29
104
14
87
FB
152 140
PB
152 142
PB
152 143
PB
152 144
PB
152 146
PB
152 151
PB
152 152
PB
152 153
PB
152 155
PB
152 170
PB
152 172
PB
152 173
PB
152 175
PB
152 176
PB
152 177
PB
152 178
FB
152 183
PB
152 185
PB
152 187
PB
152 188
FB
152 189
PB
152 190
PB
152 191
PB
152 192
PB
152 193
PB
152 194
PB
152 195
PB
152 197
PB
152 200
PB
152 233
PB
152 273
PB
152 289
PB
152 292
PB
132 294
PB
152 295
PB
152 296
PB
152 297
PB
152 298
PB
152 299
PB
152 300
PB
152 309
PB
152 310
PB 152 311
PB 152 312
PB 152 313
PB
152 314
PB
152 315
PB
152 350
PB
152 351
PB
152 352
PB
152 353
PB
152 354
PB 152 355
PB
152 356
PB
152 357
PB
152 358
PB
152 359
PB
152 360
PB
152 361
PB
152 416
PB
152 590
PB
152 614
PB
152 615
PB
152 616
PB
152 640
Page
41
6
83
109
121
94
28
64
64
90
122
86
75
76
76
7
55
113
45
42
34
104
41
42
29
42
30
66
57
97
30
78
79
75
48
36
70
103
102
5
45
110
44
86
37
45
37
38
70
39
22
70
40
89
87
100
100
46
57
89
75
56
53
119
21
1-39
Number
PB
PB
FB
PB
PB
FB
PB
PB
PB
PB
PB
PB
PB
Pb
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
PB
FB
PB
PB
PB
PB
PB
PB
PB
FB
PB
PB
PB
FB
PB
PB
PB
PB
PB
PB
PB
FB
FB
FB
FB
FB
FB
FB
FB
FB
PB
FB
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
152
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
161
171
171
171
171
171
171
171
171
171
171
X71
641
642
643
644
645
646
647
648
649
650
651
657
667
676
677
678
680
681
752
753
755
796
797
802-
802-)
805
806
807
855
093-
215
216
218
288
371-
371-
565
568
571
573
574
575
576
578
696
749
764
767
800
863
890
921
947
989
026
028
030
031
039
040
053
054
055
056
057
Page Number
35 PB 171 058
07 PB 171 059
92 PB 171 060
102 FB 171 061
32 FB 171 062
102 FB 171 063
36 FB 171 064
97 PB 171 065 ,
97 FB 171 066 I
101 PB 171 067
82 FB 171 068
43 FB 171 069
47 PB 171 070
106 PB 171 071
99 PB 171 072
114 PB 171 073
92 PB 171 074
90 PB 171 075
36 PB 171 076
54 PB 171 077
72 PB 171 078
56 PB 171 079
62 PB 171 080
84 FB 171 081
84 PB 171 082
69 PB 171 083
101 PB 171 084
62 PB 171 085
22 PB 171 086 I
58 PB 171 087 t
70 PB 171 088
93 PB 171 089
92 PB 171 090
123 PB 171 091
22 PB 171 092
22 PB 171 093
82 PB 171 094
112 PB 171 095
23 PB 171 096
120 PB 171 097
26 FB 171 098
102 PB 171 099
106 PB 171 100
52 PB 171 101
91 PB 171 102
96 FB 171 103
92 FB 171 104
91 PB 171 105
62 PB 171 106
68 PB 171 114
53 PB171 115
71 PB 171 116
75 PB 171 117
91 PB171 118
45 FB 171 119 ,
38 FB 171 120 I
39 FB 171 121
40 FB 171 122
69 PB 171 123
39 PB 171 124
5 PB 171 125
39 PB 171 126
71 PB 171 127
92 PHS G-HTS 5147
69 PIB-706
<
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Page
74
53
90
69
73
72
96
91
95
29
38
56
83
83
21
19
70
6
37
92
76
25
81
69
93
96
95
94
94
36
93
73
38
101
81
80
37
41
75
23
40
94
82
69
54
28
85
51
1
61
72
37
47
46
iq2
99
114
23
123
99
55
54
SO
13
52
Number f^
PIBAL-552 17
PIBAL-560 N
PLASTEC-1 . 75
PPL-TR-60-6 in
FSI-3000:21-2-Q us
PSI-3000:21-3-Q m
QPEA MRS-6002 1(3
QFEA R-7 lOj
R60SD391 $
R60SD-399 a
R60SD-4O9 IM
R60SD-410 87
RADCTN-60-146 gj
RADCTN-60-168 52
REA-6 32
RBA-19 31
REA-25 31
RIAL-49-1236 75
RIAL-59-4921 75
RLF-3828-3 31
Rocket R-2S65 (6
RPI Math Rep -28 »
RS-2 2
S/TD-1232 66
S/TD-1735, v-4 6J
S/TD-1855 ^
SELTR-2C7-2 II
SELTR-404-1 ,
SELTR- 1502-1 114
SELTR-2051-1 55
SELTR-2101-1 55
SELTR- 2102-1 56
SEP-TR-59-104-205-704. 3 <H
Shell S-13649 72
SIM-25 U
SIO-60-14 3J
SIO Rel-53-33 106
SM-60-6 93
Sperry-NA-8210-8199 116
Squid CAL-79-P 85
Squid Mrr-22-P 111
Squid PR-67-P, Suppl. 64
Squid PR- 67 -P- A. Suppl. 64
Squid PR-67-P-B 64
Squid SRI-5-P , 21
SRI -2231 I 56
SRI-2994 j 35
SRI -SU -2625 ' 21
SRI -SU- 3223 21
STL/TR-60-0000-00263 65
STL/TR-60-0000-09226 HI
STL/TR-60-0000- 19258 91
STL/TR-60-0000-GR-269 lli
SUDEM-124 M
SUI-59-11 J
SUl-59-22 2
SUI-59-23 , ^
TAM-152 56
TAM-153 60
TAMC Ref-59-24T 3!
TAR-TN-59-1 79
TEDADC AE-1412.1 M
TED ADC ES -7045(591 5 -M) 13
TED ADC RS-7045(59i5. M) 16
TED NAM -04614 35
TED NAM AE 1403. 1 W
1-40
Number
TED NAM -PP- 375
TRG-127-SR-2 jl
TSR-112 ^
UMRI-2065-1-F
UMRI-2096
UMRl-2406 j
UMRI-2597
UMRI-2782-1-F '
UMRI-2873-5-F
UMRI-03554-1-S !
USCEC -71-101 j
USCEC-7 1-202
USCEC -79-201
USNRDLTR-361
L5NRDL TR-364 |
USNRDLTR-399 '.
WADCTN-58-163
MDCTN-58-259.
superseded
WADCTN -59-326
WADC-TR-57-240. pt, 2.,
unclassified ^
WADC-TR-57-622
WADC-TR-58-468
WADC-TR-59-29. pt. 2
WADC-TR-59-63. pt. 2
Page
Number
Page
Number
Page
35
WADC-TR-59-416,
pt.2
93
WAW3-TR-60-244
69
120
WADC-TR -59-736,
pt.2
71
WADD-TR-60-273
95
73
WADD-TN-60-75
46
WADD-TR-60-286
47
40
WADD-TN-60-83
•
5
WADD-TR -60 -293
99
51
WADD-TN-60-88
•
39
\\^DD-TR-60-294
73
51
WADD-TN-60-89
76
WADD-TR-60-308
83
51
WADD-TN-60-115
>>
25
WADD-TR-60-352
72
96
WADD-TN-60-200
37
WADD-TR -60 -360
83
35
WADD-TN-60-230
102
WADD-TR -60 -37 6
21
51
WADD-TR-59-326
102
WADD-TR -60 -388
19
120
WADD-TR-59-486.
pi. 4
115
WAIX)-TR-60-426
96
117
WADD-TR -59-728
5
WADD-TR-60-473
70
117
WADD-TR -60-32
96
WADD-TR-60-493
6
102
WADD-TR -60 -42
95
WAL- 119/1
91
102
WADD-TR-60-74,
pt.1
94
WAL-130.5/1 "*
91
99
WADD-TR -60-74,
pt.2
94
WAL- 161. 85/1
62
37
WADD-TR -60 -106
36
WAL -893. 3/3
84
WADD-TR-60-116
93
WHOI ref. 59-54
34
102
WADD-TR-60-120
92
WHOI ref. 59-58
80
92
WADD-TR -60- 150
73
WHOI ref. 59-59
90
WADD-TR-60-157
69
WHOI ref. 60-3
33
69
WADD-TR -60- 188
38
WIS -86: 2439
122
81
WADD-TR -60 -198
74
WR-473
43
46
WADD-TR -60- 199
56
WU Ref. 58-32
33
69
WADD-TR -60 -233
53
WU Ref. 59-28
33
91
WADD-TR -60 -240
90
1-41
! ■ \.
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^
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J
U. S. DEPARTMENT OF COMMERCE FIELD OFFICES
SERVE THE BUSINESS COMMUNITY
The D<parim<-nt of Commerce maintains Field Offices to enable the business community to
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OTF CIAL BUSINESS
*«»<AtTT row PNIVATC use TO AVOlt
PAVMKNT or M>*TAaC. (JOO
I ■
^. (^orrnnnrtil
Wmn
EPORTS
I
February 10, 1961
VoL 35. No. 2
. . . A monthly listing ci
Government research reports
available to industry . . .
pthis issue:
cw«m»«tnr
) U^S'
Eplosive Metalworking (PB 161 221)
joining of Tungsten (PB 161 224)
lods and Materials for the Preserva-
tion of Small Hardware Items
(PB 161 897)
ly Research Task Summary, Fiscal
Year 1960, Vols. 1-6 '
(PB 171 000-PB 171 005)
itomated Maintenance: Theory, Prac-
|tice, and Impliutions for Training
r(PB 171 137) ;
itic and Impact Bendiog Tests of Glued
[Laminated Wood (PB 171 166)
»
^nding Preservative-treated Veneers
[(PB 171 167)
>lded Composite for Boat Hulls
[(PB 171 168)
janic Semiconddetor Study (PB 171 177)
Complete list of printed reports
begins on page Hi
'rM
1
jl
/^
^1
f,y<«^«ft^S'\yvr
U. S. DEPARTMENT OF COMMERCE
BUSINESS AKD DEFENSK SERVICES ADMINlSTlATION
Off>c« of T»clinical Services
The PB l^eports - . .
i announced in this pubikxion
*<l. usttally by agencies of the U. S.
Government, for ditsemination to the public. In moat
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The Office of Tec inical Services is reaponaible, under
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H
OW
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er
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U.S. GOVERNMENT RESEARCH REPORTS
VJS. DEPARTliENT OF COMMERCE
Lather H. Uodgea, Socretair
l»eme4 moi^fhlff
remittemre
olHee or to Sui
BUSINKSB AND DEFENSE 8EBVICES ADMINISTRATION
Williaai A. Whit*, br^ Aemlmutratmr ^
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Jaha C. Gr««a. DirtUr
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he tent to Superintendent of Dorumentti.
Um W htmet l«r prtnttaf iMt p«fcllcaM«« a#^*T«^
I
^
CONTENTS
nUKTH) REPORTS AVAE.ABLE FROM OTS ANNOUNCED IN THIS ISSUE
BBJOGRAPHY :
ASTRONOMY , ..........'.
Aatrophyslcs
BB4AVI0RAL SCIENCES ...^ !!!!!.*!!!'..".!!
Hionan Engineering .'
Personnel and Training
Paychology.
Pai
W
BOLOaCAL SOENCES
Anatomy and Riyalology
■ochemlstry
Neurology and Paychlacry ,
fUDoio^y •••• •• •••••«•••••••..<
Phamucology and Toodcology . . , ,
Radioblology ,
CHEMISTRY
Analytical Chemistry ,
Inorganic Chemistry
Organic Chemistry
Physical Chemistry
EARTH SCIENCES ,
Climatology and Meteordlogy . . . ,
Frost Science
Geodesy
Geography
Physics of the Atmosphere
BNGINEERING
Aeronautical Engineering
Chemical Engineering . . ,
QyU Engineering
Electrical and Electronic Engineering
Ordnance, Missiles, and Satellite Vehicles
Sanlunon and Safety Engineering
Ship Building
FOOD. HANDLING, AND PACKAGiNG EQuiPMENT
Packaging
• • • • • • <
MACHINERY. FABRICATION. AND ACCESSORY EQUIPMENT
Engines and Propulsion Systems
MATERIALS
Ceramics and Refractories
Fuels. Lubricants, and Hydraulic Fluids
Leather and Textiles
PWnts and Finishes
Plastics
Wood and Paper .-
MATHEMATICS '.
Computlivg Devices
MECHANICS i
Aerodynamics and Pneumatica
METALLURGY
Ferrous Metals , ,
Light Metals
Structural Metallurgy and Corrosion
JWCLEAR PHYSICS AND NUCLEAR CHEMISTRY
Blemenury Particles
hutruments and Installations
Nuclear Engineering and Power
Nuclear Reactions
Radioactivity :
KRSONNEL SUPPLIES AND PERSONAL EQuin>4ENT
IHYSICS T
• ••••••• I
\-
131
131
131
133
133
134
135
138
138
140
142
142
143
143
144
144
13
146
149
149
151
153
153
154
157
157
160
161
161
172
176
176
176
176
177
177
178
179
179
180
181
181
182
184
189
192
193
197
199
200
201
202
202
202
203
203
205
205
205
R*
58^
Acoustics ... J 207
Electricity an<i Magnetism 208
Electronics * 209
Molecular Physics and Spectroscopy 210
Solid State Physics ...' ., 214
Theoretical Physics i... .!!..!!..!.!!!.! 217
Thermodynamtcs .j ."!!*.!!*. 219
Wave Propagation j...... 222
RESEARCH METTHCDS. TECHNIQUES AND EQUIPMENT '.'.'..['.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'. 222
Information Theory i !!..!.,.!.!].! 223
Photographic Equipinent ^ ^ 223
SOOAL SCIENCES .- '. 224
MISCELLANEOUS
ATOMIC ENERGY COMMISSION REPORTS
GENERAL
BIOLOGY AND MEDICINE
CHEMISTRY L •
General ... I •
Radiation and Radiochemistry
Separation Processes for Plutonium and Uranium
CONTROLLED THERMONUCLEAR PROCESSES
CRmCALITY STUDIES • • •;•
EQUIPMENT, METHODS AND TECHNIQUES
GEOLOGY AND MINERALOGY
HEALTH AND SAFETY
INSTRUMENTS
ISOTCffE SEPARATION
METALLURGY AND CERAMICS -^ * " •;~;v^c
NUCLEAR EXPLOSIONS - PEACEFUL ^PPL CA-nONS .^.^^ •
PARTICLE ACCELERATORS AND HIGH-VOLTAGE MACHINES.
PHYSICS AND MATHEMATICS
RADIATION EFFECTS ON MATERIALS
RADIOACTIVE WASTE
REACTORS
General .
Power . . .
TECHNOLOOY
Feed Materials
SOURCE INDEX
SU^ECT INDEX
NUMBER INpEX
225
225
225
W
227
234
234
240
241
241
244
245
248
252
252
253
253
253
254
254
254
254
255
2SS
255
M
Ml
1-29
^O^
tt
Printed Reports Available from 075 Announced in This Issue
BBIAVIORAL SQENCES
Page
Bffects of varriations in specificity of knowledge of results on the
improvement of a perceptual skill. Aug 60. 32p.
(PB 171 146) $1.00 135
Task and part -task trainers and training. June 60. 9Sp. t
(FB171139) $2.25 J. 133
BBUOGRAPHY
Perroelectriclty and ferromagnetism. Sep 60. 19p. i
(GTS SB-434) 10 cents ' 208
Machine translation. Oct 60. 5p. (OTS SB-439) 10 cents ^... 222
Powder metallurgy (supplement to CTR-343). Aug 60. lOp.
(OrrS SB-423) 10 cents 199
Thermionics and cathodes. Aug 60. lip. (OTS SB-431) 10 cents. ... ^ 168
Thermistors and resistors. Aug 60. lOp. (OTS SB -42^ 10 cents 168
Thermoelectricity. Sep 60. lOp. (OTS SB-432) 10 cents .-. 168
Thermopiles and thermocouples. Aug 60. 7p. (CIS SB-430) 10 cents 168
Transistors (supplement to CTR-31()). Aug 60. 13p.
(OTS SB-433) 10 cents 169
BOLOaCAL SaENCBS; I ' ^
Army research task summary, fiscal year 1960, Volume 1. Medical,
Uological, social and behavioral sciences. 436p.
(PB 171 000) $3. 75 138
biflilence at AET upon the uptake of iron-59 by the red blood cells at
gamma-lrradlated rates. May 60. I3p. (PB 171 160) 50 cents 143
Monitoring unit for heart- and respiration-rate. Aug 60. 9p.
(PB 171 140) 50 cents ;.. 139
CHEMISTRY f
Analysis of contaminants In aviator 's breathing oxygen. 19 Oct
60. 22p. (PB 161 946) 75 cents 144
Army research task summary, fiscal year 19tt). Volume 2.
Chemistry. 385p. (PB 171 001) $3. 75 , 144
Ignition stxjdles. Part VI. The effect of chemical structure on the
sponuneous ignition at hydrocarbons. 3 Nov 60. 31p.
(PB 161 967) $1. 00 148
Influence of double layer structure on the adsorption Isotherm of
palmitic acid. July 6D. 68p. (PB 171 141) $L75 147
Radiolysls of aralkyl ketones. Aug 60. 15p. (PB 171 156) 50 cents 147
Solutions for complex systems of chemical reaction kinetics. Part I.
An irreversible unimolecular reaction followed by a second irre- i '
verslble unimolecular reaction, Aug 60. 32p. (PB 161 408 S-1) $1. 00. 149
Structure of linear polymers: lower n -hydrocarbons. Oct 60.
98p. (PB 171 181) $2.50 145
BARTH SQENCES If j
Wbild maps of F2 critical frequencies and maximum usshle frequency
factors. Oct60. 247p. (PB 151 361-^ $3. 50 155
ENGINEERING i
Army research task summary, fiscal year 1960. Ycdume 5.
Engineering. 440p. (PB 171 004) $4.25
Automated maintenance: Theory, practice, aad implicatians for
training. Aug 60. 28p. (PB 171 137) 75 cents .a.
157
178
Hi
KNONEBRING (con. )
PB|B
170
170
170
DemineraMzatlon erf saline water by electrically-induced adsorption oo
poroufl graphite electrodes. Sep 60. 63p. (PB 171 129) J1.75 MO
Domestic air traffic control radio communication equipments. Distri- j
bution airborne and ground equipments, vcdume L Aug 59. 731p.
(PB 171 131) $8.00
Domestic air traffic control radio communication equipments. Tech- i
nical charadteristics airborne and ground equipmenu. Volume U.
Aug 59. 4Hp. (PB 171 132) .—
Domestic air traffic control VHP radio navigation equipments.
Distribution and technical characteristics airborne equipmenu.
Aug59. 58lp. (PB171130) TOO
General design criteria for an optimum family of fln-staUllzed sounding
vehicles. June 60. 44p. (PB 171 180) $1. 25 175
InvestigatioD of column action during creep buckling. June 60. 54p.
(PB 171 149) $1.50 161
Oblique incidence receiving antenna array for a relative ionospheric
opacity meter. Nov 60. 17p. (PB 161 579) 50 cents IM
Research on developing design criteria for anti-friction airframe
bearings fo< high temperature use. 1960. I38p. (PB 171 151)$2.75 159
Research on dw feasibility of the Undberg gyroscope principle. Aug
60. I22p. (PB 171 157) $2.75 175
Simulated combined vibration, sustained acceleration and extreme
temperature environments. Feb 60. 17p. (PB 171 134) 50 cents 172
System for recovery o* water from urine. Part IL Design, fabrication,
and testing of the prototype system. Aug 60. 35p. (PB 17 1 145) $1. 00 I*
Technical resources directory. Missile ground support equipment tio.
3. 1 Nov 60. 22p. (PB 161 535(Rcv. 1) 75 cents -. "*
Thermal protection of structural, propulsion, and temperature -sensl-
tive materials for hypersonic and space flight. July 60. 228p. i
(PB 171 147) $3.50 12
Thermloolcs and cathodes. Aug 60. lip. (OTS SB-431) 10 cents iw
Thermistors and resistors. Aug 60. lOp. (OTS SB-429) 10 cents ^ IM
Thermoelectricity. Sep 60. lOp. (OTS SB- 432) 10 cents Iw
Thermopiles and thermocouples. Aug 60. 7p. (CTTS SB-430) 10 cents » !••
Transistors (supplement to CTR-310). Aug 60. 13p.
(OTS SB-43D 10 cents IW
MACHINERY, FABRICATION, AND ACCESSORY EQUIPMEKr
Air Force Office at Sdcntlflc Research Contractors n»eeting (No. I)
on chemical kinetics at propulsion held at General Atomic Division
ol General Dynamics Corporation, San Diego, California, 6-7
September 1960. 1960. 37p. (PB 171 184) $1.00
177
MATERIALS
Application of temperature programmed gas chroooatography to
the analysis of lacquer solvents and thinners. 7 Oct 60. 12p.
(PB 17 1 033) 50 cents
Bending radii of dense, flat-sawn Douglas fir as aflected by slope d
grain and knots. 1 Sep 59. 26p. (PB 171 169) 75 cents IW
Bending radii of Tanalith- treated southern yellow pine as affeciBd.b]r
knot size. 1 Sep 59. 15p. (PB 171 170) SO cents
Bending radii of three thicknesses of Tanalith -treated black gum and
dense and qon-dense Tanalith -treated hickory. 1 Sep 59. ISp.
(PB 171 171) SOcOTte
Bonding preservative -treated veneers. May 60. lOp.
(PB 171 167) 50 cents
Deflection characteristics of a 20-foot-diameisr laminated wood ring
subjected to compressive loading along a diameter. Sep 59, 30p.
(PB 171 165) 75cents '•*
Development of non-oocidlc refractory foenu. Apr 60. 49p.
(PB 171 17a $1.25
181
183
183
182
17»
MATERIALS (coo.)
page
Development of shade standard and tolerances for USAF Blue 157
Tiylon- rayon poplin and polyvinyl butyral coated nylon twilL July '
60. 48p. (PB 171 153) $1. 25 , igi
Btfect of board thickness on bending radii or ekki. 14 Aug 59. 8p.
(PB 171 172) 50 cents ig3
Effect of board width on bending radii of white oak and Douglas fir.
lSep59. 12p. (PB 171 173) 50 cents 183
Effect of individual lamination thickness on the strength of curved
and straight white oak beams containing cross grain. 1 Sep 59. 47p.
(PB 171 174) $1.25 .*. ...: ^ 183
Effect of lamination thickness on shrinkage and swelling of white oak
laminates. 1 Sep 59. 23p. (PB 171 175) 75 cents 184
Filterability of distillate fuels. Part I. Development of methods and
effect of fUter porosity. 3 Nov 60. 23p. (PB 1 61 966) 75 cents 180
Fire-retardant coatings. 20 Oct 60. 24p. (PB 171 182) 75 cenu !.!!.*!.*!!.!.'." 181
Flame barrier characteristics of textile fibera. July 60. 41p.
(PB 171 136) $1.25 ISO
Molded composite for boat huUa. June 60. 4^. (PB 171 168) $1. 25 .............'..../....'.'.'. 182
OBtygen- alcohol test for insulating materials. A memorandum on a '
screening test for rocket-motor blast tubes. Oct 60. 32p.
(PB 161 948) $1.00 181
Ozone resistance of elastomerlc vulcanlzates at elevated temperatures
14 Sep 60. 19p. (PB 161 969) 50 cents 179
Refractory inorganic materials for structural applications. July 60.
95p. (PB 171 148) $2.25 179
Stttic and impact bending tests of glued laminated wood. Feb 60. 56n.
(PB 171 166) $1. 50 TT 182
Strength of curved and straight dense Douglas flr laminates as affected
by Individual lamination thickness. 1 Sep 59. 47p.
(PB 171 176) $1. 25 184
MATHEMATICS
184
189
Expected values of normal order statistics
(PB 171 161) $1.25
Test of a model dynamic system synthesizer. Feb 58. 17Sp.
(PB 171 144) $3.00 T.
MECHANICS
r-
An analytical study of the dynamics of spinning aircraft. Part HI.
Calculated and flight test spin characteristics of an F-1(X)F with
•trakes. Feb 60. 17 Ip. (PB 171 13^ $3.00 195
Creep collapse of long cylindrical shells under high temperature and
eaitemal pressure. Aug 60. 126p, (PB 171 152) $2. 75 1^
Dssign, calibration and simulation capability of the Rosemount [
Aeronautical Laboratories' high temperature hypersonic facility.
July 60. 45p, (PB 171 142) $L25 197
InteractloB effects of side Jets issuing from flat plates and cinders
alined witfi a supersonic stream. June 60. 72p. (PB 171 179) $2.00 175
On the evaluation of generalized aerodynamic forces for triangular
wings with subsonic leading edges. Aug 60. 93p. (PB 171 162) $2. 25 195
UBTALLURGY
■Inary anl ternary diagrams. Aug 60. 8:^. (PB 171 154) $2. 25
Qirrent nickel -base high-temperature alloys. 17 Nov 60. lOp.
(PB 161 223) 50 cents ;
Design information on 5Cr-Mo-V alloy steels (H -11 and 5 Cr-Mo-V
Aircraft steel) for aircraft and missiles (Revised). 30 Sep 60. 51p.
(PB 151 072-R) $1. 50 T7. r.
Effects of alloying elements in titanium. Volume A. Constitution.
15Sep60. 234p. (PB 151 094) $3. 50 jqI
Bqdosive metalworklng. 3 Nov 60. 30p. (PB 161 221) SO cents !...!.!..!.......!!! 198
199
198
199*
METALLURGY (coo.)
Aug 60. 148p.
Hi^ velocity qlectrlc accelerator systema.
(PB 171 138) $2.75 •••
High-velocity ■aecalworking processes based on the sudden release of
electrical etiergy. 27 Oct 60. 15p. (PB 161 220) 50 cents
Joining erf tung$ten. 24 htov 60. 6p. (PB 161 224) 50 cents
Methods and materials for the preservation of small hardware items.
2 Aug 60. t2p. (PB 161 897) 75 cents
Minimum tougkness requirements for high-strength sheet steel.
20 Oct 60. 21p. (PB 161 78Q 75 cents
Powder metalliirgy (supplement to CTR-34^. Aug 60. lOp.
(OTS SB-42J) 10 cents
Study o# the eflects of surface films on the mechanical properties of
metals. July 60. 34p. (PB 171 150) $1.00
Welding of colwmbium and columbium alloys. 24 Oct 60. 28p.
(PB 161 219| 50 cents
MISCBLLANE^MJS
Report of NRL Progress. Jan 61. (PB 171 314) $1. 25. $10. 00/year. . .
NUCLEAR PHYSICS AND NUCLBAR CHEMISTRY
Calculation of c<dlision cross sections by use of relaxation techniques.
Aug 60. 33^. (PB 171 163) $1.00
On the scattering of/rays by nuclei. Nov 60. 28p. (PB 161 584) 75 cents.
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT
Thermal analjisis of space sultB in orbit. May 60. 21p.
(PB 171 Ua 75 cents
PHYSICS
I
Army researcii task sunmiary, fiscal year 1960. Volume 3.^ Phyalca
(PartO- 4|6p. (PB 171 002) $3.75
Army research task summary, fiscal year I960. Volume 4. Physic*
(^rt II) and geophysical sciences. 470p. (PB 171 003) $3. 75
Emlssivity and emlttance, what are they? 10 Nov 60. I7p.
(PB i 61 22^ 50 cents
Ferroelectridty 4ndferromagnetl8m.Sep60. 19p. (OTS SB -434) 10 cents.
Measurement^ of the thermal properties of metals at elevated tempera-
tures. 11 May 60. 30p. (PB 171 185) 75 cents
Method to determine the thermal dlffusivity of metals at high tempera-
tures. 14 June 60. 22p. (PB 171 183) 75 cents
Organic semiconductor smdy. June 60. 67p. (PB 171 177) $1. 75
Quarterly radjo noise data, March, April. May 1960. 19 Oct 60. 69p.
(PB 151 377"-6) $L75
Pae
197
191 'I
aoo
199
aoi
198
2M
204
»2
305
ao5
206
217
208
219
218
212
221
RESEARCH METHODS, TECHNTQUES AND EQUIPMENT
Army research task summary,
technologies, mathematics,
(PB 17100^ $4.50
Machine translation. Oct 60. Sp
fiscal year 1960, Volume 6. Materials
and operations research. 44Sp.
(CrrSSB-439) 10 cents.
222
222
For your convenience OTS order blanks (Form TS-37) are
available on request from the OFFICE OF TECHNICAL SERVICES.
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
OFFICE OF TKHNICAl SERVICES
35. No. 2
Pages 131 - 2SS
FetMTuary 10, 1961
BIBLIOGRAPHY
I ■
Lockheed Aircraft Corp. , Sunnyvale, Calif.
GENERAL RESEARCH REPORT 1959. Jan 60. 10^.
360 refs. LMSD-288164; Ar>233 098.
Order from LC mi|5. 70, ph$l6. 80 PB 148 703
The work Is described in 18 sections corresponding to
the 5 major subject areas of : Physics, Flight Sciences
Chemistry, Mathematics, and Communications. Each
section is followed by a list of the pertinent external
ud internal publications and technical presentations.
In those cases where the work summarized has not yet
been published externally, detailed internal
rcpons have been completed or are in press. In al-
most all cases the work described is a continuation of
programs started in past years and is generally a part
of the projected program for 1960. (Author)
ASTRONOMY
Harvard Coll. Observatory, Cambridge, Mass.
HK3H- RESOLUTION PLANETARY PHOTOGRAPHY
WITH A BALLOON-BORNE TELESCOPE, by Gerard
de Vaucouleurs. Scientific rept. no. 1 on Contract
AF 19(604)3074. 1 Apr 59, 40p. 12 refs. AFCRC-TN-
59-243; AD- 211 480.
Order from LC miSS.OO, phS6.30 PB 148 669
The resolution limit in planetary photography is dis-
cussed from the point of view at the platform stabiliza-
tion and guidance requirements, assunUng optimum
performance of the optical system. The elementary
geometric approach involves the conventional Rayleigh
tolerance and corresponding Dawes resolution limit for
t given aperture, the magnification of the system
matching the conventional resolution of the photo-
graphic plate. For a 24-in. telescope this treatment
•Uggests that a stabilization to a few tenths of a second
of arc for periods of a few seconds ol time may be
Mfficient. (Author)
Astrophysics
Centro dl Studio per la Pisica Delle Microonde
(Italy).
ON METEOR ABLATICW IN THE ATMOSPHERE, by
Franco Verniani. Technical note no. 4 oh Contract
AF 61(052)227. Mar 60, 32p. 32 refs. AFCRL-TN-
60-981 .
Order from LC ml$3.00. ph$6.30 PB 152 212
The usually adopted theory of the meteoric ablation is
critically examined and improved. More approximate
expressions are given for the fundamental equations
ai the ablation. New methods are proposed for deter-
mining the effective lateiK heat of ablation and the
meteoric density. The use at these methods with some
experimental data of Whipple gives a mean value of the
effective latent heat of ablation of about 10^ joule /kg,
and moreover suggest the existence of two essentially
different types of nrv^teors: compact meteors (density
of about 2, 4 gr/cm^) and dustballs (density of about
0,2gr/cm3). (Author)
\
Harvard Coll. Observatory, Cambridge, Mass.
CLASSIFICATION OF SOLAR PROMINENCES. K.
1946, by Donald H. Menzel and F. Shirley Jones.
Scientific rept. no. 5 on Contract AF 19(604)4%2.
Mar 60, 5^. AFCRC TN-60-243; AD- 234 798.
Order from LC mi$3. 60, ph$9. 30 PB 148 713
A tabulation and analysis of the behavior classification
of prominences are presented as observed at the high
altitude observatory at Climax, Colorado, during the
year 1946. (Audior) (See also PB 144 958).
Palomar Observatory, San Di^o, Calif.
ASTROPHYSICAL RESEARCH IN SPACE, by Jesse L.
Greenstein. %>ecial technical rept. na 2 (Pre-print)
on Contract AF 49(638)21. 21 Sep 59, 15p. AFOSR TN-
59-907; AD- 226 328.
Order from LC mi$2. 40, ph$3. 30 PB 152 302
Report contains a brief review of the problems and
some of the findings which may result.
131
Saskatchewan l). [Canada]. '
BASIC RESEARCH OH AURORA AND AIR(XOW, by
D. M. Hunten and A. Vallance Jones. Final rept. FRB
on Contract AF 1 9(604) 1831. 30 Apr 60. 58p. 25 refs.
AFCRC-TR-60-i75.
Order from LC fu$3. 60. ph$9. 30 PB 152 281
Abstracts or suqunaries of all the publications and re-
ports are given. A brief discussion is given on the in-
struments in usa in the work with special emphasis on
instrumentation constructed. Modifications made to
the two photographic spectrographs are described and
a brief description is given of the high speed patrol
spectrograph. Jm account is given of the status c4 in-
vestigations on qie twilight emissions In the alrglow of
sodium, lithium, ionized calcium, potassium and nx>le-
cular oxygen. Results in the spectroscopy of aurora
include important work in the obtaining of high-disper-
sion spectra of 4unlit auroral rays and of type- A red
aurora. Observations erf the behaviour of the hydrogen
emissions in thei development of aurora as seen from
Saskatoon are discussed. New information has been
obtained on the ndght airglow spectra between 1. 0 and
4, 0 »! Determinations of temperature from aurotal
spectra and fron| night airglow spectra have been made.
i
Saskatchewan U- fCanada].
RELATIVE INTENSITY OF NITROGEN BAND SYS-
TEMS IN AURORA, by D. M. Hunten. Scientific rept.
no. BR-22 on Coftraa AF 19(604)1831. Dec 59, lOp.
12 refs. AFCRC5-TN-60-278.
Order from LCr^S 1.80. ph$ 1.80 FB 152 282
1
Relative intensities are derived for certain bands of
the following systems: N2 Vegard- Kaplan, first posi-
tive, and second positive; nJ first negativeand
Meinel. Already available auroral spears, most o<
them photoelectric, were used. Factors relating the
photon intensity <)f a band to that al the whole system
are derived or c<)llected, and used to find typical
relative photon intensities for each system. Much
better results could be obtained from spectra taken
especially for the purpose, and some of the calcula-
tions couid be rejFlned also. (Author)
SfMce Sciences "Lab. , General Electric Ckx .
Philadelphia. P*.
THE DYNAMIC STABILITY OF THE UPPER ATMOS-
PHERE OF VElfJS. by Jean L F. Klng.Hept. on Con-
tract AF 04(647)P69. Oct 60, 10 p. 4 refs. Technical
Information Series rept. R60SD453.
Order from LC tt\i%L 80, ph$l. 80 PB 152 464
I
The far-infraredl limb darkening curve measured by
Slnton and Strong is used to determine the thermal
stability of the o^cally accessible Venus atmosphere.
It is found that tile stmosphere above the obscuring
layer is convectiVely stable with a lapse- rate about
half that of the Vienus adiabatic lapse- rate. The ob-
served temperature decrease with height together with
the radiative heating pattern shows similarities to the
upper terrestrial troposphere and, conversely, argues
against the presence of a low, warm, ozone- generated
stratosphere. Tkese results which are inferred from
hard- won telescopic dau point up the need and useful-
ness at near-Veilus radiation probe measurements.
(Autbor)
Stanford Electronics Labs. , Stanford U. . Calif.
THE DETECTI(»I OF RADAR ECHOES FROM THE
SUN, by R. C. Barthle. Scientific rept. no. 9 on Con-
traa AF 19(604)2193. 24 Aug 60, 58p. 13 refs.
AFCRL TN-60-969.
Order from LC mi$3. 60, ph$9. 30 PB 152 391
During several periods in 1958 and 1959 experiments
were conducted for the purpose of obtaining a radar
echo from the sun. Using a 40-kilowan tranamltter,
coded sequences of transmitted pulses, a broadside
array at rhombic antennas, conventional receiving
equipment, and a detection process which included the
use of a digital computer, solar echoes were obtained
in April 1959. For the September 1959 trials s ran-
dom length sequence at transmitted pulses wss used
with a higher-gain antenna arrangement. Increased
solar activity during the period, along with equipment
difficulties, prevented realization of the anticipated
increase in the output signal -to- noise ratios. A study
of the correlation characteristics of adjacent fre-
quency bands in the solar-echo background-noise
spearum revealed correlation coefficients of con-
sistently high values. The results of this study were
used in a data reduction technique which resulted in a
n«t improvement of the output signal-to-noise ratios.
The improvement made possible by this technique was
sufficient to enable deteaion of radar echoes from the
sun in the September, 1959. trials with computed
error probabilities which are numerically smaller
than those obtained in the April 1959 trials.
Uppsala U. (Sweden).
THE DAILY VARIATION OF THE COSMIC RAY NU-
CLEONIC COMPONENT AT MURCHISON BAY AND
UPPSALA, by Arne Eld Sandstrdm, Eric Dyring. and
Stig Lindgren. Technical note no. 2 00 Contract
AF 61(514)1312. 8 Feb 60. 40p, 24 refs. AFCRC-1>I-
60-412.
Order from LC mi$3. 00. ph|6. 30 PB 152 204
In both places the monitors were of the standard pat-
tern with 12 propprtlonal counters filled with 97 per
cent enriched B"^F3. The first and second harnwnlcs
of the mean daily variation have been determined both
for yearly periods and for each sun rotation period.
Vector sum diagrams for the first harnvanics in the
latter case are Kiven covering the intervals 31 Aug. 1956
to 15 Aug. 1959 for Uppsala and 13 Sep. 1957 to
29 April 1959 for Murchison Bay. In some insunces a
considerable phase shift has taken place from one se-
quence of sun rotation periods to another. These phase
shifts were not contemporary at the two stations. The
first harnnnlc at the 12- month means displays a high
degree of constancy with only a small secular phase
shift. The amplitudes of the second harnrKxiics are
very small. Conditions are especially favourable con-
cerning the deviation in the earth's magnetic field of
the particles registered by the Murchison Bay monitor.
Accordingly it has been {wssible to determine the di-
rfction of the anisotropy with a fairly good accuracy.
The Murchison Bay records do not show any prominent'
phase shift with the Kp index. Concerning Uppsala,
days with [Kp] ^uuc * ^* ""y ^^^ ■ ^^^ ^*^" ''"^
of maximum tnan other days. There appears to be a
small but conaistent variation of the amplitude with
Kp index. (Author)
132
N
Uppsala U. (Sweden).
FIRST AND SECOND HARMONICS OF THE DAILY
VARIATION OF THE COSMIC RAY NUCLEONIC
COMPCWENT AT UITSALA AUG 31. 1956 TO
AUG. 31. 1957, by Arne Eld SandstrOm and Stig
Llodgren. Technical note no. 1 on Contract
AF 61(514)1312. 21 Apr 59. I9p. 11 refs. AFCRL- TN-
60-663.
Order from LC ml$2. 40. pb$3. 30 FB 152 211
The mean daily variation for every single solar rota-
tion period has been treated as well as the mean daily
variation for the whole year. To study the correlation
with geomagnetic activity the days were divided into
five classes according to their Kp- Indices. The first
•od second harmonics for each class of days were de-
termined for the period Aug. 31. '56 to Aug. 31. '57.
The disturbing influence of the sharp intensity drop
(bUowlng the onset of a Forbush decrease concerning
the daily variation is discussed specially. The influ-
oice is found to be negligible not only as far as the
jrssrly mean is coocemed but also as regards the 27
days sun rotation periods. The influence becomes se-
rious only in the case of the nx>st disturbed days when
phase and amplitude are studied as functions of theKp-
Index. The mean value of the time of maximum is
found to be 1300 Q^4T f or the first harmonic and 0530
CMT for the second harmonic The yearly mean of the
amplitude is 0, 32 per cent in the first case and 0, 034
per cent in the second. The dependence of phase and
amplitude on the K-- index is very smalL (Author)
Uppsala U. (Sweden).
GE(3PHYSICAL ASPECTS OF COSMIC RAYS: DAILY
VARIATIONS OF MESON COMPONENT. PART L
TEXT, by Arne Eld Sandstrttm, Eric Coring, and
Stig Lindgren. Status rept. no. 12, Part 1, on Contract
AF 61(514)1312. 14 Apr 60, 139p. 19 refa. CRD TN-
60-614(0.
Order from LC ml$6. 90, ph$21. 30 FB^152209
A shon description Is given of the routine tests and
other means of checking the performance of the C R.
S9u4>mem and the reliability of the records. Harmooic
analysis has been performed on the mean dally varia- -
tkn of the meson component. Tables are given contaln-
llf amplitudes and phases of the first and second har-
monics for sun rotation periods as well as for 12- month
periods and calendar years. The tables contain also
the standard errors calculated from (1) tbe Polsson
distribution, (2) the residuals after fitting the first har-
moalc, (3) the residuals after fining the sum of the
first snd second harmonics. Harmonic dials and vector
sum dlagrama lllustrste the dau obtained from 9 meson
telescopes. U can be shown that In some cases a sec-
ond harmonic exists which is not due to residual stntos-
phtrlc effects. The experiment with linked asymptotic
directions proves that in a direction parallel to the
earth's axis of rotation, the mean dally variation for
12-moatfa periods has s very small or no anqtlitude.
TIm first harmonic displays a negative phase shift for
iKreasiag Kp values. (Author)
t.
Uppsala U. (Sweden).
GEOPHYSICAL ASPECTS OF COa«C RAYS: DAILY
VARIATION OF MESON COMPONENT. PART II.
FIGURES, by Arne Eld Sandstrbm, Eric Dyrii«, and
Stig Lindgren. Status rept. no. 12, Part 2, on (Con-
tract AF 61(514)1312. 14 Apr 60. 30p. GRD TN-
60-614 (II).
Order from LC mi$2. 70, ph$4. 80 PB 152 210
Figures only. (See also PB 152 209).
Saskatchewan U. (Canada).
INTERFERENCE WEDGE PHOTOMETER FOR
TWIUOIT SODIUM, by E. B. Lotochlnski and
D. M. Hunten. Scientific rept. no. BR-18 on Contraa
AF 19(604)1831. May 59. 38p. 4 refa. APCRC-TN-
59-481.
Order from LC ml$3.00, ph$6.30 PB 152 284
A deuiled description is given of a photoelectric
photometer for the automatic observation of twilight
sodium emission. Its features are simplicity of op-
eration and high sensitivity along with ease of calibra-
tion. It uses the f)roperties of a wedge interference
filter to discriminate against the strong solar contin-
uum in twilight and permits the sodium lines to be
measured for solar depressions greater than 5^ Op-
erating notes and sample observations are included.
(Author)
BEHAVIORAL SCIENCES
Human Engineering
American Inst, of Research. Plttaburgh. Pa.
TASK AND PART-TASK TRAINERS AND TRAINING,
by Robert B. Miller. Rept. on Human Engineering
Faaors in Training Equipment Design. Contract
AF 33(616)2060. June 60. 9Sp. 9 refs. WAIX) Tech-
nical rept. 60-469.
Order front OTS $2. 2S FB 171 199
Because eiKxigh simulators for sufficient snd varied
practice in Job skiUs are rarely available, simpler de-
vices are needed for training parta of uska. In addi-
tion, learning toul Jobs one step st a time may be more
efficient. Procedures for dividing total performance re-
qulremeiKs into training segments lending themselves
to distinctive types of trainers are described. Prindpel
variables in the division are phase of learning and time-
sharing of activitlea. Risks of improper part-usk
training are detailed and principles for reducing such
risks are proposed. Classes of trainer identified are:
I. Familiarization Trainers, n. Instructed- Response
IVainer^.and in. Automatized Skill Trainers. Essential
training and human engineering variables are described
(or esch of tbe sbove clssses of devices. Potentialities
of tbe Class n device sre emphasized. (Author)
133
v'
Bolt, Beranek and Newman, Cambridge, Mass.
HUMAN ENGINEERING ERINCIPLES FOR THE DE-
aCN OF SPEECH COMMUNICATION SYSTadS, by
Karl D. Krytar. Repc. on Contract AF 19(604)4061.
Aug 60. 20p. 8 refs. AFCCDD TR-60-27, formerly
AFCRC TR-58-62.
Order from LC mi$2. 40. Dh$3. 30 PB 152 255
School of Aviation Medicine. Brooks AFB, Tex.
AN EXPLORiNTORY STUDY OF CHANGES IN PRO-
FICIENCY IN A HYPODYNAMIC ENVIROhWENT, by
Bryce Hartmap, Richard E. McKenzie, and Duane E.
Graveline. July 6a 14p. 4 refs. Kept. 60-72.
Order from Lp mi$2. 40, ph$3. 30 PB 152 215
Simulated weightlessness for a prolonged period was pro-
duced by the body immersion technic. Changes in
psychomotor efficiency were assessed during im-
mersion and after return to the normal environment of
1 G. Systematic changes in a relatively simple task
were obtained during immersion. Gross disruptions in
psychorootor behavior on return to the normal environ-
ment were observed. Accompanying this were In-
creased response times on three different kinds d
tasks in a systems operator simulator. Ibese results
suggest that the functional capabilities at a man. while
adequate durii^ prolonged weightlessness, will be
seriously imptirpd during the re-entry phase of spacf
flight. (Author)
fWsonnel and Training
Naval Personnel Research Field Activity. San Diego,
Calif. I
TRAINING ANb UTILIZATION OP SOHARIABU AS-
SIGNED TO VfNE FORCE, UNITED STATES PA-
QFIC FLEET, by Edward J. Plckerii^ and Adolph V.
Anderson. Mar 60, 55p. 2 refs. Technical Bulletin
60-4.
Order from LG mi$3. 6a ph$9. 30 PB 152 121
Sixty-nine sonarmen on twenty randomly selected
Pacific Fleet minesweepers were interviewed in order
to obtain infonnation regarding cheir training and utili-
zatkn. b fenqral, the findings presented in this re-
port show that the school training of sonarmen aa*
signed to minesweepers does not match Fleet utlllza-
tion; that is, nrajch d the training given ia not uaed and
much needed training is not given. The flndli^ sug-
gest that those who are to fill the sonarman billets on
minesweepers might be trained for the specific duties
they will perform School training for this type of duty
would involve a total of 12 to 16 weeka of trainii^ in-
cluding training in basic electronics, operation and
maintenance at mine detection gear, and CIC and
radar watchstaading.
U J(t
Ohio State U ^tesearch Foundation, Columbua.
TEAM TRAINING II: INDIVIDUAL LEARNING AND
TEAM PERFORMANCE, by Jota E. Horrocka. Robert
B. Kr\jg. and Etnil Heermann. Rept. on Contract
N61339-198. Aug 6a 62p. 121 refs. Technical rept.
NAVTRADBVC5N 198-2.
Order from LC ,mi$3. 9a pbf la 80 PB 149 962
Designed primarily to evaluate the effectiveness of
team performance undier varied training conditions,
the study was developed along two lines: Task I, which
dealt with: (1) conditions at training and (2) general-
ized training; and Task II, which studied the influence
of feedback information concerning results. For
Taak I. the problem was the decoding of jumbled sen-
tences. For Task 11, it was an eliciting of Judgments
of position of a target. Neither individual vs. group
(conditions at training), nor generalized training had
any appreciable influence on performance. Knowledge
of results improved performance, particularly in
earlier trials. Specific knowledge of results proved
less effective than general knowledge of results. Pre-T
training and knowledge of results interacted such that
knowledge of results interferred with performance
when pre-training closely resembled the learning task
and facilitated performance when pre-training did not
closely resemble the learning task. (Author)
Personnel Lab. , Wright Air Development [Dlv. ]
Lackland AFB, Tex.
AIRMAN PERFORMANCE ON THE GENERAL
APTITUDE TEST BATTERY AND THE AIRMAN
CLASSIFICATION BATTERY AC-2A. by Jane
McReynoIds. July 59. I6p. WADC TN-59-42;
AD- 225 115.
Order from LC ml$2. 40. ph$3. 30 PB 152 798
This report released for sale to the public 30 Nov 60.
Tests of the General Aptitude Test Banery (GATB).
which the United States Employment Service uses for
Job counseling and placement, were administered to
large samples of male airmen in 1»49 and 1958. Com-
parisons of the results with normative data for the
general working population (male and female) are re-
ported. Airman means for the seven aptitude scores
derived from paper-and-pencil tests of the GATB were
distributed aboiA equally above and below the USES
norms, with the 1958 sample deviating from the norms
less than the 1949 sample. The more significant dif-
ferences were accounted for by known sax differences
in the aptitudes meaaured. Both airman samples has
smaller proportions of very high and very low scores
than the USES distribution. This restriaion waa atr
tributed to Air Force screening on a menul qualifying
test and to self- selection. Two tables give estimates
of proportlona of airmen qualifying for USES job
categories and for airmen career fielda. (Author)
Personnel Lab. . Wright Air Development Div. .
Lackland AFB, Tex.
FACTORIAL STRUCTURE OF AIRMAN PEER F<OM-
INATIONS. by Edwin S. Ewart. Juue 60, 1^. WADO
TN-6O-140; AI>-241 425.
Order from LC miR 40. pb|3. 30 FB ISO 790
A factor analysis of the intercorrelationa of 25 peer
nomination traits administered to 1 1 flights of alraen
In basic training yielded four Interpretable factors.
Theae were thought to represent dimensions of a gen-
eral rating factor, good naturednesa, soeUbility. and
motiration for military life. (Author)
134
University of Southern California, Los Angeles.
CURRENT TRENDS IN AUTOMATED TUTORING
AND THEIR IMPLICAT1C»1S FOR NAVAL TECHNI-
CAL TRAINING, by Glenn L. Bryan and Joseph W.
Klgney. Technical rept. no. 29 on Contract Nonr-
228(02). Dec 59. 52p. 13 refs; AD-232 771.
Order from LC ml$3. 6a ph$9. 30 PB 152 164
Current trends toward the automating ai training and
dieir effect on the Navy's technical training problems
•re described. To esublish a background for this dis-
cussion, a brief resume is presented of some of the
major difficulties involved in getting training done in
(be military sening. Teaching machines, ctxnputer-
oontrolled teaching machines, and computer -fftciliuted
systems training are discussed in terms of the re-
search being done and the applications now in exis-
tence. Comments are presented regarding some futur-
istic conceptions erf automated training. The implica-
tions of these technological advances for increasing
the efficiency of technical training in electronics are
explored for individual and systems training. It is
concluded that the appropriate role of teaching ma -
chines would be as supplements to conventional methr
ods. Completely automated systems training is clearly
unrealistic for present-day tactical data -processing
systems, but the central control computers in these
systems do offer possibilities for advances in the art
of systems training that should be taken into consider-
ation and planned for in the design of systems training ,
facilities. It is recommerxled that teaching machines
be tried on a limited basis in two places in the Naval
training complex: in Class A schools and aboard ships
as shipboard trainers. (Author)
University of Southern California. Los Angeles.
AN EXPERIVCNTAL COMPARISON OF TROUBLE
SHOOTING TRAINING TECHNIQUES, by Qenn L.
Bryan and Donald H. Schuster. Technical rept. no. 30
qn Contract Nonr-228(02). Dec 59. 75p. 9 refs;
AD-231 62a
OnJer from LC ml$4. 50, ph$l2. 30 PB 152 165
Tbe relative effectivenessof various techniques of train-
ing men to trouble shoot electronic equipment was in-
vestigated. One hundred aixl sixty-two studeqts in the
U. S. Navy Electronics School at Treasure Island
served as subjects, devoting the entire 19th week of
their training course to this end. Three forms of guid-
ance and two conditicxis of explanations were studied,
and the point at issue was the contribution which each
of these made in training men to apply good trouble
abooting principles. Each man was given a day of
standard training on tte operating details and circuitry
of the DAS-3 Loran This was followed by 3 days of
eagperimental training which was evaluated by a tab-
item criterion test on the fifth day. The criterion test
indicated that both forms of guidance effectively led the
trainee to employ good trouble shooting principles.
This was further substantiated by an independently ad-
ministered individual trouble shooting test on the SPS-
10 radar given 3-4 wk later. Men who received expla-
lations nuule significantly bener scores on the cri-
terion test than did those men not receiving explana-
tions. A subsidiary study which sought to measure the
absolute gains attributable to the training indicated
that trainees improved their trouble shooting compe-
tence significantly as a consequence of the 3 days of
experimental training. For the 47 subjects who partici-
pated in this phase of the study, there was an average
Kn of 23% in equivalent -form criterion test scores,
iihor) 135
Psychology
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright -Patterson AFB. (5hio.
EFFECTS OF VARIATIONS IN SPEaFiaTY OF
KNOWLEDGE OF RESULTS ON THE IMPROVE-
MENT OF A PERCEPTUAL SKILL, by Theodore E.
Cotterman. Rept. on Human Factors in the Design
of Training Equipment. Aug 60, 32p. 19 refs. WADC
Technical rept. 58-673.
Order from OTS $1.00 PB 171 146
Ninety male undergraduate subjects estimated indi-
vidually with respect to 120 stimulus photos how many
degrees a 1/4-inch arrow would have to be turned to
exactly parallel an adjacent arrowheaded line drawn
across a 3- 1/2 -inch circle. The stimuli were pre-
sented for five seconds with ten seconds between and
longer rbst intervals separating sets of 24. Each set
contained examples of the same 24 different stimuli in
random order -cdrrect answers ranging from 11 to 44
degrees and never being duplicated. Knowledge of
results given orally after each estimation ranged in
specificity from simple right -wrong information to
amount and direction cf error information for five ex-
perimental groups. No knowledge was given a sixth
control group. Differences in mean absolute and alge-
braic error per stimulus among groups reflect differ-
ences in specificity of knowledge given. It is con-
cluded that knowledge of results increases the rate
and level of learning to perform an absolute judgment
of spatial extent and this effect is generally g^reater
the more specific the knowledge. (Author)
California U. , Los Angeles.
DYNAMICS OF SOCIAL INFLUENCE, by Bertram H.
Raven. Annual rept. no. 1, Nov 58-Nov 59, on Con-
tract Nonr-233(54). 7 Dec 59, 18p. 14 refs.
AD- 233 353.
Order from LCml$2. 40, ph$3. 30 PB 150 500
Contents:
Bibliography of small group literature
Review of literature and development of card coding
system
Review of educational research
Measuring the relationship between belief and attitude
Development of the AB scale
An investigation of some of the theoretical and em-
pirical relations between belief and attitude
Social influence on beliefs and anitudes
Effects of coercion on change in behavior and belief
Effects of group pressures on behavior and belief in
ESP
Social referents and self-evaluation in examinations
Individual differences in social influence
The power preference inventory
Educational Testing Service, Princeton, N. J.
EVIDENCE FROM SCHOOL RECORDS ON THE
EFFECTIVENESS OF ABILITY GROUnNG, by John
W. French. Rept. on Contract Nonr- 221 4(00). Mar 59,
29p. 8 refs.
Order from LC ml$2.70, ph$4.80 PB 148 293
An imporrant queslcm In education or training pertains
to the advisability ol dividing students into clasaes so
as to form homogeneous ability groupings at two or
more levels. Thit project represents an anempc to
find evidence on tUls question in the files at Navy or
civilian schools An absence d relationship was found
between homogeneity at classes and the effectiveness
d preparing students for achievement testa either in
Navy schools or ig a h4ew York City high school. In
the high school, h^ever, students enrolled in high-
ability classes api^eared in some subjects to have a
definite advantage over students in lower-ability
clasaes, whether they were themselves fast or slow
learners. However, since this finding may be ac-
counted for by an Artifact stemming from the use ai
data in the files, it must be concluded that a definitive
answer to the protjlem can only be obtained by means
of conroUed expef iments. (Author)
J,
Human Factors Research, Inc. , Los Angeles, Calll
HUMAN PERFORMANCE AS A FUNCTICW OF THE
PINT EFFECTS OF DRIVE AND INCENTIVE MO-
TIVATION, by Donald N. Buclmer and Albert
Harabedlan. Kept, on Contract Nonr- 2453(00). Dec 59,
68p. 18 refs. AD-t32 918.
Order from LC mi$3. 90, ph$10. 80 PB 152 156
The joint effects o| the Hull-Spence motivational con-
struct, D or generalized drive, and incentive motiva-
tion, K, on human performance were investigated. Re-
sults indicated tlia| (1) the subjects who received con-
ditioning trials prior to the test trials improved their
performance significantly less than the subjects who
received no such ttials, when transmission scores
which reflected accuracy or probability of response
were used as the dependent measures; (2) the subjects
who received an opportunity to obtain a 72 hr liberty
did not improve their performance significantly noore
than the subjects who received no such opportunity,
when transmission scores indicating the accuracy or
probability at response were used as the dependent
measures; (3) whe* transmission scores were used as
tiie dependent meafures, there was a significant effect
due to the interaction between the two experimental
variables; (4) when improvement in reaction times was
used as che dependent measure, there were no signifi-
cant differences due to the experimental variations;
and (5) when score* reflecting tenprovemeiu in both ac-
curacy and speed ifere used af the dependent measures,
the low drive- - hlgH incent^ grov^ appeared to im-
prove its performance ^ij^than sb)^ other group.
Human Factors Resear^, Inc. , Los Angeles, Calif.
REVIEW AND CRITIQUE OF LITERATURE ON
VIGILANCE PERFORMANCE, by James J. McGrath.
Albert Harabedian and Donald N. Buchner. Technical
rept. 1 on Human Factor Problems in Anti -Submarine
Warfare, Contract Nonr- 2649(00). Dec 59 106p.
66 refs. AD- 237 691.
Order from LC mi^. 70, ph$l6. 80 PB 152 157
Cootents:
introductkn to die ^tudy d vigilance performance
The problem at d^nition
Vigilance tasks !
Measures of vigilfnce performance
Review and critique
ma nee
of studies at vigilance perfor-
The temporal course at vigilance performance
The effects of display characteristics
The effects at signal characteristics
The effects of environmental conditions
The effects of procedural conditions
Physiological factors in vigilance performance
Individual differences in vigilance performance
Theories of vigilaiK:e performance
Inhibition - reinforcement
Operant conditioning
Secondary inhibition
Expectancy 9 \- - ".■
Activation
A Hullian approach '
The empirical model
Filter theory
Physiological fatigue
Human Resources Research Office, George
Washington U. , Washington, D. C
EFFECTS OF CORRECT AND INCORRECT KNOWL-
EDGE OF RESULTS ON ABILITY TO COUNT AUDI-
TORy STIMULI, by Richard A. Monty. Thomas L
Myers, and Donald B. Murphy. Rept. on Cowract
DA 49-I06-qm-l. Mar 60, 21p. 11 refs. Re^rch
rept."iio. 3; AI>234 599. I
Order from LC mi$2. 70, phH 80 FBh48 728
TWO experiments were cottducted to determine the ef-
fects of correct and Incorrect feedback on the ability to
count rapidly produced auditory stimuli. The results
showed that: (1) correct knowledge of results contrib-
uted to bener performance on blip items of each
length, but with an effect proportionally more pro-
nounced on the more difficult items: (2) misinforms- ■
tion (L e. , incorrect knowledge of results) contributed
to the disruption c4 counting ability; (3) the effects of
correct infortnatlon and misinformation were evident
one hour later, in the absence of all feedback; and
(4) error in counting was directly related to the blip-
Item length, b was concluded that the usk would be
useful as a measure of the effects of sensory depriva-
tion i^xxi a variety of variables. (Author)
Lincoln Lab. , Mass . Inst . of Tech. , Lexington.
DISrANCES AND RATIOS IN PSYCHOPHYSICAL
SCALING, by Warren S. Torgerson. Rept. on Contract
AF 19(604)7400. 13 Oct 60, 15p. Rept. no. 58G-0014.
Order from LC nii$2.40, ph$3.30 PB 152 542
Maryland U. , CoUege Park.
FURTHER OBSERVATIONS ON DISCRETE WORK
ASSOCIATIONS TO VERBAL STIMUU IN A COH-
TEXT, by Charles N. Gofer. Technical rept. no. 23
on Learning, Retention and Recovery of Meaningful
MaterUl, Cootraa Nonr-59S(04). Apr 59, 5p. 5 refs.
Order from LC ml$1.80, ph$1.80 PB 148 300
Subjects were asked to use each of a list of word com-
pounds and each of a list of single words in a sentence.
Separate tabulations, were made of the words and
their frequencies which followed in the two seixenoe
positions following those of the prescribed material.
It was found that the number of different words used
by subjects in either position for either the compounds
or the single words did not differ from the number of
136
(Mfferent words given to die compound elements alone,
or to the single stimuli under more usual free-associ-
ttioa conditions. These results are at considerable
rariance with earlier reports which had described an
increase in the number of different words given in free
association to comfxjund- word stimuli. (Author)
Office of Naval Research, Washington, D. C.
PHYSIOLOGICAL PSYCHOLOGY BRANCH: BIBLIOG-
RAPHY OF UNCLASSIFIED RESEARCH REPORTS.
SUPPLEMENT NUMBER 6: JULY 1959 -JULY 1960.
31 July 60. 14p. 104 refs. AD- 242 190.
Order from LC mi$2. 40, ph$3. 30 PB 1 16 303S6
Contents:
Sensory mechanisms
Perception and orientation
Neural basis of behavior
Response mechanisms
Supplements report dated Mar 54 (PB 1 16 303) and its
supplements
Perception and Conditioning Lab. , Southern Illinois
U. , Carbondale.
BLOCKED SPEECH COMMUNICATION AND DE-
LAYED FEED-BACK: AN EXPERIMENTAL AN\LY-
SUL by Israel Goldiamond. Technical rept. no. 1
(Progress) for 1 Dec 59-29 Feb 60, on Contract
AF 19(604)6127. Feb 60, 36p.
Order from LC mi^. GO, ph$6. 30 PB 152 389
A report is presented in two parts dealing with the
operimental analysis of temporal faaors in blocked
verbal communication, with special attention to the
role of delayed auditory feed-back. These two parts
•re (1) A rationale for such analysis} (2) A progress
report of research performed during the first three
months of contract.
r
!l
[l^rception and Conditioning Lab. ] Southern Dlinoit U. ,
Oirbondale.
THE TEMPORAL ENVELOPMENT OF FLUENT AND
BLOCKED SPEECH CCMMUNICATION. by Israel
Goldiamond. Final rept. and Technical rept. nos. 2-4
on Contract AF 19(604)6127. Sep 60, 116p. 38 refs.
Order from LC mi$6. 00, ph$18. 30 PB 152 390
Contents:
Technical rept. no. 2. Effects of delayed feedback upon
die temporal development of fluent and blocked speech
communication, by Israel Goldiamond
Technical rept. no. 3. Adapution to delayed feedback
u a function of instructions not to monitor, by
Israel Goldiamond, Chester J. Atkinson, and Robert
C Bllger
Ttehnical rept. no. 4. The distribution of pause dura-
tions in speech, by Bruce Flanagan
Personnel Lab. , Wright Air Development Center,
Uckland AFB, Tex.
ARITHMETIC REASONING ITEMS WITH FORMULA
RESPONSES, by Mary Agnes Gordon. July 60. 12p.
2 refs. WADD-TN -60-210.
CWer from LC mi$2. 4a ph$3. 30 PB 152 272
This is a study of the effect of practice on item statis-
tics. Some specific practice effects were found. These
were not large enouj^ to be troublesome in selecting
items for a new test from a pool of experimenul item&
If experimental items are protected by initial practice
items and final time -filling items, nnoat of the prac-
tice effects can be controlled. Arithmetic reasoning
items with formula responses as lued in this study
were found to be suitable for moderate to difficult tests
of airman aptitude. (Author)
Psychological Labs. , Carnegie Inst, of Tech. ,
Pinsburgh, Pa.
VARIABLES UNDERLYING SOaOMETRIC STATUS.
VI. GROUP CONSENSUS AND GROUP ATTRACTIC*!.
by E. P. Hollander. Technical rept. on Contract Nonr-
1849(00). Apr 59, 12p. 5 refs. AD- 233 053.
Order from LC mi$2.40, ph$3.30 FB 148 292
From research with 8 training sections of naval
officer candidates, numbering about 30 each, data are
presented on the relationship of group attraction to
various measures of group consensus. A notably high
correspondence was found between attraction ranks
for the sections and ranks based on the smallness of
disparity between member's own ranking of a values
list and their estimate of the section's ranking. Group
consensus in the self-ranking of the values list, as
measured by the Kendall W was consistently but rat
significantly related over time to the section's attrac-
tion in terms of rank. (Author) (See also PB 145 214)
Psychophysical Research Unit, Mount Holyoke Coll. ,
South Hadley, Mass.
RELATIVE EFFECTIVENESS OF PRESENTING IN-
FORMATION TO SELECTED SENSE MODALITIES,
by E. P. Reese, H. B. Robinson and others. Rept. on
Contract N61339-5I2. June 60, 83p. 9 refs. Tech-
nical rept. NAVTRADEVCEN-512-1.
Order from LC nU$4. 80, ph$13. 80 PB 150 887
The major flndlnga of this study are: (1) As both the
number of stimuli to be counted and the rate of pres-
entation increased, accuracy of counting decreased
for all sense modalities and their comt^nations. (2)
Under all conditions, auditory stimuli and combina-
tions involving the auditory modality were counted
more accurately than uctual or visual stimuli. Tac-
tual accuracy was superior to visual except at very
high rates. (3) Auditory stimuli aixl their combina-
tions were counted accurately through a rate of 6. 5
stimuli per second; tactual were counted fairly accu-
rately through rate 4.0. At no rate employed wak
accuracy uniformly high for visual stimuli. At the
lowest rate of 2. 5 flashes per second, the percemage
of correct responses to visual stimuli dropped to
approximately 40% for series erf more than 20 flashes.
(4) As the rate of presentation of stimuli and the num-
ber to be counted Increased, the subjects' responses ,
became more varied. (Author)
Tennessee U. [Knoxville].
VALIDATION OF MORALE AND ATTFTUDE
SCALES, by Gerald H. Whitlock and Edward E. Cure-
too. Rept. on Cootraa AF 41(657)247. June 60. 26p.
8 refs. WADD-TR-60-76; AD-242 359.
Order from LC mi$2. 70, ph$4. 80 PB 152 271
i37
siete
This paper completes reporting ctf the development at
scales for measuring morale among Air Force per-
sonnel. A previously developed questionnaire keyed
for eight scales was given to an independent sample.
When the scores were compared with criteria derived
from interviews, ratings, and Air Force records,
validities were uniformly low. Although none at the
validities are hig^ enough for useful prediction, the
scales do measure expressed attitudes with consid-
erable reliability^ (Author)
Washington U. , ,Seanle.
A MATHEMATIQAL OONTRCX FOR SOCIAL E«-
SIRAMLITY RESt>ONSE SET. by George R. Burket.
Repc. on Contract Nonr-477(08) and Public Health Re-
search Grant M -743(04). Dec 59. 24p. 16 refs.
Order from LC iii$2. 70. ph$4. 80 PB 152 166
Scores obtained by presenting EPPS statements one at
a time in a ratiiu^ scale form were transformed so as
to make the acorf a themselves and also the principal
axis vectors of tlieir intercorrelation matrix uncorre-
lated with a vector erf SD values for each trait. The
results were compared with those obtained by mathe-
matically ipsatiznig the same scores without reference
to social desirability and with those obtained by ad-
ministering the same EPPS statements in their stand-
ard forced-choice form. When the SD vector was not
given in deviation f6rm, the lesults were almost iden-
tical with those o(xained by mathematically ipsatizing
without references to social desirability. When the SD
vector was given in deviation form, the results were
even less Mmilar to the EPPS than the original rating
scale. About the only definite conclusion that can be
drawn la that a mathematical control for social desir-
ability of this kln<l does not give results comparable to
a control by the forced -choice method at the EPPS.
(Author) :
Washington U. . Seattle.
THE MULTIPLE PREDICTIVE EFFICIENCY OF
IPSATIVE AND NORMATIVE PERSONALITY MEAS-
URES, by Robert D. Talboa. Rept. on Contract Nonr-
477(08) and Public Health Research Grant M-743(C3).
Feb 60, 3Sp. 24 eefs. AD- 236 862.
Order fromLC m|$3. Oa ph$6. 30 PB 147 642
An aaempt was n)ade to compare the efficiency at an
ipsatlve and a notfmative personality measure as pre-
dictors of grades of college students. Findings indi-
catad multiple correlations averaging 47 In predicting
oourae grades. Findings suggest that an Ipsatlve meas
ure has some rea) value and should be considered as a
possible addition to grade prediction batteries. The
ipsatlve did as w^ll aa the normative personality meaa-
ure and was less Influenced by response set.
U.. Beat
Washington U. , Seattle.
THE PRIMARY DIMENSIONS OF ITEM RATINGS ON
SCALES DESICNID TO MEASURE 24 OF MURRAY'S
MANIFEST NEEDS, BY Mary Marjorle Campbell.
Rept. on Public Health Research Grant M-743<C4).
Ok 59, 201p. 55 refs.
Order from LC Tn^$9. 30. ph$31. 80 PB 152 168
This research was concerned with the determination <rf
the basic traits- -the dimensions — of personalityas the
essential preliminary step in the development at uni-
dlmenslonal personality scales. It was particularly
designed to investigate the number and Identity of the
primary dimensions at one at the most comprehensive
and widely used descriptive theories at personality,
Murray's system of needs. Procedures for a modified
multiple group technique of factoring a large number of
items were developed In order to identify the items
ifepresenting each of the dimensions isolated. (Author)
BIOLOGICAL SCIENCES
Army Research Office, Washington, D. C.
ARMY RESEARCH TASK SUMMARY, FISCAL YEAR
1960. VOLUME 1. MEDICAL, BIOLOGICAL, SOCIAL
AND BEHAVIORAL SOENCES. 436p.
Order from OTS $3. 75 PB 171 000
Contents:
Medical Sciences:
Basic medical sciences
Dentistry ^ •- •- •;
Internal medicine
Preventive medicine
Surgery
Biological Sciences: /
Microbiological/bacteriology, mycology
Plant sciences
Zoological sciences
Social and Behavioral Sciences:
Experimental psychology
Social psychology and sociology
Psychometrlcs
Engineering psychology
Physiological psychology
Learning and educational psychology
Motivation i
(See also PB 151 494) '
LT
Anatom)^ and Ph)rsiolog)r
Air Force Missile Development Center, HoUoman
AFB, N. Mex. y
CHIMPANZEE TEMPERATURE-HUMIDITY TOLER-
ANCE TEST NO. 1, by Erwin R. Archibald, William
E. Ward and othera. July 60. 36p. 6 refs. AFMDC
TN-60-11; AD- 243 456.
Order from LC mi$3. 00, ph$6. 30 PB 152 428
This report describes the effect of a temperature-
humidity test on a restrained chimpanzee In an en-
ATlronmental test chamber. The subjea was a nornul
young male chimpanzee weighing 36 pounds. The pri-
nury object at the test was to determine the feasi-
bility at conducting temperature -humidity tolerance
tests on large biological specimens. The results of
this test demonstrated that such tests are feasible.
Duration at the test waa 8 hours; the subjea waa ex-
posed to an enviroament at 85°P and 80 percent rela-
tive humidity for this period. Pulse rate, respiration
rate, electrocardiogram, rectal temperature, gal-
vanic skin resistance (baaal), environmental oxygen
138
,^l
depletion, and carbon dioxide accumulation were
(^lonltored continuously during the test. Instrumenta-
tion procedures, general test techniques, and experi-
mental design are described. The subjea lost 2
pounds, CM' 6 percent at his initial body weight.
(Author)
I '
Arctic Aerortedlcal Lah. , Ladd AFB, Alaska.
EVALUATION OF VARIOUS REWARMING TECH-
NIQUES FOLLOWING GENERAL AND LOCAL HYPO-
THERMIA, by Henry E. D'Amato and Benjamin O.
Covlno Cnifts U. ). Feb 60, 21p. 8 refs. Technical
rept. 59-10.
Crter from LC ml$2. 70. phK 80 PB 152 853
General hypothermia studies were conduaed on dogs In
order to gather data as to the relationship between the
rate at rewarmlng and completeness of recovery at
cardiovascular funaions. Rapid rewarmlng at the
whole animal from deep hypothermia resulted in less
frequent cardiovascular crises. The cardiovascular
ciitls, when it did occur, was not primarily of cardiac
migin, but appeared to be of a peripheral vascular
nature. Studies at frostbite In rabbits were conduaed
to study the response of local body temperature to sub-
rero air temperatures and to evaluate the relative
merits of various rewarmlng techniques In amelio-
rating the effects of frostfcite so induced. Rapid re-
warming of a frostbitten limb was associated with die
least degree of permanent damage In rabbits. (Author)
Arctic AeromedlcalLati. , Ladd AFB, Alaska.
HEAT FLOW METERS BASED ON THE GRADIENT
PRINCIPLE AND THEIR USE DM PHYSIOLOGY OF
HEAT REGULATION, by H. T. Hammel. U. of
(Pennaylvanla, School of ^ediclne). Feb 60. Up. 5 refs
Technical repL 57-50.
Order from LC mi^. 40. ph$3. 30 PB 152 849
I
i
Arctic Aeromedical Lah- . Ladd AFB. Alaaka.
STUDIES OF SKIN, BLOOD. AND RECTAL TEMPER-
ATURES OF UNANESTHETIZED DOGS EXPOSED TO
EXTREME COLD. L TEMPERATURE CHANGES IN
THE BLOOD OF THE PULMONARY ARTERY AND
LEFT ATRIUM, by A. L. Good and A. F. SeUers
(U. of Minnesota School of Veterinary Medicine).
Feb 60, 19p. 22 refs. Technical rept. 57-52.
Order from LC mi$2. 40, .ph(3. 30 PB 152 850
Polyethylene cannulae wefe surgically placed In the pul-
monary artery and left atf ium of dogs; thermistors
mounted In polyethylene tubing and hypodermic needles
were passed through these cannulae and the tempera-
ture changea of the blood ^nd rectum rectum were re-
corded photographically. Continuous recordings of
Ifaese temperature changes in unanesthetlzed dogs were
made when the experimental animals were suddenly ex-
posed to an ambient temperature of -35° C. for 30
minutes. Shivering began Immediately after exposure
CO cold; blood and recul temperature Increased 0. 4 to
(L 5° C. during the 30 mil utes of exposure. It was
found that the rectal temperature exceeded the left
atrial blood temperatures from 0. 2 to 0. 3° C. , and
that In all experiments except one, the left atrial blood
temperature exceeded that of the pulnK>nary artery
from 0. 01 to 0. 15" C Thermodynamic considerations
of carbon dioxide and oxygen exchanges in the lun^s
and evaporation of water in the upper respiratory tract
are cited in interpreting these findings. (Author)
Audiology Lab. , Northwestern U. , Evansion, HI.
AUDIOLOGIC FINDINGS IN AN UNUSUAL CASE OF
EIGHT NERVE LESION, by James Jerger. Sep 60,
7p. 4 refs. AFSAM rept. 60-84.
Order from LC mi$l. 80. phjl. 80 PB 152 766
Remarkable recovery of pure-tone acuity following
surgical removal of a meningioma in the right cere- .
bellopontine angle provided a unique opportunity to
study several facets of auditory behavior in a single
patient. Loudness recruitment was absent, speech
discrimination was extraordinarily affected, and
severe threshold adaptation under continuous stimula-
tion was apparent. No abnormality in the masking of
pure tones by either broad- or narrow- bemd noise
could be demonstrated. (Author)
Biomedical Lab. , Wright Air Development Div. ,
Wright -Patter son AFB, Ohio.
MONITORING UNIT FOR HEART- AND RESHRA-
TION-RATE, by Adolf R. Marko. Rept. on Biophysics
Research. Aug 60, 9p. 3 refs. WADD Technical
rept. 60-619.
Order from OTS $0.50 PB 171 140
A small unit has been developed to monitor hean and
respiration rate of a man during experiments. This
unit has been used at altitudes up to 100, 000 feet in
temperature chamber tests. In aaual high altitude
balloon flights (with telemetering) and for monitoring
tests of the B-58 aircraft's emergency escape capsule
(floating in water). The advantages erf this monitor
compared with other methods are mainly the simplicity
of parts, reliability, low Cost, low wel^t (4 oz. ap-,
proximately), small size, and low power consumptidp
(22 volts, 2 ma). Also, only one communication chan-
nel is needed to convey information on two important
physiological sources. (Author)
California U. , Los Angeles.
TECHNICAL STUDIES IN CARGO HANDLING. VII.
THE HUMAN OUTPUT FUNCTION, ITS CONCEPT
AND MEASUREMENT. Rept. on Contraa Nonr-
233(07). Dec 59, 27p. 10 refs. Dept. of Engineering
rept. no. 59-75; AD-233 480.
Order from LC ml$2. 70, ph$4. 80 ^ PB 152 112
A closer approximation of a direct measure of the total
physiological energy cost to a human was. attempted for
a more accurate work analysis of tasks. Total physio-
logical energy cost was termed the human output func-
tion (HOF). An equation was developed for use with
Lauru's force plate, which is used for Indirect esti-
mate of HOF. A simplified version of HOF measures
the tension -time of holding a load plus the linear and
angular impulse that a person imparts by moving a
weight and body parts. Preliminary analyses are pre-
sented which suggest design criteria for a force plat«»
for laboratory analyses of cargo handling tasks.
139
Harvard U. , Cambridge, Mass.
HYPOTHALAMIC SECRETORY FACTOR FOR AD-
RENOCORTICOTROPIC HORMONE (SF-ACTH). by
Paul L. MunsotL Annual rept. on Contract AF
49(638)740. 2^ Sep 60, 7p. [AFOSR TN 60- 1128].
Order from LG miSl. 80. ph$l; 80 PB 150 966
The princ^uU qbjectives of this research project are
(1) to perfect aj biological assay system for the postu-
lated neural hot'mone that is thought to be the mediator
between stress: stimuli impinging on the central nervous
system and the secretory apparatus for ACTH in the
anterior pituitary, and (2) to fractionate and purify
this hormone ftom extracts of hypothalamus with the
aid of a suitable biological assay system.
Hofstra Coll. ^ Hempstead. N. Y.
AUDITORY PAIN THRESHOLDS FOR INTERMnTENT
"WHITE' NOISE, by Robert Plutchlk. Rept. on Con-
tract Nonr-225|(01). Feb 60, 12p. 4 r«f8. AD-236 942.
Order from LC ml$2. 40, ph$3. 30 PB 147 529
Four subjects were asked to match the intensity of a
white noise against pure tones d 1000 cps, 2500 cps
and 4000 cps, which were set at various known Inten-
sity levels ranging from 90 decibels to 120 decibels. A
linear ecjuation was found to approximate the matching
data for all frequencies. The subjects were then re-
quired to indicate unpleasantness and pain thresholds
using interrupt«d white noise at 3, 6, 10 and 15 pulses
per second as well as the thresholds for a pure tone at
1000 cps. The major results show: (1) pain and un-
pleasantness thresholds for the 1000 cps tone are about
15 db lower thaa for the noise; (2) pain and unpleasant-
ness thresholds, for interrupted pure tones are lower
than for corresponding white noise: and (3) there
6eemed to be no difference In threshold as a function
of pulse rates using white noise. (Author)
Ohio State U. flesearch Foundation, Columbus, Ohio.
THE EFFECT OF SPECIFIED LEVELS OF WHITE
NOISE UP»J FtlCKER FUSION FREQUENCY, by
Robert L. McCfoskey, Jr. Rept. on Contract N6onr-
22525. 18 Aug 38, 12p. 17 refs. Bureau of Medicine
and Surgery ProJ. NM 18 02 99, repc no. 80.
Order from LC fni$2. 40. ph$3. 30 , PB 153 252
This report released for sale to the public 14 Dec 60.
The Introduction of white noise, from 85 to 115 db,
into a room in wtilch Individual subjects determined
their threshold 9f fusion changed tte critical frequency
from approximately 27 to approximately 24. The level
ol noise within the range tried and the duration of the
•ybjects' exposure to noise were not conclusively or
udformly differentiating. (Author)
I
Research Lab. ; of Electronics, Mass. Inst, of Tech. ,
Qun bridge.
TWO RB^ARK3 ON THE VISUAL SYSTEM OF THE
FROG, by J. Y. (.ettvln, H. R. Maturana and othera.
Final rept. for | Sep 59-30 Apr 60 on Contract
AF 49(638)724. |l960] 34p. 6 refs. AFOSR TR-60-77.
Order from LC «niS3. 00, ph$6. 30 PB 152 399
Contents;
Plart I. Form -function relations in the retina
Part 2. Collicul4r cell activity and efferents to the retina
School of Aviation Medicine, Brooks AFB, Tex.
AIRCRAFT NOISE, by Max H. O'ConneU. June 60.
31p. 25 refs. Aeromedical Reviews no. 3-60.
Order from LC mi$3. Oa ph$6.'30 PB 152 263
Contents:
Noises during flight
Noise during ground operations
Effects of noise
Protection against noise f
School of Aviation Medicine, Brooks AFB, Tex.
INFLUENCE OF INTERMITTENT EXPOSURE TQ
SIMULATED ALTTTUDB ON ORGAN HISTOLOGY IN
RATS, by Robert A. Brooks and Johnle L. Reeves.
S^ 60, 9p. 20 refs. AFSAM rept. no. 60-81.
Order from LC mi$l. 80, ph$l. 80 PB 152 765
A study of histologic changes in kidney, lung, liver,
spleen, testis, brain, hypophysis, and striated musck
was made as part of an investigation of male Sprague-
Oawley rats exposed four hours a day to 18. 000 feet
equivalent altitude. Few histologic changes were
found which could be attributed to the altitude exposure
Hemosiderin was deposited in the renal tubules, but
not in the liver. In most instances, less lymphatic
tissue was found in the lungs of the altitude- exposed
rats than in the lungs of controls. Fatty change was
not found in the organs of the exposed animals in this
study. Morphologically, there was no indication that
intermittent exposure to 18, 000 feet altitude caused
significant pathologic alteration of the organs examined.
(Author)
School of Aviation Medicine, Brooks AFB, Tex.
RESHRATORY EFFECTS OF CARBONIC ANHY-
DRASE INHIBITION, by Stephen M. Cain. Doctoral
thesis. June 60, 52p. 75 refs. Rept. 60-48.
Order from LC ml$3. 60, pb$9. 30 PB 152 433
Contents:
Transient effects of carbonic anhydrase inhibition
The measurement of mixed venous Pco2
The effect of carbonic anhydrase inhibition on mixed
venous CO2 tension
The transport and exchange of CO2 after inhibition of
carbonic anhydrase
The physiologic role of carbonic anhydrase
Biochemisfry
Araic Aeromedical Lab. , Ladd AFB, Alaska.
ALTERATION OF THE PATTERN OF HEPATIC
CARBOHYDRATE METABOUSM BY PROPIONATE
AND BUTYRATE, by J. M. Felts, E. J. Masoro and
others (Tufts U. School of Medicine). Jan 60, 12p.
13 refs. Technical rept. 57-61.
Order from LC mi$2. 40, pfa$3. 30 PB 152 851
Butyrate and propionate caused a reduction in C^^02
and C^^- lipid production froin evenly labeled glucose,
glucose- l-C^*, gluco8e-6-Cl^, and lacuite'2-C^^.
Unlike the action of these acids on acetate meu. V>-
lism, the inhibition of llpogenesis from glucose and
140
lactate was more severe than tbe reducQon in oxlda-
Hoi at these compounds. These striking differences
^■rween the inhiblrary actions of butyrate and propio-
Mte on hepatic acetate metabolism on the one hand
and hepatic carbohydrate metabolism on the other
■eem to suggest that the metabolic path of the C-2
fragment derived from these two sources must differ.
(Author) ,
Arctic Aeromedical Lab. , Ladd AFB, Alaska.*
THB EFFECT OF PHYSICAL INJURY ON LIPID ME-
TABOLia*, by E. J. Masoro CRrfts U. School of Medi-
daeX Feb 60, 26p. 55 refs. Technical rept. 58-17.
Otder from LC mi$2. 70, jti$4. 80 PB 152 852
This paper has been concerned with the effects of physi-
cal injury on lipid metabolism as a field of study. Some
Inroads have been made on, the action of cold Injury on
(he Interrelationship of energy generation and the inter-
mediary metabolism of lipids.
Ihnrard Medical School, Boston, Mass.
THE DISTRIBUTION OF MONOAMINE OXIDASE AND
aXXHNIC OXIDASE IN BRAIN, by Norman Weiner.
Jae 60, 8p. 17 refs. AFSAM rept. 60-65
(Mer from LC mi$l. 80, ph$l. 80 PB 152 264
Itae distribution of two particulate enzymes, mono -
iBlne catldase and succinic oocktese, has been studied
to various regions of dog, cow, and human brain. Suc-
cinic oxidase is most active in the cellular areas of the
hrain, especUlly the cerebellar and cerebral cortices.
Monoamine oxidase is most active in the thalamlo and
bypotlialamlc regions. Both enzymes are found pre-
dominatly and in similar proportions in the mito-
chondrial fraction. Neither is detectable in the mlcrO-
lomal fraction or in the cell supernatant. The befaav-
kr of monoamine oxidase toward different substrates
k the various regions of the brain is similar. These
results support the hypothesis that the mttochoodrlal
(ractlons from various r«gioos at the brain are bio-
cksmlcallv heterogeneous. Either tbejc two enrvmes
reside in distinct particles or the analogous particles
contain different amounts of each enzyme in different
Hfions of the brain. (Author)
I
Heidelberg U. (West Germany).
PATE OF INTRACELLULAR I^DIOACTIVB FHOS-
mORUS, SODIUM, POTASSIUM WILL BE STUMED
M BNDOTHEL- LINED CAVITIES MEASURING THE
OUTFLOW OF SUCH TRACERS INTO THE PER-
rvSKXi FLUID, by F. Eichholtz and K. Alexander.
Itehnical final rept. for 1 Nov 56-31 Ai« 59 on Coa-
tnw AF 61(514)1006. fl959j 5p. AFOSR -TR- 60- 56.
(Mer from LC mi$l. 80, ph$l. 80 PBJ152 539
|i early periods of Inflammation the fluid In the Selye-
fnaukma of the rat is readily exchangeable with fluid
h the drcuUdon; this la true tor proteins, electrtriyts
■■d glucose, b this early period Prednisolon leads to
aa increase In the sugar content of the vesicle as acon-
(•lueoce of the increased blood sugar. On the other
Md the total amount at fluid in this period is dlmin-
Wwl by Prednisolon. The Sel ye -granuloma in a later
fkue of inflammation gives a new model for estima-
(ton of the glucoae consumption by the granulomatous
tissue and it is possible to measure the fate of other
energy produdi^ substances. Cortisones increase
sugar consianption of the granuloma. (Author)
Oklahoma State U. Research Foundation, Stillwater.
STUDIES ON UREASE, by George Gorin. Final repc
1 Sep 56-30 June 60 on Contract AF 18(603)135. Aug 60,
9p. AFOSR TR-60-115.
Order from LC mifl. 80, ph|l. 80 PB 152 247
Summary of research and papers published.
School bLMityjn Medicine, Brooks AFB, Tex.
THE EFFEQT OF FLOW RATE ON PAROTID FLUID
CCMPOSITION, by Ira L. 9)annon and John R. Prlgmore.
July 60, 13p. 28 refs. Rept. 60-77.
Order from LC mi$2. 40, ph$3. 30 PB 152 216
Five parotid fhiM accommodation samples and five test
samples were collected from each of 53 healthy young
men in two separate experiments directed towanj de-
termining the relationship between flow rate and concen-
tration. A repnxhicible ascending -descending pattern
of flow rate was obtained by using rubber band, gum
base, sugared gum, gum base, and rubber band stimu-
lation, in that order, for the collection of the speci-
mens. Withln-subject and between-subjecx correlation
coefficients and their probability of significance w6re
calculated for all variables in each experiment. IV>sitive
flow-rate correlations, s igntf leant at the i percent
level, werefoundfor bicarbonate, calcium, pH, sodium,
toul protein, and chloride. Anequally significant n^a -
tive correlation was found between flow rate and inor-
ganic phosphate. Potassium and flow rate were not
signifiaintly correlated. (Author)
Technische Hoogeschool, Delft (Netherlands).
THE STUDY OF THE EFFECT OF ULTRAVIOLET
LIGHT ON CERTAIN CONSTITUENTS OF NUCLEIC
ACIDS AND RELATED SUBJECTS, by W. Berends.
Final technical rept. for 1 Oct 59-1 Oct 60 on Contract
DA91-591-EUC-1292. 3 0a6a 2lp. 49r«fs.
Order from LC ml$2. 70, pfa$4- 80 PB 152 532
Phenomena produced by U. V. -Irradiation like muution
and reversible inactivation of cells cannot be the re-
sult of too drastic alterations on the molecular level,
but are more probably brought about by minor ctei^s.
These will undoubtedly only occur by U. V. -irradiatloa
with small doses. The aim of the work described was
a deuiled investigation of the effects of such irradia-
tions on nucleic acids and its componcnta. Attention
was paid to these compounds for several arguments
can be given which support the assumption that biolog-
ically active U. V. -Irradiation la mainly absorbed by
the iHiclelc acids.
IXrfts U. Scbooi at Medicine, Boston, Mass.
THE EFFECT OF (X3LD EXPOSURE ON HEPATIC
ACETATE METABOUa*. by Arthur L Gbhen. Rept.
on Qntract AF I8(600)S83. >ily 60. 74p. 50 nit.
Tteboicsl rept. no. 57-4.
Order from LC mlH 5a ph$12. 30 PB 1S2 531
141
hepatic
The pattern of hepatic acetate metabolism of rat liver
•lices was found to be greatly changed by cold exposure
and fasting. Tke ability of liver slices from 1- and
2-day "cold" r»ts to synthesize C^^-fatty acids from
acetate- 1-Cl**ras severely depressed; whereas, after
exposure d xM animals t6 cold f or S to lOxlays. adap-
tation occured and the previously lowered lipogenic
activity approached the control level. The oiidatiao
of acetate, as shown by the conversion <rf acetate- 1-C^*
to C ^^02, was not influenced by exposure dt rats to
coid for l' or 2 days, but an increased acetate oxldatiaa
was obaerved ^ liver slices from animals exposed to
low temperatuiie for 5 to 10 days.
f4ui
rology and Psychkitfy
Ounbrldge U. (Gt. Brit. )
STMULATIONi OF FRONTAL CX)RTEX AND DB-
LAYBD ALTEHNATICW PERFORMANCE IN THE
MCMCEY, by Utwrence Weiskrantz. Technical
(scientific) note no. 1 on Cootract AF 61(052)185.
2 Dec 59. 9p. AFOSR-TN-60-913.
Order frtxn LQ mi$I. 80. p(i$l. 80 PB 152 540
Electrical stimulation of the prefrootal cortex of monkey
can produce alterations of behavioural capacity even at
amplitudes below those which produce motor effects.
In particular it has been found that stimulation in tiie
region of sulcuy twinclralis produces a severe deficit in
delayed alteration, whereas stimulation in the region of
sulcus arcuate is without such an effect. Auditorydls-
crimination performance is not affected by stimulation
in either regio*. The results are related to those de-
rived from surfical lesion studies, and it is suggested
that die Implanted ejectrode technique, insofar at it
can produce a "reversible lesion", would aQ)ear to be
a powerful tedmique for the analysis of cortical
function. (Author)
RofneU. (Italf).
BRAIN UNIT ACTIVITY IN RELATION TO BEHAVIOR,
by Gladfranco RUcci. Technical (final) rept. on Con-
tract AF 61(052)38. 31 Dec 59. 43p. 47 ref s . AFOSR-
TR-60-55.
Order from LCknl$3. 30, pi47. 80 FB 1S2 534
Habituation of the EEC arousal to differential conditian-
ing has been studied and compared with haUtuation to
aenaory stlmulf before conditioning has occurred. A
study was perfon-med by means of microelectrode* cf
the unit activity in the occipital cortex as evoked by a
photic condiciOTAng stimulus. Several patterns of ac-
tivity and their variations during conditioned reaponaea
are described. Modifications of tbe cortical responses
evoked by thalamic stimulation in the «enaory and
motor cortex during conditioning were investigated. A
diminution ot amplitude of the components of die re-
sponse during the conditioned movement is deecribed.
(Audur)
142
Pothology
ftrooke Army Medical Center, Pert Sam Houstoo,
Tex.
BURN CTRESS PSEUDOIXABETES, by Glen K. Amey.
Elinor Pearson, and Anne B. Sutherlsind. Rept. on
Radiation and Thermal Bums, Proj. no. 6X59-06-001.
Sep 59, 27p. 32 ref s. MEDEW-RS-2-59.
Order from LC ml$2. 70, pb$4. 80 PB 152 367
Tbe syndrome of bum stress pseudodlabetes was ob-
served In two patients early in the postburn course
while they were being given a high-carbohydrate,
high-calorie intake. The clinical and laboratory mani-
festations of tills syndrome are, in the order cf ap-
pearance, hyperglycemia, glycosuria without aceto-
nuria, high urinary specific gravity, and an intense
osmotic diuresis. This results in severe dehydration
with edevation of tbe nonprotein nitrogen, hemoglobin
and hematocrit as well as a high serum sodium and
chloride. If the syndrome is recognized early, it can
be aborted by discontinuing the high -carbohydrate
intake. If it becomes fully developed, appropriate
dierapy consists primarily of vigorous water replace-
ment and sufficient amounts of insulin to control the
hyperglycemia. (Author)
frooke Army Medical Center, Fort Sun Houstoo.
Tex.
GENBRAUZBD SWARTZMAN-LDCE REACTION
FOLLOWING SERRATIA MARCESCENS SEPTICEMIA
IN A FATAL BURN, by Charles D Graber, Wilfred
T. Tumbuscb and others. Rept. on Radiation and
Thermal Bums, Prof. no. 6X59-06-001. Aug 59, 20p.
2Srefs. MEOBW-RS-1-59.
Order from LC ml$2. 40, ph$3. 30 PB 152 366
Described are the clinical course, pathologic findings
and Immunologic responses of a severely burned
patient with a ^rf^ia roarcescens septicemia who
developed kidney lesions suggestive of the generalized
Sliwartzman reaction. Evidence is presented that a
combination of stress produced by the severe bum
trauma followed by endotoxemia due to ^ mii rr«>«c^
on the wounds, genitourinary tract and blood scream
produced this rare type sensitization seen In noan.
(Audnr)
National Reaearch Council. Washington, D. C.
AN ECOLOGICAL STUDY OF TOTAL MORTALTTy
AMONG CRJATEMALAN PRE-SCHOOL CHILDREN,
WITH SPECIAL EMPHASIS OH PROTEIN MALNU-
TRITION AND KWASHIORKOR, by Herbert Slutsky
(U. of Illinois). Rept. no. 6 on Foreign Field Re-
search Program, Cootraa Nonr- 2300(09). June 59,
221p. 70 refs. AD- 226 695.
Order from LCmiS9. 90, pfa$34. 80 PB 148 7M
Contents:
Enviroomental elements '
Adequacy of die Guatemalan diet
Medical aspects of protein malnutrition and
kwaahiorkor
Methods used in the investigatian
Villages examined
Analysis of information on tbe nutritional statue of
1, 193 pre-achool children
Analysis of tlie environmental factors ss-diey aflea
tbe mortality of the pre-school child
Pharmacology and Toxicology
Industrial Test Lab. , Philadelphia Naval Shipyard,
Pi.
TOXIC HAZARDS FRC»« THERMAL DECOMPOSI-
TION OF DYNEL-CHICKEN FEATHER FILLER FOR
CREWS' MATTRESSES, by M. S. Gabis. May 54, 16p.
2refa. Evaluation rept. no. 2203-C; AD-35 492.
Order from LC mi$2. 40, ph|3. 30 PB 153 010
This report released for sale to the public 30 Nov 60.
A mixture of shredded fibers intended for use as a
Slier for crews' mattresses was evaluated to deter-
mine relative toxic hazards, when exposed to elevated
temperatures. The fiber was a mixture of 50 percent
shredded dynel (copolymer of acrylonitrile and vinyl
cfaloride) and SO percent shredded chicken feathers.
For comparative purposes, two natural animal fibers
commonly used in bedding, chicken feathers and horse
teir, were similarly tested. The dynel -chicken feather
filler, when heated produces fumes which are rela-
tively toxic, but are comparable to those evolved from
tiie natural animal fibers, chicken feathers and horse
bilr. (Author) {
i
i'
Sperling Labs. , Arlington, Va.
1.6 HEFTADIYNE, ORAL LD50. RATS. DIPROPA^-
GYL ETHER, INHALATION LD50. NITROGEN-
GENERATED. RATS. Rept. on Contract Nonr- 2727(00)
(1959) 25p. j
Order from LC ml$2.70, p(i$4.80 PB 148 294
General and autopsy observjations are given. The re-
port is made up of tables covering the investigation.
Radiobiology
1
Behavioral Sciences Lab. . Wright Air Development
Div. , Wright - Patterson AFB, Ohio.
HUMAN FACTORS IN REMOTE HANDLING: SURVEY
AND BIBUOGRAPHY. by Billy M. Crawford and
D. Frederick Baker. Rept. on Human Faaors in Ad-
vaaoedFUght. July 60. 34p(. 177 refs, WADD Tech-
nical rept. 60-476; AD-242i524.
Order from LCmi)3. 00, p^6. 30 ^ PB 153 059
The state of the art in remote handling is assessed
and related to present and diture advanced system re-
quirements. Principal features and purposes of the
main types of remote -handling systems, including
■eaaory feedback provisions, are described. Human
agineering considerations related to equipment de-
sign, motor and sensory requirements of tasks, and
perceptual difficulties, together with possible solu-
tions, are discussed. Conclusions derived from ex-
Eience and experimental studies are Usted to stlmu-
! and coordinate further research and developnnent
cAorta. Possible implications of current remote-
handling concepts for planning nuclear -powered sys-
tems and space support units are given special con-
sideration. A bibliography representing a thorough
•creenlng of information soiirces in the United Sutes.
(Canada. Great Britain, and 'France is included.
(Author)
Biomedical Lab. , Wright Air Development Div. ,
Wright -Patter son AFB, Ohio.
INFLUENCE OT AET UPCW THE UPTAKE QP
IRC»4-59 BY THE RED BLOOD CELLS OF GAMMA-
IRRADIATED RATS, by R. L. Preston and A. P. Raun.
Rept. on Physiology of Flight. May 60, I3p. 13 refs.
WADD Technical rept. bO-395.
Order from OTS $0.50 PB 171 160
Four experiments were conducted to determine the
effects of AET (2-aminoethylisothiouronium-bromlde)
injections on the erythropoietic ability of rats follow-
ing acute gamma irradiation. Incorporation of iron-59
(Fe-59) into newly formed red blood cells was used as
the criterion of erythropoietic rate. When AET was
injected intraperitoneally 15 to 20 minutes before
radiation exposure, little difference resulted in the
depression of Fe-59 uptake 1 to 4 days after irradia-
tion between the nonprotected and AET-protected rats.
AET alone had no effea upon the incorporation of
Fe-59. Rats maintained for 31 days after irradiation,
however, showed a faster recovery d erythropoiesis
when protected with AET. Faster rates of erythro-
poiesis occurred in the irradiated rats than in the con-
trols 15 to 18 days after radiation exposure. Those
protected with AET incorporated Fe-59 into newly
formed red blood cells at a rate equal to that of the
nonlrradlated rats 2 to 3 days earlier than did non-
protected rats. (Author)
Cologne U . (West Germany).
INVESTIGATIONS ON THE PROBLEM OF FORMATICW
AND PATHOPHYSIOLOGICAL SGNIFICANCE OF BIO-
GENIC AMINES IN SUBLETHAL RADIATION INJU-
RIES, by Fr. Franzen. Annual rechnical rept. no. 1,
1 Sep 59-31 Aug 60. on Contract DA 91-591-EUC-1160.
[1960] 42p.
Order from LC nd(3.30, ph(7.80 PB 152 476
Midwest Research Inst. , Kansas City. Mo.
BIOLOGICAL EFFECTS OF RADIO FREQUENCY
RADIATION. BIBLIOGRAPHY. Rept. on Contract NObs-
77142. [1960] 40p. 459 refs. RADC TR-60-205.
Order from LC mi$3.00, ph$6.30 PB 152 349
Rome Air Development Center. Griff is s AFB> N. Y.
STUDIES CW THE BIOLOGICAL EFFECTS OF MI-
CROWAVE IRRADIATION OF THE DOG AND RAB-
BIT, by J. W. Howland and S Mlchaelson. Apr 59,
45p. RADC TN-59-99; AD- 212 110.
Order from LC ml$3. 30, ph$7. 80 PB 148 277
"Hils report describes a biomedical investigation into
the potential hazards of electromagnetic radiations.
Studies were conducted on dogs exposed to 100 and
165 mw/cm^ energies of 28(X) mc pulsed microwave
for periods varying from two to six hours. Emphasis
is placed on the characterization of the physiological
changes of microwave exposure in the dog and rabbit,
preliminary study of changes in hemodynamics as
correlated with temperature change, behavior of the
circulating blood elements, description of superficial
burns on skin surfaces, as well as preliminary ob-
servations on isolated physiologic and cytologic
processes. (Author)
143
National Cancer Inst . Bethesda, Md.
RADIOACTIVE SEED IMPLA>frATICW GUN AND
MAGAZINE LOADING DEVICE, by Herman D. Suit.
Invention rept. 17 Oct 60, 29p.
Order from LC ml$2.70. ph$4.80 PB 152 570
I
CHEMISTRY
Army Researcti Office, Washington, D. C.
ARMY RESEARJCH TASK SUMMARY. FISCAL YEAR
1960. volume; 2. CHEMISTRY. 385p.
P^71 001
Order from CT^ $3. 75
Contents: .
Analytical cbem|atry
Biochemistry [
Inorganic chemistry
Organic chemisitry
Physical chemistry, colloids
Physical chemistry, general and nuclear
(See also PB 16L 134)
\nalytical Chemistry
U. , Ljfn'ence.
PHOTCMETRIC TITRATION OF AROMATIC AMINES,
by Charles A. Rpynolda. Francis Hugh Walker, and
Evelyn Cochran. Repc on Contract AF 49(638)472.
22 Apr 60, 9p. 7 refs. AFOSR-TN-60-341; AD- 235641.
Order from LC «ii$l. 80, ph$l. 80 PB 149 065
A pbotometric titration procedure has been developed
for the titration pt aromatic amines which are unsub-
stltuted or whichi are substituted with alkyl, alkoxy,
hydroxy and halqgen groups. The amines are titrated
directly with acatic anhydride in pyridine. Alcohols,
phenols, and alinhauc amines do not interfere.
(Author)
Naval Researchi Lab. , Washington, D. C.
THE ANALYSIS OF CONTAMINANTS IN
AVIATOR S BREATHING OXYGEN, by R. B. Kaga-
rlse and R. A. Sounders. Final rept. 19 Oct 60, 22^
11 refs. NRL reflt. 5554.
Order from OTS $0. 75 PB 161 946
The problem of d^ermining the nature and anxxint at
trace impurities ^n liquid and compressed breathing
oxygen has been Itudied. The comaminants were col-
lected and concentrated by an adsorption-desorpcion
cycle employing 4cuvated carbon as the adsorbing
material. A comtiination of infrared spectrocopy and
gas chromatograi^y was used for the qualitative and
semiquantitative Analysis at the contaminants. Usii^
this approach, it has been possible to detect and
Identify impurities at concentrations as low as 0.5
parts per billion. The observed contaminants are
primarily hydrocarbons in the Ci-C6 range and in-
clude paraffins. c|lefins, and alkynes. In most
Instances, the totkl concentration d impurities, orher
than methane and carbon dicocide, falls in the one to
two parts per million range, well below the toxic
level at any single observed contaminant. Two sam-
ples at odorous compressed oxygen were analyzed
and found to contain amounts of acetylene and nitrous
oxide in excess at military specifications. However,
the concentrations were far below the toxic level,
and neither compound is panicularly odorous. An ei-
aminatlon ot the infrared absorption spectrum of
liquid oxygen per se, using a 25-cm cell, did not re-
veal the presence al any material not identified by
the absorption-desorpcion sampling procedure. The
sensitivity ot this method was estimated to be 0. IS
parts per million. (Author)
Springfield Armory, Mass. 4
DETERMINATI(»I OF SULPHATE IN CHROMIUM
PLATING SOLUTIONS, by C. M. Hanna. Rept. on
Studies fOT the Improvement of Small Arms Weapons.
10 Feb 60, 8p. SA-TR16-1115.
Order from LC mill. 80, phj 1.80 PB 152 393
An investigation waa made to determine the accuracy
,ai an alternate, rapid, gravimetric method of sulphate
analysis in chromium plating solutions by reduction of
chromic add by use of sodium nitrite in place of ethyl
or laopropyl alcohol. The accuracy of the test results
obtained with the alternate method compares favorably
with the accuracy at the teit results obtained with the
sundard method. A considerable amount of time is
saved with the alternate method analysis. Suggested
procedure for sulphate determination is given.
(Author)
. - I .-
Inorganic Chemistry
Illinois Inst, of Tech. , Chicago.
SYNTHESES WITH CARBIDES, by Sidney L MlUer.
Final rept. for 1 Feb 57-31 Aug 60 on Contr^t AF
49(638)39. Sep 60, 7p. AFOSR TR-60-137.
Order from LC mi$l. 80, ph$l. 80 PB 152 528
Ir(CO)2Dipl2- The different oxidation numbers of
Iridium in this compounds are temptatively related to
ihe effective electric charge ot the meul. (Author)
The objective of this research was to develop synthi
with the carbides AI4C3, CaC? and Mg2C3. Numerous
negative results were obtained in attempts to utilize
CaC2 and AI4C3 so that no work was done with Mg2C3.
Reactions of Diazonium Salts were tried with more re-
active or gano- metallic 8, but again the results were
unpromising. More tractable systems yielded publish-
abla results.
MiUn U. (Italy).
REACTION OF POTASSIUM TETRAIODO DICAR-
BONYLIRIDtATE (III) WITH TRIPHENYLPHOSPHINE
AND ANALOGOUS UGANDS, by Maria Angoletta.
Technical (Scientific) note no. 3 on Contract
AF 61(062)83. 1 May 60, 12p. 3 refa. AFOSR TN-
60-460.
Order from LC mi$2.40, ph$3.30 PB 152 503
iar(CO)2l4 with tryphenylphoephite, P(0R)3 triphenyl-
phosphine PR3 triptenylarsine A8R3 p-toluidine (T)
and a a-dipyridyl(Oip) gives the following compounds:
Ir(P(OR)3]2l3 : Ir<CO)2(PR3)2l and Ir(C0) (PR3)2i2 :
Ir<CO)2(A8R3)l3 and lr(CO) (AsR3)2l3 : lr(CO)2T2l2 :
144
Organic (Ihemistry
Oatral Inst, for Industrial, Research (Norway).
TUB STRUCTURE OF LJNBAR POLYMERS: LOWER
■-HYDROCARBONS, by Nlco) Norman and Hans
Muhisen. Final technical rept. 1 July 59-30 Sep 60. (Mi
Oootract DA 91-591'EUC-ll^. Oa 60, 98p. 29 refs.
Orier from OTS $2.50 , PB 171 181
11» cryatal structures of n-(ictane, n -heptane,
■-faexane, and n-pentane have been determined, using
riagle crystal dau, Cu - radiation. In the case ot
i-ocune the structure haa bien refined in two projec-
HoM by the method at least squares, whereas for
■-bnane generalized proJect|ona have been used to de-
IKmlne the X -coordinates, t&e (yz) -projection beii^
nflaed by least squares. So far the n-heptane and
i-pentane structures have been studied in the (yz)-pro-
Jtctkn. The structure of the. four mentioned paraffins
IM also been studied in the liquid state by means of the
ndial distribution method. The radial distribution
canres are dominated by broad peaks due to the packing
of the molecules. Attempts have been made to deter-
Blne the shape of the molecujes by utilizing the in-
tensities in limited angula» regions. The investiga-
tkns seem to confirm the usual aaaumption that the
molecules are in their extended trans configuration in
(he liquids. (Author)
I ■<
Prltz-Haber-Instltut der Max-Planck-Gesellschaft,
BerUn-Dahlem (West Germany).
THB DEPENDENCE OF THE 2ND VIRIAL CC«FFI-
CENT ON THE CONSTITUTION OF THE END-
GRCXJP OF THE MACROMOLECULES, by Hldeto
Sanbayashl andK. Ueberreiter. Final technical rept.
io. 1, Aug 59-Aug 60, on Corttraa DA 9I-591-EUC-
1158. 31 Aug 60, 8p. 3 refs.
Order from LC ml$1.80, pli$1.80 PB 152 218
Tfcis report describes the polymerization at styrene
ilth certain end groups and a cryoscopic ap>paratu8 for
the determination of the 2nd vlrial coefficient. The
end groups 0* the polymer originate from free radical
Idtlatora which are used during polymerization. The
ddarlnes in the end groups reaa with Na202 to farm
sodium chloride, so that the eM groups can be deter-
ntud by quantitative analysis. A semimicro method
rfhlgh accuracy, which is ^sed on a Wheatstone
fcridge and galvanometer syptem with thermistors In-
Mad of a Beckmann theniKin^er to measure the
— perature, was developed, i
Illinois Inet. of Tech. , Chicago, IlL
IBACTION OF SILVER ACETYLEDES WITH ACYL
PTRIDINIUM SALTS: N-BENZOYL-2-PHENYL
nHYNYL-l,2-DIHYDR0PYlllDlNE, by Toahlo Agawa
■d Sidney L Miller. Technical rept. na 2, on Con-
tact AF 49(638)39. Dec 59, 2ip. 36 refs. AFOSR-TN-
<0-l56; AD-234 701. ;
Mer from LC ml|2. 70, phH 80 FB 148 680
4
The reaction between certain halldes, pyridine and
silver acetylldes leads to the system N-acyl 2-alkynyl-
1, 2-dlhydropyrldine (0 as well as acylacetyleoes as
coproducta. Baals hydrolysis of I gives the alkenyl
pyridines (in). RCH = CH(2-C5H.N), while potassium
hypobromite or acid hydrolysis pyea the alkynes,
RC3C(2-CcH4N): these constitute new paths to these
unsaturate!! compounds. Reaction of the dlene (0 widi
malelc anhydride leads to the isoquinuclidine system
(2-azabicyclo(2.2>2)-7-octeoe> from which the azabi-
cycIo(2<2-2) octadlene can be made. (Author)
Pennsalt Chemicals Corp. . Wyncbnoor. Pa.
AN INVESTIGATI(»< INTO THE REACTICWS OF
METAL COMPOUNDS WITH BIFUNCHONAL INOR-
GANIC MOLECULES, by John C. Grlgger and
H. C. Miller. Technical rept. no. 10 on Coittraa
Nom-2687(00). 2 Nov 59. 28p. IS refa. AD- 230 117.
Order from LC ml$2.70, phM- 80 PB 150 485
Experiments were conducted on the preparation of
thermally stable, straight -chain polymers coittaining
chelated meul atoms in the backbone of the polymer.
The 2 claaaea of meul compcMinds Investigated con-
sisted of (1) a group containing oxides, chlorides,
sulfides, and carbonates; and (2) the more reactive
alkoxides, and the very reaaive alkyls. A simplified
thermal analysis and reaction apparatus (RPA) was set
up in which, normally, powder mixtures cf the metal
compound and a ligand material were heated to about
3S(fiC at reduced pressure and in an N-flushed atmos-
phere. Thermogravimecric analysis (TGA) made on
the Chevenard thermobalance supplemented informa-
tion from the RPA. Producta of 54 reactions of meul
oxides, carbonates, and sulfides with NH2SO3H and
NH2CH2SO3H. with one exception, were H2O- sensi-
tive and thermally unstable. Trimethyl aluminum waa
reaaed with aulfamic acid (I), aminomethanesulfonic
<cid (II), and dimethylaminomethanesulfonlc add (IO).
No reaction waa apparent with I; a violent reaction
occurred with 11; and most of the reaction with in
occurred at 10° to 30'<; with a mild exothermic heat
of reaction. Cleavage of m was concluded to occur
during the reaction.
St. LouiaU. , Mo.
SYNTHESIS AND REACTIC»6 OF 2-CHLORO-
1,3. 2-DlAZABOROLINE. by Leo F. Hohnstedt and
Angelo M. Pellicdotto. Technical rept. no. I on Con-
tract Noor-2793(00). 30 Dec 59, lip. 8 refs.
AD-230 544.
Order from LC nil$2. 4a pi4S.30 FB 152 065
A slurry of a.-C(^^HH2>2 2HC1 in chlorobenzene was
treated at room temperature with cold BCI3 to produce
a white, chlorobenzene insoluble material (I)
(m. p. 234. 6°). This material, which reacted vigor-
ously with H2O, exhibited a B and CI cootent corre-
sponding to that calculated for C(Jti4iNli2)2 BCI3 When
I was heated in gently refluxing chlorobenzene, HCl
was given off and a straw-colored solution was formed
After HCl evolution was complete and no solids re-
nMined. quantiutlve recovery of C6H4(NH)2 BQ (U)
was obulned by cooling the solution and strlppii^ off
the aolveitt. The identity of U was supported by iu
145
method of formkcion. analysis, and its conversion to
the previously characterized 2-phenyi- and 2-butyl-
1.3, 2-diazaborDline. 11 reacted vigorously with
NaHl4 in diechyrleneglycol dimethyl ether to give 100%
yield of C^4.1*i)jai (HI), a light tAn aolid. m. p. 79-
80PC, which was readily soluble in benzene, and had
no appreciable vapor pressure at room temperature.
m reacted readily with H2O to liberate H. however
prolonged treattnent with a methanol -H20-Ha mix-
ture at room temperature was used to achieve com -
plete hydrolysi* of the B-H bond.
Physicoi GiemUrry
Aerojet-Gem'al Corp. , Azuaa, Calif.
HNBTIC CTUCIES OF DCSAPPEARANCE OF HY-
DROXYL RADICALS IN ICE AT LOW TEMPERA -
TURBS. by J. M Ploumoy. L. H. Baum and others.
Repi. oo Coacr«a AF 18(603)110. Aug 59, 13p.
7 refs. Aerojetj-Geneml TN-31; APOSR TN-59-539;
AD- 216 556.
Order from LC'mi$2.40, pii)3.30 PB 148 289
The kinetics d the disappearance of bydroxyl radicals
In irradiated ict has been studied at aeveral tempera-
tures in the rai^ 0* 77 to 108°IC, using electron-
paramagnetic- resonance techniques. The reaction
foUows the rate law d(OH)/dt - MOHr where
k- 6x 10l2eip(-6000/RT)(m/irf sec"!, ^g
postulated that the rate-determining process is dif-
fusion or migration at the radicals through the ice.
(Author)
Anftioch Coll. „ Yellow Springs, Ohio.
THE physical; CHEMISTRY OF WATER SOLU-
TlOie AT HlCtl TEMPERATURES AND PRESSURES.
Pinal rept. I July 55-30 June 59. on Contraa
AP 18(600)1490, [1959] I24p. 113 refs. AFOSR-TR-
59-74; AD- 220 103.
Order from LC mi$6. Sa pt4l9. 80 PB 149 701
Contents:
Hydrotbermal reactions under supercritical conditions.
V. Reactions between silica and alkaline earth metal
aalts. pub. in the Jul. of Physical Chemistry 62: 1066,
1088. 1958
Determination of gemamium by the heteropoly blue
method, pub. In AiMlytical Chemistry 30:1314. 1316,
1958 I
Hydrutfaermal rtactions in the Na20-Ge02 system, pub.
in the Jnl. at the American Chemical Society 80: 1536.
1539, 1958
A chalcedony -lit^e variety at germania, Ge02> pub. in
American Mineralogist 43:580-584. 1958
Tetrasodlum Rmeagermanate, U»^Gei9O20AetTAgaaal
form. pub. in Analytical Chemistry 31:315-316,
Feb 59
Hydrothermal reactions in the Na20-Ge02-H20 system
n. IR studies at Ge02
ni. IR studies at the alkali germanates
The effect of pH on the formation of diaspore and
corundum
A study at the effect of pH and fluoride ion on hydro-
thermal reactions of silica and Al
The conductivlt} of dilute NaCl solutions under super-
critical conditiona
146
Applied Physics Lab. , Johns Hopkins U. , Silver
Spring, Md.
MOLECULAR DIFFUSION STUDIES IN GASES AT
HIGH TEMPERATURE. RESULTS AND INTERPRE-
TATION OF THE CO2-O2. CH4-O2. H2-02, CO-O2.
AND H2O-O2 SYSTEMS, by R. E. Walker and
A. A. Westenberg. Rept. on Contraa NOrd-7386.
Aug 59, 32p. 18 refs. CM-959; AD- 229 021.
Order from LC ml)3. 00, ph$6. 30 PB 150 781
Experimental measurements of the binary diffusion
coefficients for the CO2-O2, CH4-O2, H2-O2, CO-O2.
and H2O-O2 systems over the nominal temperature
range 300-1000^ are reported. The measurementa
were made by the point source technique. The data
have been analyzed in terms of Intermolecular poten-
tial energies and the rigorous k^petic theory by using
the Lennard-Jones (12-6), modified -Buckingham
(Exp-6). point center of repulsion (inverse power),
and the exponential repulsion potential energy func-
tions. It is shown that all four of these functions are
capable of fitting the diffusion data with about the
same precision (within experimental error). However,
the potential energy values themselves which are cal-
culated from these four different fined models are
shown to be widely at variance- -especially in the
range of interaction corresponding to the lower tem-
peratures. Thus, these results provide an example of
the high degree of ambiguity (previously noted by
several others) involved In deducing intermolecular
potential energies from transport data. The use of
such fitted potentials to extrapolate transport data to
higher temperatures, on the other hand, is probably
a more reliable procedure, and diffusion coefficients
for the above five gas pairs (in their unexclted, un-
dissociated states) have been estimated to 3000^^
from the potentials based on the 300-1000°K
measurements. (Author)
i
Armour Research Foundation. Chicago, 111.
DEVELOPMENT OF A BALLOON-BORNE PARTICLE
COUNTER, by A. Lieberman. Final rept. for
15 June 59-31 Aug 60. on Contract AF 19(604)5895.
Aug 60. 28p. Rept. no. ARF 3157-14; AFCRL TR-
60-404.
Order from LC mi$2. 70. ph$4. 80 PB 152 244
The abjective of this project was the development of a
laboratory prbtotype light scattering single particle
counter which would demonstrate the feasibility of
constructing flyable balloon-borne instrumentation to
analyze particles 1 micron and larger at altitudes
ranging from 30, 000 to 100, 000 ft. Design drawings
for such flyable instrumentation were prepared. In-
vestigation of air handling, optics, and electronics
were carried out. It was concluded that an unsheathed,
Donlamlnar air stream would permit straightline par-
ticle flow in its center. A large diameter intalte and
flow system minimizes the effects of wall depositifn.
An optical design that permits a viewing volume of
50 mm^ and a signal-to-noise ratio of 2. 5: 1 for 1 mi-
cron particles was used for the prototype. Electronic
circuitry was used that permitted measurements of
signal -to-noise ratios and pulse shape for several
operating conditions. Sufficient information was cb-
uined to permit establishing feasibility of design and
the layout of transistor logic from the laboratory pro-
totype data. Based on this information, working draw-
ings for the optics and air handling sections have been
prepared and level detectors circuitry has Hten bread-
boarded for the pulse height analyzer. (Author)
I '
Chicago U. . 111.
MASS SPECTROMETRY APPLIED TO HIGH TEM-
PERATURE CHEMISTRY; by Mark G. Inghram and
Jean Drowart. Technical rept. no. 1 1 on Contract
DA 11 -022 -ORD- 1993. [1959] 44p. 137 refs. OOR rept.
1543. 16P: WAL 803/19-5; AD-228 618.
Older from LC mi$3. 30, p»ii7. 80 PB 152 679
This report released for sale to the public 16 Dec 60.
As a result at the success which the mass spectrom-
eter has had in high temperafture studies, this sum-
mary is presented to show what the technique is, what
it can do and what its shortcomings are. To illustrate
the importance of the method, a summary of the vapo-
rization results obtained to data is given. A section is
also Included to suggest a nu!mber of additional appli -
cations of mass spectrometry to high temperature
chemistry. (Author) '
Chicago U., Urbana, HI.
RADIOLYSIS OF ARALJCYL KETONES, by Weldon G.
Brown and Donald J. Coyle. Rept. on Contract
AF 33(616)3875. Aug 60, 15p. 1 ref. WADD Technical
rept. 60-41. ^
Order from OTS $0. 50 I I PB 171 156
Ftoduas from the gamma irradiation of n-butyro-
phenone, Isobutyrophenone, and benzoylcyclopropane
btve been examined. Total yields of gaseous products
decline markedly in the order named; G values for total
gas, at the lowest dose employed, namely, 6 x lO^^
ev/g, were 3.8, 0.62, and 0.13, respectively. Paral-
lel studies of the decomposition of these ketones by
ultraviolet light have been pwrformed. The predomi-
nant reaction in both radiolysis and photolysis of
o-butyrophenone is a splitting to produce ethylene and
acetophenone. This is presumed to be a molecular
excitation process of the Norrish-Bamford type. Iso-
butyrophenone gives rise to a variety of gaseous prod-
ucts, in both radiolysis and photolysis, believed to
arise chiefly ttom a splitting to benzoyl and C3 radi-
cals. Benzoyl cyclopropane is remarkably resistant to
radiolytic decomposition; photolysis studies have not
been completed. (Author)
Florida State U. , Tallahassee.
PROTON TRANSFER STUDIES BY NUCLEAR MAG-
NETIC RESONANCE. L DIFFUSION CONTROL IN
THE REACTION OF AMMONIUM ION IN AQUEOUS
ACID, by Merle T. Emerson, Ernest Grunwald, and
Robert A. Kromhout. Rept, on Contract AF
49(688)287. [1959] 31p. 23 refs. AFOSR TN-60-159;
AD-235 140.
Order from LC miW- 00, ph>6. 30 PB 148 678
A study was begun of the dependence of the proton
transfer rates of ammonium salts in acidic soluticxis
on the acid and base strengths of the proton donor and
acceptor. The rate constants were determined by nu-
clear magnetic resonance tecjhniques for tiie reactions:
mt +H2O J5Ml3-»-H30-»-;'NH3-»- H3O il^ NH4 -*-
Hrg; and Ij^f -^HH^^^ 1*13 H-NH^ in aqueous acid at
23"C The order of magnitude of k. ^ and k^ suggested
that these reactions are diffusion- controlled. Calcu-
lation of the frequency of encounters by application of
tlie Debye-Smolucbowski theqry showed that k_4 is
consistent with reaction occurring whenever H30-tai]d
NH3 are next- nearest neighbors. The steric factor for
this reaction appeared to be unity. It was concluded
that the reactanis were oriented during their ^iproach
so that the unshared electrons of the NH3 faced an
acidic H. To interpret k^, a mechanism was assumed
in which NHo and NH^1)ecame next- nearest neighbors
by sin[q>le dufuaion, aie jump to a nearest -neighbor
site then required a somewhat higher activation energy
than simple diffusion because NH3 had to displace a
tightly-bonded H2O molecule The reaction with rate
constant k^ was activation- controlled. The n^ative
salt effect on k^ suggested diffusion of charge in the
transition state. (See also FB 148 679).
Florida Stat^ U. , Tallahassee.
PROTON TRANSFER STUDIES BY NUCLEAR MAG-
NETIC RESCWANCE. IL RATE CONSTANTS AND
MECHANISM FOR THE REACTKW, CH3NH,^ tOH,
NH2CH3, IN AQUEOUS ACID, by Ernest Gnfiiwaldf
Photios J. Karabetsos and others. Rept. on Contract
AF 49(688)287. [1959] 2^ 15 refs. AFOSR TN-60-15a
AD-235 155.
Order from LC mi$2. 70, phH 80 PB 148 679
Rate constants were measured by precise nuclear nug-
netic resonaiKe techi^^gues for the reactions,
CH3l:iH3+ -»-NH2CH3 ■^OH3MH2 -t-H i5h2CH3' *™*
CH3MH3 + OH2 -4- NH2CH3 *4 CH3lffl2 -♦- HOH 4-
HNH2CH3, in aqueous acid at 25°. The ratio, kg/ky,
remmned virtually constant between 1. 7 and 8. 1 M
concentration of CH3NH3CL The rate constants were
inversely proportional to the viscosity of the solution,
and were extrapolated on this basis to infinite dilution
to yield die values, k^ - 4.0 x 10^ sec'^ M"^ and
and k^ = 5. 3 X 10® sec"^ M'^ at 25°. Acid dissocia-
tion constants, densities and viscosities for 1. 7 to 9M
solutions of CH3NH3CI in water were measured alsa
Measurements of the water activity of these solutions
showed that the mean ionic molal activity coefficients
of CHoNHoCl were virtually constant over the entire
range. The magnitude of k7, as well as the constancy
of ^j/^f.' indicated that the most probable rate-deter-
mining step for the reaction with rate constant, k-, la
proton transfer from a water molecide in the solvation
shell of CH3NH^to a. molecule of CHoNHj. to produce
the triple ion, CH3NH.,. OH. H^<HjCH3. lAuthor)
(See also FB 148 678),
Dlinois U. . Urbana.
THE INFLUENCE OF DOUBLE LAYER STRUCTURE
ON THE ADS0RPTIC»4 ISOTHERM OF PALMITIC
ACID, by H. A. Laltinen and R. F. Scarr. (Doctoral
thesis). Rept. on Surface and Interface RienOmena of
Matter, Contract AF 33(616)5446. July 60, 68p. 45 refs.
WADD Technical note 60-104.
Order from OTS $1. 75 PB 171 141
The capillary activity of palmitic acid at a stationary
mercury electrode was to be investigated by construct-
ing the adsorption isotherm by means of double layer
capacity measurements at various potentials. Suc^data
would permit later interpretation of capacitance measure-
ments for a mono- layer of oriented organic molecules.
The influence of double layer structure, which is a
function of supportii^ electrolyte concentration, was
also to be studied. Tlie double layer is compoaed-of
147
both an Inner aid a diffuse region, fbr each d which a
unique capacitatice may be defined, k it the present
hypochesis that these twocapacitancesmustbe distin-
guished In calculating adsorption isotherms. (Author)
Mlnnesoca U. < Minne«paUs.
DIPPUSION IN INHOMOGENEOUS MEDIA, by Stephen
Prager. Technical repc. no. 1 on Contract
AP 49<638)720. Mar 6a 2ap. 5 refs. AFOSR TN-
60-187; AD- 234 584.
Order from LC mi$2. 7a \*S4. 80 PB 148 676
Metlwds are given for the calculation of effective dif-
fuakn coeffidetits for inhomogeneous media, in which
the actual dlffulion coefficient varies from point to
point in a random nuinner. An exact result is obtained
in the form of «i infinite series involving correlations
between diffusion coefficients at n different points. A
procedure for <|eriving approxlniate expressions in-
volving only to«t -point correlations is also developed,
and applied, in particular, to the Important special
case at dUtuaioft through a porcxis material. (Author)
Naval Research Lah. , washli^iion, D. C
IGNITION STunma part vl the effect of
CHHk41CAL STRUCTURE ON THE SPCM^TANEOUS
K3Nrn<»l OF HVDROCARBCWS, by W. A. Affens.
J. B. Johnson. a«id H. W. Carhart, Interim rept.
3 Nov 60, 31p. 32 refs. NRL rept. 5566.
Order from OTSj $1.00 PB 161 %7
^xxxaneous ignftton properties at the bexane isomers
and other selected pure hydrocarbons in air were stud-
ied with the view to correlating these flndii^s with
molecular structure. Specifically, the influence at
chain length, chtin branching, unsaturation, and at
cyclic ard aromatic structures on the spontaneous Ignl-
tloo processes i^erc investigated. Minimum ignition
temperature in a|r for cool- or hot-flame ignition, mini-
mum reaction tetnperature, pre- ignition temperature
range, maximum temperature rise above base tempera-
ture, and oxygen consumption all appear to show corre-
latioo with ease cf oxldatioa and i^ition. h general,
decreasing chain length, addition of methyl groups, un-
saturation, and particularly chain branching were
found to increase oxidation and ignition resistance at
aliphatic hydrocarbons. Pre-ignition temperature.
raqges for highly branched paraffins were found to be
•bout six to seven times that at straight chain com-
pouids. The alldycUc hydrocarbons were found to be
more resistant to oxidation than the analogous straight
chain compounds, and the aromatic compounds were
found to be the most resistant at all the compounds
studied. Side chains decreased oxidatloa resistance for
both cyclic and aromatic hydrocarbons, and this effect
increased with chain lengtfu The cycloparaffins were
found to be unique in having exceptionally short pre-
ignition temperaoire ranges and exceptionally long
ignMon delays. Cyclopentane, however, was found to
be an exception, and its ignition characteristics differed
markedly from that at the other cyclic compounds in-
vestigated. (See tlso PB 161 105)
New York Sate Coll. of Ceramics. Alfred U.
DEFECT STRUCTURE AND CATALYSIS, by Thomas
J. Gray. Rept. on Contract AF 49(638)288. Sep 60,
16p. 27 refs. AFOSR TN-60-644; AD- 243 545.
Order from LC mi$2. 40. ph$3, 30 PB 152 344
A detailed general nKxlel for a catalyst surface based
on electron energy states in a semiconducting solid Is
presented leading to the development of a broad quali-
tative theory of electron transfer processes at cataly«
surfaces. Correlation between semfconducting. photo-
condtx:ting, and magnetic properties during the adsorp-
tion, reaction, and desorption processes are estab-
lished experimentally. These relationships are em-
ployed to induce modified catalytic properties in a
variety of materials. The significance of photo-exci-
tation of electrons is considered in relation to photo-
adsorption, photo- desorption, and photo- catalytic'
phenomena, particularly polymerization. (Author)
Pennsalt Chemicals Corp. , Wyndmoor. Pa.
THE THERMAL yTABILITY OF METAL AMMINES.
III. PLATINUM (II) AMINES, by B. P. Block, E. S. R<xl\
and Joseph Simkin. Technical rept. no. 11 on Contraa
Nonr- 2687(00). 31 Dec 59, 9p. 5 refs. AD- 230 926.
Order from LC mi$ 1.80, ph$ 1.80 PB 152 091
The generally accepted temperature at 250OC. for the
conversion of [Pt(NH3)4)Cl2.H20 to trans -
[Pt(NH3)2Cl2] leads to extensive decomposition to ele-
menul Pi in a relatively short time. Although standard
thermogravimetric analyses indicate that trans -
[Pl(NH3)2Cl2J is stable to 270°C. , constant - tempera-
ture in furnaces indicates a much lower practical de-
composition temperature. At 20(A3. the thermal de-
composition 18 slow enough that it is possible to effea
an essentially quantitative conversion of
[Pt(NH3)4]Cl2.H20 to trans - [Pi(NH3)2Cl2). (Author)
Pennsylvania State U. , University Park.
SEQUENCE AND SPACING OF n.-* tf* TRANSITIONS
IN s-TRIAZINE, by J. S. Brincn and Uonel Goodman.
Technical rqx. na 1 on Bonding in Nitrogen and Boroa
Rings for 15 July 58- 15 July 59. Contract Nonr-65621.
[1959] 16p. 19 refs. AD- 233 723.
Order from LC mi$2. 40, ph$3. 30 PB 148 726
Calculations are made by the MO method including
zeroth- order configuration interaction of the lowest
singlet and triple (n, Tf •) sute energies in s-triazine.
The four lowest singlet- singlet excitations comprisii^
one allowed and three forbidden transitions are pre-
dicted to be grouped within 1 e. v. The lowest excita-
tion is tentatively assigned to ^E''^— ^A^" (forbidden).
The lowest singlet- triplet excitation is predicted to be
orbitally forbidden (^E" ^Aj') with a split of /vO. 8
e. V. from the corresponding singlet, and slightly
lower in energy than the lowest energy C^-*lf*) multi-
plicity-forbidden transition. (Author)
Pennsylvania U. , Philadelphia.
THE DETERMINATION OF THE COVERAGE OF
CORRODABLE METALS WITH HYDROGEN DURING
ELECTROLYTIC EVOLUTICHsl, by J. 0'M.Bockris
and R. Thacker. Technical rept. no. 3 on Contract
Nonr-551(22). 31 Dec 59, 51 refs. 79pj AD-234 049.
Order from LC ml$4. Sa ph$l2. 30 PB 152 127
148
Tte following methods were established for the deter-
mination of the coverage with atomic H of a metal
evolving H: (I) galvanostatic and potentiosutic trans-
ient methods; (2) direct measurement of the adsorbed
H by transfer from a continuous rotating wire passing
through 2 vessels; (3) measui-ements involving the ad-
dition of supplementary amounts of atomic H to the
aurface of an electrode (from the solution or through
the metal); (4) direct measurfement of pressure change
in die gas phase over a solution in contact with a metal
of high surface area; (5) measurement of the variation
of the permeation rate with current densitr. and (6)
measurement of the diffusion coefficient of H in Fe
tnd calculation of the surface concentration during H
evolution from the equilibrium between the adsorbed
ffA adsorbed H and the concentration of H just inside
die metal. Preliminary investigations were made of
die rate of permeation of electrolytic H with current
density, through Fe. Pd, Ni. i Cu. Ti, Ta. and U by
usii^ a technique which involved intentional conumi -
nation of the surface. Fe, Pd, and Ni were readily
permeable to electrolytic H;
■lightly permeable.
Cu, Ti, Ta, and U were
Pennsylvania U. . Philadelphia.
EXPERIMENTAL AND THEORETICAL RESEARCH
TO SYNTHESIZE FREE RADICALS OF THE
AMINIUM SALT AND HYDRJAZYL SERIES, by Robert
I. Walter, Haverford Coll. yearly progress rept.
DO. 2, 15 Sep 58-15 Sep 59, on Study of the Preparation
•ad Physical Properties of Stable Organic Free Radi-
cals. Contract DA 36-039-SC-74917. [1959] I6p.
4 refs.
Order from LC mi|2. 40, ph^3. 30 PB 148 976
Portsmouth Naval Shipyard, i N. H.
HYDROGEN EVOI.UTION-ZINC ANODES SMALL
SCALE TANK EXPLORATORY TEST, by Roger L.
Portier and M. Anderson. Technical rept. Feb 56,
I5p. 3 refs. PNS Test T-516. Supp. 1; AD-113 786.
Order from LC mi$2. 40, ph$3. 30 PB 149 056
Stanford U., Calif.
PROTON RESONANCE SHIFTS IN PYRENE MONO-
NEGATIVE ION AT 4.20K, by M. E. Anderson.
P. J. Zandstra, and T. R. Turtle, Jr. Rept. on Para-
nugnetic Resonance. Contract AF 18(603)131. Aug 60,
'5p. 4 refa. Technical note np. 131-8; AFOSR TN-
60-1068.
Order from LC mi^l.SO, pb$1.80 PB 152 488
Theoretical Chemistry Lab, , U. of Wisconsin,
Madison.
SOLUTIONS FOR COMPLEX SYSTEMS OF CHEMICAI
REACTION KINETICS. PART I. AN IRREVERSIBLE
UNIMOLECULAR REACTION FOLLOWED BY A SEC-
OND IRREVERSIBLE UNlMQLECULAR REACTION,
SUPPLEMENT I, by Daniel D. Konowalow, James E.
Blair and others. Rept. on Chemistry of Flames and
Related Reaction Kinetics Contraa AF 33(616)3413.
Aug 60. 32p. 1 ref. WADC Technical note 59-243.
Pt. I, Suppl. I. j
FB16140eS-I
Order from OTS $1.00
In a previous report (PB 161 408), the analjrtical solutions
of the rate equations for the system A >B »C
were explored for diaracteiistic features which are
useful to the klnetlcist in determining the rate constants
from fragmentary experimental data. The present rate
amplifies and generalizes the earlier findings by intro-
ducing a reduced time which facilitates the problems of
curve fitting. In addidon, certain simplifying approxi-
mations are discuss^ and the limits of their validity
are defined. (Atxbor)
EARTH SCfENCES
Marine Physical Lab.. Scrippe Inst, of Oceanography
Lajolla, CaUf.
THE GEOMORPHOLOGY OF ABYSSAL PLAINS IN
THE NORTHEAST PACIFIC OCEAN, by Robert J.
Hurley. Rept. on Contraas Nonr -233(43), 2216(01),
and 2216(05). 1 Feb 60, 109p. 97 refs. SIO Refer-
ence 60-7; AD- 238 069.
Order from LC mi$5.70, phlH6.80 PB 148 240
The northeast Pacific Ocean contains the most exten-
sive abyssal plains in the Pacific basin. An effort to
describe the features of these plains and thereby learn
more about the processes which produced them is
studied. The continental slopes bordering tlie region
on the east are characterized by a steep lower escarp-
ment, rising to a ridge separated from the upper part
of the aidpe by a terrace or depression. This profile
is quite different from that of the east coast of the
U. S., but closely, resembles the shape of the surface
of the basement there. The northwestern part of the
area is bordered by the Aleutian Trench. The trench
floor is flat and snKXXhly graded, indicating sediment
flow toward the south and west. The abyssal plains in
the northeast Pacific are found to be steeper, up to
1.7 M/KM. The Aleutian Abyssal Plain, although
sloping away from the land, is isolated from it by the
Aleutian Trench. This plain is interpreted to be relict
Several channels are found on these plains. There are
sufficient data on one of them, Cascadia Channel, to
estimate the velocity of flow using a modified Chezy
formula. The velocities are dependent on the density
of the flows and on the roughness of the channel, but
reasonable estimates suggest a maximum of nearly
20 kn and several values near 14 kn. Inertial losses
in the sharp turns of the channel, and losses by
mixing due to breaking gravity waves at the surface df
the flow, appear to be snull at the deduced velocities.
(Author)
Climatology and Meteofx>logy
Air Weather Service, Scon AFB, 111.
WEATHER: FORECASTING ALTIMETER SETTINGS.
1 Sep 60, 38p. Air Weather Service Manual 105-54.
Order from LC ml$3. 00, ph$6. 30 PB 152 042
Four methods, differing mainly in their input-dau re-
quirements and their conditions of applicability, are
presented. The first method, which is the shortest
and the easiest to use, gives acceptable accuracy at
most sutions below 1000 feet elevation and also in
149
many caaea at ptaticxia above 1000 feet. The second
method ia more general and aomewhat longer. It is
deaigned primarily for uae at stationa above 1000 feet
in caaea when targe pressure and/or temperature
changes are expected during the forecast period, al-
riKX^ it nuiy be used at any elevation. Both the first
and second methods require concurrent values of sea-
level pressure and altimeter setting at the forecast
sution. The tHird method hlaa been developed for use
when concurrcM values d sea -level pressure and
altimeter setting are not available. It may be used at
any elevation. The fourth method enables the fore-
caster to convert a forecast altimeter setting at one
Btatlaa to a fcnecast altimeter setting at a nearby
station. Step- l>y- step procedures are outlined for each
method, and the necessary nomograms and a uble
(Appendix A) are included. A theoretical discussion of
the basis for the methods is presented in Appendix B.
(Author)
Arctic Inst. ^ North America, Washington, D. C.
A PRELIMINARY INVESTIGATION OF THE METE-
OROLOGICAL CONDmONS Oti THE CHAMBER LIN
GLACIER, 19S8, by Peter Larsson. Scientific rept.
DO. 2 on Conir»ct AF 19(604)3073. May 60, 114p.
31 refa. Research paper no. 2; AFCRC-TN-60-419.
OnJer from LC mi|6. 00, ph$18. 30 FB 152 290
A preliminary Investigation of the meteorological con-
ditions on the Chamberlin Glacier in the summer of
195« waa carried out. with emphaais being placed on
the meaaurement of aome of the parameters needed to
aaaesa the energy balance of the glacier. The .Expedi-
tion waa not e<|uipped with the Instruments necessary
to carry out a detailed micro climacological study, thuE
DO quantitative measurements of heat balance were
obtained. Concluaions aa to the present regime of the
glacier can not be made from the meteorological re-
sults alone: odier phyaical aapects at the glacier there-
fore have been taken into consideration when any con-
cluaions have been formulated. The climatological re-
cords from the glacier and those taken at the expedi-
tloo'a baae caitip were the first ones to be obtained
from tfaia area at the Brooka Range, Alaska. (Author)
Army Signal Research and Development Lab. ,
Fort Monmoath, N. J.
•mEORETICAt EVALUATKW OF CYLINDRICAL
CHAFF AS A WIND SENSOR AT HIGH ALTITUDE.
by William C. Barr. 22 July 60, 35p. 5 refa. USASRDL
technical rept, 2138; AD- 241 876.
Order from LC mi$3. 00. ph|6. 30 PB 152 1%
The equations of motion for cylindrical chaff nrioving in
the freemolecale flow region d a rarefied gas (i. e. ,
the atmoaptaere between 60 and 90 kilometers) and in
the slip- flow region (L e. , the atmosphere between 30
and 60 kilometers) are formulated and solved. The fall
rate and the response of the chaff to a simple step-func
tion wind iii|>ut are calculated. The analysis indicatea
that cylindrical chaff ia a reasonably good wind senaoF
below about 65 kilometers, even if the winda obtained
are not correQted for dynamic reqxmse. (Author)
Free U. of Berlin (Germany).
EXAMINATION OF 24 HOURS PROGNOSTIC SUR-
FACE CHARTS AND PUNCHING OF GRID POINTS
OF UPPER AIR MEAN CONTOUR CHARTS, by
R. Scherhag. Final technical rept. for 15 June 59-
15 June 60 on Contract DA 91 -591 -EUC- 1159. [1960)
15p. 2 refs. AD-243 413.
Order from LC mi$2. 40, ph$3. 30 PB 152 563
Research is continuing with emphasis on the following
problems: (1) checking of prognostic charts; and (2)
punching erf grid -point dau from mean upper -air
Chans for a S-yr and a 40-yr period. Centers of cy-
clones and anticyclones were considered exclusively In
order to connect the pressure field with actual weather.
First an analogous comparison between prognosis and
reality was made by determining the difference be-
tween predicted and occurred central pressures; the
differences in position of the pressure centers were
also determined and sutistically elaborated. (Author)
Imperial Coll. of Science and Tech. , London
(Gt. Brit.)
MULTI- WAVE LENGTH RADAR REFLECTIVITY OF
HAILSTORMS, by David Atlas and Frank Ludlam.
Technical (Scientific) note no. 4 on Contract
AF 61(052)254. May 60. lOOp. 28 refs. AFCRC-TN-
60-425.
Order fromLCml$5.40. ph$15.30 PB 152 207
Radar reflectivity of exponential and narrow size
distributions of both wet and dry hail are computed
for several wavelengths from new data. Simultaneous
obaervatlons of storm reflectivity can be used to
distinguish hail from rain. Detailed observations d a
storm in England and Donaldson's New England obser-
vations are examined, and the essential features are
explained with a new storm model which implies con-
centrations of large dry hail in a narrow size range
near the maximum of a persistent updraught tilted by
strong wind shear. (Author)
I
Imperial Coll. at Science and Tech. . London
(Gt.Brit.)
THE ROLE OF RADAR IN RAINSTORM FORE-
CACTING, by F. H. Ludlam. Technical (Scientific)
note no. 3 on Contract AF 61(052)254. Apr 60, 35p.
6 refs. AFCRC-TN- [601-424.
Order from LC mi$3.00. ph$6.30 | PB 152 206
A brief review la made of the meteorological problenu
of rainstorm forecasting, and of the essential part
played by radar in providing baaic data. The necesait)
and ease of adapting all meteorological radars for
quantitative echo measurement are emphasised; the
relatione between intensity and maximum height of
echoes, precipitation -rate, hail size, and lightning
dlacharge frequency are estimated. Radar and sferlc
data requirements, reduction and presentation are
conaidered for the distina purposes of short-period
(1-3 hour) and long- period (6 - 24 hour) rainfall
forecasting. (Aiahor)
ISO
l^sachuaetts Inst, of Tech. , Cambridge.
•ECIFICATION OF CLOUDINESS AND PRECIPITA-
TION BY MULTI- LEVEL DYNAMICAL MODELS, by
prsderlck Sanders, A. James Wagner and Toby N.
(prison. Sciefltific rept. no. I on Contract AF
19(604)5491. Sep 60. 115p. 15 refs. AFCRL-TN-60-656.
OnJer from LC mi$6.00, ph$l8. 30 PB 152 448
The relationship of cloudiness and precipitation to the
vertical motion as computed by quasi- geostrophic multi-
level numerical nvodels was sftudied. In order to de-
termine the effects of high resolution in the vertical,
bodi a rwo-pwirameter and a ten- level model were used,
•pie models were applied to two storms of a contrast-
ii( nature. One was on intense northeastward- moving
baroclinic cyclone and the other was a weak lee- side
development under predominantly zonal conditions.
Cloudiness and precipitation were best related to the
»enlcal motion in the middle and upper troposphere.
Vertical cross sections through the frontal layers in-
dicated a good correlation be^een the cloudiness, ver-
tical motion, as computed from the ten- level nKidel,
and the orientation of the frontal zone, as shown by the
potential temperature fields. Quantiutive calculations
of precipitation were made for the Intense storm. The
computed amounts were In excess of the observed to-
tals to the northwest of the stf>rm center, but grossly
deficient in the warm sector.
^ 1
Meteorologic Lab. , U. of Illinois. Urbana.
MESOMETEOROLOGlCAL ANALYSIS OF ATMOS-
PHERIC PHENOMENA, by Roy H. Blackmer, Jr.
J. B. Holleyman. and H. M. Gibson. Final rept. for
1 May 55-31 May 58, on Contract DA 36 -039 -sc -64656.
(1958) ll2p. 144 refs. AD-206 745.
Order from LC mi$6. 00, ph$18. 30 PB 152 227
The purpose of this research is to study the behavior
of the atmosphere on a scale of less than 100 miles by
conducting detailed synoptic and upper air analyses.
Twenty-eight synoptic case studies were mesoanalyzed
usli« 1947 Thunderstorm Prdject data. The Fujita
method of surface analysis w*s used. Seven classifi-
cations of mesosystems were made: thunderstorm
high, mesolow, mesocyclone, pressure jump, pres-
wre surge, mesotroug^, and depression -type wave.
There were also disturbances in the wind, tempera-
ture, and moisture fields which did not affect the pres
•ure field. It was found that squall lines produce cell-
ular pressure rises and cold fronts produce lines of
pressure rises. A study of wind fluctuations revealed
the movement of small-scale circulations across the
network. A new network especially designed for the
Kudy of mesomeleorological phenomena is recom-
mended. This network should telemeter data to a cen-
tralized digital recording system. (Author)
Sunford Research Inst. , Mfenlo Park, Calif.
STUDY OF WEATHER STATIONS FOR ARMY USE.
PHASE II. ANALYSIS, by I. G. Poppoff, G. B. BeU and
others. Summary rept. on CJontraa DA 36-030- sc-
78154. 15 May 59, 173p. 91 refs. SRI Project no. SU-
2594; AD- 226 083.
Orderfrom LCml$8.10, ph^27.30 PB 149 711
An analysis is made of the problems involved in the de-
sign of automatic weather stations for Army use. The
characteristics of sensors, such as accuracy, range,
power consumption, and reliability, are presented. The
propagation problem is analyzed, with particular em-
phasis on arctic conditions. A discussion is presented
of a meteor reflection radio link that would be suitable
for the larger stations. General notes are included re-
garding the data collectioo system and the over -all
station configuration. The power problem is analyzed
and discussed for both the small, portable, short-term
station and the large, transportable, long-term
stations. (Author) (See also PB 143 774)
Tele- Dynamics. Inc.. Philadelphia. Pa.
TELEVELOFAX DESIGN STUDY. Design study rept.
on Contract AF 19 (604)4977. Aug 59. II6p. 15 refs.
TDI publication 900; AFCRC TR-59-269; AD-242 457.
Order from LC mi J6. 00. ph$18. 30 PB 150 388
Televelofax, the swift reproduction of an exact copy at
a distance, Is a system for the efficient transmission of
analyzed weather charts. The receiver accepts digital
data from a radio or land-line communication link and
causes this information to control the firing pins of an
electrographic matrix printer. An analysis is made d
the information content of weather charts based on a
statistical sampling of over 3, 000 charts. The analysis
permits a direct measure of the efficiency of any coding
scheme for weather chart transmission. Several sys-
tem designs are evaluated, and rejected on the basis of »
low efficiency or high complexity. The final design,
which permits the transmission of alpha-numeric and
symbolic data, provides reproduction of isoline dau in
dotted form. A description of the final Televelofax de-
sign is given and cost fijoires estimated. The efficiency
of the system for weather chart transmission is com-
puted. The system, operating over a 2000-bit-per sec
communication link, will print the average 12 x 18 in.
weather chart in 41 sec. (Author)
Texas A. and M. Coll. , Collie Station
MICROMETEOROLOGICAL DATA PROJECT GREEN
GLOW. VOLUME IL INSCX^TION, REFLECTED IN-
SOLATION, NET RACHATION, WIND VELOaiY,
SOIL TEMPERATURE, SOIL HEAT FLUX, SOIL
MOISTURE, SURFACE OBSERVATIONS - STATION 3.
WET AND DRY BULB TEMPERATURE, INSOLATION,
REFLECTED INS01.AT10N. NET RADIATION, WIND
VELOCITY, SOIL TEMPERATURE, SOIL HEAT
FLUX, SOIL MOISTURE, SURFACE OBSERVATIONS -
STATION 2, by William H. Qayton. Scientific rept.
no. 1 on Contract AF 19(604)5527. June 60. 663p.
Reference no. 60-8DIt GRE>-TN-60-489.
Order from LC mi$IK10. ph$101.40 PB 152 569
Frost Science
Army Signal Research and Development La^. . Fort
Monmouth, N. J.
ICE DEPTH SOUNDINGS WFTH ULTRA-HIGH FRE-
QUENCY RADIO WAVES IN THE ARCTIC AND
ANTARCTIC, AND SOME OBSERVED OVER-ICE
ALTIMETER ERRORS, by Amory H. Waite.
16 Dec 59, 128p. 4 refs. USASRDL technical
rept. 2092; AD- 236 201.
Order from LC mi*6.30, ph$l9.80 PB 152 568
151
Measurememt through Ice and snow of the Amaraic
continental ic«- shelf in 1955/56 and 1956/57 produced
dielectric con^ant and radio wave anenuation data for
high and uJtra»high frequencies to depths of 25 ft. Cal-
culations indicated the probability that devices such as
low-power 400- mc aircraft altimeters could send radio
signals vertically through two miles of ice. First at-
tem^xs at vertical sounding in the Antaraic in 1958,
uaing mcdlfie<^ aircraft altimeters on 4-ft high vehi-
cles, proved tjie theory as readings obtained by radio
found bottom ifxler 500 feet of ice and agreed within
40 feet of accqpted (gunpowder) seismic shots. These
findings were verified over a 3- mile course in Green -
Und Sep 1959. The 4-ft Mgh, 400-mc altimeters give
false readings up to 2400 ft when over ice ol 1200- ft
thickness. Excerpts from previously classified Signal
Corps radio/lqe studies, covering a 5-year period are
included.
Army Snow, ce, and Permafrost Research Estab
lishment, Wilmene, 111.
DEEP CORE DRILLING IN THE ROSS ICE SHELF.
LITTLE AMERICA V, ANTARCTICA, by R. H. Ragle.
B. L. Hansen and others. June 60, Up. Technical
rept. 7a J
Order from LCJ ml$2. 4a ph$3. 30 PB 152 388
This report relinsed for aile to the public 1 Dec 60.
Drilling operations and core and drill hole investiga-
tions at Little America V in Oct. -Dec. 1958 as well
•a measuremeiits at Byrd Station in Dec. 1958 are dis-
cuMed. The hale at Little America V reached 836 ft.
and core recovery was 98^ at the footage drilled. No
aaline ice was f^und in the bonom core, indicating
that the bottom |ce is melting. In detailed stratigraphic
studies to a depth at 53 m. sumnier snow deposits
were coarse-grained and often associated with icy
crusts, ice layers, and glands. Winter deposits were
finer -grained, niore homogeneous, and lacked the
aoaked appearance at summer snow. Periods al 2-3
consecutive yeat-s at more or less regular intervals of
10-20 yr shoiwed intense ice formation. Layers of
foreign material, tentatively identified as volcanic
ash, were observed at 172. 1 m, 219. 4 m, and
222. 8 m. The dtpth -density curve steepened between
20. 7 and 36. 5 nL If annual precipitation is estimated
as 21 cm erf wat^r. Little America V rests on about
1225 )rr o*accun»ulated snow. Data (some of a pr»-
liminary nature) are tabulated and graphed on the"^-
depth-density profile to a depth of 53 m, the nature oT
ice at various depths, spot densities below 53 m, and
the annual Increirients at depth and corresponding
water equivalent^ at Little America V, ice tempera-
ture at various depths at both stations, and depth -
iiKlination measurements as well as the diam-vs-
depth curve at Btrd Station. (Author)
Army Snow, Ic^ and Permafrost Research
Establishment, 'Wilmette, IIL
FORMATION. GHOWTH, AND DECAY OF SEA ICE
IN THE CANADIAN ARCTIC ARCHIPELAGO, by
Michael A. BlleUb. JUly 60, 40p. 16 refs. Research
rept. 65.
Order from LC i4l$3. 00, ph|6. 30 PB 152 456
Equations relating the accretion and decay of sea Ice
to sundard meteorological data are derived empiri-
cally from obaertations at 5 sutlons (Alert, Eureka,
Isachsen. Mou. d Bay, and Resolute) with varying
periods of record from 194701957. The equations dif-
fer from existing formulas in that they are differential
in nature, to permit calculation of ice growth by In-
crements, and contain a separate term allowing for
variations In snow-cover depths. The use of the for-
mulas requires only a knowledge of air temperatures
and snow depths. A good correlation is found between
the decrease in ice thickness and accumulated degree
days above -1. 8C. The location of each station, the
names of the surrounding water bodies, and theappra-
imate water depths where ice thickness measuremenu
were nutde are listed; the techniques used in the omm-
urements are described; data on observed ice thick-
ness, and accumulated degree days of frost and aver-
age snow depths for 20- cm increments of ice growth
are tabulated. (Author)
Army Snow, Ice and Permafrost Research Establish-
ment, Wilmette. 111.
GLACIOLOGICAL INVESTIGATIONS, NUNATARSSUAO
ICE RAMP, NORTHWESTERN GREENLAND, by
Laurence H. Nobles. Final rept. on Glaclological
Studies in Nunatarssuaq Area, Northwestern U. . Con-
tract DA ll-190-eng-12. May 60. 74p. 34 refs. Tech*
nical rept. 66.
Order from LC miK 50, ph$12. 30 PB 152 387
These investigations were conducted from 1953-55 on
a gently sloping ice mass of 8 square miles extent that
forms part of the margin of the Greenland Ice Cap. The
ice has a subpolar thermal regime with a constant tem-
perature of - 14C at 25 ft. All runoff is on the surface
forming slush avalanches, algal pits, and an integrated
drainage pattern. The firn limit is at 3000 ft elevation.
The ramp has a strongly negative budget balance, with
local ablation as high as 25 in. of water equivalent.
Velocities of ice movement range up to 2 in. per day
with the vertical angle of the movement vector never
deviating from the horizontal by nrjore than 5°. Budget
and movement studies suggest complete decay of the
ramp in 300 to 600 years under present climatic coa-
ditions. Metamorphic structures of both tensional and
shear origin are corrunor and include foliation, blue
bands, amber bands. Joints, small crevasses and ice
dikes. The military trafflcability of the ramp is dis-
cussed in the appendix.
Army Snow, Ice and Permafrost Research establish-
ment, Wilmette, Ol.
PLASTIC DEFORMATION OF THICK- WALLED
SNOW- ICE CYLINDERS UNDER HYDROSTATIC
PRESSURE, by H. a G. Jelllnek. July 60, Up. 7r«fi.
Research rept. 63.
Order from LC mi$2. 40, ph$3. 30 PB 152 457
The results of experiments on the plastic deformation
d hollow snow- ice cylinders, closed at one end. as a
function d circumferential stress and temperature are
discussed. Data are graphed on deformation as a
function d time for a snow- ice cylinder under-7. 03and
14. 06 kg/cm2 hydrostatic pressure at -4. 5C, defor-
mation as a function of hydrostatic pressure from
2. 11-7 03 kg/cm2, and deformation as a function at
temperature at a constant pressure at 10. 55kg/cm2.
The natural strain rate of closure at constant circum-
ferential stress and temperature was a constant, whic*-
152
igrlcd with circumferential stress as a sinefunction
jad was exponentially dependent on temperature, with
qi activation energy o< 14. 1 kcal/mole at an average
clrcumierentiai stress at 3. I kg/cm^. The experi-
ments agree well with an eatlier interpretation of the
plastic flow process representing flow between grain
boundaries. (Author)
Washii^on U. , Seattle.
CRYSTAL FABRIC STUDIES, by Edward R. LaChapelle.
Semi-annual progress rept. for 1 Sep- 15 Nov 59 on
Contract Nonr -477(1 8). 1 Dec 59. 31p. AD -230 170.
Older from LC mi$3. 00. phJ6. 30 PB 152 148
The report summarizes briefly the course at the sum-
mer work and the results, though the analysis of the
micrometeorological data is as yet incomplete.
WAshington U. , Seattle.
DRIFTING STATION CHARLEY. Semi-annual rept.
for I June -30 Oa 59 on Projiect Husky, Contract Nonr-
477(24). I Dec 59. 44p. 6 refs. AD-229 735.
Order from LC mi$3. 30, p»f$7. 80 PB 152 149
The report includes brief summaries on principal
equipment; radio-sextant A|tN/25; celestial navigation;
oceartography; oceanographic stations and sampling;
chemical analyses; micrometeorology; ablation; pro-
gram for study of low amplitude, long period flexural
waves in Icefloe C; and transfer of solar radiation
through sea ice. Also included are: Arctic Research
Laboratory Semi-annual Report on Project Husky; Pre-
liminary Report on Sea Ice Crystal Fabrics Studies on
Sution Charlie; Project Husky. Station Charlie, Report
of the Marine Geologist; and Reflectivity-Conductivity
of Materials Having Variouf Physical Properties on Sea
Ice in Late Spring.
»eod
esy
Battelke Memorial Inst. [Columbus, Oftto).
DESIGN STUDIES FOR GLOBULAR DISPLAYS, by
J. M. Dvgan, S. A. Hawk and others. Rept. tor 22 July-
26 Sep 57 and 8 Apr 58-12 May 59 on [Contract
AF 30(602)17661 [1959] I9lp. 38 refs. RADC TR-
59-65; AD-214 597.
Order from LC mi$8. 70. ph$30. 30 PB 152 015
Design studies were conducted to deternune the feasi -
blUty of using globe-type maps for the pn-esentation of
ittelligence to Air Force commanders. Results indi-
cated that concave global maps have the best combina-
don of map characteristics to satisfy the requirements
for global planning by AF commanders. The northern
hemisphere from 20(> north latitude comprises those
geographical and political subdivisions that are most
Important for AF planning (US, USSR, China, and
Europe). The needs of AF planners for a map can be
satisfied by a map on % scale of 1 : 2, 000. 000. The
map should have considerable cartography with pleas -
lag color rendition. The map seaion should be placed
In front of and below the line of sight of the AF com-
manders. Auxiliary intelligence data such as the
order of battle or indications should be presented on
display boards located on each side of the global map.
Additional intelligence to be presented in geographical
context on the global map should be prepared on a
hemispherical planning board and projeaed onto the
large global map. This arrangement eliminates the
distractivo arising from manual platting or the use of
an X-Y coordinate plotter on the display.
Photointerpretation, Inc. , Annapolis, Md.
DETECTI(»1 OF MINUTE IMAGES ON COLOR FILM.
Final engineering rept. on Contract AF 30(602)1631.
Aug 57, 59p. RADC TR-57-153; AD-131 259.
Order from LC ml$3. 60, ph$9. 30 PB 152 303
Methods and recommendations are made by the author.
Previous literature is surveyed.
This report includes: The diachromoscope, by Hugh T.
O'Neill and WiUiam J. Nagel, (Ansco Div. , General
Aniline and Film Corp. ) puh in Fhotogranunetric En-
gineering, p. 180-185, Mar 57.
Rome Air Development Center, Griffiss AFB, N. Y.
PLANE GEOMETRICAL CONSIDERATIONS OF A
NAROL SIGNAL LOCATION SYSTEM, by Raymond L.
Allen. Sep 60, 28p. RADC-TN-60-150.
Order from LC mi$2.70, ph$4.80 PB 152 548
Investigation is made into the geometrical considera-
tions of an inverse LORAN (NAROL) Signal Location
System. General equations are derived for the maxi-
mum error of fix in terms of the electronic error of
the system. Plots are included of the various parame-
ters of the general equation to show the variations of
each. Formulas included are derive for a plane
earth. (Author)
Geography
MaryUnd U. , College Park.
PORT HINTERLANDS: THE CASE OF NEW ORLE-
ANS, by Donald J. Patton. Rept. on Cootraa Nonr-
595<05). Feb 60, 94p. 6 refs.
Order from LC mi$5.40, phJ15.30 PB 147 646
The dominant function at a port area as a nexus be-
tween continental and maritime traffic flows imparts
to such an area a nodality distinct from that of a city.
Interchange between continental and maritime trans-
port is the predominant break-in-transport service
function of most ports, although an entrepot function
assumes a major role in a minority of cases. Exclu-
sively land-based traffic flows in and out of port areas
also occur occasionally to take advantage of a harbor -
side service, more commonly to undergo processing
In tbe port area in conjunction with Incoming seaborne
goods and for other reasons. Aggregatively, consid-
erably less atteicion has been given in the literature to
traffic flows tributary to port areas as such compared
to studies of the tributary areas of urban centers. For
progress to be nude in the examination of intercon-
nections and comparisons between these two forms at
nodality. further substantive work on flows tributary
153
to peart districts is needed. Accordingly, it is pro-
posed here to Concentrate on the continental segment
of the port of New Orleans as a contribution toward
this objective.
Minnesota U. , Minneapolis.
PLACE NAMES IN I6TH AND ITTH CENTURY
BORNEO, by jin O. M. Broek. Technical repi. no. 2
on Contraa Niiu-710(09). Mar 59. 45p. 31 refs.
Order from Ld nU$3. 30, ph$7. 80 PB 148 291
For this study khe basic research tools are the maps
showing Barney from the early I6th Century onward.
This paper concentrates on the cartographic presenta-
tion of the islafid, more especially of its place names.
Physics of the Atmosphere
1
Air Force Cambridge Research (Labs. ] Bedford.
Mass. I
AN EfflTMATi OF PREaPTTABLE WATER ALONG
HIGH-ALTTTUbE RAY PATHS, by Murray Gutnick.
Mar 60, 35p. t2 refs. Air Force Surveys in Geo-
physics no. IM; AFCRC-TN-60-251; AD- 235 832.
Order from ui mi$3.00, ph$6.30 PB 149 061
Tables of the estimated water -vapor content of the
atmosphere abpve 25, 000 ft are presented for use in
evaluating, for design purposes, the amount of anenua-
tion which will be experienced during the travel of IR
signals over vdrious high altitude ray paths. Results
are given in te rms of precipitable water integrated
over the maxirium line of sight between an aircraft at
altitudes of 25j000 to 100,000 ft and a ray path skim-
ming a cloud hyer at 25.000 ft. Latitudes of 40^ and
60^ are considered. (Author) '
Blue Hill Met4 orological Observatory
[Milton, Mas • . ]
TWILIGHT INTENSITY AT 20° ELEVATION, by
F. Volz and R. i M. Goody. Scientific rept. no. 1 on
Contract AF 191(604)4546. Jan 60, 58p. 33 refs.
AFCRC TN-604284; AD- 235 385.
Order from LQ mi$3. 60, ph$9. 30 PB 148 718
A photometer 4as designed which can measure the
absolute intenstty at the twilight in 5 narrow bands of
wavelengths fr<|m the red to the ultra-violet region of
the spectrum, lor sun depressions up to 18^. A theo-
retical analysis at the twilight intensity for a pure
molecular atmosphere and some plausible dust
nxxiels indicates that the influence at dust on the late
twilight scattering is small. Two observations at the
twilight are distussed briefly in terms at the theo-
retical models.! Measurements of the night sky in-
tensity caused ^y starlight, airglow and city lights in-
dicate that usefUl information can be obtained up to
120 km for observations in blue light and up to 75 km
for observation^ in red light. (Author)
California U. . Los Angeles.
APPROXIMATION OF LIGHT SCATTERING BY
LARGE DIELECTRIC SPHERES, by D. S. Saxon,
Z. Sekera. and D. Deirmendjian. Scientific rept.
no. 3 on Light in the Atmosphere, Contract
AP 19(604)2429. June 60, 22p. 4 refs. APCRC-TN-
60-486.
Order from LC mi$2. 70, ph$4. 80 PB 152 SS2
The approximate expression for the amplitude of the
electric vector of the scattered radiation by a large
dielectric sphere is derived from an exact integral
equation solution of Maxwell equations. The unluKTWn
electric and magnetic field vectors in the interior of
the dielectric sphere are approximated by the assump-
tion of rectilinear propagation of the incident wave
through the sphere. The change in polarization is neg-
lected; however, the phase along the ray is correctly
evaluated. The final expressions for the amplitude of
the electric vector of the scattered radiation contain
four integrals, which can be reduced to the evaluation
of only one of them, I3. This integral is evaluated
approximately for different domains of its variables,
with the proper consideration of the errors of such
approximations. The resulting expressions are then
compared numerically with the exact Mie- solution of
the problems. As can be expected, the approximation
is quite satisfactory in forward directions, andrather
poor in wide angle and backward scattering. (Author)
California U. , Los Angeles.
DIFFUSE REFLECTION OF SOLAR ULTRA-VIOLET
RADIATION IN THE PRESENCE OF OZONE, by
Zdenek Sekera and J. V. Dave. Scientific rept. no. 4
on Light in the Atmosphere, Contraa AF 19(604)2429.
June 60, 53p. 8 refs. GRD-TN-60-634.
Order from LCml$3. 60, ph$9. 30 PB 152 553
The problem of diffuse reflection of solar ultra-violet
' radiation in the presence of ozone has been solved for
a plane-parallel atmosphere of finite optical thickness.
The atmosphere is divided into two layers. The scat-
tering optical thickness of the upper layer is small
enough to permit one to consider only primary scaner-
ing. Ozone is distributed in this layer according to a
definite analytical function. The scattering optical
thickness of the lower layer is large and all the order*
of scattering have been taken into consideration for it.
It is assumed that the lower layer does not contain anjr
ozone. The radiation received by an observer on the
top of the atmosphere would consist of two parts. The
first part originates from the upper layer as a conse-
quence ot scattering of direct solar radiation falling
on it. The other part originating from the lower layer
consists of four different components. TTie results of
computations presented in this report contain intensi-
ties of each of tliese five components for several
values of ozone absorption and for several directions
of incident and scanered radiations. It is expected
that the results presented in this report will be helpful
in obtaining a broad, semi-quantiutive picture of the
amount of radiation emerging from each of the layers
under different conditions which one is likely to
encounter. (Author)
154
Electrical Engineering Research Lab. . U. of Texas,
Austin. I
FREQUENCY SPECTRA ANALYSES OF ONE MILU-
aOOND TIME RESPOISE TEMPERATURE SENSORS
AT VARIOUS LEVELS NEAR THE GROUND, by
E. C Lowenberg. F. X. Bo$tick, Jr. and C. E.
McCullough. Rept. on Cont^ract AF 19(604)2249.
15 Mar 60, 59p. 2 refs. Rept. no. 6-32; AFCRC TN-
60-166; AD- 234 479.
Order from LC mi$3. 60. ph$9. 30 PB 148 710
A series of magnetic tape recorded temperature
fluctuation observations are analyzed to obtain power
cpectra covering a frequency range exceeding 100cf>8.
A 2.5 micron platinum wire sensor having a response
of the order of 1 miUi9econd was located at vari-
levels above the ground and representative 30
Moond recordings were selected for analogue com-
puter processing of the power spectra evaluations.
(Author)
■ I
Geophysical Inst., U. of Alaska, College.
EXPERIMENT LUXEMBOLIRG, by G. C. Rumi. Scien-
dficrept. no. 3 on Contraqt AF 19(604)3880. Feb 60,
27p. 23 refs. AFCRC-TN-60-275; AD-235 213.
Order from LC mi$2. 70, pti$4. 80 PB 149 062
This study is concerned with the contribution of mete-
oric ionization to the formation of the upper layer in
the D region, and to the absorption of radio waves. The
absorption of meteoric origin is detectable when the
kxrer layer in the D region is relatively weak. Evi-
dence of absorption due to sporadic meteors is deduced
from experimental data. Evidence of absorption due to
meteoric showers is found by analyzing f^in pl<^ data.
Particular attention was detoted to the Perseid meteor
Aower of 1958. During this shower, meteor rates
««re observed by mean^ of a 100 mc radar. The fmin
'iKreaaed and decreased according to the fluctuations
of the meteor rates. It is itiferred that meteors con-
tribute efficiently to the fanmation of the upper layer
In the D region. (Author) •
Geophysical Inst., U. of Alaska, College.
THE HEIGHT OF F-LAYE.R IRREGULARITIES IN
THE ARCTIC IONOSPHERE, by Howard F. Bates. Sci-
•dflcrept. no. 3 on Contract A F 19(604)1859. Mar59,
27p. 12 refs. AFCRC-TN*59-180; AD- 214 843.
Order from LCmi$2. 70, ph$4. 80 PB 148 668
Results and interpretations* of oblique incidence sound-
ings of the arctic ionosphere are presented. Anomalous
echoes are found to be prevalent in high latitudes in
oostrast to lower latitudes Where 2F groundscatter pre-
dominates. One of the echoes seen regularly at College;
Alaska was identified as direct F- layer (IF) backseat -
ter. The observations of thie IF echo provide direct
evidence of the preseiKe of irregularities in the
F-layer between heights of ^350 and 600 km . The IF
echoes are recorded regularly at night and occasionally
during the day in disturbed periods. They appear to be
uaociated with aurora] ionization. The analysis of
froundscattered (2F) echoes is extended from a plane tc
• spherical geometry, and It is shown that a geometri-
cal extension of the plane earth theory is adequate.
(Audior) ^
Geophysical Inst. , U. of Alaska, College.
RADIO PROPERTIES OF THE AURORAL IONO-
SPHERE, by G. C Reld, E. Stiltner and R. Cognard.
Final repL (Phase 1) on Contract AF 30(635)2887.
Feb 59, 89p. 19 refs. RAIX:-TR-59-39; AD-148 987.
Order from LC miH 80, ph$13. 80 PB 148 983
Ionosphere Research Lab. , Pennsylvania State U. ,
University Park.
THE STEADY CTATE OF THE CHAPMAN-FERRARO
PROBLEM IN TWO- DIMENSIONS, by J. W. Dungey.
Scientific rept. no. 135 on Ionospheric Research,
Contraa AF 19(604)3875 and National Science Founda-
tion Grant G-5939. 15 July 60, 17p. 2 refs. GRD
TN-60-60I; AD-242 573.
Order from LC ml$2. 40. ph$3. 30 PB 150 668
The steady state of the Chapman-Ferraro problem is
formulated in mathematical terms, but the three-
dimensional problem presents little hope of an ana-
lytical solution and It is not even obvious how to com-
pute the solution. The two-dimensional problem is
reduced to a standard potential problem and solved
exaaly. The solution is used to obtain an indication
of the error in the flat-faced approximate model
which has previously been used in three dimensions.
(Author)
National Bureau of Standards, Boulder, Colo.
WORLD MAPS OF F2 CRITICAL FREQUENCIES AND
MAXIMUM USABLE FREQUENCY FACTORS, by
Donald H. Zacharisen. Supplemenury repL Oct 60,
247p. 6 refs. Technical note no. 2-2.
Order from OTS $3. 50 PB 151 361-2
This report siqjplements National Bureau of Standards
Technical Note Number 2, AprU 1959 (PB 151 361),
and completes the basic data required for F2- layer
maximum usable frequency predictions. Prediction
Chans are given for the months of F^ruary, April,
May, August, October and November. Auxiliary charte
are included to aid in predicting F2- layer MUFs.
(Author) (See also FB 151 361).
New York U. ColL of Engineering, N. Y. ^ — — ^ - '
HIGH LEVEL TURBULENCE, by joaepti Clodraan,- ^-T"
Griffith M. Morgan, Jr. and John T. BalL Final rept. " "^
00 Contract AF 19(604)5208. Sq> 60. 90p. 66 refs.
AFCRL-TR-60-408.
Order from LC mlH 80, ph$13. 80 PB 152 521
A comprehensive review of the literature of high level
turbulence is carried out and conclusions are drawn as
to many of the properties of this phenomenon. The
effect of moderate topography is examined by consider-
ing two bodies of aircraft rqwrts. It is reasonably
well established that even modest obstacles of less
than l(X)0-2000 ft in height play an important role in
high level turbulence over land and that some of the
parameters involved suggest a relationship to gravity
waves although this is only pan of the mechanism.
High level turbulence reports over the North Atlantic
are examined and it is found that such turbulence is
much less common and occurs under different condi-
- i
155
tiOQS than over kuid. The basic equadons governing
the energetics of the motion are examined and conclu-
sions drawn as tD the in^x>rtant energy sources and
■Inks. A model! is used to estimate the rate of growth
due to various energy sources to detemilne plausible
mechanisms. TVo mechanisms are evolved which ap-
pear to be of pradominant inportance in the develop-
ment of high level turbulence. One of these is signifi-
cant over land a|d Involves primarily gravity waves
and strong vertical wind shear. The other is impor-
tant over water ^nd results from hydrodynamic In-
stability and reUtively low Richardson numbers. The
observational data on the turbulence is considered in
the light of thesq mechanisms and found to fit very
welL A forecast scheme for high level turbulence is
suggested on the basis of the above results. (Author)
Pennsylvania SlUte U. Mineral Industries Experiment
Station. UniverBity Park.
LARGE SCALE VERTICAL MOnON IN THE
STRATOSPHERE, by Edward S. Epstein. Final rept.
pt. 2 on Contract AP 19(604)2190. Dec 59, 133p.
45 refs. AFCRCTR -60-240(11).
Order from LC mi$6. 90, phJ21. 30 PB 152 249
An empirical study is made of the interrelations be-
tween the horlzoetal flow panem in the lower strato-
sphere and the effect of vertical motion on the budgets
d vorticity and ozone. Two periods in the winter of
1956 are stixlied. On the basis of the contours of the
200-, 150-. 100-', and 50-mb surfaces, the terms of
the vorticity equation are evaluated, and vertical ve-
locities are computed from the adiabaric equation.
Changes in total ozone amounts are compared on a
synoptic basis w|th the horizonul and vertical fields
of motion. The ltx:al change dt vorticity. vorticity
advection, and the divergence term (neglecting the
relative vorticity in comparison with the Coriolis
parameter) appear to be the only terms at importance
in the vorticity ei}uation. There is broad agreement
between the fields c* horizontal and vertical motion,
subsidence occurring in flow from ri<%e to trough and
ascending motloil in flow from trough to ridge. This
pattern, however, is not invariant, and is particularly
disturbed in the presence of short wave disturbances.
A model is presented to describe the effects of short
and long waves od the patterns of vertical motioa and
divergence. A aitiiation in which the changes in total
ozone amount were large is selected and studied in
terms of the observed and computed fields at motion.
Pennsylvania U. School of Medicine, Philadelphia.
THE RADIANT TEMPERATURE CW THE ZENITH
AT HICjH ALTITUDE IN THE SUBARCnC, by
H. T. Hanunel. May 60. Up. 6 refs. AAL Technical
rept. 57-49.
Order from LC 4i$2. 40, pfa$3. 30 FB 150 217
Three flights were made up to 40, 000 feet on 3 sepa-
rate days. The radiant temperatures obtained on the
3 days are abown. The air temperatures shown are
from radioaoode reports obtained at 1700 A. S.T. by
the U. S. Weather Bureau at Fairbanks, Alaska. The
air temperature from 30, 000 to 75, 000 feet was
fatrly constant and between -b(P C. and -bffiC. On
the other hand, tl^ radiais temperature of the zenith
was found to be highly variable above 30, 000 feet. The
temperature ranged from about -60° C. to -125° C.
for the three flights, and on a single flight the tem-
perature ranged from -60° C. to -95° C. above
30, 000 feet.
"Hierto Rico U. C^ll. of Agriculture and Mechanic
Arts, Mayaguez.
MEASUREMENT OF IONOSPHERIC DRIFT/AND
STRUCTURE BY RADIO ^AR OBSERVATIONS, by
Braulio Dueflo. Final rept. on Contraa AF^ 9(604)1918.
Aug 60. 65p. 16 refs. AFCRL-TR-60-402.
Order from LC-mi$3.90, ph$10.80 PB, 152 471
This report is divided into three parts. TTie first part
deals with fluctuation phenomena in relation to obeierva-
tions made during a period of two years. It is shown
that there exists at this location a great increase in
fluctuation activity during June and July which appears
to be associated with the large scale changes taking
place in the F-2 layer during the pre- sunrise period.
Measurements of Drift Velocities cf irregularities by
the radio star method is discussed in the second part.
It is found that for measurements made during the pre-
midnight hours the drift is predominantly towards the
sourth-east and the opposite direction for measure-
ments taken after midnight. A physical Interpretation
of this behavior is given. The third part gives informa-
tion, from a practical point cf view, on the construc-
tional details and operation of the phase switching
interferometers used In this experiment. (Author)
Stanford Electronics Labs. , Stanford U. . Calif.
IDBNTIFICATICW OF WHISTLER SOURCES ON
VISUAL RECORDS AND A METHOD OF ROUTINfi
WHISTLER ANALYSIS, by D. L. Carpenter. Tech-
nical rept. no. 5 on Contract AF 18(603)126.
15 Mar 59. 51p. 3 refs. AFOSR-TN-60-315;
AD- 235 426.
Order from LC ml$3. 60, ph$9. 30 PB 149 069
Two of the problems that arise in whistler analysis
are discussed. These are the identlficatiOD of the
causative sferic associated with a whistler, and rou-
tine analysis of whistlers based on visual frequency-
versus-time records (Sonagrams). A brief descriptioa
is given of the nature of whistlers and the type of
record used In their analysis. The principal methods
of identifying causative sferics on whistler records
are reported. A technique is presented which involves
the measurement of the delay between successive
echoes of an echo train and using this delay to predia
the. time of the causative sferic. An abbreviated form
cf routine analysis is presented for application to
whistlers for which the causative sferics cannot be
identified.
Sunford Research Inst. , Menlo Park, Calif.
UPPER ATMOSPHERE CLUTTER RESEARCH. PART
II. WGH-ALTITUDE 106. 1-MC RADAR ECHCKS
FRC*< AURORAL IONIZATION DETECTED AT A
CXOMAGNETIC LATITUE« OF 43 DEGREES, by
J. C. Schlobohm, R. L. Leadabrand and others. Final
rept. pt. 2 on Contraa AF 30(602)1762. Apr 59, 33p.
11 refs. SRI Project 2225; RADC TR-59-44;
AD- 212 617.
Order from LC ml$3.00, ph$6. 30 PB 148 286
156
Auroral echoes have been detected using a radar at
106. 1 Mc located at 43 degrees geomagnetic latitude.
The geometry of reflection for ionization aligned with
the earth's magnetic field Jines is such that, for a
geomagnetic latitude of 43 degrees, reflection can
occur as high as 300 km. The results of these ob-
servations are presented with interpretation of the
height of reflections.
I I
ENGINEERING
Army Research Office, Washington, D. C.
ARMY RESEARCH TASK SUMMARY, FISCAL YEAR
I960. VOLUME 5. ENGINEERING. 440p.
Order from GTS $4. 25 PB 171 004
Contents: I
Qvll engineering
Elearical engineering
Mechanical engineering (aeronautical and automotive
included)
Ordnance engineering
(See also PB 161 137)
Crysler Corp. , Detroit, Mich.
CHRYSLER -TYPE OXYGEN PRESSURE VESSEL:
CALCULATION, DESIQfJ, /^ND TESTING, by
H. R. Greenlee. Rept. *or 15 Mar 57-15 June 59 on
Oxygen Dispensing Assemblies, Contract AF 33(616)
AF 33(616)5188. May 60, 55p. WADD Technical rept.
fO-365. 1
Order from LC ml$3. 60. ph$9. 30 PB 153 060
The development of a lightelr, stronger, more durable
dual-pressure cylinder for two gases or a liquid and
gas was accomplished through a new concept compris-
ing a continuously wound high -pressure tube fitted and
brazed to the inskle of a cylindrical shell. A compos-
ite structure of ais type is expected to provide more
resisunce to sholtering than the sundard bottle and
make a lighter design through the successful applica-
tioft of higher strength materials. The Chrysler-type
pressure vessel termed "Balcon" makes use of a com-
plementary stress pattern qreated from the composite
design of the structure. Two pressures are contained
in this type construction: 2100 psi in the cylinder and
4000 psi in the tube. Two Jumbo-type tire valve cores,
one conventional and one reversible, are incorporated
to reduce the high pressure of the coiled tube to equal
the low pressure of the cyli(ider as the latter is used.
Whsn the two chambers have reached an equal pres-
Mue, both decay uniformly as the gas is exhausted.
Limited tests show an Increase of 22 to 49% in free
■ttrogen gas per pound of conuiner wei^ over the
•ttndard bottle. (Author)
Aeronautical Engineering
Arnold Engineering Development Center [Tullahoma.
Tenn. ]
iOCKET TESTING IN THE* AEDC PROPULSION
WD© TUNNEL, by R. W. Hensel. Rept. on ARO.
he. Contract A P 40(600)800 S/A 11(60-110). July 60.
<lp 7 refs. AEDC TN-60-136; AD- 239 925.
(Wer from LC mi$3. 30, ph$7. 80 PB 153 280
I
This report released for sale to the public 19 Dec 60.
A number of test programs involving the use of both
liquid and solid propellant multi- rocket systems were
performed in the Transonic Circuit of the AEDC Pro-
pulsion Wind Tunnel. The equipment and techniques
are summarized, atxl representative test results are
presented with particular emphasis on the liquid pro-
pellant work. The difficulties and failures with both
the equipment and techniques and their remedies are
discussed. Results show that the tunnel scavenging
s]rstem, which was designed for airbreathing engine
exhausts, also performs well during rocket tests both
aerodynamically and mechanically with the propellants
used thus far. (Author)
Avco Corp. , Nashville, Tenn.
DESIGN, DEVELOPMENT AND FABRICATION OF A
LIGHT WEiaiT AIRFRAME. Monthly progress rept.
no. 4 for Aug 60 on Contract DA 33-008- ORD- 1%8.
15 Sep 60, 29p.
Order from LC mi$2. 70, phH 80 PB 152 343
Engineering drawings of the proposed design of Light
Weight Airframe were reviewed. General approval of
the design was indicated with major comments as fol-
lows: a method should be incorporated for making the
lock ring a captive part; the lock ring safety feature
should be dvq>licated at a second position 180°^ from the
first to increase the reliability of this function; the con
tractor was requested to investigate the feasibility of
using a serrated steel insert in place of the serrations
in the aluminum alloy lock ring; the alignment pins at
the Sta. 48. 00 Joint should be made longer to permit
visual mating of parts. All tool design and tool manu-
facture have been completed. (See also PB 150 279)
Bendix Radio Div. . Bendlx Aviation Corp. ,
Baltimore. Md.
ACCEPTANCE TESTS OF AIR TRAFFIC CONTROL
CENTRAL AN/GSN-7. by Robert C. Perle. Rept. on
Contraa AF 19(604)1881. Dec 59, 30p. 1 ref. AFCRC-
TR-59-372; AD-235 256.
Order from LC mi$2. 70, ph$4. 80 PB 148 708
Air Traffic Control Central AN/GSN-7 was found in
acceptance tests to meet the engineering requirement
in all respects except that the tracker azimuth dead
zone is excessive. Time-to-go mean errors observed
ranged from 1 percent to 0. 1 percent of full scale.
TTie range-mark generator leaves much to be desired.
C^iality of tracking is comparable to that of the
AN/GSN-3. Other features are discussed. Represent-
ative dau are tabulated. (Author)
Chicago Midway Labs. , U. of Chicago, ILL.
THERMAL ?KOTECTVm OF STRUCTURAL, PRO-
PULSION, AND TEMPERATURE- SENSITIVE MATE-
RIALS FOR HYPERSONIC AND SPACE FLIGHT, by
William P. Manos, Donald E. Taylor and Anthony J.
IVizzolino. Rept. for July 58- Sep 59 on Materials
Analysis and Evaluation Techniques, Contraa
AF 33(616)6006. July 60. 228p. 30 refs. WADC
Technical rept. 59-366, Pt. IL
Order from OTS $3. 50 PB 171 147
This report presents the results of an investigation In-
tended to examine various phenomena applicable to the
157
protection erf niatcrlals subjected to severe thennal en-
vironments and evaluate their effectiveness on the sur-
vival at materiBls now available. The heating experi-
enced by matetlals in selected severe thermal environ-
ments Is reviewed. The various phenomena that might
be employed for protection are studied and evaluated
analytically. Experimental tests were performed to
aid in evaluati<)n of certain phenomepa, using the
discharge of a 1000-KW air- stabilized arc to provide
a severe theritial environment. These results are re-
ported, along With a correlation al the observed be-
havior with theory and previous tests. (Autlwr) (See
also PB 161 956)
Engineering biv. , Air Materiel Command, Wright -
Panerson AFp, Ohio.
WIND TUNNEt TESTS OF THE COANDA WING
by D. W. Young and D. Zonars. Sep 5Q
^F Technical rept. no. 6199;
AND NOZZLE
78p. 12 refs
ATl-90 054.
Order from bd miJ4.50, ph$l2.30
PB 147 374
This report re leased for sale to the public 30 Nov 60.
I
Wind tunnel telts to determine the aerodynamic char-
acteristics of I wing and nozzle, invented byM. Henri
Coanda of PariJB, France, are described. The effeas
on lift, drag. $nd pitching moment d the wing are
given for rangt of test air speed, angle of attack, slot
width, and qua^itity of air ejected. The thrust(of the
nozzle and ambunt of air entrained are given' for
ranges of test Uir speed, slot width, and quantity of
air ejected, ms concluded that boundary layer con-
trol, by use oi the Coanda method when used on wings,
causes appreciable increase in the maximum Uft and a
reduction m the drag coefficient for all angles of
attack. The a<}companying change in moment coeffi-
cient is small J Comparison of the data obtained in
these tests wiifi other referenced data on boundary
layer control indicates that- the Coanda method, as
tested, is not as good as orher means for increasing
the maximum lift coefficient and reducing the drag
coefficient. Itiis concluded that a nozzle with an
annular type slot ejecting pressurized air can be
employed as ah air pump or as a thrust augmentor.
Enirainment ratios were between six (6) and eight (8)
for the static Conditions. These values compare
favorably with those predicted by the inventor before
the tests were conducted. (Author)
Pairchild Aircraft and Missile Dlv. , Hagerstown,
Md.
DESIGN. FABHICATION, AND TEST OF HIGH-
FLOTATION tiRES AND RELATED VALVING
MECHANISM FOR ROUGH TERRAIN LANDING
GEAR. MODEL M-245, by V. Frlsby. Rept. on Con-
tract DA 44- i;7-tc-446. 27 May 60, 494p. Rept.
no. R245 -025 ;:TREC 60-39.
Order from LC mi$ll . 10, ph$75. 60 PB 152 494
This report covers the results of experiments di-
rected toward the design, developmem, and testing of
a laboratory-i^odel, rough-terrain landing gear sys-
tem using folc^ble high- flotation tires built by a novel
continuously\^ourid-Qi?rd method and using ventlng-
hub shock abs4)rption. The contemplated end use o€
such a system
rough, unprepared fields. The tires, due to their
IS for STOL aircraft operated from
relatively light weight, low Inflation pressures, and
economical methods of production, can also be ideally
adapted to land vehicles for off-road use, offering
improved croes-country trafficability with lessoned
tare weight.
The following appendices are included:
Appendix I. Development of continuously-wound-cord
tire-building techniques, by V. Frlsby. Rept.
no. R24S.015
Appendix 2. Static test high -flotation tire, by W. J.
Sawyer. Engineering rept. no. R245-010
Appendix 3. RolUng tests high-flotation lire, by B. R.
Klein. Engineering rept. no. R245-011
Appendix 4. The design and development of laboratory
models to study the feasibiUty of high -flotation tires
for aircraft, by J. A.Hoess, W. F. Prien and others
(Banelle Memorial Inst). Rept. no. R245.012
Appendix 5. Design and development of laboratory and
flight-test models of landing gear for aircraft to be
operated from rough unprepared fields, by W. F.
Prien, R. D. Fannon and others (Battelle Memorial
Inst.). Rept. no. R245-014
Appendix 6. Initial flight tests high- flotation landing
gear, by A. J. Atkinson. Rept. no. FT245-1
1 1
HiUer Aircraft Corp. , Palo Alto, Calif.
AIRBORNE PERSCWNEL PLATFORM, by Wilbur J.
Gill. Summary rept. on Contract Nonr- 1357(00),
Phase IV. 9 June 59, 65p. 13 refs. Rept. no.
ARD-236; AD-225 794.
Order from LC ml$3. 90, phSlO. 80 PB 149 075
A wind tunnel and static test program was conducted In
which 4 duct shapes and 3 propeller configurations
were tested in various combinations and an enlarged
full scale flying platform was designed and tested. The
maximum figure of merit of all the ducted propeller
models tested was 1.07 (based upon an ideal values of
^for a non-diffusing duct). This value was obtained
with a bell -mouth duct in combination with a set of
twisted, 3-bladed, contra- rotating propellers. This
same configuration showed the highest values of for-
ward flight efficiency, lift coefficient and pitching
moment coefficient for the range of speeds and pro-
peller blade settings tested. The airfoil -profile ducts
produced considerably lower figures of merit due toaa
indicated flow separation at the duct inlet. The origi-
nal 5-ft-diam platform which was under-powered was
modified to a 7-ft-diam platform. This platform, des-
ignated 1031 -A- 1, developed enough thrust to hover
out of ground effect. Theoretical studies conducted in
platform stability and control Indicated that the plat-
form was unstable In hovering and forward flight with-
out the automatic mechanical gyrostablllzer. A theory
was developed for predicting the pitching moment
characteristics of a ducted propeller in equilibrium
forward flight.
MotoroU, Inc.. Riverside, Calif.
THE DETERMINATION OF ATMOSPHERIC TRANS-
MISSIVFTY BY BACKSCATTER FROM A PULSED
UGHT SEPARATED SYSTEM, by Melvin H. Herman.
Rept. on Contraa [AF] 19(604)2213. Oa 58, 83p.
1 ref. Rept. no. RL- 3828-2; AFCRC TR-58-277.
Order from LC mi$4. 80, ph$l3. 80 PB 152 384
This report released for sale to the public 25 Nov 60.
iSS
r
As an aircraft approaches a runway, the pilot must
recognize the runway lights while sufficient altitude
remains to permit course correction. The prediction
18 to when the lights will be seen must be made from
the ground, preferably by measuring the transmission
kMS along the actual approach path. The feasibility of
determining visual range along the slant path by ob-
serving the light scattered by the atmosphere from a
pMlayl beam of Ught utilizing noncoaxial transmitter
and receiver optics was Investigated experimentally
and theoretically using two 60-inch diameter glass
searchlight mirrors. I
Narmco Industries, Inc. , San Diego, CalK.
RESEARCH TECHNIQUES; AND METHODS ON WHICH
TO BASE DEVELOPMENT OF HIGH TEMPERATURE
a,AZING ATTACHMENTS, by Gerald K. Partain,
Floyd A. Piscopo, and Roger E. Wilson. Rept. on Con-
tract AF 33(616)5763. Mar 60, 69p. 9 refs. WADD
Technical rept. 60-119; AD-240 357.
Onler from LC mi$3. 90, ph$10. 80 PB 153 259
This report released for sale to the public 14 Dec 60.
This report describes the aevelopment of processes
for the integral bonding of low expansion glasses (pri-
marily aluminosilicate) to provide for either a load
carrying attachment systein or a means of accon^llsh-
Ing an airtight seal at the {gazing edge. Test of two
types of attachments (a fused glass- to- metal and a
brazed glass- to- metal) for Corning Glass Works Code
1723 and Pittsburgh Plate Glass Co. Code 6695 alu-
minosilicate glasses and bondline shear values exceed-
ing 400 psi at -80°F and 9000F. Thus, the feasibility
of these methods of attachnpent has been demonstrated
although the degree of practicality is not yet known.
Discussions of various asp^ts of mechanically held
•nd free floating designs ate also presented. (Author)
National Research Labs. , Ottawa (Canada).
AN EXPERIMENTAL INVESTIGATION OF THE DE-
FLECTION OF A FREE -AIR JET BY A FLAPPED
WING: THE SUPERADDITIVE EFFECTS OF
SHIELC«:D flow control- E«VICES. by D. J.
Uu-sden and P. J. Pocock. July 60, 56p. 9 refs.
Aeronautical rept. LR-285;rNRC no. 5919.
Order from LC ml$3. 60, pW9. 30 PB 152 786
Methods for improving the slipstream deflection
effectiveness of a 40-percent chord single -slotted
double flap were studied experimentally using a half-
wing model mounted in a free-air jet. The tests were
conducted out of ground effect. A porous suaion strip
OKI the nose of the fore flap, when shielded on either
side of the jet by chordwlse fences. Increased
markedly the slipstream tuitning effeaiveness of the
flap. The increase was greater than that due to the
•um of the separate effects of porous suction and
fences. The tests Indicate tjiat the flapped aerofoil
with the shielded- suction system would deflect through
90 degrees the slipstream from a propeller with a
(Hameter 0. 75 times the wing chord. The suction
power required la modest- However, the turning loss
would be 30 percent or letfs, (Author)
-^.^^^^,«^-
National Research Labs. , Ottawa (Canada).
MEMBRANE THEORY OF LARGE SPHERICAL RA-
DOMES. by A. L. M. Grzedzielski. May 60, 83p.
14 refs. Aeronautical rept. LR-278; NRC 5917.
Order from LC mi$4. 80. ph$13. 80 PB 152 832
Two methods of stress analysis of large spherical ra-
domes are developed: an elementary desk calculator
analjrsis, based on the restrictive assumption of air-
load being axially synmietric with respect to the wind
direction, and a general unit load method, making use
of a medium size digital computer. Both account for
an elastic support at the foundation. (Author)
National Research Labs. , Ottawa (Canada).
PRESSURE EHSTRIBUnON AND FORCE MEASURE-
MENTS ON A VTOL TILTING WING -PROPELLER
MC»EL. PART II. ANALYSIS OF RESULTS, by
M. M. Currie and J. A. Dunsby. June 60, 76pp. 4 refs.
Aeronautical rept. LR-284; NRC no. 5918.
Order from LC mi$4. 50, ph$l2. 30 PB 152 780
This report presents in graphical form the results pre-
sented in Part I, NRC Aeronautical rept. LR-252(PB)
from pressure distribution and force measurements on
a half -wing model of a twin-engined tilt -wing VTOL
configuration. The profound influence of the slipstream
on these results is discussed in some detail. (Author)
(See also PB 143 579)
New Departure Dlv. . General Motors Corp. ,
Bristol, Conn.
RESEARCH Cfti DEVELOPING CCSIGN CRrrERL\
FOR AKn-FRICnON AIRFRAME BEARINGS FOR
HIGH TEMPERATURE USE, by W. F. ORourke.
Rept. for June 58-Oct 59 on Contract AF 33(616)5900.
[1960J 138p. 8 refs. WADD Technical rept. 60-46.
Order from OTS $2.75 PB 171 151
The purpose of this study is to develop design criteria
for ami -faction airframe bearings fen- use in air and
space vehicles. Desired operation includes 40,000
oscillatory cycles at tOCP? to 1200OF under a radial
load corresponding to approximately 5(X), 000 psi mean
compressive stress for a one-inch bore ball bearing.
Selected bearing and lubricant materials were screened
in specimen tests. Bearings made from the three most
promising material combinations were tested and the
results extrapolated to four other sizes. Results indi-
cate that performance is limited by the required load
with a maximum of 26. 500 cycles of operation having
been obtained at 90CP? and one-hall the prescribed
load, and 40,000 cycles at one-third the prescribed
load. The most promising materials are M-2 Tool
Steel and 440-CM Stainless Steel for rings and K-161B
Titanium Carbide for balls for temperatures to 9O0PF ,
and CR-2 Chromium Carbide for rings and Stellite
Star J Cobalt Alloy for balls at 1200OF. None of the
twenty-five lubricating aids showed a significant
improvement. (Author)
[Space Sciences] Lab. , General Electric Co. ,
Philadelphia, Pa.
THE THERMAL PROTECTION OF A RE-ENTRY
SATELUTE, by Sinclaire M. Scala. Rept. on Contraa
AF 04(647)269. 9 Mar 59. 30p. 14 refs. Technical
159
memo. no. 115; ^Technical Information Series R59SD336t
Aerophysics Operation Research Memo. no. 30; Docu-
ment no. 9-4639i .c, oc^
Order from LC ♦ii$2.70. ph$4.80 PB 153 2^
This report lete^sed for sale to the pubUCil6 Dec 60.
The intrinsic m4ss of coolant shield required for the
thermal protection at a re-entry satellite is a sensitive
function of the c«»oling scheme selected. Heat sinks are
not competitive. Ablating refractories constitute a
superior systemi when compared with transpiration
cooUng. Re-raclatlon cooling is extremely attractive
for satellite re-^ntry. As the ballistic parameter
varies from 50 tb 200, for a re-entry angle of 2 1/2°
from the horizojtal, the mass of shield required varies
by a factor of tw o. (Author)
Sperry Phoeniii Co. , Ariz.
THE DEVELOPMENT OF AN AUTOMATIC FLIGHT
CC»n-ROL SYSTEM AN/ASW-12(V). Quarterly prog-
ress rept. no. i 1 Oct-31 Dec 59, on Contract
DA 36-039- sc-7|5040. 31 Jan 60, 57p. 13 refs. Rep«.
no. LJ-126O-0O01-7. ^ ^^^
Order from LC mi$3. 60. ph$9. 30 PB 152 230
The installation of the Automatic Flight Control Sys-
tem AN/ASW-li(V) in heUcopiers. H-21 and H-37,
and in fixed-wi^g aircraft, RL-23, is described in
detail. Solutionis to Installation problems are indi-
cated. The flight test programs for the S-55 and H-21
helicopters are (discussed. Illustrative recordings of
pitch, roll, yavi, RPM, and altitude performance in
the S-55 are in4luded. Data outlining authority limits
for four flight cjondiiions are included to complement
a previously issued report of a computer study of the
YAO-1 aircraft stabilized by the AN/ASW-12<V).
Tests conducted to determine effects of gamma radia-
tion on electror ic components are reported. (Author)
(See also PB 14^412)
Vienna Inst. c# Tech. (Austria).
ELASTIC THeIu^AL STRESSES IN DELTA WINGS.
PART I, by H. Parkus. Rept. on Contract
AF 61(052)214. 1 15 July 60, 96p. 11 refs.
AFOSR TR-60H140.
Order ffom LC|ml$5. 40. ph$15. 30 PB 152 437
I
Contents:
General relatiotis for shallow shells
Shallow conical
shells
Solution for firit approximation
Ch#mkal Engineering
American Machine and Foundry Co. , Niles, 111.
SYSTEM FOR IRECOVERY OF WATER FROM
URINE. PART II. DESIGN, FABRICATION, AND
TESTING OF THE PROTOTYPE SYSTEM, by
J. D. Zeff andh. A. Bambenek. Rept. on Equipment
for Life Support in Aerospace, Contract
AF 33(616)5783. Aug 60, 35p. 3 refs. WADC Tech-
nical rept. 58-&62(II).
Order from OTJSJ 1.00 PB 171 145
A prototype system to recover pocable water from
urine has been designed, fabricated and tested. The
basic system evolved from phase one, and was de-
signed to require no auxiliary power, and to funaion in
a weightless environment. The second-phase system
is an improved version of the basic system. A test
setup was assembled to simulate conditions of thermal
transport in a vehicle in extraterrestrial flight. The
test program determined system capabilities and ,
quality of the recovered water. Results indicated (1)
water is of potable quality; (2) over-all yield of recov-
ered water is about 80^ due to imperfea sealing of the
vacuum system; and (3) the system operated 8at»8fac-
torily in an inverted position (evaporator over con-
denser), which imposed a 1-g penalty on the system.
An advanced design incorporating improved structural
and sanitary design features is included in this report.
(Author)
Fehman Research Labs. , Picatlnny Arsenal,
Dover, N. J.
NEW RED. GREEN, AND WHITE COMPOSITIONS
FOR HAND-HELD ROCKET-TYPE SIGNAL FLARES,
by Everen Crane and Joseph Kristal. June 60, 14p.
2 refs. Technical notes no. 50; AD- 239 166.
Order from LC ml$2. 40. ph$3. 30 PB 152 079
To meet the need for a new series of red, green, and
white flare compositions (designated XM144 through
XM149) for use In hand-held ground illumination sig-
nals, seven red compositions, four green composi-
tions, and two white compositions were developed and
tested. The requirements for the new flare series '
that they produce sharply defined, easily distinguish-
able colors lasting 60 seconds for parachute-type
flares and 8 seconds for cluster -type flares - were
most fully met by the following compositions: (a) Red
flare compoaition FR508 consisting of atomized mag-
nesium 30%. strontium nitrate 42%. polyvinyl chloride
12%. potassium perchlorate 9%. and Laminae 7%. (b)
Green flare compoeltion FG466 consisting of atomized
magnesium 35 parts, barium nitrate 22. 5 parts, poly-
vinyl chloride 13 parts, potassium perchlorate 22.5
parts, and Laminae 5 parts, (c) White flare composi-
tion FY926 consisting of atomized magnesium 49%,
sodium nitrate 43%, and Laminae 8%. Average
candlepower was 24, 800 for the best red composition,
10, 500 for the best green, and 66, 000 for the best
white. Average burning times were 63 seconds for
the red compoaition, 62 seconds for the green, and
59 seconds for the white. (Author)
Oklahoma U. Research Inst. , Norman.
DEMINERALIZATION OF SALINE WATER BY ELEC-
TRICALLY-INDUCED ADSORPTION ON POROUS
GRAPHITE ELECTRODEa Rept. on Contract
14-01-001-160. Sep60, 63p. 28 refs. Saline Water Re
search and Development Progress rept. no. 45.
Order from OTS $1. 75 PB 171 129
Anion- responsive electrodes were prepared from
treated graphites and combined in demineralizatlon
cells with cation- responsive electrodes improved by
chemical treatnwnt. Though further attention must be
paid to Increasing the demineralizatlon capacity, such
cella are of great Interest because of their very low
160
k
tiflctrode cost. Investigations were also directed to-
ward improvements in the chemical stability of these
electrodes and toward the discovery of new methods
which will yield cation- or anion- re^xmsiveness to
ir^ihite. The nature of tl^e electrode process was
■bown to be more complect in character than was ini-
tially believed. An extensive survey of the literature
suggested several intriguing possibilities for further
investigation, which should yield results not only useful
to this project but also of distinct si^ficance to ear-
bcn electrochemistry.
-I
Civil Ef>gin««ring
Banelle Memorial Inst.'", Columbus, Ohio.
AN INVESTIGATION OF COLUMN ACTICW DURING
CREEP BUCKUNG, by R., L. Carlson, W. W. Breindel
aadG. K. Manning. Rept. for 1 Mar-18 Dec 59 on Con-
traa AF 33(616)6301. June 60, 54p. 21 refs. WAEX)
Technical rept. 60-7.
Order from OTS $1.50 PB 171 149
Procedures for inspecting a creeping column for su-
faUlty are discussed, and the studies at Rabotnov and
Sheaterlkov and those Vaf de Veubeke are interpreted as
flBUnples of two essentially different possible proce-
dvea. An alternative Inspection procedure, similar to
that of de Veubeke, is proposed, and an analysis of the
mechanics Involved is performed. It is noted that the
equations evolved provide a relatively direa means of
fxperimentally investigating the validity of the Hoff
column-creep- buckling solution. The equations are
also used to illustrate the essential differences in col-
umn action between purely viscous and viscoelastic
materials and materials with a nonlinear time-
dependent compjoneni of deformation. The results of
interrupted column-creep experiments are presented,
•nd they are analyzed by the use of the theory devel-
oped in the report. The agreement between the analyti-
cal and experimental results is Judged good enough to
indicate that the Hoff-de Veubeke approach to the
column-ereep-buckling problem is basically sound.
(Author)
i
Brown U. Dlv. of Engineering, Providence, R. L
TOE MECHANICS OF THE TRLVXL^L TEST FOR
SOILS, by R. M. Haythomthwalte. Technical rept.
na 1 on Contract DA 19-020-ORD-4566. Apr 59, 35p.
19 refs. AI>217 169.
(kder from LC mlW. 00, ph$6. 30 PB 149 699
Analysis is used to discuss the significance of tests on
■and where the specimens f re caused to fail with axial
■ttauion rather than with the more conventional axial
compression. .
Electrical and Electronic Engineering
!
Aero Ceo Astro Corp. , Aiexandria, Va.
ICANNING TECHNIQUES FOR LARGE FLAT CX)M-
ttJNICATION ANTENNA ARRAYS, by J. P. Shelton,
l ». Perrino, and A. B. Davis. Scientific rept. no. 1
■ Contract AF 19(604)5217. 31 Jan 60, 70p. 15 refs.
APCRC-TN-60-158; AD-235 571.
Order from LC mi$3. 90, ph$10. 80 PB 149 059
161
A summary is presented of the progress made on I
scanning techniques for large flat communication
arrays. The effort was divided into experimental and
theoretical projeas. The experimental program has
included phase shift techniques in open two-wire line
and enclosed transmission line. The most promising
results were obtained with a circularly polarized co-
axial configuration using the TEn mode. Theoretical
studies were made in three areas -- circularly polar-
ized phase shifters, multiple beams from linear ar-
rays, and elimination of broadside resonance in
traveling -wave arrays. It was found that any circu-
larly polarized component should be fed by a hybrid
junction, the fourth output being terminated to absorb
any reflected waves. Multiple-feed systems for ar-
rays were analyzed, and networks for connecting N
inputs to N elements are presented, N being limited to
2l3"^. A method for eliminating the broadside reso-
nance in traveling-wave arrays in which the junction
may be separated from the element is described. A
tentative program for completion of the scanning sys-
tem study is given. (Author)
Aeronautical Electronic and Electrical Lab. , Naval
Air Development Center, Johnsville, Pa.
PROCEDURES FOR SHOCK AND VIBRATION TESTS
FOR NAVAL AIRBORNE ELECTRONIC EQUIP-
MENTS, by A. Cohen. Final rept. on TED ProJ.
no. ADC EL-549. 11 Jan 54, 7p. 6 refs. Rept.
no. NADC-^L-L53192; AD- 30 646.
Order from LC mi$1.80, ph$1.80 PB 153 260
This report released for sale to the public 8 Dec 60.
Tests were conducted to determine the ability of air-
borne electronic equipment to withstand the 30-g shock
requirements of Spec no. AN-E- 19-1. A Barry Corp
VD-150 shock-test machine was used for all shock-
testing of Naval air-borne electronic equipments. The'
machine was modified by Installing a pneumatically
operated diaphragm in the base to agitate the sand uni-
formly between drops, and a sand-leveHlng device was
constructed to insure that the initial surface was even
and horizontal. Modifications were also made to im-
prove the utility of the machine. It was concluded that
the nruchine did not Impose a uniform shock of 30 g
with a duration of 11* 1 msec on the equipment being
tested. It was recommended that development work on
shock-test machines be continued with the ultimate
aim of obtaining flat-topped shock pulses which can be
controlled in amplitude and duration, and that the
Barry VD-150 shock-test machine be used in the
interim until a more satisfactory machine can be
developed.
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
AN ENC«»IRE ARRAY CONTINUOUSLY PROXIMTTY-
COUPLED, by George R. Forbes. Dec 59. 23p. 5 refs.
AFCRC-TR-59-368; AD- 234 385.
Order from LC mi$2.70, ph$4.80 PB 148 705
A new type of endflre arrty that is continuously prox-
imity-coupled is described. The antenna consists of
dipole elements capacltively coupled to an open two-
wire Une. The coupling impedance is examined aa a
function of various parameters of a single dipole on a
two-wire transmission line. The array input impedance
and radiation panems are determined under various
conditions for a 7. 5- wavelength array.
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
A STEERABLE-BEAM CORNER ARRAY, by Allan C
Schell. Dec 5^. 25p. 13 refs. AFCRC-TR-59-373:
AD- 234 384.
Order from LC miSZ. 70. phK 80 PB 148 709
An anteraia suttabie for electronic beam steering or
scannii^ wtth^ a limited sector ««s designed and built.
The antenna consists of a nianber at feed elements
located within the comer formed by 2 intersecting con-
ducting planes. A Fourier series approximation to a
desired radiatnon pattern can be obtained by the proper
adjustment al element currents. Elevation andazimtjth
patterns for various conditions were computed. In the
experimental verificackn, an 11° beam was«steered
within a 30° sector by a 60^ comer array. (Author)
i
Air Proving Ground Center, Eglin AFB, Fla.
ELECTRONIC COUNTERMEASURES MATERIEL
HANDBOOK, $y Isabel K. Longaker. May 59. 34p.
APGC TN-59H25.
Order from Up mi$3.00, ph$6. 30 PB 153 067
This repoart raieased for sale to the public 2 Dec 60.
This technicaj note describes the ECM supply requisi-
tioning procedures at the Air Proving Ground Center,
Eglin Air Forte Base, Florida; discusses the Joint
Nomenclature System: and provides a ready reference
for Group B components contained in the Air Force
Electronics Oountermeasures Program. (Author)
Airborne Instruments Lab. . Deer Park, N. Y-
RESEARCH SERVICES ON MOVING-TARGET INDI-
CATION, by A. Nirenberg, E. Letscher. und
P. Seckendorn Final engineering rept. on Oontract
AF 19(604)17^1 Mar 60, 177p. 10 refs. Repc. no.
3905-1; AFClic TR-60-109; AD- 234 747.
Order from LC mi$8. 10, ph$27. 30 PB 148 711
An accurate. |ugh rate, digital radar data recording
and handling System is described. The system was
designed and fabricated to gather data on the physical
and statistical characteristics of radar ground clutter;
this informatibn will be used to provide a basis for de-
velopii^ new tnd improved techniques and circuitry
for MTl radar systems. Each of eight discrete param-
eters describing a single radar target can be quantized
into an 11 -bit binary number (each radar repetition
period) and riconled on magnetic tape. This data is
transferred ti punched paper tape and made available
in a form suiqable for the Eckert Mauchley digital
computer, wHich calculates such clutter character-
istics as signal time functions, correlation functions,
and probability distributions.
Init.
American In^t. for Research, Pinsburgh, Pa.
THE DESIGN OF TEST DEVICES FOR PREVEN-
TIVE MAINTENANCE OF GROUND ELECTRONIC
EQUIPMENT, by Robert Fitzpatrick, John Brinda, Jr.
and others. Riept. on Contract AF 30(602)1654.
Feb 59, 85p. 8 refs. AIR-244-58-FR-182; RADC TR-
58-172: AD- 2(>7 529.
Order from LC mi$4.80, ph$13.80 PB 148 284
The abjective of this study was to develop teat meas-
urement techniques from the human engineering point
of view for the preventive maintenance of ground elec-
tronics equipment by relatively inexperienced 3- and
5- level nnaintenance men in the Airways and Air
Communicatioas Service (A ACS). An initial survey
indicated that teat measurement requirements in five
years are likely to differ linle from those al today.
Hence, teat nteasurement requirements were ab-
stracted from AACS Preventive Maintenance Instruc-
tions for a representative group of prime equipments.
Varioua ubies were then drawn up to show the range*
erf electrical properties required.
Amperex Electrortc Co. , Hicksville, N. Y.
DEVELOPMENT OF HIGH POWER TUNABLE
X-BAND MAGNETRON, by David Saalaw Final rept.
on Contract OA 36-039- sc-64740. [1959] 55p.
AD- 162 022.
Order from LC mi$3. 60, ph$9. 30 PB 152 228
The objective of this program was to develop a
tron which would meet both the performance and
dimensional requirements of the type 5780 magnetron,
but would incorporate an impregnated cathode to sub-
stantially increase the life of the magnetron. The type
5780A magnetron has a longer life than, and is com-
pletely interchangeable with, the type 5780 magnetron.
The final design features a relatively low operating
temperature for the cathode and characteristics which
are essentially independent of heater voltage
fluauaUons. (Author)
[Army Signal Research and Development Lab. ]
Fort Monmouth, N. J-
ANALYSIS OF MEASURED RADIATION PATTERNS
OF TWO HF ANTENNA ARRAYS AND ONE
RHOMBIC^ by Helmut Brueckmann. Jan 57. 74p.
13 refs. En^neering rept. no. E-1198.
Order from LCml$4.50, ph$12.30 PB 152 990
This report released for sale to the public 29 Nov 60.
The measured radiation panerns of all antennas agree
in major points with theoretical expectations. Where
they deviate, plausible explanations were found.
Agreement with operational tests is satisfactory con-
sidering the organizational and technical shortcomings
of these tests. It was again demonstrated that rhom-
bics rejea interfering signals arriving from the
forward azimuth sector poorly. The antenna arrays
have auperior properties, but are relatively narrow
band devices. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
THE EFFECTS OF NUCLEAR RADIATION ON
POWER TRANSISTORS, by Frederick Gordon. Jr.
15 Aug 58, 26p. 7 refs. USASRDL Technical rept. 1981
Order from LC mi$2. 70, ph$4. 80 PB 152 804
This report presents the results of nuclear radiation
experiments performed at the Brookhaven National
Laboratory to determine the effects of this radiation
on power transitors of various types. A brief analysis
of device parameter changes and of the evaluation of
162
die lesulu is presented. In additkm. there is a short
(KseuMlOB o* the interrelation between the minlmizii^
rfihe effects at nuclear radiation on transistors and
dv ipedfic application of the devices. The device
types Ihst were exposed were homogeneous -base ger-
manium power transistots. The device parameters
itat were monitored were small -signal and large-
ilffwl grounded -emitter Orient ^n. aa well as the
reverse coUectar current. The techniques al meas-
uremeni included multiple point measurements and
curve tracer techniques. The results show fair agree-
■ moH between experimenl^l results and calculated
values. (Author)
Army Signal Research and Development Lab. ,
Fort Monmouth , N . J .
PROCEEDINGS OF THE SYMPOSIUM ON HYDROGEN
THYRATRONS AND MODULATORS [NO. 5] HELD AT
Tie HEXAGON, FORT MONMOUTH, N. J. ON
20, 21, 22 MAY 1958. [1958] 333p. 11 refs.
Order f rom LC mi$ 11.10 ^ ph^i. 60 PB 150 074
Contents :
Hydrogen thyratrons
Hydrogen thyratrons and ipagnetic devices
Modulator devices and techniques
Auxiliary devices and techniques
Modulator techniques
(See also FB 149 386)
BelJ Telephone Labs. , Inc. , Whlppany, N. J.
MICROWAVE SOLID-STATE DEVICES. Interim rept
DO. 10. 1 Apr -30 June 59. on Contract DA 36 -039-sc-
73224. 15 Aug 59. 30p. 2 refs; AD- 227 412.
Order from LC mi$2. 70. ph$4. 80 PB 149 720
Mtaer action in ruby has been studied over the fre-
quency range 1 to 9 kmc. On the basis at the study it
appears feasible to build practical traveling wave
masers using 0. 05 per cent ruby over the frequency
range 1 to 9 kmc. A preliminary report is given on
the design, fabrication and testing of diffused N*-i*'-P"*'
silicon diodes for protective limiters at microwave
frequencies. Of particular interest in protection appli-
catlona are the performance of the structure at high
and low signal levels, transition times, and thermal
properties. (See also PB lf4 934)
BeU Telephone Labs , Inc , Whlt>pany, N. J.
AN ULTRA -PRECISE STANDARD OF FREQUENCY,
by A. W. Warner. Interim !rept. no. 10, lOJan-
9 Mar 59, on Contract DA 36-039-sc-73078. 23 Mar59,
29p. Rept. no. 27480-1; AD- 220 117.
Order from LC ml$2. 70, p|44. 80 . PB 149 719
A discussion is presented ojf problems related to the
design al crystal units having low acceleration coeffi-
dents, measurements of frequency aging with respect
to crystal unit operating teitiperature, performance
figures for an experimental transistor oscillator and
o»cn, and details of some facilities. used in the fabrica-
tion of the crystal units. A number of 5-mc ruggedized
erjwul units were nude and tested. Tests of one unit
h«»e demonstrated the feasibility of meeting the re -
fiirements for missile borne applications. Tests to
waluate the redesigned 2. 5-mc ultra -precise crystal
unit have not shown the expected improvement. The
temperature controlled 5-mc transistor oscillator
circuit has a short -time frequency stability of
-1 pp IQlO and should prove satisfactory for use under
conditions of shock and vibration. (Author) (See also
PB 144 300)
California U. , Los Angeles.
DYNAMIC PROGRAMMING AND NUMERICAL EX-
PERIMENTATION AS APPLIED TO ADAPTIVE CON-
TROL SYSTEMS, by MasanaoAoki. Doctoral thesis .
Rept. on Contract Nonr-233(52). Feb 60, 22:^«r
33 refs. Dept. of Engineering rept. no. 60-16;
AD- 236 968.
Oder from LC mi$9.90. pfa$34.80 FB 147 651
Solutions of a class of adaptive control systeins,
especially those similar to the Two Armed Bandit
problems, are formulated and discussed. Attempts
are made to incorporate some of the ideas of statisti-
cal decision theory, dynamic programming, and
numerical experimentations to provide a more flexible
formulation of problems of atialysis and synthesis of
adaptive control systems. The method used consists of
setting up mathematical models, simplifying them so
that they admit analytic solutions, and using some ap-
proximating analytic or numerical techniques. Using
dynamic programming as the main tool of the investi-
gation, discrete deterministic and stochastic comrol
systems are formulated as multi-stage decision proc-
esses. Control systems with random inputs are taken
up; they are called adaptive control processes. Com-
.putational procedures of solving recurrence relations
are presented and examples are given<
California U. , Los Angeles.
DYNAMIC PROGRAMMING APPROACH TO A FINAL-
VALUE CONTROL SYSTEM WITH A RANDOM
VARIABLE HAVING AN UNKNOWN DISTRIBUTION
FUNCTION, by M. Aoki. Rept. on Conlraa Nonr-
233(52). Feb 60, 41 p. 18 refs. Dept. of Engineering
rept. no. 60-15; AD- 239 651.
Order from LC ml$3.30, pW7.80 FB 149 136
Given a criterion of performance, the duration of the
process, and the domain of the control variable, a
sequence of control variables, .^n)-. is determined as
a function of the stats vector oflKe system and lime.
The functional equation technique at dynamic program-
ming is used to derive a recurrence relation of the
criterion function of the process kn(x, z) where x Is
the state variable of the system when there remain n
control stages. A concept of suboptlmal policy is
introduced and numerical experiments are performed
to test suboptlmal policy suggested from numerical
solution. The system behavior under the suboptlmal
policy is also discussed. (Author)
Case Inst, of Tech. , Cleveland, Ohio.
IMMFTANCE SYNTHESIS THROUOI POLE -ZERO
CONFIGURATIONS, by John Peatman. Scientific rept.
no. 16 on Contract AF 19(604)3887. 29 July 60, 38p.
3 refs. AFCRL TN-60-951.
Order from LC ml$3.00, ph$6.30 PB 152 262
This paper deals with the synthesis significance at the
pole-zero configuration of an immlttance function.
163
Several d the ba|ic immitiance synthesis conceps are
described in terms of pole -zero plots and roo« locus
techniques. Theate include the poaitlve real character,
resistance and otiducunce rennoval, and >^axls sin-
gularity removal. It Is demonstrated that the 0**-180<^
phase locus d an immittance function is an invariant
with respect to resistance or conductance addition or
removal. Rank reduction of non-minimum resistance
functions is censored through combinations of resist-
ance and conductance removal, predistortion, and a
bilinear transformation. Partial fraaion renKwal is
also considered 4nd a graphical means described for
determining whether the remaining function is positive
real. (AuUkv)
Columbia U. School of Engineering, New York.
AN ADAFnVE SYSTEM USING PERIODIC ESTIMA-
TION OF THE $JLSE TRANSFER FUNCTION, by
Stephen Bigelow 4nd Herman Ruge. Technical rept.
T-40/B on Contr|ct AF 18(600)677. 30 June 6a 34p.
7 refs. CU-63-40-AF-677-EE; AFOSR TN -60-688;
AD- 243 718.
Order from LC liii^. 00. ph$6. 30 PB 152 2^3
Many schemes fqc the practical realization of adaptive
control have bee« proposed. The purpose at the in-
vestigation desc|ibed here was to gain insight into the
behavior of such^schemes by studying in detail a par-
ticular plant -ad^ive control system. In connection
with this work a general purpose digital computer has
been used for ex|)crimenul simulation. The system
considered may be described in terms of two basic
blocks, the plan( and the control computer. The con-
trol computer is a digital device, and as such its in-
puts and outputs are inherently sampled signals. It is
convenient, therefore, to treat the entire system as a
sampled data sy$tem. The plant or process to be con-
trolled is assum^ to be a continuous, low-pass
linear but time-tarying dynamic system, and to in-
clude a zero-or(ier hold which converts the sampled
input to a piecevfise- constant signal. The control
computer served two basic purposes. First from
samples c^ the p^nt input and output it computes
periodically a stjatistical estimate at the plant pulse
transfer function Second using the current estimate
of the dynamic behavior of the plant and measure-
ments of system input (setpoint) and output, the plant
input is compuiad in accordance with a suitable over-
all performance criterion. This general scheme d
plant -adaptive control obtains information about the
current dynamics at the plant from measurements d
nornnal plant input and output alone.
Crosby Labs. J Inc. , Syosset, N. Y.
FACSIMILE REPEATER STUDY, by R. Theodore
Nelson. Final rrpt. for 15 June- 15 Aug 58, on Contract
DA 36-039-8C-5i6681. 15 Aug 58, 61p. AD- 208 631.
Order from LC hiiJ3. 90, ph$lO. 80 PB 152 226
The investigation resulted in the development of three
new equipments. All provide one or ntvore facilities for
Improving facsimile operation by noise reduction tech-
niques and/ or operational functions. The units are:
CV-472 ( )-GXR| Receiving CHverslty Combiner, CV-473
( )-GXT Transmitting Converter, and AN/GXH-4 ( )
Storage System, The CV-472 is a receiving adapter
provklliv diversity combination in accordance with the
ratio- square principle; also included are other inter-
ference reduction circuits and operational featurea.
The CV-473 is an improved transmitting converter with
both dc and SCFM outputs; pre- emphasis is provided
along with several operational improvements. The
AN/CaCH-4 system provides storage of AM facsimile
signals for subsequent relay purposes. Units are in-
stalled at various ACAN facilities for long term tests.
Results to date indicate excellent interference and
multipath reductions as well as much improved opera-
tional facilities. Evaluations indicate a 7 db visual
(12 db theoretical) improvement resulting from employ-
ment of pre- emphasis and de- emphasis, an observed
balanced discriminator signal- to- noise Improvement
in the order of 10 db, an estimated average improve-
ment (under severe circuit conditions) of about 15 db
resulting from the use of diversity, and an additional
3 db (maximuni Improvement due to diversity combi-
nation, amounting to a possible 35 db Improvement over
standard converters. (Author)
Diamond Ordnance Fuze Labs. . Washington, D. C.
VARIATION OF COMPLEX Y PARAMETERS WITH
EMITTER CURRENT AND TEMPERATURE, by
Nicholas KyrUkopoulos. 17 Oct 60, I6p. 5 refs".
Technical rept. TR-885.
Order from LC mi$2. 40, ph$3. 30 PB 152 920
The effeas of elevated temperatures on the complex Y
parameters of the 2N700 transistors were studied.
Measurements were made at a frequency of 5 Mc and
temperatures of 25°C, 50°C, and 80°C of parameters,
Yib. Yie. Yfe, Yob. and a, as functions of emitter
current at constant colleaor voltage. The Yfe, Yob.
and a parameters increased with temperature, Yie
decreased while Yib did not change. (Author)
Eastman Kodak Co. , Rochester, N. Y.
DEVELOPMENT OF AMMONIA VAPOR ACTIVATED
BATTERIES, by V. M. Bryant. Jr. and B. K. Burke.
Final rept. 24 May 56-30 June 59, on Contract DA 36-
039-SC-71232. [1959] 99p. 1 ref; AD-232 343.
Order from LC mi$5 40. ph$15. 30 PB 149 702
Research was directed towards the development d 2
baneries using NH3 vapor activated electrochemical
systems as a means of evaluating the practicability d
the AVA system for various requirements. The XM-
AVA-l and XM-AVA-2 were developed which were ca-
pable of meeting the design specification only in part.
The electrochemical system Zn/NH4SC:N/Pb02 used in
the XM-AVA-1 was too greatly affected by temperature
at the required current density to be capable of operat-
ing at a given current within a voltage tolerance of
±7. 25t from -65° to I6OOF. The XM-AVA-2 package
was not within the contour specified. Service d over
20 hr was achieved at room -ambient temperature. At
OPF, service in excess of 8 hr was attained. The fall-
oft In service life at lower temperatures appeared to
be a problem of formation of solutions of proper con-
centration and the retention of such solutions in the
cells over a long period of time. From an over-all
sundpoint the XM-AVA-2 banery was concluded to
more closely meet the requirements than the XM-
AVA-l bsitery.
■■ :)••
164
Eastman Kodak Co. , Rochester, N. Y.
RADAR BEACON AN/DFN-14 (XE-3), by Edward
CorneUus. Final rept. fcxr Sep 56-Oa 58, on Contract
DA 36-039- 8C-73097. [1959] 60p.
Order from LC ntU$3. 60,, p»^9. 30 PB 152 229
The work performed In the development and provision
of design approval models of an Improved version of
the AN/DPN-14 (XE-2) Radar Beacon is reported. A
short history d the project, the purpose and the major
•1ms of the development are presented. The improved
version is briefly descri^ along with problems en-
countered In effecting imt>rovenrkents and the means of
resolution. Conclusions reached and recommendations
to be evaluated are included. A report on the elec-
trical and environmental tests performed to qualify
the AN/DPN-14 (Xfi-3) Beacon to the full extent of the
Sgnal Corps Tech. Req. 1 SCL-2918-B is appended.
(Author) '
Electric Storage Battery Co. , Yardley, Pa.
INVESTIGATION OF AgO PRIMARY BATTERIES, by
P. Reutschi and R . Amlie. Quarterly rept. no. 1,
1 June-31 Aug 59, on Contraa DA 36-039-8C-78318.
30 Sep 59, 38p. 50 refs. ♦
Order from LC mi$3. 00, ph$6. 30 PB 149 697
The fundamemal electrochemistry d sllver-zlnc
batteries Is discussed. S^lf-dlscharge and in particu-
lar gassing of AgO in various electrolytes has been
studied. Pasted and electroformed AgO plates are
compared. An automatic cut-out voltmeter relay has
been developed. (Author) (See also PB 147 974)
Electronics Research Lab. , U. of California,
Berkeley. 1
QUARTERLY PROGRESS REPORT. Rept. for 1 Apr-
30 June 59 on Contract N7onr-29529. 15 July 59. 22p.
1 ref. Series no. 60. issue no. 25; AD-226 513.
Order from LC mi$2. 70. ph$4. 80 PB 149 734
!
Contents: I
Back -scattering, from cones
Microwave plasma problems
Scattered fields from anisotropic media '
Ferrlte field -displacement device for slot coupling
control
Parametric amplifier usin|f triply resonant mode cavity
New forms of Huygens prlQciple^ '
Network theory 1
Electronics circuit research
Information theory
Solar emission and absorption
Research in high temperature semiconductor devices
Magnetic amplifiers (See ^Iso PB 145 072)
Electronics Research Lab. . U. of California.
Berkeley. 1
STUDY OF CROSSED-FIELD AMPLIFIERS, by
J. R. Whinnery, C. K. Bridsall and others. Quarterly
progress rept. no. 1. 1 Feb -30 Apr 60. on Contract
DA 36-039-SC-85278. (1960) 18p. 4 refs. AD- 240 767.
Order from LC mi$2. 40. ph$3. 30 PB 152 562
Experiments are made with the crossed -field velocity
•nslyzer, to determine the velocity-distribution curves
165
at several points across the beam for temperature-
and space -charge -limited operations of the cathode.
The results indicate high temperature at the inner edge
of the beam which may be due to some kind of edge in-
stabilities in the beam. The behavior of noise figure
with operating parameters was observed. The cathode
temperature, gas pressure, and beam -forming elec-
trode voltage were found to have a marked effect on
noise figure. A measure of noisiness was defined.
(Author) (See also PB 148 106)
Electronics Research Lab. , Stanford U. , Calif.
UNIVERSAL TUNING CURVES FOR REENTRANT
CAVITY RESONATORS, by Glenn Walters and Robert
L. Tanner. Technical rept. no. 2 on Contraa
N6-ari-106, Task DI. 15 Ai« 47, 26p. 4 refs.
Order from LC ml$2.70, pfa$4.80 ft 153 381
This report released for sale to the public 15 Dec 60.
A set of universal tuning curves for reentrant cavity
resonators is presemed. The data of these curves
were obtained from a network analyzer which, acting
as a circuit analogue for a resonant cavity, yields
solutions to the wave equation In cylindrical
coordinates. (Author)
Engelhard Industries Inc., East Newark, N. J.
INVESTIGATIVE RESEARCH PERTAINING TO
CATALYTIC HEATING OF PRIMARY BATTERIES,
by Sydney H. Reiter. Quarterly progress rept. no. 1,
1 May-31 July 59, on Research of a Suitable Fuel-
Catalyst Combination for Arctic Conditions, and
Development of a Catalytic Battery Heater, Contract
DA 36-039- sc-78914. [1959] 12p.
Order from LC mi$2.40, ph$3.30 PB 149 698
A combustion train was set up together with the equip-
ment intended for use in the cold chamber. When
operated with alcohol, self ignition was achieved with
the catalyst, the heater becoming quite warm, and the
system operated under laboratory conditions. (See
alsoPB 149 611)
General Mills, Inc. . Minneapolis, Minn.
COMPONENTS SUITABLE FOR AUTOMATIC AS-
SEMBLY, by J. W. Buffington. Flhal rept. for
15 Feb 56-15 Nov 57 on Contract DA 36-039-sc-7ll80
15 Nov 57, 259p. 12 refs. Rept. no. 1812.
Order from LCmlSl 1.10, ph$39.60 PB 150 803
Electronic components have been examined in an ef-
fort to establish design standards for rendering the
components suitable for assembly onto printed wiring
boards by automatic techniques. A particular standard
grid was established as being most practicable. The
factors governing the use <rf a grid system are dis-
cussed. A basic grid is recommended, and arguments
in support of this are presented. A system of modular
dimensions Is presented for use with all electronic
components and auxiliary hardware. The system takes
into account the space efficiency of components, sub-
assemblies and assemblies. Form factors for the
differem component types are examined. Preferred
shapes for lead -handled components are specified and
orienting of this type d compooent is discussed.
Body-held compooeiKB are also examined and the in-
dexing requirementB are established for automatic
handling. The requirements necessary to render
body-held componeilts as a group suitable for auto-
matic handling are rigid and in most cases difficult to
maintain. Therefore, the requirements are discussed
f6r body-held comptxients, themselves not suitable for
automatic handling J which are to be used with lead-
handled component^ which are suitable for automatic
handling. Leads fot both lead-handled components
and body-held compionents are examined. Thermal
requirements of thcj leads for heat generating compo-
nents are examinedjand a method of evaluating heat
dissipation is established. Component failure due to
acceleration and vibration is also examined, and
some guides are established for determining antici-
pated and allowable stresses. Proposed guide rules
for designing electrpnic components suitable for
assembly onto printjed wiring boards by aiaomatic
techniques are presented. (Author)
Georgia Inst, of Tbch. Engineering Experiment
Station, Atlanta. '
QUARTZ CRYSTAL, STUDIES AND MEASUREMENTS
PHASE I. MOTIONAL PARAMETERS. PHASE II.
EQUIVALENT ELECTRICAL PARAMETERS. PHASE
III. AGING OF QUARTZ RESONATORS, by Issac
Koga, J. E. Rhodes ^nd others. Interim rept. for
1 Mar-30 June 59, (tontraa DA 36-039-sc-78905.
[1959] 76p. 3 refs. [aD-225 275.
Order from LC mlM.50, ph$12.30 PB 152 231
Research concerns ^he study of the behavior of quartz
crystals as frequency control and filter elements. The
motional parameter! studies presented (phase I) are
(1) spectra of circular AT- cut quartz crystals and (2)
modes of motion of ^ circular AT-cut quartz crystal.
The equivalent elecitrical parameter studies presented
(phase II) are (1) substitution measurement system (2)
substitution-resisto^ construction and measurements,
(3) instrumentation, and (4) a complete high-frequency
crystal impedance nieter. The aging of quartz reso-
.uttor studies presented (phase III) are (1) apparatus,
(2) resonator ovens, (3) frequency measurement
bridge, (4) quartz b|anks, (5) 16. 25 mc resonator
studies, and (6) res<>nators fabricated at Georgia
Tech.
Hughes Aircraft C(». , Culver City, Calif.
CCRIVATIVE CGNIROL IN SHAHNG ANTENNA
PATTERNS, by A. I^sienskl. Scientific rept.
no. 3508/6 on Contrfca AF 19(604)3508. 24 Sep 59,
44p. 5 refs. AFCRd TN-60-110; AD- 233 091.
Order from LC mi$i30, ph$7.80 PB 148 297
An antenna pattern ^nthesis method is presented that
permits the approxiijriation of desired patterns with
arbitrarily prescribed error criteria. Thus smooth-
ness, lineiarity, or aurvature may be specified for any
part of the pattern. If desired, an equal ripple ap-
proximation may algo be very closely approached. The
techniques developed are applicable to arrays with
real excitation coefficients and to those capable of
complex excitations
J
Hughes Aircraft Co. , Culver City, Calif.
EFFECT OF RANDOM ERRORS ON BEAM POINTING
DIRECTION AND SIDELOBE LEVEL FOR ANTENNA
ARRAYS OF MANY ELEMENTS, by
L. A. Rondinelli. Rept. on Contract AF 30(602)1718.
Mar 59, 51p. 8 refs. Technical memo. no. 591.
Order from LC miJ3. 60, ph^. 30 PB 148 729
A theoretical statistical analysis is presented in which
a study was performed to determine the effect of ran-
dom current exciution errors iflpon the radiation char-
acteristics of a two-dimensional array of identical
radiators. A statistical nvodel is developed and it is
then argued that this model closely approximates the
nature of the radiated electric field produced by an
array of a large number of current elements, where
the individual element currents are in error both in
amplitude and phase. The analysis has been applied to
the stijdy of the following antenna characteristics: (1)
maximum sidelobe level within a specified cone about
the main beam, (2) maximum sidelobe level in the re-
mainder erf the half space outside the specified cone,
and (3) beam pointing accuracy. (Author)
Johns Hopkins U. . flalti'more, Md.
REPRESENTATION AND ANALYSIS OF SIGNALS.
PART VI. SIGNAL -SPACE CONCEPTS AND DIRACS
NOTATION, by David C. Lai. Rept. on Contracts
AF 19(604)1941 and Nonr-248(53). 15 Jan 60. 84p.
25 refs. AFCRC TN-60-167. supersedes AFCRC
TN-58-560; AD-235 151.
OrderfromLCmi$4. 80, ph$13. 80 PB 148 714
A signal is described as a geometric object, specifi-
cally, as a vector. The measurement erf a signal by
an instrument corresponds to projecting the geometric
object onto the particular coordinate axes (i. e. , the
basis of the signal space) that are established by the
specified instrument. Dirac's notation is adopted and
interpreted to provide a new representation of signals.
Based upon the 3 operations. 1. e. . sampling, time re-
versing, and filtering, new compact symbols and op-
erators are introduced to represent their mathematical
counterparts, i. e. . sifting, reversing, and convolving.
In establishing any operation or equation, the physical
and operational significance of the mathematics is
emphasized. The justification for this formulation de-
pends, aside from its internal consistency, upon its
usefulness for expressing compactly and concisely the
experimental process of analyzing signals. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
HlOi- POWER TUBE PROGRAM. Semiannual Technical
Summary rept. na 2, 1 Jan - 30 June 60, on Contract
AF 19(604)5960, ARPA Order 85-60. 30 June 60, 35p.
3 refs. AD- 241 412.
Order from LC ml J3. 00. phJ6. 30 PB 150 605
Contents:
Klystron bandwidth studies
Theoretical analysis of multicavity klystrons
MCK computer program
Hollow beam- klystron interaction
UHF klystron
Problems in fundamental limlutions
Biased collector
RF windows > ■ ■ ^
166
Secondary emission
Beam pulse heating |
Voltage breakdown
proUems in fabrication limitations
Cathodes
High- vacuum technology
Processing
(Xplexer investigations
Effect of gas purity on arc loss and recovery time
Breakdown curves
r
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
RADAR TECHNIQUES STUDY. Semiannual technical
summary rept. no. 2, ljan-30june, on Contract
AF 19(604)5960, ARPA Order no. 56-60. 30 June 60,
27p. 14 refs. AD-241 910.
Order from LC ml$2. 70, phJ4. 80 PB 150 604
Contents: ^
Radlometry
Detection of signals in non-gaussian noise I
Results for linear and limiting detector systems
Probability functions and values of parameters
Sequential detection
Radar measurement of range, velocity and acceleration
Product detectors for acceleration measurement
Delay- line analog -signal -processing techniques
Code-search experiment
Lincoln Lab. , Mass . Inst, of Tech. , Lexington.
SOME ASPECTS OF HIGH POWER WINDOW DESIGN,
byC. E. Muehe. Rept. on Contract AF 19(604)7400.
30ct 60, 27p. 12 refs. Rept. no. 46G-0003.
Order from LC ml$2.70. ph$4.80 PB 152 467
The purpose of a waveguide window as used in connec-
tion with a high power microwave tube is to let the
power through at the same time maintaining a good vac-
uum on one side of the window. As higher and higher
powers are generated witHTh microwave tubes, the prob-
lem of bringing the power out becomes' more and more
difficult . This report examines the various causes of
window failure and tries to point out methods of design
which may be used to eliminate these failures .
Lincoln Lab., Mass. Inst, of Tech., Lexington.
THE TRAVELUNG WAVE RESONATOR AND HIGH
POWER MICROWAVE TESTING, by Stanley J. Miller.
Rept. On Contraa AF 19(604)5200. 8 Jan 60. 51p.
6 refs. Group rept. 46-48.
Order from LC mi$3.60. phS9.30 PB 152 241
A comparatively new and interesting circuit element,
the travelling wave resonator, presents the microwave
engineer with a number of possible applications. The
application to be considered here is its use as a high
power simulator. The travelling wave resonator, or
ring resonator, permits one to test a transmission
component with a pure travelling wave and at field
levels considerably above those usually available to the
designer . j
I 1
Microwave Research Inst. , Polytechnic Inst, of
Brooklyn, NY.
MAXIMALLY -FLAT TIME DELAY AND ITS SYN-
THESIS, by Sid Deutsch. Re(|t. on Contraa
AF 30(602)1709. 20 Nov 58, 34p. 14 refs. Research
rept. R-696-58; PIB-624; RADC-TN-59-35;
AD- 210 114.
Order from LC mi$3.00, ph$6. 30 PB 148 980
For given values of "stray" shunt capacitance and load
resistance, the best possible linear-phase 2-terminal <
driving-point impedance is derived. The normalized
form of this Impedance is synthesized as an infinite
L-C ladder struaure that starts with a 2.718-farad
capacitor and tapers rapidly and smoothly to final
values of 2 farads and 2 henries. Whereas an uncom-
pensated RC model yleM» a time delay curve that is
down to 0.7854 at <0 «tT the optimum 2-terminal
structure yields a time delay curve that is flat to
U) '2.718. Its gain-delay bandwidth product is 3.461
times as great as for the uncompensated amplifier.
Microwave Research Inst. , Polytechnic Inst, of
Brooklyn, N. Y.
THEORETICAL AND EXPLORATORY EXPERIMEN-
TAL RESEARCH IN ELECTROMAGNETICS, NET-
WORKS AND RELATED SOLID STATE, AND PLASMA
TOPICS, by N. Marcuvitz. Final rept. on Contract
AF 19(604)4143. 1 June 60. 94p. 13 refs. PIBMRI-
806-60; AFCRC TR-60-161.
Order from LC ml$5. 40, ph$15. 30 PB 152 365
Sections dealing specifically with anisotropic discon-
tinuities, statistical investigations of plasmas, plasma
diagnostics, diffraction, bunching of charged jsarticles.
a novel ion pump, and thin films are Included. Prog-
ress in related research projects is Indicated. (Author)
Microwave Research Inst. , Polytechnic Ii\st. of
Brooklyn. N. Y.
A TRANSISTORIZED NEGATIVE FEEDBACK HIGH-
Q FILTER, by James M. Brown. Rept. on Contract
AF 30(602)1648. 13 Jan 59. 47p. 6 refs. Rept. R-664-
58; PIB-592; RADC-TN-59-37; AD-210 116.
Order from LC mi$3. 30, ph$7. 80 PB 148 984
The purpose of this project was to develop a filter
with a center frequency of 100 kcps and a pass -band of
30 cps (corresponding to a Q of 3300). It was decided
that the most desirable filter would be a circuit utiliz-
ing a transistor current amplifier and a bridged-tee
network (a ^and-stop network) in a negative feedback
arrangement. The analysis of the filter was based
primarily on the use of appropriate transistor incre-
mental models, signal flow graphs and root locus
techniques.
Moore School of Electrical Engineering. U. of
Pennsylvania. Riiladelphia.
DIAL TELEPHONE SWITCHING aRCUITS Quarterly
progress rept. no. 1, 1 July- 30 Sep 54, on Contract
DA 36-039- 8C-64445. 30 Sep 54, 76p. 23 refs.
Research dlv. rept. no. 55-02; AD-54 515.
Order ffomLC mi$4. 50. ph$12. 30 PB 153 236
This report released for sale to the public 9 Dec 61.
The object of this program is to formulate the theoret-
ical and technical background information which can
serve as a basis for the development of a dial telephone
167
central off ice us ingjirans istor- like devices to the maxi-
mum practical ext^t and utilizing the inherent charac-
teristics at such devices in the most advantageous
nianner possible.
:i.
Motorola, Inc. , liverside, Calif.'
A LOGARITHMIC fULSE AMPLIFIER, by William J.
Nolan. Final rept.lpt. 2 on Contraa [AF] 19(604)2213
June 59. 57p. RepiL no. RLF-3828-4: AFCRC TR-
59-256; AD-217 61S.
Order from LC miia. 60. ph$9. 30 PB 152 385
This report released for sale to the public 25 Nov 60.
To facilitate measifrement at pulae amplitudes cover-
ing a large dynamic range, a logarithmic amplifier
has been designed ^ith the following significant speci-
fications: Rise tim0: less than 1 microsecond. Maxi-
mum pulse duratior
polarity: negative
100 microseconds, Input pulse
!)ynamic range: over 3 decades (3
mv to 3 v). Accura^: bener than 3% at maximum
output signal.
National Bureau oi Standards, Boulder, Colo.
OBUQUE INCIDENCE RECEIVING ANTENNA ARRAY
FOR A RELATIVE IONOSPHERIC OPACITY METER,
by A. C. Wilson. Hav bO, 17p. 2ref8. Technical note
no. 78.
Order from OTS $0 50 PB 161 579
Experimental measyrements incidental to the design of
an antenna for a relative ionospheric opacity meter
(RIO Meter) are described. The frequency of operation
is 50 Mc. The antenna requirements are that the main
lobe of the antenna Is directed at 23*^ above the horizon,
the half-power bear»-width in the vertical plane does
not exceed 10°, tiie minimum front-io-back ratio is at
least 13 decibels, atid the side- lobe levels are at least
10 decibels below the maximum response in bach the E-
and H-planes. Sinc4 the antenna is for use in Alaska,
it is to be of simple design and physically able to with-
stand any anticipated wind and ice loads. The final
antenna design is ar| array of three stacked horizontal
dipoles with two optimally spaced refleaors behind
each dipole to obtai^ the required directivity. The
narrow main lobe o^ the antenna directed at an angle of
23*^ above the horizon is obtained by properly spaced
and phased dipoles above the ground. The half- power
beamwldth in the vertical plana is computed to be
7-1/4°. The front -ti)- back rado ovei'the rear 180°
seaor is not less thbn 20 decibels, and the half- power
beamwldth in the E-^lane is 74°. Two complete re-
ceiving antenna arrays were constructed, adjusted, and
tested. These amentias were installed in Alaska where
they are now in use by an auroral transmission loss
project. (Author)
[Naval Training Device Center] Port Washington.
N. Y
DESIGN SUGC^STIC^NS FOR TRAINING EQUlPMEhn*.
NAVEXOS P-1466.
Order from LC mi$t40, ph$3. 30 PB 153 007
This report released for sale to the public 29 Nov 60.
This publication has been prepared to provide a refer-
ence of human engineering suggestions and references,
with other mechanical and elearical design factors,
for consideration in the development or modification of
training equipment. The suggestions are derived from
extensive designing experiences of both industry and
Government. The proper application of these sugges-
tions to the design of training equipments by contrac-
tors will insure a high degree of reliability and ease
of maintenance.
Office of Technical Services, Dept. of Commerce,
Washington, D. C.
THERMlC»slICS AND CATHODES Aug 60, lip.
157 refs. OTS Selective Bibliography SB-431.
Order from OTS $0. 10 OTS S8-431
A bibliography of reports listed in the two OTS monthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography covers
reports added to the OTS collection during the period
1945 to September 1960.
Office of Technical Services. Dept. of Commerce.
Washington. D. C
THERMISTORS AND RESISTORS. Aug 60. lOp.
1 18 refs. OTTS Selective Bibliography SB -429.
Order from OTS %0. 10 OTS SB-429
A bibliography of repons listed in the two OTS monthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography includes
reports added to the OTS collection during the period
1950 to September I960.
Office of Technical Services, Dept. of Commerce,
Washington, D. C.
THERMOELECTRICITY. Sep 60, lOp. 117 refs. OTS
Selective Bibliography SB-432.
Order from OTS $0. 10 OTS SB-432
A bibliography of reports listed in the two OTS monthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography in-
cludes PB reports, AEC reports, and translations on
thermoelectricity added to the OTS collection during
the period 1945 to October 1960.
Office of Technical Services. Dept. of Commerce.
Washington. D. C.
THERMOPILES AND THERMOCOUPLES. Aug 60. 7p.
93 refs. OTS Selective Bibliography S8-430.
Order from OTS $0. 10 OTS SB -430
A bibliography of reports listed in the two OTS monthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography includes
reports added to the OTS collection during the period
1950 to September 1960.
•>*.
166
•w
V
once at Technical Services, Dept. of Conunerce,
Washington, D. C.
TRANSISTORS (SUPPLEMENT TO CTR-310). Aug 60.
I3p. 201 refs. OTS Seleaive, Bibliography SB-433.
Order from OTS $0. 10 ^ OTS SB-433
A bibliography of reports listed in the two OTS monthly
abltraa jour nils: U.S. Government Research Reports
■ad Technical Translations. Reports included in this
bibliography were added to the OHTS collection during
the period June 1959 to September I960.
Pacific Semiconductors, Inc. , Culver City, Calif.
INTRINSIC- BARRIER TRANSISTOR TECHNIQUES
(SILICON), by K. K. Kanazdwa, R. C. Neville, and
W. E. Roach. Quarterly rqx:^ na 9. 15 July -
15 Oct 59. on Contract DA 36-039- sc- 74887. [1959]
32p. 4 refs. PSI rept. no. 3060:15-24-Q; AD-236 219.
Order from LC mi$3. 00. ph$6. 30 PB 152 559
I
VHP transistor work was directed toward a change-
over to photo- resist processing techniques. This work
la not yet complete enough to evaluate objectively and
the body of this repon is devoted to other work con-
cerned with VHP transistor development as follows:
(1) diffusion techniques altered to produce one micron
emitter and base layers are described. (2) electrical
measurement data for small- signal VHF parameters
Is presented. (3) lumped constant tranaistor oscilla-
tors suitable for the 70 to 300 mcps range are de-
scribed, and (4) the yield problem of collector- base
reverse characteristic for the thin base, diffused ■
transistor Is reviewed and results presented. (Author)
(See also FB 146 791).
Physical Science Lab. , Newl Mexico Sute U. , Uni-
versity.
THE MISIGN AND PERFORMANCE OF QUADRA-
LOOP TELEMETRY AND CCWTROL ANTENNAS
FOR THE AEROBEE HI AND SPAEROBEE ROCKETS,
by Dennis G. Henry. Scientific rept. no. 3 on Contraa
AF 19(604)2188. 22 Feb 60, I59p. AFCRC TN-
60-281. I
Order from LC ml^. 50. ph$24. 30 PB 148 717
The purpose of this study wa^ to design and develop a
type of radiator which gives maximum aft radiation
coverage. Both non-flush and flush mounted quadra-
loops were tested with this objective in mind. The de-
llgn and performance of non-flush and flush mounted
quadraloops for telemetry and cotijmand control on the
Aerobee Hi and Spaerobee rockets Is presented. A de-
tailed radiation pattern study' has been made for each
type antenna on each missile named. The radiation
patterns have been measured for both linear and right
circular polarization. Photographs of the antenna
tested and the rocket nnockup plus a coordinate system
showing orientation of antenna are included in this re-
port. Details of both non-flush and flush mounted
quadraloops are shown in photographs and drawings.
(Author) j
Pickard and Bums, Inc. , Needham. Mass.
VHF SCATTER ANTENNA, by John E. Walsh, Hans E.
Bnd and others. Rept. en Contraa AF 30(602)1868.
3 Apr 60, 78p. U refs. P. t a rept. na 514; RADC-
TN-59-54; AD- 210 724. (
Order from LC mi(4- 50, ph^2. 30 PB 148 982
The principle of pattern multiplication is shown to
allow at least a 5 to 1 reduction, as compared to con-
ventional additive arrays, in the number of radiating
elements required to produce an antenna array with a
slngle-lobed radiation panem. An antenna of this type
is proposed herein which will produce a set of Inde-
l>endent slngle-lobed beams each approximately one-
half degree wide in azimuth In the band from 30 - 50 mc.
This set at beams will allow continuous monitoring at
multipath transmissions in the ionospheric scatter
mode over an appropriate angular sector correspond-
ing to the width of the scatter volume. The sector
Itself will be steerable over ♦ 45° In azimuth. Possi-
ble use of such an antenna as a diversity reception
device is discussed.
Radio Corp. of America, Lancaster. Pa.
ELECTRON TUBE MATERIALS. GASES. AND
GETTERS, by J. C. Tumbull. R. H. Collins and others.
Final rept. for 15 Oct 58-15 Jan 60 on Contract DA 36-
039 -sc -78226. 15 Feb 60. I25p. 9 refs. AD-237 090.
Order from LC mi$6. 30. ph$19. 80 PB 152 560
A study was concluded erf gas sources and getter ing
which determine the partial pressures of gases in
electron tubes. Methods were developed for determin-
ing thermal outgassii^ of tube materials. RF induc-
tion heating was used for determining gas content of
small meul samples, while oven heating Inside a fused
silica tube was used for samples which could not be
RF induaion heated or for large samples used for de-
termining slow outgassing at lower temperatures. Out-
gassing measurements, vacuum fusion analysis, chem-
ical analysis, and metal lographic examination were
made on the following tube materials: Ni, Mo, Ta, W,
Ti, cold rolled steel, Al clad steel, Ni plated steel,
gas carbonized Ni coated steel, Kovar. Cu. mica,
forsterlte. steatite, and alumina. A radiotracer
method was developed for determining the combined
evolution of CO and C02 from Ni. and for distinguish-
ing between quantities of CO and CO2 associated with
(1) C originally present in solution of Ni melt and cast
ingot; and (2) surface soil and C or C compounds left
In strip during hot and cold rolling. The study indi-
cated that dissolved C, rather than surface C. was
predominant source of C and that surface C could be
removed by heating or etching. Development of test
methods for determining the sorption characteristics
of flash getters at low pressures was described. In
applying the method to evaluate getter performance,
the presence of impurity gases which were slowly
sorted by gener seriously interfered with rate meas-
urement. These effects were partially overcome by
purification of test gas. however. Impurity gases
associated with hot glass tipolCand flashing of getter
were not eliminated. (See also PB 145 806)
Raytheon Co. . Waltham. Mass.
DEVELOPMENT OF A RUGGEDIZED X-BAND
MINIATURE MAGNETRON. QK588, by Ralph Bacon.
Pinal engineering rept. for 1 June 56-30 May 58 on
Contraa DA 36-039-sc-72373. [1958] 118p.
AD-211059.
Order from LC mlJ6.00. ph$18. 30 PB 148 276
The QK588 is a pulae-type miniature X-band magne-
tron mechanically tunable from 8900 to 9400 mega-
cycles and capable of producing a minimum peak
169
Ufa
power of 0. 9 kilowatts dt-<i)i)e microaecond pulse
duration and 0.003 niaximum duty cycle. It has the
same exterior physical dimensions as its prototype
cube, the Raytheon RIK6229. It is unaffected by moder-
ately severe constant acceleration shock and Is able
to operate continuously through vibration of at least
15 G intensity. Excdpt for a reduced input impedance,
the QKS88 is interchangeable with the RK6229.
Raytheon Co. Newtte, Mass.
SUPERREGENERAWE DETECTOR (T2x3 SUBMINI
ATURE FILAMENTTARY TRIODE) by Blakeslee D.
Wright. Final rept. |15 June 56-14 Sep 58, on Contract
DA 36-039-sc-72799.| 18 Feb 59, 78p. 1 refs.
Order from LCmi$4i 50, ph$12. 30 PB 149 716
The development beg^in with tubes similar to the proto-
type but with increased filament area to provide higher
peak current. This v^as done by using four filaments
and lengthening the structure. The Mu was adjusted to
give best results und^r required operating conditions.
A new plate was designed to reduce Cgp, but a shorter
version of the initial design meets all requirements and
presents fewer manufacturing problems. (Author)
RCA Service Co
DOME^IC AIR TRAFFIC
MUNICATION EQIJlllME>JTS
BORNE AND GROUfCD
Rept. on Contract, F^A/BRD
Order from GTS $8.
ulations defining the
borne LF, MF, HF,
( :herry Hill. N. J.
CONTROL RADIO COM-
DISTRIBUTION AIR-
EQUIPMENTS, VOLUME I.
-60. Aug 59, 731p. 4 refs.
PB 171 131
(0
Task 1, Airborne Eqiipment Distribution, contains tab-
quantity and distribution of air-
VHF, and UHF communication
equipments presently in use in the three fleets, mili-
tary, commercial, a id general aviation. Task 3,
Ground Equipment Distribution, indicates the geo-
graphic distribution, through a series of maps, of the
ground communicatiors stations presently in use for air
traffic control purposes. Each air traffic control sta-
tion displayed on the [geographic distribution maps is
entered on either en route or terminal tabulations which
define the function anjd quantity of each type of VHF
and/or UHF communication equipment at that station.
(Author) (See also PEJ 171 130)
)PB| 171 i:
, (Jherry
RCA Service Co. , (Jherry Hill, N. J.
DOMESTIC AIR TRaIfFIC CONTROL RADIO COM-
MUNICATION EQUIPMENTS. TECHNICAL CHARAC-
TERISTICS AlRBORh^ AND GROUND EQUIPMENTS,
VOLUME II. Rept. fi Contraa FAA/BRD-60. Aug 59,
41 Ip. 3 refs.
Order from 0TS$6.CD PB 171 132
Task 2, Airborne Equipment Characterinics, contains
a detailed laboratory ianalysis under Standard test con-
ditions of a represengative number of significant types
of airborne VHF and UHF radio communications equip-
ment. A realistic dettermination was made of actual
equipment operating Charaaeristics by performing field
tests and, when the rtsults were compared with labora-
tory findings, the degp-ee of degradation was deter-
mined. Task 4, Grotcid Equipment Charaaeri sties, is
a tabulation of techni<^l characteristics of the ground
radio equipment presently employed in air traffic con-
trol communications. (Author) (See also PB 171 131)
RCA Service Co. , Cherry Hill, N. J.
DOMESTIC AIR TRAFFIC CONTROL VHF RADIO
NAVIGATION EQllIPMENTS. DISTRIBUTION AND
TECHNICAL CHARACTERISTICS AIRBORNE EQUIP-
MENTS. Rept. on Contract FAA/BRD-61. Aug 59,
582p. 3 refs.
Order from OTS $7.00 PB 171 130
This part of Project DANCE (Domestic Airways Navi-
gation and Communication Evaluations) provides, on a
national scale, the air traffic control VHF radio navi-
gation equipment information required to determine the
optimum utilization of present VHF radio navigation
equipment. In addition, the information may be utilized
in the development of air traffic control radio naviga-
tion concepts, doctrine, frequency allocation proce-
dures, and in the formulation of parameters for the
proposed automatic or semi-automatic air traffic con-
trol position reporting system. Task 1, Airborne
Equipment Distribution, contains tabulations defining
the quantity and type of airborne VOR, ILS, and
75 megacycle marker equipment presently in-use in the
three fleets, military, commercial, and general avia-
tipn. Task 2, Airborne Equipment Characteristics,
contains a detailed laboratory analysis under standard
test conditions of a representative number of significant
types of airborne VOR, ILS, and 75 megacycle marker
equipment. A realistic determination was made of
..actual equipment operating characteristics by perform-
ing laboratory and field tests and, when the latter were
compared with laboratory findings, the degree of
degradation was determined. (Author)
Research Lab, of Ptiysical Electronics, Tufts U. ,
Medford, Mass.
STUDIES ON PIEZC«LECTRIC RESONATORS, by
C R. Minglns, R. W. I>erry and others. Progress
rept. no. 4, IS Jan- 15 June 55, on Contract DA 36-
039-SC-56764. 30 June 55, 38p.
Order from LC mi$3.00, ph$6.30 PB 152 803
A revised quantitative law of amplitude distribution is
proposed on the basis of measurements made with the
stationary-wave probing system. (See also
PB 138 825)
Rome Air Development Center, Griff iss AFB, N. Y.
A STATE-OF-THE-ART SURVEY OF DELAY TECH-
NIQUES, by Joseph B. Brauer and Kenneth C. Stiefvater.
Sep 60, 46p. 37 refs. RADC-TR-60-146.
Order from LC mi$3. 30, ph$7. 80 PB 152 547
This is a review of important parameters of delay de-
vices, presently used techniques, future requirements
of ground electronic systems, and potential new mech-
anisms for achieving delay, primarily in the frequency
range above 1 mc. Carrier frequency techniques em-
ploying propagation of both electromagnetic and acous-
tic waves in solid and gaseous media are reviewed.
Circulator and other techniques are discussed as well
as periodic delay and amplification structures. (Author)
Scientific Radio Products, Inc., Loveland, Colo.
DESIGN AND DEVELOPMENT OF PRECISION
FUNDAMENTAL MODE CRYSTAL UNITS, by Donald
L. Hammond. Quarterly rept. no. 3, 1 Apr-1 Nov 58,
on Contraa DA 36-039-8C-730O7. Il958l 49p. 3 refs.
Order from LC ml$3.30, ph$7.80 h >- PB 149 715
170
Aging data on 2.0 Mc crystal units is (n-esented. The
superior performance of third overtone crystal units
for precision resonators is shown in terms of tem-
perature coefficient of frequency, coupled modes, and
Q or quality factor at 11.5 and 20. 0 Mc. Present
ttatus of the preparation of crystal units is discussed.
(See also PB 140 648)
Short Bros, and Ha r land, Ltd. (Gl Brit. )
METAL FILM POTENTIOMETERS, by J. Potts,
S. McC Noble, and Maureen Bingham. Final technical
rept. for Nov 57- Nov 59 on Contract DA 91-508- EUC-
26a (I960] 74p. 83 refs. Technical note no. RD. 209;
AD- 234 399.
Order from LC mlK 50. ph$12. 30 PB 149 660
The production of potentiometers in which the resist-
ance element is a thin meul (film on an insulating sub-
strate is described. Vacuum evaporation was selected
aa the most suitable process for the task in hand.
After a consideration of various substrates and metals,
borosilicate glass andNichrome seemed to be a suit-
able combination. Towards the end of the contract
period samples of sintered aluminum oxide substrates
became available and these proved superior in many
ways. Some experimental pdkentiometers were made.
These meet the specification except for tenqwrature
coefficient and wear resistances.
Stelma, Inc., Stamford, Conn.
TRANSISTORIZED TELEGRAPH-TEl£PHONE
TERMINAL AN/TCC-29, by.H. Levick and S. Feld-
man. Final engineering repij for 17 June 55-30 Nov 58
on Contraa DA 36-039- 8C-64741. [19581 I26p. 7 refs;
AD-210 847.
Order from LC mi$6. 30, phjil9. 80 PB 152 513
The object was to develop service test models of
small light-weight transistorized TCC-14 equipment,
designated as AN/TCC-29, suitable for use in forward
area combat applications. Tfie design of the service
test models was such that automation techniques of
construction may be readily Adapted in further pro-
ductiOQ models, i
Systems Research Field L«p. , Johns Hopkins U. .
Jamestown, R. I. ^. ]
MOUNTING ANGLE OF 'A VJ REMOTE RADAR IN-
DICATOR AND ITS EFFECT ON OPERATOR PER-
FORMANCE, by M. Leyzore|c. Rept. on Contract
N5ori-166(011 Feb 48, 14p. 3 refs. Technical rept.
NAVTRADEVCEN 166-1-41. j
Order from LC ml$2. 40, ph$3. 30 PB 153 006
This report released for sale? to the public 14 Dec 60.
A VJ remote radar indicator jwas tnounted at seven
angles (scope -face with respect to the floor 0^, 15°,
30P, 45°, 60°, 75°, 90^ and teats were made to dis-
cover whether there is an opijimum mounting angle for
operator performance. The results of the experiment
•how that the angle at which $ VJ is mounted has no
significant effect on an 6perafor"s speed and/or accu-
racy in target indication. A questionnaire was given
to the group of subject -operators used in the experi-
ment to'determine which mounting an(tle they pre-
ferred. An analysis of these results gave the follow-
ing rank order (from most to least preferred): 15°,
45°, 30°, 60°, 0°, 75°, 90°. The 0° position is the
conventional mounting angle. (Author)
Western Developnvent Labs. , Philco Corp. , Palo
Alto, Calif.
VHF DIRECTION FINDER. Final engineering rept.
on Contract AF 04(647)97. 15 July 59. 78p. 7 refs.
WDL -Technical rept. 1164.
Order from LC mi$4. 50, ph$l2. 30 PB 153 256
Thl« report released for sale to the public 16 Dec 6(X
The VHF DF indicator maintained very good balance
throughout the temperature range. No measureable
phase shift was observed. The rather strange deflec-
tion observed on the internal meter at 40°F during the
first run remains unexplained. No such deflection was
observed on the external meter. At this temperature
level there is a rather high degree of humidity due to
condensation. A rerun was performed through the
40PF level and no deflection occurred. The indicator
was checked after termination of the temperature test
and normal functioning was observed. (Author)
Western Electric Co. [Winston Salem, N. C.)
INDUSTRIAL PREPAREDNESS STUDY LACC^UER
FILM CAPACITORS, by H. E. Uoyd. Quarterly
progress rept. no. 5, 25 Feb- 25 May 60, on Contract
DA 36-039-8C-81268. [1960] 31p. AD- 239 128.
Order from LC mi$3.00, ph$6.30 PB 153 380
This report released for sale to the public 16 Dec 60.
The installation of facilities and special tooling has
neared completion and prove- in of individual units has
progressed to an advanced suge. Effort has been
directed in the areas of mixing, lacquering, drying,
metalizing, slitting, stripping and winding. Lacquer
film material is now available for process studies of
all operations. Lots of material are scheduled to be
processed through the manufacturing and testing stages
at regular intervals during the next quarter. These
shop runs will provide control data and the required
samples. The first units will be 1 uf value with other
sizes to follow. (Author)
Westinghouse Electric Corp. , Baltimore, Md.
DEVELOPMENT OF HYPALON COATED REFLEC-
TIVE FABRICS FOR PARABALLOON ANTENNAS, by
A. T. Hawthorn. C. N. Gosnell and A. S. Hovanec.
Technical rept. on Contract AF 30(602)1939.
30 June 60, 75p. RADC-TR-60-161.
Order from LC nruM- 50, ph$12. 30 PB 152 219
An extensive engineering study and investigation of
high strength, lightweight, reflective fabric suitable
for application to the fabrication of large, precisely
contoured Paraballoon antennas has been brought
successfully to completion. The program has produced
a successful reflective Hypalon coated glass fabric, a
high strength glass fabric, and an extensible, conduc-
tive, Hypalon cociting. The specified service and de-
tailed requirements have been met with certain excep-
tions which are detailed in the body of the report. In
171
addition, the resulti of preliminary investigations Into
many diversified fillers and unsuccessful coatings and
fabrics produced during the program are discussed in
detail. (Author)
Westlnghouse Eleciric Corp. fBaltlmore, Md. ]
EFFECTS OF COMPONENT TOLERANCES ON CAS-
CADED DISTORTION FILTERS Rept. on Contcact
AF 30(602)1948. 15 Dec 58. 23p. 2 refs. RADC
TN- 59-46; AD-2I3 895.
Order from LC mi^. 70, ph|4. 80 PB 148 283
I
A general equation ii derived for the transfer function
of a network containing cascaded identical four-terminal
networks with tolerance effects. The result is the theo-
retical transfer function multiplied by a function whose
parameters are dcte(rmlned by the tolerance values in
the network. A netvtork d cascaded lattice sections is
studied and limits afe established as to the order at
tolerances necessary to determine the error due to tol-
erances. The general equation is adapted to statistical
study at the network {and the average magnitude and
phase functions are derived for a discrete distribution
of tolerances. Due tb tolerances, interesting design
criterion, which are tot generally considered', are
established.
Westlnghouse Research Labs. , Pittsburgh, Pa.
A 100-db MICROWaN'E SEMICONDUCTOR SWITCH,
by D. W. Feldman ajid B. R. McAvoy. Rept on Contract
AF 19(604)5589. 24 ^ug 60, I7p. 7 refs. Research rept
403FD449-R7; AFCRL TN-60-960.
Order from LC nu$2| 40, ph$3. 30 PB 152 348
A dual-diode microwBve switch providing in excess of
100 db switched attenuation with low insertion loss is
described. Switchlna time of the device, limited by the
diodes, is 3 x 10"^ sec. Application of the switch in a
9000 Mc superheterodyne magnetic resonance 8p>ectrom
eter as a mixer crystal protector and as a microwave
signal blanket is described. (Author)
Ordnance, Miuiles, and Satellite Vehicles
Aeronautical Acces^ies Lab. , Wright Air Develop-
ment Div., Wright-patterson AFB, Ohio.
SIMULATED COMBINED VIBRATION, SUSTAINED
ACCELERATION AND EXTREME TEMPERATURE
ENVIRONMENTS, by Neal Granick and E. A. ToUe.
Feb 60, 17p. WADC Technical note 59-351;
AD- 236 057. I
Order from OTS $0.5(0 PB 171 134
I
A simulatoir believed to be the first of its kind to pro-
duce simultaneous steady acceleration, vibratory ac-
celeratio.n, and extreme temperature is described. It
comprises a 450- pound- force electro-dynamic vibra-
tor and temperature t}ox installed on a large-mass
centrifuge. The comtiination of environments produced
by this simulator maHes possible more realistic test-
ing at certain ballistic missile components than other-
wise would be possible. Design and performance
characteristics are presented, and component testing
results are disciissedf (Author)
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
TRACKING AND DISPLAY OF EARTH SATELLITES,
by Frederick F. Slack and Allen A. Sandberg. Dec 59
25p. AFCRC-TR-59-370; AD- 234 552.
Order from LC ml$2.70, ph$4.80 PB 148 706
In a new method of displaying the predicted paths and
real-time positions of artificial earth satellites,
cathode-ray tubes are used with two types of map over-
lays; orthographic projeaion and Mercator projection.
Functions to match these projections are generated
electronically. Auxiliary satellite information is cata-
loged and made available through "light gun" interroga-
tion of the satellites displayed on the CRT. The display
and orbit simulator can be used as an integral part of a
live tracking system. A mathematical derivation of the
subsatellite path on the orthographic projection is
given. (Author)
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
A YAGI-ADCOCK SYSTEM FOR SATELLITE-
TRACKING, by H. W. Ehrenspeck and W. J. Kearns.
Dec 59, 25p. 7 refs. APCRC-TR-59-374; AD-235 833.
Order from LC ml$2. 7a ph$4. 80 PB 149 058
Substitution of high -gain Yagl antennas for the dlpoles
usually in the Adcock direction -finding system pro-
vides much higher accuracy in satellite -tracking.
Data obtained with the Yagl -Adcock system is less
subject to the deleterious effects of fading, modulation
of the signal, or tumbling of the satellite. The result-
ing advantages of this system over more complicated
ones such as those based on doppler shift techniques
and the use of interferometersarean increased signal-
to-noise ratio and multiple angular bearings.
[Army Signal Research and Development Lab. ]
Fort Monmouth, N.J.
EFFECT OF RADIO WAVES ON ELECTRICAL
BLASTING, by Theodore J. Sueta, Frank J. Trlolo.
and Helmut Brueckmann. Interim rept. Sep 52. 2^p.
3 refs. Rept. no. M-1466.
Order from LC ml$2. 70. ph(4. 80 PB 152 991
This report released for sale to the pubUc 29 Nov 60.
Measul'ed impedance values of sample electrical
blasting caps proved to be small enough to be neg-
lected in comparison to other factors. A Transformer
Coupled RF Current Indicator was designed to meas-
ure induced RF current in typical blasting circuits.
Two resonant frequencies of a typical blasting circuit
were found and the azimuth of largest pickup obtained.
Measurements of the induced current In the circuit
made along this azimuth together with certain calcula-
tions gave an indication of the hazard involved. A
graph of the antenna input power require^to induce
2S0 milliamperes of RF current in the typical blasting
circuit as a function of the distance was obtained, thus
permitting evaluation of the hazard, for any given
transmitter power. (Author)
172
•1
Arnold Engineering Development Center [Tullahoma,
Tenn.]
PBRFORMANCB OF A 40- mm COMBUSTION- HEATED
UGHT GAS GUN LAUNCHER, by M. E. Lord
(ARD, Inc.). Rept. on ARO, Inc. Contract
AF 40(600)800 ^A 11(60-110». Oct 60, 23p. 6 refs.
ABDCTN-60-176. j
Older from LC ml|2.70. ph|4.80 PB 152 554
Calculation methods and exptjrimental results are pre-
lemed for the performance of a 40- mm light gas model
launcher using a mixture of helium, hydrogen, and oxy-
gen. The effect of charing |)ressure on peak pressure
in the chamber It given and dompared to closed cham-
ber combustion. Heat losses from the chamber were
measured during cooling in the closed chamber firings
The effects of incomplete combustion were estimated.
Performance of the launcher is summarized as muzzle
felocity as a function of maximum chamber pressure
for various proiectile weiRhts . The velocity of a
40-gram (a cylindrical slug of minimum practical
weight) projectile would be 14,000 ft/sec at the maxi-
najm chamber design pressure of 60,000 |»i. (Autlior)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md. V
WIND TUNNEL TESTING FAaLITIES AT THE
BALUSTIC RESEARCH LABORATORIES, by J. C.
McMullen. July 60, 4 1 p. 4 rqfs. Memo. repi.
DO. 1292. I
Orter from LCml$3.30, ph$7.80 PB 152 435
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright- Patterson AFB, Ohio.
AUTOMATED MAINTENANCE: THEORY, PRACTICE.
AND IMPLICATIONS FOR TRAINING, by Paul E.
Pranks and Clarence W. Furnish. Rept. on Human
Faaors in the Design of Training Equipment. Aug 60.
28p. 23 refs. WADD Technical rept. 60-412.
Order from OTS $0. 75 PB 171 137
Increasing complexity of electronic equipment, shorter
reaction times and Increased accuracy of weapon ays-
lema, relative neglect of design for maintainability,
and unimproved quality of maintenance have resulted
in the development of Automatic Check-Out Equipment
(ACOE) to take over the most difficult tasks of mainte-
■ance. The need for ACOE, growth of the concept,
factors affecting a workable concept, and character-
Istlca of equipment test methods affecting utilization of
ACOE are discussed. Functions of ACOE units are pre-
sented as paralleling basic maintenance activities. A
typical ACOE approach, present sutus of the concept
ttxl its impact on other areas are reviewed. The ef-
fecu on personnel requirementa, motivation, logistics,
cost, accuracy, and training are estimated and a pro-
posed traiiung program is summarized. (Author)
Pekman Research Labs. , Picatinny Arsenal.
Dover, N. J.
INFRARED METHOD FOR DETERMINING SMALL
AMOUNTS OF DIPENTAERYTHRITOL HEXANI-
TRATE IN PETNr by Walter 1^. Fredericks and Frank
frtstera. Apr 59, 5p. Technical note no. 30;
AD- 215 960. !
Order from LCiiil$l. 80, pb$l;.aO PB 149 066
A simple and rapid method using infrared spectro-
photometry was developed ftar the determination of
small amounts of dipentaerythritol hexanitrate
(W^HN) in pentaerythritol tetranitrate (PETN). The ■
developed method is applicable to the determination of
as low as a few tenths of one percent as well as higher
percentages of DPEHN in PETN with a precision of
about 0.1%.
Peltman Research Labs. , Picatinny Arsenal. Dover.
N J.
THERMAL PARAMETERS ASSOCIATED WITH THE
IGNinCW OF THE MAGNESIUM -SODIUM NITRATE
SYSTEM, by Martin Gilford. Saul Gordon, and Garry
Weingarten. Aug 58, 31p. 14 refs. Technical notes
no. 27; AD-212 848.
Older from LC mi$a 00. ph)6. 30 FB 149 670
Variables associated with the apparatus, technique and
nature of the sample have been examined and the re-
liability of the procedures currently in use has been
established.
Frankford Arsenal, Philadelphia, Pa.
FIRE CC»4TROL MATERIALS ENGINEERIhJG. BEAR-
INGS, CAP AND SOCKET DWG C7674304 TYPE
EVALUAT1(»I OF NYU»i BEARINGS, by Jay W.
Lord, Jr. 3 Apr 53, 16p. 8 refs. Ibstrept. T53-14-1;
AD- 7994.
Order from LC mi$2. 40. pfa$3. 30 PB 153 014
This report released for sale to the public 5 Dec 60.
The mechanical operating characteristics of nylon ball
cap and socket bearings were compared with those of
the linen-filled phenolic insert with a suinless steel
ring reuiner under varying climatic conditions and
stress. Three ball cap and socket bearings of different
sizes were fabricated; one for a lS/16-in. -dlam ball
from FM 10001 nylon and one each for a 5/8- and 3/8-
In. -dlam ball from PM 3001 nylon. A phenolic insert
bearing for a 15/16-in. -diam ball was used as a refer-
ence standard. The bearings with their respective ball
and worm shafts were mounted to simulate the action
they would i-eceive when properly assembled in in-
struments. The phenolic insert bearii^ was suscepti-
ble to high humidity conditions; at 95% RH the ton]ue
increased from 1. 9 to 168, 32, and 50 OB-in. at 140^,
-40P and -65°F, respectively, when tested before dry-
ing. Low temperature had little effect on the dry bear-
ing. The FM 10001 bearlqg was susceptible to low
temperature, the torque increasing from 1. 4 oz in. at
room temperature to 140 and 170 oz-in. at -40OF and
260 to 352 oz-in. at -6SPF. Tbe bearing was unaffected
by shock, vibration, wear, and exposure to high hu-
midity, elevated and low temperature, and shock and
vibration. PM 3001 nylon appears to be satisfactory
for use in ball cap and socket bearings for FOG in-
struments up to and including sizes for a 5/8- in. -diam
ball. It appears superior or equal to the phenolic
insert bearings under conditions of high humidity,
high and low temperature, shock, vihratlan. and
173
James Pastoriza Associates, Inc., Boston, Mass.
SATELLITE ORBIT. SIMULATOR. Final rept. on Con -
traa AF 19(6O4)6l06. Ai^ 60, 56p. AFCRL TR-
60-184 1
Order from LC miS^. 60. pti$9. 30 PB 152 429
A study design and itnplementation d an equipment for
Satellite Simulation nas been accomplished. The equip-
ment consists of a l()cal storage ol satellite information
and arithmetic and ctisplay circuits, to display the track
and present positiorL The unit will receive information
on current satellite positions from punched tape, mag-
netic tape, or direct computer input. It will be capable
of displaying up to six satellites simultaneously. The
displaywill have a Mercator projection al the earth.
Presem^osition of ^ch satellite will be indicated by an
intensified position on the track trace. Any satellite
track may be interrogated by a light gun and informa-
tion withdrawn on any auxiliary read-out. The system
design has been conipleted. The physical and electrical
design of the components have been completed with the
exception o( minor modifications. (Author)
r
• Lincoln Lab. , Ma^. Inst, of Tech. , Lexingtoiu
AUTOMATIC RANGE TRACKING SYSTEM FOR THE
REENTRY PHYSICS|PROGRAM, by John E. Gillis.
Rept. on Contract AF 19(604)4559. 17 Feb 60, 39p.
21 G-0005. '
Order from LC mi$t. 00. ph|6. 30 PB 150 797
I
A brief description ^ the operation of the SCR -584
automatic range tracking system is given, after which
the modification necessary to provide tracking capa-
bility for the reentry program are described. The re-
sults of a preliminary evaluation of the system are
then discussed, andjthe final section presents the theor>
of operation of the circuits and the schematic diagrams.
(Author)
Lincoln Lab. , Mas^s. Inst, of Tech. , Lexington.
•PROCEDURES FOR OPERATING PARAMETRIC AM-
PLIFIER IN REENTRY PHYSICS PROGRAM, by
F. R. Hutchinson, tept. on Contract AF 19(604)4559.
28 July 60. 18p. 3 rifs. 21G-0016.
Order from LC min. 40. ph^. 30 FB 152 063
The S-band prinury tracking radar designed for use
with the Wallops Isl4nd reentry physics program em-
ploys a low- noise figure RF amplifier to enhance the
received signal. A description of the amplifier along
with operation and ntaintenance instructions are given
in this report. (Autl^r)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
REAL TIME CLOCK AND TELETYPE DATA TRANS-
MITTER FOR REENTRY PHYSICS PROGRAM, by
R. M. Martinson. Riept. on Contract AF 19(604)4559.
5 July 60. 68p. 21 G-0009.
Order from LC mi$a 90. ph$10. 80 PB 150 798
Equipment has been installed at the Arbuckle Neck Site
for transmission al radar data via conventional teletype
lines. Messages consisting of time in decimal form to
milliseconds and elevation, azimuth, and range in five
octal character formi each are sent at a rate of approx-
imately ten message^ per minute. (Author)
Lockheed Aircraft Corp. , Sunnyvale. Calif.
ORBIT DECAY AND PREDICTION OF THE MOTION
OF ARTIFICIAL SATELLITES, by Hernun F.
Michielsen. 19 Dec 58, 90p. 3 refs. LMSD-48360.
Order from LCmlV4.80, ph$13.80 PB 148 697
The rate d decay ci elliptic satellite orbits, due to
atmospheric drag, is investigated through variation ol
parameters and through use of an atmospheric model
involving a power function between density and altitude.
This model is shown to fit actual conditions better than
an exponential function. The effects of the equatorial
belt and the rotation ol the Earth are investigated. The
conclusion is reached that through these anomabes
atmospheric drag substantially affects the orbit ele-
ments, especially those defining the orbit plane.
Office of Defense Research and Engineering.
Washington. D. C
TECHNICAL RESOURCES DIRECTORY: MISSILE
GROUND SUPPORT EQUIPMENT NO. 3. 1 Nov 6a
22p.
Order from OTS $0. 7^ PB 161 535(Rev. 1)
Through its extensive research and engineering pro-
grams, the Department of Defense is developing ma.-
terial and equipment designed to meet present and fu-
ture military requirements. The diverse tasks em-
braced in these programs range throughout the broad
scope of miliury activities. This directory of mili-
tary technical resources is intended to encourage com-
munication in the Miliury Departments and in industr>
in the area of ground support equipment for missile
systems. (Supersedes issue no. 2, 1 May 60.
PB 161 535)
N
Remington Arms Co. , Inc. . Bridgeport. Conn.
DEVELOPMENT AND FABRICATION OF PERCUSSION
PRIMER FOR BAG LOADED WEAPONS, by
E. M. Yacka Monthly progress rept. no. 3 for July 60,
Contract DA 19-020-ORD-5200. 10 Aug 60. 7p.
Order from LC mi$l. 80. ph$l. 80 PB 152 259
Work is now being csrried on simultaneously on three
primer designs: (1) Picatinny design utilizing screw
machine parts. (2) Remington first altenute simulat-
ing the Picatinny design, but utilizing small arms am-
munition manufacturing methods to replace costly
machined parts. (3) Remington second alternate uti-
lizing a single drawn case with an external percussion.
Remington-developed, wrap-around primer which pre-
vents primer leakage. This design provides a vast
simplification in nuuiufacture and reduction in cost.
(See also PB 149 831).
Republic Aviation (>>rp. . Parmingdale. N. Y.
PARAMETER DETERMINATION FOR SATELLITE
GUIDANCE, by S. Abrahams, S. R. Cohen and others.
Rept. on Contract AF 33(616)6547. Oct 60. 31 3p.
45 refs. ARL Technical rept. 60-300.
Order fromLCmi$ll. 10. ph$58. 60 PB 150 321
The purpose of this investigation was to determine the
requirements for performing arbitrary geocentric sat-
ellite orbit transfers in terms of the specification of
the following: (1) the significant guidance system pa-
rameters. (2) the effects of subsystem errors, and
174
(3) those subsystems which are critical. The study, is
dtvided into the following three basic parts: (1) trans-
fer analysis. (2) perturbation study, atid error analy-
■iB. The study emphasizes transfers or ori>it modifi-
cations which are arbitrary in nature. The role of sys-
tem errors is analyzed and criteria of acceptability
for the final orbit are adopted. A survey of likely sat-
ellite guidance systems and components is made and
anticipated sensing errors are quoted. The complete
analytical expressions for the errors in the transfer
orbit as functions of the transfer parameters are
developed. (Author)
Systems Dynamic Analysis Div. . Wright Air Devel-
opment Div , Wright -Patterson APE, Ohio
GENERAL DESIGN CRITERIA FOR AN OPTIMUM
FAMILY OF FIN-STABILIZEp SOUNDING VB-
HICLES, by Jack L. R. Cudaback and Rinaldo F.
Vachino. June 60. 44p. 8 refs. WADD Technical note
60-71. I
Onter from OTS $1.25 ' PB 171 180
The greatest portion of the ARDC requirements for
■pace probes may be satisfied with a family of cheap,
fin-stabilized, unguided vehicles. This family of ve-
tiicles IS composed of six solid -propellant motors and
a minimum of sundard accessories, such as thrust
transfer cones, fins, insulation, sequencing mecha -
■iams. etc. The proposed gr6up of 6 motors and their
accessories may be assembled into 21 vehicles with
different payload — altitude capabilities. These motors
and accessories involve some development cost but
offer a number of long-range benefits not present in
the variety of probing vehiclep that are presently being
used for space probes. These benefits result from the
versatile vehicle combination^, the simple and effi-
cient vehicles, and the reduced handling and storage
required. (Author) 1
Universal Match Corp. , St. Louis. Mo.
RESEARCH OH THE FEASIBILITY OF THE LINI>
BERG GYROSCOPE PRINCIPLE, by John P. CapeUupo,
Allan W. Lindberg. and Raymond H. Marcus. Rept.
for 15 Feb- 15 Nov 59 on Contract AF 33(616)6201.
Ai«60. 122p. 26 refs. WADQ Technical rept. 60-174.
Order from OTS $2.75 j PB 171 157
A preliminary research study was conducted to verify
the feasibility of a two-rotor gyroscope using a spheri-
cal gas bearing support. Work was limited to research
CO two fundamental components: a spherical gas bear-
ing and an electro- optical error signal generator. Fol-
kwing a theoretical study models of each were con-
•truaed and tested to establish their operating charac-
teristics under conditions simulating those of the pro-
posed gyro. A comparative study was made to show
the effect of rotor configuration on gyro performance.
The unique design features were shown to be fundamen-
tally promising. Extrapolation of results Indicated the
feasibility of further refinements to improve gyro
performance. (Author)
Utah U. , Salt Lake City.
ANALYSIS AND DEVELOPMENT OF A UGHT-GAS
am FOR ACCELERATING PELLETS TO HYPER -
SOtaC VELOCITIES, by K. E. Boyd, R. W. Grow and
others. Technical rept. no. OSR - 1 7 on Contract
AF 49(638)462. 15 Oct 59. 88p. 9 refs. AFOSR-TN-
60-81; AD- 235 436.
Order from LC nU$4.80, ph$13.80 PB 149 071
A light-gas gun employing hydrogen as a driving gas
and using a piston-type compression cycle has been
developed and fired in two different configurations
under a variety of firing conditions. Data are pre-
sented and analyzed of a gun having a compression
tube length of 92 inches and a bore of 2. 38 inches and
designed to launch pellets either parallel to the longi-
tudinal axis of the gun or perpendicular to the longi-
tudinal axis.
Utah U. , Salt Lake City.
HYPERVELOCITY IMPACT SPRAY PARTICLES, by
W. H. Clark, R. R. Kadesch, and R. W. Grow. Tech-
nical rept. no. OSR- 18 on Contract AF 49(638)462.
1 May 60, 95p. 17 refs. AFOSR TN-60-990.
Order from LC ml$5.40, ph$15.30 PB 152 380
Several investigators have noticed that a spray of
small fast particles is ejected from a fast meul-to-
metal impact. The velocity of the fastest spray parti-
cles previously observed, measured relative to the
more massive body involved in the impact, was twice
the impacting velocity. This study has shown that
under certain conditions very much faster spray parti-
cles appear. When a 3/16-inch diameter carbon steel
sphere, with a velocity of 2 km/sec, impacted on a
massive steel target in air at 8 cm mercury pressure,
spray particles of about 0. 5 micron diameter left the
impact at velocities up to 15 km/sec. The velocity
was measured by a time of flight technique. The effect
of varying pellet and target material and the atmos-
phere on the characteristics of the sorav t»rticle was
investigated. It was found that all three variables have
strong and complicated effects. A partial theory of
the acceleration of spray particles has been developed.
Tests made on impacts of special geometry confirmed
the theoretical predictions. It is hoped that these fast
spray particles will be useful as artificial meteors for
research purposes. It is demonstrated that the faster
spray particles observed are luminous due to the same
process whereby the average visual meteor leaves a
luminous trail. (Author) ,
Utah U. , Salt Lake City.
VELOCITY AND SIZE DISTRIBUTION OF IMPACT
SPRAY PARTICLES, by R. E. Blake, R. W. Grow, and
E. P. Palmer. Technical rept. no. OSR- 19 on Contract
AF 49(638)462. 20 May 60, 48p. 10 refs. AFOSR TN-
60-989; AD-245 112.
Order from LC mi$3.30. pfa$7.80 PB 152 381
Steel and pyrex spheres having a diameter of 3/16 inch
were accelerated with a 220 caliber smooth-bore gun
to a velocity of 2.0 kilometers per second. These
spheres were impacted on a target of a composition of
the same type as the sphere. The luminous spray re-
sultiitg from the impact was detected by means of
photocircuits which produced a voltage that was re-
corded by an oscilloscope camera. Maximum meas-
ured initial spray velocities for the steel to steel im-
pacts varied between 8.5 km/sec and 10.3 km/sec and
a measured average velocity betvreen two points for
glass to glass impacts was in excess of 20 km/sec.
175
The particle radius d the ateel spray was calculated
from drag dau to b* berveen 0. 18 and 1 . 02 microns.
In order to separata tbe impacciag spray particles, a
higb speed motor was used to rotate a polished alumi-
num disk at a velocity at thirty-two thousand revolu-
tions per minute. The velocity distribution of the
spray particles in tl^ steel to steel Impacts was ob-
served to iMve two discrete velocity' classes - one at
the faster velocity ctf approximately 9 km/sec and
another moving rnvdi slower in respect to tbe initial
time of impact. This aaooMl (Macrcte velocity class
was not observed in the glaaa to glass Impacts. Parti-
cles moving at thea4 discrete velocities were of ran-
dom size. The distfibution d the crater size at vari-
ous angular poeitiaqs is presented in the report .
(Author)
Sanitation and Safety Engineering
Ballistic Research Labs. , Aberdeen Proving Ground,
SHOCK PRESSURES IN TUNNELS ORIENTED FACE-
ON AND SIDE-ON tO A UJINC DURATION BLAST
WAVE, by Robert a Qart and William J. Taylor.
Jine 60. 22p. 4 refSw Memo. rept. no. 1280; DASA
1177. I
OnlerfranLCmtB.70. phK80 PB 152 256
The orientation of ^tunnel entrance with respect to the
burst point of a bont> plays a major part In determin-
ing the strength of shock propagated through the tunnel.
Data fipm tunnels oriented face-on and side-on to a
blast mve are cornered to a shock tube with an area
dwi^e at the diaphragm. The analogy permits data to
ba extrapolated to high shock strengths. (Author)
Robert A. Tafl Safitary Engineering Center,
Cincinnati, Ohio. ,
AIR POLLUTION Df HAMILT»i. OHIO, by Paul A.
KenUne. 1960, 18p, 17 refs. Technical rept. A60-8.
Order from LCmiM. 40. pb$3. 30 PB 152 064
This appraisal of air pollution was initiated to review
and evaluate the existing and potential air pollution
ilMation, and to detelop recommendations fen- the
giMmn^ al tbe local health department in meeting the
problem of air pollMtian. The study was limited to
available informatidn relative to air pollution including
activities causing pollution, evidence of pollution
levels, meteorological and topographical influences on
the dispersion of pollutants, and to other relevant
community charactori sties. Personal visits were
made to 12 industrial plants and three municipal
properties. The study area was the urbanized
Hamilton area.
L
ip Building
David Taylor Modal Basin. Washington, O. C
ON SHIP MODEL TESTING FOR THE PREDICTION
OF EXTREME CONDmCWS IN CONFUSED SEAS, by
William E. Cummin*. Aug 60. 26p. 3 refs. Rept. 1410;
AI>242 243.
Order from LC mill 70. phK 80 PB 150 391
The problem is considered in which information is
needed as to the nature of extreme conditions a ship la
likely to encounter during a definite short period of
operation in a well defined random sea. Various model
experiments are designed which are of increasing com-
plexity and validity, each being an "optimum" design
for a given degree of sophistication. The approach is
based on the statistical properties of the ship- seaway
system, and tbe resulting experiments are intended to
provide a nuximum of valid information from a small
number of runs. (Author) . . ,
Hamburg Model Basin (West Germany).
PROPELLER SECTIONS TO BE USED IN A NON-
HOMOGENEOUS WAKE, by W. E. Alef. Rept. on
[ContraaN62558-14]. June 59. 25p. 2 refs. Rept.
no. 1187; AD- 231 562.
Order from LC mi$2.70, ph$4.80 FB 148 721
Caviution erosion is often observed on the propellerp
of single screw ships caused by a variation of the
ai^e of attack in a non- homogeneous wake. In order
to avoid tbe cavitation and the accompanying erosion a
section is developed which is insensitive against a
variation of tbe angle of attack in a sense which is
explained.
FOOD, HANDLING, AND PACKAGING
EQUIPMENT
Pockogirtg
Crown Zellerbach Corp. . San Leandro. Calif.
INVESTIGATION OF THE EFFECTS OF RADIATION
ON WAXES AND WAX COATED PAPER PRODUCTS,
by J. E. Smith. Rept. no. 4 (Final) for 23 Sep 57-
31 Oct 58. [1958] 22p. QFOAF File no. S-748.
Order from LCmi$2. 70, ph$4. 80 PB 152 794
Tilis report released for sale to the pubUc 16 Dec 60.
Various waxes, wax blends and waxed P^Pc^B were
irradiated to levels of 0.05 x 10^, 0.5 x 10^, 1.0x10^
and 5.0 X 10^ reps. Decreases in waxed jjaper
strength properties resulted. Wax blends which con-
tained polyethylene and butyl rubber exhibited in-
creasfed viscosities at higher doseage levels; other
changes in unmodified waxes and wax blends were
negligible. No increasing effects due to irradiation
occurred upon storage of samples for up to six
months. (Author)
Rhinelander Paper Co. , Wis.
PAFERBOARD CONTAINERS FOR IRRADIATED
FOODS, by R. C. Craln. Rept. no. 1 (Final) 28June57
27 June 58, on Testing Irradiated Food Packaging
Papers. (19581 7p. QFCIAF File no. S-743;
AD- 219 954.
OrderfromLCml$1.80, ph$1.80 PB 152 793
This report released for sale to the pubUc 16 Dec 60.
Samples of glassine paper, nitrocellulose lacquer
coated glassine paper, waxed glassine paper and wax
176
laminated glassine paper were subjected to irradiation
from a 2 million volt electron beam generator at dos-
tge levels of 75. 000. 500. OOBkand 5. 000. 000 rad.
Bursting strength and tearing resistance of all samples
irere essentially unaffected at tbe two lower doeage
lefels. At 5 X 10^ rad, these ^operties decreased
tHgt*ly. Strength of heat seals was not changed by
irradiation. Moisture vapor permeability of lacquer
coated glassine was not changed by irractiation; that of
waxed glassine was decreased slightly; that of wax
laminated glassine was unaffeoed at lower dosages,
and increased slightly at 5 x iOP rad, probably be-
cause of visible blistering of the wax. The color of
dyed papers was adversely affected at 5 x 10" rad.
(Author)
MACHINERY, FABRICATION, AND
ACCESSORY EQUIPMENT
Brown U. , Providence, R. L
SCHEDULING PROBLEMS FOR A MULTI- COMMOD-
ITY PRODUCTION MODEL, by Harry Ughthall. jr.
Technical rept. na 2 on Contract Nonr-562(15). 1959.
3lp. 3 refs.
Order from LC ml$3. 00. ph|6. 30 PB 149 074
A mathematical model of production in which it is pos-
sible to produce simultaneously various amounts of
N different goods can be described by a set T in N-
space. called the technology set of the modeL The set
T represents those "bundles of goods" which can be
produced in one period of time. Thus, the vector x ^
(x|, X2, . . . , xi^ is in T if it is possible to produce in
one period of time x^ units of the first good. X2 units
of the second good, and so forth.
General Electric Co. . Schenectady, N. Y.
DYNAMIC STABILITY ASPECTS OF CYLINDRICAL
JOURNAL BEARINGS USING COMPRESSIBLE AND
INCOMPRESSIBLE FLUIDS, by B. Stemlicht,
H. Poritsky, and E. Arwas. Rept. on Contract Nonr-
2844(00). Dec 59, ll6p. 16 refa. AD- 230 243.
Order from LC ml$6. 00. pfa$I8. 30 PB 152 145
Solutions are given of Reynolds equation for cylindri-
cal Journal bearings in which the velocity of the jour-
nal center is considered; however, the inertia terms
•re neglected. Solutions are obtained for compressi-
ble and incompressible fluids. Analysis of the steady
■tste forces that exist in compressible fluid, exter-
nally-pressurized cylindrical journal bearings with
oae plane of feeding is also Included. From these
mlyses the gradients of the radial and ungential
forces with respect to diaplacement and velocity are
oixalned. The equations of motion for small and large
osdUation in terms of these forces and gradients are
Mt up. and stability criteria are established for small
QSdUations and also for lai^ oadllations of a mass-
Issa rotor. Sample calculations for threshold of in-
ntiility are given and. where existing experimental
dMa is available, theoretical predictions are com-
pared with results atulned in practice. (Author)
Harvard School of Public Health, Boston, Mass.
ANNUAL REPORT TO THE COMMISSION ON ACCI-
DENTAL TRAUMA OF THE ARMED FORCES EPIDE-
MIOLOGICAL BOARPjZ-by Ross A. McFarland. Rept.
for 1 Mar 58-28 Feb 59 on Human Factors in Vehicular
Design and Operation, with Special Reference to Acci-
dents, Contract DA 49-007- MD- 166. [1959] 52p. 9 refs.
AD-215 641.
Order from LC mi$3. 60. ph$9. 30 PB 153 005
This report released for sale to the public 1 Dec 60.
In this project emphasis has been placed on the role of
human cajMtbilities and limitations in the design of ve-
hicular equipment in relation to accidents. The objec-
tive has been to increase operating safetyand efficiency
through more effective integration of the driver with
his vehicle. The methods *of epidemiology have been
applied in an attempt to understand more clearly the
multiple causation of accidents.
f
Engines and Propulsion Systems
Aerojet -General Corp. , Azusa, Calif.
CHARGED COLLOID PROPULSION SYSTEM, by
R. B. Edmonson, C. B. Kretschmer and L. B. Becker.
Semiannual rept. no. 2 on Contract AF 49(638)656.
July 60, 18p. 7 refs. Aerojet rept. no. 1880; AFOSR-
TN-60-1237.
Order from LC mi$2. 40, ph$3. 30 PB 152 546
This report summarizes research on the electrostatic
spra)ring of microscopic droplets of oil. The research
is directed toward an understanding of the mechanisms,
of charge accumulation and electrostatic spraying in
high electrical fields, an understanding which is nec-
essary for subsequent adaptation of the phenomenon to
use in high -efficiency, low-thrust propulsion applica-
tions. The work has been primarily experimental and
relates to the role of unattached electrons as pustu-
lated by Schultz. In addition, a collection probe has
been designed for the measurement of the average
ratio of charge to mass. The initial results from the
use of the probe indicate that a high degree of repro-
ducibility and accuracy can be obtained in this meas-
urement. (Author) (See also PB 146 178)
General Atornic^San Diego, Calif.
AIR FORCE OFFICE OF SCIENTIFIC RESEARCH
CONTRACTORS MEETING (NO. 1] ON CHEMICAL
KINETICS OF PROPULSION HELD AT GENERAL
ATOMIC DIVISION OF GENERAL DYNAMICS CORPO-
RATION SAN DIEGO. CALIFORNIA, 6-7 SEPTEM-
BER 1960. Program and abstracts of papers. [1960]
37p. AFOSR-TN-60-I063.
Order from OTS) 1. 00 PB 171 184
Session I: Studies of Atom Concentrations in Low Tem-
perature Plasma Jet; Chemical Reactions Using Modu-
lated Free Radical Beams; Combustion Studies at Hull
University; Recombination Processes in Advanced
Propulsion Systems; Studies of Atomic Reactions. Ses-
sion 2: The Influence of Chemical Kinetics on the Com-
bustion of Liquids in £>roplet Form; Chemical Kinetics
177
at High TemperBture Produced by Shock Waves; Prop-
erties erf Air and Propellant Reactions at HighTem-
peratures and (Yessures; High Temperature Chemical
Kinetics; Sessi^ 3: Role of Reaction Kinetics in
Steady-State Lalninar Flames; Chemical Kinetics in
Flame Processes; Report from Combustion Kinetics
Project at the University at Texas; Kinetics of Radical
Fcurmation and Kecombinations at Low Temperatures;
Photolysis of Disulfides in Matrix-forming Mixtures of
Hydrocarbons at Liquid Nitrogen Temperature Aiming
at the Determination of Radical Recombination Ener-
gies; Session 4: Reactions of Energy-rich Molecules
and Molecular fragments Studied by Means of High
Energy Flash- photolysis (200,000 Joules); Photochemi-
cal Decomposition of Ozone; Kinetics d Oxidation of
Diborane and ofjSym-diethyl Diborane; Vibrational
Relaxation at a Pitot Tube; Reactions of Organometallic
Compounds; Chemical Reactions in Shock Waves; The
Reacuons of Free Radicals Containing Nitrogen.
James Forrestjal Research Center, Princeton, N. J.
SUBSTANTIATION OF NOZZLE ADMITTANCE
THEORY BY DfRECT MEASUREMENT OF THE AD-
MITTANCE PA|AMETER. by Rudolfo Monti. Repc. on
Project Squid. Contract Nonr- 1 858(25). Dec 59. 87p.
13 refs. Technical rept. PR-102-R.
Order from LCbii(4 80. ph$13. 80 PB 152 154
A direct experimental check al the theoretical formula-
tion oi the bounqary condition represented by the nozzle
admittance theoty was made. Attentior was focused
principally on tHe behavior of linear-velocity-gradient
nozzles in the presence of nearly isentropic pressure
and velocity flu<)tuations. Nozzles of different subsonic
lengths and different entrance Mach numbers were
tested on a simill^ied rocket chamber using air at dif-
ferent pressure I levels. Small pressure oscillations
were induced byia siren-type modulator. The admit-
tance p<>ra mete i^ a was obtained by direct measurement
of air velocity fluctuations (using a hot-wire anemom-
eter) and pressi^re oscillations (using a high- response
pressure transdiicer) at the entrance to the nozzle.
Excellent agreefient was found between experimental
results and theoretical predictions. The value «i of the
imaginary part »f the admittance parameter, not being
influenced by letiperature fluctuations, provided the
best agreement:, however, when measured values at the
real part "r of tfie admittance were corrected for de-
partures from tlie isentropic assumption, satisfactory
correlation was lobserved. (Author)
Solar Aircraft Co. , San Diego, Calif.
IMPROVED PAR,T LOAD GAS TURBINE SFC STUDY,
by A. Stone and H. J. Brodie. Final rept. on Contract
DA 44-177-tc-5<9. 26 A\^ 60, 296p. 9 refs. ER 989;
TREC 60-40; AD-243 403.
Order from LC mi$ll. 10, ph$45.60 PB 152 527
This repon presents the results of a comprehensive
study into methoiis for reducing the part load (cruise)
fad caammptiofi of gas turbines applied to Army heli-
capttn and VTOL/STOL aircraft, an imponam param-
eter In determining endurance, range, and logistics
aspects of these aircraft. The power ratings consid-
ered included th^se up to 2500 1^. The techniques
studied included variable geometry, special two- spool
engine, high cycle temperature engines, cycles with
heat exchanger, multifile engine systems, and the
boosted engine. The study has shown that for the in-
tended application and with the limitations of weight,
bulk, complexity and full power sfc, the two systems
with the most promise are (a) twin engine installatioo
and (b) the use of a compact lightweight heat exchanger
(recn»erator). (Author)
Space Sciences Lab. , General Electric Ca ,
Philadelphia, Pa.
PLASMA PROPULSION: PERFORMANCE OF A
T-TUBE PLASMA ACCELERATOR FIRED INTO A
VACUUM, by P. Gloersen, B. Gorowitz and others.
Rept. on Contract AF 04(647)269. Oct 60. 26p. 3 reft.
Technical Information Series R60SD454.
Order from LC mi$2. 70, ph$4 80 PB 152 622
A study of the performance of various plasma acceler-
ators operating under pressure conditions simulating
those of outer space has been continued, resulting in
additional evidence to support the contention that such
devices will find eventual application as propulsive
units for space flight. In particular, investigation ini-
tiated previously on pulsed gas entry T-tube accelera-
tors fired into t^gh vacuum have been extended to pro-
vide a more realistic picture of accelerator perform-
ance. Included in the additional techniques employed
are streak photography, calorimetry, Kerr Cell
photography, and spectroscopy. This paper is de-
voted to a discussion of both :he quantitative and
qualitative results of these studies and of their signifi-
cance in a practical evaluation of the operating char-
acteristics of a T-tube plasma motor. (Author)
MATERIALS
I
Chesapeake Instrument Corp. , Shadyside, Md.
DYNAMIC MECHANICAL PROPERTIES OF MATE-
RIALS FOR NOISE AND VIBRATION CONTROL, by
Edward J. Cook, John A. Lee and others. Rept. on
Contract Nonr-2678(00). I Jan 60, I61p. 39 refs.
CIC rept. no. 101; AD- 236 371.
Order from LCmi$7.80, ph$25.80 PB 150 392
DyiMmic mechanical properties and their relation to
wave propagation in viscoelastic media are reviewed.
Typical variations of dynamic mechanical character-
istics with frequency and temperature were studied
for amorphous and crystalline polymers. Proposed
methods for revising the Fitzgerald apparatus to make
possible direct mechanical impedance measurement*
on resilient mounts and coated panels at audiofre-
quencies are outlined and compared with present test-
ing procedures. The variations of complex shear
compliance (J* "J' - ij") and sound velocity and atten-
uation with frequency from 50 to 5000 c from 23^ to
27% were obtained for IS materials; these included •
natural rubber gum stock and a series of 6 butyl
rubber stocks used in resilient mounts. The variablei
studied were molecular weight of the butyl rubber and
the size and amount of carbon black filler. A series
of 4 polyurethanes were also studied. The dynamic
properties of the sample of greatest hardness (Shore
A 92) were different from those of the rest of the
series; sharp resonances were found at 1550, 2700,
178
and 2950 c. A saimple of polyurethane with 82% lead
powder as filler was studied; the shear sound velocity
«M decreased, and the attenuation was greatly in-
cxMsed in comparison with the unfilled stock. The
ftrittion al dynamic properties with frequency is
f^wm pronounced for the filled stock than for the
grilled. Polytetrafluorethylene (Teflon) and a copoly-
mer at hexafluoropropylene and vinyUdene fluoride
(Vlton) showed good high -temperature stability, but
Viton had a loss faaor or damping of 2 to 10 times
tiMt d Teflon.
Rock Island Arsenal Lab. . 111.
OZONE RESISTANCE OF ELASTOMERIC VULCANl-
ZATES AT ELEVATED TEMPERATURES, by
C. 0. Crozier. 14 Sep 60, I9p. 6 refs. Rept. no.
60-2712.
Order from OTS $0. 50 PB 161 969
This report covers the results of accelerated ozone ex -
posure tests of antlozonant inhibited SBR and NBR based
vulcanizated at temperatures of 100°F, 120Pf, and
158^. and at ozone concentrations of 25 pphm and
SO pphm. It was found that the efficiency of the anti-
osonants decreased sharply with an increase In tem-
perature. It was discovered that the addition of special
heat resisunt additives greatly improved the ozone re-
sistance of the antiozonant inhibited SBR and NBR based
vulcanizates at higher temperatures. (Author)
I
Ceramics and Refractories
Bell Aircraft Corp. , Buffalo, N. Y.
REFRACTORY INORGANIC MATERIALS FOR
STRUCTURAL APPLICATK)NS, by Harry A. Pearl,
John M. Nowak, and Joseph C Contl. Rept. for fxne
59- June 60 on Ceramics and Cermet Materials,
Oootract AF 33(616)5930. July 60, 95p. 12 refs. WADC
Technical rept. 59-432, Pt. IL
Oider from OTS $2. 25 PB 171 148
A process was developed for making simple and com-
plex curvature geometric shapes from honeycomb
ceramic sandwich constructions. Final fired sections
had apparent densities as low as 26 lb/ft3. A simple
mechanical method was developed for continuous fabri-
cation of ceramic corrugated ribbon or sheet for making
honeycomb cores. The core is flexible and machinable
In its preflred condition. The skins are as easy to
handle as paper. Alumina-silica paper impregnated
with an alumina -silica slurry was used as a refrac-
tory model system for developing the fabrication tech-
niques. The paper originally acts, as a carrier but be-
comes an Intergral part of the fired refractory. The
fabrication and processing methods are adaptable to
refractory materials possessing higher strength and
temperature stability. Other types o* ceramic and
meul-ceramic composites were investigated and
evaluated. (Author) (See also PB 161 737)
Carborundum Co., Niagara Falls, N. Y.
DEVELOPMENT OF NON-OXIDIC REFRACTORY
POAMS. by Ian M. Logan, Douglas C. Wise and others
Rept. for Feb 59-Feb 60 on Ceramic and Cermet
Materials, Contraa AF 33(616)6294. Apr 60, 49p.
4 refs. WADD Technical rept. 60-124; AD- 240 638.
Order from OTS J 1.25 . PB 171 178
Fundamental technology has been developed for the
preparation at rnxi-oxidic refractory foams of con-
trolled pore diameter, spacing, and continuity. Foam-
ing procedures used in making commerciaUy available
foam plastics were employed to produce the resin-type
foams which formed the basis for the final refraaory
foams. It was shown that foam structures can be
varied as to strength, density and pare size by varying
the proportions of resins and solvents used to generate
the foams. Lesser controls were also possible by
varying the temperature and pressure during the foam-
ing process. Good control and predictable results
were obtained. Foams were prepared of the following
materials; carbides of titanium, tungsten, molybde-
num, tantalum, and columbium; borides of titanium
aixl of zirconium; and silicides of tungsten and of
molybdenum. (Author)
Fuels, Lubricanfii, and H)rdraulic Fiuidr
Instituto Nacional de Tecnica Aeronautica "Esteban
Terradas" (^in).
A THEORETICAL INVESTIGATION ON THE COM-
BUSTION OF LIQUID BIPROPELLANT DROPLETS,
by C siTnchez Tarifa and P. Perez del Notario. Tech-
nical note no. 1 on Contract AF 61(052)221. 11 Apr 60.
7^ 15 refs. AFOSR TN-59-975.
Order from LC miH 50, ph$12. 30 PB 152 502
Combustion of droplets of bipropellant systems con-
sisting of a fuel (oxidizer) droplet within the vapors of
an oxidizer (fuel) is studied considering chemical ki-
netics and for equal or different moleculai weights of
the chemical species. The problem is solved by inte-
grating the differential equations of the process by
means of an approximated analytical method, and the
approximation furnished by such method is verified by
integrating numerically the equations of the process
for several representative cases. The principal vari-
ables of the process, such as burning rates,
flame/droplet radius ratio, maximum temperature,
etc. are expressed in function of the dimensionless
product of the pressure multiplied by the droplet ra-
dius, for several values of the main parameters of the
process (activation energy, temperature of the sur-
rounding atmosphere, etc. ) Several important conclu-
sions are obtained, as for example, that when either
the pressure or the droplet radius tend towards infin-
ity results coincide with those obtained by assuming
that the reaction rate is infinitely fast, and that there
exist minimum values of either the pressure or the
droplet radius under which combustion is not possible.
These theoretical conclusions have been experimen -
tally verified. (Author)
Lockheed Aircraft Corp. . Sunnyvale, Calif.
LOW-PRESSURE DEFLAGRATION LIMITS IN THE
STEADY DEFLAGRATION OF AMMONIUM PER- .
CHLORATE PELLETS, by W. Nachbar. Technical
note on Contract AF 49(638)412. Sep 59, 27p. 9 refs.
LMSD- 288168; AFOSR TN-59-1092; AD-234 700.
Order from LC mi$2. 7a ph$4. 80 PB 148 698
Recent experimental results on the cteflagration of
pure and catalyzed pellets of ammonium perchloraicJ
179
are reviewed, and ^ proposed model to explain the ob-
served low-pressure deflagration limit on the basia of
radiative heat loss to the surroundings is discussed.
BMed upon calculations of representative estimates
Ibr the radiant energy emission from the combustion
product gases of delflagrating ammonium perchlorate,
the radiative heat transfers from the product gases
both to the surroundings and to the solid surface are
calculated for several values of pressure.
Lockheed Aircraft Corp. , Sunnyvale. Calif.
RADIANT ENERGY EMISSION FROM THE EQUI-
LIBRATED REACTION PRODUCTS OF A PURE
AMMONIUM PERCHLORATE PELLET, by D. Olfe
and S. S. Penner. 'Technical note on Contract
AF 49(638)412. Sep 59, 53p. 5 refa. LSMD- 288169;
APOSR-TN-59-109II; AD- 235 161.
OnJer from LC mi|3. 6a ph$9. 30 FB 148 699
Representative estimates are made for the radiant
energy emission from the combustion products formed
by a burning pure ttnmonium perchlorate pellet. Be-
emission and absorption of radiation by the
in the reaction zone are negligible, the compi-
lukaw may be used to estinvate radiant energy loss
from the cmnhiitfcti products, as well as radiant heat
transfer to the buraing propellant surtece. The rec-
tangular geometry chosen for the calculations is itself
of no particular importance, and the results may be
tranalated readily |o other geometric configurations.
(Author)
Naval Engineerlni Experiment Station, Annapolis.
AN INVESTIGATION OF DIESEL ENGINE OIL
\ FILTRATION AND ABRASIVE WEAR WITH HIOl
DETERGENCY LUBRICANTS BY MEANS OF RADIO-
ACTIVE TRACER TECHNIQUES, by Harry HalllweU.
20 Aug 39, 31 p. Research and Development Repts.
620320A and 83000).
Order from LC mi|3.00, pfa$6.30 PB 153 254
This report released for sale to the public 14 Dec 60.
Tbe detergent-typeiails greatly reduced the amount of
piston ring wear in comparison to the nonadditive oil.
HomeyeT, when abnasive contaminants were added to
the lubricating oil system, the detergent additive oils
permitted much more piston ring wear than the non-
additive oil. Tbe d^ergent-type oils did not reduce the
ability cf either full- flow or bypass filters to remove
wear debria from the oil system. Fitters reduced
waar rates appreciably, both with and without abra-
sives added to the oil. Full-flow filters were more
effective than bypa$s filters in reducing wear when
abrasives were adc|ed and Just as effective as the
bypass type with the higher detergent oils in the
abeence oif abrasive. Bypass filters were the more
effective ones with oils of low or no additive content
when no abrasives were added. Tbe use of radioactive
chromium-faced steel piston rings and a monitoring
system employing a scintillation detector and pulse
beigbt analyzers permined rapid and quantitative
determination of w^r rates under various operating
cooditiaDa. (Autho^)
Naval Research Lab. , Washington, D. C.
F1LTERABILITY OF DISTILLATE FUELS. PART I.
DEVELOPMENT OF METHODS AND EFFECT OP
FILTER POROSmr, by A. J. Chiantella and J. E. JoIb-
son. Interim rept. 3 Nov 60. 23p. 9refs. NRL
rept. SSo5.
Order from OTS $0.75 FB 161 966
Fuel fllterability Is basically invoTved In the evaluatioa
of fuel stability. Two fllterability methods were
studied, one a constant- flow differential -pressure
method and the other a constant-bead gravity-flow
method. Goot^correlatlOD in reaults was obtained, and
because the constant -head method appeared nKire
desirable, it was used for further studies cf factora
affecting fllterability. It was found that the porosity of
the filter medium has a major effect on the volume of
fuel that can be filtered. Variations in porosity affea
the reproduciUlity cf plugging volumes. Relative
porosities were determined and applied to correct
plugging volumes to a standard porosity so that the
filtration characteristics of fuels could be determined
under comparable conditions. Most of the studies
were made at a fixed temperature since it was found
that a variation in temperature also affected the
plugging volume. (Author)
Reactloo Motors Dly. , Thloirol Chemical Corp. ,
Denville. N. J.
STUDY OF A TRACER METHOD FOR SOLID PRO-
PELLANTS. SPECTROSCOPIC DETECTION OF
TRACER ELEMENTS IN SOLID PROPELLANT COM-
BUSTION PRODUCTS, by W. Stark and H. CWolfhard.
Final rept. for 20 June 59-20 Mar 60, Contraa
AF 29(600) 2067. Aug 60. 40p. Rept. RMD 1159-F:
AFMDC TN-60-10.
Order from LC ml$3. 00. ph$6. 30 PB 152 257
The feasibility of a spectrographic method for de*
tectlaa at tracer elements in the exhaust flames of
solid propellant rockets was to be investigated. TUs
method could then be used to determine the burning
rate of solid charges by relating the time of appearance
of previously embedded tracers in the rocket flame
with the original positians of the tracers within the
grain. After discussion of the ttieoretlcal background
of this method, experiments and their results are de-
scribed. Aqueous solutions of tracer salts were sprayed
into a stoichiometric propane-air flame. Emission
spectra in the visible region from eacb tracer element
were detected by photomultipller tubes located at the
focal plane of a spectrograph. The suitabiliry of vari-
ous tracers was evaluated for detection under a great
variety of flame conditions. To study the more comples
conditfons cf propellant flames, sultaMe tracers were
then Incorporated into small solid propellent strands of
two different compositions. Feasibility cf the method
was demonstrated by the high signal -to- background
rattoa which occur for a number of elements present in
low ooncentratioas. (Author)
LsotW and TextilM
Nonmetallic Materials Lab. , Wright Air Develop-
ment Div. , Wright- Patterson APB, Ohia
FLAME BARRIER CHARACTERISTICS OF TEXTILE
FIBERS, by Edward L. McLeod. Repc on Air Force
TextUe Materials. July 60. 41p. WADD Technical rep.
60-385.
Order from OTS $1. 25 FB 171 136
180
I^^(^nl1^ of sample preparation and testing were devel-
gati to determine the relative performance of various
tooile fibers as impedients to applied flame. Testa
vere conducted on randomly oriented compressed fiber
P^a- Jt was found that residual products of ash-form-
li^ fibers continued to obstruct applied flame while
tenyeratures detected on the apposing side increased
at a varying rate with time. Melting and non-ash form
li^ fibers receded from applied flame without an in-
crease in detected temperatiire until the point of com-
plste flame penetration. In some instances, nylon 66
^tamed some departure from the normal pattern of
od>er melt type fibers, b was established that in-
creased tenqKrature lag time while the most favorable
dnsity for each fiber occurred at aome intermediate
defree of concentration. (Autiwr)
Quartermaster Research and Engineering Center,
Natlck. Mass.
DEVELOPMENT OF 91ADE STANDARD AND
TOLERANCES FOR USAF BLUE 157 NYLON- RAYON
POPLIN AND"^ POLYVINYL BUTYRAL COATED
NYLON TWILL, by Frank J. Rizzo. Constantine J.
Megas and others. Rept. for Jan 53-Oct 58 on
Air Force Textile Materials, Concraas
AF 33(616) 53-221 and MIPR (33-616) 56-15. July 60,
48p. 42 refs. WADD Technical rept. 60-295.
Order from OTS $L 25 PB 171 153
Slide standards and tolerances for Blue 157 have
been developed for cloth, nylon-rayon poplin and
doth, rayon twill polyvinyl butyral coated. The for-
OMilatian for the nylon-rayon fabric was prescribed
and Its colorfascness to its wet cleaning is dependent
oa die stability of the durable water repellent treat-
nsent. The coated fabric derives its colorfastness
from the selected formulation and the effect of the
pigmentation in the coating. The tolerance spacing
and general standardization procedure utilized was
one developed by the Quartermaster Research and
Engineer ii^ Command following procedures which are
well known in the industry. The program was moni-
tored by both instrumental and visual methods and the
tolerance spacing provided in such as to be in har-
mony with the essential military requirements of
good appearance and the recognized capabilities of the
Industry. (Author) n
Paints and Rnishes
Coatli« and Chemical Lab. , Aberdeen Proving
Ground, Md.
THE APPUCATION OF TEMPERATURE PRO-
GRAMMED GAS CHROMATOGRAPHY TO THE
ANALYSIS OF LACQUER SOLVENTS AND THIN-
fCRS, by G. G. Eaposito. 7 Oct 60. 12p. 4 refa.
CCLi97.
Order from OTS $0. 50 PB 171 033
A rapid, specific method is described for the analysis
of lacquer sohrencs and thinner a. Temperature pro-
frammed gas chromatography is used for the separa-
tion of solvents poasessing a wide range of boiling
pointa. Good resolution of a fifteen component solvent
mixture la obtained and tbe amount of each solvent is
determined by integratioo of the areaa under their
respective peaka. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
FIRE-RETARDANT COATINGS, by R. L. Alumbaugh.
^^fet 60, 24p. 5 refs. Technical rept. 087.
oWfc from OTS JO. 75, FB 171 182
Fifteen coating and impregiMting systems fot protecting
wood from fire were weathered and tested for effective-
ness. Only one system had good fire retardancy after
more than 18 montha exposure. Also studied were the
NBS Radiant Panel, tbe ASTM Stick and Wick, and the
ASTM Fire Test Cabinet methods erf measuring fire
retardancy. The NBS showed greatest differentiation
between control and fire retardant systems. (Author)
PiosHcs
Plastics Technical Evaluation Center, Picatlnny
Arsenal, Dover, N. J.
OXYCXN-ALCOHOL TEST FOR INSULATING MATE-
RIALS. A MEMORANDUM ON A SCREENING TEST
FOR ROCKET-MOTOR BLAST TUBES, by Harold F.
Mannl^imer and AUen M. Shibley. Oct 60, 32p.
PLASTEC rept. 2.
Order fi-om OTS $1.00 PB 161 948
Several laboratory test procedures have been devised
for screening materials to be used for solid-propellant
rocket chambers, blast tubes, nozzle backups, exit
cones, aft domes, and similar applications. In this re-
port a method is described whereby a liquid propellant,
consisting of an oxygen-isopropyl alcohol-water mix-
ture, is burned in a small motor at simulated operating
conditions. Eight commercial, filled plastic materials
(phenolic and melamlne resins, with asbestos and
fiber-glass fillers) were tested. The design criteria
for the insulating sleeve in this particular missile ap-
plication is to maintain outside casing temperature be-
low a maximum of 300PF. A definite correlation could
not be made between test results and actual perform-
ance because of the effects of such factors as aero-
dynamic flow, heat-flux densities, variation in propel-
lant systems, etc. The following test data are in-
cluded in the report: (1) PercenUge of insulation weight
loss, (2) Maximum temperature rise, (3) Molding con-
ditions for fabrication of test specimens, (4) Design
parameters for simulated rocket-motor blast-tube
tests, (5) Rocket- motor propulsion data and sample
data, (6) Calculation of nozzle diameter. (AiAhor)
Stanford Research Inst. , Menlo Park, Calif.
EFFECT OF RADIATION ON THE MECHANICAL
PROPERTIES OF PLASTICS, by David L. Chamber-
lain, Jr. Quarterly progress rept. no. 6. 15 Feb-
15 May 59, on Contract DA 04-200-ORD-698.
1 June 59, 23p. 1 ref. SRI Project SU-2296:
AD- 219 800.
Order fi-om LC mi$2. 70, ph$4. 80 PB 153 008
This report released for sale to the public 30 Nov 60.
Six polyethylene reeds were Irradiated to a toul dose
of 1 25 megarep, and VIRA measurements were con-
ducted. The concentration of crosslinks per cuWc
C* N
centimeter was calculated as, C = jg^- + jjj-. where
G is the elaatic moduiua in (fynes/aq cm, R is
181
Bolrzmann's gas coastant, g is the network entangle-
ment factor, N la Ayogadro'a number, T 'a the abao-
lige icmperatxire. ^ ia the denaity, and M ia the J^^
molecular weight. Vibr«tioo- induced energy haatenM
the potential change! at the post-irradiaiion effect.
i
bod and Paper
Foreat Products Ljab. , Madiscn, Wiac.
BONDINC PRESERYATIVE -TREATED VENEERS, by
R. F. Blomquist, J, O. Blew and othera. May 60, lOp.
BuS-7.
Order from OTS $a 50 PB 171 167
Pkior research has demonstrated that veneer treated
wtth Fhior-chronie*araenate-phenol (Tanalith) can be
ghied, on a laboratory scale, with phenol- resin glue
to produce plywood meeting the bond qualities required
by Specification MIt-P- 18066, "Plywood, Ship and
Boot Construction. '* Aa an aid to ultimate full-scale
commercial produc^on, detailed procedures are
described for pilot Or semicommercial- scale trials.
Procedures described cover the range of operations
from the heating at the bobs to final conditioning of
the plywood.
lj«b..
Forest Products Uafo. . K4adison, Wise.
DEFLECTION CHARACTERISTICS OF A W-FOOT-
WAMETER LAMINATED WOOD RINO SUBJECTED
TO COMPRESSIVE [LOADING ALONG A DIAMETER,
by Fred Werren an4 Robert L. Ethington. Sep 59,
30p. 4 refs. BuS-4,
Order from OTS $(175 PB 171 165
Teats were made tq determine if the existing theory
ter curved members applied to a large glued- lami-
■■■ad wood ring loaded along a diameter. A trial
southern pine ring and a white oak ring were fabri-
cated. The rings were tested by compressive loading
along a diameter, and the vertical deflection, the
horizontal defJection, and the strain in the outer fiber
at variixia locatlona were nteasured. The compressive
loads imposed bending stresses to approximately the
proportional limit. The rings were cut into quadrants
and tested as curveil beams. The modulus o( elasticity
and modulus of rupture were determined, and outer
fiber strain data w^-e obtained. Horizontal and
vertical ring deflections were computed from theory
and compared with those from test. Strains recorded
at the various strain gage locations were compared
for the rings and b^ams at equivalent values oif bend-
'iag moment. It wai concluded that the theory waa
applicable to a laminated wooden ring at the type
tested.
Poreat Product* liab., Madison, Wiac.
MOLDED COMPOSTTE FOR BOAT HULLS, by
B. G. Heebink, G. H. Stevens, and E. W. Kuenzi.
June 60, 43p. 8 ref». BuS-8.
Order trom OTS $1^.25 PB 171 168
r
A sandwich componed of impregnated veneer facings on
s e*U"ia»- celluloaa acetate core was proposed by the
Forest Products Laboratory in 1955 aa having promise
for molding small boars for the Navy. Subsequent testa
have shown that this construction can be molded to
compnsid curvatures, which small boats require, on
thin female mokte using fluid presaitt-e in an autoclave.
Tlie strength, stiffness, and impact resistance of four
11—11 m llmii of this type before and after soaking in
sea water are presented. Close agreement between
calculated and actual sueuRtli values indicates that
performance can be predicted from desi^ values.
Buoyancy tests show the four constructions to have
buo^rancles of about 30 pounds per ciMc foot sfker 1
year under sea water. Furthermore, this exposure
produced no delaminotion or decay.
Forest Products Lab. , Madison. Wis.
PRESERVATION OP THE EXTERIOR SURFACES OF
WOODEN SHIPPING CONTAINERS TO RETAIN IDEN-
TIFICATION SYMBOLS IN LONG-TERM OUTDOOR
STORAGE: FINAL REFT. OF 4 YEARS OF EXPOS-
URE, by V. P. Mlnluttl and E. A. Mraz. 29 Jan 60. 25p.
6 refs. Rept. no. 59-2; AD- 236 519.
Order from LC ml$2.70. ph$4.80 PB 148 727
Wood shipping containers were stenciled, bound with
steel bindings of round wire and flat strap, and placed
in outdoor exposure at Madison, Wis. . (^nanu Canal
2Sone. Fort Churchill, Canada, and Yuma, Ariz. Four
marUng materials were used with seven combinations
of two undercoat and four topcoat treatments to stencil
the north, south, and top sides of boxes made of red
oak, Douglas-fir. and southern yellow pine. After 4
years at exi>osure d the boxes pretreated with a water-
repellent preservative, the best legibility was found on
the north sides for 9 of the 12 combinations of species
and site, and on the south sides for the other 3 comU-
nationa. For the pretreated boxes, all stencils made
with 4 of 12 combinations of marking material and
undercoat-topcoat treatment were legible after 4 years
of exposure on the north sides of the boxes of all
species from all test sites. After 4 years of weathering
of the untreated southern yellow pine boxes, all sten-
cils made with 8 of 12 combinations at marking mate-
rial and undercoat -topcoat treatment were legible on
the north side at all teat sites, and those made with 6
combinations were legible on the south side at all test
sites. One material preserved the legibility of the
stencils on the southern yellow pine boxes in Panama,
but not at the other three test sites. It provided pro-
tection agalnat stain and decay fungi that is needed at
Panama. (Author)
Forest Products Lab. , Madison, Wise.
STATIC AND IMPACT BENDING TESTS OF GLUED
LAMINATED WOOD, by William L. James. Feb 60,
56p. 5 refs. BuS-6.
Order from OTS 11.50 PB 171 166
Laminated apecimens, 2 by 6 by 72 inchea, were
tested as beams In edgewise bending with center load-
ing co a 66- inch span. Load- deflection curves were
obtained for all specimens. Specimens were made
from laminationa of flat-grain white oak, flat-grain
Douglas-fir, and vertical-grain Douglas-fir. Five
specimens at each type of material were tested in
static bending, and 10 specimens of each type, side-
matched to static specimens, were tested in impact
bending. The dau show considerable variation. A
gUi^fl-—* difference between the static and impact re-
ggin is that the proportional limit stress is higiher in
bendii^ than in static bending.
1S2
•nmber Engineering Co. , Washington, D. C.
KMONG RADII OF DENSE, PLAT SAWN DOU(XAS
Pit AS AFFECTED BY SLOPE OF GRAIN AND
KNOTS, by W. J. Finnorn and R. A. Holcombe. Rept.
aa Contract NObs 77018. 1 Sep 59, 26p. 2 refs.
Order from OTS $0.75 PB 171 169
Tkt magnitude of radius of curvature at the poii« o<
■rofortional limit and failure in bending dense, flai-
ggWB Dmi^* fir is significantly affected by the thici:-
oess of the bent member involved. The thicker the
gpecimen involved, the greater the radius of curva-
nre, both at proportional limit and failure in bending.
Slofe dl grain does not have a significant effeca on
raiMua of curvature at prqportional limit or failure in
denae, flat- sawn Douglas fir. Knots 5/8" in size and
above affect the radius of curvature of flat-sawn
dense Doi^flas fir specimens at proportional limit and
•t failure in bending to a greater extent than knots In
the 1/8" to 1/2" size class. In this study, no appreci-
able difference in effea was observed between the
5/8" to 1" and 1-1/8" to 1-1/2" knot size classes.
Timber Engineering Co. , Washington, D. C
BENDING RADII OF TANALITH -TREATED SOUTH-
ERN YELLOW PINE AS AFFECTED BY KNOT SIZE.
byW. J. FinnomandR. A. Holcombe. Rept. on Con -
traa NObs 77018. 1 Sep 59, 15p. 1 ref.
Order from OTS $0. 50 PB 171 170
There is no significant relationship between the knot
size and radius of curvature at proportional limit in
flat-sawn, Tanalith -treated, dense southern yellow
pine. In Tanalith-treated, dense, flat -sawn southern
pine, knots 1-1/8" in size and above affect the radius
of curvature at rupture to a greater extent than knots
In the 5/8" to 1" size class. In this study, no appre-
ciable difference in effect was observed between the
1/8" to 1/2" and the 5/8" to 1" knot size classes.
Timber Engineering Co. . Washington. D. C
BENDING RADII OF THREE THICKNESSES OF
TANALITH TREATED BLACK GUM AND DENSE
AND NON- DENSE TANALITH-TREATED HICKORY,
by William J. Finnorn and Robert A. Holcombe. Rept.
on Contract NOba-77018. 1 Sep 59, 15p. 1 ref.
Order from OTS $0. 50 PB 171 171
The bending radii of Tanalith-treated black gum at pro-
portional limit and at rupture is intermediate between
dense and non -dense Tanalith-treated hickory. Tana-
lith-treated dense hickory can be bent to sharper radii
than Tanalith-treated non -dense hickory before reach-
ing porportional limit. Tanalith-treated non -dense
hickory can be bent to sharper radii than Tanalith-
treated dense hickory before failing.
Timber Ei«ineering Co. . Washington, D. C
EFFECT OF BOARD WIDTH CW BENDING RADU OP
WHITE OAK AND DOUGLAS FIR. by William j.
Finnorn. Rept. on Contract NObs 77018. I Sep 59, 12p.
I ref.
Older from OTS $0. 50 PB 171 173
The proportional limit and breaking radii of Douglas
fir boanls are not affected by width. Width has a sig-
nificant effect on the radius of curvature at which white
oak boaixls fail when subjected to bending. While teat
i«autcs Indicated no statistically significant effect of
board width on proportional limit radius in white oak,
it should not be definitely concluded that no such re-
lationship exists.
Timber Ei^ineering Co. , Waahington, D. C
EFFECT OF BOARD THICKNESS ON BW DING
RADII OR EKKL by W. J. Finnorn. Rept. on Contract
NObs 77018. 14 Aug 59. 8p. l rrf.
Order from OTS $0. 50 « 171 172
Radii of curvature at proportional limit and at rupture
are approximately linear functions of board thickness.
Their values can be determined by the following
formulas:
Rp('=140l - 3 .
= 40t - 1.5
where:
limit
IL DsRadius of curvature at proportional
Rr -Radius of curvature at rupeure
t sBoard thickness
Timber Engineering Co. , Washington, D. C.
THE EFFECT OF INDIVIDUAL LAMINATION THICK-
NESS-ON THE STRENGTH OF CURVED AND
STRAIGHT WHITE OAK BEAMS CONTAINING CROSS
GRAIN, by W. J. Finnorn and R. A. Holcombe. Rept.
on Contract NObs 77018. 1 S^ 59. 47p.
Order from OTS $1. 25 PB 171 174
The strength of straight white oak beams made up of
laminates containing face or edge grain slope from 1:11
to 1:14 is not significantly affected by direction of load
application with respect to the glue lines. Curved i^
and straight white oak beams made up of laininations
containing face or edge grain slope from 1:11 to 1:14
do not differ significantly In strength properties.
Curved and straight beams, loaded perpendicular to
the glue line, containing laminations with maximum
slope on their wide faces are weaker In modulus of rup-
ture and work to maximum load than are beams
containing slope on the edges of their laminations.
Lamination thickness has an effect on fiber stress at
proportional limit and work to proportional limit In
curved beams and In straight beams loaded perpendic-
ular to the glue lines. In the range of lamination thick-
nesses studied (1/4" to 3/4 "). these properties were
optimum at the 1/2" thickness. In curved beams, there
is also an Indication that lamination thickness has an
effect on work to maximum load, with the optimum
thickness appearing to be 5/8".
183
Timber Engineering Co. , Washington. D. C
EFFECT OF LAMINATI(»J THICKNESS ON SHRINK-
AGE AND SWEIU-ING OF WHITE OAK LAMINATES,
by WillUun J. Piimom. Rept. on Contract NObs 77018.
1 Sep 59. 23p.
Order from OTS $0. 75 PB 171 175
Based on the wonk conducted, the number of glue lines
in a laminated white oak beam have no effect on dimen-
sional changaw^tich occurs as a result of change in
moisture contenO. In laminated oak blocks, the dimen-
•ional change perpendicular to the giue lines is signif-
icantly greater than the change parallel to the glue
lines for a given i grain direction (radial or tangential).
' In ^>ecimens made up of flat- sawn laminates, the ra-
dial shrinkage, v|rhich is perpendicular to the glue line,
la greater than tke radial shrinkage, parallel to the
glue line, in a blpck composed of quarter- sawn
laminates.
Timber Engineering Co. , Washington, D. C.
STRENGTH OF CURVED AND STRAIGHT DENSE
DOUGLAS FIR LAMINATES AS AFFECTED BY
INDiVIDUAL LAMINATION THICKNESS, by
W. J. Finncrn an|l R. A. Holcombe. Rept. on Contract
NObs 77018. 1 9ep59, 47p. 1 ref.
Order from CTSj$1.25 PB 171 176
otic
The direction ot loading with respect to the glue lines,
perpendicular or parallel, has no effect on the
strength of straight, laminated Douglas fir beams.
The modulus of ijupiure and work to maximum load in
■traigbt laminated Douglas fir beams loaded tangent to
the annual rings (ire significantly higher than in beams
loaded in a direction approximately normal to the
annual rings of tke laminations. Straight laminated
beams composed of flat grain laminations have higher
moduli ot elasticity than thoee beams made up of
vertical grain la^nationa. In curved and straight
members, work ^o maximum load is greatest in the
1/2" lamination lihickness. Modulus al rupture and
work to maximuTi load are significantly lower in
curved beams th4n in atr sight beama.
^MATHEMATICS
Aeronautical Research Labs. , Air Force Research
Div. , Wright -Pttterson AFB. Ohio.
EXPECTED VALUES OF NORMAL ORDER STATIS-
TICS, by H. Leoa Harter. Rept. on Transformations
in the Analysis of Variance. July 60, 48p. 18 refs.
ARL technical rett. 60-292.
Order from OTS ^1.25 PB 171 161
A brief history 14 given of the development of the theory
of order statistic^ and of past efforts to tabulate their
expected values fbr samples from a normal population.
A fuller account is given of the method of computation
of a five -decimal-place table of the expected values of
all order statistics for saniples of size n from a nor -
Rial populatloD. ^luded is such a table for n » 2(1) 100
and for values of ti, none of whose prime factors ex-
ceeds seven, up itirough ns400. Also included is a
discussion of an tpproocimation proposed by Blom, and
a table of values of tbe constant a required for this
apprcKimation fot selected values of n. together with
interpolation formulas for estimating • for other
values of n. A discussion is given of actual and po-
tential uses of the tables. (Author)
Air Force Cambridge Resesrch [Labs. ] Bedford.
Mass.
A METHOD OF SCHEMATIC NUMERICAL FOURIEK
SYNTHESIS OF PERIODIC POLYGONAL FUNCTIONS,
by Kurt H. Haase. Dec 59, 63p. 6 refs. AFCRC-TR-
59-371; AD- 234 553.
Order from LC mi$3. 90. ph$10. 80 PB 148 707
The study on a method for numerical evaluation of the
coefficients of Fourier series is continuing. The syn-
thesis of periodic polygcxud functions equally spaced
in the direction of the variable is discussed. An equa-
tion is derived expressing the 2n samples in the period
of a polygonal functioa An analysis theorem and a
synthesis theorem are suted. Starting with the knowa
periodic coefficients, a numerical Fourier synthesis
is shown to be constructed with the use of schemes de-
veloped previously. The analysis and synthesis of
periodic function are exemplified.
Applied Matbematict and Statistic* Labs . .
Stanford U., Calif.
AN ASYMPTOTIC EXPANSION FOR THE DISTRIBU-
TION FUNCTION OF THE CLASSIFICATION STATIS-
TIC W , by Albert Bowker and Rosedlth Sitgreaves .
Technical rept. no. 53 on Contract N6onr- 25140.
15 Nov 59, 40p. 7 refs. AD- 230 009.
Order from LCmi$3. 00, pta$6. 30 PB 152 162
Applied Mathematics and Statistics Labs. ,
Stanford U. , Calif.
BOUNDS FOR ANALYTIC FUNCTIONS OF TWO COM-
PLEX VARIABLES, by Zygmmt Charzynskl. Rept. on
National Science Foundation Grants 3361 and 10375.
29 Feb 60. 14p. 9 refs.
Order from LC mi|2. 40. ph$3. 30 PB 148 978
Applied Mathematics and Sutistics Labs. , Sunford
U., Calif.
THE LINEAR EQUATIONS PROBLEM, by WalUce
Givens. Technical rept. no. 3 on Contract Nonr-
225(37). 1 Dec 59. 28p. 9 ref a.
Oixler from LC mi$2. 7a pfa$4- 80 PB 152 160
The simplest case of a linear equations problem is
that of finding m unltoowns by solving m linear alge-
braic non -homogeneous equations with given coeffi-
cients and constant terms. If this solution is carried
out m times with the columns of the identity matrix aa
successive choices for the constant vector, the re-
sulting sets of solutions form the columns of the in-
verse of the matrix of coefficients. In both of these
special cases the usual computing techniques proceed
on tbe assumption that there is a unique set of num-
bers satisfying the given equations. If, however, the
coefficient matrix is singular, well-known theorems
give tbe conditions under which the equations have no
solution and those under which they have an infinite
number of solutions, depending on one or more pa-
rameters. Another situation which is disposed of very
184
■imply in a purely theoretical treatment but which is
OQB-trivial in practice is that in which there are more
equations than unknowns, yet a solution is known, or
at least believed, to exist. The purpose of the present
paper is to describe a method of solving in a routine
say • class of linear algebraic problems which in-
clude the various special cases already mentioned.
Applied Mathemstics and Statistics Labs. , l^nford
v.. Calif.
MULTIVARIATE CHEBYSHEV TYPE INEQUALITIES,
by Albert W. Marshall and Ingram OUdn. Technical
reot. no. 52 on Contract N6onr-25140. 3 Dec 59. 39p
9 refs. AD- 230 010.
Order from LC mi$3. 00, ph$6. 30 PB 152 161
Various inequalities are considered Involving (1) the
minimum component or (2) the produa of components
at • random vector. Derivations and proofs of sharp-
ness for these 2 classes of inequalities show re-
markable similarities. Some of each type occur as
■pedal cases of a general theorem. (Author)
California U. , Berkeley.
PROPERTIES OF SOLUTIONS OF PARABOLIC
EQUATIONS AND INEQUALITlESt by M. H. Protter.
Ttehnical rept. no. 8 on Contract AF 49(638)398.
Mar 6a 25p. 5 refs. AFOSR TN-60-282: AD- 234 945.
Order from LC mi$2. 70, ph$4. 80
PB 148 670
Ihe asymptotic behavior of solutions of parabolic in-
aqualities and the uniqueness of the Cauchy problem
for such inequalities when the data are prescribed on
• portion at a time-like surface are considered.
Ctmegielnst. of Tech., Pittsburgh, Pa. -
INTEGRAL REPRESENTATIONS OF AXIALLY SYM-
METRIC POTENTIAL FUNCTIONS, by R. C. MacCamy
Technical rept. no. 33 opjOdfitract AF 49(638)227.
8q>60, 25p. 7refi. AFOSR TN-60- 1092.
Older from LC mi$2. 70, ph$4. 80 PB 152 490
Carnegie Inst, of Tech. , Pittsburgh, Pa.
NOTE ON POLYHARMONIC FUNCTIONS, by
1. J. Duffin and Z. Nehari. Technical rept. no. 32 on
Contract AF 49(638)227. Mar 60, lOp. 3 refs. AFOSR
1X-60-328; AD-235 374.
Order from LC mi$l. 80, ph$l. 80 PB 149 661
The following theorem is proved: If u(P) is a non-
■Bfitive polyharmonic fiuiction of order n in the
m -dimensional sphere OP « r < R.
chenu(P)$AR'""^iSi£i— -, . (Author)
Connecticut U. [Siorrs].
OH THE INTERPOLATION OF LP FUNCTIONS BY
JACKSON POLYNOMIALS, by Richard P. GosseUn.
Rept. on Contract AF 49(638)606. Sep 60, lip. 4 refs.
AFOSR -TN-60- 1066: AD- 244 666.
(Mer from LCnd$2.40. ph$3.30 PB 152 444
The precise order of the upper limit of the sequence o*
Jackson polynomials interpolating an LP function at the
usual points of interpolation translated by an arbitrary
real is deterndned. The result is generalized to
certain sequences of operators, and tbe generalized
result is applied to ottiier aequetices of functions .
Electronics Research' Lab. , Northeastern U- ,
A LOSS- MINIMIZING EXTENSKW OP THE LAN-
CHESTER THEORY CW COMBAT, by Ralph E.
Bach, Jr. , Ladlslav Dolansky, and Harold L. Stufabs.
Scientific rept. no. 3 on Cootract AF 19(604)4573.
31 Jan 60, 28p. 8 refs. AFCRC TN-60- 168;
AD-235 019.
Order from LC mi$2.70, ph$4.80 PB 148 715
Problems involvii^ a conflict between 2 opposing forces
call for predictions of outcome and comparison of tbe
total effectiveness of the 2 sides in quantitative terms.
One of the first attempts to obtain such quantitative re-
sults was made by F. W. Lanchester. His relationships
in tbeir generalized form which includes operational
losses, were used to derive expressions for the total
losses of the^ victor. A simple experimental drcuitwas
used to demonstrate that it would be feasible to obtain
some at the desired answers by analog means. (Author)
Harvard U. [Cambridge, Mass. ]
DEGREE OF APPROXIMATION BY BOUNDED HAR-
MONIC FUNCTIONS, by J. L. Walsh. RepL on Coo-
tract AF 49(638)574. June 60, 12p. 4 refs. AFOSR
TN-60- 594. AD- 244 393.
Order from LC mi$2. 40, ph$3. 30 PB 152 373
There have recendy been published several notes on
degree of approximation on a Jordan curve or arc by
polynomials in the complex variable, and also a pupcT
on approximation by bounded harmonic functions, all
with emphasis on properties invariant under conformal
transformation. The last- nanrod paper admits of ex-
tensions (i) to nnore general degrees of approximation
Aand (11) to approKintatioo on a Jordan arc; the object of
the present note is briefly to set forth tliese extensions
*(Autlior) i
Harvard U. [Cambridge, Mass.]
NOTE ON POLYNOMIAL APPROXIMATION Oti A
JORDAN ARC, by J. L. Walsh. Rept. on Cootract
AF 49(638)574. May 60, 9p. 4 refs . AFOSR TN-
60- 542; AD- 244 392.
Order from LCmi$l. 80, ph$l. 80 PB 152 372
Two recent notes have dlscusaed tbe invariance of de-
gree of polynomial and trlgooometric approximation
under change of independent variable . Hoprever , those
iKXes did not emphasize approximation in the complex
plane oo a Jordan arc rather than oo a Jordan curve; tbe
object of the present note is to indicate rapidly addi-
tional results , concerning Jordan arcs . (Author)
185
Harvvd U. [C^rain-idge, Mass.]
SOME kEMARKB ON TEICHMULLER'S SPACE OP
RIEMANN SURFACES, by L. V. Ahlfors. Rept. oo
,Ccntract AF 49«^)574. June 60. 38p. 7 refs. AFOSR
TN-60-721; ADi244 394.
Order from LC <ni$3.00, pb$6.30 PB 152 374
The paper deals {primarily with the connectioD between
variations of the conformal metric and quadratic dif-
ferentials. AtteiitiOn is drawn to certain simple aspects
of this connectioli which seem to have escaped notice.
For instance, we remark that the antilinear part d the
variation d the mapping function is three times iterated
iiaegral of a quadratic differential. There is thus an
laKresting relationship with the theory of generalized
Abelian integral*, as developed by Eichler. The com-
plex structure ol Teichmllller space is derived from the
corresponding structure d L** by way of the general-
izad Rlemann mapping theorem. This approach, which
is esaencially due to Bers, is also appropriate for the
study at the fibre space whose fibres are the closed
Rlemann surfaces. (Author)
Hebrew U. OsfMl).
THE ANGULAR laSTRiaunCW OF EIGENVALUES
OF NON SELF-ADjaNT ELUPTIC BOUNDARY
VALUE PROBLEMS OF HIGHER ORDER, by Shmuel
Agmon. TechmoBl (scientific) note no. 8 on Contract
AF 61(052)187. June 60, 19p. 6 refs. AFOSR- TN-
60-1179. I
Order from LC 4u$2. 40, pt43. 30 FB 152 442
The piper gives various results on the distribution in
the comi^ex plane of non self-adjoint elliptic boundary
value problems . (Author)
U. (Isrlel)
Hebrew
LOCAL DIFFERENTIAL ALGEBRA: THE ANALYTIC
CASE, by S. HalQn and A. Robinson. Technical (scien-
tific) note no. 9 ()n Contract AF 61(052)187. June 60,
lOp. 3 refs. AFQSR-TN-60-1180.
Order from LC ifiS 1.80. ph$ 1.80 PB 152 441
A teat is obtaine4 for the existence at an analytic solu-
tion for a system of algebraic differential equations
with initial condition of a general character. (Author)
U. (Isriel).
Hebrew
THE PRODUCT OF SUMMABILTTY METHODS; NEW
CLASSES OF TRANSFORMATIONS AND THEIR
PROPERTIES. PART 3, by Amnon Jakimowski . Tech-
nical (scientific) ^e no. 10 on Cotitraa AF 61(052)187.
Ang60, 3Sp. 1 r^. AFOSR -TN-60- 1181.
Order from LC nti$3. 00, ph$6. 30 PB 152 439
A new class of Iliiear transformations is defined and
inweatigated. Ne(iessary and sufficient conditions for
the regularity of tnother class of linear transforma-
tkms are given aitd tauberian theorems for still
anodwr class of linear transformations are proved.
(A«lnr)
I
Hebrew U. (Isniel).
SOME RESULTS K>J CONVEX BODIES AND BANACH
SPACES, by Aryeh Dvoretzky. Technical (scientific)
note ao. 11 on Ca«traa AF 61(052)187. Aug 60, 65p.
U refs. APOSR-rN-60-1182.
Order from LC nmJ3. 90, ph$10. 80 PB 152 440
The paper deals with a theorem on almost spherical
sections of convex bodies in Banach spaces, and its
applications. (Author)
Institute for Advanced Study, Princeton, N.J.
PROPERTIES OF SOLUTIONS OF DIFFERENTIAL IN-
EQUAUTIES, by M. Lees. Rept. on Contract
AF 49(638)253. Aug 60. 14p. 2 refs . AFOSR [TN]-
60-1130; AD- 244 398.
Order from LC mi$2.40, ph$3.30 PB 152 491
This paper investigates the maximum permissible rate
of decay of solutions to certain abstract differential in-
equalities in a Hilbert space. These results are then
applied to parabolic differential inequalities , subject to
general homogeneous boundary conditions . (Author)
Institute of Mathematical Sciences, New York U. ,
N. Y.
THE FUNCTIONAL SYNTHESIS OF UNEAR PLOTS,
by R. F. Dressier and J. P. Vinti (National Bureau of
Standards). Rept. on Contract AF 49(638)161 . Dec 59.
lip. IMM-NYU 264; AFOSR TN-60-40; AD- 234 919.
Order from LC mi$2. 40, ph$3.30 PB 148 691
In practical engineering or experimental work, a func-
tion F of many variables, F(x's, y's, z's), is repre-
sented only by the families of curves obtained by plot-
ting F against each of the x's on Cartesian graph paper,
against each of the y's on semi-log paper, and against
each of the z's on double-log paper. These curves are
often all approximately straig^ lines over some limited
range of interest. On the assumption that they are all
true straight lines, the study shows how to synthesize
all the graphical representations for any number of
parameters into the most general formula expressing F
as the produa of a general multilinear function ctf the
x's and the exponential of a constant -free multilinear
function of the y's and of the log z's, with the coeffi-'
cients in both multilinear functions being independent
of the x's, y's, and z's. (Author)
r ,''
Institute of Statistics, U. of North Carolina,
Chapel Hill.
THE ASYMFTOTIC POWER OF THE KOLMOGOROV
TESTS OF GOODNESS OF FIT, by Dana Quade. Rept.
on Contraa AF 49(638)261. Dec 59, 99p. 19 refs.
Mimeograph series no. 243; AFOSR TN-60- 55;
AD- 235 096.
Order from LC mi$5.40, ph$15.30 PB 148 692
The asymptotic power of the one-sided and two-sided
Kolmogorov tests of goodness of fit of a hypothesis
distribution H(x) against sequences of alternatives
Gn(x) for which »)iP/nlH(x)-Gn(x) I tends to a Umit is
investigated by application of Doob's "heuristic proce-
dure" ; bounds on the power are found, and some
numerical examples provided.
Institue of Statistics, U. cf North Carolina [Chapel
Hill).
LOWER BOUNDS FOR THE EXPECTED SAMt»LE
SIZE AND THE AVERAGE RISK OF A SEQUENTIAL
PROCEDURE, by Wassily Hoeffding. Rept. on Contract
AF 49(638)261 . June 59, 31p. 15 refs. Mimeograph
series no. 227; AFOSR TN-59-800; AD- 235 093.
Order from LC mi$3.00, ph$6.30 PB 148 683
186
ipmcT bounds are considered for the expected sample
size Ed(N) of an arbitrary setiuential test whose error
nrobabilitles at two parameter points, Gj and 62, do
001 exceed given numbers ai and 02, where Eo(N) is
evaluated at a third parameter point &o- The bounds
are shown to be attainable or^nearly anainable in cer-
uin cases where 60 lies between Oi and 62- Lower
bounds for the average risk of a general sequential
procedure are obtained. (Author)
Institute of Statistics, U. of North Carolina,
0>^>el HiU.
ON THE APPLICATION OF THE GEOMETRY OF
QUADRICS TO THE CONSTRUCTION OF PARTIALLY
BALANCED INCOMPLETE BLOCK DESIGNS AND ER-
ROR CORRECTING BINARY CODES, by D. K. Ray-
Chaudhuri. Rept. on Contract AF 49(638)213. June 59,
134p. 27 refs. Mimeograph series no. 230; AFOSR-
TO-59-796; AD- 235 092.
Order from LC miJ6. 90, ph$21. 30 PB 148 6%
Contents: ' '' .
Some preliminary results on the geometry of quadrics
in finite projective space
Some classes of partially balanced incomplete block
(PBIB) designs with 2 associate classes obtained from
the configuration of linear spaces contained in a
quadric
Some classes of PBIB designs with 3 associate classes
A class of 2 error correcting codes with rate of trans-
mission arbitrarilv close to unitv and fractional
replications preserving main effects and 2 factor
Interactions 1
Institute of Statistics, U. of North Carolina, Chapel
HiU.
ORTHOGONAL LATIN SQUARES AND gULER'S
CXWJECTURE, by R. C Bose, S. S. Shrikhande. and
E. T. Parker. Rept. on Contract AF 49(638)213. Jan 60
35p. 36 refs. Mimeograph series no. 245; AFOSR TN-
59-1241; AD-235 095.
Order from LC mi$3.00, ph$6. 30 PB 148 687
This is an expository paper describing the recent work
by the authors. Some of the proofs have been simplifiec
and enou^ back ground material has been included to
make it possible for graduate level students of mathe-
matics, or persons with equivalent training, to follow
the work.
Institute of Statistics, U. of North Carolina
[Chapel Hill].
TWO-STAGE EXPERIMENTS FOR ESTIMATING A
(XJMMON MEAN, by Donald L. Richter. Rept. on
Contract AF 49(638)261. June 59, 20p. 3 refs. Mimeo-
graph series no. 231; AFOSR TN-59-973.
Order from LC ml$2. 40, ph$3. 30 PB 148 684
This investigation treats the problem of estimating the
common mean ti of two populations using a fixed num-
ber n of observations. If the population variances were
known, the most efficient procedure would be to take
•11 n observations from that population with the smaller
variance. When prior information about the variances
it lacking or is too vague to be quantified, it Is natural
to consider the pnxedure which consists of taking a
preliminary sample of size m from each population,
computing estimates of the variances, and then taking
the remaining n-2m observadoos from that population
with the apparently smaller variance. Since, if m is
chosen too large or too small, the advantage of the
two- stage sampling scheme over the procedure of tak-
ing n/2 observations from each population will be loet,
the important question is to determine for some good
estimator an optimum choice of m as a function of n,
not dependent on the unknown variances.
Johns Hopkins U. . Baltimore. Md.
ON BOUNDARY VALUE PROBLEMS FOR SYSTEMS
OF ORDINARY, NON-UNEAR SEOWD ORDER. DIF-
FERENTIAL EQUATIONS [AND) ON THE DIFFER-
ENTIATICW OF A MULTIPLE INTEGRAL DEPENI>
ING ON A PARAMETER, by PhiUp Hartman. Tech-
nical note no. 15 on Contract AF 18(603)41 Jan 60.
34p. 16 refs. AFOSR TN-60-lll; AD- 234 918.
Order from LC mi$3.00. phJ6.30 PB 148 693
On boundary value problems for systems of ordinary,
non- linear, second order differential equations: Non-
singular and singular boundary value problems are
considered for a system of equations of the type
X =f(t, X, x), in which x and f are vectors. The prin-
cipal results depend on a priori bounds ^or the first
derivatives of bounded solutions x- x<t). These a priori
bounds are generalizations of Nagumo's results for the
scalar case. Nagumo s condition | f| ^ 4' (| '^'l )• *t»ere
^(u) satisfies/* udu/t(u)- •o. does not suffice for
the existence of a^ priori bounds in the vector case and
must be supplemented by other conditions. On the dif-
ferentiation of a multiple integral depending on a
parameter: Sufficient conditions and a simple proof,
involving a minimum of topological conndepations, are
given for the differentiability of a multiple integral in
which both the integrand and domain of integration
depend on a parameter.
Liege U. (Belgium).
RESEARCH IN HYPERBOLIC DIFFERENTIAL EQUA-
TIONS, by Florent J. Bureau. Annual summary rept.
no. 2. 15 Mar 59-14 Mar 60. on Contraa AF 61(052)86.
15 Mar 60. 4p. AFOSR-TN-60-1058.
Order from LCmiS 1.80. ph$ 1.80 PB 152 43t
See also PB 149 585
Lincoln Lab. . Mass . Inst, of Tech. . Lexington .
UNEAR RECURSIVE SEQUENCES AS FINITE DIF-
FERENCE EQUATIWIS. byG. Solomon. Rept. on
Contract AF 19<6O4)5200. 15 Mar 60. 15p. 5 refs .
Group rept. no. 47.37; AD-243 047.
Order from LC mi$2. 40, ph$3. 30 PB 150 793
Maryland U. , College Park.
ON UNIQUENESS IN CAUCHY PROBLEMS FOR
ELLIPTIC SYSTEMS OF EQUATIONS, by Avron
Douglis. Rept. 00 Contract AF 49(638)590. Mar 60,
2^. 11 refs. AFOSR TN-60- 249; AD-235 377.
Order fron LC mi$2. 70, ph$4. 80 PB 148 672
The question has been raised as to whether the solu-
tions of systems of linear, first order, partial differ-
187
eotUl equations In two independent variables, in the
case al non-analytic coefficients, are uniquely deter-
mined by their Caiichy data. The answer to the ques-
tion in the affirmative, when the characteristics are
complex. siifficien|ly regular, and d multiplicities
not greater than tifo. (Aucbor)
tiiOL
[Pennsylvania U. , Philadelphia].
UNIVERSAL MINIMAL SETS, by Robert Ellis. Rept.
on Contract AF 491638)569. [19591 Sp. AFOSR TN-
59-1119; AD- 234 911.
Order front LC mi|l. 80. ph^l. 80 PB 148 685
Let T be an abstract group. Then a universal minimal
set for T is a transformation group (X, T) with com-
pact phase space X, such that (X, T) is minimal and
such that any ocber] transformation group (Y, T) with
Y compact and (X, |T) minimal is a homomorphic
image of (X. T). Iq this note it is shown that such a
uniTersal minimal set exists for every group T and
is unique. Moreover, the action a< T on X is strongly
effective. (Autborjl
Princeton U., N.J.
OBSTRUCTIONS TO IMPOSING MFFERENTIABLE
STRUCTURES, by |ames Munkres. Rept. on Contract
AF 49(638)431. Ju^ 60, 38p. 13 refs. APOSR-TN-
60-921. I
Order from LC nnl^3.00. ph$6.30 PB 152 545
i.
Purdue Research iPouidatlon [Lafayette, Ind. ]
ONE-DIMENSIONAjL MONOTONE RETRACTS, by
A. Lauria and C. irNeugebauer. Teciinical note
DO. 23 on AnalytiaU Theory of Continuous Transfor-
nutlons. Contract AF 18(600)1484. July 60, 47p.
18 refs. PRF-1203k AFOSR -TN- 60- 758; AD- 244 695.
Order from LC mi$3.30, ph$7.80 PB 152 543
This paper deals w|th the problem of classifying all
regular curves whit± are nKXKXone retracts of a Pea no
space P. Unless r(i*) < oo, the degree of muratMher-
eoce of P. this class of retracts may be vacuous. If
r(P) ■ n, n < «•, tjie class of all regular curves R
with r (R) ■ n wbid^ are monotone retracts of P, is
characterized.
idk
Rice U . , Houston , Tex .
(W THE LEBESGUE CONVERGENCE THEOREM, by
Arlen Brown. Rept; on Contract AF 49(638)632.
16 Sep 60, 13p. AFOSR TN-60-720; AD- 244 284.
Order from LC mi|2.40, ph$3. 30 PB 152 430
n LC mi|2.40,
U., N. t.
by
Syracuse
CXSKTTNUOUS PARAMETER MARKOV CHAINS.
K. L. Chung. Resaarch rept. 18 on Contract
AF 48(638)265. Sep 58, 15p. 22 refs. AFOSR-TN-
58-889; AD- 204 097. |
Order from LCmi«2.40, pli$3.30l PB 149 717
rfses
This work summarizes the recent work on continuous
parameter Markov chains done with direct probabi-
listic methods and ^eixions a few open problems.
(Author)
University Coll. , Cork (Eire).
FOURIER SERIES FOR TWO- POINT BOUNDARY -
VALUE PROBLEMS, by Patrick M. Quinlan. Technical
note no. 8, 1 Dec 58-30 Nov 59, on Contraa
AF 61(514)1163. Nov 59, 143p. 12 refs. AFOSR-TN-
59-744; AD- 233 280.
Order from LC nU$7. 20, ph$22. 80 PB 149 073
The eeneral solution of the differential equation
F(D^ - g(x) is obuined in the form of a Fourier Sine
or Cosine Series. The result is expressed in terms of
Fourier-Sum Functions, involving 2 parameters K and
a which are tabulated for K,0(. 1)2; «/»', 0(.l). 1. The
method is illustrated by numerical application to an
eight order differential equation. (Author)
Uppsala U. (Sweden).
STANDARD ERRORS AT HARMONIC ANALYSIS, by
Eric Dyring and Bengt Rosen. Technical note no. 3 on
Contract AF 61(514)1312. 25 Mar 60, 17p. 5 refs.
AFCRC-TN-60-433.
Order from LC mi$2. 40, ph$3. 30 PB 152 206
Standard errors of harmonic analysis have been cal-
culated by three different methods. These methods
are discussed and numerical calculations have been
carried out from the results of harmonic analyses
made on data from the neutron monitors in Uppsala
and Murchison Bay. Periods covering from single days
up to the mean of three years have been used for the
comparison between the results. Although the stand-
ard error calculated according to the three methods
include different types of variations, the results show
good similarity. One of the methods' also gives indi-
cations that only in some cases the addition of a sec-
ond harmonic will be an improvement of the fit.,
(Author)
Washington U. , St. Louis, Mo.
VARIATION DIMINISHING TRANSFORMATIONS AND
ORTHOGONAL POLYNOMIALS, by Isidor I. HirscJi-
man, Jr. Rept. on Contract AF 49(638)218. June 60,
24p. 13 refs. AFOSR -TN- 60- 640. AD-244 260.
Order from LC ml$2.70, ph$4.80 PB 152 396
Washington U. , Seanle.
RELATIONS AMONG m ^TS OF VARL^BLES, by
Paul Hot St. Rept. on Contract Nonr- 477(08) and
Public Health Research Grant M-743(C4). Dec 59,
33p. 8 refs; AD- 233 506.
Order from LC mi$3. 00, ph$6. 30 PB 152 167
The problem of determining linear funaions for 2
sets of variables so as to maximize the correlation
between the 2 functions has been solved by Hotelling
(Biometrlka 28:321-377, 1936). A more efficient com-
putational solution is presented for the case of 2 sets
of variables. A generalized solution for any number of
aeta ia also presented. Applications are discussed,
and a numerical example is Included to demonstrate
the solution for more than 2 sets. (Author)
lis
Washington U. , Seattle. Div. of Counseling and
Testing Services.
AN IBM TYPE 650 PROGRAM FOR TRANSFORMING
A CORRELATION MATRIX TO BE ORTHOGONAL
' TO A NORMALIZED VECTOR, by George R. Burket.
Rept. on Contraa Nonr -477(08) and PubUc Health Re-
learch Grant M-743(C4). Feb 60, 7p. 2 refs.
Order from LC mil 1.80, ph$ 1.80 PB 148 608
Washington U., Seattle. Div. of Counseling and
Testing Services.
A MODIFIED IBM TYPE 650 PROGRAM FOR A
NON-SYMMETRIC CORRELATION MATRIX WFTH
SUMMED QUANTrriES, by August Dvorak, Calvin E.
Wright, and George R. Burket. Rept. on Contract
Nonr-477(08) and PubUc Health Research Grant
M-743(C4). Feb 60, lip. 4 refs. AD- 236 861.
Order from LC mi$2,40, ph$3.30 PB 147 643
This program is a further modification of the non-
iymmetric correlation matrix programs reported
previously by Dvorak & Wright (Technicaf Report,
Nonr-477(08) University of Washington, AD- 161 904,
AD- 236 861). The essential new feature is the option
gf punching the sums, sums of squares and sums of
cross products in a form which can later be added or
wbtraaed, as well as reloaded, without additional
DM Type 533 panel wiring. By means of control cards,
the following operations may be performed in any
sequence: read case cards, punch summed quantities,
«dd summed quantities, subtract summed quantities.
Any sequence of operations must begin with the reading
of a header card, and will normally end with the
punching of means, standard deviations, and correla-
tknu. Wiring and operator's instructions are included.
(Atfhor)
Wayne State U. , Detroit, Mich.
TABLES USEFUL FOR THE SELECTION OF LIFE
TEST ACCEPTANCE SAMPLING PLANS, by Benjamin
Bpstein. Technical rept. no. 3 on Contraa
Manr-2475(00X 1 June 59, 62p. 2 refs.
Order from LC ml$3. 90, ph$IO. 80 PB 148 719
Computing Devices
Air Force Cambridge Research Center, Bedford,
JENNY: AN IMPROVED HOMEOSTAT, by George G.
Hsroules and Paul F. Haire. Apr 60. 31p. 10 refs.
APCRC-TN-60-379.
(Wer from LC mi>3. 00, ph$6. 30 PB 152 202
Ai improved and enlarged nxxlel of Ashby's homeosut
i* described, in which conventional 60-cycle electro-
necfaanical analog computer techniques are used in-
•ttid of the original dc techniques, the numlier of ele-
■■u available as main variables is increased from
fcw to sixteen, and provisions ijre made for electrical
•wwatod (dau) inputs and main variable outputs. Ap-
PH'^tiona for an experimenul program in adaptive
" are mentioned. (Author)
Bolt , Beranek and Newnwn , Inc . , Cambridge , Mass .
COMPUTATIONAL CHAINS, by Thomas Marill and
T. G. Evans. Scientific rept. no. 1 on Contract
AF 19(604)7290. 21 Oct 60, 26p. Rept. no. 778;
AFCRL-TN-60-1110.
Order from LC mi$2.70, ph$4.80 PB 152 519
A formalism is developed within which questions re-
lating to the efficiency of information- manipulative
processes may be studied. An example of the applica-
tion of this -theory to the simplification of a computer
program is giren. The direction of future work Is indi-
cated. (Author)
California U. , Los Angeles.
INVECTIGATIONS IN DIGITAL TECHNOLOGY RE-
SEARCH, by G. Estrin, C. Leonides and others.
Annual summary rept. on Contract Nonr-233(52).
May 59, 186p. 13 refs. Dept. of Engineering rept.
60-25.
Order from LC mi$8.40, ph$28.80 PB 152 213
Physical studies were mainly related to the theory of
ferromagnetism and the behavior of ferromagnetic
devices used for switching and storage. The program
was divided into three parts* The measurement of
properties of magrnetic materials as a funaion of tem-
perature; the measurement of magnetic properties of
thin films; the system evaluation and experimental in-
vestigation of a modified form of the BTL Twisior.
These particular problems were chosen because of
both specific questions oi immediate interest and their
long term value in establishing familiarity with the
behavior of ferromagnetic elements and their meas-
urement. All three programs are still in process.
During the latter part of the year a literature study
related to parametric oscillation was also initiated.
(Author)
Electrical Engineering Research Lab. , U. of
Illinois, Urbana.
THE REAUZATION OF BIOLOGICAL COMPUTERS,
by H. Von Foerster. Quarterly progress rept. no. 5,
15 Jan- 15 Apr 59 on Contract Nonr- 1834(21).
15 Apr 59, 28p. AD- 220 006.
Order from LC mi$2. 70, ph$4. 80 , PB 148 290
Contents:
Topology of neural nets: Reliability
General elementary component: General neuron
The Bulbar Plexus
Comments on the logical and mechanical charaaer of
elements in a self organizing system: Abstract
model; Detailed specifications; Self recognition;
Inhibitory^ control; The set of elements; Signal net-
work; Connection matrix; Energetic struaure
An allegory for excitable tissue
Institute for System Research, U. of Chicago, 111.
TEST OF A MODEL DYNAMIC SYSTEM SYNTHE-
SIZER, by R. C. Mikulich, ed. Rept. on Contraa
AF 33(616)2797. Feb 58, 175p. 7 refs. WAIX: Tecii-
nical rept. 57-623.
Order from OTS $3. 00 PB 171 144
A mathematical (as oppose to engineering) test pro-
gram, conduaed in conjunction with a program to de-
189
sign and develop performance tests for continuous com-
fxtters and involving unique tests, was effected to test
an experimental Eighteen -amplifier analog computer
developed by the iRadio Corporation of America. This
report is an acctljnt at that test program and includes
a comprehenslveTanalysls at the components, a full
account of the sygtem tests, a discussion of individual
system and results, and a presentation d operational
aspects. The thaoretical basis for this program can be
found in PB 171 QBO. (Author) ,
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
COMPRESSION AND CODING, by Edwin Weiss. Rept.
on Contract AF <9(604)7400. 11 Oct 60. 3p. 55 G-0028.
Order from LC |m$l. 80, ph$l. 80 PB 152 638
The conclusion
schemes is the
codes.
ife that the search for data compression
same as a search for error- correcting
Lincoln Lab . . ^toss . Inst . of Tech . , Lexington .
ERRORS IN DATA TRANSMISSION SYSTEMS, by
R. G. Eniicknap. Rept. on Contract AF 19(604)7400.
29 Sep 60, 17p. 4 refs . Rept. no. 25G-0020.
Order from LC |ni$2.40. ph$3.30 PB 152 465
The program of nieasurements can be conveniently di-
vided into two rxj^in areas: one. the recording and analy-
sis of errors in channels used for digital dau trans-
mission: and twA, the recording and analysis of dis-
turbances in cir:uits of the type used for dau trans-
mission. (Author)
Lincoln Lab. . Mass. Inst, of Tech. , Lexington.
INERTL^L SEL iCTION FOR MAGNETIC CORE
LOGIC, by Rog4r H. Tancrell. Rept. on Contract
AF 19(604)7400.1 11 Oct 60. 29p. 11 refs. 52 G-0014.
Order from LC km$2. 70, ph$4. 80 PB 152 637
With the Inertul Selection scheme logical functions can
be performed bf connecting toroidal ferrlte cores to-
gether with single turn windings only. A "flux gain"
feature is ther^y obtained which allows more flux to
be switched intci a receiving core than la received
there from a transmitting core. To achieve these char-
acteristics, thei Inenial Selection scheme utilizes two
thresholds of Idw coercive force ferrite cores. It also
uses the property that one of these thresholds can be
changed by eledtrlcal means. In this repon detailed
discussions ard given of the factors involved in under-
standing these uiagnetic characteristics and their uti-
lization in logic^ applications. (Author)
Lincoln Lab. .'Mass. Inst, of Tech. , Lexington.
INFORMATIWi PROCESSING. Quarterly progress
rept. , Dlv. 5, i Mar-31 May 60. on Cortraa
AF 19(604)5200; 15June 60. 56p. 16 refs. AFCCDD-
TN-60-1013; Ap-242 284.
Order from LC|ml$3. 60. ph$9. 30 PB 150 602
Contents: computer development, magnetic flfrn engi-
neering. Information processes, character recogni-
tion, current -operated logic circuits, magnetic-core
appUcatioos. c^puter program for Morse automatic
decoding (MAUDE), magnetic materials, magnetic
films, semiconductor components, MAUDE, learning,
linguistic studies, transient queues with finite storage
on a system of integrodifferentlal equations occurring
in reactor dynamics 1 1 . sequences and residue class
rings, some further properties of Bose-Chaudhuri
codes, on decoding linear error correcting codes.
man-machine communications, human information
processing
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
LOGICAL DESIGN OF CG24 (A GENERAL -PURPOSE
COMPUTER) by G. P. Dlnneen. J. A. CXimanlan and
others. Rept. on Contract AF 19(122)458. 15 Apr 57.
47p. Technical rept. no. 139; AD- 147 496.
Order from LC mU 3. 30, ph$7. 80 PB 148 281
A detailed design is presented for a high-speed
general -purpose digital computer. The design con-
siderations are governed by the assumption that im-
plementation of the machine is to be accomplished
using only solid state devices. Sections I through V
describe the essential characteristics, structure and
method of design of the computer. Sections VI through
IX discuss its detailed logical structure. (Author)
Lincoln Lab.. Mass. Inst, of 1>ch.. Lexington.
THE TX-2 ELECTROCTATIC DISK^Y SYSTEM, by
R. E. Savell. Rept. on Contract >Cf 19(604)5200.
22 Aug 60. iSp. 1 refs. Rept. nof. 51G-0016.
Order from LC mi$2.70, ph$4.8JL ^ 152 468
The display Is produced In a 7- inch square on the face
of an electrostatically deflected cathode- ray tube. Ta
bits are used in each axis to address the location of the
spot to be displayed. The bits are decoded to produce
the deflection voltages . and after a 7- microsecond $«-
Lip time, the spot is intensified for 10 , 20 , 40 or 80 mi-
croseconds according to Instructions received from the
computer . At present . no focus correction is used wW
the system; the output of the focus -correction amphfier
is tied to ground. Work is In progress on a focus -cor-
rection circuit and on modifications to improve decoder
stability. The display Is used for visual observation,
photographic observation using Polaroid. 16- mm or
35- mm cameras . or photoelectric observation. In the
photoelectric application . a photodiode mounted in a
"light pen" is used to sense the display output . The
light pen output can then be used to modify the computer
program. This system has also been used as a flying-
spot scanner, with a photomultiplier replacing the
light pen, to provide photographic and character- recog-
nition Inputs to TX-2. (Author)
UncolnLab., Mass. Inst, at Tech., Lexington.
WALLOPS ISLAND PRELIMINARY PROCESSING
COMPUTER PROGRAM, by S. M. Omsteln. Rept. os
Contract AF 19(604H559. 25 July 60, supersedes
same of 13 Jan 60, 25p. 21 G-0003. AD- 243 045.
Order from LC ml$2. 70, phJ4. 80 PB 150 795
Lockheed Aircraft Orp. . Sunnyvale, Calif.
A SELF -ORGANIZING BINARY SYSTEM, by
R. Mattson. Technical rept. Sep 59. 30p. 4 refs.
LMSD-288029; AD- 227 943.
Order from LC ml$2. 70, phM- 80 PB 149 652
190
A precise model for an adjustable logical device and a
ooorergent iterative adjustment procedure is presented
■ad analyzed. Four demonstrations are given to syn-
diesize optimum logical functions for pattern -recog-
■mon problems containing from 25 to 216 binary vari-
abiea. These problems were simulated on the IBM
704 computer, and each problem required less than 2
minutes erf computer time to synthesize an optimum
truth function for the process considered. (Author)
Moore School of Elearical Engineering, u. of
Pennsylvania, Philadelphia.
MULTIPLE TASK STUDY ON AUTOMATIC DATA
PROCESSING, by R. O. Lucler, H. J. Gray. Jr. and
others. Quarterly progress rept. no. 2. 1 Jan-
30 Mar 60. on Contraa DA 36-039-8C-75047.
31 Mar 60. 71p. 2 refs. AD60URI; AD- 239 954.
Order from LC ml$4. 50. ph$12. 30 PB 152 989
This report released for sale to the public 29 Nov 60.
Ab account of the Increasing difficulty of obtaining
programmers, and the problems expected to arise In
diis field are stated. The model for the nerve cell
oooatruction is discussed on a sounder basis. Ex-
tended machine programming is continued, with
emphasis on the control of sequences by the allocation
interpreter. (Author)
Nival Ordnance Test Station, China I^ke, Calif.
DATA HANDLING FOR A RESEARCH AND DE-
VELOPMENTAL STATIC TEST STAND, by Thomas
Wong. 15 Aug 60, 8p. NOTS TP-2527; NAVWEPS rept.
7103.
Order from LCmi$l. 80, ph$l. 80 PB 152 345
Ibis paper describes a data acquisition system for a
static test complex. The system can measure phe-
aoRiena from rocket motors having an ^erage thrust
of 1, 000, 000 pounds and a peak thrust ^ 10, 000. 000
poinds. The data measurement capacity is 200 channels,
■flje test complex is designed to be a research and de-
velopmental toohTather than a production-testing
facility, with emphasis on flexibility in accommodating
new test program together with ease and minimum cost
of operation. As such a tool, it is used to test new
components and methods and to advance the state of the
•rt. Discussion is concentrated on the technique of
data handling art* measurements, real time digitlzationr.
•tfomatic calibration and stored program data control,
hduded is a description of a new sampling technique
for oommutating multiple data channels. The samplii^
fonnat is programable and can be altered during a test
•ccordlng to existing conditions. (Author)
Washington U. , Seattle. Div. of Counseling and
Testing Services.
CONVERTING BETA TO fe WEIGHTS ON THEIBM
TYPE 650, by August Dvorak and Clifford E. Luime-
Iwrg. Rept. on Contract Nonr -477(08) and Public Health
Re«earch Grant M-743(C4). July 59, 6p. 5 refs.
AD- 229 939.
(Wer from LCmlSl. 80, ph$ 1.80 PB 148 735
This program is designed to scale sundard p-predic-
^ weights by appropriate mean and variance estl-
n>«e8, thus generating prediction weights (b. weights)
suitable for employment with unstandardized predictor
observations. The method was specialized to provide
the derived weights in a form suitable to be employed
with the grade prediction program. (Author)
Washington U. , Seattle. Dlv. of Counseling and
Testing Services.
AN IBM TYPE 650 PRCXJRAM TO FACILITATE
OBTAINING SCATTERGRAMS, by George R. Burket.
Rept. on Contract Nonr-477(08) and Public Health Re--
search Grant M-743(C4). July 59, 3p. 1 ref.
AD- 227 919,
Order from LC mi$l. 80, ph$l. 80 PB 148 734
Washington U. , Seattle. EMv. of Counseling and
Testing Services. ,
A METHOD FOR COMPUTING RATING SCALE
ITEM STATISTICS ON THE IBM TYPE 650, by
Mary Marjorie Campbell. Rept. on Contract
Nonr -477(08) and Public Health Research Grant
M-743(C4). July 59, 4p. 1 ref. AD- 227 920.
Order from LC mi$l. 80, phjl. 80 PB 148 733
A modification was made of a fixed-point matrix
multiplication routine designed to meet the problem erf
computing rating scale item statistics with a large
number of items. Given frequency data, the program
may be used to obtain item means, variances, stand-
ard deviations, sums, sums of squares, and sums of
higher powers. Item sums are restricted to a maxi-
mum value erf 999, 999 and not more than 9, 999 cases
may be processed per item. There is no restriction
on the number of Items. The program performs
matrix multiplication augmented by processes for
computing means and measures of variability.
(Author) (See also re 148 734)
Washington U., Seattle. Div. of Counseling and
Testing Services.
MULTIPLE REGRESSION ANALYSES PROGRAM FOR
THE IBM TYPE 650, by Calvin E. Wright. Rept. on
Contraa Nonr-477(08) and Public Health Research
Gram M-743(C4). July 59, 8p. 3 refs.
Order from LC mi$1.80, ph$1.80 PB 148 732
The program computes P matrices and multiple corre-
lations according to the following matrix equations: (1)
rmmTtnm *Pmm and (2) PnmTmn =Rnn. where rmm
represents the Intercorrelation matrix of predictor
variables, Tmn a matrix erf the cxtrrelatlons erf the m
predictor variables with the n criterion variables, pmn
the m by n matrix of regressiem weights, and Rnn a
matrix whose diagemal elements are the squares of the
multiple correlations erf the predictor variables with
the criterion variables. The closeness of the inverse
involved can optionally be checked by computing the
Identity matrix. The program is restricted to m, the
number erf predictor variables, equal to or less than 38
and n, the number erf criteriexi variables, equal to or
less than 50 with the further restriction that the prcxluct
mn be less than 1600. The Input and e>utput with the
exception of the Inverse are In fixed point form, but the
computations are performed in stanelard 8 -digit fle>ating
point. Provisions were ma^ie so that the outputs of the
symmetric and non- symmetric correlation matrix
programs (AD- 204 459) may serve as input. (Author)
191
MECHANICS
Applied Mathcn^tics and Statistics Labs. . Stanford
U. . Calif.
ESTIMATES AT
EQUATIONS OF
INFINITY FOR SOLUTIONS OF THE
VISCOUS INCOMPRESSIBLE FLUID
FLOW, by Robetft Finn. Technical rept. no. 84 on
Contract Nonr- 245(11). 7 Dec 59, 56p. 8 refs;
AD- 230 254. i
Order from LC iii$3. 60. ph$9. 30 PB 152 163
Asymptotic properties of time- independent solutions
are presented of !the Navler-Stokes partial differential
equations, which are defined in a neighborhood ^of
infinity in 3 dimAisional Euclidean space, and which
have the propert; that the velocity vector w(jt) tends
continuously to a
(XI. X.
X3).
limit vector w^asi
(Ai ithor)
Providence.
Brown U. Div. of Applied Mathematics.
ON THE INTEGRATION OF THE EQUATIONS OF
MOTION IN THfe CLASSICAL THEORY OF ELAS-
TICITY, by Eli itemberg^ Technical rept. no. 7 on
Contract Nonr-5e2(25). ]«y 59. 31p. 33 refs.
562(25)/7; AD-2t5 548. ^ ^^
Orxler from LC ^i$3. 00. ph$6. 30 PB 148 725
1
The theory of integration is considered for the dis-
placement-equartons of motion in the linear theory of
homogeneous ani isotropic elastic solids. These eqMa
tions,
are of the^form:VTJ "♦"-
1 „^„ Pd\
-21^ u dtT
where u(x. t) is ^ displacement vector; x the triplet
of rectangular cartesian coordinates (xi. X2>iE3)* ' ^**
time; the conata^its /o, ^ and j>' designate the mass
density, the she#r modulus, and Poisson's ratio, re-
spectively; and V is the usual del -operator. (Author)
T
Duke U. [Durham. N. C.J _
BOUSSINESQ S fROBLEM FOR A HEATED PUNCH.
I. GENERAL THEORY, by D. L. George and Ian N.
Sneddon. Rept. ion Contraa AF 18(600)1341. Aug 60.
I6p. 10 refs. At^OSR-TN-60-1047; AD-243 145.
Order from LC mi$2. 40. ph$3. 30 PB 152 069
I
This paper is concerned with the problem c* deter-
mining the stresses in a semi-infinite elastic body
when the rigid punch is a solid of revolution which is
heated and so ptoduces a non-uniform distribution d
temperature on |the free surface of the solid.
oi.
Harvard U. D<v. of Engineering and Applied Physics.
Cambridge, Mass
TRANSIENT INTERACTION OF AN ACOUSTIC
WAVE WITH A; CTRCULAR CYLINDRICAL ELASTIC
SHELL, by Rot*rt G- Payton. Technical repc. on Con-
tract Nonr-186< (20). July 59. 27p. 7 refs.
Oixler from LC|mI$2. 70. ph»4. 80 PB 149 627
A cylindrical elastic shell submerged in an acoustic
fluid is subjected to a plane pressure pulse. Exact ex-
pressions are ft>und for the subsequent shell nrKition in
the form of a d<^le integral by the use of integral
transform techniques These integrals are then evalu-
ated asymptotically for small lime to determine the
initial shell behavi-r after impact. (Author)
Institute of Mathematical Sciences , New York U. ,
N. Y.
FINAL REPORT. Rept. on Contract AF 49(638)446.
Aug 60. 7p. 6 refs. IMM-NYU 272: AFOSR-TR-60-93.
OrderfromLCmi$1.80, ph$l.80 PB 152 445
Summary of work on: propagation of shock waves
through non- uniform regions; structure of magnetohy-
drodynamic shock waves; three- shock intersection;
boundary -layer transition to turbulence; solar spicule*
secondary shocks within spherical and cylindrical
blasts .
Lockheed Aircraft Corp. . Sunnyvale, Calif.
STRESSES IN THE ADHESIVE OF A TWO-LAYERED
ROTATIONALLY SYMMETRIC HEATED ELASTIC
SHELL. byH. L. Langhaar and E. V. Pittner. Tech-
nical rept. on Flight Sciences. Dec 59. 98p. 3 refs.
LMSD-480391; AD-234 278.
Order from LC mi$5. 40, ph$15. 30 PB 148 298
A two-layered shell of revolution is considered to be
subjected to axially symmetric loads and thermal gra-
dients. The Uycrs may taper in thickness, and they
n>ay consist of different materials. Various edge con-
ditions are admitted. The linear theory of elasticity
is used.
Rensselaer Polytechnic Inst. , Troy, N. Y.
STATI^ICAL BIFURCATION OF FRICTION, by
F F. Ung and R. S. Weiner. Technical note no. 5 on*
Welding Aspect of Sliding Friction between Metallic f
Surfaces, Contract A F 49(638)67. 10 Jan 60, 27p^
13 refs. AFOSR TN-60-207; AD-234 296.
Order from LC mi$2.70. ph$4.80 PB 148 674
A description is presented in modified form of an
apparatus used earUer for measuring adhesion, pure-
shear and friction; the modification made it possible to
extend the range of normal load so that the so-called
extreme pressures are reached. The result of a lar|B
number of tests shows a statistical bifurcation of frk-
tlonal resistance for lead on lead. Below extreme prer
sures there are two branches of the coefficient of fric-
tion normal load relationship. The nature of the upper
branch of the coefficient of friction vs. normal load
relationship is explicable in terms of the weld-Junctifli
theory exclusively.
University of Southern California . Engineering
Center , Los Angeles .
LOW -SPEED PLANE COUETTE FLOW OF A RARE-
FIED CONDUCTING GAS IN A UNIFORM TRANS-
VERSE MAGNETIC FIELD, by Hsun-Tiao Yang. lU^-
on Contract AF 18(603)95. Aug 60 . 30p . 6 ref s .
USCEC rept. 56-218; AFOSR TN- 60- 1002.
Order from LC ml$2.70, ph$4.80 PB 152 ?»
The newly developed nvament equations and boundary
conditions for magnetogasdynamlcs are applied to low-
speed plane Couette flow of a rarefied conducting ga» ■
192
a uniform transverse magnetic field. The purpose is to
demonstrate the feasibility of the new system and to
pim i«der»t«nding of the effect of rarefaction on mag-
afltofasdynamlcs of Couette flow . The tai^entlal flow
4|uandtief like velocity, shear stress , and tangential
htat flux can be solved separately frqm the normal
^Matltlet like pressure, temperature (density), norma)
lUWMl, and normal heat flux.
Tlimiyntial quantities are greatly influenced by the
timsverse magnetic field, while there is llnle or no
effect of the magnetic field on the normal quantities .
The explicit expressions for ungential as well as nor-
mal quantities are obtained. I
Aerodynamics and Pneumatics
Arnold Engineering Development Center [Tullahoma,
Tenn.l
EFFECTS OP UNIT REYNOLDS NUMBER, NOSE
BLUNTNESS, AND ROUGHNESS ON BOUJ4DARY
UYER TRANSITION, by J. Leith Potter and Jack D.
Whitfield. Rept. on ARO, Inc., Contract AF 40(600)800
Mar 60, 81 p. 37 refs. AEDC-TR-60-5; AD-234 478.
(Merfrcm LCmD4.80, ph$13.80 PB 147 878
PWaora affecting transition and the effects of unit
Iqraolds number and very small degrees of leading
adi^ bluntness are discussed in detail. A means of
estimating the effect of roughness on boundary layer
transition is suggested. (Author)
Amoid Engineering Development Center [Tullahoma,
Tenn. ]
AN INVESTIGATION^ OP THE BOUNDARY-LAYER
CHARACTERISTICS IN THE TEST SECTIC»4 OF A
« BY 40-INCH SUPERSONIC TUNNEL, by Jerry
Jonea. Rept. on ARO, Inc. Contraa AF 40(600)800
S/A 11(60-110). Oct 60, 20p. 4 refs. AEDC-TN-
60-189.
Order from LC mi$2. 40, ph$3. 30 PB 152 758
A le« program was conducted to investigate the bound -
try-layer characteristics of the von Karman Gas Dy-
■mics Facility's 40 by 40-in. , continuous, supersonic
•Ind ninnel (Tunnel A). The program was divided into
two parts: (1) A survey of the boundary layer at one
KHioa at the center of the flexible nozzle plate (curved
mU) and (2) a survey at one sution at the center of the
' aidewall. Results of the investigation at Mach
trs from 1. S to 5. 5 in half Mach number incre-
I are presented in the form of boundary -layer
total thicknens. displacement thickness, and momen-
OiBn thickness over a Reynolds number range of 1. 0-x
10Pto6. 5 X 10^ per foot. For the minimum Reynolds
■■b^. the boundary -layer displacement thickness is
PMIBT 00 the aidewall than on the flexible nocEzle plate
■ all Mich ibmbers, whereas at maximum Reynolds
■nbers the displacement thicknesses are essentially
*e same. The measured diaplacentent thicknesses on
ifctflmMe noBzle plate and sidewall showed good
yuuuieu with theory when the turbulent skin friction
WrfBcients were evaluated from Reynolds numbers
kand on wall density and kinematic visooaity. Theo-
f**cyl estimates of the displacement thicknesses de-
*^'**»^> by using Reynolds numbers baaed on free-
■■■Bi denalty and kinematic viscosity were cunslat-
•tiy higher than the experimenul values. (Author)
193
Arnold Engineering Development Center [Tlillahoma]
Tfenn.
FLOW PROPERTIES OF AN UNYAWED 10- DEC
CONE FOR Y -1. 28 TO 1. 40 AT MACH NUMBERS OF
1.5 TO 8. by W. T. SIrike, Jr. and B. R htorton. Jr.
Rept. on ARO, Inc. Contract AF 40(600)800,
S/A 11(60-110). October 60, 81p. 2 refs.AEDC-
TN-60-178.
Or^r from LC ml$4. 80, ph$13. 80 PB 152 260
Numerical solutions for a nonlinear differential equa-
tion proposed by G. L Taylor and J. W. Maccollto
describe the flow about a cone were carried out on an
I^ 704 high speed computer for variable ratios of
specific heats. The solutions were obtained for an un-
yawed 10-deg semi-angle cone at Y«i. 40, 1.36, 1.32,
and 1. 28 at Mach numbers within die raiwe of 1. 5 to
8.24. (Author)
Arnold Engineering Development Center [Tullahoma
Tenn. ]
A PROTOTYPE HK31 SPEED DIGITAL SYSTEM FOR
HOTSHOT TUNNELS, by a E. GiUey and
M. L. Bunn, Jr. Rept. on ARO, Inc. , Contract
AF 40(600)800 S/A 11(60-110). Oct 60, 45p. 2 refs.
AEDC-TN-60-177.
Order from LC mi$3. 30. ph$7. 80 PB 152 555
A prototype high speed digital system has been built
and tested in two of the arc-discharge wind tunnels at
the von Karman Gas Dynamics Facility, AEIX:. The
system is used In conjunction with a carrier- amplifier
and recording oscillograph system to obtain digital
data in parallel with the analog data. Numerical trans-
formation of the analog signals is acconqilished by us-
ing a high speed electronic commutator to switch the
signals into an analog- to-digital converter. The digi-
tal data are stored at high speed in a magnetic core
storage and at a later time transferred to paper tape.
The purpose of the digital system is to obtain a large
amount of raw data in a form compatible for reduction
with digital conputers. (Author)
Arnold Engineering Development Center [Tullahoma,
Tenn.]
TESTS ON STING-SUPPORT INTERFERENCE CON-
DUCTED IN THE TRANSONIC MODEL TUNNEL.
PHASE I, by Bruce B. Estabrooks. (ARO, Inc.).
Jan 55, declassified 25 July 58. 59p. 1 ref. AEDC-
TN-54-28.
Order from LC ml$3.60, pfa$9.30 PB 153 379
This report released for sale to the public 15 Dec 60.
An experimental development program was conducted
in the Transonic Model Tunnel (TMT) on a 1/16-scale
model of the Transonic Circuit of the Propulsion Wind
Tunnel (PWT) sting-support system, including several
wall modifications. Results of the tests indicate that
when perforated walls were installed on the four walls
of the tunnel, disturbances were not propagated up-
stream from the support strut into the test region in
the Mach number range from M *1 to M > 1 . 2. The
utiUzation of solid-wall modifications (bulges which
increase the cross- sectional area) in the vicinity of
the suppcHt strut reduced the auxiliary mass-flow re-
quirements to values somewhat less than the values
required for the tunnel configuration having no support
I
strut or wall mcilificationB . The forward-deep wall
modificatian api:^eared to have the most favorable
cemerline Mach: number distribution and auxiliary
mass-flow characteristics.
1.
Avco- Everett |lesearch Lab. , Mass.
LOW- DENSITY ISHOCK TUBE FOR CHEMICAL KINE-
TIC STUDIES. |y Shao-Chi Lin and Walter L Fyfe.
Rept. on Contract AF 04(647)278. July 60, 39p. 32 refs.
Research rept. pl; AFBMD TR-60-183.
Order from LC \m%^ 00. ph|6. 30 PB 152 426
,L
Some problems fconcerning the extension of high temper-
ature shock tuba experiments to low gas densities are
discussed. Speqific examples are cited on the operation
and actual perfotmance of.a 24" diameter shock tube
that has been co*istructed for chemical kinetic studies
at gas densltieslin the neigfeorhood of lO'^ normal at-
mosphere (i. e. . about 80 km simulated altitude). Some
preliminary results on the dissociation and ionization
rates, as well as the visible radiation profile, behind
strong normal ^ocks in air (12 < Mg ^ 22) at these
low densities aie presented.
Avco [Evereal Research Lab. [Mass. ]
RADIATIVE TRANSPORT WITHIN AN ABLATING
BODY, by Leo f. Kadanoff. Rept. on Contraa
AF 04(645)18. Oct 58. 33p. 5 refs. Research rept. 37;
AD- 205 517. I
Order from LC|mi$3.00. ph$6.30 PB 148 720
The emission abd reabsorption of thermal radiation
within a semitrpnsparent material provides a mecha-
nism which supjplements ordinary thermal conduction in
transporting enfergy from hotter to colder regions. A
method has beeii developed for the calculation of net
radiative flux a^ temperature distribution within a
semi-infinite bixJy which emits, absorbs, and scatters
this radiation a^Ki which allaws some radiation to
escape from it4 surface. This method has been applied
to the problem pf calculating temperature distributions
within bodies ill steady state ablation.
Brown U. Div. of Engineering, Providence, R. I.
ON TRANSONIC FLOW ABOUT TWO PARALLEL
BODIES OF REVOLUTION, by Eric J. Softley. Repc.
on Contraa AP 49(638)444 May 60. 63p. 7 refs.
Technical rept, WT-33; AFOSR TN-60-706.
OrderfromLdmiS3.90, ph$10.80 PB 152 413
Potential theor|, based on linearization o* the transonic
flow equation. Is applied to the case o( two slender
bodies of revolution, situated with parallel axes and
within a regionj where Interference effects cannot be
neglected. Thd forces on the bodies are discussed and
as an example }he drag of one body is computed and
compared with experimental results ofacained by
G. Drougge. (Author)
Institute of A^rophysics, U. of Toronto (Canada).
PRESSURE MBASUREMENTS IN FREE MOLECULE
FLOW WITH A ROTATING ARM APPARATUS, by
E. P. Mumz. Hept. on Contract AF [18X600)1185.
May 58, 57p. U refs. UTIA Tochniaa note 22;
AFOSR TN-58''904; AD- 204 431.
Order from LG mi$3. 60, ph$9. 30 PB 148 494
Ia rotating arm apparatus has been developed and usod
to measure the impact pressures of orifice and long
tube type pressure probes in the free molecule flow
regime. Usii* this equipment, the validity for low
speed ratios of a theory due to Harris and Patterson
for the pressure rise in long tube free molecule im-
pact probes has been established. An approximate
short tube theory is also presented and its application
to the geometrical conditions necessary to provide an
effective true orifice is discussed, (Author)
Johns Hopkins U. [Baltimore, Md. ]
DIRECTIONAL SENSITIVITY FOR A FINITE HOT-
WIRE ANEMOMETER, by S. Corrsin. Rept. on
Contract AF 49(638)248. [I960] 14p. 6 refs. AFOSR
TN-60-171; AD- 234 946.
Order from LC mi$2. 40. ph$3. 30 PB 148 677
For an infinite heated cylinder oblique to a uniform
flow, it follows from the equations of motion that the
total heat loss rate depends only on the normal com-
ponent of undisturbed velocity. This corresponds to
the cosine law of cboUng. When the cylinder is of fi-
nite length, with ends maintained at ambient fluid tem-
perature, departures occur which Increase with the
relative heat loss rate to the ends. (Author)
Lockheed Aircraft Corp. , Sunnyvale. Calif.
ON MASS TRANSFER AND SHOCK- GENERATED
VORTICITY. PART 1: AXISYMMETRIC FLOW, by
H. Hoshizaki. Technical note. 22 May 59, 40p. 12 refs.
LMSD- 49721.
Order from LC mi$3. 00, ph$6. 30 PB 148 701
The effects of shock- generated vonlcity and mass-
transfer on stagnation-point heat transfer rates are In-
vestlgated. The complete Incompressible Navier-
Stokes equations are considered In the flow region be-
tween the bow shock and the surface of spheres and
cylinders. Boundary conditions are applied immedi-
ately behind the shock and at the wall The numerical
solutions to the flow equations for the sphere, with
air Injection Into the shock layer, show that the Inter-
action between the vortlclty generated by the wall and
by the curved shock reduces the effectiveness of m*««
transfer cooling.
Lockheed Aircraft Corp. , Sunnyvale, t::alif.
ON MASS TRANSFER AND SHOCK- GENERATED
VORTICITY. PART 2: CYLINDRICAL FLOW, by
H. Hoshizaki. Technical note. Nov 59, 35p. 8 refs.
LMSD- 288075; AI>229 046.
Order from LC mi$3. 00, ph$6. 30 PB 148 702
The effecu of shock- generated vortlclty and mass-
transfer on stagnation- point heat transfer rates arelr
vestlgated. The incompressible Navier- Stokes equa-
tions are considered in the flow region between the bcw
shock and the surface of cylinders. Boundary condition!
are applied immediately behind the shock and at the
wall. Numerical solutions to the flow equations, wltli
air injection Into the shock- layer, ahow that the inter
action between the vorticity generated by the wall aad
by the curved shock reduces the effectiveness of mssr
transfer cooling. Yawing the cylinder was found to
have a relatively small effect on the increase in he«
transfer rates caused by vorticity interaction. (AuM
(See also PB 148 701).
194
u
Michigan U. , Ann Arbor.
DirrERACTION EFFECTS OF SIDE JETS ISSUING
FllClM FLAT PLATES AND CYLINDERS ALINED
UTTH A SUPERSONIC STREAM, by James L. Amick
and Paul B. Hays. Rept. on Contract AF 33(616)5946.
June 60, 72p. 9 refs. WADD Technical rept . 60-329.
Order from OTS $2.00 ^ PB 171 179
Bsperimental results are presented for side jets ■
Isauing through axisymmetric nozzles normal to flat
plates and cylindrical afterbodies. The forces due to
aide-Jet interaaion on a flat plate are found to be
iKfe, exceeding twice the jet static force in some
CMM. A simple empirical equation correlates the
interaction force on a flat plate for Mach numbers 3. 5
to 4. 5, stream-to- jet stagnation pressure ratios of
0.1 to 10, and various geometrical parameters. De-
tails of the flow structure in the interaction region are
flixalned from surface pressure measurements.
•cfaUeren pictures, and surface streamline observa-
dons. For side jets on cylinders, much of the helpjful
ioKraction force is lost. (Author)
Kfidwest Research Inst, , Kansas City, Mo.
ON THE EVALUATION OF GENERALIZED AERO-
DYNAMIC FORCES FOR TRUNGULAR WINGS WITH
SUBSCWIC LEADING EDGES, by Edmond F. E.
Zeijdel and Robert R. Blackburn. Repc. for 1 Jan-
31 Dec 59 on Contract AF 33(616)5476. Aug 60, 93p.
11 refs. ARL Technical rept. 60-298; supersedes
WADC-TN-59-1.
Order from OTS $2. 25 , PB 171 162
The work comprises a numerical method for computa- ,
tkn of the generalized aerodynamic forces for trlan-
fular wings with subsonic leading edges. Numerical
solutions developed by previous workers used a box
mednd where It is assumed that the downwash Is con-
stant throughout each box. The proposed method elim-
inates this assumption while special anention is given
to the region of the leading edge. (Author)
Laboratoire Medlterraneen de Recherches Thermo-
dynamlques (France).
PRODUCTION OF A MOLECULAR BEAM AT A
VERY HIGH SPEED AND RELATIVELY GREAT
DBNSITY. REALIZATION OF A MOLECULAR GUN,
by F. Marcel Devienne and J. Souquet. Technical note
on Contraa AF 61(052)296. June 60, 41p. AFOSR TN-
60-906.
Order from LC ihlJ3. 30, ph$7. 80 PB 152 504
The aim Is to obtain molecular beams whose intensity
esoeeds 10^8 molecules/square centimeter, per sec-
ond, with speeds ranging between 10 and 30 Km/sec-
(ad, or higher. In order to have such a molecular
beam, the charge or momentum exchange is produced
between ions and a molecular beam. The cylindrical
iailc beam is obtained by the high frequency ionization
oft molecular beam, coming from a hypersonic noz-
de. This beam passei through a quartz tube around
•Wch a coil is wound. A high frequency current flows
tbrough the coil. The ionization efficiency exceeds
lOJ. The ions are separated from the molecules by
■esne at a magnetic field generated by an elearo-
■fnet. Then, the ion beam Is accelerated and
•■Wight to the satisfaaory voltage by a linear accel-
erator and then crosses a molecular beam coming out
of another hyTjersonic nozzle. In the interaaion space
of the two beams charge or momentum exchanges are
then produced and after deflection erf ions and pumpage
of slow molecules, a beam ol high speed molecules in
the initial direalon of the ion beam is obtained. The
molecules belonging to the molecular beam are de-
tected by means of a tungsten strip heated at a rela-
tively low temperature. The speed is measured with a
special device. The measurements that must be made
by means of a high speed molecular beam, are carried
out in test chamber where a mrdel carriage is placed.
This carriage is apt to move Into two direaions. The
apparatus called "MOLECULAR GUN" has three dif-
fusion pumps and two large primary pumps and per-
mits the study of all the interaaions phenomena be-
tween a body moving at a cosmic speed, and a very
rarefied gas in free molecular flow regime. (Author)
Michigan U. Research Inst. . Ann Arbor.
ELECTRICAL METHODS OF HEATING GAS. by
Harold Early. William Lawrence and others. Rept. on
Contraas AF 18(600)763 and AF 40(600)720. Dec 58.
42p. 10 refs. AEDC TR-58-21; AD-206 691.
Order from LC mi$3. 30, ph$7. 80 PB 149 672
This report discusses the use of an elearical dis-
charge for adding thermal energy to the air in a hyper-
sonic wind tunnel. Research has been conduaed on the
use ct inductively stored energy for arc heating of the
extremely dense air used for driving the "Hotshot"
type erf transient wind tunnel. Problems of arc initia-
tion and electrode erosion were also studied. A sec-
ond objective of the research was to investigate the
feasibility of heating a supersonic air stream by means
of a rapidly pulsed corona type discharge. In demon-
stration experiments, such a discharge would deliver
approximately 15 kilowans into a subsonic air stream
at atmospheric pressure. The use of supersonic heat-
ing is apparently limited to extremely low density
tunnels.
North American Aviation, Inc. . Los Angeles, Calif.
AN ANALYTICAL STUDY OF THE DYNAMICS OF
SPINNING AIRCRAFT. PART III. CALCULATED AND
FLIGHT TEST SPIN CHARACTERISTICS OF AN
F-IOOF WITH ^TRAKES. by John H. Wykes. Rept. on
Contraa AF 33(616)5285. Feb 60, 171p. 2 refs.
WADC Technical rept. 58-381, Pi. III.
Order from OTTS $3.00 PB 171 135
This report is the third part of a study designed to ex-
plore an analytical approach in predialng spin charac-
tpristlcs and demonstrates the utility of this approach
in support of an actual flight test program Initiated to
develop a set of sprtn recovery strakes for the F-IOOF
airplane. Wind tunnel data, obuined for support of the
spin calculations, reveal that strakes cause the airplane
to become markedly unstable direaionally at angles of
attack beyond stall. Spin calculations and flight test
data are pre^nted which show that It Is this static
charaaeristic of strakes, rather than the damping
charaaeristic, which make them useful in spin recov-
eries. It is also shown that if strakes are of the fixed
type, they can influence spin entry and buildup charac-
teristics to a significant degree. TTie importance of
control sequencing during initiation of spins is explored
and shown to be a very potent influence on spin entry
195
•nd buildup. Correlations at calculated and flight test
•pin time histories indicate that the analytical tecb-
■Iques emplcyeti provided valid answers far the air -
ptane with strakes installed. A set of wing-nuxuited
rocket packages, installed as emergency recovery
devices, were lovestigated by actual (Ught test to
evaluate their irifluence on the basic airplane's spin
characteristics., Only calculated spin time histories
were used to evaluate the rockets' effectiveness in
accomplishing recoveries. Calculatioo and fUght test
results indicate the instaUation to be an excellent
emergency recovery device which does ncc unduly com-
promise basic spin characteristics. It is concluded
that an analytical program al the type described can
provide timely 9pd valuable support to spin demonstra-
tioo programs. (Author) (See also PB 151 918)
Hatre Dame Ui , Ind-
SOME CHARACtTERISnCS OF THE PERIODIC
VORTICAL ELEMENTS WITHIN THE TRANSITION-
ING BOUNDARY LAYER, by F. N. M. Brown. Repc.
on (Contract NC^d-17702l. Feb 60, 60p. 17 refs.
AD- 238 669. I
Order from LC knl$3.60, phJ9. 30 PB 148 521
An optic study of the boundary layer showing the
mechanism of tfansition in the zero gradient on tangent
ogive noeed cylinders to be the dissolution through
distortion of sp^taneously formed vortical elements
within that laye^. The frequency ct formation d the
vortical elemeris is a function at the three halves
power of air spi led. (Author)
Polytechnic In^t. of Brooklyn, N. Y.
ON THE PLK METHOD AND THE SUPERSONIC
BLUNT BODY PROBLEM, by Roberto Vaglio- Laurin.
Repc. on Contract AF 49(638)217. Aug 60, 85p.
16 refs. PIBALirept. no, 546; AFOSR TN-60-430;
AD- 243 947.
Order from LCjmi$4. 80. ph$13, 80 PB 152 245
Detailed analysts of the subsonic and transonic por-
tions of the flo^ field' about either very blunt or asym-
metric configunstions requires successive approxi-
mations; these can be carried out in a systematic
fashion only if 4n appropriate convergent perturbation
procedure is svtailable. It is shown that, with either
"direct" or "inverse" methods of analysis, a straight-
forward linearisation scheme leads to divergent series
solutions: however, the situation can be remedied by
introducing a simultaneous stretching of coordinates
in the spirit of the ft>incare-Lighthill-Kuo (PUC)
method.
Polytechnic Ink- of Brooklyn. N. Y.
ON THREE-DIMENSIONAL FREE-MIXINC, by
Martin H. Blooiti. Rept. on Contract AF 49(638)217.
Aug 6a 13p. 3|refs. PIBAL repl. no. 474; AFOSR
TN -60-986; AD- 244 103.
Order from LCimi$2. 40. ph$3. 30 PB 152 432
I
The purpose of khls note is to point out the quasi-two-
dimensional naiire of certain type* of free three -
dlmensioaal viatous flows of a quasi -parallel nature.
Theae flows ar« presumed to be descrlbable in bound-
ary layer term$ and are imbedded within flows which
are essentiaUy inviscid. In particuUr. flows of free-
wake and Jet type are considered. Flows of this char-
acter can originate, for example, from the boundary
layers or shock-layers of non-axially-symmetric
bodies or from non-axially-symmetric Jet-proAioert.
(Author) .
■1 -
Princeton U. [N. J. 1
DfVENSIONLBSS PARAMETERS FOR VISCOUS
SIMILARITY, by Andrew C Hammltt. Rept. on Coa-
tract AF 49(638)465. Dec 59. lOp. Rept. 491; AFOOl
TN-60-226; AD- 235 788.
Order from LCmi$l. 80, pK 1.80 PB 148 673
Viscous similarity of two flows can be achieved by
matching Reynolda number only if viscosity is essen-
tially constaot tHrougbout the flow. If large differences
of static temperature occur and viscosity follows a two
parameter Sutherland law. then both Reynolds number
and ratio of static temperature to Sutherland tempera-
ture must be matched. Errors of the order of faaora
of 2 or 3 in Reynolds numbers near the stagnation paiM
can occur in hypersonic flows if no attention is paid to
the second parameter. (Author)
Princeton U. , R ).
HEAT TRANSFER THROUGH A REGION OF
CLOSED- STREAMLINE, by i H. Lam. Rept. oo
Contract AF 49(638)465. May 59. 27p. 3 rrfs.
Rept. 469; AFOSR-TN-59-727.
Order from LC mi$2. 70, ph$4. 80 PB 152 739
It has been shown diat the pertinent parameter in this
class of problem is the Peclet number ^ * RePr-
Since this number conuins a characteristic length,
the solution is not invariant with respect to a scale
transformation. When A is small, the solution tends
to the simple conduction solution, which is invariant
with respect to a scale transformation. For any
y^ >0 and for any steady flow pattern, die gross heat
transfer rate through the region is always higher tbm
Qq. For small X, the increase of gross heat trans-
fer rate is proportional to A^. For large A the
gross heat transfer rate is proportional to A*/^.
Both results are for a>-0 only. Dissipation In the
region will, in general increase the heat transfer
rate through the coU boundary and decrease the heat
transfer rate through the hot boundary, (Author)
Rensselaer Polytechnic Inat.. Troy, N. Y.
RECENT ADVANCES IN NONEQUlLffiRIUM FLOW
IN GAS DYNAMICS, by Ting Yi U. Rept. on Contraa
AF 18(600)1591. May 60, 60p. 46 refa. TR AE MOl;
AFOSR-TN-60-597.
Order from LC inl$3.60. pli$9.30 PB 152 4»
The present paper consists mainly of three parts. Us
first part deals with general concepts which Include (1)
the fundamental equations and bouiidary conditions in
problems of steady adHabatic invlacid flow of a reactii|
mixture of perfect gases and (2) « feaeral study rf «1»
chemical relaxation in a faaaaua ajratem. The secoad
part deals with the steady one dimensional nozzle Ooa
with nooequilibrium chemical reactions. An importitf
nondlmensioiwl parameter la used to classify the lua*
zle flow into (1) equilibrium flow (2) nonequiUbrium
196
4.
I •->
(|o« and (3) frozen flow. Significant departure from
equilibrium flow in a hypersonic shock tunnel nozzle
vouU lead to frozen flow further downstream. The
iMrd part preaenta the results of a numerical analysis
dttte inviscid adiabatic flow of a reacting mixture of
pariect gases past a blunt body. These results show
jkat significant changes in the flow conditions of the
ibock layer region can be attributed to the chtoiical
MSSqiMlitarium effects. (Author)
•r Polytechnic Inat. . Troy, N. Y.
A STUDY OF SOME FLUID MIXING PROBLEMS, by
K. Tcba, M. Breslau. and K. T. Yen. Rept. on Con-
tna AF 49(638)2a Aug 5a 37p. 2 refs. TR AE 6003;
APOSR TN -60- 1023; AD-2B 859.
Order from LC ml$3. Oa ph)6. 30 PB 152 250
Ao analytical study of some two-dimensional fluid mix
i$g problems is carried in this report. First, the con-
dttlaw under which similar solutions exist for mixing
■der Btreamwise pressure gradients are determined,
k is shown that the two streams should have the same
ittcb numbers, and the main-flow velocity distribu-
lk»s should be of the weclge or exponential flow type.
Next, transverse pressure gradieiKs are also included
in the consideration. It is found that the free -stream
velocity distributions should also be of the wedge or
etpcneAial flow type and. in addition, the total heads
of the rwo^uid streams should be the same. Finally,
die von Karman-Pohlhausen method is used to allow
for more realistic pressure gradients. The dependence
of the interface curvature on the "injection velocity",
die pressure gradients, etc. are incUcated. (Author)
losemount Aeronautical Labs. , U. of Minnesota.
Mtaneapolis.
OBSKN. CALBRATION AND SIMULATION CAPA-
njTY OF THE ROSEMOUNT AERONAUTICAL LAB-
ORATORIES'HIGH TEMPERATURE HYPERSOIIC
PACILrrY, by Rudolph Hermann, James O. A.
Sumkevics and others. Rept. on Contracts AF
33(616)6077. AF 33(616)473 and AF 49(638)190. July 60.
4Sp. 8 refa. WADD Technical note 60-108.
Order from OTS $L 25 FB 171 142
This report describes the high temperature hypersonic
(acllity of the Rosemount Aeronautical Laboratories.
IMrersity of Minnesota. The discussioif of failures,
kafirovements and additions to the facility outlines the
piugress through the years since original construction.
Pferformance graphs for the faciliiy are included as
sell as a discussion of related iitstrumentation and
epical equipment. The facility presently operates with
1 12 in. by 12 in. test section at Mach number 7. with
■lapatloa pressures from 50 psia to 150 psia and
stagnation temperatures from lOOO'^R to 3000°R. Po-
leatial development of the facility is suggested in the
performance curves and discussed in the conclusions.
(AMhor)
f
Southwest Research Inst. . San Antonio. Tex.
CHEEP COLLAPSE OF LONG CYLINCMIICAL
SHELLS UNDER HIGH TEMPERATURE AND EX-
TERNAL PRESSURE, by Thein Wah and R. K. Gregtn-y.
Kept, for 14 Apr 58-15 Mar 60 on Contract
AF 33(616)5727. Aug 60. 126p. 37 refs. WAIX) Tech-
Hcalrept. 60-230.
Otoder from OTS |2.75 FB 171 152
This report presents theoretical and experimental
work on the creep collapse of long cylindrical shells
subjected to a uniform external pressure and high
temperature (300°-500^). In addition it presents the
results of several tests to determine the creep prop-
erties of aluminum alloy 3003-H14 and also a fairly
comprehensive survey of existing engineering theories
of creep. Fair agreement between theoretical predic-
tions and test results was observed. (Author)
Technische Hochschule. Munich (West Germany).
NUMERICAL INVESTIGATIONS ON THE SOLUTION
OF THE NON-UNEAR EQUATION OF SUPERSONIC
FLOW BY FINITE DIFFERENCE METHODS (PART
II) by Gerhard Seegmllller. Technical note no. 1 on
Contract AF 61(052)377. 25 July 60. 29p. 2 refs,
AFOSR TN-60-1141.
Order from LC mi$2.70. ph$4.80 PB 152 492
Part II contains a proof of a theorem which estabUshes
the local existeiK:e and uniqueness of the solution of
the difference equations resulting from a mean-value
approximation and secures the convergence of a cer-
tain Newton- sequence. Information is given on finding
the true solution by extrapolation on a sounder basia.
Furthermore, there is a discussion on streamline-
integration. Numerical illustrations of some questions
are also added. (Author) (See also PB 145 856)
University of Southern California. Engineering
Center, Los Angeles. .
K-BAND MICROWAVE INTERFEROMETER: DE-
SCRIPTION AND INITIAL EXPERIMENTS IN A
PILOT- MODEL OF THE U. S. C LOW- DENSITY
WIND TUNNEL, by Herbert R. Pass. Technical note
on Contract AF 49(638)831. Aug 60, 73p. 29 refs.
USCEC rept. 56-217; AFOSR -TN- 60- 1087.
Order from LC mlH 50. ph$12. 30 PB 152 550
A K-band microwave interferometer has been assem-
bled and has been used to measure the phase shift
through both nitrogen and argon afterglows of a con-
tinuous r-f discharge in a model of the USC low-den-
sity wind tunnel. The Interferometer is completely de-
scribed and the results of proof or checkout teste are
included; the model wind tunnel and the r-f discharge
apparatus are briefly described. This is followed by a
presentation of the experimental procedure and by the
results of some initial tests. The calculation proced-
ure for reducing the phase shift to electron density,
including assumptions and justifications, is then out-
lined. Order-of-magnitude estimates of the percent-
ages of ionization and of the recombination coefficient
are given and. finally, with the presentation of some
emission spectrograph measurements, the processes
involved in the afterglow are very briefly examined.
(Author)
METAUURGY
Bolt, Beranek and Newman, Inc. , Cambridge, Mass.
HIGH VELOCTTY ELECTRIC ACCELERATOR SYS-
TEMS, by Jordan J. Baruch. Dennis U. Noiseux and
others. Rept. for Apr 58 -June 60 on Materials Analy-
sis and Evaluation Techniques, Contract as 33(616)5730
A F 33(616)5730. Aug 60, 148p. 12 refs. WADD Tech-
nical rept. 60-468.
Order from OTS $2. 75 FB 171 138
197
Accelerators designed to convert electrical energy to
particulate kinetiq energy have been investigated and
their capabilities and limitations ascertained. Ex-
perimentally, speeds up to 14, 500 ft/sec have been
obtained with a 201 000 Jo*^^ energy output. Four dif-
ferent mechanismB for electrical -kinetic energy con-
version have been worked out and teste^^xperi-
mentally (Author)
Carnegie Inst, at Tech. , Pittsburgh, Pa.
THEORY OF NUQLEAR RESONANCE INTENSITY
IN DILUTE ALLOYS, by W. Kohn and S. H. Vosko.
Technical rept. no. 10 on Contract Nonr-760( 13).
[1959] 27p. 11 refi. AD-229 720.
Order from LC mi$2. 70. ph$4. 80 PB 152 106
Experiments of Blpembergen and Rowland (Acta Met.
1:731, 1953) have ishown that the intensity of the nu-
clear resonance signal in metallic Cu rapidly de-
creases when sm4ll quantities of other elements are
alloyed with it. These results require that each solute
atom produces significant electric field gradients in
its vicinity, sometimes affecting as many as 85 neigh-
boring Cu nuclei. Field gradients of approximately the
required magnitixie are shown to ariae from the re-
distribution of the conduction electron charge density
near the solute at<>ms. A crucial feature of this theory
is that at large diltances r from a solute atom the
electron density behaves as co8(2kOr -Kft|/r3 where ko
is the Fermi wav4 number and <^ is a phase. Agree-
ment with experiment is a confirmation of this be-
havior. Such an oBcillatory behavior is a consequence
at a discontinuous drop at the Fenni surface of n(k),
the occupation prcjbability of the conduction band func-
tion with wave vector k. (Author)
Defense Meuls {information Center, Banelle
Memorial Inst . , Columbus, Ohio.
CURRENT NICKJL-BASE HIGH -TEMPERATURE
ALLOYS, by C. H- Lund. [Rept. on Contract
AF 18(600)13751- 17 Nov 60, lOp. 12 refs. DMIC
memo. 73.
Order from GTS 10.50 PB 161 223
This memorandum deals with the physical meullurgy
ot nickel-base alloys used in high- strength, high-
temperature applications.
Defense Metals Information Center, Battelle
Memorial Inst. ,1 Columbus, Ohio.
EXPLOSIVE MEtALWORKINC, by Charles C.
Simons. [Rept. o*» Contract AF 18(600)1375],
3 Nov 60, 3()p. 40 refs. DMIC memo. 71.
Order from OTS lO. 50 P^ 161 221
Prior to 1957, th4( application of impulsive load for
performing a meqalworking operation had received
very little attention; since that time it has been rap-
idly becoming recognized as a feasible method for
performing a wide variety of metalworking operations.
The use of intriaite shapes formed from high-
strei^lth refractcjry metals, as well as the forming of
large parts from these and other materials, has ne-
cessitated the detelopment at a process by which the
tremendous energies required to form these desired
shapes could be generated. The purpose of this
memorandum is to explain in generalities the princi-
ples of impulsive or explosive forming, a technique
by which such energies can be developed, and at-
tempt to remove some of the mystery which has en-
veloped the process. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
JOINING OF TUNGSTEN, by R. E. Monroe. [Rept.
on Contract AF 18(600)1375). 24 Nov 60, 8p. 3 refs.
DMIC memo. 74.
Order from OTS $0. 50 PB 161 224
This memorandum has been prepared to evlew exlai-
ing infornrwtion on the joining of tungsten by welding
and brazing. The memorandum enumerates the known
techniques, the known metallurgical effects which have
a bearing on joining, and the appbcations currently
being investigated to provide additional background on
tungsten joining. (Author)
Defense Metals Information Onter. Battelle Memortal
bst. , Columbus, (Dhio.
WELDING OF COLUMBIUM AND COLUMBIUM .
ALLOYS, by W. ]. Lepkowskl, R. E. Monroe, and
P. J. Reippel. [Rept. on Contract AF 18(600)1375).
24 Oct 60, 28p. 16 refs. DMIC memo. 69.
Order from OTS |0. 50 PB 161 219
The purpose of this memorandum is to compile, review,
and evaluate available unclassified information on the
weldii^ of columbium and its alloys. Such information
is limited and the known meullurgical characteristics
of columbium alloys have been used in attempting to
anticipate specific problems that may be involved ii!
welding. Unalloyed columbium is noted for being read-
ily weldable by techniques developed for welding simi-
lar metals such as titanium. However, unalloyed colum-
bium is relatively weak at the desired service temper-
atures and also has poor oxidation resistance. Mostof
the alloys that are stronger and more oxidation resist-
ant are also less weldable and may present serious
welding problems. It should be re-emphaslzed that
most of these alloys are In the early development
stages, and little information is presently availableoo
their weldabllity. This memorandum has been prepared
to summarize the small amount of information nqfw
available in what will be an important facet of the djfvelop-
ment of useful columbium alloys. (Author) ^l
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
HIGH-VELOCITY METALWORKING PROCESSES
BASED ON THE SUDDEN RELEASE OF ELECTRI-
CAL ENERGY, by H. J. Wagner and F. W. Boulger.
[Rept. on Contract AF 18(600)1375]. 27 Oct 60, 15p.
27 refs. DMIC memo. 70.
Order from OTS |0. 50 PB 161 220
In the past 2 years commercial applications have been
found for a number of metal -forming processes in
which the energy applied to the workpiece originates
as electrical energy stored in a bank of high -voltage
capacitors. These methods differ chiefly in the man-
ner in which the electrical energy is converted to ths
mechanical energy used to deform the metal. In two
(^ the methods, a high -amplitude, short-duration
current pulse is used to create an underwater shock
Mve, either by causing a spark to jump across a
it^nerged spark gap or by literally exploding a sub-
merged filament wire in the vicinity of the workpiece.
In a third method, the current pulse produces a rap-
Idly changing magnetic field in a coil. This changing
iMgnetic field exerts a force on the workpiece. Each
of the processes is discussed separately.
Illinois Inst, of Tech.. Chicago.
jgOTE ON THE CHANGE IN STORED ENERGY
PRODUCED BY REVERSED DEFORMATION, by
A. S. Iyer and Paul Gordon. Technical rept. no. 3 on
Contract Nonr- 1406(03). jan 59. 6p. 3 refs.
Order from LCmi$ 1.80. ph$ 1.80 PB 152 017
Illinois U. [Urbana)
ANEUSTIC MEASUREMENTS OF DIFFUSION COEF-
I FICIENTS, by James Stanley and Charles Wert. Rept.
on Contraa AF 18(603)22. 25 Mar 60. 43p. 29 refs.
AFOSR TN-60-203; AD- 235 947.
Order from LC ml$3.30, ph$7.80 PB 148 675
A discussion is presented on anelastic measurements o(
metals and alloys in terms of detailed atomic motion
and on calculations of diffusion coefficients for them.
The correlation between anelastic measurements and
diffusion can be seen if the coefficient of diffusion, D,
Is written in the form D - K«^ , where a is the lattice
parameter. T is the mean time between successive
Jumps of a given atom, and K is a geometrical constant.
The term, anelastic solid, is used to specify those
sohds whose behavior obeys a homogeneous, linear dif-
ferential equation in stress, strain, and their first time
derivatives. Constants in this equation may be written
Mr-t- Tctf-iMR {t,-*-%t). where «■ andfe are the
stress and strain, respeaively, andTg, Tq. and Mr
are all constants of the material. Two solutions are
discussed, one for the case where rf" «0 and the other,
the general solution. A new set of measurements is
reported for the Fe-V alloy system in an attempt to
determine a relationship between relaxation time and D
for a simple solid solution alloy with bcc structure.
DUfuaion measurements with radioactive isotopes
indicated that ferromagnetic ordering of spins which
occurs below the Curie temperature (840OC) greatly
reurds diffusion.
New York U. Coll. of Engineering. N. Y.
BINARY AND TERNARY DIAGRAMS, by Elraars Ence,
Paul A. Farrar. and Harold Margolin. Rept. for
I May 58- 15 Mar 60 on Metallic Materials. Contract
AF 33(616)5704. Aug 60, 82p. 19 refs. WADD Techni-
cal rept. 60-316.
Order from OTS $2. 25 PB 171 154
L T^-Al-Cr System: The Tl-rich comerof the T!-Al-Cr
system has been reinvestigated from 600 - 1400^
(up to 40 wt. percent al and 32 wt. percent V). Partial
lasothermal sections have been constructed at 1400.
1200. 1100. 1000, 800. and600OC. IL Tl-Al-V System:
The TB-Al-V system has been reinvestigated from 50
to 1(» wt. percent tlUnium and from 500^ to 1400OC,
Ming X-ray diffraction and metalloRraphlc techniques.
198
I
Isothermal sections were delineated at 5(K), 600, 700,
800, 900, 1000, 1100, 1200, 1300 and 1400oa Vertical
sections at 2, 4, 6. 10, and 16 wt. percent aluminum;
2. 4, 6, 10, and 16 wt. percent vanadium and 90 wt. per-
cent Tl were constructed. (Author)
Office of Technical Services, Dept. of Commerce,
Washington, D. C.
POWDER METALLURGY (SUPPLEMENT TO CTR-
343). Aug 60. lOp. 103 refs. OTS Selective Bibliogra-
phy SB-423.
Order from OTS $0. 10 OTS SB-423
A bibliography of reports listed in the two OTS nrranthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography includes
PB reports, AEG reports and translations on powder
metallurgy (as well as related reports on sintering)
added to the OTS collection during the period May 1958
to September 1960.
Stanley Tliompson Labs. , Columbia U. , New York.
EFFECT OF SURFACE ACTIVE AGENTS ON THE
STRENGTH PRCX'ERTIES OF METALS; by Leonard
Nanis. Rept. on Contract Nonr-266(64). 4 Dec 59,
36p. 15 refs. AD- 231 155.
Order from LC mi^.OO, ph$6. 30 PB 152 147
A review of the literature of the British and American
sdiools on the Rrfibinder effect shows that no effects
are found for polycrystalline wires, although creep ^
enhancement is observed on single cryrtals. These
schools relate such effects to removal of a thin sur-
face film which alcMie produces strengthening. The
Russian and German schools find creep enhancement
for polycrystalline wires, presumably by a lowering
of metal surface energy. The interpretation of creep
for polycrystalline copper by the Russian school is
based on a time-elongation formula wtiich is in com-
plete disagreement with experimental data, particu-
larly with respect to the existence of a defined initial
creep rate. The loads used by the Russian school are
insufficient to produce the creep elongations reported
by them. Since grain size, heat treatment and pre-
strain were reproduced as nearly as possible, the
absence of observable creep in the present work sug-
gests a gross experimental error on the part of the
Russian school. With the best cleaning and coating tech-
nique developed for the present work, no significant
difference was observed between coated and uncoaced
copper wires in numerous individual tests. (Audior)
Ferrous Metals
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
DESIGN INFORMATION ON 5Cr-Mo-V ALLOY
STEELS (H-11 AND5 Cr-Mo-V AIRCRAFT STEEL)
FOR AIRCRAFT AND MISSILES (REVISED) by
R. J. Favor and W. P. Achbach. Rept. on Contract
AF 18(600)1375. [28 Aug 59] rev. 30 Sep 60, 51p.
30 refs. DMIC rept. 116R.
Order from OTS $1. 50 PB 151 072- R
i99
U-
Thia repon is a Nummary of design information per-
tinent to the use W the 5Cr-Mo-V (H-11 type) alloy
steels In aircrafi and missile applications. Heat treat-
ment, melting priactice, and corrosion protection are
considered. Manufacturing problems such as machin-
ing, forming, antl joining are also briefly discussed.
Data on the eleva|ted- temperature mechanical proper-
ties of these H-ll type steels have been collected and
evaluated. The siimmation of design- allowable
strengths has be<n accepted by the Structures Sub-
committee of the Federal Aircraft Design Criteria
Committee. (Auttior)
James Forrestal Research Center, Princeton, N. J.
OXIDATION OF IRON-CHROMIUM ALLOYS, by
D. Lai, R. J. Borg and others. Rept. on Contract
AF 49<638)533. 7f) Feb 60. 36p. 26 refs. Metallurgy
rept. no. 22; AFOSR-TN-60-387; AD- 235 785.
Order from LC rii$3. 00, ph$6. 30 PB 149 068
The rates of oxldption of iron alloys containing 0. 2 to
10 pet. chromiur^ have been measured from 750 to
1025%. The accelerations in rate during an isothermal
measurement do hot occur at reproducible times or
average thicknestes, which suggests that scale fracture
plays an importait role. The ways in which chromium
might contribute \o a reduced rate Ol oxidation of iron
•re discussed.
Naval Research Lab , Washington. D. C
MINIMUM TOUGHNESS REQUIREMENTS FOR HIGH-
STRENGTH SHEtT STEEL, by J. A. Kies.
H. L. Smith and (Khers. Interim rept. 20 Oct 60, 21p.
3 refs. NRL reptj 5521.
Order from GTS io. 75 PB 161 786
The minimum toi^^hness requirements for high-strength
steels are discus$ed in terms of an assumed flaw (or
crack). Other factors, of course, play an important
part in determini^ these minimum requirements, such
as temperature a$d strain or stress history. The as-
sumption of a through crack twice the sheet thickness
in length is nMde) this assumption is based on past ex-
perience as being commonly encountered. Tests meas-
uring the critical driving force, or work per unit area,
required for specimen fracture at the point &f crack
growth instabilityj yield the result that a test specimen
width of at least 3 inches is required for most mate-
rials in order to guarantee a strength equal to or above
the yield strength in a pressure vessel containing a
largest crack 2t or less m length. The through crack
length requirement is further generalized to include
specimens 2Nt in llength. where t is the specimen
thickness and N 14 s factor. Toughness measurements
indicate that kno«^ steels used at 240, 000 psi stress
level will requirejjhe factor N to be much less than
unity. A quality factor rating for steel, which amounts
to a strength to weight ratio, in the presence d a crack
is Mioasted. Thijs quality factor would reflect the ad-
»■«■§■■ of low density, high yield strength, high
toug^tfiesa, and hi|h modulus. (Author)
^
Light Metals
Lockheed Aircraft Corp. , Sunnyvale, Calif.
BERYLLIUM. SURVEY OF THE LITERATURE,
comp. by K. D. Carroll. Quarterly supplement no. 2
to Special bibliography for Apr -June 60. Aug 60, SSp.
228 refs. LMSD 288190, suppl. no. 2.
Order from LC mi$4. 80. ph$13. 80 PB 152 378
Citations include those published, reviewed, or re-
ceived during the period April-June 1960. Citations
are arranged alphabetically by author or source tnder
broad subject headings. l\\c general field of beryllim
metallurgy, alloys and applications have been sur-
veyed. Cu-Be alloys have been omitted as have most
items pertaining to nuclear reactor applications and
toxicity problems.
Lockheed Aircraft Corp. , Sunnyvale. Calif.
BERYLLIUM CRACK PROPAGATION AND RELATED
STUEMES, comp. by K. D. Carroll. Special bibli-
ography. 24 Aug 60, 4Sp. 141 refs. SB-60-30.
Order from LC nfl$3. 30, ph$7. 80 PB 152 377
Citations have been compiled pertinent to surface
cracks which develop in beryllium when it is subjected
to bending loads, its recovery from stress and bending
and fracture of crack propagation to catostrophic
failure. Due to the sparsity of publications dealing
directly with this problem, items were selected in
three categories: (1) Beryllium crack propagation and
fracture investigations; (2) Mechanical properties of
beryllium related to crack or fracture tendencies
(ductility, brlttleness, tensile, etc. ); (3) Selected
references on the theory and analysis at crack propa-
gation and fracture. Since the literature on the analy-
sis and theory of crack propagation is so extensive
Part 3 Is restricted to Items which present a theoryor
procedure which m ight be adapted or extended to be-
ryllium alloys. (Author)
National Research Labs. , Ottawa (Canada).
SOME EXPERIKENTS ON THE EFFECT OF TIME
AT TEMPERATURE ON THE ROOM TEMPERATURE
REVERSED BENDING FATIGUE CHARACTERISTICS
AND ON THE TENSILE STRENGTH OF 24S-T
ALCLAD ALUMINUM ALLOY, by J. A. Dunsby.
8 Aug 60, 24p. 6 refs. Mechanical engineering rept.
MS -102, NRCno. 5927.
Order from LC mi$2. 70, ph$4. 80 PB 152 785
ExperimeiKs are described in which specimens of *-
24S-T aluminum alloy were held at temperatures of
4000P or 300^^ for periods ranging from 11/2 to 100
hours prior to conducting room temperature reversed
bending fatigue or tensile tests. The physical proper-
ties of the material change radically with such treat-
ments and it is diown that these changes can be corre-
lated for varying times and temperatures by the use of
the Larson-Miller parameter. The results of the tea-
sile tests are in good agreement with previously re-
ported tests provided that proper allowance is made
for the initiaJ condition of the material. It is showp
that these earlier tests can be used to determine the
effects of time at temperature on the tensile strength
on a given sample of this material provided that the
initial yield strength is known. (Author)
aoo
Structural Metallurgy and Corrosion
Brawn U. Div. of Engineering, Providence, R. 1.
VARIATION OF RESIDUAL MICROSTRESSES WITH
COMPOSmON OF TWO-PHASE ALLOYS, by
I Gurland. Technical rept. no. 4 on Contract Nonr-
562(19) Dec 59, 25p. 26 refs; AD- 230 558.
Order from LC mi$2. 70, ph$4. 86- PB 152 169
rhc variation of residual microstressfes with compo-
sition of two-phase alloys is estimated on the basis of
simple models of elastic spheres embedded in a plas-
tic matrix. The calculations neglect the interference
of stress fields of neighboring particles and apply
quantiutively only to relatively low concentrations of
(be second phase. Nevertheless, it is shown that the
average principal stresses and the average maximum
ghear stress of the matrix, as well as the strain en-
ergy of the alloy, are smallest at the ends of the com-
position range and attain a maximum at some inter-
mediate composition. As the volume fraction of the
dispersed phase is increased, the stress in the parti-
cles becomes less uniform and a component of stress
of apposite sign is introduced. (Author)
Defense Metals Information Center. Battelle
Ntemorial bist. , Columbus, Ohio.
TOE EFFECTS OF ALLOYING ELEMENTS IN TITA-
NIUM. VOLUME A. CONSTITUTION, by
D. J. Maykuth. H. R. Ogden and R. L Jaffee. Rept.
on Contract AF 18(600)1375. 15 Sep 60, 234p. 223 refs.
K41C rept. 136A.
Order from OTS $3. 50 PB 151 094
The available information on the constitution and
structure of binary and ternary alloys of titanium is
presented. Phase diagrams are presented for 37 bi-
nary tiunium alloys, and partial information is pre-
sented for 14 others, as well as for 67 ternary tita-
nium-alloy systems. (Author)
Franklin Inst. Labs, for Research and Development,
Philadelphia, Pa.
PURIFICATION AND SUBSTRUCTURE FORMATION
OF METALS AND PROPERTIES OF HIGH PURITY
METALS, by Marvin Herman. Final repc. for
1 Oct 55-31 Mar 60 on Contract AF 18(600)1581. (I960)
9p. 5 refs. Rept. no. F -A 1 878; AFOSR-TR -60-81.
Order from LC mi$l. 80, ph$l. 80 PB 152 074
Fulmer Research Inst. . Ltd. (Gt. Brit. ).
■fflE SPACING OF SLIP LINES IN METALS, by J. T.
Bimby and Joan S. Seel. Annual technical rept. no. 3.
June 59- June 60, Contract DA 91-591-EUC-
1164.01-1499-59. Sep 60. I3p. 1 ref. R. 113/9.
Order from LC ml $2. 40. ph$3. 30 PB 152 261
Thli report describes a study of thin films of copper
and brass by transmission electron microscopy, with
the aim of correlating internal defect structure with
the slip line spaclngs observedon the surfaces of these
meuls. A subsidiary objective has been to determine
whether thin films of these meuls are best prepared
by microtome-cutting or by electropolishing. It was
found that microtome-cut specimens are so badly de-
formed by the cutting operation that no clear interpre-
tation can be given of the structure seen under the
electron microscope. It Is believed that the electro-
polishing technique developed to thin specimens was
successful, but few of these films have been examined
due to a technical fault on the electron microscope.
(Author) (See also PB 143 118)
Martin Co. , Baltimore, Md.
A STUDY OF THE EFFECTS OF SURFACE FILMS
ON THE MECHANICAL PROPERTIES OF METALS,
by Irvin R. Kramer. Rept. for Jan-Dec 59 on New
Synthetic Methods. Contract AF 33(616)6220. July 60.
34p. 11 refs. WADD Technical rept. 60-31.
Order from OTS $1.00 PB 171 150
It is shown that by removing the surface of aluminum
single crystals while they are being deformed, the
extent and slope of Stage 1 and Stage II are affected.
The stress at which Stage 111 starts is also lowered.
A dislocation pop -out phenomenon was observed when
the^^te of meul removed was suddenly increased
during the tensile deformation. Deformed crystals of
zinc, aluminum, and copper immersed in solutions
containing surface active agents reacted with these
agents to form metal soaps. (Author)
Rock Island Arsenal Lab. , 111.
METHODS AND MATERIALS FOR THE PRESERVA-
TION OF SMALL HARDWARE ITEMS, by R. L.
Murrens. Final rept. 2 Aug 60, 22p. 4 refs. Rept.
no. 60-2314. «, .,t. oo-,
Order from OTS $0.75 » 161 897
Tests for improving the application of MIL-C- 16173,
Grade 1 corrosion preventive to small hardware items
(i.e. screws, bolts, nuts, etc.) did not prove success-
ful. Attempts to obtain adequate, quick drying and
uniform coatings by spraying, were unsatisfactory.
Spin-drying techniques were more successful, but did
not solve the problem of small parts sticking together.
A water-base compound, MIL-C-40084 (Ord), sought
as a replacement fot MIL-C- 16173, Grade 1, showed
satisfaaory utility during application procedures. The
water base compound, when applied to small hardware
produced a thin uniform coating which dried quickly
and did not cause items to stick together. The pro-
tective ability of MIL-C-40084 (Ord) compounds were
evaluated in a three year storage program and it was
found that equal protection was provided by either
MlL-C-40084 (Ord) or MlL-C- 16173, Grade 1 where
adequately coated sw^aces were compared, but
greater over all protection was provided by MIL-
C-40084 (Ord) compounds due to their aUlity to cover
more adequately sharp edges and recessed areas. It
is recommended that MIL-C-40084 (Ord) corrosion
preventive replace MIL-C- 16173, Grade 1 and MIL-
L-3150 which are presently specified in MIL-P-II066.
Also, it is recommended that MIL-C-40084 (Ord)
corrosion preventives be considered for other military
applications wherein MlL-C-16173, Grade 1 and
MIL-L-3150 are being used. (Author)
201
NUClf AR PHYSICS AND
NUCLEAR CHEMISTRY
El imentary Particles
Air Force Special Weapons Center, Klrtland AFB,
N Max.
THEORY OF GEOMAGNETlCALLy TRAPPED PAR-
TICLES. PART U SCATTERING LOSS OF GEOMAG-
NETICALLY TRAPPED PARTICLES. PART II. CON-
FIGURATION 0F| THE EARTHS RADIATION BELTS,
by J. A. Welch, jk Sep 60. 32p. 24 refs. AFSWC TN-
60-29. f
Order from LC nJl$3. CO, ph$6. 30 PB 152 639
Part I: A reformulation of the loss of geomagnetically
trapped partidles due to scanering has been made. The
result demonstraqes the relative importance of ;he
first and second spatial derivatives of the distribution
function in determining the time derivative. The down-
ward drift erf mirfor points appears as a valid concept
whenever the firs^ spatial derivative term is dominant.
For low mirror points the coefficient of the second
spatial derivativeiis much smaller than for the first
derivative. Part I|: Accurate calculations have b«en
made of the observed configuration of the Argus shells
of sceomaKneticallit trapped electrons and the lower
edge of the Van Allen belt of high energy protons. The
method uses the «diabatic invariant theory of charged
particle nuxion ii^ a magnetic field. The calculations
were based on thei high order spherical harmonic ex-
pansion of the geotnagnetic field developed at the Air
Force Special Weapons l^enter. This work is the first
quantitative agreepient of theory with the observed
configurations. (/|uthor)
Cambridge U. (C* Brit. ).
LOW ENERGY PI(>N SCATTERING, by J. Hamilton
and T. D. Spearman. Technical scientific note no. 9
on Contract AF 6l«]52)233. June 60, 41p. 16 refs.
AFOSR TN-60-10$l.
Order from LC mi^3. 30. ph$7. 80 PB 152 424
Partial wave dispefsion relations are used to investi-
gate low energy s-^ave pion-nucleon scattering. The
various terms in tlie relations are examined. It is
shown that the Bonj terms are very small, and the re-
maining terms are of the same order of magnitude as
the observed scattering amplitudes. The evidence for
a low energy pion-|)ion interaction from s-wave pion-
nucleon scattering |s examined. A comparison of Che
dispersion relatione, for s- and p-wave partial ampli-
tudes IS made. (Author)
Cambridge U. (G<. Brit.).
SOME SINGULARITIES OF SCATTERING AMPLI-
TUDES ON UNPHYSICAL SHEETS, by J. Gunson and
J. G. Taylor. TecHnical scientific note no. 11 on Con-
tract AF 61(052)231. July 60. Up. AFOSR TN-
60-1083. J
Order from LC ml|2. 40, ph$3. 30 PB 152 422
An investigation of the consequences on unphysical
sheets of a Mandel^um type representation holding
for a two particle stanering amplitude on the physical
202
sheet is described. The domain of analyticity in the
energy and momentum transfer variables is con-
structed and compared with perturbation theory. A
theorem on multiplication of singularities for
Legendre polynomial expansions used in our discus-
sion is proved. (Author)
Cambridge U. (Gt. Brit. )
UNITARITY AND THE MANDELSTAM REPRESEN-
TATION, by R. W. Lardner. Technical scientific
note no. 12 on Ckmtract AF 61(052)233. July 60, 17p
AFOSR TN-60-1084.
Order from LC mi$2. 40, ph$3. 30 PB 152 421
The three particle terms in the units rity expansion for
a scattering amplitude are examined on the assump-
tion that the relevant production amplitudes satisfy
single dispersion relations. It is shown that they
satisfy the Mandelstam representation. The proof is
extended to the four partiele terms. (Author)
National Bureau of Standards, Washington, D. C.
ON THE SCATTERING OF v RAYS BY NUCLEI, by
U. Fano. Nov 60, 28p. 6 refs. Technical note 83*.
Order from OTS $0.75 PB 161 584
The theory of scattering by electric dipole interaction
is developed by tensorial techniques, which permit an
early separation of geometric and dynamic factors. The
geometric relationships are formulated in terms of
variables that represent arbitrary partial polarization
of the incident and scattered y rays. TTie relevant dy-
namic properties of a nucleus are represented by a
scalar, a veaor, and a quadrupole polarizability.
These polarizabilitles correspond respectively to the
values 0, 1, and 2 al the quantum number j which indi-
cates the angular momentum transfer in the scattering
process. The analysis of scanering according to angu-
lar momentum transfer is compared to the ordinary
theory at angular distributions. The nuclear polariza-
bility is discussed from the standpoint of different
models. The magnitudes of the three polarizabilities
can be determined by experiments with unpolarized
nuclei but with some degree of circular polarization of
the Y rays; linear polarization contributes no additional
information. Nuclear polarization is required to deter-
mine the phases of the polarizabilities.
Insfruments and Installations
Naval Radiological Defense Lab. , San Francisco,
Calif.
A SEARCH FOR IMPROVED NEUTRON SPECTROME
TER, by R. L. Mather. P. J. Cressman and J. R.
Hubbard. 30 Oct 59, 18p. 22 refs. Research and
development technical rept. USNRDL-TR-380:
AD- 230 420.
Order from LC ml$2.40, ph$3.30 PB 153 253
This report released for sale to the public 14 Dec 60.
A new type of spectrometer for measuring the energy
distribikior jf neutrons is proposed. The proposal
relies on a dlffer'oce in electrical pulse shapes from
a lithium crysta jcintlUator depending on the type at
event produced In the cry«al. Pulse differences were
(jemonstrated with stilbene crystals but differences
oould not be demonstrated with a commercial Li^I(^il)
crystal. Other lithium-containing scintillators are
listed and further experiments proposed. (Author)
Westinghouse Electric Corp. . Baltimore, Md.
u6i(Eu) NEUTRON SPECTROMETER, by J. C. Rit-
ter, S. L. Ruby, and R. V. Babcock. Final rept. on
C^ntraa AF 19(604)5617. 15 Aug 60, llOp. 20 refs.
Materials Engineering rept. no. 6033-4801-A;
AFCRLTR-60-180,
Order from LC mi$5. 70, ph$16. 80 PB 152 411
U^I(Eu) crystals provide a reasonably convenient
high efficiency, moderate resolution, absolute neu-
tron energy spectrometer in the energy range above
1 mev. Line shapes far monoenergetic neutrons have
been measured as a function of Eu doping and temper-
ature. Voltage pulse height resolution of 12% for
4. 9 mev monoenergetic neutrons is obtained at liquid
nitrogen temperature with a highly doped
(Q. 15 mole %) Eu crystal. Information is presented
on y-ray discrimination and the linearity between neu-
tron energy and voltage pulse height. Such effects as
light output pulse shape, light emission frequency,
temperature, and crystal doping are considered. A
design is given for a neutron energy spectrometer
probe which operates at low temperatures. Methods
for unscrambling neutron spectra are also given.
(Author)
Nuclear Engineering and Power
Admiral Corp. , Chicago, III.
EVALUATION AND [KVELOPMENT OF MIL-C14157
CAPACITORS FOR NUCLEAR RADIATION ENVIRON-
MENT, by E. R. Pfaff. Scientific rept. no. 2 on Con-
traaNObsr-77612. Jan 60, 3Pp. 8 refs. AD- 234 120.
Order from LC nii$2.70, p*i$4.80 PB 148 979
Gas evolution tests on various dielectric fluids indi-
cated that bis(phenoxyphenyl) ether and monoisopropyl-
biphenyl have promise. Capacitors impregnated with
these fluids had low insulation resistance and the capac
itance o* monoisopropylbi phenyl impregnated capacitor
increased by twenty per cent. Passively irradiated
sundard CI^08 capacitors exhibited low insulation
resistance after irradiation and half of the units failed
the dielectric breakdown test. Several different dielec-
tric tissues are in the process of evaluation. (Author)
Naval Research Lab. , Washington, D. C
ENVIRONMENTAL ASPECTS OF THE NAVAL RE-
SEARCH LABORATORY, by S. E. Golian, E. H. Bebbs
and others. 23 Feb 54, I36p. 43 refs. NRL rept. 4308.
Order from LC ml$6. 90, ph$21. 30 PB 153011
This report released for sale to the public 2 Dec 60.
An analysis of the environmental aspects of the Naval
Research Laboratory has been made in conneaion with
• nuclear reactor feasibility study. The environmental
data is here gathered into one report. This study,
while not intended to be a comprehensive environmental
report, considers such factors as topography, geology,
geography, hydrography, hydrology, climatology,
meteorology, seismography, sanitation, and back-
ground radiation. (Author)
Naval Research Lab. , Washington, D. C
SUPPLEMENT TO PROPOSAL FOR NRL RESEARCH
REACTOR, by E. H. Krause. 1 May 53. 89p. 31 refs.
NRL rept. no. 4164, supp. to NRL rept. 4129;
RDno. 257.
Order from LC miH 80, ph$13. 80 PB 153 012
This report released for sale to the public 5 Dec 60.
This report is intended to present additional hazard
studies with respect to the proposed reactor, and to
bring up to date the reactor and building designs.
Nuclear Reactions
Bartol Research Foundation, Franklin Inst. ,
Swarthmore, Pa.
DETERMINATION OF NUCLEAR DISINTEGRATION
ENERGIES, by C E. Mandeville, D. M. Van Patter
and others. Final rept. for 1 Nov 54-31 Oct 58 on Con-
tract AF 18(600)1320. (1958) 82p. 291 refs. AFOSR-
TR-59-28; AD-211 322
Order from LC mi$4. 80. ph$l3. 80 PB 149 700
Precise determinations were made of nuclear disinte-
gration energies using a magnetic spectrometer for
charged particles in conjunction with a Van de Graaff
accelerator.
Included in the report are:
Q-value measurements for phosphorus and chlorine,
pub. in The Physical Review 103:656-661. 1 Aug 56
Nuclear reaction Q-value measurements made recently
at the Bartol Research Foundation, pub. in Nuclear
Masses and their Determination, Pergamon Press,
1957. p. 99-108
Comparison of masses obuined from mass -spectro-
scopy and nuclear reaction data. pub. in Nuclear
Masses and their Determination. Pergamon Press,
1957. p. 143-160.
Q-value measurements for aluminum and chlorine, pub
in The Physical Review 106:1016-1019. 1 June 57
Inelastic proton scanering from phosphorus and zinc,
pub. in The Physical Review 107:171-175, 1 July 57
Nuclear disintegration energies. II, pub. in Reviews of
Modern Physics 29:757-766. Oct 57_
Levels in Cr^O, Cr52, Cr53, and Cr>*, pub. in The
Physical Review 112:468-474, 15 Oct 58
Proposed systematica for E2 transition prc4>abilities of
even -even nuclei, pub. in the Jnl. of the Franklin
Inst. 266:411-413, Nov 58
Illinois U. . Urbana.
A STUDY OF THE PROPERTIES OF RADIOACTIVE
NUCLEI BY OPTICAL ORIENTATION, by Mark N.
McDermott. Walter Bauer, and Donald Trimmer.
Final rept. for Nov 59-July 60 on Contract
AF 49(638)781. I960. 5p. 2 refs. (AFOSR TR-60-821
Order from LC mill. 80. ph$l. 80 PB 160 860
203
Apparatus was designed and constructed for the de-
termination of t^^e spins and moments of Cdl07 and
Cd^^. The tectfiique employed was essentially the
'.veil -known optiqal double resonance method of Bitter
and Broasel. Th(s technique requires a cadmium
spectral lamp, ai cadmium scattering bulb, a photo
detector, controlled magnetic fields, and suitable po-
larizing optics. Considerable effort was devoted to
the development pf intense spectral lamps.
Isiltuto dl Fislda deH'Universiii, Trieste (Italy).
ON THE TOTAU SPECIFIC IONIZATION, by P. Budini,
L. Taffara, and C. Viola. Scientific note no. 1 on
Contract AF 6l((i52)211 . 12 July 60, 28p. 13 refs.
AFOSR-TN-60-lb86.
Order from LC rtu$2.70, ph$4.80 PB 152 420
A method is give|i for calculating the absolute value of
primary, secondary and total specific ionization gen-
erated by a ionizing particle traversing a given me-
dium. Density e^ea is taken into account. Numerical,
results are given for H and He and compared with
existing experimental data. It is shown that primary
ionization preseits higher relativistic increase..(lower
density effea), tian total ionization when the dilution
d secondary ionitsation is felt. Further primary ioni-
zation is indepen^lent of maximum transferable energy
in close collisioda which on the contrary influences
sensibly ionizaticjn of higher generations. Simplified
formulae are givtn where the influence d the physical
characteristic of Ithe medium on the phenomenon ap-
pears evident an4 which are apt to be compared with
the experimental 'results. (Author)
RANg^E
l4nsburgh
CHARGE TRAN^^ER IN MOLECULAR HYDROGEN,
by T. F. Tuan (Doctoral thesis) and E. Gerjuoy. Tech-
nical rept. no. 1} on Capture- Loss and Ionization
Cross -Sections of Ions and Neutral Particles, Contraa
Nonr-624<06). Fib 60, 30p. 20 refs. AD- 237 493.
Order from LC nii$2.70, ph$4.80 PB 147 542
The effects of thei molecule of electron capture by
protons in hydrog)en gas were investigated in first Born
approximation wilh different types at elearonlc wave
functions. It always was supposed (1) that if the inci-
dent proton velocity is large compared to electronic
velocities, molecular effects may be negleaed, and (2)
that one may then, assume that one H2 molecule is
equivalent to two nydrogen atoms for fxirposes of
charge transfer. Instead, it appears that charge trans-
fer in H2 at high energies bears no simple relationship
to charge transfet in atomic hydrogen. In particular,
•mong other effeqts. it is found that (1) in the high
energy limit 1/2^ «1.2 - 1.4 (T^ and (2) at lower
energies there is Important interference between the
capture amplitudeis from the two atoms in the mole-
cule. It also is fo^nd that transitions to ungerade
states of H2 1 although unimportant in the energy
range of present Experiments, become appreciable at
high energies. (Author)
Pittsburgh U. , Pi.
DETECTION OF NEGATIVE IONS FORMED BY
CHARGE TRANSPER, by T. M. Donahue and
F. Hushfar. Tech^iical rept. no. 13 on Capture- Loss
and Ionization Crotas- Sections of Ions and Neutral
Particles, Contraa Nonr-642(06). Dec 59, 4p. 2 reft
AD- 233 004.
Order from LC nfu$ 1.80, ph$ 1.80 PB 152 133
A mass spectrometer was designed to detect and
identify the negative ions formed in gases through
which atomic H beams pass. H' ions occurred at
energies of 13 to 19 Kev for the incoming atom in H2.
H" and O" occurred in H2O vapor and in air, and Q"
was found In 02- No negative ions were detected in N,
He, or Ar. In CO the cross seaions for negative ion
formation at the electron loss maxima occurring at 12,
13.75, and 16.29 Kev were 4.6, 5, and 5. 8 times as
large as at the minimum which occurred at 14. 34 Kev
and 3, 3.4, and 3.9 times as large as the much less
pronounced minimum at 17.42 Kev. At 12 Kev the
cross section for negative ion formation was meas-
ured crudely to be of the order of 10'^" sq cm. The
predominant ion in the 12 Kev peak is CO' and C*
first was found in the 34 Kev peak. According to the
mechanism of ion formation proposed, the electron
carried by the H atom did not have enough energy to
dissociate CO' below 12.55 Kev.
Pittsburgh U. , Pa.
FORMATIOM OF NEGATIVE IONS IN CO BY ELEC-
TRON CAPTURE FROM FAST HYDROGEN ATOMS,
by T. M. Donahue and F. Hushfar. Technical rept.
no. 10 on Cl|pture-Lo8s and Ionization Cross-Seaions
of Ions and Neutral Particles, Contract Nonr- 624(06).
Nov 59, 9p. 6 refs.
Order from LC mi$l . 80, ph$l . 80 PB 150 857
Plasmadyne Corp. , Santa Ana, Calif.
CALCULATION OF COLLISION CROSS SECTIONS
BY USE OF RELAXATION TECHNIQUES, byEmllJ.
Hellund. Rept. for May 59-June 60 on Research on
Particle Dynamics, Contract AF 33(616)6698. Aug 60,
33p. ARL Technical rept. 60-303.
Order from OTS $1.00 PB 171 163
The report discusses the methods of calculating colli-
sion cross sections and the advantage of using the
"relaxation method . 1S-2S and IS-2P excitation reac-
tions of electron with hydrogen atoms are calculated.
The detailed steps of calculus are outlined, and the
computed results are compared with those by experi-
ments ctf other investigators. Interpretations on the
discrepancies by different authors are made and dis-
cussed. Further applications of the relaxation mettxxl
are ^ggested. (Author)
Vienna U. (Austria).
THE TWO MESON APPROXIMATION FOR THE
REAL NUCLEON, by G. Eder. Scientific note no. 3
on Contract AF 61(062)265. 24 May 60, 14p. 6 refs.
AFOSR-TN-60-710.
Order from LC mi$2.40, ph$3.30 PB 152 482
The method of momenta proposed by F. Halpwrn is
applied to the description of the real nucleen state in
the two meson approximation. The static model of
Chew and Low for an extended source has been used.
It seems possible to get a weakly coupled model which
gives a good value of f^ and which fits rather well the
sum rules for the pion nucleon scattering amplitudes.
(Author) 1 - '
204
Radioactivity
Air Force Cambridge Research Center, Bedford,
Mass.
A DIFFUSWN- DEPOSITION MODEL FOR IN-FLIGHT
RELEASE OF FISSION FRAGMENTS, by
M. L. Barad, D. A. Haugen, and J. J. Fuquay (General
Electric Co. ). June 60, 36p. 15 refs. Air Force
Surveys in Geophysics no. 123; AFCRC-TN-60-400.
Order from LC mi|3. 00, ph$6. 30 PB 152 283
A diffusion-deposition model is developed for use in
estimating dosage levels due to in-flight release of
fission fragments from a nuclear -powered aircraft.
The model is based on the work of Sutton for diffusion
and the work of Chamberlain for deposition. The nKidel
considers an elevated instantaneous point source and
an elevated instantaneous line source oriented at an
arbitrary angle to the mean wind direction. Suggested
values of the various deposition, rain-out, and diffu-
sion parameters to be used with the nvxlel are pre-
sented along with a qualitative discussion of the uncer-
tainties of the model and the suggested parameters.
(Author)
Naval Radiological Defense Lab. , San Francisco,
CaUf.
A FALLOUT PLOTTING DEVICE, by E. A. Schuert.
30 Nov 56, 17p. Research and Development technical
rept. USNRDL-TR-127; AD-124 406.
Order from LC mi$2.40, ph$3.30 PB 152 795
This report released for sale to the public 16 Dec 60.
A fallou plotting device was developed. The method
requires no drafting equipment and is ideally suited for
field use. At Operation REDWING it was found that un-
trained personnel could quickly become proficient in
its employment. (Author)
Radiation Effects Information Center, Battelle
Memorial Inst., Columbus, Ohio.
MONTHLY ACCESSION UST 30. Rept. for 1 Nov-
30 Nov 59 on Contract AF 33(616)6564; continuation of
AF 33(616)5171. 15 Dec 59, 21p. 68 refs. REIC
Accession List 30; AD- 230 184.
Order from LC mi$2.70, ph$4.80 PB 153 258
This report released for sale to the public 16 Dec 60.
Contents:
Electrical and electronic systems
Polymeric materials
Fuels, lubricants, and hydraulic fluids
Metals and alloys
Organic chenucals
Inorganic chemicals
Dosimetry
Space radiation
Stevens Inst, of Tech. , Hoboken, N. J.
LITERATURE SURVEY Oti THE EFFECTS OF
RADIATION ON ELECTRON TUBE MATERIALS^ by
E. R. Johnson. Quarterly rept. no. 10, 1 Sep-30
Nov 59, on Contract DA 36-039-8C-73146. [1959] 60p.
9 refs; AD-232 188.
Order from LC rpi$3. 60. phf9. 30 ~ PB 149 714
Subminlature tube types Sylyania 6111, 5902, 6943,
5840, 5905, subminature gas thyratron tN-pe 5643, and
ceramic tube types SN-1724, SW-2225, and SN-2146,
when exposed to a total integrated dose of lO'^ nvt,
show no significant change in electrical charaaeristics.
A decrease in dynam ic hum has been found in the irr'adi-
ated tubes. (Author) (See also PB 149 713)
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Aeronautical Research Lab. , Wright Air Develop-
ment Div., Wright -Patterson AFB, Ohio.
THERMAL ANALYSIS OF SPACE SUITS IN ORBIT,
joy Thomas F. Irvine, Jr. (North Carolina State Coll.)
and Kenneth R. Cramer. Rept. on Equipment for Life
Support in Flight Operations. May 60, 21p. WADD
Technical note 60-145.
Order from OTS $0.75 PB 171 143
The thermal analysis of a model space suit in orbit is
presented as a guide for designers and as a basis for
more extensive studies for the prediction of a suited
man's thermal environment in an earth orbit. Results
demonstrate the feasibility of passive suit-tempera- '
ture control through the proper choice of materials
and surface spectral properties. (Author)
(^rtermaster Field Evaluation Agency, Fort Lee,
Va.
AN INVESTIGATION TO DETERMINE A PRACTI-
CAL. PREQSE AND RELIABLE METHOD FOR DE-
TECTING LEAKS IN RUBBER HANDWEAR, by James
C. Perkihs, Jr. Mar 60, 35p. 7 refs. Technical rept.
R-6; FEA MRS 6001.
Order from LC mi$3. 00, ph$6. 30 PB 149 674
This study was conducted to develop a practical, pre-
cise, and reliable method of inspecting rubber protec-'
live handwear under field test conditions. Three
methods were tested They are (1) high definition
fluoroscopy, (2) halogen detector and, (3) infrared
nitrous oxide analyzer. Each of these methods em-
ploys a tracer gas and a detector or sensing element.
The leak detector tracer gas (halogen) was found to be
the most satisfactory method for nuking determina-
tions of rubber handwear serviceability. (Author)
PHYSICS
Army Research Office, Washington, D. C.
ARMY RESEARCH TASK SUMMARY, FISCAL YEAR
I960. VOLUME 3. PHYSICS (PART I). 4«6p.
Order from OTS $3. 75 PB 171 002
Contents:
Multiple subfields of physics
Astronomy and astrophysics
Atomic and molecular physics
Biophysics
Electricity and magnetism
205
Electromagnetic wafes
Electron physics
Heat and ihermodyn^inics
Light and optics
Nuclear physics
Sdund and acoustics
(See also PB 161 131 )
WBfrt
lyilr
Army Research Oifice, Washington. D. C.
ARMY RESEARCH TASK SUMMARY. FISCAL YEAR
1960. VOLUME 4. I PHYSICS (PART U) AND GEO-
PHYSICAL SCIENCES. 470p.
Order from OTS $3,] 75 PB 171 (»3
Contents:
l^ysics (Part II):
Mechanics (except ablid state)
Solid state physics
Geophysical Sciencas:
Cartography and geodesy
Earth physics j
Geography j
Geology and geophysics
Meteorology
(See also PB 161 13^)
Centro di Studio p4r la Fisica Delle Microonde
(Italy). !
DESIGN, DEVELOBMENT AND TEST OF AN AD-
VANCED. FIXED BOSmON RADIO ASTRONOMY
ANTENNA, by P. R Checcacci, LRonchi, and
V. Russo. Final retot. on Contract AF 61(052)234,
Apr 60, 37p. 6 refsi AFCRL-TR-60-186.
Order from LC mi$P.00. ph$6. 30 PB 152 201
A type of microwav^ antenna was previously studied
which seemed to present particularly suitable features
for application to radioascronomy. This antenna may
be called a 'steppedjzone spherical mirror'. The pre-
sent report studies a method for improving the perform-
ance of this mirror.! and, at the same time, investi-
gates the possibility of ofacaining other mirrors with
more suitable feacufes than the preceding one, starting
from the same prii^iple at stepping the reflecting
surface.
i Acoustics
Chesapeake Instri^nent Corp. , Shadyside, Md.
RADIATION IMPEQANCE C«' ARRAYS OF FINITE
SPHERICAL SOURCES, by B. D. SimmoAs. Technical
rept. on [Cootract Moor -3067(00)] 15 Aug 60, 19p.
14 refs. CIC no. 133; AD- 243 127.
Order from LC nii$l2.40. pfa$3.30 PB ISO 833
Calculations were ctxAined of the radiation impedance
at acoustic arrays donsisting of simple spherical
sources at finite ratfii. These results apply to array*
at low frequencies Such that the dimensions of individ-
ual elements are si«aU compared to a wavelength. By
varying the radii at the spheres the overall dimenaions
of the array can be Iraried. or, with given dimension
d the array, the amount of packing can be varied. Re-
sults are given for the radiation resistance of square
arrays consisting of sixteen and twenty-five elements.
(Author) , . ,
John Carroll U. , Cleveland, Ohio.
ULTRASONIC ABSORPTION IN ETHYL ACETATE, by
E. F. Carome and S. R. Burlage. Technical rept.
no. I on Contract Nonr-2577(01). 15 Dec 59, 7p.
8 refs. AD-230 596.
Order from LC mi$l. 80, ph$l. 80 PB 152 150
Measurements of ultrasonic absorption in ethyl aceute
in the range 2 - 20 Mc indicate the relaxation frequency
below 10 Mc reported by various investigators is spur-
ious and probably due to diffraction effects. (Author)
Naval Research Lab. , Washington, D. C.
THE MECHANICAL SELF RESISTANCE AND THE
MECHANICAL MUTUAL RESISTANCE OF AN UN -
BAFFLED RIGID DISK (Ka< 1) RADIATING SOUND
FROM A SINGLE FACE INTO AN ACOUSTIC ME-
DIUM, by S. Hanish. Interim rept. 24 Oct 60. 54p.
12 refs. NRL rept. 5538.
Order from LC mi$3.60, ph$9.30 PB 149 296
The acoustic radiation properties of an unbaffled. rigid,
oscillating disk (ka< 1) are reviewed in the light of
Gutin's theory of superposition and Bouwkamp's analysii
Two such unbaffled. rigid pistons are placed in juxta-
position in a plane and are driven with equal velocity
amplitude. Formulas for the radiation characteristic
and mechanical radiation resistance of the pair as a
function of separation distance d are derived. From
these formulas the mechanical self- resistance coef-
ficient and the mechanical mutual resistance coefficient
for separation distance up to kd = 2^are deduced .
Tables of self and mutual radiation Ksi stance for an
unbaffled, rigid disk are computed out and printed in
the appendix. (Author)
Naval Research Lab.. Washington, D. C.
THE RADIATION MECHANICAL IMPEDANCE OF
MULTIZONE RADIATORS IN A PROLATE SPHE-
ROIDAL BAFFLE, by & Hanish. Interim rept.
4 Oct 60, 12p. 4 refs. NRL rept. 5515.
Order from OTS $2. 40, ph$3. 30 PB 147 964
The velocity potential at many zonal radiators in a
rigid prolate spheroidal baffle each vibrating with a
given velocity amplitude and phase is derived analyti-
cally. The total mechanical radiation impedance of
the array is then derived from the velocity potential
by a series at integrations, lixlividual elements at
this total are identifiad as the self and mutual radi-
ation impedance of two ring zones. Procedures for
simplifying numerical computation are discussed.
Actual computations are reserved for a companion
report. (Author)
Naval Research Lab.. Washington, D. C
THE USE OF SPHEROIDAL WAVE FUNCTIONS IN
THE EMPIRICAL DESCRIITICW OF SCALAR WAVE
FIELDS, by S. Hanish. Interim rept. 4 Oa 60. lOp.
4 refs. NRL rept. 5514.
Order b-cm LCmi^I.SO, pt]$1.80 PB 147 963
206
The empirical description of scalar wave fields by
gpherical wave functions with experimentally deter-
mined expansion coefficients is critically reviewed
and Its restrictions to spherical surfaces at measure-
ment noted. To avoid these restrictions a modified
(beory is developed which abandons spherical wave
functions in favor at spheroidal wave functions thereby
permitting measurement over ellipecndal surfaces.
Formulas are developed for determining the analytical
and empirical expansion coefficients of scalar wave
fields in spheroidal wave functicms. Traveling waves
and standing waves in echoic chambers are analyti-
cally separated, and formulas for the far-field direc-
tivity patterns are obtained. (Author)
Electricity and Magnetism
)
British Columbia U. (Canada).
WORLD WIDE CHARACTERISTICS OP GEOMAG-
NETIC MICROPULSATIONS, by J. A. Jacobs and
K. Sinno. Scientific rept. no. 2 on Contract
AF 19(604)4068. 11 Apr 60, 59p. 22 refs. AFCRC-
TN -60-436; AD- 243 464.
Order from LC mi$3. 60, ph$9. 30 PB 152 208
A detailed investigation Is carried out on geomagnetic
micropulsations recorded by rapid-run magnetograms
durii^ the I. G. Y. (1957-1958) from 17 obaervatories
as widely distributed geographically as possible. A
number of well defined cases (14 Pt's and 3 Pc's) are
investigated in detail. Diurnal and world wide char-
acteristics are derived and the equivalent overhead
current systems \*hich may .give rise to the micropul-
sations are constructed. Attention is drawn to the oc-
currence at long period, continuous pulsations (called
LPc's) which have a longer period than Pc's and usually
appear simultaneously with Pc's in polar regions.
(Author)
Electrical Engineering Research Lab. , U. of Texas,
Austin.
INITIAL OBSERVATIONS OF EARTH CURRENT
AND MAGNETIC FIELD MICROPULSATIONS, by
George Hopkins, Jr. , P. F. Law and R. R. Boothe, Jr.
Rept. on Contract Nonr-375<01). 23 Dec 59, 29p.
3 refs. Rept. no. 112.
Order from LC mi$2. 70, ph$4. 80 PB 152 159
This may be considered a progress report on the de-
velopment of systems for the measurement of geomag-
netic and earth current micropulsations. The present
systems and their development are outlined, along
with current plans for their improvement and refine-
ment. Typical data samples and preliminary power
spectra are Included. (Author)
Electrical Engineering Research Lab. , U. of Texas,
Austin.
A SURVEY OP THE CHARACTERISTICS AND
ORIGINS OF GEOMAGNETIC MICROPULSATIONS,
by P. F. Law and R. R. Boothe, Jr. Rept. on Contract
Nonr-375(01). 1 Dec 59, 21p. 19 refs. Rept. no. 111.
Order from LC mi$2. 70. ph(4. 80 FB 152 158
This report is a review of observations and theories
pertaining to very low frequency fluctuations of the
earth's magnetic field as reported by investigators in
the field. These fluctuations, called micropulsations,
are of the order of a few gamma in amplitude and have
periods ranging from 0. I second to 10 minutes. Re-
ported observations include the frequency of occur-
rence of these pulsations and their diurnal variation,
the amplitude and duration of the pulsations, and solar-
geophysical relationships. Several theories given in
the literature as to the origin of these micropulsations
are presented, the [n'inciple argument being based
upon hydromagnetic oscillations initiated by the in-
vasion of ionized particles of solar origin. A method
of ion density prediction from micropulsation data is
also included. For detecting micropulsations, the
principal types of sensing elements used are large
air-core coils or smaller mu-metal core coils. Vari-
ous types of D-C amplification systems are used to
obtain the necessary gain. These systems include in-
tegrating circuits having about one minute time con-
sunts to give an output which is proportional to the
measured flux density. (Author)
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
A SIMPLE NULL-INCHCATING SATURABLE CORE
MAGNETOMETER FOR THE C«TECnON OF
STATIC MAGNETIC FIELDS, by E. P. McCurley and
C. Blake. Rept. on Contract AF 19(604)5200.
15 Apr 59, 8p. 1 ref. Technical rept. no. 202;
AD-215 625.
Order from LC mi$l. 80, ph$l. 80 PB 152 301
The construction of a simple null -indicating magne-
tometer employing a saturable core is described. The
device is useful for detecting static magnetic fields of
the order of 0. 1 millioersted. It was built to enable
the establishment of a near zero magnetic field over a
limited volume by nreans of pairs of Helmholtz coils.
A test signal incorporated into the instrument affords
a check on the sensitivity. (Author)
National Cash Register Co. , Hawthorne, Olif.
RESEARCH ON MAGNETIC ROD STORAGE AND
SWITQ-nNG DEVICE, by A. J. Kolk. Final research
rept. on Contract AF 19(604)5890. 31 July 60, I05p.
18 refs. AFCRL-TR-60-I82.
Order from LC mi$5. 70. ph$16. 80 PB 152 520
This report presents the results of a study concerned
with the magnetic properties of thin film, iron -nickel
alloys electrodeposited in a Rod configuration. These
properties were found to be critically influenced by the
physical condition of the conducting substrate surface.
Silvered -glass aixl beryllium -copper substrates were
subjected to intensive investigation. The effects of
-varying other plating parameters such as current den-
sity, pH, bath compositiotk temperature, organic ad-
ditives, plating time, and the presence of an axial mag-
netic field were also studied. Electron micrographs
were made of the substrate surface and the plate at dif-
ferent plate thicknesses. An attempt was made to cor-
relate residual stress measurements with the proper-
ties of the plate. Preferred orienution in the plate was
investigated by means of X-ray diffraction' techniques.
Finally, a series of experimental switching curves
were detennined and a mechanism for the switching
phenomena proposed. (Author)
207
Office of TechnK
Washington, D-
FERROELECTRIC
Sep 60, 19p. 330 U
SB-434.
Order from OTS $<
Services, Dept. of Commerce,
AND FERROMAGNETISM.
OTS Selective Bibliography
OTS SB-434
A bibbography of reports listed in the two OTS monthly
abstract Journals: U. S. Government Research Reports
and Technical Traiislatlons . This bibliography in-
cludes PB reports, AEC material and translations on
ferrites, ferroelectricity and ferromagnetism added
to the OTS collection during the period 1950 to
October 1960.
Springfield Arwoiy. Mass.
MAGNETIC METHOD OF MEASURING DISPLACE-
MENT AND VELOCITY: APPLICATION AS FUNC-
TION GENERATOR, by H. P. Hatch. Kept, on Basic
Studies in Ordnanc* Engineering. 15 Aug 60, 15p.
SA-TR2O-60a5.
Order from LC mi$2. 40, ph$3. 30 PB 152 394
i$2.40.
A study was made |o investigate geometry and core
materials to increase the linear displacement range of
Springfield Armoryt magnetic displacement transducer,
to investigate a direct-current version responding di-
rectly to velocity cf nxxioo, and to explore the feasi-
bility of using ttiis device as a function generator, b
appears feasible from experimental work that displace-
meius greater than 5 inches can be measured. The $
output of the d. c. oxcited transducer is linear with re-
spect to armature f elocity. However, because of the .
large transverse response, the measurement of veloc-
ity appears impractical for all applications except
tfaoac in which the armature is constrained to only one
plane of motion, l^ie displacement transducer can be
described by a roc^ted cam. Experimental procedure
Is giren. and results discussed. (AUdlior)
1 U. , Mldit
Wisconsin U. , MWison.
USE OF THE FAHADAY EFFECT IN DETECTINC
SMALL CHANGES IN THE EARTH'S MAGNETIC
FIELD AND MEASUREMENTS OF THE FARADAY
EFFECT IN GASES AND VAPORS, by L. R. IngersoU
and D. H. Uebenberg. Final rept. for 15 June 50-[1959]
on Contract Nonr-07100. [i960] 36p. 21*-refs.
AD- 242 160.
Order from LC mifc3. 00, ph$6. 30 PB 149 909
A photoelectric mdthod of measuring magneto- optical
rotations as small as I" of arc was developed. The
apparatus was used initially to determine the small
magnitude shon period changes in the earth's local
magnetic field to a|i accuracy of 1 part in 1440 of the
horizontal component. Verdet constants at 22 wave-
lei^ths throughout the spectral range 3695 to 9875A
were measured for" the following gases, helium, neon,
argon, krypton, x^non, nitrogen, oxygen, hydrogen,
deuerium, nitrou^ oxide, carbon mottoxide. carbon
dioxide, sulfur heWloride, Freon- 12, sulfur dioxide,
ammonia, methane^ ethane, acetylene, propane, cy-
clopropane, ethyletie, n- Butane, isobutane, water
vapor, deuterium oxide, ethyl alcohols, methyl alcohol,
chloroform, ether, carbon disulfide, and carbon tetra-
cloride. The Verdft constants of the liquids were
measured also for the liquid of the last eight listed va-
pors. Pressure and temperature dependences were
measured in the ranges lOcm Hg to 220cm Hg and 20"
to 50^*0, reqjectively. Comparison is made with the
results of other investigations where possible and a
discussion of the results in terms of the current theory
is presented for some of the simpler gases. (Author)
Electronics
Baitelle Memorial Inst., Columbus, Ohio.
INVESTIGATIONS OF RARE -EARTH OXIDE CATH-
ODES, by J. B. Baker and G. B Gaines. Scientific rept.
no. 4 on Cootraa AF 19(604)5691. 1 Aug 60, I6p.
AFCRL-TN-60-977.
Order from LC mi$2. 40, ph$3. 30 PB 152 538
Thermionic emission was determined far a mixture of
neodymium and gadolinium oxides on refraaory- metal
bases of tantalum and molybdenum, as well as for an
additional sample on an undoped tungsten wire. The
emission level at 1400OC was about 0. 15 to 0. 35
amp/cm^ for all cathodes. Prospects appear good for
obtaining higher currents by adding reducing agents to
the coating. (Author) (See also PB 150 424)
Electronic Communications, Inc. , Timonium, Md.
SURFACE -WAVE PROPAGATION ON A DIELECTRIC
ROD OF ELLIPTIC CROSS SECTION, by Marcia J.
King and James C. Wiltse. Scientific rept. no. I on
Contract AF 19(604)5475. Aug 60, 70p. 10 refs.
AFCRL-TN-60-962.
Order from LC mi$3.90, phJlO.80 PB 152 524
The problem of wave propagation on a dielectric rod of
elliptical cross section is analyzed in detail. Formal
solutions are derived for the field quantities and propa-
gation constants for various modes, and some numeri-
cal results are also given. A special technique is em-
ployed to remove some of the complexity which arises
when the infinite- series representations are used In the
boundary condition equations. By a general analysis It
is found that field components may be represented in
one region by terms involving only Mathieu functions of
one specific order. The field components in the second
region must then be represented by an infinite series,
but the problem Is nonetheless sufficiently simplified
to permit one to obtain modal descriptions. The
elliptical solutions obtained here describe modes which
go smoothly over to the known circular modes as the
ellipae degenerates to a circle. Other elliptic modes
also appear to be poesible but are not present when the
ellipse goes to a circle. "Cut-off" behavior of several
of the elliptic modes is analyzed (in particular, for
eccentricity close to unity). As in the circular rod,
there appears to be one dotnlnant mode which has zero
cut-otf frequency. Certain simplifications which ap-
pear in the solutions are discussed for the case when
the ellipse degenerates to the flat "tape" . (Author)
Lockheed Aircraft Corp. , Sunnyvale, Calif.
IMPUCATIONS OF PARITY NONCONSERVATION AND
TIME REVERSAL NONINVARL\NCE IN ELECTRO-
MAOIETIC INTERACTIONS, by Mendel Sachs. Tech-
nical rept. 31 Dec 58, 32p. 23 refs. LMSD- 48373.
Order from LC mi$3.00, ph$6.30 PB 148 700
As ioveadgatiaa of impticaHoas d parity ncncansenra-
tioo and time reversal naoimrariance in electromagnetic
iiaeractians is carried out in terms at a theory wh4cfa
mBiotains the baaic poatulates of the theory d relativity
uid preserves Maxwell's field equations. The theory is
constructed by generahzing the electrcmagnecic four-
■if ijl ao aa to include an axial-vector part as well
aa a twaor part. The axial-vecUM- part is cbosen ao as
to reverse the roles played by the electric and magnetic
Qeld variables in interacdons with charged spin one-
luff partidea. A qualitative discussioa at atomic aad
paranugnetic reaooance spectra is given in the light of
tte present theory. It is pointed out that the effects of
dK tlKory are optimized when applied to bound systems
ft^ecxed to nonoeiaral electric potentials. (Author)
OafordU. (Gt. Brit.).
UM3ULAT0R EXPERIMENTS AND HARMONICS FROM
A lACROWAVE GAS DISCHARGE, by H. Motz and
0. Walsh. Technical note no. 7 on Contract
AF 61(514)1183. June 60, Up. 4 reft. AFOSR TN-
60-1043.
Older from ljCini$2. 40, |i43. 30 PB 152 487
Rome Air Development Center, Griffiss APB, N. Y.
IfBASUREMENT OF HALL VOLTAGES AT MICRO-
WAVE FREQUENCIES, by Aichony D. Ri«ari. Sep 60.
16p. 7 refs. RADC TN-60-164.
Order frotn LC mi|2. 40. pi]$3. 30 PB 152 406
The measurement of Hall voltages at frequencies of
3S00 and 9050 mc/s and its application to the measure-
ment of microwave power is described. The Hall crys
lals used were fabricated from indium arsenide and
iadiian arsenide phosphide, both members of the semi-
ooaductor class known as the intermetallic compounds.
Tbeae materials jvere chosen becauae they possess a
large electroo mobility at room temperature, and thus
exhibit a pronounced Hall effect capability. Measure-
aMK at power at a frequency of 3500 mc/s is dis-
CMaed. The results obtained show approximately two
orders of magntidue of improvement over other re-
ported work in this area. These are believed to be the
first reported measurements of a Hall vohageat micro-
wave frequencies with the intermetallic compounds and
indicate the feasibility of an automatic field power
meaauring inatrument uaing tt/e Hall effect. (Author)
Molecular Physics and Spectroscopy
Kansas State U. , Manhattan.
THE SPECTRA OF NFrRQCEN OXIDES. 0. THE
UREY- BRADLEY FORCE, CONSTANTS IN IM^ AND
THE INFRARED SPECTWJM OF SOLID Nj^b^. by
L C Hisatsune. Scientific rept. no. 2 on dontract
AF I9(604)22S5 and PukAic Health Research Grant S-63.
Feb 60, Sip. 29refa. AFCRC TN-60-277; AD-235 037.
Order from LC nii$3.60, phf9. 30 FB 148 716
Force constants have been calculated for nitrogen di-
oxide, nitrite ion. and dlnitrofen tetroxide. For tlie
latter molecule, aa IBM 6S0 DiKital Computer has been
programmed. The results of these calculations sub-
stantiate the assignment of the fundamentals made pre-
viously and also the existence of pronounced interac-
tion of the two oitro groups in N20^. The infrared
spectrum of N^^O^ in the solid phase between 2 and
35 u has been obtained. Approximate temperature de-
pendence of the solid spectrum has also been investi-
gated. The complete infrared and Raman spectra of
N2O4 are summarized and interpreted. (Author)
(See also PB 143 667).
Kansas Sate U. , Manhattan.
THE SPECTRA OF NITROGEN OXIDES. III. THE
SPECTRUM OF N2O3, by I. C. Hisatsune. Scientific
rept. no. 3 on Contract AF 19(604)2255 and Public
Health Service Research Grant S-63. Feb 60, 42p.
30 refs. AFCRC -TN -60-263; AD-235 038.
Order from LC mi$3L 30. ph$7. 80 PB 148 712
The infrared spectra of N2 O3 in the liquid and solid
phases, the infrared spectrum of N^^03 solid, and the
Raman spectrum of N^'*03 in nt>ethylene chloride solu-
tions are reported in mis document. Statistical entropy
calculations have been made which indicate that both
the torsional frequency and the potential barrier ugainst
internal rotation about the NN botid are very low. The
temperature dependence studies of the N2O3 solid .
spectrum have also been made and they show that an
unstable isomer of N2O3 exists. (Author)
Mellon Inst. , Pittsburgh. Pa.
INFRARED SPECTRUM OF SINGLE CRYSTALS OF
LIOH, LiOD AND LiOH LiOD, by R. M. Hexter. Rept.
on Contract AF 49(638)542. 16 Mar 60. 36p. 18 refs.
AFOSR-TN-60-404; AD- 243 658.
Order from LC mi$3. 00. ph$6. 30 PB 152 076
High resolution infrared absorption spectra of single
crystals of LiOD and of the solid solution LiOH- LiOD
are reported. These are compared with each other and
with the spectrum of monocrystalline LiOH. Compari-
sons with the spectra of Mg(OH)2 and Ca(0H)2 are also
made. The differences in selection rules for the two
types of hydroxides are discussed together with dif-
ferences in spectra to be expected upon changing the
mass of the cation and upon deuterium substitution.
The discussion is in terms of the current theory of the
spectra of such crysuls. It is concluded that the com -
plex spectrum of these minerals in the high frequency
region (2000 - 5000 cm^) is entirely due to OH" (or
OD") ion nxXion. The motion is quite localized; the
motions of the several OH' ions or the crystal are
pcnrly coupled. (Author)
Michelson Labs. . Naval Ordnance Test Station,
China Lake, Calif.
ADVANCEMENTS IN MICROSPECTROSCOPY, by
Robert F. Hummer. Jan 60, ^. 5 refs. Technical
Article 2; NOTS TP 2372; AD- 232 815.
Order from LC mi$L 80, ph$l. 80 PB 148 681
This article discusses some recent refinements in
color-translation equipment. It describes a new sys-
tem of translating invisible colors to visible ones so
that the application of the technique is more precise
and more useful to chemical and biological research
scientists. (Author)
209
Noyes Chemical ^ab. . U. of Illinois, Urbana.
RATE PROCESSED AND NMR SPECTRA. III. PROTON
EXCHANGE AND I HYDROLYSIS OF AMIDES, by
A. Saika. Technidal repc. no. 25 on Contract Nonr-
1834(13). 16 Dec $9. 21p. 17 refs. AD-230474.
Order from LC ni|$2. 70, ph$4. 80 PB 152 094
The chemical excl^I%e of the NH protons in pure
liquid N-methylformamide (NMF) and N-methylacet-
amide (NMA) and the hydrolysis of the compounds in
acid aolution procon magnetic resonance methods. The
activation energy required for exchange among the NH
protons is found to be 14 1 2 kcal mole" 1 for both NMF
and MNA. The ra|e constants of the acid hydrolysis
were determined it three different temperatures, giv-
ing activation enefgies of 13 £3 and 15 ^3 kcal nK)le*'
for the hydrolysis of NMF and NMA respectively. The
relationship between the proton exchange and the acid
hydrolysis is discussed, and it is proposed that the
N-protonated form oT the amides is that which under-
goes the acid hydflolysis. (Author).
University of Southern California. Engineering
Center, Loe Anoeles.
MOMENT EQUATIONS AND BOUNDARY CONOl-
TIONS FOR MAGNETO- GAS DYNAMICS, by
Hsun-Tiao Yang. Technical note on Contract
^AF 18(603)95. 29 July 60, 58p. 10 refs. USCEC
rept. 56-216; AFCiSR'TN-60-963.
Order from LC n^$3.60. ph$9.30 PB 152 549
Based on the work of Burgers and particularly of
Kolodner. momenl equations are obtained from the
Boltzmann equatio|i for a conducting gas in electric and
magnetic fields. The moment equations consist at the
conaervation equations of mass, momentum, and
energy with arbitrary stress and heat flux: and the
conatitutive equations of stress and heat flux. By
•ssumiRg the Gra(l distribution function and slight ioni-
zation, it is poesible to obtain relatively simple stress
and heat flux equations yielding single-fluid descriptior
al the gas mixture. The associated boundary condi-
tioaa are obtained by talcing the assumed distribution
function and applying conservation laws near the wall.
These moment equations and boundary conditions
together with MaxJweU's electromagnetic equations and
their boundary conditions form a determinate system
to describe the dynamics of a rarefield conducting gas
in electric and magnetic fields. This system includes,
as limiting cases, both the Grad thirteen- moment
equations for rarefield gases and the usual continuum
magneto-gas dynainic equations. (Author)
t
lid Sfate Physics
Av^o-[Everen] Research Lab. (Mass.)
THERMAL CONDUCTIVITY OF CLEAR FUSED
SIUCA AT HIGH TEMPERATURES, by Kurt L. Wray
and Thomas J. Connolly. RefX. on Contraa
AF 04(647)278. Fleb 59. 15p. 2 refs. Research
rept. 44: AD-211 !724.
Order from LC nf$2.40. ph$3.30 PB 149 669
The thermal conductivity of clear fused silica was
measured over the temperature range 300 - 2100^ in
an experiment which minimized radiative energy
transport. This was a steady state experiment involv-
ing the measurement of the electric current and volt-
age drop through a fine tungsten wire which was em-
bedded along the axis of a cylindrical silica rod. The
wire served both as a heating element and as a resist-
ance thermometer . Thermal conductivities were cal-^
culated by graphical evaluation of the rate of change dF
electric power with temperature at different tempera-
tures. The experiment yielded thermal conductivities
between 2.6 x 10"^ and 2.8 x 10"3 cal/cm sec°K at
roan temperature, and between 4.5 x 10" ^ and
5.5 X 10"^ cal/cm sec^K over the temperature range
1000 - 2100OK. (Author)
Aviation Medical Acceleration Lab. , Naval Air
Development Center, Johnsville, Pa.
ADAPTATION OF BENSON- LEHNER DATA REDUC-
TION EQUIPMENT FOR X-RAY DIFFRACTION
FILM MEASUREMENT, Jjy Enruna Fessenden and
Carl C. Clark. Rept. no. 2 on ProJ. MR005. 15-
0002.11. 31A»«60, 13p. 1 ref. NADC-MA-6029.
Order from LC ini$2.40, ph$3.30 PB 152 469
A description is given of the adaptation of Benson-
Lehner Data Reduction Equipment for use with routine
x-ray diffraction analyses of unknown biological crys-
talline materials. The calibration technique is de-
tailed. This method enables one to obtain both two
theu values and intensity evaluations direaly from the
film. A film shrinkage correction is encompassed in
the two theta values. (Author)
Banelle Memorial Inst. , Columbus, Ohio.
INFLUENCE OF CONDUCTIVITY GRADIENTS ON
GALVANOMAGNETIC EFFECTS IN SEMI-
CONDUCTORS, by R. T. Bate and A. C. Beer. Tech-
nical note no. 3 on Contract AF 49(638)222. 15 Oct 60.
19p. 13 refs. AFOSR-TN-60-1225,
Order from LC mi$2. 40, ph$3. 30 PB 152 760
An approximate solution is found of a boundary— value
problem arising from the continuity equation in an in-
homogeneous semiconduaor, leading to rotational
current vectors. Results are used to predict the ef-
fect of carrier-concentration gradients on magneto-
resistance. The predicted weak-field effects are es-
pecially significant in degenerate semiconductors and
a-type ni-V intermetallics wher^ the "intrinsic"
magnetoresistance Is small. In strong fields, even
small gradients in carrier concentration can com-
pletely alter the field dependence of the magnetore-
sistance. Experimental results indicate that trans-
verse currents, which do not occur in the simple case
discussed, do appear in general, and further perturb
the magnetoresistance. The influence of inhomo-
geneous magnetic fields is discussed briefly. (Author)
Cornell U. [Id»aca, N. Y. ]
SOME SOLID STATE STUDIES OF SILVER-DOPED
Wa>. by M. J. Sienko and B. R. Mazumder. Rept. on
Coittract AF 49(638)191. 19 Dec 59. 7p. 9 refa. AFOSR
TN-60-6.
Order from LC ml$l. 80. ph$l. 80 PB 148 690
210
A material corresponding to Ag Qip^O- has been
isolated from the thermal equilibratioh oi WC|o with
various sources of silver. Single crystal stixfies in-
dicate that it is orthorhombic (a =7. 35 A. b =3. 73 X.
»nd c = 3. 85 A) and that it conducts as a metal between
25° and 600°C.
Diamond Ordnance Fuze Labs. , Washington. D. C.
EFFECTS OF ELECTRO) BOMBARDMENT RATE
OH CONDUCTIVITY OF N-TYPE GERMANIUM, by
Robert A. <3oldstein. 25 Oct 60. 29p. 17 refs. Tech-
nical rept. TR-868.
Order from LC mi>2. 70, ph$4. 80 PB 152 918
The effects of electron bombardment rate on the con-
ductivity of n-type germanium crystals have been in-
vestigated. Six samples with initial conductivity of
about 0.8 (ohm-cm)"^ were irradiated with 4.6 Mev
elearons to a total dose of about 2.5x10^* elec-
trons/cm^. and the change in conductivity was meas-
ured as a function of irradiation rate. The decrease
in conductivity is shown to be strongly dependent upon
the irradiation rate. The carrier removal efficiency,
88 calculated from the conductivity change after room-
temperature anrtealing, was found to increase from
1.77 to 2. 34 for irradiation rates of 1.65x10^5 to
5.12x10'" electrons/cm^-sec. The irradiated sam-
ples were annealed at temjwratures up to 215°C. The
annealing behavior of all samples was found to be
identical, indicating no differences in defect configu-
ration. Six additional samples were irradiated with
1 Mev elearons to a total dose of about 7. 5 x 10*^
electronsZcm^, at irradiation rates (rf 6. 09x 10*^ to
1.30x10^* electrons /cm^- sec. The carrier removal
efficiency was found to be independent of irradiation
rate below about 10^^ electrons /cm -sec. A mecha-
nism to acclxint for the observed rate effect is
discussed. (Author)
Eagle -Picher Research Labs. . Miami, Okla.
INVESTIGATION OF INTEGRALLY COMPOSED
VARIABLE ENERGY GAP PHOTOVOLTAIC SOLAR
ENERGY CONVERTER, by L. E. Stone, J. B. Powderly,
and W. E. Medcalf. Technical summary rept. no. 1,
1 Sep-31 Dec 59 on Contract DA 36 -039 -sc -85246.
10 Jan 60, 41 p. 3 refs; AD- 232 286.
Order from LC mi$3. 30, ph$7. 80 PB 14? 705
This report released for sale to the public 16 Dec 60.
An investigation of integrally composed multiple
energy gap solar cells is described. The objective is
to contrast the efficiency and other characteristics of
Buch cells with the characteristics of conventional
single energy gap cells. The multiple band gap cell
under study in this project is a composite solar cell
made up of gallium phosphide and gallium arsenide.
Gallium arsenide single gap cells and the gallium phos
phide-gallium arsenide cells are studied in parallel.
Fabrication of approximatelv 20 sinjtle energy gap
gallium arsenide solar cells was carried out and pro-
cedures for evaluating efficiency, contact resistance
and diffusion depth were established. Six composite
variable gap cells were composed of gallium phosphide
and gallium arsenide with the larger energy gap mate-
rial (gallium phosphide) located at the front of the cell
facing the incident radiation. A comparison of the
characteristics of a single gap cell with that of a vari-
able gap cell showed: ( 1 ) both cells were fabricated
from the same gallium arsenide crystal and fabrication
techniques were identical except that phosphorus was
diffused in one crystal to form the gallium phosphide
portion; (2) the 2 cells had very low and almost identi-
cal contact resistance, and rather high but itearly
identical sheet resistance: (3) the composite cell had
1. 4X greater short circuit efficiency and 2X greater
maximum power efficiency; and (4) the composite cell
had a conversion efficiency of 3. 785^ at 1 ohm load.
Problems of depth of junction, depth of phosphorus dif-
fusion, sheet resistance and lifetime in the diffused
area are being studied with the purpose of increasing
tiie junction efficiency in both single gap and composite
variable gap cells. (Author)
General Electric Research Lab. . Schenectady, N. Y.
THE DIFFUSION RATE OF U IN Si AT LOW -TEM-
PERATURES, by E. M. Pell. Scientific rept. no. 3 on
Contract AF 19(604)5551. 28 Mar 60, 16p. 9 refs.
AFCRC-TN-60-357; AI>235 629.
Order hrom LC mi$2. 40, ph$3. 30 PB 149 063
The method of ion drift in the electric field of an np
Junction has been used to measure the diffusion con-
stant of lithium in silicon between 25° and 125°C. When
tliese data are combined with previous high tenmcrature
data, there is obtained D - (2. 5 ± 0. 2) x 10*-* exp
[- (a 655 ± . 01)q/KT] cm^/sec.
General Telephone and Electronics Labs. , Bayside,
N. Y. .
ANALYSIS OF TRACE IMPURITIES IN SILICON
CARBIDE, by R. L. Rupp and G. H. Morrison. Scien-
tific rept. no. 2 on Contract AF 19(604)4944. 7 July 60,
74p. 14 refs. ERD-TN-60-758.
Order frtm LC miK 50, ph$12. 30 PB 152 434
Investigations have resulted in an emission spectro-
graphic technique wherein the sensitivity has been in-
creased by two to three orders of magnitude. Re-
finements in each of the three major components of
emission spectroscopy, namely the light scource, the
optical system, and the detector have yielded increased
sensitivity, with the most marked results being achieved
through a better understanding of the volatilization-
excitation processes uking place in the light source.
Studies using silicon carbide as a matrix have shown
that increased sensitiviry is most pronounced in the
case of the more volatile elements, i. e. , As. Hg. P,
Pb, Sb. Sn. Tl. and Zn, with Hg and P having been
detected down to 5 parts per billion as compared to
sensitivities of the order of 10 to SO parts per million
previously obtainable.
Included in the report are: Spectrographic analysis of
high purity nickel, by Richard L, Rupp, George L.
IQecak, and George H. Morrison, pub. in Analytical
Chemistry 32:931-932. July 60
Spectrographic analysis of high purity •illcon carbide.
by George FL Morrison, Richard L. Rupp, and
George L. IQecak. pub. in Analytical CKemistry
32:933-935, July 60
211
U. (isrit
.161
Heta-ew U. (l^rlel).
NUCLEAR RESOIANCE ABSORPnON IN Dy*
SITUATED IN 0^2^ AND DYSPROSIUM IRON
GARNET, by S. fXer. P. Avivi and others. Teclmical
ncte no. I on Coi^tract AP 61(052)347. July 60, 12p.
7 refs. AFOSR-tN-60-1041.
Order from LC T$i%2. 40, ph$3. 30 ' FB 152 4S0
Tl^ recoil-free qesooant absorbtion at the 26 kev
/-r«y ( f'^A X 10" 8 sec) emined in the decay of
Tbl6r by absorb^s containing Dyl6l has been inves-
tigated. High Moasbauer efficiencies at room tem-
peratures have been observed for sources and ab-
sorbers in the form d oxide and rare earth iron gar-
net. The line shi^pes obtained were very broad, even
up to 100 times die natural wiifth, and showed no re-
solved sharp line^. The broad lines are iuerpreted
as due to a wide Complicated hyperfine specirian
wfaoae details ha^e been smoothed out by transitions
between magnetic sub- levels induced by paramagnetic
relaxation. In th< rare earth iron garnet, the ex-
change field acting on the rare earth ioo should de-
couple the nucleat and electron spins. The effective
magnetic field at the nucleus in the rare earth pmet
is about 2 X 10^ joe. (Author)
Hughes Aircraft
Co. . Cuhrer City, Calif.
ORGANIC SEMICONDUCTCm STUDY, by J. B. Ruat.
F. A. Haak and j. P. Nolu. Rept. for 1 July 58-
30 Sep 59 on Non-^Metallic and Composite Materials,
Contract AF 33(616)6024. June 60. 67p. 18 refa.
WADO Technical rept. 60-1I1.
Order from OTS 1 1.75 PB 171 177
Experimental results for the temperature dependence
of the resistivity ^e presented for thirteen organic
compounds. Exp^imental results regarding the
rectification properties at copper phthalocyanine and
other netal derivatives ol phthalocyanine are pre-
sented. A teioative theory based on the formatioa at
a space chsrgc dt^ to the presence of an oxidizing
afsnt in the systefn has beien developed. Preparatlona
for the study at ttie effects of high electric fields on
anthracene and phenanthrene are discussed snd some
qualitative resulta are presented. (Author)
Illinois U. [Urfasba].
DIFFUSION IN A FERROMAGNETIC ALLOY, by
James Stanley and Charles Wert. Rept. en Contract
AP 49(638)672. 7 lune 6a 26p. 8 refs. AP06R-TN-
60-883. I
Order from LC mi$2. 70. ph)4. 80 PB 152 291
Diffusion constants in an alloy of Fe ♦ ISJJV have been
determined over a wide temperature range by a com-
bination of radioactive tracer and anelastic methods.
The region of measurement extends over s consider-
able interval on bi)th sides of the magnetic Curie tem-
perature. The daqa show a pronounced effect of ferro-
magnetic spin -ordering on diffusion. Diffusion in the
well ordered ferromagnetic state is abou 100 times
slower than would tbe expected from extrapolation of
dau in the paramagnetic region. Part of this retards-
tion appears to be an increase in the activation energy
and part a decrease in D^. (Author)
Istituto Elettrotecnico Nszionsle "GaUleo Perrarir'
(Italy).
REMARKS ABOUT THE INTERPRETATION OP
THERMOLUMDCSCENCE. by G BonfiglioU,
P. Broveno. and C. Corteae. Technical note no. 1 on
Study of Traps in Dielectrica by Thermoluminescence
Experiments, Contract AF 61(062)328. [1960] 7p.
12 refs. AFOSR-TN-60-II43.
Order from LC nii$l . 80. pfa$l .80 PB 152 451
Lincoln Lab.. Mass. Inst, of Tech.. Lexingian.
ON THE BAND STRUCTURE OF TRANSTTION
METALS AND THEIR ALLOYS, by J. B. Goodenoi^.
Rept. on Contrsct AF 19(604)5200. 1 Sep 59, 60p.
117 refs. Technical rept. no. 208; AD- 231 241.
Order from LCini$3. 60. 1*1)9.30 PB 150 5%
A departure from the conventional approach to the
energy-band problem is achieved in two ways: fir«, it
ia aasumed that, for elements of the first long period,
cubic crystaUine fields sitfficiently separate the
atomic d states tfast several d subbands are formed
from linear combinations of primarily one or the
other of the two subsets eg and t2- at atomic d orbit-
als; second, the relative energiea of the varioua aub-
bands are first obtained from quakitative physical
argumema abou the multielectran problem chat intro-
duce intuitively the spin correlations and hence the
characterization of the subbands, the one-electron
description being used separately for each subband
only after their characterization and relative energy
have been specified. SimpUfied density-of- states
curves for the b. c.c. and f.c.c. traiudtion elements
are constructed with the aid of available experiment^
and theoretical information. These conatructions are
shown to provide a conalatcni interpretation for the
wide variety of band- structure-dependent properties
of the transition elements thst hsve been messured.
The poatulst^ snd resulting bsnd nwdel for trsnsitios
elements are extended to various disordered, sub-
stitutional alloya. The principles br the constructioa
of s bsnd model for the trsnaitian elements are ap-
plied to some ordered, substitutional slloys. (Author)
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
SOLID STATE RESEARCH. Quarterly progress rept.
on Contract AP 19(604)5200. 15 Jan 60, 95p. 71 refs.
APCRC TN-60-IOOa AD- 234 915.
Onler from LC nii$S. 4Gl pl41S. 30 FB 153 251
This report released for sale to the public 14 Dec 601
Contents:
Semiconductor device design
Chemistry
Metallurgy of materials
Bsnd structure of solids
Micrcsfsve snd magnetic properties of mstter
Magnetic materials
Magnetic films
Semicondbcting components
Display techniques
(See also FB 150 603) I
212
litoryland U . , College Part.
ON THE VIBRATION SPECTRUM OP A DISORDERED
LINEAR LATTICE . I . by ] . Mahanty . Rept . on Con-
tract AF 49(638)399. Oct 60. 9p. 7 refs.Dept. of Phys-
ics, Technical rept. no. 198; AFOSR-TN-6Q-1124.
Older from LCmi$ 1.80, pfa$ 1.80 , » 152 447
la lUs psper the average eigenf requency equation of a
disordereid t#o-companent linear chain is derived by a
direct algebraic mednd. It is shown that the moments
of die frequency spectrum can be evaluated easily
from tliis equation. (Author)
[Materiala] Resesrcfa Lab. , U. of CaUfomia.
Berkeley.
0BPORMAT1GN AND FRACTURE OP MA(94BSIUM
■CRYSTALS, by J. D. Mote and J. E. Dam. Techni-
cal i«pt. no. 6onContracx.DA O4-200-5O7-ORD-171,
T. O. 6. 6 Mar 59, 34p. 10 refs. lER aeries no. 73.
issue no. 7; OOR rept. 821.6; AD-215 281.
Oder from LC mi$3.00, pt46. 30 FB 149 656
TMs tavestigstion waa undertaken to study the eOectB
of pUed-up srrsys of dislocations on inducing slip,
laiaiiai. sad fracturing in msgnesium UcrysuLs,
tsflnaaiy oriented snd tested in tension. Piled-up
arrays of dislocations st the grain boundary could,
lasler appropriate conditiona, induce alip, twinning
aad cracking.
Materials Resesrch Lab. , U. of California, Berkeley.
VACANCY CLUSTERS IN ALKAU HAUDE CRYS-
TALS, by C A. Johnson and E. R. Parker. Technical
rept. nou 3 on Ductile Ceramics Resesrch, Contract
AF 49(638)601, ARPA Order not 24-59, Task 2. Aug60,
76p. 46 refs. lER series dol 150. issue no. 2; AFOSR
TN-60-979.
Order from LC mi$4. SO. pb$l2. 30 FB 152 427
11k possibility of the fbrmation of small dislocation
loops la alkali halide crystala by ttie precipitation of an
eaoeaa of vacancies is cUscussed on the bssis of the
Bom-Mayer theory of cohesion in ionic crystals. It is
rinvB that there are strong attractive interactions
amoag vacancies and vacancy cluatera in the alkali hal-
idea. Arguments concerning the effecta of these inter-
actkaa on the energy of a vacancy duater of arbitrary
Aape and aize are preaente± b is shown that these
arguments lead to the conclusion that vacancy precipi-
tatea in the alkali haiides will predominanUy be in ttie
form of monolayer plates, aa required for dislocstion
in contrsdicdon to previously advanced ar-
which predict die formation of apheroidal pre-
(vdda) on the baaia of aurCace energy consid-
The conclusion that monolayer vacancy pre-
cipitates srill iM^donvinate ia reached by considering in
detail die aequence of renctJons leading to the fbrma-
doa of planar and aplieroidal vacancy clustera. and im-
posing tiie requirement that a cluster grow in such a
way aa to keep ita energy a minimum. It is shown thst
die formstlon of spherotdsl vscancy precipitates is in-
hibited by the sppearance of high energy clusters in
the sequence of reactions lending to a apheroidal
precipitate. (AuiIkv)
Ohio State U. Research Foundation. Columbus.
OXIDATION C»» SILICON IN STEAM, AND SNOW
PLOW EFFECT, by Dawon Kahng and M. O. Thurston.
Quarterly technical rept. no. 2, I Apr -30 June 59. on
Resesrdi on Diffusion of Impurities into SiUcon
Throi«h an Oxide Layer, Contract DA 36-039-sc-
83874. July 59. 17p. 2 refs. Rept. 896-2; AD- 225 722.
Order from LCmi$ J. 8a pl4 1-80 PB 152 186
An additional marlter experiment by means of radio-
active phoapbDrus confirmed the earlier result diat the
oatidation of ailicon in steam occurred at the oxide -
allioon interface. The anew plow effect produced in
course of fsst ootidstion of silicon wss examined. A
simple aiMlysis of the snow plow ^ect shows the
dopant in ailicon redistributes itself ao that the con-
centration near the ailicon surface is nKxlified. In thef
case of phosptioriis the concentration increased by a '
factor of 1. 6. If the loss of the freed impurity into the
notide Isyer is negligible, the surfsce concentration in-
crease depends on the diffusivity of the impurity in
silicon. For some impurities, for instance arsenic,
an increase of as much as by a factor of 3 is predicted
under s given condition. (Author)
hctflc Semiconductors, Inc. , Culver City, Calif.
STUDY OF SURFACES IN SEMICONDUCTOR DE-
VICES; by A. L. Hsrrii«ton and M. F. Millea. Final
technical rept. for 15 June 58- 15 June 59 on Contract
DA 36-039- sc-78049. fl959] 48p. PSI rept. no.
3000:21-4-0: AD- 229 944.
Onler from LC mi$3. 30. ph$7. 80 PB 149 f67
The sensitivity of the electrical properties of high-
lemperature-generated silicon oxide films on silicon
diode surfaces to specific impurities introduced by
diffusion during oatidation is considered. The delete-
rious effects on diode electrical da racteristics proAiced
by diffusion of such impurities into the oxide and the
adjacent silicon during high-temperature oxidation are
eliminated by resorting to relatively low-temperature
OKidation in high-pressure steam. The effect of heat
treatment on the reverse current in silicon p-n junctions
has been investigated. (Author) (See also PB ISO 812)
Stairford Research Inst. . Menlo Park, Calif.
THE INTBRACTKW OP SLOW ELECTRONS WITH
INSULATING CRYCTALS. I. THE ABSORPTION OO-
BFFiaENT FOR PURE AND IRRAIXATED MgO. by
Charlea J. Cook and William J. Fredericks. Rept. on
Contract AP 49(638)353. 31 Mar 60. 20p. l^ refs.
SRI Projects SU-2741 snd SU-2480: APOSR-TN-60-
269; AD-234 921.
Order from LC nil$2. 4a ph$3. 30 FB 148 671
An Bttempt was made to determine the absorption co-
efficient,^ a. for electrons incident on MgO and irra-
diated K^gO when the impacting ener^gy ranges from
a 2 ev through the conduction band (about 7. 3 ev). It
waa found that electron trapping was so severe that the
crystala would not therrmlly discharge at tempera -
cures below 350^. Consequently, the charged crys-
tala were neutralized by a less satisfactory teduiique.
high energy electron bombaufciieut.
'l
Uppsala U. (Swtxlen).
THE CRYSTAL STRUCTl/RE OF RujiBg, by Jan
AseliuB. Techiuoal note 17 on Ckxitract AP 61(062)40.
3 Aug 6a 16p. 1« refs. AFOSR-TN -60-797.
Order frooi LC i|i$2. 40. ph$3. 30 FB 152 452
The powder phoCdgraph gave the foUowing,dimen8ion8
at the o(;thorhom|>ic i^c cell: g z 11. tQo A, ^ x
11. 342 A, c = 2. |36 A and Lf = 373. 4 A^. It is evident
that RuiiBg is oithorhcmbic. (See also PB 142 588
iithoi
UppMlaU. (Sweden)
A NOTE ON THE COMPOSmC«« AND CRYSTAL
STRUCTURES OP MnB2. MngSi, MnsSia AND FeSi2,
by Bertil Aronsson. Technical note no. 16 on Contract
AF 61(052)40. 20 July 60, 14p. 14 refs. AFOSR-TN-
60-686.
Order from LC 4i$2. 4a ph$a 30 PB 152 453
The existence of a manganese diboride. MnB2- with
the AlB2-8tructune has been confirmed. Faint super-
structure lines o* the powder photographs of alloys
containing MnsSi indicate that in this phase, as in
FesSi, some ordering of the silicon and metal atoms
ukes place at temperatures below lOOO^C. The re-
ported crystal stfuctures of Mn5Si3 and FeSi^ have
been confinned alid refined with single crystal data.
(Author) I
UppsaUU. (Sw^n).
STRUCTURAL FEATURES OF NEW PHASES WITM
THE CEMENTITB AND RELATED STRUCTURES.
by Bertil Aronssofi and Stig Rundqvist. Technical note
no. 14 on Contract AF 61(062)40. 1 July 6a 20p.
31 refs. AFOSR pl-60-e84.
Order from LC nii$l. 40. ph$3. 30 n 152 454
Uppsala U. (Sweden).
X-RAY INVESTIGATIONS ON Me-Sl-B SYSTEMS
(Me=Mn. Fe, Co). IL SOME FEATURES OF THE
Fe-Si-B AND MnrSi-B SYSTEMS, by Bertil Aronsson
and Ingvar Engstrtim. Technical note no. 15 on Con-
tract AF 61(052)40. 20 July 60. 23p. 7 refs. AFOSR-
TN-60-685.
Order from LC n[4$2. 7a phM 80 PB 152 455
mUJ
The main feature^ d the Fe-Si-B system at tempera-
tures around lOOO^C have been determined using X-ray
diffraction methods. Four ternary phases exist in the
metal-rich part c4 this system. Fe4 g6^i2B is isomor-
phous with C04. 7Si2B but has a more metal -rich com-
poaitioiL Fe5SiB2 has the Cr5B3 (CSi)- structure.
while the structure of a phase with the approotimate
composition Fe2Slo. 4B0. 6 **■ "o* '**" solved. There
is also a ternary Pe-Si-B phase that crystallizes in the
cementite- structure, but the equilibria in which this
phase is involved have not been clarified. In the
Mn-Si-B system. Which seems to be quite complicated,
particularly in the metal -rich part, a phase Mn5SiB2
(isomorphous with Fe5SiB2) has been identified.
(Author) (See also PB 139 342)
Westinghou^ Electric Corp. , East Pittsburgh, Pa.
MAGNETO.OPTICAL EFFECTS IN FERRIMAGNETIC
OXlDBSyJty P. Bailey. Scienti^c rept. no. 2, 15 June-
15 Sep 59, on Contract AF 19(604)5529. 8 Jan 60, 3ap.
11 refs. AFCRC-TN-60-121: AD-235 902.
Order from LC mi$3. 00, ph$6. 30 PB 148 981
The reflection coefficients of yttrium iron garnet, and
the (11 1) plane of •-Fe203, have been measured from
the near ultraviolet, through the visible and into the
infrared, up to a wavelength of 25 microns. The ab-
sorption spectrum of a (1 11) section of «-Fe203 was
measured at. liquid nitrogen temperature. Crystals of
the rare -earth iron garnets of terbium, dysprosium,
holmium, erbium and ytterbium were grown, and their
absorption spectra measured in the visible and near
infrared.
Theoretical Physics
Avco-Everett Research Lab. , Mass.
SCALING RELATIONS FOR PLASMA DEVICES, by
G. S. Jones. Rept. on "Research on Plasma Propulsion,
Contraa AF 49(638)659. Dec 59, 13p. 1 ref. Re-
search repi. 80; AFOSR-TN-60-367; AD-235 532.
Order from LC ml$ 1.80. ph$ 1.80 PB 149 067.
A derivation is given of a set of scaling relations for
plasma devices in which the dominant interparticle
interactions occur as a result of coulomb collisions.
These scaling relations have application in the avoid-
ance at redundant experimentation and in the design of
laboratory scale experiments to simulate the principal
conditions of interest to an engineering objective.
(Author)
Cambridge U. (Gt. Brit.).
THE COMPLEX STNGULARITIES OF PARTIAL-
WAVE AMPLTTUDES IN PERTURBATION THEORY,
by J. G. Taylor and A. E. A. Warburton. Technical
scientific note no. 10 on Contract AF 61(052)233.
June 60, 4p. AFOSR TN-60-1082.
Order from LCmi$ 1.80, ph$ 1.80 ,. PB 152 423
It is shown that the complex singularities which in-
validate Mandelstam's representation do not cause
complex singularities of partial-wave amplitudes.
This result is of importance in that the most useful
analyticity property for scattering amplitudes is in
practice a cut plane of analyticity for the partial-wave,
amplitudes. There may also be expected kinematic
complex branch points if the outgoing particles differ
from the incoming particles. (Author)
Electrical Engineering Research Lab. . U of
Illinois. Urbana.
INVESTIGATION OF MICROWAVE DUPLEXER
SWITCHING MECHANISMS, by S. Takeda. M. Roux,
and K. Rose. Quarterly progress rept. no. 3. 1 Sep^
30 Nov 59, on Contract DA 36 -039 -sc -7831 3. J
30 Dec 59, 40p. 14 refs. AD- 240 697. *
Order from LC mi$3. 00. ph$6. 30 PB 152 561
i
214
Tlieoretical aspects of compression and heating at a
plasma by Shockwaves are described on the basis at'
ginple thermodynamlcal considerations. The pres-
fure, density and temperai\ire ratios across the shock
froot as functions of the shock Mach number are given.
Excellent agreement is found between electron and gas
density ratios, for non- ionizing Shockwaves. Lower
electron temperatures than gas temperature is ob-
served, as expected, in the shock front. The peak of
electron temperature appears behind the shock front.
Comparison between theoretical and experimental
values of i/ei/n is made. Agreement and disagreement
between microwave and light Intensity measurements
are tentatively explained. Research on semiconductor
behavior in high level microwave fields was continued
using resonant cavity techniques at eight millimeter
wavelengths. A modification of the previous technique,
allowing greater precision in the iKerpretation at the
dau, was developed and aotne prelimioary. results
were obuined. Some calculations pertinent to this
technique and the general use of resonant cavity tech-^
niques for the study of deviations from Ohm's law in
semiconductors are discussed. The results of experi-
ments for investigating Hall effects at microwave fre-
quencies and the possibility at breakdown in InSb filmt
•re described. (Author) (See also PB 148 110) ^
Institute of Optics. U. of Rochester, N. Y.
CORRELATION THEORY OF STATIONARY ELEC-
TROMAGNETIC FIELDS. PART II: CONSERVATION
LAWS, by P. Roman and E. Wolf (U. of Manchester).
Technical note no. 2 on Contract AF 49(638)602.
Feb 60. 21p. 2 refs. AFOSR -TN-60-186; AD-235 570.
Order from LC mi$2. 70, p^4. 80 PB 149 070
Two new second order space -time correlation tensors
*Jk^*l' 12'''') ■'•'^ Ljk(»l' *2' ''^ "■* introduced, which
•re simple linear combinations of the correlation ten-
sors discussed in Part I of this investigation (xi, X2
■re position vectors of two points and T a time delay).
These new tensors are intimately related to certain
leneralizations of the (time averaged) energy density
and the energy flow vector. Differential equations
which Wj^ and Li|^ satisfy in free space are derived,
and from them four new conservation laws are de-
duced. In the limit Ji-»X2.T-*0 two of these laws
reduce to the usual laws (in time averaged form) for
the conservation of the energy and the nnomenum in
an electromagnetic field. The other two laws reduce
only to trivial identities in this limit, so that they
have no analogy in the framework at the usual theory.
(Author) I
Maryland U. , College Park.
RELATIVBTIC QUANTUM MECHANICS AND (QUAN-
TUM FIELD THEORY. VOLUME I. by J. Sucher.
Rc|X. on Contract AF 49(638)24. Sep 60, 22^ 11 refs.
fhysics Dept. technical rept. no. 192; [AFOSR] TN-
60-948; AD- 243 836.
Order from LC mlJ9. 90, ph$34. 80 PB 152 214
Scattering Theory
The basic equations or pictures of quantum mechanics.
Study of the U-operator in the interaction picture.
The S- matrix.
The derivation of formulae of stationary state scat-
tering theory.
An example: The nan- relativistic single-particle
Schroediager equuion.
The lore of 2ii:
Further topics in scatteriAg dieory.
An introduction to elementary particle physics.
Relativistic Wave Equations.
Lorentz transformations and Minkowski space.
A review at the theory of the electron as of 1926-7.
The development at the Dirac equation for a free
electron.
The Dirac theory of an electron in an external elec-
tromagnetic field.
Difficulties at the relativistic "c- number' theory and
related topics.
The quantization of fields.
Canonical quantization.
The second quantization of the non- relativistic
Schroedinger equation: Canonical and anti-canonical
quantization,
llie quantization of the Dirac field.
Appendix
Two- body reactions: Partial waves and unitarlty.
Maryland U. , College Park.
SINGLE -PARTICLE EXCITATIONS OF A DEGENER-
ATE ELECTRON GAS, by A. J. Qick am)
R. A. Ferrell. Rept. on C(»tracts AT(40-1)2098 and
Nonr- 1797(00). Dec 59. 35p. 18 refs. Dept. of Physics
Technical rept. 161; AD-235 627.
Order from LC mi$3. 00. ph$6. 30 PB 152 179
The continuum of single -electron excitstioos deter-
mines the properties of the degenerate electron ^s
and also many properties of metals. Lindhard's fre-
quency and wave number dependent dielectric constant
for the electron gas (Mat. Fys. Medd. 28:8. 1954) is
rederived by considering only these excitations. Col-
lective screening, and' thus plasma effects, are then
automatically taken into account by means of the
Kramers-Kronig relations which the dielectric con-
stant satisfies. Experiments on inelastic scattering
by meul films revealed the collective plasma excita-
tion but did not give much information about the actual
band structure and sin^e -electron excitations in a
metal. Sttidy of the plasmon can at best only give
some of the moments of the single -particle spectrum.
Using the dielectric theory as a guide, an experimet< *
is suggested here to gain information about the con-
tinuum directly. The most favorable scattering angle
for studying the single -particle excitations is found to
be just beyond the plasmon cut-off. (Author)
Microwave Research Inst., Polytechnic Inst, at
Brooklyn, N. Y.
A PROPOSED DIAGNOSTIC METHOD FOR CYLINDRI-
CAL PLASMAS, by J. Shmoys. Rept. on Contract
AF 19(60^143. 16 May 60, 30p. Research repc
PIBMRl-828-60; AFCRC TN-60-751.
Order from LC ml$2. 70. phH 80 PB 152 364
For a cylindrically synunetrlc plaama colunu whose
electron density N is a slowly varying, monotonically
decreasing function of radius r, it Is possible p calcu-
late explicitly both the diffraction panem from the
knowledge of N(r) and, conversely, N(r) from the
knowledge of the diffraction pattern. If the diffractiaa
21s
panem la obtained experimentally, N(r) can be calcu-
lated by a cumber aome numerical precedure. hatead
of doing chla, the diffraction pattern can be approKl-
mated by ooe at a (amily of convenient analytical ex-
pressiona for whidi tiw integratloa can be aanied out
eaaily. Altematlvtiy, one can attein|X to Infer N(r) by
assuming a functicnal form for N(r) wltb oa't or lapre
parameters, calrijare die dUfractiqn pattern mai, com-
pare it with die ob$erved one. (Audior)
New York U. CoJi. d Bngineerii^ N. Y.
ACX:URATE THOMAS- FERMI POTENTIAL DlSnU-
BUnON FOR THB ALKAU ICWS, by Harvey J.
Brudner. Technical repc. no. 3 on Electron Scattering
Project, Contract Nonr-28S(15). IS June S9. 41p.
ISrefs; AO-228 164.
Order from LC mi$3.». pl47.80 FB 148 722
Accurate solutions are presented to the Thamas-Perml
equation for the positive alkali ions. Tables d the
dimensionless potantial, 4 (and p")n the dimenslaB-
less length, x, are presented for Li*, Na*, K*, Rb +
and Ca* ; the cabuia(ted values are accurate to better
than 1 part In 10^. The statiatical model at tfae atom
is reviewed, and the method used to otaaia the solution
is described in deUil. The tables praaeaKd can be
used to determine carrespoDding Tliamaa-Fermi
charge distributiooB also, since ^ is proportioaal to
(#'7x). (Author) 1^ >
OsloU. (Norwsy)
ON OSaLLATIONS IN AN BLBCTRON PLASIA. by
AsbJ#rn KildaJ. Sclemific rept. no. 4 oa Coacract
AF 61(062)49. 1959. 2Sp. 14 refs. AP06X TN-60-
6»7.
Order from LC mi|2. 70. pfa|4 M) FB 152 41f
The works d Vlaao(r. Landau and Vaa gampwi on
classic plasma oscillation theory are reviewed. The
integral expression for the dispersion relation d plane
waves moving through a plasma is considered. It ia
shown tiiat the results of tlie authors mentioned may
be obtained by expressing the perturbatian in electron
density in two different ways, using tfae ordinary equa-
tion d motion in tb* one case, and the proper
Maxwellian equatioos in the other. EUmination d Ae
density variation from both equations yields the de-
sired dispersion relation. The same method is a^
plied to the case when an external magnetic field ia
present. The dispersion relation as found by Qroaa on
solving Boltznunn'a eqpatifai is then obtained, and the
frequency gaps are Lnailwd (Author)
Riyslcal Research ;LabL, Skiace Tech. Laba. , Inc..
Los Angeles. Calil
THE USE OF LOW IMPEDANCE TRANSMISSION
LINES IN PLASMA HEATING AND CONFINEMENT
STUDIES, by M. H. Dazey, V. Joscpfaaon. aul
R. F. Wuerker. Refjt. on Contract AF 04(647)309.
8 Aug 60, 33p. 7 rels. STL/TR-60-0000-09255.
Order from LC mi$l 00. pM6. 30 FB 1S2 034
An 18 kv type "C" tmnamissiaB Itee of 0. 28 ddna char-
scteriatic impedanct, 10 usee pulse length and 0. 5 iisec
rise time has been connected dirougb a triggered
hy IS cm la length nuntnaiftig a cylinder a
sure Dj 8*a. Experimental meaaurements d the
▼erae ptecfa heariiag and co^aement phenomena have
been made via smear photographs and magnetic protea.
The gas (25-500 A-Hg preaaure) was pre- ionized
5 paec prior to the appUcation d the transverse field
by a 2S0 kc/aec linear diacharge d several thousand
amperea. Application of the faat- rising constant-cur-
rent cransverae pinch field to the conduc tiqg plasim «
tS )i pressures vields both radial imiilosian velocittea
('^-'lO cnypsec) and aheath oaclllarory frequenciea
(1-2 mc/sec) expected from theory. Diffuhion d the
enemal field into the interior d tfae diamagnetic
plaama matrhra tfae rate of plaama loaa thitx^ the
enda d the confiaiag region; e. g. , at 2S u, longmidl-
nal streamiag vekxrltiea as high aa 20 cm/Vmec have
been observed. Ihe effect d the rate of the traasverae
Oeia on tfae magnetic piston velocity aad sbeath dilck-
neaa has been Investigated by varylag tfae aumbar d
tranaml salon line ■rrtiona. (Audior)
Ramo-Wooklri^ge Corp- . Lo* Aagelea. Oaltf.
GQNFINBMBKr OP A PLASMA COLUMN BY RA-
DIATION PRESSURE AND ITS APPLICATION TO
FUSION POWER QBNERATIGN. by Erich & Weibel.
Rept. on [Contract AF 04(647)127] 26 Ai« 57. 66p.
I2refa. ARL-57-1026; AFBMDDoc na 8-2849.
Order from LC ml$3. 9a pl4ia 80 PB 152 517
Tliia report
to die puMlc 16 Dec Ml
the value of a plaama coaflnemeut
scheme three main requirementa afaould be oonaideretfc
the loaa d plasms by diffusion, the stability d the con-
figuration aad the puwei required for containment, la
the preaeot case d confinement by radiation presaura
it was found that loan d plasms by diffoston ia virtu-
ally abaent Thia property does not depend on tfae par-
ticular gecmetry but can be npwtwt to peraiat in any
arrangement. Two ooiMguraciana have been inveati-
gated for atability. Botfa are imstable. However for
(he TM-mode there la Juat one deformation type
(a • 0 or "aauaage^. which la aot atafale. The puwer
required for containment is quite lai;ge due to the tre-
mmdoiia dlaalpatton of r. f. energy in the cavity walls.
As s conoetpience the mlnimian power level at which
aa ecoaomical reactor may operate is very large.
Torteo U. (kaly).
sokm, TGncs in PonrBKriAL scattering Tie-
ORY AND ITS HIGH ENERGY LIMIT, bf Mario
Verde. Technical (final) rept. on Concract
AF 61(052)230. 31 Mar 60. 26p. 18 reCa. AFOSR-
TN-60-680.
Order from LC mi$2.70, ptaM.80 FB 152 481
air gap to a one tun
copper solenoid 10 cm la diameter »X9
Thia Report oontalaa a dtacuaalon of pntwartal acatter-
Ing theory with die purpose of inveadgadng the func-
tional dependence of some analytic properties of the
scattering amplitude from the oorreaponding onea of
the potential. Section 1 refera to the caae of fixed and
real angi^lar momentum. An integral equation, which
la a kind cf dlapersian relation'a equacioa for tfae
wate function, forma the baaia for deriving asjnnp-
totlc expanaions of phaae-shifts valid for large valuea
cf the energy. The coefDcienta of theae ezpaaaiona
the diatrifatfloa of ifae
21*
tingularliles of the S or R matricea. Section 2 refers
to the case of fixed and real energy. A careful study
tea been made on the nature and distributioo of singu-
larities of the scattering amplitude in the complex
pUoe of angular momentum. The use of the so called
HgKoo-transfarmation leads to an asymptotic esti-
maie of the total scattering amplitude for large values
of cos 6 which is an important result needed for the
derivatloa of the so called Mandelstarn representation
IB potential scattering. (Author)
Weizmann Inst, of Science (Israel).
COLLECTIVE MOTION IN MANY -PARTICLE SYS-
TEMS. PART n. TREATMENT OF COUPLED SYS-
TEMS, by Harry J. LipUn. Technical note no. 4 on
Cootraa AF 61(052)337. 1 July 60. 14p. 8 refs.
AFOSR TN-60-1142.
(]rder from LC mi$2. 40. pb$i. 30 FB 152 493
IIk previous treatment of collective motion using
ladqiandem particle wave functions is extended to
apply to cases where there is coupling between the
collective modea and the other degrees of frtedom of
the ay stem. The method ia shown to be equivalent to
the use of redundant variables and canonical trans-
formations, but is simpler and more easily inter-
preted. The wave functions are considered to be trial
functions which give a good approximate description
of all the degrees of freedom except tbfc collective
modes. A simple model of center of mass motion with
additional coupling is used to illustrate the method.
(Author)
Weizmann Inst, of Science Osrael).
ON THE USE OF FORMAL OPERATOR TECHNIQUES
IN (JUANTUM STATICTICAL MECHANICS, byA. S.
Reiner. Technical note no. 3 on Contract AF 61(052)337
1 Apr 60, 2^. 20 refs . AFOSR- TN- 60- 727.
Older from LCmi$2. 70. phM- 80 PB 152 483
This work contains an alternative derivation of the
linked cluster expansion for a quantum gas . The t ma-
trix formalism is then applied in a palculatioo of clus-
ter coefficients of a boson gas . (Author)
Thermodynamics
AvcoCorp.. Wilmington. Mass.
■DBTBRMINATION OF THE TEMPERATURE DB-
PENDBNCE OF MATERIAL PROPERTIES IN MAGE
FURNACES, by Tibar S. Laszlo and Murray S.
Klamkln. Scientific rept. no. 1 oo Contract
AF 19(604)7204. 18 Oct 60, lOp. 1 ref. Tecbirical
memo. RAD-TM-60-67; AFCRL-TN-60-797.
(Mar from LCml$ 1.80. ptiS 1.80 FB 152 472
A special testing method is described which makes It
possible to determine a property of a specimen for
narrow temperature intervals from measuremencs in
the wide-range temperature dtatrihution of an image
furnace. The determlnatlan Is baaed on the meaaure-
ment of the property at several, different flux levels
cf known temperature distribution. (Author)
California U. , Berkeley.
PHOnrOGRAPHIC OBSERVATICW OF ACCELERATING
FLAMES, by W. Baumann, P. A. Urtiew, and
A. K. Oppenheim. Technical note DR 8 on Contraa
AF 49(638)166. July 60, 51p. 14 refs. AFOSR-TN-
60-932.
Order from LC mi$3. 60, ph»9. 30 FB 152 484
Streak photographs of the transition from slow- burning
to detonation have been obtained by self- light photog-
raphy of the flame using a rotating drum camera . Ex-
periments were performed with stoichiometric hydro-
gen-oxygen mixtures contained in plastic tubes closed
at one end and ignited by pilot flames. The investiga-
tion included the effect of tube diameter and distance
of ignitor from cloaed end oo the development of deto-
nation. The plots of detonation induction distanoea and
times as a function of tube diameter indicate the ex-
istence of asymptotes. Above a certain value of tube
diameter there should tie no further increase of induc-
tion distance and time with increasing tube diameter.
A graph of average detonation induction velocity, that
ia. the ratio of average induction distance to time,
shows that wall effects are noticeable only for tubes
with a diameter smaller than about 1 cm. Maximum
observed flame velocities, attaining the value of
3. 1 km/sec, have been observed immediately follow-
ing the onset of retonation before the combustion front
settles down to the Chapman-Jouguet detonation with a
velocity of 2. 8 km/sec. The plot of world lines on the
log- log scale revealed that the development process
Can be bracketed between two asymptotes, ooe corre-
sponding to an acceleration which decreases, or is
sometimes even negative, and the other with accelera-
tion that increases with tiine. The average value of
observed accelerations was of an order of 10" m/sec^.
Photographs revealed interesting details of flow and
wave patterns behind the flame front, and in particular
tfae generation of a shock reflected from the cloaed end
and its interaction with the accelerating flame.
(Audior)
Cornell Aeronautical Lab. . Inc. , Buffalo. NY.
HEAT TRANSFER FROM DISSOCIATED GASES IN A
SHOCK TUBE, by R. A. Hartunian and P. V. Marrooe.
Rept. on Contract AF 18(603)141. Nor 59, 78p.
38 refs. Rept. no. AD-1118-A-7; AFOSR TN-59-10e7.
Order ft-om LC mi$4.50. ph»l2.30 PB 148 682
Messurements of the heat tranafer from dissociated
oxygen to the side-wall of a shock tube have been made
over a wide range of operating conditions using the
methods of thin-fllm thermometry. Techniques by
which thin-film thermometers can be used to measure
heat transfer from ionized gases and, also, to study
the effects of surface catalytic efficiency oo the heat
transfer from dissociated gaaes are described. The
results of exploratory experiments using the latter
technique are dlacuaaed. The results cf calculationa
are presented which Illustrate the reductions in hest
tranafer to the sugnation point of re-entering vefaidea
that may be achieved through the uae of a noncatalytic
Burface.
Defenae Metals brformadan Center. Battelle
Memorial Inst.. Columbua. Ohio.
BMISSIVnY AND EMITTANCE, WHAT ARE THEY?
by W. D. Wood, H. W. Deem, and C. F. Lucka. [Rept.
on Contract AF 18(600)1375]. 10 Nov 60. 17p. 8 refs.
DMIC memo. 72.
Order from OTS W-SO FB 161 222
217
The process at tmlssion at radiant energy by a body
which depends en Its temperature is a universal proc-
ess. All bodies, by virtue at their temperatures, emit
electromagnetic radiation at all wavelengths in
amounts varying with the wavelengths emitted. Th»
rate of radiatioa from an ideal eminer, or blackbody,
is proportianal Qo tiie fourth power of its absolute tem-
perature. The tmte at radiatioa from non^lackbodies
depends upon th« material, surface condition, and
temperature and is never greater than that from a
blackbody. The blackbody is, therefore, used as a
standard or reference. The two main classificationB
at radiation sources, total radiatioa and spectral
radiatioa, are defined and discussed. Emittance,
emlssivity, and related properties are defined and
their rel^onshtps to the basic laws governing thermal
radiation were ahown. Some general considerations
derived from th« radiation laws are included as an aid
in Che better usa and understanding of the radiation
data found in tba literature.
,1
Cmb Dynamics Lab. , Northwestern U- , Evanston,
m.
THE EQUATION OF STATE OF AN IONIZED GAS.
by Donald P. Duclos.. Rept. on Contract AP 40(600)748
Oct 60, 154p. 7S refs. ABDC-TN-60-192.
Order from LC |ni$7. Sa pti$24. 90 PB 152 443
The equatiao at m*te at an tonized gu has been in-
vestigated for electron densities below about 10^2 per
cm3 and temperatures below about 1, 000, 000°K. The
gas 18 assumed to be monatomic, electrically neutral,
and m tberroodyaamic equilibrium, hut the composltioc
at the gM is artttrary. that is, multiple lonlzatioo at
any degree is allowed. The perfect gas approKlmatiaa
is found to be valid for electron densities at least as
high as I0l6 per cm^ and. in some cases, even higher
It 18 shown that tpprozlmations to the perfect g^s ex-
pressions can ba made which will greatly simplify cal-
culations. It is alao shown that black -body radiation
may be imporum at low denaities. The daaaical cor-
rections to the perfect gas expresaions due to elastro-
static forces and the finite size of particles which are
obtained from theories of Debye and HUckel, Mayer,
and others, are Investigated, and their limits of va-
Udlty are determined. In acme cases, improved ex-
pressions are derived and suitable apprcocimations are
suggested. It is noted that a fundamental weakness of
the results based on these theories is that a basic pa-
rameter, the distance of closest approach of charged
particles, is not known accurately. Several approKi-
mate ezpreaalooa for this distance are given. Quantum
corrections for alectrcn degeneracy and electron in-
teractions are aliso given. Theories which are appli -
cable at higher densities and temperaturea than those
at interest in tliis investigation are also discuasad
briefly. Finally, the equation of state cf a denaa,
silgbcly knlzed |aa ia derived. (Author)
UbcoIb Lab., Maaa. last, of Tech. , Lexington.
A HELIUM^ REFRICXRATOR, by Conrad J. Rauch.
Rept. on Contract AF 19(604)5200. 9 Sep 60. 19p.
5 refa. 81 G-0028.
Order from LCi*l$2. 40, ph$3. 30 FB ISO 800
The use of He^ tt^ cooling to temperaturea below 1<^
requirea a cloaed syston dictated by the coat
($0. 15/cc at STP) and availability of gas. A closed
cycle refrigerator has been designed and performance
dau are prediaed from the T-S diagram which has
been computed below 2°K from recent experimenul
data. A comparison between predicted aiid observed
performance is given. (Author)
Material Lab. , New York Naval Shipyard. Brooklyn.
A METHOD TO DETERMINE THE THERMAL DIP-
FUSIVITY OF METALS AT HIGH TEMPERATURES,
by J. E. Dennis, A. Hirschman and others. Pinal rept
14 June 60. 22p. 5 refs. Lab. Pro]. 5046-3, Part 123;
DASA-1187; AD- 242 669.
Order from GTS %0. 75 PB 171 183
An experlmetxal method has been devised for the de-
termination of the thermal diffusivitles of solid mate-
rials in the form of small diacs over the temperature
range f nxn 400^ to the melting point of the sample.
Measurements in the range 400 to 1000^ for three
metals are reported. Sp^::imens are irradiated with a
chopped beam in a carbon-arc image furnace. Phase
lag between the square wave irradiance impinging upaa
the frott face at the specimen (measured by a photo-
voltaic cell) and the resultant sinusoidal temperature
of the rear face (measured by a thermoelectric probe)
provides a rapid determination of thermal diffusivity.
Phase opposition of a square wave and sine wave pro-
duces a null LisMjous figure on an oadlloacope. The
diffusivitv of Iron was measured to range from 0. 1461
0. 012 cmV»ec at 400PK to 0. 03 1 0. 01 cm^/sec at
lOOOOK; of cqpper from 1.0102 an^/aec at SOOPK to
0. 8 1 0. 1 cmVsec at 900^. The diffusivity of brass
was 0. 29 1 0. 04 cm^/sec throughout the range from
400to900PK. (Author)
National Research Laba. . Ottawa (Canada).
EXPERIMENTAL EXAMINATION OF LOCAL PROC-
ESSES IN PACKED BEDS OP HOMOGENEOUS
SPHERES. PART I. THE LOCAL PACKING IN RAN-
DOMLY STACKED SPHERE BEDS. PART II. THE
LOCAL HEAT TRANSFER OVER THE SURFACE
AREA (^ A SPHERE IMMERSED IN A PACKED
BED OP INFINTTB DIMENSIONS AND ARRANGED IN
RHOMBOHBDRAL ARRAY, by J. Wadsworth. Feb 60,
83p. 13 refs. Mechanical engineering rept. MT-41;
NRG no. 5895.
Order from LCml$4. 8a ph$l3. 80 PB 152 784
Part L The local packing, occurring in cylindrical
containers when randomly stacked with homogeneous
spheres. Is examined over a range of 4 to 24 of the
ratio of coocainer diameter to sphere diameter. Sphere
packlnga are examined both as a function of radial and
vertical posltkn in the bed. It ia concluded that only
one kind of dose packing exists or tends to exist in
random packing, i. e. rhombohedral. Some under-
standing of the packing mechaniam has evolved for the
tsrgest cylindrical ooncainer, i. e. container to ^>here
diameter ratio of 24. Part It A three -dimenaional pic-
ture ia presented of the heat tranafer over the surfaos
area of a sphere when immersed in a packed bed of
" infinite" dimimainna arranged In rhombohedral Na 6
bkxrked paaaage array for a range of Reynolds num-
bera of 8, 000 to 60, OOa where Re number is based as
sphere diameter, average velocity of the coolant
across die cross-section of the bed in the ahseixx of
the spheres, and fluid properties evaluated at the me«
film cooditlaaa. (Author)
2lt
Naval Radiological Defense LAb. , San Francisco,
Calif.
MEASUREMENTS OF THE THERMAL PROPERTIES
OF METALS AT ELEVATED TEMPERATURES, by
R. L. Rudkin, W. J. Parker and R. W. Westover.
11 May 60, 3iOp. 12 refs. Research and development
technical rept. USNRDL-TR-419.
Order from OTS %0. 75 ■ PB 171 185
The thermal properties of tungsten have been mtosured
from 1500°K to 2900^^. using a resistance heated 10 mi
wire suspended in a vaduum of 10"5 mm Hg. The total
hemispherical emittancb was measured to vary from
0.27 at 1500°K to 0. 36 at 2900Ok while the range of
heat capacity was from 0. 030 cal/gm°K to 0. 048
cal/gm°K in the same temperature interval. The
product of the thermal tonductlvlty and the electrical
resistivity divided by tl^e absolute temperature was
■early constant and was about 10% lower than the
theoretical value of the Lorentz number.
I
Wave Propagation
Antenna Lab. , Ohio St»te U. Research Foundation,
Columbus.
APPROXIMATE SOLUTIONS TO SCATTERING
PROBLEMS BY MULTTPOLE MATCHING, by Edward
WL Kennaugh and Raphael Tsu. Rept. on Bi-statlc
Reflection Characterist^s, Contract AF 19(604)3S0L
24 July 59, 28p, 6 refs. Rept. 827-4; APCRC TN-
59-557. \
Order from LC ml$2. 70^ ph$4. 80 PB 152 258
The mulclpole approxim^^tion appears useful for the
approximate solutions t9 scattering problems in the
resonance region. The method is sufficiently general
JO handle conducting bo(J^es of arbitrary (smooth)
•h^>e, and could be programmed for machine com-
putation. An Inherent advantage of this method is that
estimates of the error io a given approximation can
be obtained by ccxnparing matching and exact fields
on the scanerer surface. It may be desirable to ob-
tain least-squares aooroximations to the exact tan-
fatlal fields, rather than exata matching at discrete
potots, and this would require only a minor nKxllfl-
catlon of the procedure.
Antenna Lab. , Ohio State U. Research Foundation,
OohanbuB.
EXTENSION OT THE PHYSICAL OPTICS APPRGXI-
MATK»I TO SMALL BODIES, by Jon Eberle. Rept.
caContraa AF 19(604)3501. 1 Nov 59, 2lp. 4 refs.
Kept. 827-6; AFCRC-TNi«0-102; AD-23I 996.
Order from LC m42. 7a ph)3.80 FB 153 255
This report released for 'sale to the public 14 Dec 60.
A number of extensions or corrections to phjrsical
optics methods were formulated, with the major con-
cern being to extend the physical optics approxima-
tldBs to smaller bodies in terms of wavelengdia. The
first of these was the work by Fock (AFCRC-TN-
S7-102, June 1957), and later that of Keller (Resesrch
Report No. BM-115, New York Univ. , July 1958). The
conclusions that may be drawn from the correctiona
to the physical optics current distribution are that the
distributions are basically wrong in the resonance re-
gion, and that smaU corrections are not sufficient to
obtain good results. The methods of Fock show that
the fields on the lifted as well as on the shsdowed
side must be adjusted. The discontinuous jump at the
shadow boundary in the physical optics current dis-
tribution results in a periodic variation of the back-
scattering curve with frequency which is of the wroi^
period in the resonance region. This effect must first
be eliminated in the corrected current distribution be-
fore good agreement can be obtained in the resonance
region. (Author)
Antenna Lab. , Ohio Sute U. Research Foundatioa,
Columbus.
THE THEORY AND APPLICATIC»i OF THE SCAT-
TERING MATRIX FOR ELECTROMAGNETIC
WAVES, by Raphael Tsu. Rept. on Monostatic and
Bistatic Measurement of Scattering Shapes and Synthe-
sis of Scattering Shapes, Contract AP 19(604)6157.
I Aug 60, 88p. 20 refs. Rept. 1073-2; AFCRL TN-
«-950.
Order from LC mi$4.80, ph$13.80 PB 152 242
The .theory and application of the scanerlng matrix for
electromagnetic waves are discussed. The scattering
matrix relates the vectors in a multi -dimensional
space (function space) which represent the outgoing
part of the total field (incident plus scattered) and the
incoming part of the total field. This matrix is defined
in terms of arbitrary source- receiver arrangements;
therefore it in turn defines the scattering properties
of a body independent of the angles of incidence and
scattering. Therefore the scattering matrix com-
pletely specifies the properties of a given scatterer.
The theory of the scanering matrix is presented in
Chapter I. A general scattering relationship is de-
rived and its familiar form for plane wave incidence
(the cross-section theorem) is obuined. The deter^^
mination of the scanering matrix from measurement^
is discussed in Chapter III. A method for obtaining
the scattering matrix from measurements is demon-
strated with examples. A specific application of the
scattering matrix to the study of optimum scatterer s
is considered. Examples erf the optimization of the
scattering panerns for spherically symmetric bodies
are presented. The scattering matrix corresponding
to the given optimum conditions is obtained. These
results can be used in the study of scanering pattern
synthesis where a spherically symmetric scatterer is
employed. (Author)
Brown U. Dlv. of Bngiiieering, Providence, R. I.
ON THE THEORY OF MPFR ACTION BY A COM-
POSITE CYLINDER, by Ralph D. Kodis. Scientific
rept. no. 7 on ContraCXt AF 19(604)4561 and Nonr-
562(24). Dec 59, 31,p. 8 refs. Scientific rept.
AF 4561/7; AFCRC TN-60-I07; AD- 233 188.
Order from LC ml$3. 00, ph$6. 30 PB 148 296
Formulas are developed for the diffracted field around
a perfectly conducting cylinder with a dielectric sleeve
of arbitrary thickness. Hiese formulas represent the
field due to a unit electric line source parallel to the
cylinder (either inside or oisside the dielectric sleeve)
as a spectrum of radial eigenf unctions. It is shown
that in each case the field in the regton containing the
219
source can be expressed as tbe •um at 2 terms, the
first d which \b a spectral representation of the fleJd
when tbe outer as well as the Inner s urface at the
dielectric is a perfectly cooductlng boundary. The
second term at the sum, which alone involres tbe
properties ol tke dielectric, is an integral that con-
verges rapidly at high frequencies. (Author)
Cohonbta U. School at Engineering. New York.
A DIELECTRIC SURFACE WAVE STRUCTURE: THE
V-LINB, by P. Dlament, S. P. Schlesinger, and
A. Viganta. Technical repi. no. 6 on Contract
AF 19(604)3879. 1 July 60, 40p. 8 refs. CU- 11-60-
AF-3879-EE; QRD-TN-60-781.
Order from LC mi$3. 00, pbS6. 30 FB 152 474
TWs work considers the properties oT the V-Une a
surface-wave structure comprising a cylindrical dielec-
tric binding medium a€ sectoral cross section sup-
ported by a wec^ at two conducting plates, and at the
higher order hybrid HEnni modes that may propagate oo
such a wavegiiide. Analytic and graphical relations are
presented to determine various parameters describing
the propsgation oo this structure, and new cutoff condi-
tions, associatad with a set of modes complementing
those known pravioualy, are derived. The signlficaiice
at the solidons of the equations is discussed and ex-
perimental venfioatlan of the theory is descrlhed.
Promising modiflctioos of tbe V-Une are suoBested.
(Author)
Diamond Ordnfcnce Pure Labs. , Washii^or, D. C.
MULTIMODE PROPAGATION IN GYROMAGNBTIC
RODS AND ITS APPLICATION TO TRAVELING-
WAVE DBVICE$, by J. E. Tompkins, P. Reggla, and
L. Jowph. 21 July 60, 16p. 13 refs. Technical rept.
TR-8^1
Order from LC tnl$2. 4a ph$3. 30 PB 152 653
Results are suntnarized of exact calculations of the
microwave propagation constants in longitudinally mag-
netized gyromajietic cylindrical rods. Theoretical
data are presenoed for the domlnaiK and higher order
hybrid modes excited from a TEi i circular waveguide
mode that is circularly polarized in the anti-Larmor
sense. CompariBon of tbe solution for the dominant
^ mode with data (br the DOFL rectangular waveguide
reciprocal phase shifter suggests probable anti-
Larmor circular polarization within the ferrite in this
device. Experiments are described that support this
conclusion, and a new broadband microwave absorption
modulator or switch is described. Calculations for
values of magnetic field near resonance reveal the
characteristic shift in the resonance field as a function
of rod radius r^, which Is in gtxxl agreement with the
results predicted by tbe perturbation theory of
Morrison for r^ < — s — . (Author)
Btoctrical Engineering Rssearcfa Lab. , U. at
Iteas, Austin.
THE EFFECT OF RADIOSONDE TIME LAG ON IN-
DEX OF REFRMmON LAYER HEIGHT, THICKNESS
AND GRADIENT, by N. K. Wagner. Repc on Con-
tract AF 19(604)2249. 10 Apr 60, 16p. 2 refs. Rept.
na 6-33; AFCRC-TN-60-188; AD- 235 631.
Order from LC Hii$2. 40, ph$3. 30 PB 149 060
The height and thickness of anomalous layers in the
atmosphere reported by the radiosonde differ from the
true height and thickness as a result of sensing ele-
ment time lag. Correction factors are derived for var-
ioua combinations of time lag and layer thickness by
employing a standard form of the time lag equation and
minlmax curve fitting techniques. Emphasis is placed
on radiosonde distortion of index of refraction layers;
however, the technique employed is not restricted to
this application. (Autiior)
Electronics Research Lab. , U. of CaUfornia.
Berkeley.
ON THE "SADDLE POINT" PROPERTY OF SEVERAL
VARIATIONAL EXPRESSIONS, by N. Kusnezov. Rept.
on Contraa N7onr-29529. 31 July 59, 28p. 10 refs.
Rept. no. 91; Series no. 60, issue no. 245,
AD- 228 120.
Order from LC mi$2.70. ph$4.80 PB 149 735
Varlatlaoal expressions obtained by X. Schwinger for
tbe electromagnetic, quantum mechanical or acoustic
scattering problema, based on tbe scalar free space
Green's function were considered previously by C. L.
Dolph Oour. Soc. for Ind. and Appl. Math. 5:89-104,
1957). Dolph arrived at the conclusion that Schwlnget%
expressiana for the amplitude of the scattered wave ex-
hlbit a stfddlb point behavior in a small neighborhood d
the exact distribution. Reaction (Phys. Rev. 94:1483-
91, 1954) variational expressions are parallel to those
of Schwinger for the same configuration. Reaction ex-
pressions involve vector products and the dyadic
Green' a function alnce they are obtained from Maxwell's
equations directly without use of the solution of a
scalar Wave equation as an intermediate step. T}ie
concluaioos reached by C. L. Dolph are reexamined in
tbe caae of the scalar scattering and the extremum
properties are investigated of the various variational
expressions formulated on tbe basis of the reaction
principle. (Author)
Geophysics 0>rp. of America, Boston, Mass.
A STUDV OF AN ADVANCED ELECTROMAGNETIC
COMMUNICATIONS SYSTH^, by Jerome Pressman.
Leonard M. Aschenbrand and others. Pinal technical
rept. 1 July-31 Dec 59. on Contract DA 36-039-SC-78971
[1959] 254p. AD-232 865.
Order from LCmi$l 1.10, ph$39. 60 PB 152 232
This report discusses the utilization of artificial
electron clouds (artificial ionospheres) as a possible
tool for communication purposes. Three major areas
are considerefl, namely the physics, chemistry and
applications of electron cloud. The first is concerned
with the general considerations associated with tbe
ganeration. dynamics and other physical character-
istics of the artificial electron cloud. For this there is
presented a general survey of the data and analysis
from several experiments designed and performed ex-
pressly for obulning critical engineering parameters
required for the systematic development of these clouds'
as a propagation medium. Alkali metals -aluminum
generation of artif ical elearon clouds is analyzed with
tiie aid of a simple deflagration model for reaction
which allows calculation of the observed chemical yield
of neutral alkali atoms. From the initial equilibrium
ionization thus calculated, the electron yield of the ex-
panded cloud is obtained from an elementary model of
220
tisctron-ion recombination during tlie initial expansion.
Tbe third area suggests one typical communications
icbeme. For the case discussed, the RP communi-
osttODS capability of the artif IcUlly generated iono-
ifttrt will be presented. (Author)
(XKtlngen U. (West Germany).
ABSORFTION AND TRANSMISSION OF ELECTTRO-
IIAGNETIC WAVES. PHASE F. EFFECTIVENESS
OF CM-WAVE ABSORBERS AS A FUNCTION OF
fOLARIZATIWi UNDER OBUQUE INaC«NCE, by
K. Walther. Technical final rept. on Contract
AF 61(514)1041. 3rjuly58. 60p. 14 refs. RADC TR-
S9-26B; AO- 210 938.
Order from LC mi$3.60, ph$9. 30 FB 148 287
See also PB 132 771
GOttingen U (West Germany).
ABSORPTION AND TRANSMISSCW €»» ELECTRO-
MAGNETICi WAVES. PHASE H: WIDE-BAHD AB-
SORPTION OF ELECTROMAGNETIC CM-WAVES BY
A THIN DISSIPATIVE LAYER ON A METAL PLATE
by Reinhard Pottel. Technical final rept. on Contract
AF 61(514)1041. 31 July 58, 26p. 9 refa. RADC TR-
S^-lbD; AD-210 940.
(Wer from LC ml$2. 70, pfa$4. 80 FB 148 288
I
SseaJsoPB 146 709
Institute of Geophysics and Planeury Ftiyslcs, U. of
California, Los Angeles.
AN EXPERIMENTAL INVESTIGATIC»< OF THE
P«0PA(3ATION OF ATMOSPHERICS WITH BMPHA-
SB OP BXTREMBLY-LOW-PREQUENaES, by
B. J. Smith and L. R. Tepley. Final rept. on Contract
AF 19(604)3466. June 60. 192p. 21 refs. APCRC-TR-
60-269.
Order from LC ml$8. 70. ph$30. 30 PB 152 174
Nit I. The propagation of low -audio frequency elec-
tromagnetic waves
P»n II. A comparison of sferlcs as observed in the
»ery low frequency and extremely low frequency
iMtltue of Mathematical, Sciences. New York U. ,
DECAY EXPONENTS AND DIFFRACTION COBFPI-
OBJfrS FOR SURFACE WAVES ON SURFACES OF
MON-CONSTANT CURVATURE, by Joseph B. Keller
•nd Bertram R. Levy. Rept. on Contraa
AF 19(604)5238. Oa 59, 40p. 13 refa. Research rept
io. Ek-147; AFCRC TN-59-953; AD- 233 254.
(Her from LC ml$3.00, pfa$6. 30 PB 148 295
IW diffraction of a plane scalar wave by a hard elliptic
qraadcr is invewlgated theoretically. The field la ob-
**f^ •nd expanded asymptotically for inddeot wave-
■•pha amall compared with the dimensions at the gen-
•nttng ellipse. The method of obtaining the asymptotic
wptoaion of the dlffraaed field parallels previous
■«J>oda. However, additional terma in the asyanCotlc
2JM10O ire olJtalaed. It waa ahown that tbe «#ymp-
■toc expansion of the dlffraaed field waa in agreement
with the geometrleal theory of diftractlon previously
presented [Proc. of Symposia in Applied Math. ,
8:27-52, McGraw-Hill, 1952] and [I. R. E. Trans, on
Ant. and Prop. , Smyp. on Elearomagnetic Wave
Theory, AP-4:312-32l, July, 1956] The additional
terms in the field obtslned are interpreted geometri-
j cally as higher order corrections to the decay expo^
nents and diffraction coefficients. "Finally, additional
terms are obtained to those given [Bell System Tech J.
33:417-502, March, 1954] for the asymptotic expansioa
of tbe field diffracted by a paraboUc cylinder. (Author)
National Bureau of Standards, Boulder, Colo
QUARTERLY RADIO NOISE DATA, MARCH, APRIL.
MAY 1960, by W. Q. Crichlow. R. T. Disney, and
M. A. Jenkins. 19 Oct 60, 69p. 11 rafs. l^cfanlcsl
notes na 18-6.
Order from OTS $1. 75 PB 151 377-6
See also PB 151 377-5
New York U. Coii. of Ei«ineerii«, N. Y.
ELASTIC AND PLASTIC WAVE PROPAGATICW IN
LONG CYLINDRICAL BARS, by Ralph Papimo and
George Gerard Final rept. on Impaa Tube PioJ. Con-
tract DA 30-[0)69-ORD- 11 38. Aug 58, 84p. 24r«fa
Technical rept. SM58-10, WAL 112/83-17.
Order from LC vaiU- 60, ph$13. 80 PB 152 398
This report released for sale to the putdic 1 Dec 6a
This paper is concerned with theoretical and experi-
mental investigations of the propagation of longitudinal
eUstic and pUstlc wavea of deformation In lotw round
cylindrical bars. The elastic phenomena are treated
separately from the plastic phenomena. In the elastic
case verification elements are derived frosn a lecemly
published theory of elastic wave propagation in which
the effects of radial inertia are included. Experlmenu
are descrlhed in which the predictions at theory with
respect to wave velocity and dlspersite are verified.
Stanford Research Inst. , Menlo Park, CaUf.
A CTUDY OF PROPAGATION DATA OOLLECTBD
FROM ARTIFIOAL SATELLITES, by R. H. Light.
Pinal rei«. oo Contraa AF 19(604)4968. Mar 60. 45p.
11 refs. SRI Projea 2718; AFCRC-TR -60-121:
AD- 235 665.
C^derfromLCinU3.30, pb>7.80 FB 149 064
An iBveMlfBtion was conducted on Ionospheric propa-
gation effecu by using the radio transmissions from
artificial earth satellltea. A total of 74 observations
were made of 1958 Beu. 1959 Delu, 1959 Epeilon,
1959 Zeu, 1959 Eta, 1959 lou, and tbe Ruasian Lunik
P; Signal amplitudes and Doppler dau were taken of
several peases. Various antennas and polarizatlona
were used to receive the satellite transmissions, and
comparisons were made of these signals. The equip-
ment, observations, and results of the rsdio sstelUts
monitoring are described. (Author)
221
RESEARCH 'methods, TECHNIQUES
AND EQUIPMENT
I Office,
Army Research Office, Washington, D. C.
ARMY RESEARCH TASK SUMMARY, FISCAL YEAR
1960. VOLUME 6» MATERIALS TECHNOLOGIES,
MATHEMATICS, AND OPERATK»4S RESEARCH.
445p. I
Order from GTS $f . 50 PB 171 006
I
Contents: i
Materials TechnolfttJes:
Ceramic technology
Chemical technology
Food technology
Metallurgical technology
Non- metallic materials technology
Photographic technology
Mathematics:
Algebra and number theory
Analysis |
Compuution methods and techniques
Geometry and topQkxrv
Mechanics .
Numerical and graphical methods
Operations analysis
Probability and statistics
Operations Research
(See also PB 161 38) i
Institute of Statiitics, North Carolina U. , CJiapelHlU.
CONTRIBUTIONS TO THE STATISTICAL ANALYSIS
OF EXPERIMENtS WITH ONE OR MORE RE-
SPONSES (NOT NECESSARILY NORMAL), by Vasant
P Bhapkar. Rept4 oo Contracts Noor- 855(06) and
AP 49(638)213. Jttly 59. 135p. 39 refs. Mimeograph
•eries no. 229; ApOSR-TN-59-795: AD-219 882.
Order from LC mi$6. 90, ph«l. 30 PB 148 695
Experimental dat4 are considered which are given In
the form at frequencies In cells determined by a
finitely multi-way cross-classtficatlon, with predefined
categories, finite In number, along each wayo<cla«tl-
flcstlon. Hypotheses are imposed which are considered
to be generalizations appropriated in (1) classical
normal univariat« fixed effeas analysis d variance
(ANOVA), (2) nomisl multivariate fixed effects analy-
sis of variance (M ANOVA). and (3) analysis of various
kinds at normal independence. Sample te«Ti aregivCT
for these hypotheses. Two theorems on minimum A |
are proved, and the univariate 2-factor problems are
studied. The 2-vwy classification test Is extended to
cover Incomplete block situations. An extension d
the U- statistics theorem is stated and proved, and a
new test -criterion for the problem d c samples Is
given. Some regression problems and someWvarlate
problems In d»e nonpsrametrlc set up are studied.
Most of the test -criteria developed are atympttXlc In
nature.
Naval Research Lab. , Washington, D. C.
DESGN AND 1N$TRUMENTATI0N OF A POUND-
WATKINS NUCLEAR MAGNETIC- RESONANCE SPBC-
TROMBTER, byP. B. Geiger, Jr. FlnslrejK.
27 Oct 60, 41p. ai refs. NRL rept. 5923.
Order from LCitd$3. 30. p*47.» PB 148 663
The various problems of instrumentation of a Pound-
Watkins nuclear magnetic - resonance spectrometer have
been investigated. Experimental data have been col-
lected for the sensitivity of the oscilUtor to a signal
from a Watkins calibrator as a function of nxxlulatlon
frequencies from 30 cps to 5 kc and rf unk voltages
from 0.05 to 0.7 v^nis • The results confirm Wakins'
oscillator theory. An expression has been derived for
the amount at frequency nxxiulation o* the rf oscillator
by the Watkins calibrator. For representative values
of rf circuit components , this frequency modulation Is
roughly 0.5 cpe at 10 Mc . The rf sample probes con-
structed for this project are alnnost free of modulation
(rtckup in nwduhtlon fields as high as 23.5 oersteds
280 cps) and a steady field of 7000 oersteds . Trouble-
some sources of nxxiulation pickup other than rf probes
have been Investigated, and methods have been de-
veloped for reducing or eliminating them. A complete
set of circuit diagrams and a component block diagram
is given.
Office of Technical Services, Dept. of Commerce,
Washington. D. C.
MACHINE TRANSLATICW, Oct 60. 5p. 46 refs. OTS
Selective Bibliography SB-439.
Order from OTS $0. 10 OTS SB-439
A Wbbography of reports listed in the two OTS monthly
abstract Journals: U. S. Government Research Reports
and Technical Translations.
Information Theory
Institute of Statistics. U. of North Carolina,
Chapel HiU.
ON A CLASS OF ERROR CORRECTING BINARY
GROUP CODEa by R. C. Bose and D. K. Ray-Oiaud-
hurl. Rept. on Contract AF 49(638)213. Sep 59. 15p.
5 refs. K^Cimeograph series no. 240; AFOSR TN-
59-1240; AD- 235 094.
Order from LC ml$2. 40, ph$3.30 PB 148 686
A general method of constructing error correalng
binary group codes is obtained- A binary group code
with k tnformatlan places and n places is called an
(n, k) code. Explicit method of constructing t -error
correcting (n, k) codes are given f or n • 2^- 1 and
k - 2™-l-nu for general t. An example is worked out
to illustrate the method of construction. (Author)
Willow Hun Labs. , U. of Michigan. Ann Arbor.
CC»(IPUTATION. BEHAVIOR. AND STRUCTURE IN
FIXED AND GROWING ATUOMATA, by Arthur W.
Burks. Rept. on Project Michigan, Contract DA 36- >
039-SC-78801. Mar 60, 34p. 26 refs. Rept. no. 2900- |
128-R; AD-234 469.
Outer from LC m43. Oa P»46. 30 PB 149 673
Cootents: ,
Structure. beiMTior, and compuution in fixed automiO
and generalized turlng machines
AiMdyals and synthesis of automata
Growiog automata
Some problems cooceming growing automata
222
Phohsgraphlc Equipment
Army Signal Research and Development Lab. . Fort
Monmouth. N. J.
EVALUATION OF LE-15, 16-INCH FOCAL LENGTH
f/5.6 TBLEPHOTO LENS FOR CAMERA SET lCS-6,
by L. D. Goldfarb. 2 May 60, 20p. USASRDL Test
rept. 1481.
Order from LC mi|2.40, ph$3. 30 PB 152 567
The optical and mechanical characteristics of the lens
and auxiliary vlewflnder atta(j|iment are presented
together with the test results of photographic resolu-
tion using Plus X film. (Author)
Army Signal Research and Development Lab.
Port Monmouth, N. J.
EVALUATION OF VIEWER, 3 1/4" X 4" AND 70MM
STRIP, by L. a Goldfarb and George Gordon.
2 May 60, 8p. USASRDL Test rept. 1480.
Order from LC mill. 80, ph$l. 80 PB 152 566
The viewer, a ponable optical device operating from
115 VAC. is designed to produce an enlarged illuml-
oated image on a viewing screen. Either 3 1/4" x 4"
slides or 70mm strip transparencies can be used with
the viewer. Tests performed on the viewer are dis- -
cussed. In general the viewer was found to be in ac-
cordance with die technical requirements. (Author)
Palrcfalld Camera and Instrument Corp. , Syoeset,
N. Y.
VIEWER, STILL HCTURE. Final development rept
Aug 57-May 58 on Contract AF 30(602)1727. 29 July 58
18p. SME-AG-3; RADC TR-58-160; AD- 206 314.
(^der from LC ml$2.40, phJ3.30 PB 148 285
This report describes the investigations, design, engi-
neering, and fabrication accomplished to produce a
prototype rear projection viewer having high resolution
ud magnification capabilities. The viewer is a porta-
ble, ruggedly constructed unit, designed for field use
to enable an operator to identify and read data con-
tained on Minlcards. The following pages describe the
approach to the problem, the steps taken in arriving at
solutions to the more important requirements erf the
viewer, and suggestions as to improvements which
mlgte be made in the final model prior to the production
Of this type of viewer. (Author)
Lincoln Ub. , Mass. Insi. of Tech., Lexington
PRECISION SPEED CONTROL OF A HIGH SPEED
CAMERA, by D. A. Cahlander. Rept. on Contraa
AF 19(604)7400. 20 Sep 60. 15p. 47G-00O5.
Order from LC mi$2. 40. ph$3. 30 PB 150 974
I« many applications where a high-speed movie cam-
era is used, it is desirable tq control the piaure-
tiking rate accurately. The method of control de-
•oUwl incorporates a reluctance pickup, which is
••M to generate an electrical signal when a tooth on
tte camera's film-drive sprocket passes near it. The
ctoirance between the pickup and a sprocket tooth is
•005 inches. By timing the interval between the pul
from this pickup, the speed of the camera between the
two preceding frames is determined. This speed is
electrically compared with the desired camera speed,
and the voltage appUed to the cameras motors is ad-
justed correspondingly. This method, althou^ seem-
ingly complicated, is actually quite simple and ex-
tremely versatile.
Oslo U. (Norway).
A HIGH-SPEED ROTATING DISK SHUTTER FOR
PHOTOGRAPHING THE SOLAR DISK, by KjeU Brekke.
Scientific rept. na 1 (23) on Contract AF 61(052)186.
1959, 2^. 7 refs. AFCRC TN-59-470; AD- 232 268.
Order from LC ml$2. 70, phK 80 PB 148 299
A high -speed rotating silt- shutter was built for photo-
graphing the solar disk in direct focus of a long- focus
instrument at the Solar Observatory, Harestua. The ^
phenomenon of variable vignetting, inherent in rotatiiw
shutters, are removed by suitable tilt of the edges of
the slit. The theory behind the technical desi^ is pre-
sented. Technical details erf die shutter equtoment are
included. (Author)
SOCIAL SCIENCES
Bens on -Lehner Corp., Santa Ktonlca, Calif
A CLASSFICATION SYSTEM FOR ANY DATA
BANKING (INFORMATION STORAGE AND
RETRIEVAL) PROCESS, by Peter Garrett. Rept. on
Contract Nonr-2666(00), 15 June 59, Up. Research
rept. 59'-6; AD-219 090.
Order from LC ml$2.40, ph$3.30 PB 148 977
Study was started to discover and state explicitly the
fundamentals of data banking (more commonly called
information storage and retrieval). A clear oqxwitlon
of these fundamentals will be useful in directing the
development of equipment to meet particular applica-
tion requirements. A logical framework or hierarchical
tree is displayed that includes all possible data bank-
ing processes and shows their similarities and dif-
ferences. The ba«is of this framework is the oipmlza-
tion of the store and the method of search, not the
physical form of either the items of information or the
search equipment . (Author)
223
Brown U. , Providence, R. L
AGGREGATION OF UTILITY FUNCTIONS, byEdmaad
Eisenberg. Technical rept. no. I on Contract
Nonr-562(15). 1959, 46p. 6 refs.
Order from LC miisj. 30. ph$7. 80 PB 152 016
This rqwrt is concerned primarily with the existence
of an sggregate utUity function in an economy and Its
relation to eccmomic equilibrium. In the discussion
and results obtained a social welfare function plays a
fundamental role. ^)ecifically, the economy consists
of m consumers competing for a siqjply <rf n goods
available in die economy. Each individual has a fixed
income, or personal budget, and acts so as to maxi-
mize his personal utility functi(Mj within his budget.
The question of economic equilibrium is: to find prices
of the available goods such that, under diese prices,
the total demand does not exceed the supply (the so-
called "market- budget" condition) and the coat of the
■(fiply does not exceed the sum total of the personal
budgets.
Institute for Quintltatlve Research In Economics and
Management, Psrdue U. , Lafayene, Ind.
A MARKET ADJUSTMENT MECHANISM, by Stanley
Relter. Rept. on Coittract Nonr- 1100(16). Dec 59. 28p.
5 refs. Institute Nper no. 1: AD-231 101.
Order from LC i»i$2. 7a phM. 80 PB 152.125
A martet sd)usti»ent process, an equilibrating mech-
uAmu, capable at supporting the static theory of mar -
kets. is presented. The approach to tt>e problem a< in-
fonnatlon transfer and communication is to begin with
a market in whidi formal arrangementa for Informa'
tion transfer are minimal. The assumption is made
fti«f people acquire information only through their own
individual market contacts and remain completely
ignorant of the experience of others. The case of an
equUibratii^ process in unorganized markets is dis-
cussed in which it)e mechanism at communicabon ia
explicit, individuals have limited capacity to communi-
cate and behavior is consiatent with both the hypoche-
sis d maximizatton and 'he awareness on the part of
indlvlduala at tMlr own limited resources for commu-
nication, as well as for trade. The concept of a mar-
ket sequence can provide a new way of organizing ob-
•ervatkias of malrket transactions uken over time, and
provide an approtch to dynamic analysis of trans -
actlona data froif unorganized markets.
li« Us prior accompUshnients In s given number of
areaa cf study. New achievement carda are produced
which contain not only his total credits and grade polKi
in the area bix also his actiieved and predicted grade
potA averages. The program also accionulates, by
sex, the total credits and toul grade points from each
class card processed, so that at the end of the process-
ing the achieved grade point average for men and
women whose claaa cards were summarized during the
proceasing may be punched out. The general flow of
tke program Is described, and the card controla and
card forms are listed. Also, instructions are pre-
sented for the sequential operator, and the input-output
wiring for the program is Usted.
Northwestern Technological Inst. , Evanston, 111.
ON THE INVAAIANCE OF DEMAND FOR CASH
AND CTFHER ASEETS, by R. W. Glower and
M L. Burstein. ONR Research memo. no. 22 on
Temporsl Planning and Management Decision under
Risk and Uncertainty, Contraa Nonr -1228(10). Feb 60,
lip. 9 refs. AI>237 867.
Order from LC iW$2.40, pb$3.30 PB 148 196
Washington U. ,| Seattle. Div. of Counseling and
Testing Services.
AN IBM TYPE 660 PROGRAM TO SUMMARIZE
MULTIPLE CRITERIA DATA ON ACADEMIC
ACHIEVEMENTS, by Calvin E. Wright, Glenn E.
Roudabush, and George R. Burket. Rept. on Cootraa
iioaT-4T7((») and Public Health Research Grant
M-743(G4). June 59, 49p. 4 refs. AD- 227 912.
Order from LCini$3. 30, ph$7. 80 PB 14« 723
The Unlreraity df Washington Registrar's office adopted
an IBM type-650 registration system making it possible
to sianmarlze credit s and grade pdata for individual
students into 50 or more course areaa. For each stu-
dent concerned, cards containing Information about the
courses he recently completed and the grade that he
received are merged with achievement cards represent -
I
MISCELLANECXJS
. ^ It
Nsvsl Research Lab. , Washington, D. C.
REPORT OF NRL PROGRESS. Jan 61.
Order from CTTS »1 . 25, $10. 00/year PB 171 314
Articles:
Botanical Approach to a Dual- Purpose, Alr-Purlflc|ttios
System for Submarines, by F. J. Hannan
Plaah Etch Study of <100> Dielectric Breakdown
Dendritea on LiF Cleavage Surfaces, by J. Pasternak
and J. W. Dsvlsscn
Effect of Take-Off Angle on Electron Probe CaUbrattfls,
by L. S. Blrks and R. E. Seebold
Sdeotlflc program:
Chemistry: An Isocysnste primer- sealer for masonry.
NRL Model EH-5753 Freon leak detector
Mathematics: Relation between strict convexity of a
function and positive defimteoess of its Hessian
matrix
Mechanics: Bffea of nnechanlcal scrsln upon the elec-
trical reslsunce of Au-Cu alloy in the ordered and
disordered state at 78<>K and XfPK.
Metallurgy and Ceramics: Deooddstlan of noolybdenim.
Fractograpby of Ugh- strength steels with the electroi
microscope. Rates of corrosion of structural alloys
in molten sodium sulfate. Effect of irrsdlstlan tem-
persture on the trsnsitlon temperature character-
istics of pressure vessel steels. Effectiveness cf
best treatment for the recovery of propertiea cf
Irradiated steels. Removal of iocerstltisl impurltle*
from UoUum by xlnc-nioUum compounds. DuraUHqr
of the xlnc-base costing for niobium
Nuclear snd Atomic Physics: Ray-tracing technique for
ion-optical meaaurements. Readout control unit for
automatic type punch systems. Reladvlstlc Brllkwla
flow
Radio: Performance of transosonde rsdlo equlpmeK
during experimenul flights since May 1960. Power
control drculta for protecting soUd- state electroslc
systems agslnat catastrophic failure. Improved
"twist -turn" wsveguide Junction
224
ATOMIC ENERGY COMMISSION REPORTS
OcX^i^ S^SSitoi^^^^^^"^ instructions on the Inside front cover of the U. S.
obtained from the iJ. S. Sfp^^ d^ SmSrrF^^ir^ x **'",I^' , ^ "'i "* **** libraries may be
Reproduction In whole^^nS anv^^^Iur J?i^ *^7***°*'''^ Services, Washington 2i 6. C.
Ci«2i.slon. subJectTtte a^^c^al erf IXJs S^rl^n^^^^^ AtUc Snerpr
MM about AEC-developed iXmSion XSd b^rJr^t^rr?r^ ^ ^T^ inquiries from the Infistrlal
bargy Commission, wSSngton 25 D C *"'^**=^«' ^° ^ hidu«rlal Informatioo Branch, Atomic
General
lewyry of hvdrogen fluprlde from a rnnl«nr-l 14-
eng-26. S4p
pM9. 30
Order from LC.
Tenn.
-7405-
Mi$3.60,
ORNL-1359
Uoodye
mouth^Jhla Jul v 60. Conirsci AT(3"^2)
Ip. Order from LC, Mi $1,80, ph il. 80.
GAT-p-19
Atomic Corp. , Porta-
13-2)- 1.
irslon of dissolved material in the Cnlumh<«
' P- Honstead: Ceneral Klearic Co,
Dispersion of d
fryer, by J.'
Hanford Atoi
Pinal deyim of Sandla> aupersonlc narachute teat
44p. Order from (JTS. $1.25. SC-4449(RR)
» u '^toinlc Produas Operation, Richland,
Wash. Mar 57. Contract W-3l-109-En£-52
I6p. Order from LC. Mi $2. 40, ph $3/30 '
HW-4900e
^larterly progress reports to the United Stat«>«
Atomic hnergy Commisalon tor UctoEe?~TJri^**fn-
^^J^^O^TRiHonaTTureiuor^^
ajuoai^ WaaUngion, D. C. Decl. March 2,
i2v-; -I'P- ^*^^ '^oro w:- Ml $3. 30,
I* $7. 80. NBS-D-121
fte- *"• .extract AT(30-l)-l<J^. 78p. '
Order from LC. Ml $4. 50. ph $12. 30.
NYO-7759
Akyraft nuclear propul^oo protect quarterly nror-
JSjyv O^ Rid«, Temi, 1^52. Decl.^rlS
iSS?*^™**'^!' l**'- Contract W-7405-
XX'J*^^- Order from LC. Ml $7.50.
'■♦^•»- ORNL-I170c6el.)
Aircraft nuclear propulalca protect auarterlv
_rc
L^ '.^iEJCSl rri !T3U!Miiv
High exDlo^ves. armin£. and svatemiirir« pinal
ffPOTtofproie^cflWanv, hyi u,i.. -f^jnj^^
rS^"^^' Albuaierque, N. Mex. and Unlver-
•ity of California, Lawrence Radiation Labora-
tory, Uvermore, Calif. June 60. 43p. Order
from LC. Ml $3. 30, ph $^. 80. Stf-482^)
Fifty-fUth progreas report through October 31. 19M.
Massachusetu Institute o* Teanology, Can!-
brldge, Maaa. Nov 59. Contracta AT(30-1)-
2098: NASw-37; NASw-75: and AT(30-lH06.
133p. Order from LC. Ml $6. 90, ph $21.30
TID-5766
Biolog)f and Medicine
Radiological Phvalca Dtylaja. ■imn.«n..,i ^.y»^
L. D. Marlnelll. Argopne Nadcoal Laboratory
iP'^SS^ ^^LA"t.^ Contract W-3l-109-ear
38. wop. Order from OTS. $2.75.
ANL-6199
Seaalon III--gffltt
N. Y. Mar 58. I6p
Ml $2. 40, ph$3.30:
"w Him ^T^gini 11111
iven National Laboratory.' UpcoB,
X^.
Order from LC'
BNL-a624
/^
Summary ri^
warrea and G
ofHRPln-t
Laboratory,
tract W-7405
cont)«ion test
TSvHT
o. J^S^^- "" ^S9^ National LabOTatory,
Ridtt Tenn. Aug ST Decl. with deledoM
ber23, 1959. Contract W-7405-«m-26.
fink
October
127p. Order from LC
Oak Rid«e NaUoaal
" ?59. COB-
fromLC.
Ca'-59-9-74
Ml $6. 90, pb $11.30.
ORNL-1294(Del. )
225
H««ford Wonca, Rldilaiid, Waah. July 49. Dec]
Jfrch 2. 196a f^C^ from LcT M $1. 8^
PB|1.»0. HW-1S949
7.
Accumuladpo of TadxoiacKapes in rats chronically
expoeed to reactor effluent ^'^'ter by R. F.
Palmer. General Electric Co. Hanford Atomic
Products Operation, Ridilaod, Waah. May 58.
Decl. April 28. I960. Contract W- 31- 109-Eng-
52. 18p. Order from LC. Kdi $2. 40. ph $3. 30.
1 HW-53362
Potaaaium, cesium -137 and rubidiLim-86 relation-
ships In plant uptake, aoil diffusion rates ajid"ir-
rigation practices, by J. F. Cline. General
E Metric Co. Hanford Atomic Products Operation,
Richland, Wash. May 60. Contract AT(45-1)-
1350. I2p. OtderfromLC. Ml $2.40.
ph$3.30. HW-62037
Metaboliam at Zn^ in the rat— -chronic administra-
tion studies and age effects, J. E. Ballou. Gener-
al Electric Co. Hanford Atomic Products Opera-
tion, Richland, Wash. Jan 60. Contract AT
(45-l)-1350. 2$p. Order from LC. Mi $2.70.
ph$4.80. , HW-63047
Decontaminatioo o^ pUntt exposed to a aimulated
reactor bum, 1^ F. P. Hungate, ). D. Stewart,
R. L. Uhler. and J. E. Cline. Hanford Atomic
Products Operation. Richland, Wash. July 60.
Contract AT(45rl)-l350. 18p. Order from OTS.
50 cents. HW-63173
Qg-project exposijre from Hanford reacror effluent,
by R. F. ^teorand R. L. Junkins. General
Electric Cc. Hanford Atomic Products Operation,
Richland, Wash. Feb 60. 47p. Order from LC.
Mi $3. 30. ph$7.80. HW-63654
The metabolism ahd ftmctional signiflCTnce of cobalt-
proteins. Ptntf technical report. Johns Hopkins
University, Institute for Cooperative Research.
Baltimore, Md, [195?1 Contract AT(30-l)-933.
I06p. Order ftotn LC. Mi $5.70. ph $16.80.
NYO-4870
Annual report on tesearcA project. Columbia Unl-
veraity. Radiological Research Laboratory.
New York, N. Y. July 60. Contract AT-30-1-
GEN-70. I60pi. Order from LC. Mi $7.50,
ph$24.30. NYO-9205
Semi-annual pr
m
rss ret
report for January 1, 1960
through June 3Q, 1960, by P. L. Anderson anH"
others. University oT Tennessee- -ABC Agricul-
tural ReMsrch Laboratory, Oak Rldfe, Tenn.
Nov 60. Contract AT-40- 1 -GEN-242. 73p.
Order from Orrs. $1.75. ORO-310
A selected list o< references on naarlne and aquatic
radiobiology, by A. W. Klement, Jr. and L B.
Wallen. iSvisfon ai Biology aad Medicine. Ur«.
Atomic Energy Commission, Washington, D. C
May 60. 42p. Order from OTS. $1.00.
TID-3903
Genetics research program of the Division of
Biology and MedicineT5y P. T. Ives and omers.
USAEC Office of Technical Information Extension,
Oak Ridge, Tenn
OTS. $1.25.
117p.
Order from
TID-4041
Effects of radiocobalt irradiation of- rabbit germ
cells and embryos. Annual progress report and
renewal propoaai, by M.C. cWg. Worches
ter Foundation for Experimenul Biology, Shrewa-
burg.Ma8s. [1960]. Contract AT(30- 1)- 1934.
28p. Ordter from OC. Mi $2.70, ph$4.80.
TID-5633
The relation of genome nun\ber to radiosensitivlty.
feriod covered from June 1. 1959 to May 31 .
TgrorSy A. M. Clartc. University of Delaware,
Wewark, N. J. June 60. Contract AT(30-l)-1752.
I3p. OcderfromLC. Mi $2. 40. ph43.30.
TID-6051
Study of die condensing units in nucleic acid biosyn-
thesis. Report of activities for June 1, 1959-
May 31. I960, by T. D. thrice. fcolumbTT
Presbyterian Medical Center, NewYork, N. Y.
Feb 60. Contract AT(30-1)-2208. 32p. Order
fromLC. Mi $3.00. ph $6.30. TID-5709
Effects of irradiation on the calcifying mechanism o<
epiphyseal cartilage. Period covered: May 16,
19S9 to May 15, i960, by A. Hirschman. Uew
York Sute University, Research Foundation,
New York, N. Y. June 60. Contract AT(30-l)-191S
1913. I3p. Order from>LC. Mi $2.40,
ph$3.30. TID-6054
A study of die medianlcal impedance to flow in ^
feinoral peripheral vascular bed of the dog, by
H. M. Yanof and R. W. Stacy. University of
California, Lawrence Radiation Laboratory.
Berkeley, Calif. July 60. Contract W- 7405 -eng-
48. 24p. Order from OTS. 50 cents.
UCRL-92SS
The influende of a single doee of I^^^ on the reten-
— tlon and dlstributiooatf 1^31 jn the rat by P. W.
Durbin and oAers Uni veraity of California,
Lawrence Radiation Laboratory. Berkeley. CaW.'
June 60. Contract W-7405-eng-48. 42p. Ordar
from OTS. $1.00. UCRL-9256
wBn trapezoidal-waTe electromagnetic blood flo»i
"meter and iti appUcatlon to die atudy of blooO
flow In die dog-^PbeaU by H. M. YmmI. UgVef
■Ity ol Callfbrnia, Lawrence Radlatlan Laboratocy,
226
Berkeley, Calif. Aug 60. Contract W-7405-eng-
48. 72p. Order from OTS. $1.75.
UCRL-9375
Pr
Chemithy — General
tute. Troy. N. Y. Sep 59. Contract AT(30- 3)-
241. 127p. Order from LC. Mi $6. 30.
tt%l9;60. AECU-4449
A new method for preparing hydroxide -free alkali
chioride melts, by D. L. t^arlele and D. N. —
Hume. Massachusetts Institute of Technology,
Laboratory for Nuclear Science, Cambridge,
Maea. [1959] Contract AT(30-l)-905. 8p.
Order fromLC. Ml $1.80. ph$1.80.
AECU-4551
Neutron activation analyaia. A literature search.
by E. U. Kauer. Du POnt de Nemoura CE. I. )
and Co. , Savannah River Laboratory, Aiken,
S. C. Feb 60. Contract AT(07- 2)- 1. 6p.
Order fromLC. Mi $1.80, ph $1.80.
AECU-4713
Tbe thermodynamic and tranaport properties of
sodium and sodium vapor, by E. L. Dunning.
Argonne National Laboratory, Argonne. 111.
Oct 60. Contract W-31-109-eng-38. 32p.
Order from OTS. 75 cents. ANL-6246
Solubility of xenon in liquid biamudi. by A. M.
Babayaaod W.F. Kenny. Brookhaven National
Laboratory. Upton, N. Y. Jan 59. 50p. Order
from OTS. 50 cent*. BNL-617(T-186)
K*^tlon damage to water, by A. O. Allen. Brook-
Uaven National Laboratory, Upton, N. Y.
119547). 14p. Order from LC. Ml $?.40.
1*^3.30. BNL-1960
Preparatinncf thorium oxide from ORNL diorex
nittate. by W. T. McDutfee and 0. 0. Yarbro.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Feb 57. Decl. May 4. 1960. I3p.
Order from LC. Mi $2. 40, ph $3. 30.
CF-57-2-Ii3
Altminum determination in reactor cooling water
oy J. F. Emery and C. W. Leddicotte. Oak ^
Ridge National Laboratory. Oak Ridge, Tenn.
Sep 58. 3p. Order from \LG: Mi $1.80.
l*$l-80. CF-58-9-20
ogress report on die fluorox process for April
Sb, i<)57 -January U.l^Sg. by I. B. AdanJa,
L. M. Ferria and C. D. Scott. Oak Ridge Na-
tional Laboratory, Oak Ridge, Tenn. Sep 58.
32p. Order fromLC. Mi $3.00. ph$6.30.
CF-58-9-66
Summer quarar 1958, co-op report, by M. O.
Smith. Oak Kidge National Laboratory, Oak
Order from LC.
CF-58-9-72
Ridge, Tenn. Sep 58. 16p.
Mi $2. 40. ph $3. 30.
Some effects of radiadon on solvent extraction
procesaes, W. Davis. Ir. and R. M. Wapii«.r,
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Jan 59. Contract W-7405-eng-26. 14p.
Order from LC. Mi $2. 40, ph $3. 30.
CF-59-1-90
Heyne eattraction-coulometrlc titration of uranium,
by E. L. Blevins. Oak Ridge National Labora- '
tory, Oak Ridge, Tenn. June 59. 4p. Order
fromLC. Mi $1.80, ph $1.80. CF-59-6-82
Evaluation of flame photometry for the determina-
tion of elements of the rare -earth group, by
0. Menis. Oak Ridge National Latoratory,
20p. Order from
CF-59-8-141
Oak Ridge, Tenn. Aug 59.
LC. Mi $2. 40, ph $3. 30.
>ra-
Retentionof boron with niannitol during the evapoi
tion of acid and acid-fluoride solutions, by c/"
Feldman and P. v. Hoflman. OaklG^ National
Laboratory, Oak Ridge, Tenn. Nov 59. 4p.
Order from LC. Mi $1 . 80, ph $1 . 80.
CF-59-11-87
Results of differentialbed study of the kinetics of
the absorption of UFa on sodium fluoride, P. R.
Proves, jr. Oak Ridge National Laboratory.
Oak Ridge, Tenn. Jan 60 . 35p. Order from
LC. Mi $3. 00, ph$ 6.30. .CF-59-12-10
F
Check-out of Bettis dissolved oxygen analyzer.
Models, by R. S. Greeley and others. Oak
■ Ridge Naaonal Laboratory, Oak Ridge, Tein.
Jan 60. I3p. Order from LC. Mi $2.40,
P*>>3.30. CF-60-1-57
Differential thermal analysis. QuallMtive sttidy of
nitrate-butyl phosphate systems, by W.H.
Baldwin. Oak Ridge National Laboratory. Oak
Ridge, Tenn. Jan 60. Contract W-7405-eng-26.
., I2p. Order fromLC. Mi $2.40. ph$3.30.
CF-60-1-99
227
A— aT methoda ii»ed In the ORNL radioisocope
by E I. Wyut and otheri OBc RldgB
re3SrL«bor«ory, 'Oii ndffe, Tenn Feb 6^
12p. Order from LC. NA $2 40. ph $3 30
IfrMJMm hexafluorlde: A aurvey o< theohylco-
chemiol propertiee. by R. DeWin Goodyear
Atomic C^rporationT Portamouth, Ohio Aug 60
Contract AT(33-2)-l I63p Order from OTS
I
CF -60-2-39
earth chroqiatographY aBlng bla(2-etbYHiexirt)
thophoephoric acid, by ] W Wlncheeter Okk
dge National Laboratory. Oak Rldae. Tenn
Kare. earth chroqiatofla-yphY
orthop
Mar 60 9p Order from LC
ph$l 80
Nfl $1 80.
CF-60-3-158
ium/nn to chromium fVT> In
the pryaoe <K pla tlnum ty*lt. ''XN l,^***™-
R. S. Grediey. and J C Grlew Oak R]d«e
h4atiaaal Laboratory, Oak Rldoe. Tenn May 60
5p. Onlerfr^mLC Mi $ I 80, ph $1 80
CF-60-5-112
The reactjon betyeen sulfuric acid and aliphatic
hvdrocarbooa AtJ^CO ilS-Jl. by yTTrnSadwln.
Oik ndffe Mtticnal Laboratory. Oak Ridge.
Tenn. June 60. Contract W-7406-eng-26. 9p.
Order from LC. Ml $1. 80. ph $1. 80.
1, CF-60-6-48
Plloc plant preparation
n oxidq du
&s
um oadde and thorium
year, 196a by irir
uranium -■ ,, . - ^^
3 onaJ Laboratory. Oak
Ridfe. Tenn July 6d Contract W-7405-eng-26
18p Order from CC Kfi $2 40. ph $3 30
CF-60-7-59
Coulometiic tltrttlgn of uranium In nitric acid aolu-
M 0 Fulda E I du Pont de H
^
Expli
. lemours
Co 6xp|o«lve8 Department. Atomic Energy
DtTiainn. Technical Dlvlalon. Savannah River
Laboratory, Aiken, S. C. July 60 Contract AT
(07-2)- 1 13^ Order from OTS
SO cents
DP- 492
Preciae determinatjon of uranium tn uran^ nitrate -
aluminum nitrate aoiutiooa. by C. M. MicDooald.
E. I. da Pont ie Nemours h Co. Exploaivea De-
Srtment. Atomic Energy Dtyislon. Technical
rlalon. Savannah River Laboratory, Aiken
S. C, July 6a Contract AT(07-2)-l. Tp. Order
from CfyS. S€ cents. DP-503
tflgh-t#.fn»*raturf chemiatrv o^ PMlTT-grrAlgif
Auaiw 1. 1959. byU. MertCT and w7 E. B^.
General Atomic Division. General Dynamica Corp.
San Oleffo. Calif. Sep 59. Project no. 35. In-
cludea append! V The dissociaacn preasure ot
ruthenium trichloride, by W. E. Bell. M. C.
Garriaon, andU. Klerten Contract AT(04-3)-l64
31p. Order from LC Ml $3 00. ph $6 30
^ GA-942
A lubrication -oil test program for rhr marlrlmr nn-
cooled reactor program, by I rtxppert and B
Welaaman Qeneral Dynamica Corporation, San
OlegD. Calif Apr 60
32p Order from GTS
Contract Af(04-3)-l87
$1 25 GA-1466
$2 75
GAT-280
The determination of uranium in Impure solutlonf
using an electron bqnbardment-type ny»« apec'
trometer. by C D Tabor. G. F kauf^man and
F S. Voaa Goodyear Atomic Corporation,
Portannouth, OWo Sep 60 Contract AT(33-2)-l
Up Order from OTS 50 cents GAT-292
Clean-up reactor dust separation Interim repon. by
B W7 Penland, M L. Geneva and E H. Tenner
Goodyear Atomic Corporation, Portamouth. Ohio
Jan 60 Contract AT(33-2)-l lOp Order fron
LC Ml $1 80, ph$l 80. GAT-P-15
Two Infrared methods for calculating Isomer
In dlchlorotetrafluoroet
rcent-
latlng Isomer Perce
ages in dichlorotetranuoroethane (C^4Q2). tiy
¥. C. Steinbach. Goodyear Atomic CorporadoB,
Portanwuth. OWa Nov 59. Contract AT(33-2)-l.
lOp. Order from LC. N* $1. 80. ph $1 80.
GAT-T-700
The determination of traces of vanadium In the mff
ence of an eiceas of nickel, by A. L. Cardenas
Goodvear Atomic Corporation. PortanKxith, ONo
J an 60 Contract AT(33-2)-l. 4p. Order from
LC, Ml $1.80. ph $1.80 GAT-T-715
Preparation of self botided borldee. by E W Hoyt
and Juan (jhome^ Vallecltoa Atomic Laboratory,
Genera) Electric Company. Plaasanton, Calf.
June 60. Contract ATT04-3)-189. I5p. Order
from OTS 50 cents GEAP-3332
Analytical procedures for the Plutonium metal fabrl'
cation process XI The deternilnatlon of fluo-
ride, by G.J. BeMlng. E W Chrlstopherson, and
TTTT IGsndall. Hai^Tord Worka, Richland. Waah.
Jan 51 Decl. March 7, i960. Contract W-31-
lOy-Eng-52 lip Order from LC Nfl $2 4(1
ph $3 30 HW-20036
Analytical procedures for the metal fabrication proc'
eaa. X. Determination of carbon In Plutonium
metal by a micro- cotrtwstlon metftod. by M. B.
Leboeu/. Hairford Works, Richland. Waah. Fib
51. Decl. March 7, 1960 Contract W- 31-1 (»•
Eng-52. 20p. OrderframLC. Ml $2 40,
pk $3. 30. HW-2a212
Analytical applications of refractive Index, by L. L.
Burger General tJlectrlc Co Hanford Atonic
Products Operation. Richland. Wash. Jan 52.
Decl February 17, I960. lOp. Order fnrn LC.
Ml $1 80. ph $1 80 HW- 23228
Rei?ort e< Invention on the preparation of Plutonium
trifluoride. by L. L. Burger and W E Roake
Hanford Wotks. Rlcnland, Wash. Oct 52. Ded.
January 28. I9o0. 3p. Order from LC
Ml $1.80, ph $1.80. HW-26aa
228
Plutonium trichloride: Prjparatiop raaction with
laene or carbon tetrachloride, and bonA re-
ion"to naetal. W.B. Tdley. General Electric
Hanford Xtomic Products Operation. Rich-
land. Wash. Dec 53. Decl. March 15, I960.
Contract W- 31 -109- Eng-52. 28p. Order fon
LC. Ml $2. 70, ph $4. 80. HW- 30121
Purlflcatlan of mercury metal, by K. Koyama. Gen-
eral Electric Co. Hanford Atomic Products
Operation, Rlchiaid, Wksh Nov 55 Contract
AT(45-1)-1350. 4p Order from LC Mi $1 80.
phil.SO. HW- 40123
Determination of total uranium and U^^ In Al-U
fuel elementa. bv W. L Delvln. H E Palmer.
and U. L. Upaon General Electric Co Hanford
Atomic Products Operation, Richland, Wash
Sep 58 Decl April 28, I960 Contract W- 31-
109-EnB-52. 22p. Order from LC hfl $2 70.
ph $4. 80. HW- 57464
An aqua regla flowaheet for uranium dissolution, by
yj. SKScik. Cen«-al Electric Co. Hanford
Atomic Products Operation, Richland. Waahk
uly59. Contract AT(45-1)- 1350. 6p. Order
LC. Ml $1.80. ph$1.80.
61048
Bvalutfiop of deoKYgenating ion exchange r«»lna. by
T.F. Demmltt. General Electric Co. Hanford
Iiomic Producta Operation, Richland. Waah.
Sep 59. Contract AT(45-1)- 1 350. Up. Order
. _ ^^_^
fromLC. Ml $1. 80. ph $1. 80.
-61872
Preliminary feport on the uae of activated carbon aa
_ It for the dissolved ontygen- aqueous hv
razine reactlcy. by T. F. Demmitt. General
Electric Co Hanford Atomic Producta Operation,
Richland, Waah Feb 60 Contract AT(45-1)-
1350 8p. Order from LC \fl $1 80, ph $1 80.
HW^63917
Thf.anat
lutonlum'241 in urine, by J. D.
analvaia of tJutonlum-241 , ,
Ludwlck General Electric Co Hanford Atomic
Products Operation, Richland, Wash May 60
Contract AT(45-l)-1350. 9p. Order from LC
Ml$1.80. ph$1.80. HW-64170
A detailed study of the carrier concentration nnethod
cf spcctrocoanilc^ analyaia. by I. L. Daniel.
General Electric dlo. Hanford Atomic Producta
Operadan, Richland, Waah. May 60. Contract
AT(45-1)-1350. 97p. Order fxm LC. Kfl $5. 40.
ph $15. 30. HW-64299
htJlnAnary report on pH control j^y Ion exchange
in high pH svatenM. by T.F. Denunltt. General
Blactric Ca Hanford Atomic Producta Operadan,
Richland, Waah. Apr 60. Contract AT(45-1)-
1350. Idp. Order bt>mLC. Ml $2. 40,
ph $3. 30. HW-64403
atillzattoo of cealum (hiring calcination and
Voiatillza
Bouae
.__ - ■- and hYTT
Hanford Atomic Producta Operadon, Richland.
Waah. May 60. Contract W- 31 -109- Eng-52.
6p. Carder from LC. NA$1.80, ph$1.90.
HW-64528
High flow rye operatloD of a duplex Ion exchamBe
syatjBm. by T.F. Denunltt. Hanford Atomic
Producta Operation. Richland. Waah. June 60.
Contract AT(45-1)-1350. 3lp. Order from OTS.
$1.00. / MW-65478
A atudy of the feaalbUlty for the large scale recoyery
of Ionium (thorium-230) from the uranium ore
milling Inouatry in the United States, by C A.
Rohrmiuui General Electric Co H anford
Atomic Products Operation, Richland. Wash
June 60 19p Order from LC Ml $^ 40.
ph $3 30 HW-65518
An analytical method f or gulfur In nuclear reactor
Ite, by D. M. Robertson Hanford Atomic
eta Operation, Richland, Waah. June 60.
Contract AT(45-1)-1350 12p Order from
OTS. SOcenta. HW-65522
Water chemiatry for KER loop l-'lune 29. 1959 to
December Si! 1«9. by TVP. Kmmltt and E.R.
Wood. General Electric Co. Hanford Atomic
Producta Operation, Richland, Waah. June 60.
Contract AT(45- 1)^350. lOp. Order from LC.
Ml $1 . 80, ph $1 . 80. HW-65632
A potendometric study of zirconium— nitrate and
jdrconium — fluoride systems, by A. I. Moffat.
Philllpa Petroleum Company7 Atomic Energy
DlYiaion^ Idaho Falla, Idaho. Aug 60. Contract
AT(10-1)-205. 12p. Order fromOTS. SOcenta.
IDO-14517
Denaitiea of anunonium fluoride— anrnmnlum nitrate
~-ammonium hexafluorirconate s^utlons. by
L. Teague and D. P. Pearson Philllpa Pwrxr
eum Company, Atomic Energy Dlviaion, Idaho
Falla, Idaho Oct 60
15p Order from GTS
Contract AT(lO-l)-205
50 cents IDO- 14528
Determinadon of total flasion product molvfadenum.
technetium, and tellurium in ICPP waste tanks,
by W.J. MSeck. P. W Dylcea, and sl. Yaim-
mura. Philllpa Petroleum Ctmmany, Atomic
Energy DlTialon. Idaho Falla, Idaho. Sep 60.
Contract AT(10-1)-206. 24p. Order from OTS.
SOcenca. IDO-14S29
Recwt developmenu In the analydcal chenriatry
of thorium and Ita compounda. by C. V. Banto.
Amea Laboratory, Amea, Iowa. Feb 58. CoiP-
tract W-7406'-eng-82. 54p. Order fromLC.
Ml $3. 60. ph $9l0. ISC-9M
. meMurementa. br G. A.
ivec. Amea Laboratory, Anaes,
Nor 58. Contract W-7406-enrS2 S7p.
CKlar frooi OTS. $1.00 ISC-USB
229
i
Safe hancQlnK ai chorine tiifluoriite «nd the chenal«- Supriementyy technical report on >n Improved
try o< the chlcylne oaddea and OKyfluorideg. by
R. L. Farrar. Jr. Union Carbide Nuclear Co. ,
CMviaion at Union Carbide Corporation, Oak
I^idge Gaseous Diffusion Plant, Oak Ridge, Tenn.
Nov 60. Contract W-7405-eng-26. 33p. Order
fromOTS. 73 centa. K-1416
AnalvBlg of hyili>yeii~ tritium mtxturea by the therm-
al conductivity rnet hod. byF.K. Heumann.
ICnoUs Atomic Power Laboratory, Schenectady,
N. Y. July 53, Decl. March 15, 1960. Con-
tract W-31-109-Bng-52. 20p. Order from LC.
Ml %2. 70. ph U 80. lCAPL-970
ratloo of hvita'ogen iaotopea by aorpdoii In
" ■ " F. K. Heur
The a< ^ .. „ .
palladtum. by O. N. Salmon and F. K. Heumann.
knoUs Atomic Power Laboratory, Schenectady,
N. Y. Jan 55 Decl March 28. 1960 Contract
W-31-109-Enr52 29p Order from LC
Mi $2 70. ph |4 80. ICAPL-1249
4
The polarofraphld determination of niobium in
«P
conium base ajloyg. by D. P Strlcoa June
iCnolla Atomic Power Laboratory, Schenectady,
N. Y. Contract W-3l-109-Eng-52 jto Onfer
fromLC. N«$1.80. ph $1 80. lCAPL-M-[»S-3
The determination of lead and tellurium in lead—
teUurluni alloya. by O. I. Artlcoio. IGioUs Atom-
ic Power Laboratory, Schenectady, N. Y. June
60. Contract W- 31 -109- Eng-52. lip. Order
fromLC. Mi $2. 40. ph $3. 30. KAPL-M-OjA-2
Correl<ttiop of the|-naobalance data, by J. H. Paahley.
Carbide and Carbon Chemlcala Co. , K-25 Plant,
Oak Ridffe, Tom. Jan 55. Decl April 28. 1960.
Contract W-74l06-eng-26. 23p. Order from LC.
KA$2,70, ph|4.80. iCLD-46
The potarographic, determination
preaence of ptjitonium. by ^
AlamoB Scientific Laboratory,
Decl. July I, 1956 Contract
3(^ Order fipm LC. Mi $2
uranium in the
Smith. Cos
N. Mex. Ma* 51.
W-7405-eng-36.
70. ph $4 80
LA -1249
. carbon in uranium,
by W. G. Smilay Loa Alamos Scientific Labora-
tory, N. h^x May 54 Decl March 15. 1960
Contract W-74l05-eng- 36. 28p Order from LC
Ml $2. 70. ph $4. 80. LA-1733
raity of California,
Aiamoa Scienttfic Laboratory, Los Alamos.
N. Mex. Sep 60. Coutraa W-7405-eng-36. 98p.
LAM5-2457
Order from OTS. $2.25.
ioD at, eauipment to cutdoyn the dust
losses in the TA-7[UPa] unlosdlng
tfpenttlqn. by W. A. Unpoid. Malllncln-odt cfemi
cal Worka, St. Louis. Mo
March 7, 196a
phSl.SO.
Dec^. Decl.
Order fromLC. Ml $1.80,
MCW-160
proceae for the manufacture of high purity cal-
Period cwered November 10. 1948 to
ciuni.
tanua'ry 31. 1949. by H. Brown and P.
Metal Hydridea, Inc. , Beverly, Maaa.
Decl. February 16, 1960. Contract >
GEN-213.
ph $7. 80.
42p. Order from LC.
Woodberry.
Oec4S.
AT-30-1-
Mi $3. 30,
MHC-5
Analvala of hydrogen iaotopea by maaa Bpectronaetg,
by K. W. Foster. Mound Laboratory, Monaanto i
Oiemlcal Company, Research and Engineering
Division, Nfiamisbur^ Ohio. Nov 60. Contract
AT-33-I-GEN-53. 16p. Order from OTS.
50 cents. MLM-1099
The solubllltY of salta In metals, by S.J. Yoslm and
E.B. Luchsinger Atomics International Division
North American Aviation, Inc , Canoga Park,
Calif Aug59 15p Contract AT-11 -l-GEN-8
15p Order from LC Ml $2 40, ph $3 30
NAA-SR-3940
A thermogravi metric balance for the InveatiiBtticj
of high tenriperature reaction kinetics an<
results of a beryllium oxidation sttidy. by M. M.
Nakau Atomics International, A Division of
North American Aviation, Inc. , Canoga Park,
Calif Nov 60 Contract AT(11-1)-(!en-8. 27p.
Order from OTS. 50 centa. NAA-SR-'4747
The radlolyslB of deuterated biphenylB: Mechanism
of hydroBpn formation, by I. G. Burr and I. M.
rough. Atomica Intematioial. Divialoo
of North American Aviation, Inc. , Canoga Park.
Calif. July 60. Contract AT-U -l-GEN-8. 29p.
Order fromLC. Mi $2. 70. ph $4. 80.
NAA-SR-4961
>e synthesis of blphenyl-2. 2 ' 6. 6'-d4. blphenyj-
2. 2\ 3 3-. 5. 5-. 6. 6--d8. ami bl5RiirYl-dHv by
R.I. Akawle. Atomics International. Auivlsioa
of North American Aviation. Inc. , Canoga Park,
Calif. Nov 60. Contract AT(ll-l)-GEN-8 12p.
Order from OTS 50 cents NAA-SR-5547
closed system to
iss^
by G. M. Wolten and
The conmatibllltv of key jyne witn sodium in a
Beds'.. ^
R.A. Meyer Atomics Intertiatiooal A Division
of North American Aviation, Inc , Canon Park,
Calif Nov 60 Contract ATdl-D-GQ^B lip
Order from OTS 50 cents NAA-SR-568f
azakl. North Ai
IS a poaalMe reactor cooiant. byT.T. SUnr
azakl. North American Aviation, Inc. , Downey.
Calif. June 53. 6p. Order from LC. Kfl $1 . 80^
ph$1.80. NAA-SR-KfenBO-713
Sodium vai
(Mum vapor detection test. byD.L. Whitlock.
North American Aviaiion, Inc. , Downey, Calif.
Jan 56. 8p. Order from LC. Ml $1. 80,
pii$1.80. NAA-SR-Meino-15S2
taken from
. , Lawrence! Atomics
Intematlonal Dlvlalcn, North American Ariadon,
230
Inc. , Canoca Park. Calif. Oct 58. 4p. Order
fromLC. Ml $1. 80, ph $1.80.
NAA-SR-Nfcmo-2928
T|iy Mgh temperature chemical reactivities of the
uranium carbides, by L. Silverman. Atomic
International, Division of North American Avia-
tion, Inc. , Canoga Park, Calif. Aug 59. I6p.
Order from LC. Mi $2. 40, ph $3 30.
NAA-SR-Mentjo-4269(Rev. 1)
[■'
Literature survey on properties of sodium vapor. by
C. Ervin, Jr. Atomics International Division
of North American Aviation, Inc. , Canoga Park,
Calif. Sep 59. I3p. Order from LC Ml $i: 40,
po$d.30. NAA-SR-Memo-4417
A naethod of correcting mass patteroa of deuterated
hydrocarbons for Isotopic impurities of carbon-
13. hydrogen and deuterium, by R. H. Shudde.
Atomica international. Division of North Ameri-
can Aviation, Inc. , Canosa Park, Calif. Apr 60.
Contract AT-11 -l-GEN-8. 12p. Order from
LC. Mi $2. 40, ph $3. 30. NAA-SR-Memo-5125
The pciarographlc determination of uranium (VI) in
uranium tetrafluoridy. by M. W. Lemer and F.
Jaffa. New Brunswick Laboratory, Atomic Ener-
SConunisslon, New Brunswick, N. J. Oct 56.
. Order from LC. Mi $1 . 80, ph $1 . 80.
NBu-132
i
Sdttttsn technique in an41yBis of ntetal allova by
X-ray fluorescent spectrometry. byF.A. Bau-
man, B. Wessling, and L. Zopatti. Nuclear
Metals, Inc. , Concord, Mass. Mar 60. Con-
trad AT(30-1)- 1565. 22p. Order fromLC.
tA $2. 70, ph $4. 80. i NMI-1231
First annual progress report. byJ.G. Floss Tem-
rie University, Research Institute, Philadelphia,
Pa. Sep 58. Contract AT(30-l)-2082 24p
Order from LC. Ml $2. 70, ph $4 80
I NYO-2155
Enthalpy titrations in fused salts. Proffess report
and request for Contract renewal. Summary of
progress: lanuarv 1. 1959- -December 3l7l?59.
Jordan. Pennsylvania State University,
. Jege of Chemistry and Physics, University
Park, Pa. Jan 60. Contract AT(30-1)-2133. 19p.
Order from LC. Mi $2. 40, ph $3. 30.
NYO-2216
I
Anrilrarions of ultrasonic energy. Proflress report
no. 15 covering period April 1. 1959 to May 31,
1959. AeroprolectB. Inc.. West Chester. PaT"^
June 59. Contract AT(30-1)-1836. 28p. Order
from LC. Ml $2. 70, ph $4. 80. NryO-2569
!
Utilization of radloactlv^ isotopes in cosl process
research. Quarterly technical status report no.
m
report
bvT. V
2 for lunel. 1959- August 31. 1959. byr~M:
Vavorsky and E. Gorin. Consolidation Coal Co
Research and Develdpmeni uivlskxi, Library,
Pa. Sep 59. Contract AT(30-l)-2350 34p
Order fromLC Ml $3 00, ph $6 30
- i I NYO-2594
Utilization of radioactive isotopes In coal process
research. Quarterly technical status report no.
4for Decendwr I. 1959-_-Februarv 29. f960. bv
P. M. Yavorsky and E. Gorin. Consdidation
Coal Co. Research and Development Division,
Library, Pa. Mar 60. Contract AT(30-1)-2350.
29p. Order from LC. Mi $2. 70, ph $4. 80.
NYO-2596
>8lon product apolicauons using gaseous beta
soufces Quarterly progress report no 3 for
Septen^r 1. 1 959 to November 30. 1959. bv
H.S. Miller and J. H. Zufall Air Reduction Co
Inc Central Research Laboratories, Murray
Hill, N. J. [1959] Contract AT(36-l)-2343
19p Order fromLC Ml $2 40, ph $3 30
NYO-^6Q5
Preparative radiatlan chemlBtry: Reaction of nitric
oadde with some organic liquids induced bv high
energy electrons, bv A. Hen^eln. Mellon Insti-
tute.Radiation Research Laboratory, Pittsburgh.
Pa. Dec 59. Contract AT(30-1)-2310. I6p.
Order from LC. Mi $2. 40. ph $3. 30.
NYO-2870
Preparative radiation chemistry: The resctions of
hydrocarbons with phosphorus trichloride and
otter inorganic chlorides under the influence of
hiidi energy electrons, by A. Henriein. Mellon
Institute. Radiation'kesearch Laboratory, Pitts-
burgh, Pa. Dec 59. Cbntract AT(30-l)-23lO.
18p. Order from LC. Mi $2. 40, i* $3. 30.
NYO-2871
Thermodynamic, spectral and structural studies of
complexionB^ Annual reporT Massachusetts
Institute of Technology, Cambridge, Mass
Mar 60 Contract AT(30-1)- 1965 24p Order
fromLC Mi $2 70, ph $4 80 WO-2932
Study of radiation induced sc^ld state polymerization.
Annual progress retyrt for February 1. 1958 to
February 1. 1959 Fed vtechnic Institute. Brook-
lyn, N. y. L 19591. Contract AT(30-1)-1715
3Sp. Order fromLC Mi $3. 00, ph $6 30.
NYO-7231
The rates of adsorption of polvmeric flocculating
agenta on chemically pure Boilds. Electrophoref
Ic mobility in relation to potential (teterniinlng
. ' :i'^l '^Tr^- "' * • "^^ '-■'^^r ana f\. n. ar
Jr. Ccfumbia University, New York, N. Y.
Aug 59. Contract AT(30-1)- 11 89. 32p. Order
from LC. m $3. 00. ph $6. 30. NYO-7405
Electron spin resonance spectra of molten salts.
Teclmical progress report, by M. Kukk and B. S.
Sundheinx New York University, New York,
N.Y. Jan 60. Contract AT(30- 1)- 1938. 50p.
Order from LC NA $3. 30. ph $7. 80.
NYO-7743
Some electron and proton resonance studies in heter-
ogeneous catalysis, by I. Turkevlch and others.
231
Princeton University, N. J. June 60. Contract
AT(30-1)-I15a. 31p. Order from LC. Mi $3. 00.
ph $6. 30. NYD-8009
The latent heat o€
',fualon of lithiuna hydride from
cryogenic meaaureipenta. by C. K. M ~
Tufta Uoiveratty, Mec&ord. Maaa
tract AT(30-n- 1410.
Ml (1.80. phll.80.
^iesaer
Ntey60
Order from LC
I NYO-8a27
Con-
The heat d formatinn ci >liim«mifn hvdrlde from
heat of reytlcyi with hvdrochlfgic acid, by C. E
Meaaer Tufta University. Medford, Maaa
May 00. Conuact AT(3O-l)-1410. 8p Order
fromiX:. Mi $1.80, ph$1.80. NV0)-8Q28
Effective cadmium cutoff enendea. by R. W. Stough*
lon, J. Halperin. and M. P. Lietzke. Oak Ri^,
National Laboratory, Oak Ridge. Tenn. May M.
Contract W-74l05-eng-26. 34p. Order from LC.
Ml $3. 00, pfa 16. 30. ORNL-2823
Stou^cii. J.
ight
sNai
inergiea. Supplement, by
Halperin. and M. P. Lietzke.
Effective cadmium cUtofl «g>er
Oak Ridge National Laboratory, Oak Ridge, Tenn.
May 60. Contract W-7405-enff-26. 6p. Order
fromLC. Mitl.80. ph$1.80.
I ORNL-2823(SupplJ
PurifirariOD trf kilQcurie guanlrlea d prnTtigth<uni-l47
by ion exchanfle. by R. S. Preaaly and othera.
dak Ridge National Laboratory, Oak Ridge, Tenn.
Jul, 60. Contract W-740S-eng-26. Up. Order
fromLC. Mi (2 40, ph $3. 30. ORNL'2928
NL-2983
A bUAloKryhy of Research on kinetic iaotppe effecta.
by A. Fry and cithers. Univeraity at Arkanaas.
Fayettevllle, Ark. [1969]. Contract AT(40-1)-
277. . 31p. Order from LC. Mi J3. 00. ph $6. 30.
I OR6-252
The tmprrtfv anal^^la ci anw^rtoiT^ aolutlooa. by A.
J. Anderson and E. Vejvoda. The Dow Chemical
Cbnmany, Rocky Plata Plant, Denver, Colo.
Sep 60. Contract AT(29- 1)1106. 28p. Order
fromOTS. SOcenu. RFP-194
tnteraytem crnaai^y from Mgh«»r fntritt^ mtmtitm in
complex molecyles. byR.E. Whan and G. A.
Crosby. Sandi^ Corporation, Albuquerque,
Mbx, Oct 60. 20p. Order from Ore.
SCTM-234-60(5I)
N
SO
Selected bil>liograi]^Y of phYsicochemical properties
In liquid anunocia and relyedsoi vents, by R. F.
Sankuer and |. L. Dye. Kfichiian Sute Univer-
aity, Eaat Lansing. Mich. Oct 59 Contract
AT(11-1)-312 96^ Order from OTS $2 00
TID-3904
Interim andprogreas report for pertod covering
February 16 to March 15. 1960. by H. G. Petrow
tonica. tnc.. Cambridge. Maak Mar 60. Con- '
tract AT(3O-l)-2470. ITp. Order from LC.
Ml $2. 40, ph $3. 30. TID-5056
Spectiophotonnetrlc Investigations of alkali metali
in liquid ammonia Theala. byR.C. Douthlt
Kflchigan State Univeraity, East Lansing. Mich.
1959 Contract AT(11-1)-312 I15p Order
fromLC N« $6 00. ph $18 30 TID-5657
I.
mnedca and niechanism for the electrochetnical
reduction of benzophenone In acidic media. Re-
port no 53. by M. Suzuki and P. >■ Elving "
KflcMgan University, Ann Arbor. Nflcn Feb 60
Contract ATu 1 - 1 )-70. 40p. Order from LC.
Mi $3. 30, ph $7. 80. TID-571 1
rogreaa report. I The thermodynamics and
klnetica of coordination comixxinds. II ~
Progreaa report
netica of coordination conyou
chenniatry of uranium alats In sdution. by M."
he
Cefcda and P. Gentile. Forham University,
New York. N. Y. Mar 60. Contract AT(30-1)-
906. 54p. Order from LC. Ml $3. 60. nh $9. 30.
tlD-5738
The use of a fluidized bed reactor for the continuoua
oduction of uranium trJOTlde. byW. c. Philoon.
F. Sanders, and W. T. Traak. Malllnckrodt
ChemicAl Worka. Uranium Divlaion. Weldon
Spring, Mo. [ 19601 Cotract W-14-l08-eng-8.
19p. Order fran LC. Kfl $2. 40. ph $3. 30.
TID-5750
Annual prop-ess report and renewal proposal on In-
yesttgation o< the conatruction of fused electro-
lytes, by I. O'M Bockris University of Penn-
sylvania, Philadelphia, Pa Contract AT(30-1^
176y 29p. Order fromLC. Mi $2. 70,
ph U 80 TID-575I
Radium procedure. Progress report covering period
March 16 to April 15. 1960. Ionics. Inc. .Cam-
bridge, Maaa. Apr 60. Contract AT(30-1)-2470.
18p. Order from LC. Mi %2. 40, ph >3. 30.
TID-5772
Tbg gffggt o(
K gfft
aden^
loaine trl
ralba.
... ■ **L "y ^- ^- ' *""
Waahington Univeraity, St. Louia, Mo.
Mar 60. 92p. Order from LC. Ml $5. 40,
ph $15. 30. TID-5875
ThermocrvtallQgraphv of the hvdrld«>« nf ritaniunt,
zirconium and hafalunt by E.I. Goon and J.
Malglolio. Tufta Univeraity. Medford. Maaa.
[1959?]. lOp. Order fromLC. Mi^l 80,
ph$1.80. TID-5913
Phaee equilibria, kinetic and thermodynamic studies
ol some rare eartn and other metal oxide and
tract ATU l-l)-72 l37p
Ml $6 90. ph$21 30.
Con-
Order from'LC.
TID-5914
232
1
Tr|nalent electrode potentials of mercury. Techni-
cal report no. XXXVII. by C. D. Spear and
others. University «'if Utah. Institute for the
Study of Rare Procet sea, Salt Lake City, Utah.
May 60. Contract A|f(ll-l)-82. 104p. Order
from LC. Ml $5. 40, ph $15. 30. TID-5968
^palvia of experimental data on the holdup of
radloactlye gases on.charcoal adsorption traps.
by T.J. Delaney and others. Massachusetts
Institute of Techncdcwy, Engineering Practice
Schooi. Oak Ridge, Tenn. Mar 59 27p.
Order from LC. Ml $2. 70. ph $4 80.
> TID-6079
^orpdcn spectra and -bonductlvity meaaurementa
of some metal chelates Period covered: £"
tenaber 15, 1959 to and including June 15. I"
by M P. Uoekley Georgian Court College,
Lakewood, N. J June 60. Contract AT(30-1)-
2069. 35p. Order from LC. Ml $3. 00,
ph $6. 30. TID-6069
Tafalea of ionization potentiala. by R. W. Kiaer.
Department of Chemistry, iCansaa State Univer-
sity, Manhanan, Kan. June 60. 202p. Order
from OTS. $3.00. TID-6142
Petroleum refinery atreAma aa oroapective reactor
coolartts: Thermal atabillty investigations, by
LG. CarroU. Calif {>mia Reaearch Corporation,
m Francisco, Calif. May 60. Contract AT
(ll-l)-174. 47p. Order from GTS. $1.25.
TID-6367
A new liquid explosive. NTN. by A. von Egidy and
othera. The University of California, Lawrenpe
Radiation Laboratory, Livernxn-e, Calif. Jani
60. Contract W-74(B-eng-48 12p. Order
frOuiLC. Mi $2. 40. ph $3. 30. UCRL-5861
Thermal e:
\
manaion of hteh tenroe
Kriborian. L^iiverslty
rature materlala.
O. H. Kriborian. Ujiiversfty of California
Lawrence Radiation Laboratory, Llvermore.
Calif. Sep 60. Contract W-7405-eng-48. 7p.
- ' ,-6l
Order from OTS. 50 centa.
UCRL-6132
Chemiai
imiatrY of »pnae hydrolYzed Cr ni polymers, by
J. h. FinhoiLt. University of California. Caw-
rence Radiation Laboratory, Berkeley. Calif.
Apr 60. Contract W-7406-eng-48. btm. Order
from OTS. $1.50.
I
:RL-8879
Rate of elimination of water nydecules from the
first coordination sphere of paramagnetic
catjona aa determined by nud^y magnetic
Wt
^glft. by
nia. Law-
reaonance meaaureirtenta of _ . --
E.D. Stover. University of Caltfomiar
rence Radiation Laboratory, Berkeley, Calif.
July 60. Contract W-7405-eng-48. 33p. Orxier
from OTS. 75 centa. UCRL-9265
A mass-spectrometrlc Investigation dt sulfur vapor
as a function o|f tetryefature. Thesis, by M.
C. Zietz University of California Lawrence
Radiation Laboratory, Berkeley, Calif June 60
Contract W-7405-eng-48 82p Order from
OTS $2 00 UCRl-9277
Hirfi-pressure vapor-liquid equilibrium apparatus
lliefiia. byR. L. Miner University of Califor-
nia Lawrence Radiatlm Laboratory, Berkeley.
Calif July 60 Contract W-7405-eng-48 56p.
Order from OTS. $1 25 IX:RL-9285
Some low-temperature nuclear- orientation studies.
Thesis, by I. P. Schoolev. University of Cali-
fomia. Lawrence Radiation Laboratory, Berke-
ley, Calif. July 60. Contract W-7405-eilg-48.
43p. Order from OTS. $1.00. UCRL-9296
Perturbation of alyrfia-^mma angular correlationa
in iransuranium iaotopes. Thesis, by E.
Flamm. University of Callfonda, Lawrence
Radiation Laboratory, Berkeley, Calif Aug 60.
Contract W-7406-eng-48. 58p. Order from
OTS. $1.25. UCRL-y325
Infrared 8t)ectra of rnarainally metallic syBtems.
Theais. byt.A. Beckman University of Cali-
fornia, Lawrence Radiation Laboratory, Berke-
Ic y. Calif Aug 60 Contract W-7405-eng-48.
7zp Order from OTS $1 25 UCRL-9330
Some problenne of crystallography Theaia. by
Q. C. Johnaon Univeraity of California Law-
rence Radiation Laix/ratory. Berkeley, Calif.
Aug 60 Contract W-7405-eng-48 59p Order
from OTS. $1 50 U(mL-9350
Search for a 0* . 2*. ,4* tritrfet in the vlclnitv of
i .140 Mev 1^06. by IT E. Boach ^ & I.
Horen. University of California. Lawrence
Radiation Laboratory, Berkeley, Calif. Sep 60.
Coutract W-7406-eng-48. I6p. Order from
OTS. 50 centa. UCRL-9385
aecttlcal PTOPertlea of organic aolid« I
of organic aolid« I Klnetica
1 donora. Theaia. by D. R. othera. University of California. Lawrence
mechaniam of .
fiee phthalocyaniiy . ^ . ^ „
tron acceptors and donora. Theaia. by D. R
ICeama Univeraity of California. Lawrence
Radiation Laboratory, Berkeley, Calif, Mar 60.
Contract W-7405-enf-48. 121p. Order from
OTS. $2.50. UCRL-9120
Bio- organic chemistry quarterly report for March,
April, Kfcy 1960,by G. 'CIaes6nVAd dtfuttk
CJnlveraU/dl UAllfomia. Lawrence Radiatkn
Laboratory, Berkeley, Calif June 60 Contract
W-7406-eiir48. 13Sp Ortler from OTS $2 50
^ UCRL-9208
233
University i
Radiation Laboratory, Berkeley. Calif. Sep 60.
Contract W-7405-eng-48. 51p. Order from
OTS. $1.25. UCRL-9408
The determination of uranium in uranium xlrcaalum
alloys, by G. W. Goward and othera Weatlng-
IKUM Electric Corpcratlon, Bettls Plant, Btta*
burgh. Pa Apr 56 Contract AT- 11-1 -GEN-
14 8p Order fromLC Ml $1 80, ph $1 80
WAPD-CTA«a.A)-20l
The determinatlan of total uranium in hlghpuiity
uranium dioxide by Ignition, by G W Goward
and V. R. Wiiderkehr Westinghouse Electric
Corporation, Bettia Plant. PittsburRh, Pa Feb
58. Contracc AT-11-l-GEN-U. 3p Order
fromLC. V4 $1. 80, ph $1. 80.
WAPD-CTA(GLA)-536
Chemistry— Radiation- and Rodiochemistry
A method of determtng total U-235 In flat con -
fJauratlonB. by F. K. WHte and R. B. Perr]
Chicago Operations Office, ABC Argonne,
minaticyi of uranium in high puriiY uranl-
uni OKides. by G. W. Goward anid V. R. Wleder*
kehr. Weatinghouae Electric Corporation,
Bettls Plant, Pittsburgh. Pa. Feb 58. Contract
AT-11-l-GEN-U. 7p. Order fromLC.
Ml $1. 80. ph $1. 80. WAPD-CTA(GLA)-537
The determinaticy of tetravalent uranium In high
purity uranluai oxide, by G. W. Goward and
V. R. Wiedetkehr Westinghouse Electric
Corporation, Bettls Plant, Plnsburgh, Pa Feb
58 Contract AT-II -I -GEN- 14 Sp Order
from LC Ml $1 80. ph $1 80
WAPD-CTA(GLA)-S38
I
ni. and Argonne National Laboratory, Argonne
ni. Nov 60: 23p Order from OTS
50 cents. COO-272
Neutron actlyatlon analysis by means of short-
lived isotopes, byj. L. Brownlee, Jr. Univer-
sity of Kflchigan, Department of Chenaiatry,
Ann Arbor, Mich June 60 Conrract ATJlll-I)
70 208p Order from OTS $3 00
TID-6311
Chemistry — Separation Processes for
Plutonium and Uranium
The determlnatlai of uranlam in high purltv enrich- PMrtflc^Ugn pf thorgx VTKW ggtvgnt Final rCT
ed uranium n^etal t>e'leta. by G W Goward and
others Westinghouse Ele ctrlc Corporation,
Bettls Plant, tMttsburgh, Pa Mar 58 Contract
AT-ll-l-GEN-14 8p Order from LC
Mi$l 80, ph$l 80 WAPD-CTA(GLA)-553
Laboratory manfial: naethods for the diemical and
spectrochemical analysis of zlrcoBlum and
arcaloY. by G W. Goward and R. M. lacoba.
Westinj^Kiuse Electric Corporation. Bettls
Atomic Powej Laboratory, Plrtsburgfh, Pa.
Nov 59. Contract AT-Il-l-GEN-14. 170p.
Order from UC. VB $7. 70. oh $30. 30.
WAPD-M(GLA)-790
for December 1. 1958 to November 1.
9^ by F Slcilio and others
The determinatiai of uranium in PWR Zlrcalov base
fuel alloy, by G. W. Goward and qthers West-
inghouse EleQtric Corporation. , Bettls Atomic
Power Laboratory, PlnsburgtL Pa Apr 60
Contract AT-ll-l-GEN-14 8p Order from
LC. MI $1 8P. ph $1 80 WAPD-M(GLA)-830
Ion exchan
ct AT-11-l-GE
A $1 8b. ph $1
fperformano
resins Stai
J. Sli^ey V
ormance of mixed bed ammqnium-
Status report, by G P Simon
ey Westinghouse Electric
hydroxyl res
a^ W J.
Corporation, Atomic Power Division, Pittsburgh
Pa June 56 Contract AT-ll-l-GEN-U 36p
Order from UC Ml $3 00, ph (6 30
WAPD-SFR-PD-in
Georgia Instl-
tute of Technlcology, Engineering Experin^ent
Station. Atlanta. Ga. Jan 60 Contract W-
7405-eng-26, subcontract no 1374 49p
Order from LC Ml $3 60. ph $9 30
AECU-4716
Chemical engineering division summary report
for October. November, and December 1956.
Argonne National Laboratory Argonne. Til
Mar 57. Decl March 21. 1960 Contract
W-3l-109-eng-38. lllp. Order from LC.
Ml $6. 00, ph $18. 30. ANL-5668
Chenaical engineering division summary report
for April. May. June. 1960. by S. Lawroekl
and others Argonne National Laboratory,
Aroonne. Ill Contract W-3l-l09-eng-38
178p Order from GTS $2.75 ANL-6183
Nltridatlon of crucible skulls from melt refining.
byR. K Sleunenberg. T R Johnson, and GTp.
Brunzie Argonne National Laboratory. Arooo*
ne. III Sep 60 Contract W-31-l09-eng-38
23p Orda- from GTS .50 cents ANL-6211
The determlnatl
lithium chlor
J. H. Rowan
Di
r
cii qI trace quantities of glnc In
r^^by ^terivatlvy poiarograpt^Y, by
union Carbide Nuclear Conmany,
vision of Union Carbide Corporation, Y-12
Plant. Oak Ridge, Tenn. Oct oO. Contract W-
7406-eof-^6. 21p. Order from OTS. 50 cents.
Y-1320
FTOa
bterson and
, Columbus,
OWo Aug 60 Contract W-740S-eng-92 62p
Order from GTS $1.50 BMI-1459
Recovery ct uranium from nurex lEU Profloresa
rpjort. by E._M ^ampson, Jr. _ OakJRld^e^
tricdcwr
eterniinatipnfrf carhop in
M Massey. Union Cargide
Divlaion at Union Carbide
Tenn. July 52. Decl.
tract W-7406-eng-26.
Ml $2. 40. ph$3.30.
March 23. 1960. Con-
15p. Order from LC.
CF-52-7-I63
beryllium, by E.
clear Company.
Corporatlan. Y-12 Plant, Oak Rldffe. Tenn
Oct 60. Contract W-7406-eng-26. 2lp. Order
from OTS. SOcenu. Y-1321
gii lYi^f m Irrr \lrr IdiJr
^ -^-- -,.-,,-flgPl«nt. by J. M Hoi
Oak I«d9B National Laboratory, Oak Ridge.
234
Tenn Nov 52
Order from LC
Decl March 23. 1960 41p
Ml $3 30. ph $7 80
i CF-52-11-39
Thnrex Pilot plant: System for concentrating second
urai^um. by W. L. Albrecht Oak Ridge Nation-
al Laboratory. Oak Ridge. Tenn Jan 57 Decl
Ntoy4, 1960. Contract W-7406-eng-26. 25p.
Order from LC. Ml $2. 70, ph $4. 80.
CF-57-1-149
TgP atripping in bubble-cap ^oiunin and concomitant
gap f c
Broduct evaporation. „. .. .. — ._. ^
atlonal Laboratory, Oak Ridge, Tenn. Mar 57.
Contract W-7406-eng-26. 15p. Order from LC.
Ml $2. 40, ph $3. 30. CF-57-3-80
Oiemical technology diyisioo unit operations section
monthly progress report Frf)ruarY 1958. by J.
C. Bresee and othera. Oak Ridge National Labor-
atory, Oak Ridge. Tenn June .SB Contract W-
7406-eng-26 53p Order from LC Ml $3 60,
ph$9 30 CF-58-2-139
qtemical technotogy division unit operations section
monthly progress report April 19S8. by 1 C
Bresee and others Oak Ridge, National Labora-
tory, Oak Ridge. Tenn Sep 58 Contract W-
74(B-eng-26 65p ; Order from LC Mi $3 90,
ph $10 80 CF-58-4-123
Chemical technoloyv divlaion unit operatiOD sficUflL
monthly progress report lune 1958. by I. C.
Bresee and othera. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. Oct 58. Contract W-
74(B-eng-26. 66p.". Order irom LC. Ml $3. 90,
ph$l0. 80. CF-58-6-85
Oiemlcal technolofv division unit OPeratlOM section
monttdy progress report. September 1958, by
" C. Bresee and others. Oak Ridge National
-aboratory, Oak Ridge, Tenn. Nov 58. Contract
W-740S-eng-26. 3lp. Order from LC. Mi $3. 00,
■in
ph$6.30.
CF -58-9-62
Chemical
Oak Ridge, Tenn Dec 58
26. 47p Order frpm LC
Contract W-7405-eng-
Ml $3 30, ph $7 80
CF-58-10-90
Chemical technotogy division unit operations section
monthly progress report for January 1959. by
R. W. Norton and others Oak Ridge National
Laboratory. Oak Ridge, Tenn Apr 59 72p
Order from LC Mi H- 50. ph $12. 30
CF-59-I-74
i
Chemical technology division, unit operations section
monthly progress report for lanuary 1959. by
C. D. Watson and ojhers. Oak Ridge National
Laboratory, Oak Rldae. Tenn. June 59. 87p.
Order from LC. Mi $4. 80, ph $13. 80.
j CF-59-2-45
8
Chemical technology division , unit operations
stections monthly progress report for March
1959. by M. E WhatTey, and others Oak Ridge
TJatTonaf Laboratory, Oak Ridge Tenn June 59
69p Order from LC Mi $3. 90, ph $10. 80
CF-59-3-61
fects offuel burn-up on the dissolutlai process-I.
by W. Davis, Jr Oak Ridge National Laboratory.
Oak Ridge, Tenn. Mar 59 Contract W-7405-eng-
26. 9p. Order from LC. Mi $1 . 80. ph $1 . 80.
CF-59-3-75
Chemical technc^oyv division unit operatlone sectlai
monthly progress report for May 1959 by R. W.
Horton and others. Oak Ridge National Labora-
tory, Oak Ridge, Tenn Aug 59. 103p. Order
from LC. Mi $5 70, ph $16: 80. CF-59-5-47
Chemical technology division, unit operations section
monthly progress report for June 1959. by M. E.
Whatlev and others Oak Rlojpe National Labora-
tory, Oak Ridge, Tenn Sep 59 64p Order
from LC Vfi $3 90. ph $l6 80 CF-. 59-6-63
Ho
>mogeneouB reactor fuel processing studies, by
W. D. Burch and others Oak Ridge NJational
Laboratory. Oak Ridge. Tenn June 59 Con-
tract W-74as-eng-26 5p Order from LC
Mi $1 . 80. ph $1 . 80 CF -59-6-74
Chemical technology division, unit operatiCTis sec
tion monthly progress report for July 1959. by
R. W. Horton and others Oak Ridgs Natloial
Laboratory, Oak Ridge. Tenn. Oct 59. Il6p
Order fromLC. Ml $6. 00. ph$l8.30
CF-59-7-58
Chemical techndogy division, unit operations section
monthly progress report for August 1959. by J. C.
Bresee and others. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. Dec 59. 95p. Order
fromLC Mi $5. 40, ph$15. 30. CF-59-8-76
Denwnatration of the zirflex proreas on Irradiated
PWR blanket fuel. byT. A. Gens and others Oak
Ridge National Laboratory, Oak Ridre. Tenn
Aug 59 I8p Order fromLC Mi $2. 40.
ph$3.30 CF-59-8-142
A preliminary study of t he dynaniics of solvent ex -
traction cascades. I. Program for dlritalandTnalpg
aitnulation. by O. L. Updike and ME. Whatley
Oak Ridge National Laboratory, Oak Ridge, To
Sep 59 23p
ph$4 80
Order from LC
„ . Tenn
Ml $2 7S,
CF -59-9-47
Chemical technology division, unit operations section
naonthlv progress report for September 1959, by
J. O. Blc«neke and otners Oak Ridge National
Laboratory, Oak Ridge, Tenn. Jan oO I25p.
Order fromLC. Ml $6. 30, ph $19 80.
CF-59-9-69
Chemical techno!
uon montm
igy division, unit operations
oftress report fbr Ucl<»*r 19597
by A. L). R)fa! fcnd «h*rg Utf Kiflgfe NAHOMl
Laboratory. Oak Ridge. Tenn Feb 60 11 Op
Orxter from LC^ M $6. 00. ph $18. 30
CF-59-10-77
i. Oak
nLd
Estimate of potential fuel reprocesalng. revision
no 30. Pitn A. by I. W. Ollmann T)ak Ridge
National Laboratory. Oak Ri
9p Order from LC Mi $1
Tenn Mar 60
0, phSl.SO
CF-60-3-50
jnical technoioftv division, unit operations sectior
naonthlyproprtss report for Noven}ber 1959. by
J. O. Blomelte and others Oak Ridge Nstional
Labo-atory. Otk Ridge, Tenn f 1959] 66p
Order from LC. Mi $3. 90. ph $10. 80
CF-59-11-54
Chemica< technology division, chemicsl deve'opment
section C progress report for February- MarcH
1960. by K. B Brown Oak Ridge National Labor-
atory. Oak Ridge. Tenn Apr 60 45p Order
fromLC Mi $3 30, ph $7 80 CF-60-3-136
HRT-chetnical plant runs 18 and 19 summary, by
O. O. Yarbro Oak Ridge National Laboratory.
Oak Ridge, Tenn. Mar 60. Contract W-740S-
eng-26 22p Order from LC. hfl $2 70,
ph$4.80. CF -60-3-161
Mi$3.3<i, ph$7.80. CF-59-12-49
Chemical technotoyy divlsioo. chemical development
section C progress report for DKrember 1%9 and
lanuary 1960 .by K. B. Brown and othera. Di5
National Laboratory, Oak Ridge. 7
VPP-design crlter
hydrogen flui
an installation to remove
and fluorine from the cells 1
■4
lagT
Mar 60. 48p.
ph $7. 80.
Tenn.
Proposed hydr
I
Laboratory, Oak Ridge. Ten
• Order fromLC. *« fi 30,
CF-60-1-119
and 2_ventllIatlon gases prior to filtration, by
J.B. Ruch. Oak Ridge National Laboratory. Oak
Ridge, Tenn. Apr 60. Contract W-7405-eng-
26. 19p. Order fromLC. N« $2 40, ph )3 30.
CF-60-4-38
Chemical technology division, chemical developmem
. ' - . ., , . Chemical technology division, chemical developmeni
^rogeTj^safetv and disposal prpgedurea section C proc'^ss report Vot April"May I960.
PRFR rfl« plant, by M. tiolmesand by K. B ff^o«^ Oak'ftldgp National Lab^atoiV,
Oak Ridge National Laboratory. Oak C^ pj^ge. Tenn luly 60 49p Order from
Tenn Jan 60 lOp Order froniLC _ _ ic M1^3.30. oh $7.80 CF -60-5- 114
for the PRFlTailot plant, by I
others Oak Ridge National Laboratory. Oak
Ridge. Tenn Jan 60 '
Ml $1.80. ph $11.80
Order from LC
CF-60-1-124
i
llttTlil trf^*nce flowsheets. byL.B. Shappert Oak
Wd^ National Laboratory, Oak Ridae, Tei
Feb 60 3lp Order from LC Mi $3 30.
ph $7 80.
ratory. Oak Ridge, Tenn
- 1 $3 30,
CF-60-2-12
Chemical lechnolQgv divlaion, anit operations aftrtinn
iajia;U£
for February 1 960. by
rs. Oak Ridge National
nynthlypr ogres s r
M. E. Whatley and ot
Laboratory, Osk Ridae. Tenn. May 60. 18p.
Order from Ld. Kfl $4. 80. ph $13. 80.
1 CF-60-2-56
istj^nce m-ogram. Progress report
thyoujtfi December 1959. by E.L7~
id E. M. Shank. Oak Ridge Natlona]
Eurocheniic assist^^nce
for October tfe
Nicholson and E. M. Shank. Oak Ridge National
Laboratory. 0«k Ridge. Tenn. Mar 60. Up.
OrderfromLC. Mi $1. 80. ph $1. 80.
CF-60-2-72
Anpllcatlonif n m«gpA^ium diffusion to the reprocess-
ing o< zircoftiufn- clad fuel elements, by J. I.
Federer Oak Ridge National Laboratory. Oak
Ridge, Tenn Mar 60 28p Order fron LC
Ml « 70, ph $4 80 CF-60-3-21
SwraUgn of .trwjrimwilum lod rirc.gtph.g!cmgntB
by liquid- liquid" extraction, by R D. Baybarz and
R. E. Leuze Oak Ridge National Laboratory,
Oak Ridge. Tesn June 60 Contract W-74(fc-
eng-26 14p Order from LC Mi $2 40.
ph $3. 30. CF -60-3-22
Eurochemlc assistance iwogram: tabulation of Hapo-
blue print file numbers, by E M. Shank Oak
Ridge National Laboratory. Oak Ridge. Tenn
June 60 37p Order from LC Ml $3 00.
ph $6 30 CF -60-6-4
Ertraction of uranium from IMC phosphoric acid
with various dialkylpyrophosphoric acids by
J. E. Magner Dow Chemical Co. Western Dlvl'
slon, Pittsburg, Calif. Sep 57 Contract AT-
30-l-GEN-236^ l6p. Order from LC. Ml $2. 40,
ph $3. 30. DOW- 160
Corrosion of stainless stw-l In HNOy-HF scrfutlons.
by P. M. K!rsnzlein and others. E. I. du Pont
de Nemours & Company. Explosives Department,
Atomic Energy Division, Savannah River Labora-
tory Aiken, S. C. July 60 Contract AT(07-2)-
1. 32p Order from errs 75 cents. DP- 486
Reprocessing of power reactor fuels ^^c"th quarter-
ly progress report for January 1, 1960 to April
1, IWO, by E. S. UccMplntl and others ITT.
du Pont de NenKXirs li Company, Explosives
Department, Atomic Energy Division, Savannah
River Laboratory. Aiken. S.C. Oct 60 Con-
tract AT(07-2)-l 14p Order from OTS
SO cents
DP- 491
idlochemlcal separations plant study Part I
Site con^deradon by ^ I Chri'tl E^
font de Nemours & Company. Explosives I>
ment. Atomic Energy Division, Savahnah River
Laboratory, Aiken. S. C. Aug 60 Contract AT
du
Depart-
236
(07-2)-l. 9p. Order; from OTS.
i
50 cents.
DP- 507
na
of the feasibility of aqueous recovery of spent
__gls Part 6. Partial material balance for sqiie-
ous recovery plant by I. G. Lewis and H. A
Ohlgren University of Michigan Engineering
Research Institute, Ann Arbor, Vflch June 54
Decl April 21, 1960 21p Order from LC
Kt $2 40, ph $3 30 ERI-2240-6-F
ae calculation for the determination of the num-
tranafer unita in countercurrent extracUon
ualf by W. A. Buma Hanford Works,
isnd. Wash Sep 49 Decl Msrch 24, 1960
7p. Order fromLC; Ml $1 80, ph $1 80
HW- 14445
WTpinB-affiry scavenging sttxiles for the deconumlna-
don of redox soiutions. by W. E. Roake and C. S.
Lowe. Hanford Worka. Richland. Waah, May60.
Decl. Mar 60. Contract W-31- 109- Eng-52. ilp.
Order from LC. Mi $2. 70, ph $4. 80.
HW-147a2
garlfjcatlon o< redox dissgiver soluclan by centrlfur.
gatlon with scavenger, by A. W. Allen. Hanford
Works, Richland. Wash. June 50. Decl. March
28, 1960. Contract W- 31 -409- Eng- 52. 25p
Order fromLC. M| $2 70, ph $4 80
j HW-17481
Preparation ajxl propertlea of RAF solutions: low
add TBP flowsheets HW tiumber 4 snd number 5.
bvR.F Maness and M K Harmon Hanford .
Works. Richland. Wash July 50 Decl March
28.1960 Contract W-31 -109- Eng-52 12p
Order from LC ^fi $2 40, ph $3 30
i HW-18407
Purex pulse-column studies with unirradiated u
eloDi
Develcyment of specifications for tl
Pilot idant. by J. G. Bradley Hanfi
s, Richland, Waah Feb 51. Decl.
12p. Order from LC
March
N«$2.40.
HW-20281
Kinetlca of rtutonlum rdJuctlon In the redox IB
coiunm^ by R.L. Moore. Hanford Worka, Rich-
land. Wash. Mar 51. Decl. March 28, 1960.
Contract W-31- l09-cng-52. lOp. Order from
LC. Ml$1.80, ph$ri.80. HW-20580
Plutonium enractl
iter unit reoulre-
~.LenMKi. Han-
AugSl I>cl
March 24, 1960 Contract W-31 -109- Eng-52
Up Order from LC Ml $2 40, ph $3 30
HW-21677(Db1 )
xxaum enractlcy stage and transfer ur
mCIlTTi. ^edoK lA column, by R. B. Len
ford Works. Richland. Waah Aug 51
ytnrir»ry ietnonstradon o< redox feed hesd-eod
treatment: ruthenium votatllizaaon and naanm-
aese dJoxlde acavenelpg, bv H G Hide* simT
ewera Hanford Wor& Richland. Wash lulr
Richland. Wash July
Decl March 28, I960 Contract W-31-109-
52 6lp Order from LC MI $3 60.
9 30 HW- 22076
1
Investigation of explosive characteristics of twrea
solvent decomposition products (red oil), by R M
. Wagner General Electric Co Hanford Atomic
Products Operation, Richland. Waah Mar 53
Decl May 3. 1960 Contract W-31 -109-eng-52
8p Order fromLC NA $1 80, ph $1 80
HW-27492
Pll«-Dlant studiea dt mercurv-catalvzed <lasotvlng
of aluminum- jacketed fuel elements, by J. L.
Bradford and K. L. Adler. General Electric Co.
Hanford Atomic Producta Operation, Richland,
Waah. July 54 Decl. March 28, 1960. 22p
Order from LC. Ml $2 70, ph $4 80
HW-32316
"Mt? «"r ■*"^<nii rf mrrnirrrarfflyTyil ftHmnlYlny
of aluminum- lacketed fuel elenaents. J. L. Brad-
ford and K. L. /fcuer General Electric Co ,
Hanford Atomic Producta Operation, Richland.
Wash July 54 Decl March 28. 1960 22p
Order from LC Ml $2 70. ph $4 80
HW-323l6(Del )
Proposed alternate dlasolvlng flowsheets for the
redox rt*nt. by M H Curtis and M K Harmon
General filectrlc Co , Hanford Atomic Products
Operation, Richland. Wash Aug 54 Decl April
21, 1960 Contrsct W-31 -109- Eng-52 Up
Order from LC Kfl $1 80, ph $1 80
HW-32823
Duel functjon system for ganama radladon monitoring
In a extraction proems pllqt jalsnt. by M. B Le-
boeuf and othera. General Electric Co Hanfbrd
Atomic Producta Operation. Richland, Waah
Noy. 54. Decl with deledona February 5. 1960. *
Contract W-31 -109-Eng-52. 37p. Order from
LC. Ml $3. 00. ph $6730. HW-33901(nel. )
Operating lives of redone mechanical eoulomwit. by
R. L. Stevenson. Genersl Electric Co Riuiford
Atomic Products Operstion, Richland, Waah
Apr 55 Decl March 28, 1960 1^ Order
from LC Ml $2 40. ph $3 30 HW-37i21
A new approach to concatgiatlon qfpulsed
by J Otiver Ludlow General Electric
gplunwt,
TKi-
fbrd Atomic Products Operatian. Richland. Wash
Aug 55 Decl March 28, 1960 7p Order
from LC NA $1 80. ph $1 80 HW-38667
Aff mlYlii <* the in-line uranium photometer data
from purge hot semi -worka. runa px-2 throuim
PX-9. bvF A Scott General Electric Co , Han-
ford Atomic Producta Operation. Richland, Wash
DbcSS Decl March 28, 1960 21p Order
from LC Ml $2 70i ph $4 80
-40313
Hapo interest, by R. H. Moore. General Electric
Co. , Hamord Atomic Products Operstion. Ridr
lancC Wash Feb 57. Decl. March 28, 1960.
Coatract W-31-109-Enr-S2. 21p. Order from
LC. Ml $2. 70l ph $4/10. HW-48S08
Graded plate cartridge for purex a-type extractloo
column, by R. G. Geier and G. M. Heason"
General Electric Co. Hanford Atomic Products
Operation, flichlaivl. Waah. May 57. E)ecl.
June 10. 196<>. 9p. Order from LC. Mi $1.80,
ph$1.80. 1 HW-49149
5rd
Technology of npo-production reactor fuela reproc-
esaingybudyt activity 2790. Quarterly rCTortT
by V. R. CtSper. General Electric Co. Hanfoi
Atomic ProdvctB Operation, Richland, Wash.
June 58. Decl. March 28. 1960. Ccotract W-31-
109-Eng-52.I 7p. Order from LC. Mi $1.80,
pii$1.80. i HW-56477
Precipitation m<ttKxl for the recovery of plutooium
from chloridb a lag and crucible -progress r^ort,
byR^W. HeokensT General Electric Co. Han-
ford Atomic products Operation, Richland, Wash.
Oct 58. Deal. March 31, 1960. Contract W-
31-109-Eng-52. 8p. Order from LC.
Mi $1.80, pll$1.80. HW-S8021
Parameters
of oil
is solver
nt design poorer
eouipment design
W.A. Graf. Gen
fuel reproce»8ing. byW.A. Graf. General Elec-
tric Co. Ha tford Atomic Products Operation,
Richland. W$sh. May 59. Contract W- 31 -109-
Eng-52. 8p. Order from LC. Mi $1.80.
ph$1.80.
HW -60436
The effect of solution and vessel tfaennsl exmnsion
on volume measurements in the chemica
easing deparfanent, by W
if proc
proc-
General
_ epartment, by w. H. Johnson.
Electtic Co. ' Hanford Atnnic Products Operation,
RichUnd, Wish. May 59. Contraa W-31-109•
Eng-52. 8p. Order from LC. Mi $1.80.
ph$1.80. 1 HW-60455
The zirflex process; interim developntent sumnaary,
By A, M. Piatt and C. R. Cooley . General
Electric Co. Hanford Atomic Products Operation,
Richland. WMh. June 59. Contract AT(45-1)-
1350. 31p. Order from LC. Mi $2.70,
ph$4.80. HW-60597
Technology of non -production reactor fuels reproc-
essWpuket activity 2790, by V. R. Cooper.
General Eledtrlc Co. Hanford Atomic Products
Operation, Richland, Wash. July 59. Decl.
August 5, 1959. 20p. Order from LC.
Ml $2. 70. pl|$4.80. HW- 60928
Project CGC-83p. plant modifications for reprocess
Lag non-pro<!^caoo reactor f»«Ia- P^*^g°5't'f'^
for builaing J13-U caak transfer facility, by M.
E. Yatea. GJeneral Electric Co. Hanford Atomic
Products Oporadon. Richland, Wash. July 59.
9p. OrderfromLC. Ml $1.8a ph$1.80.
HW-61076
Analysis of a nuclear incident in a redox diasolver.
by V. I. Neeley. General Electric Co. Hanford
Atomic Products Operation, Richland, Wash.
Aug 59. Contract AT(45- 1)- 1350. 17p. Order
from LC. Mi $2. 40, ph $3. 30. HW-61609
Quarterly report on technology of non -production
reactor fuels reprocesaing budget acitivlty 2790,
by V . R . Cooper' GeneralElectrlc Co. Hanford
Atomic Products Operation, Richland, Wash.
Sep 59. Decl. December 2, 1959. Contract
AT(45-1)-1350. 1^. Order from LC. Mi $2. 4a
ph $3. 30. < HW-62063
idpowcrreactor
rofluorlc ac
Dissolutloo of stainless steel clad
fuels with nitric acid and hydrofluoric add, by
C.R. Cooley. General Electric Co. Hanford
Atomic Products Operation. Richland. Wash.
Oct 59. Contract AT(45-1)- 1350. 18p. Order
fromLC. Mi $2.40. ph $3.30. HW-62199
Darex pilot plant studies, by J. J. Shefcik
Electric Co
— _^ General
Hanford Atomic Products Operatioo,
Richland, Wash. Oct 59. Contract AT(45-1)-
1350. 20p. OrderfromLC. Mi $2.40,
ph$3.30. MW-62537
by L. C. Amos. Dec 59.
Non-production fuels reprocessing, centrlfugation
studies on various dissolver effluent solutions,
Apptaidix A:
K. Harmon
TSIy^.
clariflcaticin studies, by M
Appendix B: Nonproduction fuel clarification
BWdJCB, by R. B. Bums. General Electric Co.
Hanford Atcxnic Products Operation. Richland,
Waah. Sep 59. Contract AT(45-1)- 1 350. lOp.
OrderfromLC. Mi $1.80, ph $1.80.
HW- 62840
Low apeed saw testing, by V. L. Hanunond and
V.P. Kelly. Hanford Atomic Products Operation.
Richland. Wastv June 60. Contract AT(4S-1)-
1350. 40p. Order from OtS. $1.25.
HW- 62843
Zirflex diasolutloo of the annular cladding of slmuU-
tedpower fuel elements, by P. W. Sn^th. Gener-
al electric Co. Hanford Atomic Producta Opera-
tion, Richland, Wash. Dec 59. Contract AT
(45-l)-1350. 5p. OrderfromLC. Mi$1.8a
4 ph$1.80. HW-63043
Development and testing of an improved agitator ftar
gg redox and purex separations pUntsr by J,
Dunn and R. J. Sloat. General Electric Co.
Hanford Atomic Producu Operation, Richland,
Wash. Dec 59. Contrsct AT(45-1)-1350. 6p.
OrderfromLC. Mi $1.80, ph $1.80.
HW-63175
238
i
0^»rterly report on technology of non-production
reactor fuels reprocessing budget activity 2790,
by V. k. Cooper. General Electric Co. Han-
ford Atomic Producta Operation, Richland, Wash.
Jan 60. Contract AT(45-1)-1350. 17p. Order
trOBiUC. Mi $2. 40, ph $3. 30. HW-63406
' t
Laboratory sttidies on the filtration of MTR dissol-
ver solutions. CP^ Start up rejport no. 34, by
G. K. Cederberg. American Cyanamid Co.
Atomic Energy Division, Idaho Falls, Idaho.
Feb 53. Decl. March 28, 1960. Contract AT
(10-1)-177. 26p. Order frcMn LC. Mi $2.70,
pta$4.80. i IDO- 14223
Mercury in the "25" process, by A. E. Erhard and
R. H. Perkins. American Cyanamid Co. At(»nic
Energy Division, Idaho Falls, Idaho. May 53.
Decl. March 28, 1960. Contract AT(10-1)-177.
13p. Order from LC. Mi $2. 40, ph $3. 30.
IDO- 14242
Auwmatic slug charge^- design proposal, by H. •
Schneider. Phillips Petroleum Co. Xtomic
Energy Division, Idaho Falls, Idaho. June 54.
Decl. March 28, 1^60. Contract AT(10-1)- 205.
lip. Order from L(C. Mi $2. 40, ph $3. 30.
IDO- 14377
ess
Idaho chemical processing plant technical prcy(
report for April thrpupi June 1957, by C. 5.
Stevenson. Phillips Petroleum Co. Atomic
Energy Dlvisioh, Idaho Falls, Idaho. Sep 57.
Decl. May 4, 1960, Contract AT(10-l)-205.
7^. Order from LC. Mi $4. 50, ph $12. 30.
IDO-14419
^
m
Idaho chemical
uly througfa&pti
Stevenson, mil lips Petroleum Co
rocesslng plant technical progress
through September 1957, by C.E.
I Pet
report forj _^
Xtixnlc En
ergy Division, Idahd Falls, Idaho. Dec 57.
Decl. May 4, 1960. Contract AT(10-1)- 205.
148p. Order from DC. Mi $7.20. ph $22.80.
i IDO-14422
Performance of the TBP process for aluminimn fuels;
' IdalK? cJiemical proQesslng plant, 1955-1956, by
t.. L. Rohde. Phillips Petroleum Co. Atomic
Energy Division, Idaho Falls, Idaho. Jan 58.
Decl. May 12. I960; Contract AT(10-1)- 205.
53p. Order from LC. Mi $3. 60, ph $9. 30.
IDO- 14427
' i
Neptunium separation tcftm uranium, plutonium.
and fission products: an annouted bibliography,
by B. J. Newby. Riillipe Petroleum Co. Atomic
Energy Division. Idaho Falls. Idaho. Dec 58.
Decl. June 9. 1959. Contract AT(10-1)-205.
2^. Order from LC. Mi $2.70, ph $4.80.
IDO- 14459
Barium fluozirconate precipitation from hydrofluor-
ic acid-zirconium fuel reprocessing solutions.
Part I. Process cfaemistiV, by B. E. Paige.
Phillips Petroleum Company, Atomic Energy
Division, Idaho Falls. Idaho. Sep 60. Contract
AT(10-l)-205. 37p. Order from OTS. 75 cents.
IDO- 14511
Corrosion in neutralized radioactive waste, by N.
D. Stolica and G. S. Adams! Phillips Petroleum
Company, Atomic Energy Division, Idaho Falls,
Idaho. Sep 60. Contract AT(10-l)-205. 15p.
Order from OTS, 50 cents. IDO-14531
An investigation of the KMn04-Mn02 head-end pro-
cedure for the removal of rutfaeniumand niobium
in. A large-scale study with non-
-ge
the
zirconium.
irradiated uranium in the separations pilot plant,
by J. F. LaBoote and E. F. Palmer. Knolls
Atomic Power Laboratory, Schenectady, N. Y.
Mar 53. Decl. April 21, 1960. Contract W-31-
109-Eng-52. 35p. OrderfromLC. Ml $3. 00,
ph$6.30. KAPL-795(Pi. lU)
A low waste volume, first cycle, 1 A purex flow
sheet, by J. K. Davidson and W. O. Haas, Jr.
Knolls Atranic Power Laboratory, Schenecudy,
N. Y. July 56. ttecl. May 18, 1960. Conti-act
W-31-109-Eng-52. 71p. Order from LC.
Mi $3.90, ph $10.80. KAPL-1543
An index and summary of chemical work on the
redox assistance to Hanford program. Volume
II. Part m. Redox pilot plant (fevelopiraent
studies, by W. S. Andrus and others. Knolls
Atomic Power Laboratory, Schenectady, N. Y.
Apr 53. Decl. May 4. 1960, Contract W- 31-
I09-Eng-52. 88p. OrderfromLC. Ml $4.80,
ph $13.80. KAPL-M-FCS-1 (Vol. II)
Interim report on operation of the TVP hexane ex-
traction pilot plant, by L. H. Krone and othera
Mallinckrodt Chemical Works, St. Louis, Mo.
May 56. Decl. May 4. 1960. 22p. Order from
LC. Mi $2.70. ph $4.80. MCW-1390
Separations chemistry progress report for the
period October, Novemper and December 1952.
by E. Mocu and M. Yar^Iey. North American
Aviation. Inc. . Downey. Calif. Jan 53. Decl.
May 3. 1960. Contract AT-U-l -GEN -8. 59p.
OrJer from LC. >li $3. 60, ph $9. 30.
NAA-SR-220
Technical report on the expanded Harshaw TBP e«-
gaction process, by D. A. Hammond. Harshsw
Chemical Co. , Cleveland, Ohio, Apr 54. Decl.
March 15, 1960. Conti-act W-7405-ENG-276.
99p. OrderfromLC. Mi $5.40, ph $15.30.
NYO-1468
239
A cost inalysla of tbe Idaho chemlatl jgocesaing
pljuit. by P. L. Robertaon and W. G. Stodufale.
Oak Ridge Nadooal Laboratory, Oak Ridge, Tenn.
Jan S5. Decl. Juoe S. 1959. I60p. Order from
LC. Mi 17.^ ph $24. 30. ORNL-1792
Zirflez
Reviaed
rflex proce»B| for PWR blanket fuel. II. Reyii
flowA^t. by L. M. Perrla and J. F. Land.
Oak Ridge National LaJSoratory, Oak Ridge, Teno.
[nd]. Contract W-740S-eiig- 26. 2^. Order
fromOTS. 50 centa. ORNL-2940
lihrlum extraction characterieatlca of alkyl
amiaea and ijuclear metala in nitrate ayatema.
no. 6 for the
Quarterly prbgreaa report no.
dctofaer I -bomber C 1959.
Hod
Quarterly report
VI byE.A. 'MaaooaadV. C. Vaighen. MaT^
aachuaetts Institute at Technology, Cambridge,
Maaa. Feb (0. Contract W-7405-eag- 26. 29p.
Order from (jC- Mi (2.70. ph $4.80.
'nD-5720
F.Minination ol itaniima 'tMni coll from a purex
evaporator by F. W. FtA.
loadtuie, Xolumbus, Ohio.
Battelle Memorial
Mar 60. 8p. Order
fromLC. Mi $1.80. ph $1.80. TID-S724
Controlled Thermonuclaor Processes
Quarterly Btatu4 rqxnrt o< die laal controlled
thermonuclear reaearcfa pnyam for period end-
ing August 2d I960, by S. Glaaatooe. The Uni-
versity <rf California, Loa Alamoa Scientific
Laboratory, Los Alamos, N. Mez. Sep 60.
Contraa W-7405-BNG-36. 40p. Order from
OTS. $1.00., LAMS-2464
Pynaxnic aheatii^in an axial iMgnetic field, by F. L.
Ribe. The ubiveraity of CaUfomla. Loa AUmoa
Scientific Lakiratory, Los Alanaos. N. Mez.
Jan 60. Contract W-7405-ENG-36. lOp. Order
from OTS. 3D centa. LAMS-2471
The efiect erf nxlation on the atabilized irincfa, by A.
Pytte. Project Matterfaom, I^inceton Onlveraity,
Princeton. N.J. June 60. Contract AT(30-1>-
1238. 7p. G^der from OTS. 50 centa.
MATT-44
TUtlai confining fiekl coils tor the C stellennor, by
U. Chriaienafn . Project Matterhom. Princeton
University, EVlnceun. N. J. July 60. Contract
AT(30-1)-1238. 25p. Order from OTS.
75 centa. MATr-46
ing die period April 1 to
I, by L. Goldberg
Quarterly report coveri „ .
June &, 1960, by L. floldberg and otfiers.
Project Matterbom, Princeton University,
Princeton Univeraity, Princeton, N. J. July 60.
Contract AT(30-1)-1238. 32p. Order from OTS
$1.00. MATT-Q-ll'
P-4, A Bteady-sme plasma system, by A. L. Gard-
ner and ooiera. Univeraity ol California. Law-
rence Radiation Laboratory, Livermbre, Calif.
May 60. Contract W-7405-eng-48. 41p. Order
from OTS. $1.00. UCRL-S904
Probe measurements on the P-4 syatem in single
caftode operadon. Thesis, by D. M. Gall
University of California. Lawrence Radiation
Laboratory, Livermore, Calif. May 60. Con-
tract W-7405-eng-48. 27p. Order from OTS.
75 centa. UCRL-S996
The effects of apace charge and relativity on the
ahapea of chargrf-pardcle beania, by N. W.
Hetherington and C. H. Woods. University of
California. Lawrence Radiadon Laboratory,
Uvennore, Calif. Aug 60. Contract W-7405-
eng-48. 20p. Order from OTS. SO centa.
UCRL-6010
Some aapecta of the economics of fusion reactors,
by R, F. Poet. Univeraity of California. Gir-
rence Radiation Laboratory, Livermore, Calif.
Aug 60. Contract W-7405-eng-48. 62p. Order
from OTS. $1.50. UCRL-6077
Fast neutral particle injection into a mirror ma -
chine, by R. F. Poat. University of California.
Lawrence Radiadon Laboratory, Livermore,
Calif. Aug 60. Contract W-7405-eng-48. 27p.
Order from OTS. 75 cents. UCRL-6078
Velocity- space instabilides in the mirror machine,
by R. F. Post. University of California. Law-
renoe Radiation Laboratory, Livermore, Calif.
Aug 60. Contract W-7405-eng-48. 26p. Order
from OTS. 50 centa. UCRL-6079
Hydromamedc atability diagrams for a linear pincfa,
D. Z. FreedmaiT University of California,
Lawrence Radiadon Laboratory, Livermore,
Calif. Aug 60. Contract W-7405-eng-48. 20p.
Order from OTS. 50 centa. UCRL-6064
Controlled thermonuclear research quarterly re
t. March. April May I960, by C. M. Van"
tu and odiera. University of California. Law-
rence Radiadon Laboratory, Berkeley, Calif.
June 60. Contract W-7405-eng-48. 136p. Order
from OTS. $2.50. UCRL-9243
240
Cnticality Studies
CoBMisriBon of kpo meaaurementa in a critical as- '
aerobly with kpo meaaurements in die physical
conatanta testiqg reactor, by J. T. Mihalczo.
Oak Kidge National LaEoracory, Oak Ridge,
Tenn. May 60. Contpract W-7405-eng-26. 3^.
Order fromLC. Mi $3. 00, ph $6. 30.
CF-60-4-24
I
A propoaal for cridcality control meaaurements
uaing pulsed neutron metfaode, by E. G. Silver.
OakRldge Nadonal Laboratory, Oak Ridge,
Tenn. May 60. Contract W-7405-eng-26. 8p.
Order from LC Ml $1.80. ph $1.80.
i CF-60-5-130
i
Program for computing minimum critical sphere
radii for urai^um aalta, by T. B. Patteraon.
Goodyear Atomic Corporation, I\3rt8mouth.
Ohio. Nov 59. 5p. Order from LC. Mi ^.80,
I«i$1.80. I GAT-DM-792
Nuclear aafiety apedflcatfons for fuel element manu-
tacoiring mrooeea<agi General Electric Co. Han-
lord Atonuc Products Operation, Richland. Wash.
Oct 55. DecL April 28, 1960. Contract W-31-
109-Eng-52. 19p. Order from LC Ml $2.40,
lrii$3.30. 1 HW-37952
Neutron aoe calculationa
I
(IxiOKMeneous systems),
iral Efectric Co. Haitfo
by N. ^tzlacfa. General Electric Co. Hanford
Atomic Producta Operation, Richland. Wi sh.
July 59. Contract AT(45-1)-1350. 6p. Order
fromLC. Mi $1.80. ph $1.80. HW-61054
Plutonium oxide -plaadc mlxturea for critloil maaa
atudiea, by H. W. Crocker. General Electric
Co. Hanford Atomic Products Operation, Rich-
laod. Waah. May 60. Contract AT(45-1)- 1350.
ISp. Order fromLC. Mi $2. 40. ph $3. 30.
HW-65207
Nuclaarly aafe masa limits
-nat
General Electric Co. Hanferd Atomic
larly aate masa limits. Volume limita, infinite
Under diametera aiK^ alab tfalcknei
Bmpiriail atudtea of critiCTl mass data. Part IIL
byC. L. Schuske andJ.W. Morfia. Carbide and
Carbon t3iemicals Co. Y-12 Plant. Oak Ridge,
■ Tenn. Jan 52. Decl. March 7, 1960. Contract
W-7405-eng-26. 13 p. Order trcMn LC.
Ml $2.40. ph$3.30. Y-83»
jBTlched uranium rode In
Clayton.
a for alig^y
water, byB.D.
Producta Operation. Richland. Waah. May 60.
CaBCraaAT(45-l)-13S0. ISp. Order from LC.
Mi $2. 40. ph$3.30. j HW-65328
Nuclear aafety e
ad urantinn
nta on plutonltmi and enrlcfa-
irogen moderated aseembliea con-
by G. H. Bidinger and odiera.
experimei
The Dow^2anicala Company, Rocky Plats, Den-
ver. Colo. Oct 60. Contract ATX2 9- 1)1 106.
14p. (teder from OTS.; SO centa. RFP-201
prop
,ty informi
Schuske.
CarlRde and Car -
^jplJCTtion of cridcallty information to Y-12 Plant
blems, by C. I
Chemicals Co. Y- 12 Plant. Oak Ridge. Tenn.
Mar 52. Decl. March 2, 1960. Contract W-
7405-eng-26. 37p. Order from LC. Mi $3.00.
ph$(>.30. Y-»S3
Critical maseeaa and lattice paramecere of H^O —
UO2 critical eaqieriments. A comparison of
dieory and ejqieriment. by W. H. Arnold, Jr.
Westughouse E lectric Corporation, Atomic
Power Department, Pittsburgh, Pa. Nov 59.
Contract AT(30-3)-222. 47p. Order from LC.
Mi $3. 30. ph$7.80. YAEC-152
Equipment, Methods and Techniques
Cyclic preaaure tests of large size pressure vessels,
Progreaa report no. 16 for January 16, 1960 Co
February 15, 1960, by M. M. Lemcoe. South-
west Research Institute, San Antonio, Tex.
[I960]. Contract AT(30-1)-2140. 18p. Order
fromLC. Mi $2. 40. ph $3. 30. AECU-4730
Remote ahearing, by A. A. Afabatiello. Oak Ridge
Nadonal LaEoracory. Oak Ridge, Tenn. Nov 58.
1^. Order fromLC. Mi $2.40. ph$3.30.
CF-58-11-S7
Notea on heat tranrfer in the ORR care at powers
greater than y Mw. by J. P. Wett, Jr.- Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Sep 59. 12p. Order fromLC. Mi $2.40.
ph$3.30. CF-59-9-68
irtjto. 1 on vacuum ayatema, by
E. Normaa^. Oak Ridge National Laboratory
Oak Ridge, Ttsnn. Jan 60. 22p. Order from
LC. Mi $2.70. ph$4.80. CF-60-1-17
May 60. 1^.
ph $3. 30.
Order from LC.
T^nn.
Mi $2.40.
CF-60- 3-103
T>»at of HRT CP muldckae no. 1 toUami
ring re
from rtyctor cell, by O. O. Yarinro. OmE
National Laboratory, Oak Rldgs. Teon.
removal
10^
241
]uDe60. Cdtract W-7405-eng-26. lOp.
Order from [jjC. Mi $2. 40, ph $3. 30.
Cy-60-6-l05
Hydraulic Instaiiility in a natural circulation loop
with net steato generatioo at 1000 peia. by S.
Levy and B. S. Beckjord. General Electric Co.
Atomic Powet BquinxKnt Department, San Joee,
Calif, July5!J. Contract AT(04- 3)- 189. 47?.
Order from UC. Mi (3. 30. ph $7.80.
GBAP-3215
Deaign coosideriitiopB and region of operatioo al
tte jet diffualop equipmenC by J. W. Eerkena.
University a(^ California. Institute of Engineer-
ing Researd^ Berkeley, Calif. July 57. Cdn-
tract AT(ll-l)-34. 20p. Order from LC.
Mi $2.40. I%$3.30. HE-150-15B
Some Btudies on ultrasonic testin;
by R. L. Mancuae
with lamb waves,
General Electric Co. Han~
ford Atomic t>roductB Operation. Richland, Waah.
Feb 57. Decl. March 31, 1960. Up. Order
fnxnLC Mi $2. 40. ph $3. 30. HW-48754
T
I
Deepwell turbine .
duroctle bushin;
neral Electric Co.
teak-
age, by]- I>taP- fteneral Electric Co. flanfbrd
Atomic Products. Operation, Richland, Wash.
Dec 57. DeCl. March 28. 1960. 12p. Order
fromLC. K^ $2. 40. ph $3. 30. HW-53530
Interim report- - PT- 63 sea teformatioo in heat ei-
ohaM^ra ufliog raw Colinmbia River water, by
W. D. Bainara. General Electric Co. Hanford
Atomic Protiiicts Operation, Richland. Waah.
June 58. Cottract AT(45-1)-1350. 31p. Order
frtxn LC. Mi $3. 00, ph $6. 30. HW-56537
pments if the HLO bearing test program;
rim report, by R. W. Wirta. General Elec-
Co. Haaford AtonUc Products Operadon.
Development
interim
trie Co. llaaford AtonUc Products Operadon.
Richland, Wash. Jan 59. Contract AT(4S-1)-
1350. ?5p. Order fromLC. Mi $2.70,
pll$4:S0. 1 HW-58639
TbenxMil contact conductance of fuel element mate-
riala, by R. G. Wheeler. General Electric Co.
HaSord Atomic Products Operation, Richland,
Waah. Apr $9. Contract AT(45- 1)1 350. I6p.
Order from tC. Mi $2. 40. ph $3. 30.
HW-60343
Computational ajda for eatimating performance of
liquid to boilibg water heat exctiiMiera, by WT^.
Love. General Electric Co. Hanford Atomic
Products Operacioa, Richland, Waah. Sep 59.
17p. Order ftram LC. Mi $2. 40, ph $3. 30.
HW-61738
Statiatical analysis- -accuracy of volume measure-
ments in a large proceas vessel, by C. G. Hourt.
General Electric Co. Hanford Atomic Products
Operation, Richland, Wash. Oct 59. Cootraa
AT(45-1)-1350. 36p. Order from LC.
Mi $3.00, ph $6. 30. HW-62177
Gaa shiefcted Arc welding process, by J. Maginnia.
Union Carbide Nuclear Company, Division of
Union Carbide Corporation, Oak Ridge Gaseous
Diffusion Plant. Oak Ridge, Tenn. Sep 60. Coo-
tract W-7405-eng-26. 9p. Order from OTS.
50 cents. K-1456
ttive performance of four main coolant
"valves during closure, by T. H. Glasser
and others^ Knolla Atomic Power Laboratory,
Schenectady. N. Y. Dec 59. 35p. Order from
LC. Mi $3.00. ph $6.30. KAPL-M-SMS-104
Snap-Ill — Thermoelectric generator enviroomenttl
oest. Volumie III, by l" W. Groes and E. J.
ScfaramnT Martin. Co. Nuclear Division,
Baltimore, Md. Jan 60. Contract AT(30-3)-217.
73p. Order fromLC. Mi $3.90. ph $10.80.
MND-P-2101-ni
Bvaluadoa of prrfabricated pipe Insuladoo- heater
sectjons, 1^ C ). Baroczy. Atomics Intematioa-
aT Division of North American Aviation. Inc. ,
Canoga Park, Calif. July 58. 12p. Order from
LC. Mi $2.40. ph$3.30. NAA-SR-Menx>-2898
E3q;>erlinental evaluation of conoenoric cylinder,
spiral -flow heat ejcfaanger, by J. S. McDonakl.
Atomics International. Dlvlaion of North Ameri-
can Aviation. Inc. . Canoga Park. Calif. Mar 59.
Sip. Order from LC. Mi $3.00. ph $6.30.
NAA-SR-Memo-3528
Design of 3400gpm 40 psi linear induction pump for
tf» 250 MWBoverflow r«*ctoir. by R. S. BakeiFr
Atomics IntematioDal. Diviaion of North Ameri-
can Avlsdoo. Inc. . Canosa Park. Calif. July 59.
1^. Order from LC. Ml $2.40. ph $3. 30.
NAA-SR-Memo-4413 (Rev. 1)
Burnout protectioii retirements and |>rellmlBary
burnout protection aystem design, py R. P.
Audette. Atomics International. Diviaion of
North American Aviation. Inc. , Canop Park,
Gallf. Oct 59. 13p. Order from LC. Mi$2.4a
ph $3. 30. NAA-SR-Memo-4469
ThCTmal conductivity of soap materials, by R. A.
Barney. Atomics Intematioual. Division of
Ikmh American Aviation. Inc. , Canoga Park,
Calif. Oct 59. 15p. Order from LC. Mi $2.40^
ph $3. 30. NAA-SR-Memo-4Sai
Ejmerlmental systems and procedures utilized in
^studying the phenomena of nucleate boiUng and
burnout by D. A. Hubejr. Atomica International
Division of North American Aviation, Inc. ,
Canoga Park, C^if. Oct 59. Up. Order from
LC. Ml $2.40. ph$3.3p. NAA-SR-Memo-4553
Teats of an -type tube ooupwigfi, by C. Sutherland.
Atomics Inumational. Diviaion of North Ameri-
can AvUtion. Inc. . Canoga Park. Calif. Dec 59.
8p. Order fromLC. Mi $1.80, ph$1.80.
. NAA-SR-Memo-4772
Test of prototype HNPF large valve remote cyerator.
by W. F. Marten. Atomica International. Divi-
alon of North American Aviation, Inc. . Canoga
Park. Calif. May 60. 13p. Order from LC.
Mi $2. 40. ph$3.3Q NAA-SR-Memo-S250
Study of the industrial potential of radioi
' ' ' le i«' "
jisotopic
irterly t
metJKXls in the textile indueory. Quarterly prog-
reas report for the period October 1. 1959-
December 31, 1959, by L Rebenfeld and H. ].
White, Jr. Textile Research Institute, Prince-
ton, N. J. Contract AT(30-l)-2365. 27p. Order
fromLC. Mi $2.70. ph $4.80. NYO-2639
Flow equauona for a
■Tp.
York University,
*nlca!
irogress
conducting
report, by B.
ionic liwid, Ttech-
R. Sunmelm. New
Y. Jan 60. Contract AT
(30-l)-1938. 32p. Order fromLC. Mi $3. 00.
ph $6. 30. NYO-7744
Slurry feed-pump development, by B. C. Hise.
Otk Ridge National Laboratory, Oak Ridge,
Tenn. [nd. ]. Contract W-7405-eng-26. 21p.
Order from OTS. SO ce^ita. ORNL-3008
RacMometric flaw detector, by W. T. Gannon.
General Electric Co. General Engineering Lab-
oratory. Schenecudy. N. Y. June 53. Decl.
November 20, 1959. 2^. Order from LC.
Mi $2.70, Fh$4.80. R53GL132
Fluah printed circuit boards for timijag switchM fof
military applications, by R. E. WMtford. Sandia
Corporation ReprlnC Albuquerque. N. Mex.
Oa60. 18p. Order from OlS. 75 centa.
SCR-227
Molded rubberized hair shock mitigating and oish-
ioning pada. by W. W. Chapin. Sandia Corpora-
don. Albuquerque. N. Mex. Jan 60. lOp. Order
fromLC. Ml $1.80. ph $1.80. SCTM-9-60(25)
A drop-testing device used tor small-scale, dynam
itingdevl
Ic," curtiiomng experlmenta In Sandia
tion'a "Component recovery program
I
I
Corpora-
". fcyW.J.
Halpin. Sandia Corporation. Albuquerque,
N, Mex. Mar 57. Contract AT(29-l)-789. 31p.
Order from LC. Ml $3. 00. ph $6. 30.
^ SCIM-49-57-14
High-vacuum techniques, G. L. Krieger. Sandia
Corporation, Albuquerque, N. Mex. Mar 60.
2Sp. Order fromLC. Mi $2.70. ph $4.80.
SCTM-76-60(14)
^
velocity shock testing, equipment and naethods,
W. W. Walker. Sandia Corporation, ADxi-
querque, N. Mex. July 60. 3^. Order from
OTS. $1.00. SCIM-196-60-16.
Use of an air dead-weight tester for the precise
control of constant ^s pressure in closed sys-
tenas, by M. K. Laufer. Sandia Corporation,
Albuquerque, N. Mex. Dec 59. 6p. Order
fromLC. Ml $1.80. ph $1.80.
SCTM-339-59(27)
Tranamission of short duration acceleration pulses,
by M. L. Walker and P. M. Barba. Sandia
Corporation, Albuquerque. N. Mex. Dec 1959.
22p. Order fromLC. Ml $2. 70. ph $4. 80.
SCTM-361-59(14)
Screw thightness, by G. W. Chandler. Sandia
Corporation. Albuquerque. N. Mex. Dec 59.
6p. Order fromLC. Mi $1.80. ph $1.80.
I SCnyI-409-59-25
Resistance temperature detector lead cable -100-K
area, by R. L. Loundagin. General Electric
Co. Hanford Atomic Products Operation. Rich-
land, Wash. Dec 57. 6p. Order from LC.
Mi $1.80, ph$1.80. TID-5621
Hydrostatic pressure drop in two phase flow, by
J. H. Vohr. Columbia University, Engineering
Research Laboratories, New York, N. Y. Dec
59. 7p. Order fromLC. Mi $1.80, ph $1.80.
TID-5673
High energy storage ceramic capadtcy.
reportno, lOfor April 1, 1959-Iune30,
>rterlv
reportno. lU tor April i, lV5V-Jurie30, 1^59, by J.
M. Blank. General Electric Co. Missile and Space
Vehicle Department, Philadelphia, Pa. [1959].
Contract AT(30-1)-1963. 66p. Order from LC.
Mi $3. 90, ph $10.80. TID-5696
243
Perturbation analysis of the stability of self-acting.
gaa-l\ibricated journal bearings. Interim report.
ByV. Castelli and H. C. ElrS. Jr. Pranklfii .
Institute. Laboratories for Research and Develop-
ment, ntiladelphia. Pa. Feb 60. Contract Noor-
2342(00). 31p. Order from LC. Mi $2.70.
ph$4.80. TII>-S704
The dealgn (rf Urge cj jfugiilc ™*gpet coUa, P»per
no. ^ by <X 6. Taytor and K. F. Boat. Univer-
aity of California. Lawrence Radiatlan Labora
tory, Llvernx)re. Calif. (Oct 59j. Ooacract W-
7405-en«-48f iSp. Order from LC. Ml $2. 4a
pii(3.30. UCRL-S631-T
trradiatiop te«» at Mark I Pglae InatnimeMa. by
0. F. SwiAhad oifaera. Weatingtimiar Electric
Cocp. . Atomic Power DiTlalon. Plttaburgb. Pa.
JulyS2. Decl. March 2. 1960. Contract AT-
ll-l-GEN-14. 12p. Onfer from LX:. Ml $2. 4a
ft $3. 30. WAFD-RM-137
Slmularlon at a tetream generator, by W. L. Camkon
and L. L. Iloth. WCTringho<inr Biectrlc Corpor-
ation, Bettla Plant, Plttaburgh. Pn. Aug 56.
6lp. Order from LC. Ml $3. 9a ph $10. 80.
WAFD-S3W-A-1865
I
on final hlfl
hi A heat flu» taaf •£ 2000 KIA op
parallel flk>w I roda. by A. Weiaa. Weadnghouee
Biectrlc Gor]xiratlan. Attmic Power Dlvlalan.
Plttahurgh. Ik. Feb 59. 8p.
Ml (1.80. pti$1.80.
Order from LC.
WAPD-TH-478
Bvahmdop of dtacondnultiea in a aT"«nl«'T# ateel
weldment wlm radiographic and ultraaonic tech-
nlquea, by F^ J. Lambert and P. J. Long. Un-~
ion Carbide Nuclear Company, DiylaioB at Union
Carbide Corporatian. Y-12 Plant. Oak Ridge.
Tenn. Apr 59. Contract W-7406-«ng-26. 22p.
Order from OTS. SO centa. Y-1309
Geology
and Mineralogy
I
Determinatiop c^ tfaorluna in rock aanylea >g gm
apectrometry, by S. A. Reynolda
National Laboratory, Oak lUdge. Tenn
lZHZQA
Contract W-7405-eng-26
Mi$1.8a Fh$1.80.
JiaeW.
7p. Order from LC.
CF-60-6-37
The detection aieaiihnuakts by water- level reccgd-
era, by M. W. McOonlga. General Electric Co.
Hanfbrd Atomic Producta Operation, Richland,
Waah. Nov 56. Contract W-7406-Bi«-52. 1^.
Order from- LC. Ml $2.40. ph$3.30.
HW-S7711
BTaluatlon o< utoaaonlc attenuatloe technlqaea ftar
tearing hoUowj uraniumcorea fbr tranatemaHon,
by C. U Fre<ieiick. General Electric Co. Haa-
iord Atxmlc Producta Operation, Richland, Waah.
Mar 57. Dec}. March 16. 1960. 9p. Order
fromLC. Ml$1.8a ph $1.80. HW-48875
The aurgice o< the baaah bedrock l>egeath die Haa-
ford Worka, by R. B. Brown and D. ]. Bipwn.~
General Electric Co. Hanfbrd Atomic Producta
Operation. Richland, Waah. Not 58. Contract
AT(45-1)-1350. 6p. Order from LC. Mi $1.|Q^
|ii$1.80. HW-5793S
Tbchnlquea for eatiiMtlng the apecMc retention
properdM of Hanfordaoila. hy W. H. BieradieA
General Electric Co. Hanford Atomic Produaa
Operation, Richland. Waah. Aug 59. Contraa
AT(45-1)-13S0. 44p. Order from LC.
Mi$3.3a ph$7.80. HW-61644
Sufaaurface geology of the Harford aeparatlon areaa,
by D. J. Brown. General Electric Co. Haaftxd
Atomic Producta Operatidn. Richland, Waah.
Oct 59. Contract AT(45-1)- 1350. 20p. Orxkr
fromLC. Ml $2. 7a ph $4. 80. HW-61780
Iborlum iaocopea method for dating marine aedl-
menta. TbMJa, by I. Almodoyar. Carnegie
Inatltuce of Technology, Plttaburgh. Pa. May 60.
Contract AT(30-l)-844. 125p. Order from LC.
Mi $6. 3a ph $19. 80. NYO-8919
Probing the earth with nuctear eyloaiona, by D. T.
Grlgga and F. Preaa. Rand Corporation. Santa
Monica, Calif. Sep 59. Contract AT(11-1)-1 35.
41p. Order from LC. Ml $3. 00. ph $6. 30.
RM-2456-ABC
Gamma -only aaaaylng fbr
tlona, by J. H. Scott and P,
um correc-
Tsaar
ProductiOB
Evaluation Divlaion, Grand JiBK:tioo Operationa
Office, ABC Grand Jtmction, Colo. Apr 60.
20p. Order from 015. 50 centa. RMB-135
The vaiiabllitT of atmoapherMpreaaure. Part P.
by B. N. Charlea. SflBdia (jorporatian, AQuquer-
que, N. Mex. May 56.
Mi $2. 7a Fh$4.80.
22p. Order from LC.
SCTM-160- 55-51
Conaparli
tlWrei
laon of the root curvature of a uniform can-
tilever beam laider dynaaalc loada with the root
curvature under a atatlc loaif
i
producing^
»andC.^
the aama
deflectlop, byM. V. Barton and C.
Laman. 'Sandia Corporation. Albuquerque,
N. Mex. Oct 54. Changed from OFFICIAL USB
ONLY Ortober 27. 1959. 15p. Order from LC.
Ml $2. 4a ph$3.30. SCnM-217-54-51
Ogonoaphere wlnda and temperawirea from acouatlc
obeerratlona of 1955 atomic teata. by J. W. Reed.
Sandi^ Corporation. Albuquerque. N. Mex. Oct
56. 12p. Order fromLC. Ml $2. 40, ph $3. 30.
SCIM-253-56-51
244
Onparlaoo of diickneaa, grade, and depth of radi(
active ^fara aa deteimlnBd by ganuna-ray log-
dns and oy core aampllng, by C. M. Bunker.
dns
ill
tampllng, by C. M. Bunker,
logical Survey. Waah>on. D. C. Aug 59.
33p. Order from LC.
Ml$3.0a ph$6.30.
■ lEI-dU
Baylneerlng geoloCT bearing oo harbor aite aelec'-
" don aioM die Sulf of Alaaka from Point WMtriied
to Cape Yatotaga, AJaaka, by R. KachadoorlaHT"
Geological Survey, WaaUngton, D. C^ Dec 59.
32p. Order fromLC. Mi $7.50, ph $24.30.
TEI-642
of Dolomite Hill. Nevada teat site, Nye
Nevada, by D. D. Dickey and P. A.
McKeown. Geological Survey, Washington,
D. C Nov 59. (^. Order from LC.
Ml $3. 9a ph$10.80. 'IEI-7B5
Hgnnolumlnearenoe of aome Dolomlce, tug, and
panltlc rock aanplea from the Nortfa-Oenttil
hrt of the Nevada test alae, Nye County. Nevada.
BjNyeCouwy^
D. Dickey. Geo!
A PTOgreaa report, by D. D. Dickey
calSiffvey, WaaUngton. D. C. July 60
Order from LC. Ml $2. 7a pd $4.80.
TBI-765
30p.
Wayal radlocarfaon in die Atlaittlc Ocean, by W. S.
Broecker and otihera. Columbia Unlveraity,
Lamont Geological Obaenratory, Paliaadea, N.Y.
Mar 60. Contract AT(30-1>- 1808. 73p. Order
fromLC. Ml $4. 5a ph $12. 30. TID-5735
Stnicture characterlatlca of clay minei^la aa
liKltrafrHJ by infrared apeotroacopy. Technical
art no. VTL by T. L, Mackay and otfaerB~
veralty of Utah. Inatltute for the Study of
Nov 54. Contract AT(49-1)-
633. 17p. Order from LC. Mi $2. 40,
pb$3.30. TID-5851
laatapLc gwochemlati-y of uranium and lead. Project
renewal propoaal covering period from Junet,
IW to ttay^lTlW, by]. L Kulp. Columbu
UBlveraityf Lamont Ceologlcal Obaervatory,
PaUaadea, N. Y. Apr 60. Contract AT(30-1)-
1114. 14p. Order fromLC. Mi $2.40.
ph $3. 30. TID-5B81
Health and Safety
gg-ate animal JnveetlptkMi project. Second an-
jBtl Ttnort, by G. R. Farmrf. Army VSttrP'
HiyCupa. . Laa Vagaa. Ner, Jtae 9i. Con-
tnctAT(29-l>-162. 20p: Order from LC.
Ml $2. 4a lih$3.30. ABCU-4613
The radiological aaaessment and recovery of oon-
tamlnairid ary , by C F. Miller. U. S. Naval
Radiological Defenae Laboratory, San Franclaco,
CaUf. Mar 58. 68p. Order from OTS.
TSoenta. CEX-57.1
and crew on
radla-'
Radiation doee received by naaornBerB and <
Planee carrying the maxfiman mimbei^of
don uolta, by D. M. Davia and others. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Mar 57. Contract W-7405-eng-26. 27p. Order
fromLC. Mi $2. 7a Fh$4.80. CP-57-3-152
SRE fujBl elementa rejg-Qceaslng aafetv report, by
B. B. KUma. Oak Ridge Nadooal Labcnratary,
Oak Ridge, Tenn. Feb 60. Contract W-7406- -
eng-26. 37p. Order from LC. Mi $3.00,
Fh$6.30. CF-S9-ll-122ateT.)
Fuel element cataatrqphe etudtee; Hazarda of
faaaion product releaae from inadlated uranium,
G. W. Parker and otfaera. Oak Ridge National
Laboracory, Oak Ridge, Tenn. June 60. Con-
tract W-7405-eng-26. 87p. Order from LC.
Ml $4. 8a ph $13.80. CF-60-6-24
Plutonium hantBlng— a lecture preaeiutBd to the re-
actor achoolon July 12, 1960, by C. J. Bafttn.
Oak Ridge National LaboraiDry, Oak Ridge,
Tenn. July 60. 12p. Order from LC. Ml $2. 4a
ph$3.30. CF-60-7-28
Sepil -annual progreaa ryoart, by C. N. Stover, Jr.
Unlveraity of Utah. RJadlohlokigy Laboratory,
Salt Lake City, Utah. Sep 59. Contract AT
(11-1)-119. 66p. Order fromLC. Mi $3.90.
ph $18.80. COO-219
Radiation aurvey, Coltnnbia Unlveraity Van De
Graafl. New York Operadona Office. Health
and Safety Laboratory, Atooiic Energy Commia-
aion. N. Y. Nov 58. I6p. Order from LC.
Mi$2.4a ph$3.30. HASL-50
Summary of available data on the atrontlum 90 coa-
tent of fooda and of total dieta in die Ualte9
gtatea, by J. H. Harley and J. Rivera. Pgted
States Atomic Etmnrr Commisaion. New York
Opera£iona Office, New Ybck, N. Y. Aug 60. 7Lp.
Order from OTS. $2.00. HASL-90
of nmmed film resulta tfarou^ Decem-
9S9:byJ. H. Harely, N. A. lUlden
L. D. Y. Oog. U. S. Atomic Energy Oommia-
aloB. New York Operationa Otfloe, New York.
N.Y. Sap 60. 30Sp. Order from OlS. $3.50.
HASL-93
248
M«n«l at r^uaop protection standardB. General
Electric Coi Hanlord Atcxnic Produca Operation,
Richland. Wash. Mar 60. Oootract AT(45-1)-
1350. 82p. Order from LC. Mi $4.80.
ph 113.80. , HW-25457 (Rev. 2)
Radiological aciencea department quarterly
rqiOTt GO raaearcfa and devel<»pient acdvitiea
for July— September 1953, by H. M. Parter.
General Electric Co! Ranford Atomic Products
Operation, Richland, Wash. Oct 53. Decl.
March 2. 1960. Contract W- 31 -109- Eng- 52.
35p. Order fnan LC. Mi $3. 00, ph $6. 30.
HW-29519
Radiological acJencea department quarterly progreaa
report on rasearch and development acdVltliM
report on rasearcn ana aeveiopaient actlTiaas
far April- jjune 1954, by H. M. Parker. General
Elecoic Co. , Hanford Atomic Products Operation.
Richland. Wash. Jiily 54. Decl. March 2, 1960.
Co«ract W-31-109-Bng-52. 29p. Order from
LC. Mi $2.70. ph$4.80. HW-32406
I
Radiological sciences department progreaa report
on rCTcarcfaand development activict«i for July-
September WSi byH. M. Parker. Get
Electric Co.' Hanford Atomic E*roducts Operatian.
iUcfaland. Waah. Oct 54. Decl. March 2. 1960.
Contract W^31-109-Eng-52. 27p. Order from
LC. Mi $2.70, phM.80. HW-33437
Preliminary Inteatlgarion of the Unlskaa proce—
for tfaejxttTision or aizing o< tuiiular sectlona,
by A. T. TWylor. General Electric Co. Han-
fard Atomic Products Operation, Ridiland, Wash.
hiov54. DecL January 29, I960. Contract W- 31-
109-Bng-52. 36p. Order from LC. Ml $3. 60.
ph$9.30. HW-33896
Nuclear
General B
la iB array*, by N. Ketzlach.
. Hanford Atooiic FtoAxxb
Mar 56. Decl.
9p.
c Co
Operaricin. Richland, Waah
Juneia I960. Contract W-31-109-Eng-52
OrderfromLC. Ml $1.8a ph$l JO.
HW -41899
FeasibiUt
isslbillty at iy yIyd plumnium meaauremeyta. by
W. C RoeschandJ. W. Baum. General Uectrlc
Co. Hanfortf Atomic Products Operation. Rich-
iand. Wash. Msy 56. Decl. with deletioos Janu-
ary 24. I9SS. Contract W-31-109-Ei«-S2. 7p.
OrderfromLC. Ml $1.80. ph $1.S0.
HW-43370(DeL)
Noise reducttai^
fapttai^ procram 300 area. Protect CG-640v
r. W. Gore. Hanftwd Atomic Products Opera-
don. Richlaad. Waaih. Mar 57. Decl. July 27.
1960. Gootzact W-31-109-Bnf-S2. 3Sp. Order
OTS. 40oeat», HW-48980
Dispoeltloii at contaminated processing eqvdpment
at Haflfard Atomic Products Operation. 1958-
1959, by P. S. Kingsley. General Electric Co.
Hanford Atomic Producta Opexatlon. Richland.
Wash. Feb 60. Contrsct W-31-109-Bng-52.
43p. Order from LC. Ml $3. 30, ph $7.80.
HW -63703
Radiological chemiatry operation semiannual repon
tuly-^December, 1959, by J. M. Nielsen. Han-~
tord Atomic ProducoRjperstion, Richland. Waik.
Mar 60. Contract A'It45-l)- 1350. 68p. Order
from OTS. $2.00. HW-63824
Evaluation of radloi
of Hanford
Junkina and
Operation. Richland.
AT(45-1)-13S0. 4Sp.
tsdlologlcsl coi
Ajaril tnrougb J
1 others. Hann]
conditions in the vicinity
■ -une 1 W. by R. L
'ord Atomic Products
Waah. Aug 60. Contraa
Order from OTS. $1.25.
HW-66287
Annual rCTort. of the healA and aafety division,
1958, byj. R. Horsn. Idsho Operations"T%lce
HealBi and Safety Division. AEC. Uaho Falls,
Uaho. 1958. 165p. OrderfromLC. Ml$7.8a
ph$2S.80. IDO-120U
The effects of a nuclear e:q)losion on commercial
oommiinlcatlons eqtdpment, by R. H. Williamaci
and others. Rsdio-Blectfonics -Television
Manufacturera Associatian. Waahington. D. C
and Federal Civil Defense Admlnistratian, Battk
Creek. Mich. M«y 55. 64>. Order from 01^.
$1.50. ITR-1193
Heahh plytei Quarterly repwt tor JaBusry--Marcl
I960, py R. f. Felnberg. Knolls Atonuc Power
Ldnratory, Schenectady, N. Y. 1960. Con-
tract W-31-109-Bng-52. 22p. OrderfromLC
Ml $2. 7a pli$4.80. KAPL-M-HP-i
Health
althpiwBlcs quarterly report for April— June 196(\
by R. J. Feinberg. tCnolls Atomic Power Laborr
tory. Schenectady, N. Y. 1960. Contract W-
31-109-Bng-S2. 2Sp. Order from LC.
Mi $2. 7a ph$4.80. KAPL-M-HP-S
A mtutf at two-stage sir samplers designed to siafr
Iste the mier and kwper resptrstnry tract, by
E. C Hyatt end others. The Ihilversity of
Callforala. Los Alamos Scientific Laboratory.
Loa AUoDoa. N. Max. Jioie 60. Contract W-
74Q6-ENG-36. S3p. Order from OIS. $1.25.
LA-2440
Bihsit f—tilatlon requirements for proponed FM
Mast csMaet, by B. C Hickey. Atonalcs Infer^
of North Anerlcnn AvlstlOB,
atf
toe., Canoga Park, calif. July 58. 6p. Order Environmental beta-gamma radio activity in air at
fnxn LC. Mi $1.80, ph $1.80.
^ NAA-SR-Memo-2924
vity in air
Sandia Laboratory] First quarter 1960, by A.
Qoud—An IBM 709 prograin for conqyting gai
ray done rate from a radioactlye ctoudT py D,
mma-
Duncan. Atomics International . Diviaion of
Nocih American Aviation, Inc. , Canoga Park,
Calif. [1959 J. 93p. OrderfromLC. Ml $5. 40.
ph $15. 30. NAA-SR-Memo-4822
Hespiratory protective eyipment. Progress report
— for June 1959 to April 1960, by L. Silvermsnind
others. Harvard University, School of Public
Health. Boston, Mass. June 60. Contract AT
(30-l)-2355. 59p. Ordq^from LC. Mi $3. 60,
ph $9. 30. ^ NYO-9322
Applied health physics *npu»l report for 1958, by
J. C. Hart. Oak Ridge National Laboratory,
Oak Ridge, Ttnn. 1958. Contract W-7405-eng-
26. 57p. Order from OTS. $1.50. ORNL-2777
Healdi physics division *"n"f 1 progress repon for
riod ending July 31. 1960, by K. Z. Morgan."
k Ridge National Labors tory. Oak Ridge,
Tenn. I960. Contract W-7405-eng-26. 294p.
Order from OTS. $4.00. ORNL-2994
Radioactive fallout. Annual progress report, by
P. K. Kuroda. University of Arkansas. College
of Arts and Sciences. FayettevlUe, Ark. Dec
59. Contract AT(40- 1)- 2529. 56p. Order from
LC. Mi$3.90, ph$10.8Q. ORO-234
On-site radiological safety report.
Operation
HARDTACK -Phase U. Reynolds Electrical and
Engineering Company, Int. , Radiological Safety
Division, Las Vegas, Net. 1958. Contrsct AT
(29-2)-l62. 141p. OrderfromLC. Mi $7. 20,
ph $22.80. OTO-58-5
General instructions for the recovery of rsdioactlve
contaminated eqigpment, by S. Glassstone, snd
others. Sandia Corporation, Albuquerque,
N. Mex. Aug 60. 21p. Order from OTS.
SO oenu. 1 SC-4225(M)
Juskiewlcz and others .
Albuquerque, N. Mex
from OTS. SO cents.
ory ■ First qua
others. Sandia
Sandia Corporation,
Oct 60. 8p. Order
SC-4495(RR)
Environmental beta -gamma radio activity in air at
" -" " P<^ quarter 1960, by
H. L. Rarrick and others. Sandia Corporation,
Sandia Laboratory. Second quarter~Is
Albuquerque, N. Mex. Oct 60.
from OTS. 50 cents.
8p. Order
SC-4496<RR)
Environmental beta-gamma radio activity in air at
Sandia Laboratory. Third quarter, by R. E.
WcMnelsduff. Sandl Corporation, Albuquerque,
N. Mex. Oct 60. lOp. Order from OTS.
50 cents. SC-4497(RR)
Fallout contours at Albuquerque, New Mexico, by
D. A. Young. Sandia Corporation, Albuquerque.
N. Mex. Jan 60. 78p. Order from LC.
Mi $4. 50, ph$12.30. SCTW- 195-59(51)
Inmri
ovementa in personnel metering pg-o^dures at
RTC, by F. V. Cifyerley and W. P. Gammlll.
Idaho Operations Office. Health and Safety Divi-
sion, AEC, Idaho Falls, Idaho. [1959]. 1^.
Order from LC. Mi $2. 40, ph $3. 30.
TID-5662
Studies of nuclear debris in precipitation. Quarterly
progress report no. 3. Isotopes, Inc. , West-
wocS. N. J. Mar 60. Contract AT(30-1)-2415.
6^. Order from LC. Mi $3. 90, ph $10. 80.
f TID-5710
A conceptual study of poesible collecting systems for
use in stratospheric sampling. Western Preclpi-
Ution Corporation, Loe Angeles, Calif. Apr 59.
Contract AT(04-3)-234. 91p. OrderfromLC.
Mi $5. 40, ph$15.30. TID-5847
A conceptual study of poesible collecting systems for
use in stratospheric sampling, by Western Pre-
cipitation Corporation, Loe Angeles, Calif. Apr
59. Contract AT(04-3)-234. 86p. Order from
OTS. $2.00. TID-5971
Environinental beta -gamma radio activity in air at
Sandia Laboratory, May ttirough Deceinber 1957,
by R. E. Womelsduff and others. Sandia Corpor-
ation, Albuquerque, N. Mex. Oct 60. 25p. Or-
der from OTS. $1.00. SC-4492(RR)
f
Environmental beu -gamma radio activity in air at
Sandia Laboratory, May through December 1959,
by H. L. Rarrick and otblers. Ssndis Corporation.
Albuquerque, N. Mex. Oct 60. 15p. Order
from OTS. 75 cents. ; SC-4494(RR)
247
Lung hazards from inhaled radioactive particulate
Public Health, Pittsburgh, Pa. July 57. Contract
AT(30-l)-912. 65p. Order from LC. Mi $3.90,
ph $10.80. TID-5961
The measurenaent of environmental radiation, An-
nual report and proposed program for the period
I
&e|)ceniber i, I960 to Ai^t 31. 1»61. New
Yoort University, Graduate Sdwol of Ana and
Sciences, New York, N. Y. July 60. 35p.
Order froo^ LC. Ml $3.00. pii$6.30.
TID-6123
A comprnrtiiim, d. Informstioo ftar use In ccMtrolling
' mdastioo enieigeucies. Including lecture notes
^^ -khoPsI
froin •
traiaing i
session at Idaho Falls, Msho,"
U-a \m, A. Brodsky ana offii^.
of Teduical Informatian Bjttension.
Oak Ridge. Teon.
cm. $1.00.
Sep 60. loop. Order from
TII>-8206(ReT.)
eicon
A iour-dianael oonfimioiwly recording monitor tor
air-borne a^^ha-actJTJty, by D. A. Morten and
R. H. Wilaoo. The University at Rochester,
Atomic Energy Protect. Rochester, N. Y.
July 60. Ckvtzact W-7401-eog-49. 31p. Order
from 013. 75 cents. UR-576
InstrufiMnts
<^
jBietic recorder for nudear pulye application.
Period covered: October 6, 1959 to December
5, 1»59, by G. M. Burgwald. Illlnoia Imtitutt
of Tecfanolofy. Armour Research Foundation.
Chicago, 111. Dec 59. Contract AT(ll-l)-702.
Up. Order from LC. Mi $2.40. ph $3.30.
ARF-1151-3
tic recorder far nuclear pulse application.
OTvejed: February 6^ to April 5, I960,
by G. M. Burgwald and R. M. Norton, niio^
Institute d Technology, Armour Research Foun-
dation, Chicngo. 111. Apr 60. Contract AT(11-
l)-702. 7p. Order from LC. Mi$1.80,
Fh$1.80. ARP-llSl-5
Resesrch study CO neutron interactiooe in mstter as
related to image formation. Report on phase I.
July r l^ ^^
April I to July 1, \¥A: by H. V.
ncncomh. iXluiois Institute d
mage
Period cpverea:
Watts and T^ Stii
Tectuiology. Armour Research Foundation,
Chicago. Ul. Aug 60. Contract AT(ll-l)-578.
43|>. Order from* LC. Mi $3. 30. ph$7.80.
ARF-1164-3
Notes on beliunt leak detection, by H. J. Metz.
Oak Ridge National Lafirai^ry, Oak Ridge.
Tenn. July )9. 30p. Order from LC. Mi $2. 70.
ph$4.80. CF-S8-l-20(ReT.)
cimei
Miniature TV camera manipulatpr, by P. P. Holz.
Oak Ridge Nitional Laboratory, Orit RkJ^fe.
TIenn. Nov 99. Contract W-7466-eng-26. 2Sp.
Order from LC. Mi $2.70. pb $4.80.
CF-59-ll-m
^
current saturation characteristics at the
'RNL compensated lonizetion chamber (Q-10451
by I. LTKlu&nui. Oak Rit^e Natlnnal libo^
tory. Oak Ridge, Tenn. May 60. Contract W-
7405-eng-26. 4p. Order from LC. Mi$1.8Qk
ph$1.80. CP-6O-S-104
Use of silicon surface-barrier counters in fast-
neutron detection and specyoscopy. by T. A«
Love and R. B. Murray. Oak Ridge National
Laboratory. Oak Ridge. T^nn. May 60. 25p.
Order from LC. Mi $2.70. ph $4.80.
CF-60-5-121
An electron multiplier as a detector for a surtace
ionizadonmass spectrometer - design, by L.
Cathey. E. I. du Pont de Nemours iTco. Ex-
plosives Department. Acomic Energy Division.
Technical EM vision, Savannah River Laboratory.
Aiken, S. C. Aug 60. Contract AT(07- 2)- 1.
18p. Order from OTS. SO cents. DP-498
Ion ptmy for the line recorder ntss spectrometer,
by P. I. Davis and C. H. Eubank. Goodyear
Atomic Corporation. Portsmouth, Ohio. Jan 60.
Contract AT(33- 2)- 1. 7p. Order from LC.
Mi $1.80. ph$1.80. GAT-T-726
Pressure transmitter, by J. B. Walker. Goodyear
Atomic Corporation. Postsmoutli. Ohio. May 60.
Contract AT(33-2)-l. 4ip. Order from LC.
Mi $1.80, ph$1.80. GAT-T-786
Test of high atability scaler for the detenninatioa
in redoat uranium, by F. P.
ral Electric Co. Haoford Atomic
of fission
Brauer
high
laioo
Products Operation, Richland, Wash. Aug 54.
Decl. March 2, I960. 1^. Order from LC.
Ml $2. 40. ph$3.30. HW-32708
Gamma photometer use for nondestructive deter -
niination of uranium content of enriched "C"
sluff , by D. O. Richards. General Electric Co.
Haoford Atomic Products Operation. Richland.
Waah. Mar 55. Decl. May 4, 1960. Contract
W-31-109-Eng-52. 4p. Order from LC.
Ml $1.80, ph $1.80. HW-35939
Manual for tlie effluent water gamma monitar, by
M. C. Greene and others. General Electric Co.
Hanford Atomic Products Operation, Richland.
Waah. [nd]. 34p. Order from LC. Mi $3. Oa
ph$6.30. HW-38191
248
Aa ultrasonic bond tester f or tfag Hanford canning
•^liae, by D. C. Worlton. General Electric Co~
Hanford Atomic Products Operation, Richland,
Wash. Nov 55. Decl. |une 10, 1960. 34p.
Older from LC. Mi $3. 00, ph $6. 30.
I j HW-39849
Project CAI-816-105-N desto criteria confinement
gystem instrumentatian, py W. A. Richards an3
J. K. FUckinger. General Electric Co. Han-
ford Atomic Producu Operation, Richland, Wash.
Nov 59. Contract AT(45j-l)- 1350. 8p. Order
ffomLC. Mi$1.80, ph;$1.80. HW-60440
Sack effluent monitor operation and maintenance,
by R. A. Harvey and G. D. Crouch General
Electric Co. Hanford Atomic Products Operation,
RichJaod, Wash. July 59. 29p. Order from LC.
Mi $2. 70, ph$4.80. ; HW-61194
A rotating source for gtllbration purpoees, by L. F.
Kocfaer. General Electric Co. Hanford Atomic
Products Operation, Richland. Wash. Oct 5^.
Contract AT(45-1)- 1350. 5p. Order from LC.
Mi $1.80. ph$1.80. HW-62386
lyansistor pre -amplifier tor neutron monitors, by
P. R. Kelly. General Electric Co. Hanford
Atomic Products Operation, Richland, Wash.
Apr 60. I6p. Order from LC. Mi $2.40,
ph$3.30. HW-64698
A needle -valve type of variable leak for uranium
heiafluoridjB aaass spectrooaeters, by E. F.
Babelay and L. A. Smith. Carbide and Carbon
Chemicals Co. K-25 Plant. Oak Ridge. Tenn.
Sap 52. DecL March 7, 1960. Contract W-
7405-eng-26. 17p. Order from LC. Mi $2. 40,
ph $3. 30. lC-935
Healdi
ics manual of calibration procedurea tor
ble and fixed »urvcy instrumentation, by
R. Kennedy and H. Aceto. Knolls Atomic
Bdver Laboratory. Schenectady, N. Y. Nov 59.
Gootract W-31-109-Eng-52. 76p. Order from
LC. Ml $4. 50, ph$12.30. KAPL-A-HP-S
An electrical resistance measuring device for
determining tjie diicknesa of a welded monel over-
lay on carbon ■teel. by A. C. Lind. KnoIS
Abamic Power Laboratory, Schenectady, N. Y.
Apr 60. Contract W-31-109-Eng-52. 29p.
Order from LC. Ml $2.70, ph $4.80.
I KAPL-M-ACL-2
Application of solid-state derlcea to ouclear plant
tscfapotogy, by R. F. Shea. Knolls Atomic
fcwsr Laboratory, Schenectady, N. Y. Apr 60.
Contract W-31-109-Eng-52.
LC. Mi $1.80, ph $1.80,
lOp. Order from
KAPL-M-RFS-1
Doaimetry tor the little Eva critical assembly,
neutron flux, spectrum, and tissue dose evalua-
tions, by J. A. Sayeg. D. G. Ott, and P. S. Harfia.
The University of California. Los Alamos
Scientific Laboratory, Los Alamos, N. Mex.
May 60. Contract W-7405-ENG-36. 24p. Order
from OTS. 50 cents. LA-2466
Fast response, low inertia vacuum furnace, by L. H.
Rachal. Atomics International. A Division of
North American Aviation, Inc. , Canoga Park,
Calif. Oct 60. Contract AT(ll-l)-CaEN-8. lOp.
Order from OTS. 50 cents. NAA-SR-5387
Transient tests of HNPF prototype sodium pump
drives, by R. W. Atz. Atomics International.
Division of North American Aviation, Inc. ,
Canoga Park, Cal if. Oct 59. 7p. Order from
LC. Mi$1.8a |)h$1.80.
NAA-SR-Memo-4127
Sunmury of progress on specific heat naeasure-
ments for zirconium hydride, by W. J. Tomasch.
Atomics International. Division of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. Nov 59.
20p. Order from LC. Mi $2.40, ph $3. 30.
NAA-SR-Memo-4654
Development of \
aent of kryptoo-85 static elimination oquiP'.
nient, by F. Palmeri, Jr. , H. P. Ccyeland. and I
J. G. MacHutchin. United Sutes Radium Corpor-
ation, Engineering Division, Bloomsburg. Pa..
Jan 60. Contiract AT(30-l)-2306. 83p. Order
from OTS. $2.00. NYO-2490
Final engineering report on automatic scanning of
nuclear emulsions, by K. C. Speh and S.
Becker. Airborne Instruments Laboratory, Divi-
sion of Cutler-Hammer, Inc. , Deer Park. N. Y.
Dec 59. Contract AT(30-1)- 1786. 97p. Order
fromLC. Ml $5. 40, ph $15. 30. NYO-2926
A multi-channel unit of solid Btate cwmters for
nuclear spectroscopy, by O. M. Bilaniuk and
others. University of Rodiester, Rochester,
N. Y. May 60. Contract AT(30-1)- 87 5. 24p.
Order fromLC. Mi $2.70. ph $4.80.
NYO-9026
The CWUNS human radiation councera. A prellmi-
nary rqxat, by M. Rnicer. Oak Ridge Institute
of Nuclear Studiea, Oak Ridge, Tenn. July 60.
I40p. Order from OTS. $1.50. ORINS-38
Large area
It P. J
rmanlum surface-barrier counters.
Oak Ridge National
alter and others.
Laboratory, Oak Ridge, Tenn. Feb 60. Con-
tract W-7405-eng- 26. 29p. Order fromLC.
Mi $2. 7a ph$4.80. OllNL-2877
249
Developinent o^ high speed electron accelerator
atructures. Interim report no. 10 for November
1. 1959— ja^iary 31 1J60. by). A. Balcker and
others. DaTld Sarnoff Research Center, Prinoe-
laa. N. J. I960. Contract AT(30-1)- 1958. 23p.
Order from !LC. Ml|2.70, phM-80.
RIB-43
Interim report joo developmeat ol deaign criteria
for relaya. Thla report covera tfae period 1
April to 31 iUy 1966. by School ot Electrical
Engineering! Oklahoma Stace (Jniveraicy, Stlll-
water, Okla^ Sandla Corporation. Albuquerque,
N. Mex. Ckt 60. 72p. Order from OTS.
$2.25. I SC-44S6(RR)
0€t60.
An improved P^ dlacriminator-detecror for air-
borne telemetry receivers, by G.
E. LandJ Sandla Corporation,
N. Mex.
75 oenta
Sep 60. 26p.
E. Reia and
Albuquerque,
Order from OTS.
SCR-208
The electrical behavior at
Experimental apparatus *nd te^
wirea. Part I.
que«, by
P. W. NelUbnaodL D. McKlnney Sandla
Corporation^ Albuquerque, N. Mex. Feb 60.
74ip. Order from LC. Ml $4. 50, ph $12. 30.
SCTM-8-60-(51)
The Wiancko pteaaure transducer (an evaluatloo
with aumeaapd naodificationa), by E. I. Vulgan.
SajKlia Corporatloa, Albuquerque, N. Mex.
Nov55. 33^
ph$4.80
Order from LC.
Mi $2.70.
SCTM-Il-56-51
Randon sync gBperator, by W. P. Nielsen. Sandla
CorporatlMi, Albuquerque, N. Mex. Mar 54.
9p. Order^omLC. Ml $1.80. ph $1.80.
SCIW-35-54-52
I
Oeclducerjfcomblnation oscillator andtranaduoer)
nnodel O6-l(l00, pressure -0 to 15 PSIA
Corporation^ Albuquerque, N. Mex. Jan 60.
7p. Order ^omLC. Mi $1.80. ph $1.80.
SCI>fl-38-60-(52)
A fast cloeing dnechanically operated electrical
awitch utilizjing a diflerentlai preaaure principle
Performance of the firat experimenul model, by"
W. J. Halpln and K.E. Hendricks. Sandla (Jor-
poration, Albuquerque. N. Mex. Apr 59. Coo-
tract AT(29-l)-789. 44p. Order from LC.
Ml $3.30, p> $7.80. SCTM-39-S9-(51)
Hl^-vacumn tacfaoiquea, by G. L. ICrlegsr. Sandla
Corporation,! Albuquerque, N. Mex. Mar 60.
27p. Order from OTS. $1.00.
SCIll-76-.60-(14)
Ejqgrlmental study of inverted L-, T-, and relate<
tranamiasion-line antennas, by S. Prasad and
R.W.P. King. Sandla Corporation, Albuquerqw,
N. Mex. Mar 60. 55p. Order frcxn LC.
Mi $3. 60, ph $9. 30. SCTM-82-60-a4)
Thermoelectric cells aa an aujdLliary power supply
In satellltea and apace mlaallea, by H. G.
Laursen. Smdia Corporation, Albuquerque.
N. Mex. Apr 60. lOp. Order from LC.
Mi $1.80, ph$1.80. SCTM-86-60-(52)
TWo-hour timer evaluation report, by R. K. Heck.
Sandla Corporation, Albuquerque. N. Mex. Mar
60: Up. Order from LC. Mi $2. 40. ph $3. 30.
SCIM-100-60-(13)
Time mark genenuor, by R. K. Hedc. Sandla
Corporatron. Albuquerque. N. Mex. Mar 60.
lOp. Order from LC. Mi $1.80. ph$1.80.
SCTM-101-60-(13)
The printed wiring technique applied to unit packag-
Injg o< a plug- In FM oscillator and DC amplifier,
by R. P. N«)le. Sandla Corporation< Allniquer-
que, N. Mex. May 55. I6p. Order from LC.
Ml $2.40. ph$3.30. SCTM-ia7-55-53
Transistors applied to an FM-FM airborne radio
telemetry system, by R. H. Gablehouae. Sandli
Corporatian, Albuquerque, N. Mex. May 56.
74p. Order from LC. Mi $4. 50. ph$12.30.
SCn\I-107-56-52
A survey of fast -rising balloona and RAWN rcftec-
tors by T. J. Raftery and H. J. Plagge. Sandla
Corporation. Albuquerque. N. Mex. Oct 60.
lOp. Order from OTS. 50 cents.
SCmvl-142A-57(S2)
The fabrication and application at switching and
oommutatlng druma, by W. O. Johnson. Sandla
CorporationT Albu^ierque, N. Mex. May 59.
lip. Order from LC. Ml $2.40, ph $3. 30.
SCn>«-160-59-(l5)
Tbe uee at tranalent analysla In the evaluation of
eleOTomagnedc relays, by R. C. A. Sadler.
Sandia Corporatian, Albuquerque, N. Mex.
July 60. 28p. Order from 015. $1.00.
SCTM-I76-60-(14)
A nttoarlal sigyey jf Informatlfln storage devices,
by O. K. Skoueen. Sandla Corporation. Albu-
querque, N. Mex. Sep 59. 6^. Order from
LC. Ml $3. 9a ph $10.80. SCTM-262-59-(l5)
290
TILA-PECXJM" -Model A (A transistorized Pam
— aecommuutor), by P. R. Palmer and odiers.
Sandla Corporation. Albuquerque, N. Mex.
Sep 58. Contract AT(29t-l)-789. 71p. Order
from LC. Mi$4.80, ph.$13.80.
' SCTM-282-58-(52)
A plug- i" magnetron radio frequency power source
~ fOT the antenna pattern range facility, by J. P.
Sandla Corporatian, Albuquerque.
DankwortK
N. Mex. Sep 60. 32p
Order from OTS. $1.0a
SCTM-282-60-(14)
Electrical fuses and their utilization in Sandla
Corporation systemB, by C. D. Longerot. Sandla
Corporation, Albuquerque, N. Mex. Nov 60.
22p. Order from OTS.
75 cents.
* SCTM-304-60-(14)
Constant current battery discharger, by R. J.
Tockey. Sandia Corporation, Albuquerque.
N. Mex. May 59. Conti^act AT(29-l)-789. 14p.
Order from LC. Mi $2.j40. ph $3. 30.
SCTM-359-58-(8l)
Automatic reacout system Berkeley to galvanometer,
by C. M. Warthen. Sandia Corporation, Albu-
querque, N. Mex. Nov {59. 16p. Order from
LC. Mi $2. 40, ph$3.30. SCTM-364-59-(16)
A Sandia prototype system erf the Zeus capacitor
bank, by R. D. Aden and H. E. Morris. Sandia
Corporation, Albuquerque, N. Mex. Jan 60.
15p. Order from LC. Mi $2. 40, ph $3. 30.
SCIM-377-59-(12)
A method for determining the curie loading erf Kr^^
in nuclear batteries, by A. Thom. Sandia
Corporation, Albuquerque, N. Mex. Jan 60.
1^. Order from LC. Mi $2.40. ph $3.30.
SCn>4-381-59-(l6)
i I
The application of super -njgeneration to UHF. by
R. L CNan. Sandia Corporation, Albuquerque,
N. Mex. Jan 59. Contract AT(29-l)-789. 34p.
Order from LC. Mi $3.«), ph $6. 30.
SCTM-431-58-(14)
Pinal report on miUmeter wave components, by L.
L. Bertan. PXR. Inc., Woodside, N. Y. July
59. Contract AT(ll-l)-663. 30p. Order from
LC. Mi $2.70, ph$4.80. TID-5623
The channeled image interttifier. Seventh quarter-
ly progress reporf! University of Chicago.
Ouca^ Midway Laboratories. Chicago, 111.
I«b60. Contract AlXl 1^1)- 647. 21p. Order
from LC. Mi $2.70. ph$4.80. TID-5665
Radioisotope X-ray generator. Quarterly progress
report no. 3 covering the period froni January 1,
to March 31. 1960, by M. W. Chisholm and
others. Picker X-Ray Corporation, Picker Re-
search Center, Cleveland. Ohio. 1960. Contr
tract AT(ll-l)-746. lOp. Order from LC.
MI $1.80, ph$1.80. TID-5793
Unitized system of image intensifiers using fiber
<ylcs. Progress report for Noverober~1959
throug^March 196C. byj. S. Kalafut. Westlng-
houseElectric Corporation, Electronic Tuber
Division. Elmlra. N. Y. I960. Contract AT
(30-l)-2176. I9p. Order from LC. Mi $2.70,
ph$3.80 TID-5890
Hirti temperature thermometry seminar held Octo-
ber 1-2. 1959 at Oak Ridge National Laboratory,
by W. R. Grimes and D. R. Cuneo. Oak Ridge
National Laboratory, Oak Ridge. Tenn. Aug 60.
I 171p. Order from OTS. $1.80.
TID-7586(Pt. I)
Proceedings of the eighth conference on hot labora-
tories and equipment held at San FranciBCO.
California on December 13-15, 1960. by L. G.
Stang, Jr. and others. The American Nuclear
Society, The Hot Laboratory Division. 1960.
Book 1 - 296p. Book 2 - 250p. Order from 0T5.
Toul price $5. 75. TID-7599
Scintillation counter y- spectra unfolding code for
die IBM -650 comjJuter, by H. I. West. Jr. and
B. Johnston. University of California, Law-
rence Radiation Laboratory, Livermore, Calif.
Feb 60. Contract W-7405-eng-48. 26p. Order
from LC. Mi $2.70, ph $4.80. UCRL-5808
The vemi-ray, an inatnanent to measure the unl-
formity of di in foils, by J. Benveniste and others.
University of California. Lawrence Radiation
Laboratory, Livermore, Calif. Aug 60. Con-
tract W -7405 -eng- 48. 8p. Order from OTS.
50 centa. UCRL-6049
Evaluation of high-speed two- tube configurations.
Part I. Greattr gatn-bandwldth in trigger cir-
cuits. Part it. Transient analysis of the white
cathode follower. Thesis, by M. Brown. Uni-
versity of California. Lawrence Radiation
Laboratory, Berkeley, Calif. Nov 59. Contract
W-7405-eng-48. 60p. Order from LC.
Ml $3. 60, ph $9. 30. UCRL-8954
Nuclear materials control system (NMCS). Phase
II. A doorway monitor for safeguards use, by
P. J. Arsenault. Wesringhouse Electric Corpoir-
ation. Atomic Power Department. Pittsburgh, Pa.
Feb 60. Conu-act AT(30-1)-2176. 63p. Order
from LC. Ml $3.90, ph $10.80. WCAP-6038
251
TraiMlatortzed pulae counting equipment, bjrj. J.
Henry. Union Carbide Nuclear ComiMny, Diri-
■ioa of 'Joiot Carbide Corporatloa, Y-12 Plant.
Oak Ridge, Tenn. July 60. Contract W-7405-
eng-26. 33d. Order frcin OTS.
75 cents.
Y-1313
Isotope Separation
An experimental
irradiator for hoapital
oapit
omei
gamma
sterilization, byj. H. Frankfort anToaiera.
Associao^Tlucleaonics, Inc. , Garden City.
N. Y. Mar 60. Contract AT(30-1)- 2349. 96p.
Order from ens. $1.50.
AN-119
An imtusttial gynma irradiator for medical snyliea.
by J. H. Fraakfort and othera! Associated
NMcieonica, Inc. , Garden City, N. Y. Feb 60.
Goainct AT(30-l)-2349. 138p. Order from
GTS. J2.00i -___ AN-120
Mela
llurgy and Ceramics
SummarY repott on irradiation at piototyue EBR
m
n fuel f leroents, by J. H. Mooaweck
Soira. Argoilne National Laboratory, Argonoe.
m. Sep 60. Contract W-31-109-eng-38. 3^.
Order from 015. 75 cents. ANL-6010
Stabilizing eflecta erf oxide additjona co uranium
oride byW. 6. Wilson and A. P. Gerda. Bat-
telle Memorial Institute, Columbus, Ohio.
Sep 60. Contract W-7405-eng-92. 13p. Order
fromOTS. 10 cents. BAI-1467
Alumina coating^ o< UO? shot by hydrolysis of aluml-
num chloride vapor, by M.F. Browing and
others. Ba tte 1 le Memorla 1 Institute, Columbus.
Ohio. Oct 6Q. Contract W-7405-eng-92. I2p.
Order from OnrS. SO cents. mAl-l47l
I
/
Determination d interstitial soUd-solublUty limit
in tanttlum aiid identiflcadon of the
iaea, by D^ A. Vaugban and others
MUty 11
precapi
tate
Battelle
>rial Institute, Columbus, Ohio. Oct 60.
28p. Order ^om OTS. 75 cents. Bi«I-1472
r
Fabrication of d>e PRTR Zlr(aloy-2 high pressure
process tubM, by R. L. ICnedtf. wnford Atom-
ic Products73i>eratioo. Richland, Waah. July 59.
Contract AT(«5- 1)- 1350. 4^. Order from
OTS. Jl.25. HW-60358
PieHerred orientaticnB in exguded Zlrcaloy-2 tub^
by J. J. Laidler. General Electric Co. Hanfo^
Atomic Products Operation, Richland. Wash.
Apr 60. Contract AT(45-l)-1350.35p. Order
from OTS. $1.50. HW-6481S
r'. .ft --.
>loeiona la
Some seismic effects of underground expi
cavities, by G. L. Lamb, jr. The university
of California . Loa Alamos Scientific Laboratoiy,
Loa Alamos. N. Mex. Feb 60. Contract W-
7405-ENG-36. $1.25. .. LA-2405
Kinetlca and mechaniam of the oxidation of uranium
dioxide and uranium dioxide plus fissia sintereB
pellets, by T. Smith. Atcnnics International.
A Divlalon of North American Aviation. Inc. ,
Canoga Park, Calif. Nov 60. Contract AlXll-
l)-GEN-8. 96p. Order from OTS. $2.00.
NAA-SR-4677
A dode for indexing poeder patterna, by I. R. Tan-
nenbaum and otners. Atomics International. A
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Nov 60. Contract AT(ll-l)-
GEN-8. 67p. Order from OTS. $1.75.
NAA-SR-4710
Melting and forming erf SB R fuel rods, by P. S.
Drennan. AtomTcs International. A Division
of North American Aviation, Inc. . Canoga Park,
CsUf. Oct 60. Contract AiXH-l)-GEN-8. 30p.
Order from OTS. SO cents. NAA-SR-4762
Uraniimn alloy fuel element fabrication development
for HNPF core 1, by S. M. Cobb. Atomics
Intematicxial. X Division of North American
Aviation, Inc. . Canoga Park. Calif. Nov 60.
Contract AT(ll-l)-aBN-8. 55p. Order from
ens. $1.25. NAA-SR-5291
Measurement of surface area of uranium dioxide
powder and sintered pellets, by T. Smith.
Atomics International. A Division of North
American, Aviation, Inc. , Canoga Park, Calif.
Oct 60. Contract AT(ll-l)-GEN-8. 47p. Order
from OTS. $1.00. NAA-SR-5319
Corrosion of materials by lithium at elevated tern
%
peratures, by E. E. Hoffman. Oak ^idge Nation-
al Laboratory, Oak Ridge, Tenn. [nd). Contract
W-7405-eng-26. 147p. Order from OTS. $2.75.
r ORNL-2924
Metallurgy of Zlrcaloy-2. Part I. The effects of
fabricadon variables on the anisotropy of me
cfasnical properties, by P. L. Rittehouse and
M. L. Plckleslmer. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. [nd.) Contract W-7405-
eng-26. 106p. Order from OTS. $2.25.
, . ORNL-2944
252
Study of pses in metals. -A Literature survey, by
J. P. Pemsler. Nucleaf Metals, IncorpraFabed,
Concord, Mass. Aug 59. Contract AF-33(616)-
6627. Sip. Order from OTS. $1.00.
NMI-9B00
An iojat^UP electromametic dispersion experiment,
by S. D. Softky and R. K. Squire. Uniwrsity
of California, Lawrence Radiatioa Laboratory,
Uvermore, Calif. May 60. Contract W-74a5-
eng-48. 21p. Order from OTS. 50 cents.
UCRL-5966
Nuclear Explosions — Peaceful Applications
An evaluation of the factors lirfluenclng the sfMHty
of a Urge underip-ound cavity, by D. U. Deere
and others. University of Illinois, Urbsna, O;.
Nov 59. 81p. Order from OTS
$2.00.
AECUf4654
Particle Accelerators and High-
Voltage Machines
I
Remarks on elementary particles and tfaelr inter-
actions, by D. B. Lichtenberg. Midwestern
Universities Research Association, Madison,
Wis. Aug 59. Contract AT(ll-l)-384. 211p.
Order from OTS. $3.00. TID-6537
Physics and AAathemotics
The scattering of positrons by atomic h,
Formulation, by W. I. Codv and 1^, 'fimlt
Arfonne National Laboratory, Argonoe, 111.
Oct 60. Contract W- 31-
from OTS. 50 cents
09-eng-38.
17p. Order
ANL-6121
Calculation of heterogeneity effects in ZPR-m fast
aaaemblles using die D^ prop-am. by D. Mene-
ghettl and M. F. Loomls. Argonne National
Laboratory, Argonne, 111. Nov 60. Contract W-
3l-l09-eng-38. 31p. Order from OTS. 75 cents.
ANL-6218
T^ calculation of transient temperature diatribu-
Ogns In a solid cylindrical pUi. cooled on tty
mlacenM-704 program X24/RB-li7. bvt.
Heestand and others. Argonne National Labora-
tory. Argonne, III. Oct 60. Contract W-31 -109-
«Og-38. 140p. Order fro|n OTS. $2.50.
ANL-6237
i
description of thermal conductivity and dynamic
>^coelty of water in the critical region, by C. A.
Fritsch and R. J. Grosh. Argonne National
Laboratory, Argonne, UL Oct 60. Contract
W-31-109-eng-38. 40p. Order from OTS.
$1.00. ANL-6238
A technique for observation of die nuclear nmgnetic
resonance of some short-lived nuclloes and its
W-31-109-eng-38.
$2.25.
Order from OTS.
ANL-6263
Richland, Wash. Apr 60. Contract AT(45-1)-
1350. ISlp. Order from OTS. $2.75.
HW-64866
The study of mulrt- region reactions wldi an analog
computer, by 1. C. Peden. Hanford Attmir
Products Operation, Richland, Wash. July 60.
Contract AT(45-1)-1350. 50p. Order from OTS.
*l-25. HW-65578
PUBOO-Il an IBM 704 code for
die ideal
tfaermodynamlc functions erf a dLatonrdc gas
°»'ecule, by L. R. Sitnev. Tlie Unive^alry nf
California. Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. Mar 59. Contract W- '
7405-ENG-36. 82p. Order from OTS. $2.00.
LA-2304
Theory of angular momentum in N-dimenaional
space, byl. U. UXiCk. 'Hie UnJveratry n/
California. Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. May 60. Contract W- 7405
7405-ENG-36. 298p. Order from OTS. $4.00.
LA-2451
WAT: A numerical mettiod for two-dimensional
unsteasy fluid flow, by W. B. Goad. Tlie Univer-
sity of California. Los Alamos Scientific Labora-
tory, Los Alamos, N. Mex. Sep 60. Contract
W-7405-ENG-36. 21p. Order frtmi OTS.
50 cents. LAMS-2365
CRLff>ICH - An IBM-704 code for calcuUting succes-
sive first-order reacticwB. by M. P. LietzK~aia
H. C. Claiborne. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Nov 60. Contract W-7405-
eng-26. 46p. Order from OTS. $1.25.
ORNL-2958
EQCOPOISE - An IBM-704 code tor the solution of two-
groiq), two-dlmenMional, neutron diffusion
253
I
equatiOQg in cylindrical geometry, by M. L.
Tobias and T. B. Fowler. Oak Ridge National
Laboratory, Qak. Ridge, Tenn. [nd]. Contract
W-7405-eng-J6. 87p. Order from 013. $2.00.
ORNL-2967
Ca
ipture-gamma determination erf vanadiu'Ti leyela,
by J. ETschiiiager. University of California.
Lawrence RalUation Laboratpry, Uvermore,
Calif, Jan 60. Contract W-7405-eng-48. 96p.
Order from (yi5. $2.00. UCRL-6003
J.
Meaaurement of the temperature dependence of
neutron diffusion properties in beryllium using
a pulsed neutron technioue. Theaia, by W. M.
Andrews. University at California. Lawrence
Radiation Laboratory, Uvermore, Calif. Aug
60. Contract W-7405-eng-48. 232p. Order
fromOTS. 13.00. UCRL-6083
Studlea of the oonductiYlties of disperaiona. Thesis
by R. E. Meredith. University of California,
Lawrence Radiation Laboratory, Berkeley, Calif.
July 59. Contract W-7405-eng-48. I33p. Order
fromOTS. ^2.75. UCRL-8667
Scatterln
itterlng of positive pions on protona at 310 Mev:
Recoil- nucleon polarizatioo and phase -shift
analysis, Thesis, by J. H. Foote. University
of California, Lawreace Radiation Laboratory,
Berkeley, Callif. Sep 60. Contract W-7405-eng-
48. ISlp. drder from OTS. $2.50.
UCaiL-9191
Graphs and tables o< zero- fie Id hype rfine- structure
level ordering in free atoms, oy F. S. Baker.
University oi California, Lawrence Radiation
Laboratory. Berkeley, Calif. Aug 60. Coo-
tract W-740J$-eng-48. I47p. Order from OTS.
$2.75. UCRL-9364
Electron triplet production by high-energy photons
In hydrof^n, by D. C. Gates. University of Cali-
fornia. Law fence Radiation Laboratory, Berke-
ley. Calif. $ep 60. Contract W-7405-eng- 48.
Il5p. Ordet from OTS. $2.25. UCRL-9390
Radiation EfFacts on AAoterials
Speclficatioos fbr ttaerroocouples, suinless steel
sbeatfaed, corrosion resistant, for nuclear "seir-
byB.s:
vice,
ford Atomic
Wash. Apr 60
ph$1.80.
Koeut. General Electric Co. Han-
Products Operation, Richland,
3p. Order from LC. Ml $1.80.
HW -64744
i
i.
US ABC conference on the sMtus <rf radiation effecu
research on structural materials and the inrtpli-
cations to reactor design held at Chicago, Illi-
SoIirOctober 15-16, 1959, by J. B. Trice and
others. USAEC Office of "Technical Informatioc
Extension, Oak Ridge, Tenn. Oct 60. 306p.
Order from OTS. $4.00. TlD-7588
Fast neutron effects on DuPont 1290 film, by S.
Block and L. Hughes. University of Ca lif omia .
Radiation Laboratory, Livermore, Calif. June
58. Contract W-7405-eng-48. 7p. Order from
LC. Mi $1.80, ph $1.80. UCRL-5264
Radioactive V/a%\m
Radioactive waste disposal, by W. A. Rodger.
Argonne National LaEoratory, Argonne, HI. Sep
60. Contract W-31-109-eng-38. I69p. Order
fromOTS. $2.75. ANL-6233
Techniques for estimating the specific retention
■^Bf opertles of Hanford soils, by W. H. Bierschenk.
fuLnford Atomic Products Operation, Richland,
Wash. Aug 59. Contract AT(45-1)- 1350. 38p.
Order from OTS. $1.25. HW -61644 REV.
The effect of temperature and flow velocity on the
decontamination of reactor effluent water with
aluminum, by W. B. Silker. Hanford Atomic
Products Operation, RichUnd. Wash. Dec 59.
Contract AT(45-1)-1350. 19p. Order from OTS.
75 cents. HW -62874
Reactors — General
Removal of EBWR fuel element scale by slurry
honing, by 1. Charak. Argonne National Labora-
tory, Argonne, 111. Sep 60. Contract W- 31-
. 109-eng-38. 18p. Order from OTS. 50 cents.
* ANL-6216
Some calculations for a plutonluro-fueled ZPR-lIl,
A. R. Baker. Argoni^ National Laboratory,
Argonne. 111. Sep 60. Contract W- 31 -109 -eng-
38. 24p. Order from OTS. 50 cents.
ANL-6217
On the problem at liquid entrainment, byG. C.K.
YdiandK. ZidKr. Argonne National Laboratory.
Argonne. 111. Oct 60. Contract W- 31 -109 -eng-
38. Il6f>. Order from OTS. $2.50.
ANL-6244
254
Proceedings of the conference on transfer functioo
"meaaurements and reactor stability analysis
held at Argonne National Laborato;
ory, Argonne,
DeShoogT Jr.
Illljiols May 2-3, 1960 by J. A. DeShoog. Jr.
and others. Argonne National Laboratory,
Argonne, 111. I960. Contract W-31-109-eng-38.
33^. Order from OTS. $4.00. ANL-6205
I
Reactor development program progress report, by
N. Hilberry and otners. A rgoime National
Laboratory, Argonntf. 111. Nov 60. Contract
W-31-109-eng-38. 59p. Order from OTS.
$1.50. ANL-6253
Addendum to hazards summary report for the
GCRE critical-asseinbly eiqierlments. by J. W.
Cbastaln. Battelle Memorial Institute, Columbus.
Ohio. Sep 59. Revised November 14, I960.
Contract W-7405-eng-92. 30p. Order from
OTS. 75 cenu. BMI-1379 (Rev. )
I
A ■tudy at sodium fires, by J. D. Grade and J. J.
Drooer. Atomics International. A Division of
North American Aviation, Inc. , Canoga Park,
Calif. Oct 60 Contract AT(ll-l)-GEN-8. 84p.
Order from OTS. $^.00. NAA-SR-4383
Testing of HNPF freeze-seal Pump. by R. W. Atz.
Atomics International. A Division of North
American Aviation, Inc. , Canoga Park, Calif.
Nov 60. Contract AT(11-1)-GEN -8. 48p.
Order from OTS. $1.00. NAA-SR-4387
Iqua OMR purification system development, by
W, N. BleyandR. W- Burkhardt. Atomics In-
ternational. A Dlv^ion at North American
Aviation, Inc. , Canoga Park, Calif. Nov 60.
Contract AT(ll-l)-GEN-8. 65p. Order from
OTS. $1.50. NAA-SR-5073
A test cell for evaluating the air leakage of building
components, by L. Baurmash and otters.
Atomics International. A Division of North
American Aviation, Inc. , Canoga Park. Calif.
Sep 60. Contract ATXll-l)-GEN-8. 21p. Or-
der from OTS. 50 cents. NAA-SR-5138
Exponential "eaqjerlments widi gaphlte-moderated
uranium-naetal lattices, by R. W. Campbell
and R. K. Paschall. Atomics International.
A Division of North American Avlatlnn. Inc. ,
Canoga Park, Calif. Sep 60. Contract AT(11-1)-
GEN-8. 32p. Order from OTS. 75 cents.
NAA-SR-5409
Reactors — Power
Cost study of a 100-Mw fe) direct -cycle boiling
water reactor plant, oy C. F. Bullinger ana J.
M. Harrer. Argonne National Laboratory,
Argonne. III. July 60. Contract W- 31- 109-eng-
38. 96p. Order from OTS. $2.25. ANL-6178
Operational tescs of EBWR vapor recovery system,
by R. J. Gariboldi and D. R. Jacobson. Argonne
National Laboratory, Argonne, III. Aug 60.
Contract W- 31- 109-eng- 38. 48p. Order from
OTS. $1.25. ANL-6189
Design study sodium modular reactor, by J. F.
Cage, Jr. and others. General Electric Co.
Atomic Power Equipment Department, San
Francisco Operations Office, San Francisco,
Calif. Jan 60. Contract AT(04-3)-189. 366p.
Order from OTS. $5.00. (SAP-S334
The response surface cytimlzatlon technique, by
W. D. Leggett. Atcxnics International! A Divi-
sion at North American Aviation, Inc. , Canoga
Park, Calif. Sep 60. Contract AT(ll-l)-aEN-
8. 73p. Order from OTS. $1.75.
NAA-SR-4604
Nuclear power tanker design and economic >Mly-
sis indirect cycle boiling water reactor, by G.
H. ^arbman and od>ers. Westingbouse Elec-
tric Corporation. Atomic Power Department,
Pittsburgh. Pa. Jan 60. Volume 1 235p.,
Volume II. 148p. Order from OTS. $7.00.
WCAP-1340(Vol. I li U)
Technology — Feed Materials
Expansion
ram at St. Louis Ares — Project no.
ion re-
Louis
irea Office, Oak Ridge Operations Office. AEG,
Oak Ridge. Tenn. Oct 60. 344p. Order from
OTS. $3.50. TID-5886
mysim program at St. Louis Ares — Projo
224-506oA. Project history and completic
port, by F. H. Belcher and others. St. I
2SS
^.
-t .■.■■.«■? - •■■
SOURCE INDEX
Source
Atknlral Corp.
Chicago, UL
Aerp Geo Ascro Corp. ,
Akxaodria, Va.
Aerojet-General Cor^p.
AziM. Calit
Page
ao3
161
146
177
Aeronautical Accessories Lab. ,
Wright Air Development Dlv. ,
Wright -Patterson AFB, Ohio 172
AtfrooaiKical Electronic and
Electrical Lab. , Naval Air
Development Center,
Jolmaville, Pa.
Aeronautical Research Lab. .
Wright Air Development Div.
Wright -Patterson AFB, Ohio
Aeronautical Research Labs. ,
Air Force Research Div. ,
Wright -Patterson AFB, Ohio
Air Force Cambridge Research
Center.
Air Force Missile Development
Center, Holloman AFB,
N. Mex. j
Air Force Special Weapons
Center, Kirtland AFB.
N. Mex.
Air Proving Ground Center,
BfUnAFB, Fla.
Air Wea'bier Service,
Scott AFB, m.
Airborne Instruments Lab. ,
Deer Park, N. Y.
American Inst, for Research,
Ptttaburgh. Pa.
PB Number
148 979
149 059
148 289
152 546
171 134
161 153 260
205 171 143
184 171 161
Bedford, Mass.
189
205
152 202
152 283
Air Force Cambridgt
! Research
Labs.,
Bedford, Mass.
154
161
162
172
149 061
148 705
148 709
148 706
149 058
•
184
148 707
138 152 428
ZS2
. 152 639
162
153 067
149
152 042
162
148 711
133
162
171 139
148 284
Source
^r
PB Number
American Machine and
Foundry Co. ,
Niles, UL
160
171 145
Amperex Electronic Co. ,
Hicksville, N. Y.
162
152 22S
Antenna T ,ab. , Ohio U.
Research Foundation.
Columbus
219
152 242
152 1<S8
153 255
Antioch Coll. , Yellow ^rlngs,
Ohio 146
Applied Mathematics and
Statistics Labs. .
Stanford U., Calif.
Applied Physics Lab. , John
Hopkins U. , Silver
Spring. Md.
Arctic Aeromedical Lab. ,
LaddAFB. Alaska
Arctic Inst, of North America,
Washington. D. C
Armour Research Foundation,
I Chicago. IlL
Army Research Office.
Washington, D. C.
Army Signal Research and
Development Lab. , Fort
Monmouth. N. J.
149 701
IM
148 978
152 160
152 162
185
152 161
192
152 163
146
150 781
139
152 849
152 8.'in
152 853
140
152 851
141
152 8S2
150
152 290
146
152 244
138
171 (XX)
144
171001
157
171004
206
171003
222
171005
150
152 196
151
152 568
162
152 804
152 990
163
150 074
172
152 991
223
152 566
152 567
M
Source
», Ic
Page PB Number
Arm> Snow, Ice and Permafrost
Research Eetabllshment,
Wllmene, llL 152
Arnold Engineering Develop-
ment Center, Tullahoma,
Tenn.
ARO. Inc..
Tullahoma,
159
173
193
Tenn.
159
173
193
Associated Engineers. Inc. .
Springfield^ Mass.
Audlology Lib. . Northwestern
U. . Bvanston, 111.
Avco Corp, ., Nashville, Tenn.
AvcoCorp.
Wilmington, Mass.
Avco-Bvereit Research Lab. .
Mass.
139
157
217
194
210
214
Aviatlan Medical Acceleration
Lab. . Naval Air Development
Center, Jofansville, Pa.
Ballistic Reteftrch Labs. ,
Aberdeen Proving Ground, Md.
Bund Reseirch Foundation,
Franklin Inat. .Swarthmore,
Bsttelle Metioriid Inst. .
Columbus, Ohio
153
ISB
161
aoe
210
iehsvioral Sciences Lab. .
Wright Air Development Dlv. .
Wright-Pwttersoo AFB, Ohio
135
143
173
152 387
152 388
152 456
152 457
153 280
152 554
147 878
152 260
152 555
152 758
153 379
153 280
152 554
147 878
152 260
152 55
152
555
758
144 152 393
152 766
152 343
152 472
148 720
152 426
149 669
149 067
210 152 469
173 152 435
a03 149 700
152 015
152 494
171 149
152 538
152 760
171 146
153 059
171 137
Source
Bell Aircraft Corp. ,
Buffalo. N. Y.
Bell Telephone Labs. . Inc. ,
Whippany, N. J.
Bendlx Radio Div. . Bendix
Aviation Corp. ,
Baltimore, MdL ,
Benson-Lehner Corp. , Sanu
Monica, Calif.
Biomedical Lab. , Wright Air
Development Div. , Wright-
Patterson AFB, Ohio
Blue Hill Meteorological
Observatory, Milton, Mass.
Bolt, Beranek and Newman, Inc.
Cambridge, Mass.
British Columbia U. (Canada)
Brooke Army Medical Center,
Fort Sam Houston, Tex.
Brown U. , Providence, R. I.
Brown U. Div. at Applied
Mathematics. Providence,
R. L
Brown U. Div. of Engineering,
Providence, R. I.
California U. , Berkeley
California U. , Los Angeles
Page
179
163
157
223
139
143
PB Number
171 141
149 719
149 730
148 708
148 977
171 140
171 Itt
154 148 718
134
189
197
207
142
177
223
Cambridge U. (Gt. Brit)
Carborundum Co. . Niagara
Falls. N. Y.
1-2
152 255
152 519
171 138
152 208
152 366
152 367
149 074
152 016
19^ 148 725
161
149 699
194
152 413
201
159169
219
148 296
185
148 670
217
152 484
135
ISO 500
139
152 112
154
152 552
152 553
163
147 651
149 136
189
152 213
142
152 540
202
152 421
152 422
152 424
214
152 423
179
171171
Source
I
Page PB Number
Source
Page PB Number
(jtrncgle Inst, of Tech. ,
Pittsburgh, Pa.
Case Inst, of Tech. , |
Cteveland, Ohio I
OMtral Inst, for Industrial
Research (Norway).
Centro di Studio per la Flsica
Odle Microonde (Ital^
Chesapeake Instrument Corp. ,
Shadyside, Md.
Chicago Midway Labs. , U. of
Chicago, 111.
Chicago U., Dl.
185
198
163
145
131
206
178
206
157
147
Cologne U. (West Gennan^
Columbia (J. School of
Engineering, New York ,
Connecticut U. , (Storrs).
Q>mell Aeronautical Lab. ',
Inc., Buffalo, N. Y.
Cornell U. , Ithaca, N. Y.
Crosby Labs. . Inc. ,
Syosset, N. Y.
Crown 2>llerbach Corp. . San
Leandro, Calif.
Drrid Taylor Model Basin.
Washington, D. C
Defense Metals Information
Center, Battelle Memorial
last, Columbus, Ohio
DUmond Ordnance Fuze
Wuhington, D. C
••4
149 661
152 490
152 105
152 262
171 181
152 212
152 201
150 392
150 833
171 147
152 679
171 156
Crysler Corp. , Detroit, Mich. 157 153 060
Coating and Chemical Lab. ,
Aberdeen Proving Gound,Md.
181
171033
143
152 476
164
220
152 253
152 474
185 152 444
Duke U. , Durham, N. C. 192
Eagle-Picher Research Labs. ,
Miami, Okla.
Eastman Kodak Co. .
Rochester, N. Y.
Educational Testing Service.
Princeton, N. ].
211
164
165
135
Electric Storage Battery Co. ,
Yanfley. Pa. 165
Electrical Engiiteering Research
Lab. , U. of Illinois. Urbana 189
214
Electrical Engineering Research
Lab. . U. of Texas, Austin 155
207
220
Electronic Communications,
Inc. , Tlmonium, Md.
Electronics Research Lab. ,
Northeastern U. , Boston,
Mass.
Electronics Research Lab. ,
Stanford U., Calif.
Electronics Research Lab. , U.
d California, Berkeley
1-3
152 069
149 705
149 702
152 229
148 293
149 697
148 290
152 561
148 710
152 158
152 159
149 060
208 152 524
185
148 715
165
153 381
165
220
149 734
152 562
149 735
217
148 682
Engelhard Industries. Inc.
210
148 690
Wast Newark, N. J.
Engineering Div. , Air Materiel
165
149 698
164
152 226
Command, Wright -Patterson
AFB. Ohio
158
147 374
1
176
152 794
Fairchild Aircraft and Missile
Div. , Hagerscown. Md.
158
152 494
il76
150 391
Fairchild Camera and Instniment
Corp.. Syosset, N. Y.
223
148 285
Feltman Research Labs. ,
198
161 219
Picatinny Arsenal, Dover,
161220
N.J.
160
152 079
161221
173
149 066
161 223
149 670
161 224
199
151 072-R
Florida State U. , Tallahassee
147
148 678
201
151094
148 679
217
161222
Forest Products Lab. ,
164
152 920
Madison. Wis.
182
148 727
211
152 918
171165
220
152 653
171 166
taarcm
Forest Produpts L«b. ,
Madiaon, Wlls. <can.)
Page
1S2
FB Number
171 167
171 166
Prankford Af senal,
Rilladelphi4, Pa.
Franklin Insc Lal». for Re-
search and Development,
Philadelphl4. Pa.
Free U. ol B^lln (Germany)
173 153 014
201
150
Frltz-H«ber*In8titut der Max-
Planck-Gesellachaft, BerUn-
Dahlem (Wtst Germany) 145
Fulmer ReMarch Inst. , Ltd.
(Gt. Brit.) I »1
Gas Dynamics Lab. , North-
western U.. Evanston, IlL 218
General Atomic, San Diego,
Calif. 177
General Electric Co. ,
Richland. Wash. 205
General Electric Co. .
Schenectady. R Y. 177
Getter al Electric Research Lab. ,
Scbenectadly. N^^Y^^ 211
General MiU*. Inc. .
MinneapoLls. Minn. 165
General Telephone and
Electronics Labs. , Inc. ,
Bayside. H Y. 211
Geophysical' Inst. , U. of
Alaska. College 155
Geophysics Corp. at America,
Boston, Mfss. 220
George WasUngton U. >
WMhiiigto<i, D. C ISS
144
1S7
Georgia Inst, of Tech. Engi-
neering Experiment
Station. Atianu
206
222
Goctingen Ul (West Germany) 221
152 074
152 563
152 218
152 261
152 443
171 184
152 283
152 145
149 063
150 803
152 434
148 668
148 983
149 062
152 232
171000
171001
171004
171002
171003
171005
166 152 231
148 287
148 288
Source
Hamburg Model Basin
(West Germany)
Harvard Coll. Observatory,
Cambridge, Mass.
Harvard Medical School,
Boston, Mass.
Harvard School ai Public Health,
Boston, Mass.
Harvard U. ,
Cambridge, Mass. '
Harvard U. Div. of Engineering
and Applied Physics,
Cambridge. Mass. 192
age
PB Numbsr
176
148 721
131
148 669
148 713
14^
152 264
177
153 005
140
185
186
150 966
152 372
152 373
152 374
Hebrew U. (Israel)
•■; 1 '
186
212
Hlller Aircraft Corp. . Palo
Alto, Calif.
Hofstra Coll. , Hen^stead,
N. Y.
Hug^s Aircraft Co. ,
Culver aty, Calif. 166
i 212
Human Factors Research, Inc. ,
Los Angeles, Calif. 136
Human Resources Research
Office, George Washington U.
Washington, D. C
Ollnois Inst, ol Tech. , Chicago
Illinois State Water Survey,
Urbana
Illinois U.. Urbana
144
145
199
142
147
199
203
212
Imperial Coll. of Science and
Tech. , London (Gt. Brit.)
1-4
149 627
152 439
152 440
152 441
152 442
152 490
152 539
Heidelberg U. (West Germany) 141
«
158 149 075
140 147 529
148 297
148 729
171 177
152 156
152 157
136 148 728
152 528
148 680
152 017
151 152 227
148 734
171 141
148 675
150 860
152 291
150 152 206
gonrce {
loqierlal Coll. of Science ^ad
TKh., London, (Gt. Brit.)
(con.)
tudustrial Test Lab. ,
niladelphla Naval Shipyard.
t
budtute for Advanced Sticly,
Princeton, N. J. i
Institute for Quantiutive
Research In Economics
and Management, Purdue
U., Lafayette, Ind.
«
Institute for System Research,
U. of Chicago, 111.
badtute of Aerophysics, U.
of Toronto (Canada)
Institute of Geophysics and
Planetary Physics, U. of
California, Los Angeles
badtute ol Mathematical
Sciences, New York U. , N. Y.
ha^tute of Optics, U. of
Rochester, N. Y.
JHdtute of Sutistics, U. of
North Carolina. Chapel Hill
Page PB Number
ISO 152 207
143
186
224
189
194
186
192
221
loMqibere Research Lab. ,
tamaylvania State U. ,
Umverslty Park
Iidtuto Nacional de Tecnica
Aaronautlca Esteban
Terradas (^Min)
Irttoto dl Fisica dellUnlver-
*i, Trieste (Italy^
179
204
taltuto Elettrotecnico Naziooale
■^Qillleo Ferraris" (Italy) 212
]>■•• Forrestal Research
C«er, Princeton, RJ.
■ Pkstoriza Associates,
• I Boston, Mass.
178
200
174
JitaarrQU U. , Qeveland, Ohio 206
f
153 010
152 491
152 125
171 144
148 694
221 152 174
148 691
152 445
148 295
215 149 070
186
148 683
148 692
187
148 684
'
148 687
148 696
222
148 686
148 695
155 150 668
152 502
152 420
152 451
152 154
149 068
152 429
152 150
I-S
Source
John Hopkins U. , Baltimore,
Md.
Page ra Number
166
187
194
Kansas State U. , Manhattan 209
Kansas U. . Lawrence
Labor atoi re Mediterraneen de
Recherches Thermody-
namlques (France)
UegeU. (Gelgium)
Lincoln Lab. , Mass. Inst, of
Tech., Lexington 136
166
167
174
Lockheed Aricraft Corp. ,
Sunnyvale, Calif.
Martin Co. , Baltimore,
Md.
Maryland U. , CoUege Park
1«7
190
207
212
218
223
131
174
179
180
190
192
194
200
208
148 714
148 693
148 677
148 712
148 716
144 149 065
195 152 504
1(7 152 438
152 542
150 605
150 604
152 241
152 467
150 797
150 798
152 063
150 793
148 281
150 602
150 795
152 465
152 468
152 637
152 638
152 301
150 596
153 251
150 800
150 974
148 703
148 697
148 698
148 699
149 652
148 298
148 701
148 702
152 377
152 378
148 700
Manchester U. (Gt. Brit.) 215 149 070
Marine Inst Physical Lab. ,
Scrlpps of Oceanograi^iy,
San Diego, Calif.
149 148 240
201 171 150
136
148 300
153
147 646
187
148 672
213
152 447
Source
KUryland U. ,
(coo.)
Page PB Number
College Park
Menon bsL J Pittsburgji. Pa.
Meteorologic Lab. , U. ct
miDOls, UPbana
Michelson Libe. , Naval
Ordnance Test Statioo,
China Lake), Calif.
Michigan U. , Ann Arbor
Michigan U. Research Inst. ,
Ann Arbor
Microwave fesearch Inst. ,
Polytechnic Inst, d
Brooklyn, R Y.
Reic
Midwest Reiearch Inst. .
Kansas a(y. Mo.
I *
MUanU. O^Y)
Minneaoca y. , Minneapolis
Minnesou V). School at
Veterinary Medicine,
St. Paul
Motorola
Calif.
1
Mpl of Elec
srl|ig, U. of
vaiaia,]
I, Inc. ,
Moore School of Electrical
Bngliieei-^^.
Pfcnnsyivaiiia, Philadelphia
Riverside.
215
Massachusetts Inat. of Tech. ,
Cambridge
Material Labi . New York
Naval Shipy^d, Brooklyn
Materials Research Lab. , U.
of California 213
151
218
209
151
209
195
167
215
143
195
148
154
152 179
152 214
152 448
171 183
149 656
152 427
152 076
152 227
148 681
171 179
195 149 672
Moiaic Wilson Observatory
Narmco Industries, Inc.,
San Diego. Calif.
National Bsreau of Standards,
Boulder, Colo.
167
191
158
168
131
159
155
168
221
148 980
148 984
152 365
152 364
152 349
171 162
144 152 503
148 676
148 291
139 152 850
153 236
152 989
152 384
152 385
152 302
153 259
151 361-2
161579
151 377-6
Source
National Bureau of Standards,
Warfiington, D. C.
National Cancer Inst. ,
Bethesda, Md.
National Cash Register Co. ,
Hawthorne, Calif,
National Research Council,
Washington, D. C.
National Research Labe. ,
Otuwa (Canada)
Page PB Number
Naval Civil Engineering Lab. ,
Port Hueneme, Calif.
NavalBngl nee ring Experiment
Sution, Annapolis, Md.
Naval Ordnance Test Sution,
China Lake, Calif.
Naval Personnel Research Field
Avtlvity, San Diego, Calif.
Naval Radiological Defense Lab.
San Francisco, Calif.
Naval Research Lab. ,
Waahington, D. C.
186
7D2
207
142
1
159
20O
218
181
180
191
134
\
Naval Training Device Center.
Port Washington, N. Y.
New Departure Dlv. . General
Motors Corps. , Bristol, Coon.
New York Sute Coll. of
Ceramics. Alfred U.
New York U. CoU. of Engl-
Bring , N. Y.
202
205
219
144
148
180
200
203
206
222
224
148 691
161584
152 570
152 520
148 724
152 780
152 786
152 832
152 785
152 784
171 182
153 254
152 345
152 121
153 253
152 795
171 185
161946
161 9«7
161966
161786
153 Oil
153 012
147 963
147 964
149 298
148 663
171 314
168
159
148
155
199
216
221
153 007
171 151
152 344
152 521
171154
148 722
152 391
Source
Iteometalllc Materials Lab. .
Wright Air Development
Dlv. , Wright-Patterson
AFB, Ohio
North American Aviation, Inc.
Los Angeles, Calif.
Nonh Carolina Sute Coll. , i
Raleigh ^
Northwestern Technological
bst , Evanston, Ql.
Page re Number
lao
195
205
224
Northwestern U. , Evanston, 111. 152
Notre Dame U. , Ind. 196
Noyes Chemical Lab. , U. of
Illinois, Urbana 210
Office of Defense Research and
Engineering, Washington, D. C. 174
Office of Naval Research,
Washington, D. C.
Office of Technical Services,
DtfL of Commerce,
Washington, D. C.
168
169
199
208
222
1-6
GUo Sute U. , Columbus
(Mo State U. Research
PouDdation, Columbus
Cklihoma State U. Research
Foundation, Stillwater
CUahoma U. Research InsL ,
Nonnan
(MoU. (Norway)
f^*>rdU. (Gt. Brit.)
Settle Semiconductors, Inc.,
W*«rClty, Calif.
134
140
213
216
223
109
213
Observatory, San
Dbp>. Calif.
171 136
171 135
171 143
148 196
152 387
148 521
152 094
161 535
(Rev. 1)
137 116 303S6
OTS SB-429
OTSSB-430
OTS SB-431
OTS SB-432
OTSSB-433
OTS SB-423
OTS SB-434
OTS SB-439
135 171 146
149 962
153 252
152 186
141 152 247
160 171 129
152 419
148 299
209 152 487
152 559
149 667
131 152 302
Source
Pennsalt Chemicals Corp. ,
Wyndmoor, Pa.
Pennsylvania Sute U. ,
University Park
Pennsylvania State U. Mineral
Industries Experiment
Sution, University Park
Pennsylvania U. , Biiladel|*ia
Pennsylvania U. School of
Medicine, Philadelphia
Perception and Conditioning
Lab. , Southern Illinois U. ,
Carbondale
Personnel Lab. , Wright Air
Development Div. , Lackland
AFB, Tex.
Rtotointerpreution, Inc.,
Annapolis, Md.
Physical Research Lab. , Space "
Tech. Labs. , Inc. , Los
Angeles, Calif.
Physical Science Lab. , New
Mexico Sute U. ,
University Parte
Pickard and Bums, Inc. ,
Needham, Mass.
PltuburghU. , Pa.
Page re Number
145
148
Plasmadyne Corp. ,
Sanu Ana, Calif.
Plastics Techincal Evaluation-
Center, Picatlnny Arsenal,
DowT, N. J. m
Polytechnic Inst, of Brooklyn.
N.Y. 196
Portsmoudi Naval Shipyard.
N. H.
Princeton U. , N. J.
150 485
152 091
140 148 726
156 152 249
148
149
188
152 127
148 976
148 685
139
156
152 849
150 217
137
152 389
152 390
134
137
150 790
152 798
152 272
153
152 303
216
152 034
169
148 717
i<9
148 982
30i
147 542
150 857
152 133
304 171 163
188
196
161948
1,52 245
152 432
149 149 056
152 545
148 673
152 739
1-7
psychological L«b«. . Carnegie j , .- ^o
test. oTreA. , PlttBburgh. Pa- 137 / 148 292
fBychof>hy«lckl Research Unit.
Mount Holy^ke Coll. . South
Hadley. iAam:
Ftertyo Rico U. ColL d
A^cultura and Mechanic
Arta. Mayaguez
Purdue Reseirch Faundadoo.
Lafayette. Ind.
Quartermaa^r Field Bvaluatloa
Agency, F^rt Lee, Va.
Quartermaater Research and
EBfJimenik Center.
Natick. MM*.
Itadiation Bdects Information
Center. Wttelle Memorial
Inst. . Colymbua, Ohio
Radio Corp., d America,
Lancaster, Pa.
lUmo-Wooldndge Corp. .
Loe Angeles, Calif.
Raytheon C^.. Newton>*ass.
Raytheon Ob. . Waltham, Maas.
KCA Service Ca , dierry
Hill. N. J,
Reaction Motors Dlv. , Thiokol
Chemical Corp. , Denville,
N. J. I
Remington Arms Co. , Inc.
Bxidgepoft, Cooa.
Renaselaer Polytechnic Inat. .
Troy. N.i Y.
137 150 887
156
188
205
152 471
152 543
149 674
181 171 153
205
153 258
m
152 560 ,
216
152 517
170
149 716
169
148 276
170
171 130
171 131
171 132
180
152 257
174
152 259
192
196
197
148 674
152 480
152 250
Republic A^latioo Corp. ,
Farmingjlale, N. Y.
Raaearch Lah. d Electrooica.
Maas. Uat. of Tech. .
r
Research Lab. of Physical
Electronics, Tufu U. ,
MedforcL Maas.
Rhlnelander Paper Co. . WU.
174
140
190
170
176
152 399
149 652
152 803
152 793
Source
Rice U. . Houston, Tex. ,
Robert A. Taft Saniury
Engineering Center.
Cincinnati, Ohio
Rochester U. School of
Medicine and Dentiatry, N. Y.
Rock laland Arsenal Lab. , HI.
Rome Air Development Center,
Crlffiss AFB, N. Y.
Page PB Numbar
152 430
176 152 064
143 148 277
179
201
143
153
170
209
161969
161 897
148 277
152 548
152 547
152 405
RomeU. Otaly)
Roeemount Aeronautical Labs. .
U. of Minnesou,
Minneapolis v ,.
St. Louis U. , Mo.
Saakatchewan U. . (Canada)
School of Aviation Medicine,
Brooka AFB, Tex,
142 152 534
Scientific Radio Products. Inc.
Loveland, Colo.
Short Bros, and Harland, Ltd.
(Gt. Brit.)
Solar Aricraft Co. . San
Diego. Calit
Southwest Research Inat. ,
San Antonio, Tex.
197
145
132
133
135
140
141
170
171
171 142
152 085
152 281
152 282
152 284
152 215
152 263
152 433
152 765
152 216
149 715
149 660
178 152 527
197 171 152
Space Sciences Lab. . General
Electric Co. , PhUadelphia. Pa. 132
I/O
150 321 SperUng Labs. , Arlington, Va. 143
160
Sperry Phoenix Co. , Ariz.
Springfield Armory, Mass.
Sunford Electronics Labs. ,
Stanford U., Calif.
Vj ;
144
208
132
156
152 464
152 622
148 294
152 230
152 39S
152 394
152 391
149 069
Sunford Reaearch Inst. ,
MenloPark, Calif.
151 149 7U
5«i£« 1 "i.
Stufbrd Research Inst. ,
Menlo Park. Calif, (con.)
SnnfordU. , Calif.
Stanley Thompson Labs. , '•
Columbus U. , New York '
Sttlma, Inc. , Stamford, Conn.
Stevens Inst, of Tech. ,
Hoboken. N. J.
Syracuse U. , N. Y.
Page PB Number
156
181
213
m
199
171
205
188
Systems Dynamic Analysis Div. ,
Wright Air Development Dlv. ,
Wright -Patterson AFB, Ohio 175
Systems Research Field Lab. ,
Johns Hoplins U. .
Jameatown, R. I.
Technische Hoogeschool.
Delft (Netherlands)
TBClmlsche Hochadiule,
MuBlch, (West Germany)
Tele-Dynamlca, Inc. ,
Philadelphia, Pa.
Tennessee U. , Knoxvllle
I A. andM. CoU..
College Sution
Theoretical Chemlatry Lab. ,
U. of Wiaconaln, Madison
Ttadwr Engineering Co. ,
Washington, D. a
171
141
197
151
137
151
149
183
I-t
I^BrtBoU. ataly)
Tte U. , Medford, Maas.
WksU. School of Medicine,
ioMOQ, Mass.
*Hwrsal Match Corp. ,
Sl Louis, Mo.
184
216
139
140
141
175
*twralty CoU. , Cork (Brie) 188
148 286
153 008
148 671
149 064
149 152 488
152 147
152513
149 714
149 717
171 180
153 006
152 532
152 492
150 388
152 271
t52 569
161 408S-I
171 169
171 170
171 171
171 172
171 173
171 174
171 175
171 176
152 481
152 853
152 851
152 531
152 852
171 157
149 073
Source
Page
PB Number
University of Southern
California, Loa Alleles
135
152 164
152 165
University of Southern
California. Engineering
Center, Los Angeles
192
197
210
152 551
152 550
152 549
UppaalaU. (SwedeiO
i . J
. ! .
1
132
133
188
214
152 204
152 209
152 210
152 211
152 205
152 452
152 453
152 454
152 455
UtahU.. Salt Lake City
175
149 071
152 380
152 381
Vienna Inat. of Tech. (Austria)
160
152 437
Vienna U. (Austrli^
204
152 482
Washlngtoo U. . St. T,ouis. Mo.
188
152 396
Washington U. , SeatUe
138
147 642
153
188
152 166
152 168
152 148
152 149
152 167
Washington U. . Seattle. Dlv. at
Counseling and Testing
Services 199
191
224
147 643
148 608
148 732
mw
148 735
148 723
Wayne State U. , Detroit, Mich.
189
148 719
Weizmann InaL of Science
(larael)
217
152 483
152 493
Western Development I .aha. ,
PWlco Corp. , Palo Alto.
Calif.
171
153 256
Western Electric Co. . WInsrrm
Salem. N. C.
171
153 380
WesHnghouse Electric Ccrp. ,
Baltimore. Md.
171
172
JOS
152 219
148 283
152 411
Westlnjdxxise Electric Corp. .
Bast Rttaburgh. Pa.
214
148 981
Westinghouse Research T Jha. ,
Pittsburgh. P».
172
152 348
Willow Run Labs. . U. of
Michigan. Ann Arbor
222
149 673
Wiaconaln U. . Madisoa
208
149 909
1-9
I.I
r
y -•.. ^A i
f:, !%■»"'.■ 1<
- <
SUBJEa INDEX
tuWect 1 1 '' '
Page
FB Number
Subject
Page
PB Number
AklMian
131
152 212
Airplane noise
s
194
148 720
--Analysis
140
192 263
Al^adoo materials
157
171 147
Airplanes
Acceleration >
--Control systems
159
152 786
— Testing equipment
172
171 134
Alg^ra
Accelerators
--Applications
213
152 447
"Parformance
178
152 622
--Theory
186
152 441
Acetates
Alkali metal halide crystals
-Metabolism
141
152 531
--Crystal structure
213
152 427
Achievement tests
--Luminescence
212
152 451
"Reliability
138
147 642
Alkali metals
ACOB
173
171 137
--Atomic structure
216
148 722
Acoustic impedance
AUoys
— Mathematical analysis
206
147 964
--Crystal structure
212
150 596
149 298
—Diffusion
199
148 675
150 833
--Stresses •-
201
152 169
Aooastlc materials
Altimeters
— Derelopment
178
150 392
--Applications
149
152 042
Acoustic nerve
Aluminum alloys
--Surgery
139
152 766
- -Creep
197
171 152
Acoustic waveguides
--Fatigue
200
152 785
"Mathematical analysis
192
149 627
--Temperature factors
200
152 7415
AAesives
Aluminum-chormium -titanium
—seres ses
192
148 298
alloys
Aerial photography
--nutse studies
199
171 154
--Military requirements
153
152 303
Aluminum crystals
Aerial recomiaissance
--Deformation *'
aoi
171 ISO
— Effectiveness
153
152 303
Aluminum oxides
AerobeeHl
169
148 717
--Chemical effects
173
149 670
Aerodynamic heating
194
148 701
148 702
Aluminum -titanium -vanadium
alloys
'- Countermeasures
157
171 147
--Phase studies
199
171 154
160
153 257
Amides
194
148 720
--Hydrolysis
210
152 094
Air
--Resonance
210
152 094
•-Contaminatlaa
176
152 064
Amines
-Heatii«
195
149 672
--Determination
144
149 065
Air force equipment
--Oxidation
149
148 976
"ScheduUng
162
153 067
--Toxic effects
143
152 476
Air IntBlllgence
Ammino compounds
•'bstrumentatioD
153
152 015
--Thermal properties
148
152 091
Air traffic coatrd systems
Anmionia
"Communication systema
170
171 130
171 131
--Applications
Anunmium carbonate
164
149 702
171 132
--Hydrolysis
141
152 247
"Test results
157
148 708
Ammonium ions
Aircraft
--Exchange reactions
149
148 678
—Aerodynamic
Anunonium perchlorate
characteristics
195
171 135
--Combustion
179
148 698
-Ooacrol systems
160
152 230
180
148 699
"Sttbllity
195
171 135
Analytic functions
X3
Aircraft tires
--Theory
184
148 978
"Test results
158
152 494
»>
186
152 374
Airframes
Anemometers
*-Oevelopment
157
152 343
--Sensitivity
194
148 677
"Materials
179
171 148
Anodes<Electrolytlc cell)
199
151 072-R
--Coatings
149
149 056
"TMBperature factors
159
171 151
Antenna radiation patterns
AlrpUoe landings
--Measurement
162
152 990
-Bqidprneot
156
152 384
168
161579
Ml
Subject
Page PB Number
Antenna radladon pattenis(can. )
- -Sutistlcal, analysis 166
--Synthesis
--Design
--Focusing
--Materials
AntlfrictloD bearings
Approximate compuutioo
Aptitude testt
--BffBCtlt«*ess
--Sutistlcal analysis
Astronomical cameras
--Design
AstrophyslcJ
Atmosphere |
--Absorptive properties
--Conamlnatlon
—Light transmission
—Mathematical ani ysls
—Meteorology
—Moisture content
--Motion I
•-Optical properties
—Reflective effects
—Temperature
—Turbulence
Atomspherlc refraction
— Melsureipent
—Meteorological factors
AtmospherlcB
--Analysis!
--Electromagnetic effects
--Recording devices
Atomic structiire
--Mathemaitical analysis
Attention
— Fhysldofical factors
Attitudes
--Measurement
--Psychological factors
Auditory acuity
--Measurement
Auditory perception
--Test methods
Auditory thnMholds
--Measurement
Aurorae
--Reflectite effects
•-Spectra
Automau
Automated msintensDce
Automatic pilou
--Design
Aviation personnel
—Attitude*
--Qasslflcsrion
166
219
161
162
166
206
166
171
159
184
185
<34
135
137
223
131
156
205
158
156
151
154
156
154
154
155
155
220
155
221
221
156
216
136
137
137
139
136
140
156
132
222
173
Subject
Avlstion persoonel (con. )
--Clothing
--Test methods
Axlally symmetric flow
--Analysis
Badnrard-wave ampllflers
--Devielopment
Ball bearings
—Friction
--Lubrication
■, BaUlstics
\ -Test facilities I
Banach spaces
Band-paas filters
--Development
Band structure
Batteries
--Development
Beama
--Creep ,
--Deformation '
BearlligB
--Materials
Beryllium
--Bibliography
--Fracture
Bibliography
--Beryllium
•-Cathode ray tubes
--Ferroelectric materials
- -Ferroelectrldty
- -Ferroougnetism
149 060
148 710 --Group dynamlca
—Machine translations
152 174 ' — Ottlce at Naval Research.
152 174 Washington, D. C.
149 069 •-Oscillators
--Physiological psychology
148 722 •-Powder metallurgy
•-Radiation damage
152 157 — Radioblology
--Remote control systeoas
152 271 --Resistors
148 292 --Rocket propulsion
^ --Scientific reports
152 766 —Scientific research
•-Thermionic emission
148 728 —Thermistors
- -Tliermocouples
147 529 -•Thermoelectricity
--Thermopiles
148 286 .•-Trsnsistors
152 281 -Vigilance
152 282 Binary diagrams
149 673 Biology
J71 137 --Instrumentation .^.
Black gum boards
Blast tubes
Blood chemistry
152 271 Blood circulation
152 798 --Temperature factors
1-12
Page PB Number
148 729
148 297
152 242
149 059
148 709
161 579
152 201
148 729
152 219
171 151
148 7v;
152 372
152 373
152 798
148 293
152 272
148 299
152 302
150 217
152 283
152 384
152 249
152 227
149 061
152 249
152 552
152 553
148 710
152 521
160 152 230
137
134
181
205
134
194
165
159
159
173
186
167
212
ov
161
161
173
200
200
20O
168
208
208
189
208
135
222
137
189
137
199
205
143
143
166
177
131
177
166
I6i
168
168
168
169
136
199
lt9
Its
Ul
143
171 153
171 143
150 790
148 701
152 562
171 151
171 151
152 435
152 440
148 984
150 596
164 149 702
171 149
171 149
153 014
152 3n
1^2 378
152 377
152 3n
152 378
OTSSB-431
OTSSB-434
0TSSB-4M
152 213
OTSSB-434
150 SOO
0TSSB-4SI
116 30381
152 213
116 30381
orrsa-48
149 714
152 349
153 059
OTSSB-41
171 184
148 703
171 184
OTSS8-4SI
OTSSB-41
OTSSB-41
OTSSB-48
0TSSB-4»
0TSSB-4SJ
152 157
171 154
148 290
171 171
161948
171 160
139 152 850
I
Subject
Huntbody
Bodies of revolution
--Boundary layer
—Heat transfer
—Transonic characteristics
Bolli
••Corrosion prevention .
Bonding j
--Theory '' u
Boroo compounds (Organici
—Chemical reactions -
—Synthesis
Boundary layer
—Heat transfer
—Thickness
—Turbulence
Boussinesq s problem
Brtln
--Bnzymes
— Physiology
Brass
- -Deforms tion
Breathing masks
"Effectiveness
Bums
—Pathology
Camera shutters
"Design
Cmeras
"Equipment
Cqwdtors
— Insulation
"Production
CarUdes
—Phase studies
Qubohydrates
-Metabolism
Carbonic anhydrase
"Phyalological effects
CirgD
"Handling
-Transportation
Gualysts
"Applications
—Surfaces
Cathode ray tubes
"Bibliography
Cuhodes (Electron tubes)
"Materials
Cwchy problem
Cwity resonators
"Development
C«n»entiie structures
Cerebral cortex
"Stimulation
Cerenkov radiation
Q»pman-Ferraro problem
(¥rley
Oibysbev inequalities
Page PB Number
193 147 878
196 152 245
193 147 878
194 148 701
148 702
152 413
194
201
148
161 897
148 726
145 152 085
145 152 085
196 152 739
193 152 758
193 147 878
196 148 521
192 152 069
141 152 264
142 152 534
201 152 261
144 161 946
142 152 366
152 367
223 148 299
223 152 567
203 148 979
171 153 380
214
140
140
152 454
152 851
152 433
139 152 112
153 147 646
165 149 698
148 152 344
168 OTS SB-431
308 152 538
18S 148 670
187 148 672
X ' Subject
^Chentical impurities
^ --Determination
Chemical reactions
--Msthematical analysis
Chemistry
Chromscographic analysis
--Applications
Chromium -iron aUoys
--Oxidation
Chromium plating
Chronographs
--Design
Classification statistic
Qothing
--Flreproofing
Clouds
--Meteorological factors
Coanda effect
Collision cross sections
Color film
--Applications
Color photographs
--Identification
Colored flares
--Development
Colors
--Standards
Combinatorial analysis
Combustion
--Heat transfer
--Theory
Combustion chambers
—Design
Commerce
--Borneo
--Economic aspects
--Geographical factors
Complex compounds
--Chemical reactions
Complex variables
Computational chains
Conftrmal mapping
Conical bodies
--Aerodynamic
characteristics
Containers
--Military requirements
Control systems
-"-Development
--Mathematical analysis
- -Perfoi luanoe
--Synthesis
165 153 381 Convex bodies
167 152 241 -Theory
214 152 454 Convex sets
Copper
142 152 540 -Defbrmation
167 152 365 --Phase studies
155 ISO 668 Copper alloys
153 1^ 149 --Resonance
185 1S2 161 Copper wire
—Test results
1-13
Page FB Number
144 161 946
149 161 408 S-1
144 171 001
181 171 033
200 149 068
144 152 393
174 150 798
184 152 162
180 171 136
151 152 448
158 147 374
204 171 163
159 152 303
153 152 303
160 152 079
181 171 153
187 148 696
180 148 699
179 152 502
178 152 154
154 148 291
224 152 125
153 147 646
144 152 503
184 148 978
186 152 442
189 152 519
186 152 374
193 152 260
182 148 727
160
163
164
164
163
152 230
147 651
149 136
152 253
152 253
147 651
149 136
186 152 440
185 152 161
201 152 261
199 152 017
198 152 105
199 152 147
Subject
Comer array
Correlatloo fiyictloas
— AppUcation*
— DetermliuKloa
Corrosion Intibltors
--Derelopm^nt
Cosmic radiation
—Geophysioal facmra
-kUttamuttcal analysis
1 tunnel
Page
162
215
189
201
132
133
132
133
Coamic wind
Couette flow
Creeping columns
Crystal fabric
Cryatal oscillators
--Design
Crystal stnidture
--Analysis
--Mathematical analysis
--X-ray analysis
Crystal units
--Development
Crystals
--Spectra
--Vibraiiod
Cybernetics
Cyclic compounds
- -Decompoeltion
Cylinders
--Bectromagnetlc effects
--Supersonic characteristics
Cylindrical chaff
Cylindrical f hells
--Creep
--Theory
Dance
Data
—Coding
— Process jng
--Punched card methods
Dau storage systems
--Development
--Theory
Data transmission systems
--Coding
--Development
--Errors
Delay lines
--Applicacioos
--Development
--Processing
Detonation waves
--Propagation
Diachromo4cope
195
192
161
153
FB Number
148 709
149 070
147 643
148 608
161 897
152 204
152 209
152 210
152 211
152 204
152 209
152 210
152 211
152 504
152 551
171 149
152 148
163 149 719
213
213
210
213
213
191
219
195
ISO
197
192
170
187
191
224
123
223
222
151
190
222
170
170
107
217
153
152 427
152 447
152 469
170 149 715
152 447
152 447
152 989
147 171 156
148 296
171 179
152 196
171 152
149 627
171 130
171 131
171 132
150 793
148 732
148 733
148 734
148 723
148 285
148 977
148 686
150 388
152 465
148 686
152 547
152 547
150 604
152 484
152 303
Subject
Dielectric films
--Preparation
Dielectrics
--Physical effects
Diesel engines
--Lubrication
Difference equations
Differential equations
--Theory t
Page FB Number
171 153 380
208 152 524
r ..'.
Differential inequalities
Diffraction
--Mathematical analysis
Diffusion
--Madiematlcal analysis
—Measurement
Diodes
--Applications
--Development , '
Dlpole antennas
--Electromagnetic properties
Dlpropargyl ether
--Toxit effects
Dlrsc's noutions
Direction finders (RF)
--Development
Direction finding antennas
--Design
Disks
--Radiation
Displacement measuremenu
Display systems
--Design
--Development
Diversity reception
--Applications
Documentation
--Theory
Douglas fir boards
Douglas fir laminates
Drops
--Combustian
Dynamic system synthesizer
Dysprosium isotopes
--Resonance
Earth
--Radiation
Bartii models
— Applications
Economic conditions ,
—Analysis
—Mathematical analysis
Education
--Sociological factors
Ekki boards
180
1S7
197
215
186
188
114
221
148
211
199
212
172
163
213
161
I-U
153 254
150 793
152 492
149 070
152 441
152 442
152 491
152 438
149 073
152 491
143
166
171
172
•-■»
906
208
153
172
190
164
223
183
184
177
179
189
212
202
153
224
223
135
183
152 546
152 502
171 144
152 450
152 639
152015
148 196
152 016
148 293
171172
Subject
Baitlc shells
—Sandwich construction
—Theory
Elasticity
— Mathenutlcal analysis
Elastomers
--Temperature factors
Electric accelerators
Electric detonators
"Effects of radiation j
Electric discharges
—Analysis
—Applications
Page raNimiber
148 295
Electric filters
-Synthesis
148 676
Electrical double layer
149 063
—Measurement
148 675
Electrical energy
152 291
—Applications
"Sources
152 348
Electrical networks !
149 720
—Mathematical analysis
149 667
—Synthesis
148 705
Etectroca rdlography
148 294
Electrochemistry
148 714
Electrodes
—Adsorptlve properties
153 256
.
Elactromagnetlc fields
149 058
"Mathematical analysis
149 298
152 394
"Tlisory
ESectromagnetic theory '
152 015
148 706
Electromagnetic waves
>152 468
"Absorption
152 226
— DUfractlon j
148 977
171 IW
—Physiological effects
171 173
171 176
-Scaoerlng
-Tranamlaslon
Bectroa accelerators
—Design
Blactron bombardment
-AppUcatlaaa
-Blsctrical effects
192
192
192
179
197
213
211
148 298
149 627
148 725
152 069
161969
171 138
172 152 991
216 152 034
195 149 672
197 152 550
198 161 220
172 148 283
147 171 141
198 161 220
197 171 138
172 148 283
163 152 262
167 148 980
190 149 652
139 171 140
147 171 141
147 171 141
148 15^ 127
219 148 296
153 255
220 152 474
215 149 070
219 153 255
221 148 295
221 148 287
148 288
215 152 364
219 148 296
221 148 295
145 152 349
208 152 524
220 149 060
152 232
152 474
221 152 174
219 152 242
152 258
153 255
220 149 735
221 148 287
148 288
148 295
197 171 138
148 671
152 918
Subject
Page
n Number
Electron capture
--Mathematical analysis
204
147 542
•-Measurement
204
150 857 .
152 133 ^
Electron gas
--Mathematical analysis
216
148 722
- -Properties
215
152 179
Electron microscopy
--Applications
201
152 261
Electron tubes
--Development
166
150 605
—Effects of radiation
205
149 714
--Materials
169
152 560
205
149 714
Electronic equipment
- -Countermeasures
162
153 067
--Design
165
150 803
--Development
165
149 734
--Effects of radiation
205
153 258
—Human engineering
168
153 007
•-Maintenance
135
152 165
'
162
148 284
173
171 137
--Parts catalogs
162
153 067
--Production
165
150 803
--Standards
165
150 803
--Testing equipment
162
148 284
Electronic equlpment(Alrbome)
--Shock resistance
161
153 260
--Test methods
161
153 260
Electronics
--Theory
208
148 700
Electrons
-Energy
216
152 481
--Bxclution
215
152 179
--ScJitterlng
215
152 179
216
152 481
Electrophotography
--Api^cations
151
150 388
Electrosutic display system
190
152 468
Emlsslvlty
217
161 222
Endfire array
161
148 705
Engineering
157
171004
Equations of state
218
152 443
Erythrocytes
--Absorptive properties
143
171 160
Ethyl acetate
--Sound transmlsalon
206
152 ISO
Euler's conjecture
187
148 687
Europium
--Optical properties
V3
152 411
Evaporators
--Design
160
171145
Exchange reactions
—Velocity
147
148 678
148 679
Exhaust flamea
- -^pectrographlc analysis
180
152 257
Exhaust nozzles
—Pressure distribution
178
152 154
Experiment Luxembourg
155
149 062
Experimental dau
--Statistical analysis
222
148 695
Explosive charges
198
161221
M5
Subject
BxploalTe forming
Bxpoaure '
- -Physi(doglc4l effecu
Bxtra-cerre«trMl radio wavea
--Refractlaii ,
F2 critical fre^ucndea
F-IOOF
Facalmlle comtnunlcatiaa
syatema
--Equipment
Factor uialysl^
--AppUcadooB
Faraday effect
Fatigue (RiyslQlogy)
--MeaaurenMnt ,
Fatty adda
— Btochemlcal effecta
Ferritet
--Magnedc properties
--Wave traninlaalon
Ferroelectric tnaterials
--Bibliography
Ferromagnetic materiala
--Diffusion
--Optical properties
--Resonance
Ferronoagnetl^m
— Bibliograptiy
Fin-staUllzed rocketa
--Design
, Fire control e^pcnent
--Design
Fire resistant coatings
— BftectlTen«sa
Fire resistant paints
— Effectiveness
Fission fragments
--Diffusion
Flsme velocitlBS
— FhocograptHc analysis
Flicker fuslooj frequency
Fluid flow
—Analysis '
--Mathematical analyals
--Viscosity
Flying platforms
--Development
Foams
--Materials
Food J
--Contatoers
Fourier aeries
--Applications
Free radicala
— C3iecpical reactiooa
"Hyperflne structure
--Productlan
Friction
- -Testing e^ultment
Frogs
—Physiology
m
141
156
155
195
PB Number Subject
161 220 F»»*l filters
161 221 --Porosity
Fuels
152 850 --Effects ot radiation
152 531 --Stability
Functions
152 471 --Applications
151 361-2 -Theory
171 135
Page PB Number
180 161 966
164
188
134
138
208
139
140
214
220
220
208 errs SB-434
152 226 Fuaion power generation
152 167 Gamma radiation
150 790 --Chemical effects
152 168 --Scattering '
149 909 Garnets
--Resonance
152 112 --Spectrographic analyals
Gaa bearings
152 851 —Performance
Gas chromatography
148 981 Gab diffusion
152 653 --Mathematical analysis
152 653 --Measurement
--Temperature factors
Gas discharges
--Electrical propertiea
212 152 291 Gaa How
214 148 981 -Analysis
220 152 653 ^ ,
> --Magnetic factors '
189 152 213 --Oscillation
208 errs SB-434 V "Viscosity . Ij
I Gaa ionization
175 171 180 -Analysis
--Magnetic factora
173 153 014 --Mathematical analysis
— Measurement
181 171 182 -Theory
Gaa turbines
181 171 182 --Fuel consumpdoa
Gaseous electronics
205 152 283 Gaaea
I —Chemical reactions
217 152 484 —Density
140 153 252 —Detonation
--Heating
194 148 702 - -Thermodynamic properties
192 152 445 Geogrsphy
192 152 163 -Borneo
Geomagnetic mlcropulsatlooa
158 149 075
179 171 178 Geophysics
Germaidum crystals .
176 152 793 -Conductivity
184 148 707 GUders
188 149 073 -Alaska
--Greenland
177 171 184 <aass
149 152 488 -Bonding
149 148 976 Glass textiles
—Applications
192 148 674 —Costings
Gtoves
140 152 399 "Test naethods
M6
205
153 258
180
161966
186
148 691
184
148 707
185
152 372
152 444
188
152 430
216
152 517
147
171 156
202
161 584
212
214
175
181
210
146
146
194
196
192
178
196
194
210
204
216
218
178
214
196
194
217
195
218
154
207
206
211
190
1S2
171
171
152 4S0
148 981
171 157
171033
152 549
150 781
150 781
209 152 487
148 694
152 480
152 551
152 154
148 673
152 426
152 549
152 420
152 034
152 443
152 527
152 561
152 480
152 426
152 484
149 672
152 443
148 291
152 158
152 159
152 208
171003
152 918
152 290
152 387
19? 153 259
152 219
152 219
149 674
ect
Page PB Number
Graphite electrodes
Gravimetric analysis
--Applications
Gravity
--niysical effects
Green Glow
Group dynamics |
--Bibliography
.--Sociological factors
Groups (Mathematics)
--Theory
Gyroscopes
•-Design I
Hail
--Physical propertier
Hall effect
Harbors
--Louisiana
Hardware Items
Harmonic analysis
--Errors
Harmonic functions
•-Applications
"Theory
Heanbeat
--Measurement
Heat exchangers
"Deaign
Heat production (Biology)
--Measurement
Hsat resisunt alloys
-Metallurgy
Heat tolerance
—Determination
Heat transfer
--Mathematical analysii
--Measurement
Helicopter engines
--Development
Helicopters
"Control systems
•-Operation
Helium (Liquid)
--Cooling
"Production
Hemopoiesis
Heptadiyne
:--Taxic effects
Hickory boards
High altitude
--Riysiological effects
Wgb frequency discharges
< —Analysis '
Wfh speed cameras {
"Control systems
High temperature research
••Equipment
Homeostats \
Houbot
NBnidity
"Physiological effects ,
T
144
m
137
135
135
188
175
ISO
209
153
201
209
188
185
185
139
218
139
198
138
196
218
218
160
133
218
218
143
143
183
139
140
223
218
217
189
193
195
138
153
171 129
152 393
148 697
152 569
148 292
ISO 500
148 293
148 685
171 157
152 207
152 405
147 646
161 897
152 487
152 205
152 373
149 661
171 140
152 784
152 849
161 223
152 428
152 739
152 784
171 183
178 152 527
152 230
171 139
150 800
ISO 800
171 160
148 294
171 171
171 140
152 765
209 152 487
ISO 974
171 183
152 472
152 202
152 555
149 672
152 428
152 149
Subject
Hydrazine derivatives
--Oxidation
Hydrocarbons
--Crystal structure
--Ignition
--Molecular structure
Hydrogen
--Adsorption
--Determination
--Electron transitions
--Neutron cross sections
--Proton cross sections
Hydroxyl radicals
--Chemical reactions
--^)ectra
Hyperbolic equations
- -Theory
Hypersonic flow
—Heat transfer
--Mathematical analysis
Hypersonic wind tunnels
--Design
--Development
--Equipment
Hypervelocity guns^
—Development
--Performance
Hypervelocity projectiles
--Launching
--Penetration
Hypervelocity vehicles
--Cooling
--Materials
Hypotiialamus
- -Physiology
Hypothermia
--Physiological effects
Ice
--Antarctic regions
--Arctic regions
--Deformation
--Temperature factors
--Testing equipment
--Wave transmission
Ice augers
- -Applications
Image furnaces
Impact shock
--Analysis
Industrial equipment
--Development
Industrial production
--Economic aspects
--Scheduling
Inertial guidance systems
--Design
Page PB Number
149 148 976
145
148
148
148
149
204
204
204
146
146
196
193
194
196
173
195
197
193
195
175
173
173
175
160
157
151
152
151
152
153
152
146
152
151
152
217
197
165
223
177
171 181
161 967
161 967
152 127
149 056
147 542
171 163
150 857
152 133
148 289
148 289
187 152 438
152 739
152 260
152 420
148 673
152 435
152 504
171 142
152 555
149 672
149 071
152 554
152 554
152 380
152 381
153 257
171 147
140 150 966
139 152 953
152 566
152 388
152 568
152 456
152 149
152 457
148 289
152 388
152 568
152 388
152 472
171 138
ISO 803
152 016
149 074
175 171 157
1-17
4
«
Subject
bf ormatlcB thaory
--Application^
Infrared apectrta
--Analyaia
Page PB Number
Infrared
- -Transmlaslon
Insulating matarlala
Integral equations
--AppUcationa
—Theory
Interferometerti
--Application^
--Design
Intermetallic ctxnpounds
--Electron transitions
International Geophysical year
lonoehpere
--Arctic regipns
—Electromagnetic properties
--Motion I
--Reflective Effects
--Wave transmission
Iridium compounds
--Chemical neactions
Iron
--Purlfi cation
Iron isotopes (Radioactive)
--Metabolism
Iron-niclcel alloys
- - Klecirodeposi tion
Iron-vanadium, alloys
--Diffusion i
Jackson polynomial
Jenny
Jet mixing floiM
—Mathematical analysis
--Supersonic: characteristics
Jet plane noise
--Physiologiaal effects
Jets
--Control .
- -Deflectldii
Jordan arc
Journal bearings
--Hydrodyna<riic
characteristics
--Performance
Junior
Kolmogorov teet
Ketones
--Effects of radiation
Kidneys
-Test resuli a
187
222
190
209
156
181
192
187
156
197
209
221
155
155
156
156
155
155
144
201
143
207
212
185
189
196
197
195
195
159
185
177
177
189
186
182
183
148 696
148 686
149 673
150 602
148 712
148 716
152 076
150 217
161 948
148 725
148 693
152 471
152 550
152 405
151 377-6
148 668
148 668
148 983
149 062
149 069/
152 471
148 668
151 361-2
152 503
152 074
171 160
152 520
152 291
152 444
152 202
152 432
152 250
171 179
140 152 263
171 179
152 786
152 372
152 145
152 145
171 144
148 692
147 171 156
142 152 366
171 165
171 166
171 174
Subject
Laminates (con. )
--Test results (con.)
Lanchester theory .
Landing gear
--Design
Laplace integrals
Latin squares
Leadership
Leakage detectors
--Design
Learning
--Measurement
--Psychological factors
--Statistical analysis
--Test results
Lebesgue theorem
Light
--Scattering
Light ranging systems
--Design
Lindberg gyroscope principle
Linear equations
--Applications
--Theory
Lipids
--Metabolism
Liquid rocket propellants
--Combustion
--Heat transfer
--Test results
Liquids
--Atomization
Lithium hydroxides
--Spectra
Lithium hydipxides-d
--Spectra (
Lithium iodicK crystals
--Physical properties
Lithium ions
--Diffusion
Liver
--Biochemistry
--Physiology
Logarithmic instruments
--Design
Lor an ^
--Applications
--Errors
Lubricants
--Effects of radiation
--Physical effects
Machine translaticms
--Bibliography ,
Magnesium '
--Combustion
Magnesium crystals
--Deformation
--Fractiure
Magnesium oxide crystals
- - Bombardment
Magnetic cores
--Applications
Page PB Number
184
185
158
185
187
137
140
141
153
153
205
180
222
173
213
213
213
190
171 175
171 176
148 715
152 494
152 490
148 687
148 292
205 149 674
135 171 146
136 148 300
134 149 962
136 148 728
188 152 430
152 552
152 384
171 157
9
150 793
152 160
148 672
141 152 852
179 152 502
181 161 948
159 153 280
177 152 546
209 152 076
a09 152 076
202 153 253
203 152 411
211 149 063
152 851
152 531
168 152 385
152 548
152 548
153 258
153 254
OTS SB-439
149 670
149 656
149 656
148 671
152 637
1-18
Subject
Magnetic cores (con. )
--Materials
Magnedc fields
--Detection
Electromagnetic effects
--Measurement
• -Physical effects
--Theory
Magnedc materials
- -Spectrographlc analysis
Magnetic recording systems
--Applications
Magnetic resonance
--Analysis
--Applications
--Measurement
--Theory
Magneto- hydrodynamic waves
--Mathematical anlaysis
Magneto-optic rotation
--Measurement
Magnetogasdynamics
Magnetometers
--Design t
Magnetrons
--Development
Maintenance equipment
--Development
Maintenance personnel
--Training
--Training devices
Many particle systems
Markers
--Deterioration
Markov chains
Maser
Mass spectrometers
--AppU cations
Materials
--Heat transfer
—Mechanical properties
Mathenutical computer data
--Coding
-Processing
—Punched card method
Mathematical computera
--Ai^ cations
"Circuits
-Design
—Development
—Equipment
Page re Number
152 394
52 301
52 760
52 394
52 551
52 034
53 251
48 710
52 488
48 679
48 678
52 105
52 094
52 450
52 105
49 067
52 419
52 445
49 909
52 549
52 301
52 228
48 276
71 137
71 137
52 165
52 493
48 727
49 717
49 720
52 679
71005
71 147
50 392
52 468
52 638
52 345
52 202
50 795
52 989
48 735
52 164
48 711
52 555
48 723
49 652
48 290
48 281
50 602
52 520
52 213
ao7
210
208
192
216
212
155
149
147
149
198
210
212
198
214
216
192
208
210
207
162
169
173
173
135
217
182
188
163
147
222
157
178
190
191
189
190
191
191
135
162
193
224
190
189
190
190
207
Subject
Page
re Number
Mathematical computers (con. )
--Equipment (con.)
190
152 468
152 637
--Errors
190
152 465
--Performance
189
171 144
—Scheduling
189
147 643
148 608
191
148 732
148 733
148 734
148 735
222
149 673
—Theory
189
152 519
Mathematical logic
--Applications
190
149 652
222
149 673
Mathematics
222
171005
Matrix algebra
187
148 687
--Applications
172
148 283
188
152 167
1
191
148 732
148 733
Mattresses
--Materials
143
153 010
Measure theory
188
152 430
Medical research
138
171000
- - Instrumenution
189
148 290
Mesometeorological analysis
151
152 227
Mesons
--Determination
133
152 210
--Nuclear reactions
204
152 482
--Scattering
202
152 424
Metabolism
--Pathology
142
152 367
Metal borides
--Crystal structure
214
152 453
152 454
152 455
Metal carbides
--Chemical reactions
144
152 528
Metal films ^
- -Production
171
149 660
--Resistivity
171
149 660
Metal -glass adhesives
--Applications
159
153 259
Metallic soaps
--Production
201
171 150
Metalorganlc compounds
--Polymerization
145
150 485
Metals
--Corrosion
148
152 127
--Creep
199
152 147
--Deformation
201
171 150
—Diffusion
199
148 675
--Effects of radiation
205
153 258
--Electron transitions
215
152 179
--Mechanical properties
201
171 150
- -Micros true ture
201
152 074
--Processing
198
161 220
161221
--Purification
201
152 074
—Surface properties
199
152 147
--Surfaces
201
171 150
--Thermal properties
218
171 183
219
171 185
M9
Subject
Meteorites
--SimulatiaB
Meteorological jchart*
--Analysi*
— Application*
--Production ,
Meoeorologlcall dau
— TaUes
--Theoretical corrections
Meteorological instruments
--Calibration!
Meteorologlcall radar
--ApplicatlomiB
Meteorology
--Alaska
Meteors
—Atmosphere entry
--Velocity j
Methyl amine^
--Bichange reactions
Michigan
MicrtMneteorology
- - Instrumentation
--Washingto^i
Microscopes
--Developmtnt
Mic ro8pectro^hoton»eter 8
--Design
Microwave amplifier »
- -Development
Microwave equipment
--Design
--Devclopmrnt
!
--Testing e^juipment
Microwave optics
--Theory
Mlcrowavw
--Physiological effects
--Propagatipo
MIL-C14157I
Military equipment
--Directories
Military
resiardi
MUiury sup|dies
--Storage
Miliary training
--Psychological factors
Miniature electron tubes
--Development
Missile trajectories
— Recording devices
MiasUes
—Equipment
—Guidance systems
175
ISO
155
151
154
149
149
ISO
PB Number
152 380
152 381
152 563
151 361-2
ISO 388
149 061
152 042
\
152 042
152 206
152 207
150 152 290
131
131
147
222
153
151
152 212
152 212
148 679
149 673
152 148
152 149
152 569
209 148 681
209 148 681
163 149 720
197
165
214
167
165
219
206
143
220
203
174
138
144
157
ao6
2)6
222
182
134
169
152 550
149 734
152 561
152 241
149 734
153 255
152 201
148 277
152 653
148 979
161 535
(Rev. 1)
171000
171001
171004
171002
171003
171005
148 727
149 962
148 276
Subject I i
Missiles (con.)
--Maintenance
--Materials
--Test facilities
--Tracking
I. •
Mixtures | '
--Diffusion
Molecular beams
--Sources
Molecules
--Chemical reactions
--Diffusion
--Motion
Monotone retracts
Motor accidents
--Analysis
Moving target indicators
--Development
--Human engineering
Multipath transmission
- -Countermeasures
Narol
Naval personnel
--Training
Naval research
Negative ions ,
Neoplasms
--Therapy
Neutron spectrometers
--Design
Newton method
Nickel
--Impurities
— Spectrographic analysis
Nickel alloys
--Temperature factors
Night sky
- -Luminescence
NloUum
—Welding
Niobium alloys
--Welding
Nitrogen
--Spectra
Nitrogen oxides
--Spectra
Noise
--Physiological effects
174 ISO 798
174 161 535<Rev
175 171 157
1)
'PB Number
171 137
151 072-R
153 280
171 134
150 797
152 063
148 676
152 S04
161 408 S-1
150 781
148 694
152 543
177 153 005
Page
173
199
159
172
174
148
195
149
146
IM
ect
Page PB Number
Itt
17i
164
153
135
224
204
148 711
153 006
152 226
152 548
152 164
152 165
171 314
152 133
144 152 570
202
203
197
211
211
198
154
198
198
132
209
140
221
Noise (Radio)
- -Measurement
Nomographs
--Preparation " 180
Noo -linear differential e<piations
--Applicatians 193
--Theory ^^
Nozzles
--Aerodynamic
characteristics
--Model test results
158
158
153 253
152 411
152 492
152 434
152 434
161 223
148 718
161 219
161 219
152 282
148 712
148 716
147 529
153 252
151 377-6
148 691
152 260
148 693
147 374
147 374
1-20
jihiclear reactions |
-Boergy
--Mathematical analysis
Nuclear spectroecopy
--Applications \
- -Instrumentation
Nuclear spins
--Resonance
Nuclei
--Bombardment
—Radioactivity
Nucleic acids
-•Effects of radiation
Nuu (Mechanics)
--Corrosion prevention
Nylon
—Applications
— Fireprooflng
Ocean bottom
—Pacific Ocean
OceaxKsgraphy
--Arctic re^ons
Opacity meter
Operations research
Operators (Mathematics)
—Applications
—Theory
Optical instruments
— Deisgn
Orbit simulator
Orguic compounds
—Applications
Organic semiconductor
Organic solvents
--Chromatographic analysis
Orifices
—Pressure distribution
Oscillators
-Bibliography
—Physiological effects
QKide cathodes
—Properties
Ocygen
— Cootainers
—Heat transfer
—Impurities
OKygra (Liquid)
—Impurities
OBone
—Physical effects
Packagii^
—Btfects of radiation
—Teat methods
Mb thresholds
lurement
203
202
204
210
203
203
203
141
201
173
180
va
188
166
185
222
185
217
186
223
174
212
212
181
194
189
141
208
157
217
144
154
179
176
201
140
149 700
152 424
161 584
152 482
171 163
152 094
150 860
203 ISO 860
149 700
150 860
152 532
161 897
153 014
171 136
149 148 240
152 149
161579
148 714
148 715
171005
148 670
152 483
' 152 442
152 491
152 566
152 429
171 177
171 177
171033
148 694
152 213
152 264
152 538
153 060
148 682
161 946
144 161 946
152 553
161969
152 793
152 794
161897
147 529
Subject
Paint thinners
- -Chromatographic analysis
Palmitic acid
- -Adsorption
Paper
--Effects of radiation
Paraballon antennas
Partial differential equations
--Applications
--Theory
Particle trajectories
--Determination
Particles
--Ionizing effects
--Motion
--Nuclear reactions
--Production
--Scattering
Page PB Number
181
171033
1-21
147 171 141
176
171
192
185
187
—Velocity
Particles (Airborne)
--Counting methods
--Radioactivity
--Scattering
Peano spaces
Pellets
--Acceleration
Pentaerythritol tetranitrate
--Spectrographic analysis
Personality tests
—Development
—Reliability
Perturbation dieory
--Analysis
Riosphines
--Chemical reactions
Riotoelectric cells
--Development
Photographic recording systems
--Applications
niocography
--Equipment
Riotometers
--Design
Riysical chemistry
- -Instrumentation
Riysics
Riysiological psychology
--Bibliograj^y
--Theory
Piezoelectric crystals
—Vibration
Piezoelectric resonators
--Development
204
210
217
204
175
202
204
175
197
146
205
202
188
175
173
138
138
202
214
144
211
223
223
133
154
146
146
205
206
137
136
170
170
152 794
152 219
152 163
148 670
152 490
148 672
205 152 795
152 420
152 549
152 493
171 163
152 380
152 421
152 42^
152 424
171 163
152 381
171 138
152 244
152 283
152 795
152 639
152 543
149 071
149 066
152 166
152 168
147 642
152 422
152 423
152 503
149 705
148 285
152 566
152 284
148 718
149 701
152 244
171002
171003
116 303S6
152 542
152 803
152 803
Sui>lect Page
Pllou
—Training
Piston rings
--Lubricatiota
Pistons I
--Theory I
PUneury atmAspheres
--Analysis
Planets |
--PhotograpWy
Plasma o8cill4tlon8
Plasma (Physiis)
--Electromagnetic (actors
--Electromagnetic properties
• -Mathematical analysis
--Stability
--Theory '
Plasma propullslon
nasties
--Effects of radiation
— Mechanicafl properties
--Temperature factors
Platinum comOounds
-Stability 1 I
Plywood '
--Applications
--Production
Polymers
--Crystal structure
-Effects of radiation
Polynomials
--Applicatiolis
--Theory
Foroua filters:
--Effectiveness
Porous materials
--Diffusion
--Physical properties
Potential theoW
Potentiometerls
--Design
Powder meuljurgy
--BLbliograptiY
Power supplle
--Circuits
Precipitation
--Meteorolc^cal factors
Pressure
--Measurei^nt
Pressure vessels
--Design
Primary batteries
--Arctic refjons
- -Elect rodelB
--Heating
Primates
--Physiologjr
Primers
- -Developmtent
Prob^ility (Statistics)
133
180
X>6
132
131
214
216
178
216
167
215
210
216
214
178
181
181
181
FB Number
Subject
Probability (Sutistlcs) (con.)
171 139
--Applications
--Theory
153 254
ProJectlYe geometry
--Applications
149 298
Propellants
--Combustion
152 464
Propellers (Marine)
148 669
--Cavitation
149 067
--Pressure distribution
152 419
Protective clothing
152 622
--Materials
152 034
--Thermal insulation
152 365
Protective shelters
152 364
--Blast effects
152 549
--Pressure distribution
152 517
Protein starvation
152 561
- -Guatemala
152 622
Procolysis
Page PB Number
182
182
145
205
185
188
180
148
179
185
171
199
164
151
194
206
165
165
165
174
184
185
153 008
153 008
161 948
148 152 091
171 168
171 167
171 181
153 258
152 372
152 444
152 396
161966
148 676
171 178
152 490
149 660
OTS SB-423
152 920
152 448
i
148 694
147 963
157 153 060
149 698
149 697
149 698
138 152 428
152 259
152 162
152 161
Proton cross sections
--Determination
- -Measurement
Protons
--Exchange reactions
Pseudodlabetes
Psychology
Psychomotor tests
--Test results
Pulse amplifiers
--Design
--Operation
Pyrene
--Resonance
Pyridines
--Chemical reactions
Pyrotechnics
--Analysis
Q-values '
Quantum mechanics
—Theory
Quartz crystals
--Aging
— Frequency measurement
--Properties
—Testing equipment
Quartz resonators
--Development
- -Oscillator circuits
--Production
Radar beacons (Airborne)
--Development
Radar confusion reflectors
—AppU cations
Radar duplexers
--Equipment
Radar echo areas
- -Analysis
1-22
186
222
m
176
176
181
176
176
l«l
147
204
204
147
149
142
138
168
168
149
145
173
203
202
216
217
215
217
166
166
166
166
170
163
166
150
214
132
156
148 663
148 695
149 717
W 148 696
148 698
148 699
148 721
148 721
171 153
171 143
152 256
152 256
148 724
148 678
148 679
147 542
150 857
152 133
148 679
148 678
152 367
171000
134 152 215
152 385
152 385
152 488
148 680
149 670
149 700
152 421
152 481
152 493
152 214
152 483
152 231
152 231
152 231
152 231
149 715
149 719
152 231
165 152 229
152 196
152 561
152 391
148 286
Subject }
Page
PB Number
Subject
Page
PB Number
Ksdar interference
Radiolysis
147
171 156
-Reduction
162 148 711
Radiometers
Radar operators
--Sensitivity
167
150 604
--Performance
171
153 006
Radiosondes
Radar scanners '.<
- -Performance
220
149 060
—Development j
171
153 006
Radomes
Radar scanning i
--Load distribution
159
152 832
—Equipment
161
149 059
--Stresses
159
152 832
Radar signals
Rare eartii compounds
-Analysis
162
148 711
--Magnetic properties
214
148 981
—Detection
167
150 604
Rare earths
Radar targets
- -,^;iplications
208
152 538
--Detection
171
153 006
Reaction (Psychology)
-Velocity
167
150 604
--Sutlstical analysis
136
152 156
Radar tracking systems
137
150 887
—Equipment
174
150 797
Reaction time
—Test results
157
148 708
--Measurement
137
150 887
RadUtion
Reactors
—Chemical effects '
146
148 289
--Hazards
203
153 012
Radiation damage
—Location
203
153 011
-Bibliography
205
149 714
153 012
—Measurement
162
152 804
Reasoning
Radiation injuries
--Measurement
135
171 146
--Pathology
143
152 476
--Test methods
137
152 272
Radio astronomy
155
148 983
Re-entry aerodynamics
157
171 147
--Instrumentation
206
152 201
160
153 257
Radio communication systems
Refractory materials
—Military requirements
220
152 232
--Applications
179
171 148
Radio communication systems
--Development
179
171 178
(Airborne)
--Physical properties
179
171 178
—Equipment
170
171 131
Refrigeration systems
,
171 132
--Development
218
150 800
.iadio frequencies
Relativity theory r
-Standards
163
,149 719
--Applications
215
152 214
Radio Interference
Reliability
• -Countermea sures
164
152 226
--Sutlstical anlaysis
189
148 719
Radio navigation systems
Remote control systems
(Airborne)
--Bibliography
143
153 059
—Equipment
170
171 130
Residual stresses
201
152 169
Radio repeaters
Resistors
--Development
164
152 226
--Bibliography
168
OTSSB-429
Radio signals
Respiration
--Mathematical analysis
166
148 714
--Analysis
140
152 433
--Measurement
139
171 140
"Frequency measurements
220
152 232
"Retina
Radio waves
--Riyslology
140
152 399
—Attenuation
151
152 568
Rewarming techniques
139
152 853
—Electrical effects
172
152 991
Riemann surfaces
186
152 374
—Propagation
166
- 161 579
Rocket antennas
,
221
149 064
--Design
169
148 717
Rocket cases
"Handling
143
153 059
--Materials
200
161786
144
152 570
--ThernuQ Insulsdon
181
161948
Radioactivity
Rocket flares
— Countermeasures
203
148 979
--Development
160
152 079
—Recording devices
205
152 795
Rocket motors
Radiobiology
--Exhaust gases
180
152 257
— Mhliography
143
152 349
"Test facilities
159
153 280
T-Equipment
144
152 570
--Test equipment
191
152 345
Rudiofrequency amplifiers
--Thermal Insulation
181
161948
--Signal to noise ratio
174
152 063
Rocket propellanu
R*dlofrequency power
--CombustiOD
177
152 546
— Measurenoents (
209
152 405
180
152 257
Mdlolsnrnprs
Rocket propulsion
'-Applications
180
153 254
—Bibliography
177
171 184
1-23
Subject
Rocket propul^^on (con.)
--Theory
Rods
--Wave tran^mlasioii
Rubber
--Test methods
Runway lights
--Viaibility |
Runways '
--Surfaces
Ruthenium botldes
--Crystal stfuctiire
Saddle point Property
Saliva I ;
--Caiemical Analysis
Sampling (Staijistics)
--Tables
--Theory
Saadwlch pai
--Test results
Saniury engineering
-Ohio
Satellite vehidle research
Satellite vehicle trajectories
--Determlniitlon
--Mathematical analysis
Satellite vehicles
--Guidance vy stems
--Tracking
Satellites
-ModoB
Page PB Number
ands
177
221
205
1S8
158
214
220
141
186
189
184
Scheduling
--Appllcatiqna
Scientific reports
--Bibliography
Scientific realearch
—Arctic regions
-^ --Bibliography
Sea water
- -Desalination
--ElectnrfyBis
Seed Implantation gun
Semlconductltig fUms
--Test results
Semlconductdrs
--Applications
--Development
--Effects- of radiation
- -Electromagnetic properties
-Materii
176
131
221
174
172
174
174
172
174
174
191
163
131
131
224
153
177
160
160
144
1
--Physical properties
—Surface properties
perdepdon
Test resalts
163
212
211
210
210
211
212
210
213
152 546
152 398
149 674
152 384
152 494
152 452
149 735
152 216
148 683
148 719
171 161
182 171 166
152 064
152 302
149 064
152 429
148 706
148 697
150 321
148 706
149 058
150 321
148 697
148 734
147 651
149 136
148 703
148 703
171 314
152 149
171 184
171 129
171 129
152 570
213 149 667
149 720
153 251
152 918
152 760
152 760
149 705
152 434
171 177
148 690
148 671
149 667
137 150 887
Subject
Sequential and ysls
Series expansions
Sheets
--Mechanical properties
Ship bulla
--Materials J
Ships
- -Hydrodynamic
characteristics
--Model test results
Shx± tubes
--Applications
- -Heat transfer
Shock waves
--Analysis
--Physical effects
--Propagation
Signals
--Development
Siliddea
--Crystal structure I
SlUcon
--Conductivity
--Diffusion
—Impurities
--CBtidation
Silicon carbide
—Impurities
--Spectrographic analysis
Silicon crystals
— AppUcationa
--Surface properties
Silicon dioxide
—Absorptive properties
—Conductivity
Silver
--Piyslcal effects
Silver acetyllde
--Chemical reactions
SilTer oxides • -< <
—Analysis
Sin{^ crystals
--Spectrographic analysis
Single crystals (Metallurgy)
--Crystal structure
SUp lines
Social conununicatlan
--Economic aspects
Social desirability
Social sciences
--Theory
Sodium
--Spectra
Sodium nitrate
—Detonation
Soils
--Stresses
—Test methods
Solar energy
— Appllcatlona
Page PBNumbg
I-M
200
176
m
m
192
160
214
211
211
213
213
211
211
109
213
213
210
210
145
165
209
214
201
224
138
224
133
173
161
161
148 683
152 162
161786
171161
150 391
ISO 391
152 426
148 682
152 561
152 256
148 701
148 702
152 445
152 079
152 453
152 455
149 063
149 063
152 186
152 186
152 434
152 434
152 559
149 667
152 186
149 669
148 690
148 680
149 697
152 076
152 452
152 453
152 4S4
152 261
152 215
152 166
152 125
152 2M
149 670
149 699
149 699
211 149 705
lidar flares
—Classification
—Electromagnetic effects
Solar furnaces
--Development
— Tsmperature *.
Scdlds
--Diffusion
—Elasticity
—Luminescence
— Magnetic properties
Solutions
--Properties
Scnagrams
Sonar personnel
--Performance
—Selection
-Training
Sounding rockets
-Design
Spaceflight
—Hazards
Space radiation
^ce suits
^ceshipe
- -Propulsion
Spaerobee
Spectrometers
-Design
--Equipment
Speech
-Intelligibility
Speech transmission
-bteUigibillty
Page PB Number
131
155
217
217
143
192
213
212
J46
1S6
136
134
134
175
157
205
205
173
169
222
— Haat transfer
-Radiation
—Reflective effects
Spheroidal wave functions
-AppUcatians
Squid
SttUlity Indicators
-Design
Stars
"Radiation
Satisdcal analysis
"Tablea
"Theory
SMstlcal tests
Sailadcs
"Theory
Steam
"Chemical effects
Steel
"Mechanical properties
"Military requirements
te^ied zone mirror
ttag support interference
Storms
"Radar analysis
137
134
213
154
219
206
178
im
156
187
134
184
185
137
136
136
213
199
300
206
193
ISO
48 713
50 668
52 472
52 472
48 676
48 725
48 671
53 251
49 701
49 069
52 156
52 121
52 121
71 180
71 147
53 258
71 143
52 622
48 717
48 663
48 663
52 389
52 390
52 255
52 784
47 964
50 833
52 552
52 258
47 963
52 154
52 202
52 471
48 687
71 161
52 162
71 161
52 161
48 684
48 692
48 692
52 186
51072-
61786
52 201
53 379
152 207
Subject
Strakes
Streamline
Stress analysis
- -Theory
Styrenes
- -Polymerization
Subminiature electron tubes
--Development
Sulfates
- -Determination
Sun
--Riotography
--Wave transmission ^
Superaerodynamics
Super regeneration
Supersonic flow
--Mathematical analysis
Supersonic wind tunnels
--Boundary layer
--Design
Surface -active agents
--Hiysical effects
Surface fUms
Surfaces
--Friction
Surfaces (Mathematics)
--Analysis
Surgery
- -Riysiologlcal effects
Switching circuits
--Design
— Development
--Theory
Synthetic fibers
--Color
--Fireprooflng
--Temperature factors
Tanalith
Task summaries
Page PB Number
Teaching machine
Team training
Teichmuller space
Telemeter systems
--Development
--Equipment
Telemetering transmitters
--Design
Telephone communication
systems
--Circuits
--Development
Telephoto lenses
--Test results
Telescopes
--Applications
1-25
195
196
159
145
170
144
223
132
196
170
193
197
193
173
199
201
192
186
167
172
207
214
167
181
180
143
182
183
138
144
157
205
206
222
135
134
186
174
174
167
171
223
131
171 135
152 739
152 832
152 218
149 716
152 393
148 299
152 391
152 480
149 716
152 260
152 492
152 758
152 435
152 147
171 150
148 674
152 374
319 152 766
153 236
152 348
152 520
152 561
153 236
171 153
171 136
153 010
171 167
171 170
171 171
171000
171001
171004
171002
171003
171005
152 164
149 962
152 374
150 797
152 063
174 150 798
153 236
152 513
152 567
148 669
ect
steiiifi
Teletype syst
--Bquipment
Televelafax
Tensor analysis
Ternary diagrajna
TerrMtrial iiiataietisni
— MeMureoMpt
--Sources
--Theory
Test sets
--Design
Textiles
-- Fireproof ing
Thermal radiadoe ,
--Mathematiaal analysis
--Theory
Thermionic enlissioo
— Bibliographiy
Thermistors
--Bibliography
Themaochemialtry
- - Ins trumentatioo
Thermocouple$
--Bibliography
Thermoelec tr icity
— Blbliograpt^y
The rmoluminebcence
Thermoplies
--Bibliography
Thin films i
--Analysis |
-- Elect rodepositlon
--Magnetic jiroperties
--Properties
Thyratrons I
--Developmeint
Titanium i
--Purificatioti
Titanium alloys
--Crystal structure
--Phase studies
Titration j
--Applicatiois
Topology
I
--Applicatioiis
--Theory
Training
--Psychologiical factors
Training devices
--Development
--Human engineering
Transducers |
--Applicatict»s
'--Design j
--Inapedancd
Page
174
151
192
199
207
207
202
207
162
'180
PBNtunber
150 798
150 388
152 163
171 154
152 159
152 158
152 639
152 158
152 208
148 284
171 136
Sub|ect
Page PB Number
194
148 720
217
161 222
156
150 217
208
152 538
168
errs SB-431
166
147
166
168
212
201
171
207
167
163
201
201
201
144
188
187
188
Transfer function
Transformations (Mathematics)
135
133
166
208
175
206
164
188
arSSB-429
152 679
arSS8-430
errs SB-432
152 451
168 OTS S8-43b
152 261
149 660
152 520
152 365
150 074
152 074
151094
151094
149 065
148 685
152 543
148 693
152 545
137 150 887
152 164
171 139
153 007
152 394
171 157
147 964
149 298
150 833
152 253
148 685
152 396
Transformatioos 0><iathematics)-
(coo.)
-Theory 186
188
Transistors
--Bibliography i,
--Circuits
--Development
--Effects of radiation
Transition elements
--Crystal structure
Transmission lines
- - Electromagnetic properties
Transonic flow
--Boundary layer
--Mathematical analysis
Transonic wind tunnels
--Performance
Transparent panels
--Attachment
Traveling wave tubes
--Development
Triangular wings
--Aerodynamic
characteristics
--Stresses
Triaxial test
Triazines
--Electron transitions
Triodes
--Development
Trouble shooting
Tungsten
--Brazing
--Electrical properties
•--Thermal properties
—Welding i
Tungsten oxides
--Electrical properties
Turbulent boundary layer
--Analysis
Ultrasonic radiation
--Absorption
Ultravialet radiation
--Biochemical effects
--Reflection
Underwater sound generators
- -Pressure
Unimolecular reactions
Universities
--Standards
Upper atnooephere
--Analysis
Urease
- -Cry 8 tallization
--Synthesis
Utility functions
Varnishes
--Analysis
--Processing
Vehicles
--Human engineering
1-26
169
164
109
162
212
161
194
196
194
196
159
159
165
195
160
161
170
135
198
219
219
19t
193
196
n
141
IM
206
149
224
156
141
141
223
181
171
152 439
152 543
OrrSSB-433
152 920
152 559
152 804
150 596
148 705
152 413
152 245
152 413
152 245
153 280
153 259
152 562
171 162
152 437
149 «99
149 148 726
149 716
152 165
161224
171 185
171 185
161 224
210 148 690
ect
147 878
148 521
152 ISO
152 532
152 553
147 963
161 408 S-1
148 723
148 286
152 247
152 247
152 016
171033
153 380
177 153 005
Venus
—Meteorology
Verbal behavior
—Analysis
Vertical take-off planes
—Model test results
Very high frequency antennas
-Design i
^bration <
—Testing equipment
^ration isolators
--Materials
Viewer .;
^^gilance performance
Vlrial coefficient
Visibility
—Measurement
^ion
--Fhysicdoglcal factors
Visual perception
--Test methods
Visual thresholds
--Acoustic factors
Voice communication systema
-.-Development j
"FBychological factors |
Vortices
--Analysis
Vulcanlzates
—Preservation
—Temperature factors
Warfare
—Mathematical analysis
Water
--Recovery j
Water vapor i
—Determination
Wkveguide switches ' ('
-Design I
Waveguide windows j
--Failure <
Waveguides i
—Dielectric propertlea
—Theory
Wues
--Effects of radiation
Weadier communicatlona
—Recording devices
re Number
132 152 464
136
137
159
169
172
178
223
136
145
158
140
135
140
134
137
179
179
185
160
154
172
167
208
220
176
151
148 300
152 389
152 390
152 780
148 982
171 134
150 392
148 285
152 566
152 157
152 218
152 384
152 399
171 149
153 252
152 255
152 389
152 390
196 148 521
161969
161969
148 715
171 145
149 061
152 348
15% 467
152 524
149 735
152 794
150 388
Subject
Weather forecastii
— Germany
--Radar analysis
Weadier stations (Automatic)
--Design
--Equipment
Weightlessness
--Kiysical effects
Welding
--Materials
Whistlers
White noise
White oak boards
White oak laminates
Wind
- -Measurement
Wind tunnel models
--Aerodynamic
characteristics
Wind tunnels
--Equipment
Wings
--Aerodynamic
characteristics
-Lift
--Model test results
Wood
--Preservation
--Test results
Page re Number
I
Wounds
--Physiological effects
X-ray diffraction analysis
- - Apidlcatlons
Yagl-Adcock system
Yellow pine boards
Zinc coatings
--Test results
Zirconium
--Rirlfication
Zodiacal light
--Sliectra
1-27
151
ISO
150
151
151
198
156
140
183
183
184
152 448
152 563
152 206
149 711
149 711
134 tf 2 215
161 219
149 069
147 529
171 173
171 174
171 175
150 152 196
193
153 379
197
152 550
158
147 374
159
152 786
158
147 374
182
148 727
182
171 165
171 166
183
171 169
171 170
171 171
171 172
171 173
171 174
184
171 175
171 176
141
152 852
210
152 469
172
149 058
183
171 170
149
149 056
201
152 074
132
152 281
"V.'f-A '^' ,}■'
•.•vi.
r<
•.••.••< -
<!*' 'r
Mnber
.£»c
NUMt
Number
AAL-TR-57-4
141
AD- 225 722
AAL-TR-57-49
1S6
AD-225 794
AAL-TR-57-50
139
AO-226 083
AAL-TR-57-52
1»
AD-226 328
AAL-TR-57-61
•1 ^ ' 140
AD-226 513
AAL-TR-58-17
141
AD-226 695
AAL-TR-59-10
139
AD-227 412
ACTH -Secretion
14D
AD- 227 912
AD-7W4
17S
AD-227 919
AD-30 646
161
AD-227 920
AD-35 492
143
AD-227 943
M)-54S15
107
AD- 228 120
AD-113 786
149
AD- 228 164
AD- 124 406
aos
AD- 228 618
AD- 131 259
153
AD-229 021
AD- 147 496
190
AD-229 046
AD- 148 987
1S5
AD-229 720
AD- 160 869 BUfwrseded 166
AD-229 735
AD-162 022
162
AD-229 939
AD-204 097
18t
AD-229 944
AD-X>4 431
194
AD-2X009
AD-2D5 517
194
AD- 230 010
AD-205 745
151
AD- 230 117
AD-»6 314
223
AD- 230 170
AD-X)6 691
195
AD-230 184
AD- 1)7 529
162
AD- 230 243
AD- 208 631
iM
AD- 230 254
AD-210 114
107
AD-230 420
AD-210 116
167
AD-230 474
AD-210 724
169
AD-230 544
AD-210 847
171
AD-230 558
iD-210 938
221
AD-230 596
AD-210 940
221
AD-230 926
AD-211059
169
AD-231 101
AD-211322
303
AD- 231 155
AD-211 480
131
AD-231 241
AD-211724
210
AD-231 562
AD-212 110
143
AD-231 620
AD-212 617
156
AD-231 996
AD-212 848
173
AD- 232 188
AD-213 895
172
AD-232 286
AD-214 597
153
AD- 232 268
AD- 214 843
155
AD-232 343
AD-215 281
213
AD-232 771
AD-215 625
207
AD-232 815
AD-21S 641
177
AD-232 865
AD-215 960
173
AD-232 918
AD-216 556
146
AD- 233 004
AD-217 169
1 161
AD-233 053
AD-217 615
161
AD-233 091
AD-219 090
223
AD-233 098
AD-219 800
131
AD-ZVi 188
AD-219 882
223
AD-233 254
AD-219 954
176
AD-233 280
AD-220 006
169
AD-233 353
AD-220 103
146
AD-233 480
AD-220 117
163
AD-233 506
AD-225 11S
134
AD-233 723
AD-225 275
166
AD-234 049
AD-22S548
192
AD-234iaO
NUMBER INDEX
"i-
Page
1-29
Number
213
AD-234 278
158
AD-234 296
151
AD-234 384
131
AD-234 385
» 165
AD-234 399
142
AD-234 469
163
AD-234 478
224
AD-234 479
191
AD-234 511
191
AD-234 552
190
AD-234 553
220
AD-234 584
216
AD-234 599
147
AD-234 700
146
AD-234 701
^194
AD-234 747
r'^n
AD-234 798
rs3
AD-234 915
191
AD-234 918
213
AD-234 919
184
AD-234 921
185
AD-234 845
145
AD-234 946
153
AD-235 019
205
AD-235 037
177
AD-235 038
192
AD-235 092
202
AD-235 093
210
AD-235 094
145
AD-235 095
201
AD-235 096
206
AD-235 140
148
AD-235 151
224
AD-235 155
199
AD-235 161
212
AD-r« 213
176
AD-235 256
135
AD-235 374
219
AD-235 377
205
AD-235 385
211
AD-135 426
223
AD-235 436
164
AD-235 532
135
AD-235 570
209
AD-235 571
220
AD-235 627
136
AD-235 629
204
AD-235 631
137
AD-235 641
166
AD-235 665
131
AD-235 785
219
AD-235 788
221
AD-235 832
188
AD-235 833
135
AD-235 902
139
AD-23S947
188
AD-236 057
148
AD-236 201
148
AD-236 219
203
AD-236 371
192
192
16S
161
171
193
las
isi
172
164
146
136
179
145
162
131
212
lf7
166
213
135
209
167
166
107
106
147
166
147
100
107
105
107
154
1S6
17S
ss
161
215
211
144
20O
196
184
172
2M
199
172
151
109
170
Nunaber
AD-236 519
AD-236 861
AD-236 862
AD-236 942
AD-236 966
AD- 237 090
AD- 237 493
AD- 237 691
AD-237 867
AD-238 069
AD- 238 669
AD-239 I2g
AD-239 166
AD-239 651
AD-239 925
AD-239 954
AD- 240 638
AD- 240 697
AD-240 767
AD-241 412
AD-241 425
AD-241 876
AD-241 910
AD- 242 160
AD-242 243
AD-242 284
AD-242 359
AD-242 457
AD-242 524
AD-242 573
AD-242 669
AD-243 045
AD- 243 127
AD-243 145
AD-243 403
AD-243 413
AD-243 456
AD-243 464
AD-243 545
AD-243 658
AD-243 718
AD-243 836
AD-243 859
AD-243 947
AD-244 103
AD- 244 260
AD-244 392
AD-244 393
AD-244 394
AD-244 398
AD-244 666
AD-244 695
ABDC-TN-54i-28
AEDC-TN-60t-l36
AEDC-TN-60-176
AEDC-TN-6Q-177
AEDC-TN-6C|-178
ABDC-TN-60-189
ABDC-TN-6Q-192
ABDC-TR-:
ABDC-TR
AF TR-6199
AFHMD-8-2849
AFBMD-9-4689
AFBMD-TR-«)-183
1-58-21
l-60(-5
Page Nunaber
182 AFCCDD-TN-60-1013
189 AFCCDD-TR-60-27
138 AFCRC-TN-58-560,
140 superseded
163 AFCRC-TN-59-180
169 AFCRC-TN-59-243
204 AFCRC-TN-59-470
136 AFCRC-lN-59-481
224 AFCRC-TN-59-953
149 AFCRC-TN-60-102
196 AFCRC-TN-60-107
171 AFCRC-TN-60-121
160 AFCRC-TN-60-188
163 AFCRC-TN-60-1000
159 AFCRC-TR-58-277
191 AFCRC-TR-59-256
179 AFCRC-TR-59-368
214 AFCRC-TR -59-269
165 AFCRC-TR -59- 370
166 AFCRC-TR-59-372
134 AFCRC-TR -59-373
150 AFCRC-TR -59 -374
167 AFCRC-TR -60 -121
208 AFCRL-TN-60-110
176 AFCRL-TN-60-158
190 AFCRL-TN-60-166
137 AFCRL-TN-60-167
151 AFCRL-TN-60-168
143 AFCRL-TN-60-243
155 AFCRL-TN-60-251
218 AFCRL-TN-60-263
190 AFCRL-TN -60-275
206 AFCRL-TN -60 -277
192 AFCRL-TN -60 -27 8
178 AFCRL-TN -60 -281
150 AFCRL-TN -60-284
138 AFCRL-TN -60 -357
207 AFCRL-TN -60-379
148 AFCRL-TN -60 -400
209 AFCRL-TN -60-4 12
164 AFCRL-TN-60-419
215 AFCRL-TN-60-424
197 AFCRL-TN -60 -425
196 AFCRL-TN -60 -433
196 AFCRL-TN -60 -436
188 AFCRL-TN-60-486
185 AFCRL-TN-60-489
185 AFCRL-TN -59 -557
186 AFCRL-TN-60-601
186 AFCRL-TN-60-6l4a)
185 AFCRL-TN-60-614(II)
188 AFCRL-TN -60 -634
193 AFCRL-TN -60 -663
157 AFCRL-TN -60 -950
173 AFCRL-TN -60-951
193 AFCRL-TN-60-962
193 AFCRL-TN -60-977
193 AFCRL-TN-60-981
218 AFCRL-TN -60- 656
195 AFCRL-TN-60-751
193 AFCRL-TN -60 -7 58
158 AFCRL-TN-60-781
216 AFCRL-TN -60 -797
160 AFCRL-TN-60-960
194 AFCRL-TN -60-969
1-30
Page
Number
Pai
190
AFCRL-TR-59-371
184
134
AFCRL-TR-60-109
162
AFCRL-TR-60-161
167
164
AFCRL-TR-60-180
203
1»
AFCRL-TR-60-182
2U7
131
AFCRL-TR-60-184
174
223
AFCRL-TR-60-1E6
206
133
AFCRL-TR- 60 -240(11)
156
221
AFCRL-TR-60-257
132
219
AFCRL-TR -60 -269
221
219
AFCRL-TR -60 -402
1S(
214
AFCRL-TR-60-404
146
220
AFCRL-TR-60-408
1S5
212
AFMDC-TN-60-10
in
158
AFMDC-TN-60-11
13a
168
AFC6R-TN-58-889
18S
i6l
AFOSR-TN-58-904
194
151
AFOSR-TN-59-539
146
172
AFOSR-TN-59-727
196
157
AFOSR-TN-59-744
181
162
AFCSR-TN-59-795
222
172
AFOSR-TN-59-800
186
221
AFOSR-TN-59-973
187
166
AFOSR-TN-59-796
187
161
AFOSR-TN-59-907
131
155
AFOSR-TN- 59-975
179
166
AFO6R-TN-59-1087
217
185
AFOSR-TN -59- 1092
179
131
AFOSR-TN- 59- 1094
180
154
AFOSR-TN-59-1119
18t
209
AFOSR-TN -59- 1240
222
155
AFOSR-TN-59-1241
187
209
AFOSR-TN- 60-6
210
132
AFOSR-TN -60 -40
186
169
AFOSR-TN- 60-55
186
154
AFOSR-TN -60- 81
175
211
AFOSR-TN-60-111
1S7
189
AFOSR-TN -60 -156
145
205
AFOSR-TN-60-158
147
132
AFOSR-TN-60-159
147
150
AFOSR-TN-60-171
194
150
AFOSR-TN-60-186
215
ISO
AFOSR-TN-60-187
141
188
AFOSR-TN -60 -203
199
207
AFOSR-TN-60-2U/
192
154
AFOSR-TN -60- 226
196
151
AFOSR-TN-60-249
187
219
AFOSR-TN -60- 269
213
155
AFOSR-TN -60 -282
185
133
AFOSR-TN-60-315
156
133
AFOSR-TN -60 -328
185
154
AFOSR-TN-60-341
144
133
AFOSR-TN-60-367
214
219
AFOSR-TN -60 -387
200
163
AFOSR-TN-60-404
309
208
AFOSR-TN-60-430
196
208
AFOSR-TN -60 -460
144
131
AFOSR-TN -60 -542
185
151
AFOSR-TN -60 -594
lis
215
AFOSR-TN -60 -597
196
211
AFOSR-TN-60-640
in
220
AFOSR-TN -60 -644
m
217
AFOSR-TN -60 -680
216
172
AFOSR-TN-60-684
214
132
AFOSR-TN-60-685
214
Nimber
APOSR
AF06R
APOSR
AFOSR
AFC6R
AFOSR
AFOSR
APOSR
AFOSR
APG5R
APOSR
APOSR
APOSR
APCSR
APOSR
APOSR
APOSR
APOSR
APOSR
AFOSR
AFOSR
APOSR
APOSR
APOSR
AFOSR
AFOSR
AFOSR
AFOSR
AFOSR
APOSR
APOSR
APOSR
APOSR
AFOSR
AFOSR
AFOSR
AFOSR
APOSR
AFOSR
APOSR
AFOSR
AFOSR
APOSR
AFOSR
AFOSR
APOSR
APOSR
APOSR
APOSR
APOSR
APOSR
APOSR
AFOSR
APOSR
AFOSR
AFOSR
AFOSR
AFOSR
APOSR
AFOSR
APSAM
APSAM
AFSAM
APSAM
APSAM
TN-60
TN-60
■TN-eo
TN-eo
TN-60
-TN-60
TN-eo
TN-60
TN-eo
TN-60
■TN-eo
TN-eo
TN-eo
TN-60
TN-eo
TN-eo
TN-eo
TN-eo
TN-60
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-eo
TN-60
TN-60
TN-eo
TN-eo
TN-eo
TN-60
TN-eo
TN-eo
TN-60
TN-60
TN-eo
TN-eo
TN-eo
TN-60
TN-60
TN-eo
TN-60
TN-eo
TN-eo
TN-eo
TR-59
TR-59
TR-eo
TR-eo
TR-eo
TR-eo
TR-eo
TR-eo
TR-eo
TR-60
TR-eo
-60-48
-60-65
-60-72
-60-77
-60-81
4^
6^
766
710
720
721
727
758
797
883
906
913
921
932
948
963
979
986
989
990
1002
1023
1041
1043
1047
1058
1063
1066
1081
1082
1083
1084
1086
1087
1088
1092
1124
1128
1130
1141
1142
1143
1179
1180
1181
1182
1225
1237 •
28
74
55
56
77
81
82
93
115
137
140
Page
Number
Page
Number
214
AFSAM -60 -84
139
RRS-830 003
in
216
AFSAM -AR -3-60
140
EM- 147
221
164
AFSWC-TN-60-29
202
ERL-91
220
194
AGC-1880
177
FAT53-14-1 /
173
204
AGC-TN-31
146
FAMD-FT-245-1
ISB
188
AIL-3905-1
162
FAMD-R245-(010-012)
158
186
AINA-2
150
FAMD-R245-025
158
217
A1R-244-58-FR-182
162
FAM:>-R245. 014-R245. 015
158
188
APGC-TN-59-25
162
FIF-A1878
201
214
APL/JHU CM-959
146
FPL-59-2
182
212
ARF-3157-14
146
FFLBuS-4
iMZ
195
ARL -TR-60 -292
184
FPL BuS-6
182
142
ARL-TR -60-298
195
FPLBuS-7
182
188
ARL -TR-60- 300
174
FPLB16-8
112
217
ARL-TR -60-303
204
FRI-R. 113/9
201
215
ARPA Order 24-59, Task 2
213
GE Aerophysics ORM-30
160
210
ARPA Order- 56- 60
167
GMI-1812
165
213
ARPA Order -85- 60
166
GRDAFSG-120
154
196
ASRDL-1481
223
GRDAFSG-123
205
175
ASRDL-1983
162
HAC TM-591
166
175
ASRDL-2092
151
HH ARD-236
ISi
192
ASRDL-2138
150
HMB-1187
176
197
ASRDLE-1198
162
HitoRRO-RR-3
136
212
ASRDL M-1466
172
lER -60-25
165
209
ASRDLT-1480
223
IER-60-245
tao
192
ATI-90 054
158
IER-73-7
US
187
Avco RAD-TM-60-67
217
IER-150-2
213
177
Avco RR-37
194
IMM-NYU-264
186
185
Avco RR -44
210
IMM-NYU-272
192
202
Avc» RR-80 I
214
IQREM IP-1
224
214
Avco RR-91
194
IRL-135
155
202
AWSM- 105-54
149
ISMS-227
186
202
BLC-59-6
223
ISMS-229
222
204
BRL MR-1280
176
ISMS-230
1S7
197
BRLMR-1292 ' '
173
ISMS-231
187
149
BTL-27480-1
163
ISMS- 240
222
185
BuMed-MR005. 15-
ISMS-243
186
213
0002.11. R-2
210
ISMS-245
187
140
BuPers 1^-60-4
134
ITL-22n3-C
143
186
CALAD-1118-A-7
217
JFRC MR -22
200
197
CCL-97
181
lCS-6 camera
223
217
ac-ioi
178
IJ.-21G-0003
IfO
212
CIC-123 1
206
LL-21G-0005
174
186
CU-11-60
220
LL-21G-0009
04
186
CU-63-60 "1
164
LI,-21G-0016
174
186
DASA-1177
176
LL-25G-0020
190
186
DASA-1187
218
14,-46-48
167
210
DMIC-116R
199
LL-46G-0003
167
177
DMIC-136A
201
LL -47-37
157
203
DMIC-M-69
198
LL-47G-0005
221
146
DMIC-M-70
198
LL-51G-0016
190
142
DMIC-M-71
198
LL-52G-0014
190
141
DMIC-M-72
217
LL-55G-O028
190
140
DMIC-M-73
198
I.1,-58G-0014
136
201
DMIC-M-74
198
LL-81G-0023
218
203
DOFL TR-861
220
IJ.-TR-139
190
192
DOFLTR-868
211
LL-TR-202
207
141
DOFL TR-885 .
164
LL-TR-208
2U
144
DlMB-1410
176
LMSD-48 360
174
160
DWG C7 674304
173
LMSD-48 373
201.
140
BBRL-6-32
155
LMSD-49 721
194
141
RKRL-6-33
220
LMSD-288 029
190
134
KBRL-Ul
207
LMSD-288 075
194
141
EBRL-112
207
LMSD-288 164
131
140
BBS -620 320A
180
LMSD-288 166
179
1-31
)
Number
LMSD-288 169
LMSO-288 190 sup(d. 2
LMSD-480 391
LockSB-60-30
MEDEW-RS-1«59
MILNYNS - 50*7 . pC 123
MOT RL-3828»2
MOT RLF -3828-4
MRI R-664-S8
MRI R-696-58
MSEE-55-02
MUPTR-161
kfUPTR-192
MUPTR-198
NADC-EL-L53i92
NADC-MA6029
NAVEXOSP-1466
NAVTRADEVCQ^ 166-1-41
NA\TRADEVCQ* - 198 - 2
NAVTRADEVCEN-512-1
NAVWEPS-71C|3
NBS-TN-2-2
NBS-TN-78
NBS-TN-83
NBS-TN-1816
NCBL R-087
NM-18-02-99, R-80
NCrrSTA-2
NCyrSTP-2374
NCrrSTP-25i
NRCC-5895
NRCC-5917
NRCC-5918
NRCC-5919
NR<X:-5927
NRCC LR-27J
NRCX; LR-28
NRCC LR-28!
NRCCMS-loa
NRCC MT-41
NRL-4129. 8i|pp.
NRL-4164
NRL-4308
NRL-5514
NRL-5521
NRL-5523
NRL-5538
NRL-5554
NRL-5565
NRT -5566
NRL RD-257
NSF-G-3661
NSF-G-5939
NSF-G-1037S
OORR-821.6
OORR-1543. I6P
CSURF-827-4
OSURF-827-4
C3SURF-896-J
CSURF-1073'2
C6W RDPR-45
OrrSCTR-3lO. suppl.
OrrSCTR-34$, 8uppl.
crrsaB-423 ;
arsss-429
Number
Number
180
ore SB-430
i J 166
re 146 666
20O
OTS SB-431
• . ■> 166
re 148 667
192
Cri"SSB432
{ •• 166
re 146 690
200
aiS SB 433
1 169
re 146 691
142
el's SB 434
- 208
re 146 692
218
OTS SB-439
, V 222
re 148 693
158
PltP-514
169
re 146 694
166
PA TN-27
173
re 148 695
167
PA TN-»
173
re 148 696
167
PATN-50
ci 160
re 148 697
167
PB116 303S6
i 137
re 146 698
215
PB 147 374
158
re 146 699
215
FB 147 529 \
140
re 148 700
213
n 147 542
204
re 146 701
161
FB 147 642
138
re 148 702
210
PB 147 643
189
re 146 703
166
PB 147 646
153
re 148 705
171
FB 147 651
163
re 148 706
134
PB 147 878
193
re 148 707
137
PB 147 963
206
re 146 708
191
PB 147 964
206
re 148 709
155
IB 148 196
224
re 148 710
168
n 148 24a
149
re 148 711
202
PB 148 276
169
re 146 712
221
PB 148 277
143
re 148 713
181
PB 148 281
190
re 148 714
140
PB 148 283
172
re 148 715
209
PB 148 284
162
re 148 716
209
PB 148 285
223
re 148 717
191
PB 1^8 286
156
re 148 718
218
IB 148 287
221
re 148 719
159
re 148 288
221
re 148 720
159
re 148 289
146
re 148 721
159
re 148 290
189
re 146 722
20O
re 148 291
154
re 148 723
1S9
re 148 292
137
re 148 724
isr
re 148 293
135
re 148 725
159
re 148 294
143
re 148 726
VK)
re 148 295
221
n 148 727
218
re 148 296
219
re 148 728
203
re 148 29/
166
re 146 729
203
re 148 298
192
re 146 732
203
re 148 299
223
re 148 733
206
re 148 300
136
re 148 734
200
re 148 521
196
re 148 735
222
re 148 608
189
re 146 976
206
re 148 663
222
re 148 977
144
re 148 668
155
re 148 978
180
re 148 669
131
re 148 979
148
re 148 670
185
re 146 980
203
re 148 671
213
re 148 981
184
re 148 672
187
re 148 982
1S6
re 148 673
196
re 148 983
184
re 148 674
192
n 148 984
213
re 148 675
199
re 149 056
147
n 148 676
148
re 149 058
219
re 148 677
194
re 149 059
219
n 148 678
147
re 149 060
213
re 148 679
147
re 149 061
219
re 148 680
145
re 149 062
160
re 148 681
209
re 149 063
169
re 148 682
217
re 149 064
199
re 148 683
186
rei49 065
199
re 148 664
187
re 149 066
166
re 148 665
188
re 149 067
222
187
210
IM
IM
117
194
222
117
174
179
180
208
194
194
131
161
172
184
1S7
1«2
ISS
Itt
an
131
m
m
m
m
isi
m
IM
m
HI
' 2M
142
192
148
111
138
188
191
m
m
m
1«
m
m
m
w
m
m
m
m
i«
m
m
m
m
m
a
148
m
Hi
1-32
Number
n 149 068
PB 149 069
n 149 070
IB 149 07 1
n 149 073
PB 149 074
PB 149 075
PB 149 136
PB 149 298
PB 149 627
PB 149 652
PB149 656
PB 149 660
PB 149 661
PB 149 667
PB 149 669
PB 149 670
FB 149 672
FB 149 673
PB 149 674
PB 149 697
PB 149 698
PB149 699
PB 149 700
PB 149 701
PB 149 702
PB 149 705
PB 149 711
PB 149 714
PB 149 715
PB 149 716
FB 149 717
PB 149 719
PB 149 720
PB 149 734
FB 149 735
FB 149 909
FB 149 962
FB ISO 074
FB ISO 217
FB ISO 321
PB ISO 388
PB 150 391
PB ISO 392
FB ISO 485
FB ISO 500
PB 150 596
PB ISO 602
FB ISO 604
FB ISO 605
FB ISO 668
PB ISO 781
FB 150 790
PB 150 793
FB 150 795
PB 150 797
FB ISO 798
FB1S0 800
FB 150 803
FB 150 833
n 150 857
FB ISO 860
PB ISO 887
PB 150 966
PB 130 974
Page
200
156
215
f 175
• 188
177
158
163
206
192
190
213
171
185
213
210
173
195
»222
^205
165
165
161
203
146
164
211
151
205
170
170
168
163
163
165
220
: 208
134
163
156
174
151
176
178
145
135
212
190
167
166
155
146
134
187
190
174
174
218
165
206
204
203
137
140
223
-2
-6
Number
re 151 072-R
re 151 094
re 151 361
re 151 377-
re 152 015
re 152 016
re 152 017
re 152 034
re 152 042
re 152 063
re 152 064
re 152 069
re 152 074
re 152 076
re 152 079
re 152 085
re 152 091
re 152 094
re 152 105
re 152 112
re 152 121
re 152 125
re 152 127
re 152 133
re 152 145
re 152 147
re 152 14^
re 152 149
P6 152 150
re 152 154
re 152 156
re 152 157
re 152 156
re 152 159
re 152 160
re 152 161
re 152 162
re 152 163
re 152 164
re 152 165
re 152 166
re 152 167
re 152 166
re 152 169
re 152 174
re 152 179
re 152 186
re 152 196
re 152 201
re 152 202
re 152 204
re 152 205
re 152 206
re 152 207
re 152 208
re 152 209
re 152 210
re 152 211
re 152 212
re 152 213
re 152 214
re 152 215
re 152 216
re 152 218
re 152 219
Page
Number
199
re
152 226
201
re
152 227
155
re
152 228
221
re
152 229
153
re
152 230
223
re
152 231
199
PB
152 232
216
re
152 241
149'
re
152 242
174
re
152 244
176
re
152 245
192
re
152 247
201
re
152 249
209
re
152 ZW
160
re
152 253
145
re
152 255
148
re
152 256
210
re
152 257
196
re
152 256
139
re
152 259
134
re
152 260
224
re
152 261
148
re
152 262
204
re
152 263
177
re
152 264
199
re
152 271
153
re
152 272
153
re
152 281
206
re
152 282
178
re
152 283
136
re
152 284
136
re
152 290
207
re
152 291
207
re
152 301
184
re
152 302
185
re
152 303
184
re
152 343
192
re
152 344
135
re
152 345
135
re
152 348
138
re
152 349
188
re
152 364
138
re
152 365
201
re
152 366
221
re
152 367
215
re
152 372
213
re
152 373
150
re
152 374
206
re
152 377
189
re
152 378
132
re
152 380
168
re
152 381
150
re
152 384
ISO
re
152 385
207
re
152 387
133
re
152 388
133
re
152 389
133
re
152 390
131
re
152 391
189
re
152 393
215
re
152 394
134
re
152 396
141
re
152 398
145
re
152 399
171
re
152 405
Page
164
151
162
165
160
166
220
167
219
146
196
141
156
197
i64
1S4
,176
(180
219
174
193
201
163
140
141
137
137
132
132
205
133
ISO
212
207
131
153
157
148
191
172
143
215
167
142
142
185
185
186
200
200
175
175
158
168
152
152
137
137
132
144
208
188
221
140
209
1-33
^
Number
PB 152 411
PB 152 413
FB 152 419
PB 152 420
PB 152 421
PB 152 422
PB 152 423
PB 152 424
PB 152 426
PB 152 427
PB 152 428
PB 152 429
FB 152 430
PB 152 432
PB 152 433
PB 152 434
FB 152 435
PB 152 437
PB 152 438
PB 152 439
PB 152 440
PB 152 441
FB 152 442
PB 152 443
FB 152 444
PB 152 445
FB 152 447
FB 152 448
PB 152 450
PB 152 451
FB 152 452
PB 152 453
FB 152 454
FB 152 455
PB 152 456
PB 152 457
FB 152 464
IB 152 465
PB 152 467
PB 152 468
PB 152 469
PB 152 471
PB 152 472
PB 152 474
PB 152 476
FB 152 480
PB 152 481
PB 152 482
FB 152 483
FB 152 484
FB 152 487
FB 152 488
FB 152 490
FB 152 491
PB 152 492
PB 152 493
PB 152 494
PB 152 502
PB 152 503
PB 152 504
PB 152 513
PB 152 517
P3 152 519
PB 152 520
FB 152 521
PftfB
Number
ao3
PB 152 524
194
PB 152 527
21*
PB 152 528
XM
PB 152 531
ao2
PB 152 532
201
PB 152 534
214
PB 152 538
202
PB 152 539
19«
PB 152 540
213
PB 152 542
I3t
PB 152 543
174
PB 152 545
18S
PB 152 546
196
PB 152 547
140
PB 152 548
211
PB 152 549
173
PB 152 550
160
PB 152 551
187
PB 152 552
186
PB 152 553
186
PB 152 554
186
FB 152 555
186
FB 152 559
218
PB 152 560
185
PB 152 561
192
PB 152 562
213
PB 152 563
151
PB 152 566
212
PB 152 567
212
PB 152 568
214
PB 152 569
214
PB 152 570
214
PB 152 622
214
PB 152 637
152
PB 152 638
152
PB 152 639
132
PB 152 653
190
PB 152 679
167
PB 152 739
190
PB 152 758
210
PB 152 760
156
PB 152 765
217
PB 152 766
220
PB 152 780
143
PB 152 784
196
PB 152 785
216
PB 152 786
204
PB 152 793
217
PB 152 794
217
PB 152 795
209
PB 152 798
149
PB 152 803
185
PB 152 804
186
PB 152 832
197
PB 152 849
217
PB 152 850
158
PB 152 851
179
PB 152 852
144
PB 152 853
195
PB 152 918
171
PB 152 920
216
PB 152 989
189
PB 152 990
207
PB 152 991
15S
PB 153 005
Page
Number
208
PB 153 006
178
PB 153 007
144
PB 153 008
141
PB 153 010
141
PB 153 011
142
PB 153 012
7M
PB 153 014
141
, PB 153 059
142
PB 153 060
136
PB 153 067
188
PB 153 236
188
PB 153 251
177
FB 153 252
170
PB 153 253
15S
PB 153 254
2U^
PB 153 255
197
FB 153 256
192
PB 153 257
1S4
PB 153 258
154
PB 153 259
173
PB 153 260
193
PB 153 280
169
PB 153 379
169
PB 153 380
214
PB 153 381
165
PB 161 219
ISO
PB 161 220
223
PB 161 221
223
PB 161 222
151
PB 161 223
151
PB 161 224
144
PB 161 408 S-1
178
PB 161 535(Rev. 1)
190
PB 161 579
190
PB 161 584
202
PB 161 786
220
PB 161 897
147
PB 161 946
196
FB 161 948
193
PB 161 966
210
PB 161 967
140
PB 161 969
139
PB 171 000
159
PB 171 001
218
PB 171 002
200
PB 171 003
159
PB 171 004
176
PB 171 005
176
PB 171 033
205
PB 171 129
134
PB 171 130
170
PB 171 131
162
PB 171 132
159
PB 171 134
139
PB 171 135
139
PB 171 136
140
PB 171 137
141
PB 171 138
139
PB 171 139
211
PB 171 140
164
PB 171 141
191
PB 171 142
162
PB 171 143
172
PB 171 144
177
PB 171 145
171
1(8
181
143
303
203
173
143
1S7
162
167
212
140
202
in
219
171
160
2)5
159
161
157
193
171
1«
191
191
191
217
191
191
149
174
161
302
200
201
144
181
180
148
179
138
144
205
206
197
222
181
160
170
170
170
172
195
180
173
197
ISS
139
147
197
2)5
189
160
1-34
Number
li 171 146
IB 171 147
PB 171 148
n 171 149
n 171 ISO
FB 171 151
n 171 152
FB 171 153
FB 171 154
FB 171 156
FB 171 157
FB 171 160
FB 171 161
FB 171 162
fB 171 163
FB 171 165
n 171 166
FB 171 167
FB 171 168
PB 171 169
FB 171 170
PB171 171
PB 171 172
IB 171 173
IB 171 174
FB 171 175
IB 171 176
IB 171 177
FB 171 178
IB 171 179
FB 171 180
PB 171 181
PB 171 182
FB 171 183
PB 171 184
FB 171 185
FB 171 314
IHS G M-743(04)
PHS G M-743(C3)
FHS G M-743(C4)
IHS G M-743<C4)
IHS G M-743(C4)
IHS G M-743(C4)
IHS G M-743(C4)
IHSGS-63
IHSGS-63, SR-3
ID-S92
ID-624
niAL-474
nAL-546
PmMRI-806-60
PnMRI-828-60
PLASrBC-2
IHST-516, 8iq)pl.
PRF-1203
Proj. 6X59-06-001
PSI-3000:15-24-Q
Page
Number
iPage
Number
135
PSI-3000:21-4-Q
213
TDI900
151
157
PUAEL-469 ^
196
TED ADC EL-549
161
179
PU AEL-491 H
196
TREC 60-39
158
161
QFCIAF S-743, R-1
176
TR EC 60-40
178
201
QFCIAFS-748. R-4
176
TX-2 display system
190
159
QFEA MRS-6001
205
UCLA-DE-59-75
19
197
QFEA R-6
205
UCLA -DE -60- 15
163
181
R59SJ)336
160
UCLA-TE-60-16
163
199
R60SD453
132
UCLA-DE-60-25
189
147
R6nsr>454
178
UMRI-2900-i28-R
222
175
RADC-TN-59-35
167
USCEC 56-216
210
143
RADC-TN-59-37
167
USCEC 56-217
197
184
RADC-TN-59-46
172
USCEC 56-218
192
195
RADC-TN-59-54
169
USNRDL-TR-127
205
204
RADC-TN-59-99
143
USNRDL-TR-380
202
182
RADC-TN-60-150
153
USNRDL-TR-419
219
182
RADC-TN-60-164
209
UTU-TN-22
194
182
RADC-TR-57-153
153
WADC-TN-59-1. superseded
195
182
RADC-TR-58-160
223
EADC-TN-59-42
134
183
RADC-TR-58-172
162
^ WADC-TN-59-243. PL 1,
183
RADC-TR-59-26B
221
Siippl. 1
149
183
RADC-TR-59-26D
221
WAnC-TN-59-351
172
183
RADC-TR-59-39
155
WADC-TR-57-623
189
183
RADC-TR-59-44
156
WADC-TR-58-562, pL 2
160
1
183
RADC-TR-59-65
153
WADC-TR-58-673
135
184
RADC-TR-60-146
170
WADC-TR-59-366, pt.2
157
184
RADC-TR-60-161
171
WADC-TR-59-432, pt.2
179
,f
212
RADC-TR-60-205
143
WADD-TN-60-71
175
« I
179
RATSEC-A60-8
176
WAUU-TN-60-104
147
r
195
RBIC MAL-30
205
WADD-TN-eO-108
197
175
RIAL 60-2314
201
WADD-TN-60-140
134
145
RIAL 60-2712
179
WADU-TN-60-145
205
181
RMD-1159-F
180
WADD-TN-60-210
137
218
RPITR AE-6001
196
WADC-TR-58-381, pt.3
195
177
RPI TR AE-6003
197
WADD-TR-60-7
161
219
RW(ARL-57-1026
216
WAlX)-TR-60-31
201
224
SA-TR16-1115
144
WAUD-TR -60-41
147
138
SA-TR20-6005
208
WAUD-TR-60-46
159
138
SBH RO. 209
171
WAIlI)-TR-60-76
137
138
SIO Ref-60-7
149
WADD-TR-60-111
212
188
SIPRE-RR-63
152
WADD-TR-60-119
159
189
SIPRE-RR-65
152
WADD-TR-60-124
179
191
SIPRE-TR-66
152
WAED-TR-60-174
175
224
SIPRE-TR-70
152
WADD-TR-60-230
197
209
SM 58-10
221
WADD-TR-60-295
181
209
SME-AG-3
223
WAHO-TR -60-316
199
167
Solar BR -989
178
WADD-TR -60-329
195
167
Sperry-LJ- 1260-0001 -7
160
WADD-TR-60-i365
157
196
Squid PR-102R
178
WAnn-TR-60-385
180
196
SRI -2225
156
WAID-TR -60-395
143
167
SRI-2718
221
WADU-TR-60-412
173
215
SRI-SU-2296
181
WAI)I)-TR-60-468
197
181
SRI-SU-2480
213
WADD-TR-60-469
133
149
SRl-SU-2594
151
WAI)l)-TR-60-476
143
188
SRI-SU-2741
213
WADD-TR-60-619
139
142
STL/TR-60 -0000 -09255
216
WAL 112/83-17
221
109
TAMC Ref-60-8Dn
151
WAL 803/19-5
147
WDLTR-1164
171
WRL 403FD449-R7
172
]
WT(BU)33
194
1-35
•n, •
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_.4si I
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RTS
March 10, 196l> ""^""^''
Vol. 35, No. 3 ^R 2 0 1981
A monthly listing of
Government research reports
available to industry
IS issue:
-Speed Image Shutter Unit.
>B 171 197) I
itigation of Organic Semiconductors.
»B 171 340) i I
I Present Status of Ku!>sian Metallurgy.
»B 171 307)
»gen Tetroxide Corrosion Studies.
»B 171 301) \
i . .
)n»e of Plates to»Moving Shocks.
B 171 302)
[Analyzer for Moisture and Solids in
Fuels. (PB 171 303)
losed Circuit T\ System for Passive
at Night. (PB 161 968)
ctive Coatings for Refractory Metals.
PB 171 193)
It Developments in Casting Resins
Technology foij Electrical Encap-
lUon Applicatioii-s. (PB 171034)
tw of Some Lncoijventional Methods
Machining. (PB 161 225)
ibility and Mechanical Properties
High-Strength Steel Extrusions.
151097)
Complete list of printed reports
begins ttn pafte Hi ^
I
Chemistry
Z-
1
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CONTENTS
Page
PRINTED REPORTS AVAILABLE FROM OTS ANNOUNCED IN THIS ISSUE lu
BIBLIOGRAPHY . . . ; 257
ASTRONOMY ....', 257
Astrophysics . . . i 257
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sychc
)LOG
BIOLOGICAL SCIENCES 265
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l\itUA\JkJL\JX\JtL}f •■•■•••••••■■•••■■•••■••••■•••••••••■•■•oa*>««ao«a«>**«a*ooaa**»*aa*«oo««***«» ^/O
^jKjKjAyJfLy •••••■a*4************>****<*********'***o***«oo************o**o*>***O>a*****0**«»* ^/O
CHEMISTRY j 274
Inorganic Chemisfry 274
Organic Chemistry 274
Physical Chemistify 275
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Frost Science 281
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282
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MACHINERY, FABRICATION, AND ACCESSORY EQUIPMENT 310
Engines and Propulsion Systems ' 310
Manufacturing Equipment and Processes 31 3
Transport, Tractipn and Hoist Facilities 313
Wt^\ X C* l\l ^VL^O ••••••^••■•••••••■•■•••■■••••■■••••a««««aa*>a>aa*aaaa**a*a*a*»(aaaaaa*aaa«aaaaa OLO
Fuels, Lubricants,^ and Hydraulic Fluids 314
Plastics . 315
Rubber and Elastomers 316
MATHEMATICS 317
Computing Devices 323
MECHANIcfS 324
. Aerodynamics and Pneumatics 325
Hydrodynamics, Hydraulics, and Hydrostatics 327
Sutics, Kinematics, and Kinetics 328
METALLURGY i 329
Ferrous Metals , 330
Structural Metallurgy and Corrosion ." 330
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY 331
Elementary Particles 332
Instruments and Installations i 333
Radioactivity _ 334
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT 335
PHYSICS ) 336
Electricity and Magnetism 336
Electronics ". 337
Molecular Physics and Spectroscopy & % 338
Optics 339
Solid State Physics 341
Theoretical Physics 346
Thermodynamics 348
Wave Propagation 349
RESEARCH METHODS, TECHl^IQUES AND EQUIPMENT 351
Information Theory 351
Photographic Equipment 352
MISCELLANEOUS j J 352
ATOMIC ENERciY COMMISSION REPORTS
BIOLOGY AND MEDICINE
CHEMISTRY .J
General
Ess
353
353
353
353
Separation Pitxesaes for Plutonium and Uranium 353
COOTROLLED THERMONUCLEAR PROCESSES
ENGINEERING AND EQUIPMENT
HEALTH AND SAFETY
INSTRUMENT$
ESOTOPES
354
354
354
354
354
METaLsT ceramics" and materials'. '.'..'.WWWIW. 355
NUCLEAR EXCLUSIONS • • 371
particle ACCELERATORS AND HIGH-VOLTAGE MACHINES 371
372
385
387
387
387
388
390
390
I-l
1-5
1-13
PHYSICS AND
RADIATION HI
RADIOACIIVH
BPArTOHS J
MATHEMAl
•FECTS ON
WA^XF
ICS
MATFRIALS
...■••••
TECHNOLOGY
Feed Materia
SlQjJRCE INDEX-
sCrejECT INDEX
NUKB^R INDEX
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Printed Reports Available From OTS Announced in This Issue
\ 1
ASTRONOMY ?, ' Page
Development of a computer subroutine for planetary and lunar posltlcms.
Aug60. 99p. (PB k71 196) $2.25 _ 258
BEHAVIORAL SCIENCES
Bibliography of aerospace medical division reports in the fields of •
engineering psychology and training psychology, 1945-1960. May 60.
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260
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272
BIOLOGICAL SCIENCES
Aerospace Medicine and Biolc
annotated bibliography. Volume III:
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(PB 171 333) $2. 50 . . '. 265
Cumulative effects of borane toxicity as revealed by a clinical test. Aujr 60.
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Human psychomotor performance under varied transverse accelerations.
Aug 60. 54p.(PB17l 304) $1.50 269
Radiological health data. Volume 1, No. 9. Dec 60. 56p.
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CHEMISTRY ;
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ENGINEERING
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14p. (PB 171 223) 50 cents
Closed circuit TV system for passive use at night. 23 Nov 60. I8p.
(PB 1 61 968) 50 cents .... .V.
Comparison of special perturbatlcm methods In celestial mechanics.
Aug 60. 56p. (PB itl 337) $1. 50
Corroaion of metals in sea water. Dec 60. 62p. (PB 171 344) $1. 75 '..'.'.'.
DC current instruments 1.0 to 200 amperes full scale. 26 Nov 58.
20p. (PB 171 210) 50 cents
DC resistance, O.OOOOl to l.Oohm. 6July60. Up. (PB 171 205)50 cents !.!!!!.'!!!!!*
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ill
289
289
289
289
290
290
290
290
302
309
28.S
290
290
291
291
ENGINEERING (con.)
Decade reaiBtorB 0. 1 to 100.000 OHMS per step (using LiN 4232- Al
bridge). 2 May 60. I7p. (PB 171 211) 50 cenia
DC voltige 1 . oj to 1000 volts. 27 Feb 58. 7p. (PB 171 214) 50 cents ....
DC voltaie 0 to 1 000 volts. 21 Feb 58. lip. (PB 171 215) 50 cents
DC voltage instruments 15-1000 volts fuU scale. 3 Nov 58. 14p.
0^ 171 217> 50 cents V ;>* " '^o * " ; il
DC voluge insttruments 1-1500 MV full scale. 16 Oct 58. 16p.
(PB 171 21 $ 50 cents ., • • • -ri- ■ :
Dry chemical System for carbon dioxide removal from submarines.
23 Nov 60. 8p. (PB 171 046) 50 cents ■••;••,
Effects at temperature-time- stress histories on the mechanical
Drooerties of aircraft structural metallic materials. Part II.
ft^sed e^iosure of 7075-T6. Sep 60. 1 iSp. (PB 171 328) «. 50 . . . .
Frequency TeS^aae to GPS to 10 MCPS, 0. 5 MV to 5. 2 V and AC
voltage calllH-ation DC to lO MCPS, 0. 1 to 5. 2 volts. 18 Jan 60.
29p. (PB111216) $1.00 ;••;."
HvDcrscnic fre^ flight research. Part I: Instrumentation evaluation
^^ data anilysis. July 60. 45p. (PB 171 194) Si. 25...
Hypersonic frefe flight research. Part II: Investigations of teat u-ansfer
^ aerodynamic stability. July 60. 93d. (PB 171 195) $2. 25
Inductance, 1.0>iH to 10 H direct method. 28 Aug 58. 23p.
(PB 171 208) 50 cents ;• ;• y ' L{'\\k
RADC reliabilllty notebook. S»fl?plement 1. 1 Sep 60. 215p.
(PB 161 894f 1) $3. 50 V^ • • • r r " 1
Removal of orianic contaminants from air by type 13X molecular sieve.
6 Dec 60. T9p. (PB 171 051) 50 cents ^ ,VVV«^""
Self impedancd of a circular loop in a conducting medium. 17 Aug oo.
I3p. (PB 171 353) 50 cents • -,- • • • ■■■■ •■'•'•
Smear- camer4 techniques. 18 Aue 60. 21p. (PB 171 352) 75 cen s ....
Standards inductors. 100 uH to 10 H general radio 1482 series (using
GR 1632 Abridge). l§Mav60. 13d. (PB 171 201) 50 cents .... .
Standard resistor MBS type 1 ohm to lOO. 000 ohms (using LiN 4232 Al
bridge). 27 Apr 60. 12p. (PB 171 200) 50 cents
Supersonic aetoelastic effects on static atabilitv and control. Pa
Aeroelastic interaction. July 60. 371p. (^ 171 192) J5.00
Supersonic sp«ed flutter analysis of circularpanels *^th olges elas-
tlcally restrained against rowtion. Aug 60. 85p. (PB 171 199) $2.25 .
Vapor cycle choline systems for space vehicles. July 60. 27p.
fpa \j\ XiSb 75 cents •
Voltage standing wave ratio, X-band (8.20 to 12.40 KMC) 1.01:1 to 10:1.
13 July 60. I3p. (PB 171 204) 50 cents •.••
Part III.
MACHINERY
Analytical studies on Ion propulsion. Aug 60. 77p. (PB 171 305) $2.00 .
Effects of various exhaust blast deflectors « the acoustic noise charac-
teristlcs o< 1,000-pound- thrust rockets. Sep 60. 65p. (PB 171 308)>l-75
Review of sonie unconventional methods of machining. 2V Nov ou. .^up.
(PB 161 223) 50 cents ;••' • .• • '••J.'^'
Rocket-nizle testing and evaluation. 7 Dec 60 17p. ^O^^fl 227) Scents
Status of DOFL fuel cell program on 1 October 1960. 24 Oct 60. 13p. >
(PB 171 050) 50 cents
)•■•••*<
>•••••<
291
291
291
291
291
309
2S?
292
293
286
292
304
309
SOB
308
292
292
285
286
305
292
312
, 311
, 313
, 311
. 311
MATERIALS
Analyzer for iwisture and solids In Jet fuels. Sep 60. 34p.
(PB171 30$) $1.00 ...• y'-;A"fskW"
Experimental, studies of sub- atmospheric combustion. Aug 60. 03p.
(PB 171 304) $1. 75 • • • • •; • •
Heat fused ceramic coatings for aluminum components ol rocket
launchers.] 21 Oct 60. I9p. (PB 171 047) 50 cents .......... ...
Internal and sMrface temperatures of rubber exposed to direct sunlight.
31 Aug 60. Up. (PB 171 042) 50 cents ..•••••• • ; •
Investigatic«6f the high speed Im,^ behavior ^^^^^^ 7%7*^«-
Part 1- Detign and apparatus. Sep 60. 39p. (PB 171 dll> >i.uu
Ozone resistaiice of SBR vulcanlzates. 31 Aug 60. 34p.
(PB 171 04(3) $1 00
Recent develcipments in casUng resins and technolomr '^ el«:trlcal
encapsulation applications. Nov 60. 34p. (PB 171 034) $1.00 ....
MATHEMATICS
Distribution-lree statistical tests: Aug 60. 387p. (PB 171 312) $5.00.
Existence thearem for the equation Uxyz'f- 12 July CO. 24p.
(PB 171 34p) 75 cents ^. . •,•••'
F ^ , iV - .
315
SIS
314
317
314
317
316
311
321
Page
MATHEMATICS (con.)
First aid for pet projects injured In the lab or on the range or what to
do until the statistician comes. 29 Jan 52. 59p. (PB 171 327) $1. 50 S21
Unear bounded automata. June 60. 29p. (PB 171 339) 75 cents 324
Qb calculation solutions of quasi- linear, first order partial differential
eauations. 1 Sep 60. 26p. (PB 171 350) 75 cents 321
On the capacity of the icosahedron. 1 Sep 60. 1 Ip. (PB 171 354) 50 cents 321
The solution of the characteristic and the Gauchy boundary value
prcAlems for the Bianchl partial differential equation in independent
variables by a generalization of Riemann's method. 27 July 60.
I92p. (PBl7l55l) $3.P0 ••.... 321
Some results on transformations In the analysis of variance. Aug 60.
24p. (PB 171 334) 75 cents • '»''*
Uooer and lower bounds for the capacitance of the regular solids.
TS Sep 60. I04p. (PB L71 355) $2. 50 321
MECHANICS
1
!
Force 0 to 60, 000 lbs. (approx. ) tension only. 15 July 60. 34p.
fPB 171 203) 75 cents
Response of plates to mo>^tng shocks. Aug 60. 37p. (PB 171 302) $1. 00 326
330
329
331
329
METALLURGY '
Availability and mechanical properties of high- strength steel extrusions.
26Oct60. 63p. (PB 151 09-^ $1.75 AA\i:AA
Handbook of Soviet alloy compositions. 25 Aug 59. 258p. (PB 171 331)$4.00
Nitrogen tetroxlde corrosion studies. July 60. 64p. (PB 171 301) $1-75
Notch sensitivity of refractory metals. Sep 60. Il5p. (PB 171 198) $2. 50
Notes on large- size furnaces for heat treating metal assemblies. 25 Aug
60. 9p. (PB 161 213) 50 cents .i.uv« i^
Present status of Russian metallurgy. Sep 60. I3p. (PB 171 307) 50 ceiits 329
Production and availability of some hl^-purlty metals. 2 Dec 60. 48p.
(PB 161 226) 50 cents ^'
h-otective coatings for refyactory metals. Aug 60. 54p.
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Research and development on the effects of high pressure and tempera-
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(PB 171 348) $2.00 Allk-'^A
Toughness of steel sheet: the advantage of laminating. Oct eo. 24p.
(PB 171 044) 75 cents
330
352
MISCELLANEOUS
Report of NRL Progress. Feb 61. (PB 171 315) $1.25. $l0.00/ycar
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY !
Energy distribution of electrons from ionizing colllslans of heavy
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Polymerization of styrene jand butadiene by ganuna radiation. 31 Aug
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PHYSICS
342
Investigation of organic semiconductors. Sep 60. 83p. (PB 171 340) $2. 25
Investigation of the infrared absorption of selected aromatic compojuids
in tte region of 2 to 35 microns. Sep 60. 44p. (PB 171 342) $1. 25 339
Mass in air 1 gram to 30 kilograms direct weighing method. 8 June 60.
20p. (PB 171 202) 50 cents : ' * V • 'J ' •,
Research on the pyroelectj-lc properties of slnde crystals of cadmium
sulfide and zinc sulfide. Aug 60. I5lp. (1% 171 338) $2^5... 345
Quarterly radio noise dat«, June, July, August 1960. 4 Nov 60. 68p.
/no I ^i ^77- 7\ J 1 75 i • jov
Steel mirrors for a 'streak'cai^VaV Aug 60'. 'l3p. (PB 171 191) 50 cents 341
Stoichiometry and electronic properties of PbTe. July 60. 6lp.
(PB 171 356) $1. 75 • • V ••••••
Theory of plasmas. Part I. Aug 60. 69p. (PB 171 336) $1. 75
Thermophysical properties of solid materials. Volume I. Elements
(Melting temperature ^ve lOOOop). Aug 60. 735p. (PB 171 329-1)
, $8.00 .... .V. 17. 3*'
345
347
RESEARCa' ME
High-speed imlige shutter unit. Apr 60. 62p. (PB 171 197) $1.75
I .
HODS, TECHNIQUES AND EQUIPMENT
Page
352
For your convenience GTS order blanks (Form TS-37) are
available on request from the OFFICE OF TECHNICAL SERVICES.
v.. Jti .
I • «-.!•' r
«.-!•-'
'«■••:,•(
ri
^ U 4 . ■ % -
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
OFFICE OF TECHNICAL SERVICES
^^^^ Vol. 3.S, No. .3
Pages 2S7-3W
March 10, 1961
1 .[
I
•
BIBLIOGRAPHY
David Taylor Model Basin, Washington, D. C
UNCLASSIFIED LIST OF REPORTS ISSUED THROUGH
30 JUNE 1957 AND SUPPLEMENTS I-XI, 1 JULY 1957-
30 JUNE 1960. Sep 57, rev. July 60. I67p. 2,047 refs.
Rept. 1160, supersedes TMB rept. 597.
Order from LC mi$7.80, ph$25.80 PB 153 726
This report released for sale to the public 16 Jan 61.
TWa list is divided into four' sections, each numbered
■eparately, as I-l, II-l, III»1 andIV-1. Section I
contains the regular series of TMB formal reports
numbered consecutively without any preceding letter
designation. Section II contains the R-serles, which
waa discontinued in 1947. Reports in this series are
dealgnated as R-1, R-45, etc. Section III contains the
C-reports which have been declassified. These reports
still carry the C designation preceding the number.
Section IV contains the translations, which are num-
bered as T-1, T-25 and so forth. Numbers listed with-
ow titles are either unpublished or not available for
distribution. Missing numbers in the list are for
classified reports not included in this list.
ASTRONOMY
fcnnsylvania U. , Philadelphia.
THE CORRELATION OF STELLAR SHADOW BAND
PATTERNS WITH UPPER AIR WINDS AND TURBU-
LENCE, by W. H. Protheroe and Kwan-Yu Chen. Final
technical rept. on Contract jSF 19(604)1570. 1 Sep 60,
16lp. 11 refs. CRD no. TR^ 60- 287; AD- 245 500.
Order from LC mi$7.80, pl^25.80 PB 152 834
Measurements leading to a correlation of stellar
•clntillation and upper air \%4nd8 have been made using
two techniques. The first c(^nsisted of comparing the
ratio of the high frequency component, 300 ops, to the
low frequency component, lO cps, of the scintillation
■ignals derived using a telescope of 4-in aperture, to
upper air winds as measured using GMD-1 rawinsonde
equipment or CPS- 10 radar equipment. The correla-
tions lead to a relationship of the form V » aR^, where
V is the speed of the winds, a and b are constants, and
R is the ratio of the 300 cps signal to the 10 cps signal.
By using a rotatable lx4-in slit a directional effect in
the scintillation is found which correlates with the
uppser air wind direction. An analogue computer for
determining the autocorrelation function of an elec-
trical signal is described. The second technique
utilizes the Optical Fourier Analyzer, whidi permits
the direct measurement of th^ spatial power spectrum
of a 2-dimen8ional function which is, or can be, rep-
resented by a 2-dimen8ional light pattern. The shadow
band pattern associated with stellar scintillation is
actually in motion with directions and speeds in the
usual range of the upper air winds. The technique
permits the direct determination of this velocity in
units of m/sec. The pattern is continually changing,
showing decay times which are measured in millisec-
onds. The spatial power spectra show that the usual
pattern has elements with a characteristic size erf the
order of 15 cm on the average, but that the character-
istic size can frequently be larger than this value, the
actual size being indeterminate due to instrumental
limitations. (Author)
Astrophysics
Aero-Space Labs. , North American Aviation, Inc.
[Downey, Calif. ]
GEOPHYSICS AS APPLIED TO LUNAR EXPLORATION
by J. Green. Final rept. on Contract AF 19(604)5886.
30 June 60, 280p. 26Zrefs. MD 59-277; AFCRL-TR-
60-409; AD- 245 513.
Order from LC mi$ll. 10, ph(42.60 PB 152 846
This report released for sale to the public 17 Jan 61.
Recent geophysical literature was applied to lunar ex-
ploration. Simple combinations of already existing
hardware were prescribed to perform specific geo-
physical tasks on four vehicles. Experiments and sur-
veys were discussed and described for use in hovering,
surface, and subsurface probes. For the hovering and
257
I
surface aurveys, certain mor|)hologlcal features of
Impected and volcanic terrains were described. Em-
phaaiB was placed cx| caldera and lava plain features
because of ^e advantages that volcanism offers over
impact processes with regard to terrain and minerali-
zatiOii. Comparison [curves of Keophvslcal instruments
over craters of the t|wo opposing mechanisms of origin
are compared. The I wo -curve magnetometer offers
much in terrain analysis of the lunar surface. Instru-
mentation details of kelevisian and infrared surveying
are detailed. A nested geophone and pulser define a
possible system for both surface and subsurface seis-
mic research. For iiurface and subsurface analysis,
specific adaptations oi conventio.ial well logging de-
vices, both horizontal and vertical, are outlined with
emphasis on the seaich for water. Four instrumented
vehicles, two hovering and two scrft-landed, are
described for the pei'formance of specific missions.
(Author)
High Altitude
HEUUM
PHERE. by Hollis
tific repc . no . 28 on
Sep 60, 69p. 110
Order from LC nru$
Obsetvatory, Boulder, Colo.
gQUlUBRlUM IN THE SOLAR ATMOS-
Johnson (Doctoral thesis). Scien-
Contract AF 19(604)2140.
reft. AFCRL TN-60-652.
90. ph)10.80 PB 152 946
Chap. 1. Helium liress in the solar spectrum
Chap. 11 . The equili >num of a radiating gas
Chap. Ill . Parametric solutions of the equilibrium
equations for Hel
Chap. IV. A self-cotisistent solution for Hel
Chap. V . Temperatiire in the helium chromosphere
Chap. VI . Turbulence in the helium chromosphere
Lockheed Aircraft [:k)rp. , Sunnyvale, Calif.
DEVELOPMENT OF A COMPUTER SUBROUTINE FOR
PLANETARY AND LUNAR POSITIONS, by Herman F.
Michielsen and Mart n A. Krop. Rept. on Contract
AF 33(616)6638. Auj 60. 99p. 9 refs. LMSD rept. no.
311864; WADD Techi jcal rept. 60-118.
Order from OTS $2. J5 PB 171 1%
Ephemerides of the nine major planets and the Moon, as
obtained from the Arierican Ephemeris and Nautical Al-
manac, are processed and converted into a format spec-
ifically tailored for i^se in space flight activities. The
original degree of accuracy is maintained throughout.
The information is aven with respect toaninertial ref-
erence system, theTi^an Equinox 1950.0, and ex-
pressed primarily irj rectangular coordinates, although
spherical coordinate^ are also obtained. The ephemer-
for the planets and geocentric or
loon. The report is an explana-
of the computer subroutines de-
he IBM 709 or Remington Rand
1 103AF computers. fThese subroutines determine, at
the option of the usei, either exact ephemerides or ap-
proximate positions. The former are only available for
a limited period of tfrie (presently 1960-1963). The
latter are valid for many decades in the future and in
the past. This appro0cimate ephemeris Is of sufficient
accuracy to be used lis a basis for the planning and de-
sign phases at a spa^e flight project and, to a large ex-
tent for the determination of perturbations in actual
flight plan analyses. (Author)
ides are heliocentri
heliocentric for the
tion and substantiati
veloped for usage in
Maryland U. . College Park.
DISTRIBUTION OF DENSITY IN A PLANETARY
EXOSPHERE, PART n, SUPPLEMENT, by E. j. Oplk
and S F. Singer. Rept. on Contract AF 19(604)3861.
14 Oct 60, 9p. 12 refs. CRD TN-60-606, suppl.
Order fran IX mi) 1.80, phll. 80 PB 152 936
The approach and results obtained in a previous paper
(CRD- TN-60-606, PB 149 952) are compared with those
obtained by Chaniberlain(A8trophys. J. 131, p. 47-56,
1960), by Johnson and Fish (A atrophy s. J. 131.
p. 502-515, 1960), and by Brandt and Chamberlain
(Physics of Fluids 3, 485, 1960).
Minnesota U. School of Physics, Minneapolis.
BALLOON STUDY OF HIGH ALTITUDE RADIATI04S
DURING THE INTERNATIONAL GEOPHYSICAL YEAR,
by John R. Winckler. Rept. on 2. 12 Cosmic Ray In-
tensity at High Altitude, Contract [Nonr-710(19)1.
Mar 60, 69p. 38 refs. Technical rept. no. CR-26;
AD- 238 764.
Order from LC mi$3.90, ph$10.«0 PB 148 494
Results of a series of 85 constant level balloon flights
to measure cosmic rays and other types of radiation at
high altitude are summarized. Each flight carried an
ionization chamber, a Geiger counter, and nuclear
emulsions, and renuined at about 10 g/sq cm depth for
times between 2 and 24 hr. The majority of flights were
made at Minneapolis, Minn. The large decrease in
primary cosmic ray intensity between 1956 and 1958
was observed at high altitude. The high altitude meas-
urements correlate with sea level neutron instruments.
Many special events were detected, including x-rays
produced by electrons incident on the atmosphere dur-
ing strong aurorae and solar cosmic rays deteaed oo
10 occasions and correlating with other known obaerva-
tions made in the polar regions. In one case y-rays
originating on the solar surface were detected in a
short burst. Several cases of radioactive layers in the
atmosphere at low level resulting from nuclear explo-
sions were found. (Author)
Minnesota U. School of Physics, Minneapolis.
OBSERVATIONS OF THE VAN ALLEN RADL\TI(»I
REGIONS DURING AUGUST AND SEPTEMBER 1959,
PART I, by R. L. Arnoldy, R. A. Hoffman and
JR. Winckler. Rept. on Cosmic Ray Program, Coo-
traa NASw-56. Mar 60. 41p. 13 refs. Technical rept.
no. CR 25; AD- 235 804.
Order from LC mi$3.30, ph$7.80 PB 149 645
An integrating ionization chamber and a single Geiger
counter were flown on V- S. satellite Explorer VI in an
elliptical orbit extending to 48,000 km. In addition to
the Van Allen inner zone and the great outer zone, a
stable and distinct intermediate zone was deteaml
throughout August and September 1959. The outer woe
intensity showed a large decrease following the sudden
commencement of a geomagnetic storm. Later in the
storm the outer zone increased to much in excess ol
its pre-storm level. During stable periods the outer
zone was fairly constant and less intense than observed
with Pioneer III or Pioneer IV on the first Soviet cosmic
rocket. Cosmic ray background counting rates were
reached on most passes in August and September near
apogee of the satellite. The radiation dumped from the
2S6
outer zone during the geomagnetic storm fits very well
with the intensity and latitude distribution required to
gccount for balloon observations of auroral x-rays
made during the IGY period. (Author)
Minnesota U. School of Ptysics, Minneapolis.
yrANDARDIZATION OF ibNIZATION CHAMBERS, by
R. A. Hoffman. Rept. on 2. 12 Cosmic Ray Intensity at
High Altitude, Ckjntraa [Nonr-710(19)I. Mar 60, 45p.
26 refs. Technical rept. CR-27; AD- 238 765.
Order from LC mi$3.30, f|h$7.80 PB 148 495
I
Introduction: time variatidhs of cosmic rays: brief
description of instruments| measurement of the energy
flux. Methods of standardization of the chambers: cali-
bration of charge per pulse: electrometer amplifier,
calibration of the condenser, three calibration methods,
discussion of the calibration; Co"^ gamma calibration:
normalization factor, constant curreiK from Co"^
source, other corrections; results and errors. Con-
tinuous current chamber: construction; current under
the Ck>^ source. Application to balloon flights: nor-
malized charge/pHilse; nor^lized rate of ionization;
example data. Intercomparison of results with
H. V. Neher.
I
j
New Mexico State U , University Park.
HEAVY NUCLEI COMPONENT OF THE COSMIC
RADIATION AT BALLOON ALTITUDES, by Robert E.
McDanlel. Rept. on Contract AF 29(600)2025. Sep 60,
26p. 10 refs. AFMDC TR-60-28.
Order from LC mi$2. 70, ph$4. 80 PB 152 968
Nuclear emulsions were ex|;}osed to the cosmic radia-
tion on high altitude balloon flights from a geomagnetic
latitude of approximately 55°N and were examined for
tracks of nuclei of charge greater than or equal to 6.
These tracks were analyze^ for charge and energy dis-
tribution. The tracks caused by nuclei al energy
greater than approximately. 800 Mev/nucleon were
identified by a combination of gap density and delta-ray
dsaaity measurements. Tracks of energy less than
no Mev/nucleon had their energy and charge deter-
mined by the variation of delta-ray density with range.
The nuclei were divided into three charge groups:
M(6lZ <10), H(Z210), VH(Z220). The flux ob-
served on Flight 1 was 8. 2!± 1.6 particles/m^/sec/Sr
and the M/H and M/V H ratjos were 2. 4 ±0. 6 and
10. 3 ±2. 6, respectively. The charge and energy of the
low energy tracks were tabulated. The average flux
observed on Plight 2 was 7, '9 ± 2.0 particlea/m^/sec/St
and the M/H and M/VH ratjos were 3. 2 ±.0. 8 and
15.5 ±4.0 respectively. (Author)
Ohio State U Research Foundation, Columbus.
STUDY OF LUMINOSITIES OF LONG -PERIOD
VARIABLES (AND] ABSOLUTE MAGNITUDE OF
THE MIRA VARIABLE X I^ONOCEROTIS, by Philip
C Keenan. Final rept. for Jl Oct 58-31 Dec 59, Con-
tract Nonr- 2530(00). Feb 60, 9p. Rept. 823-1;
AD- 236 460.
Order from LC mi$l. 80. ph$l. 80 PB 152 171
R
A two-dimensional classification was extended to
more than 50 Mira variable^. The need for some in-
dependent calibration of thetlassif ication in luminosity
led to the study of the interstellar D-lines in the vari-
ables of high velocity. Individual absolute magnitudes
are available for only 2 Mira variables (X Oph and
X Mon) in the northern sky, but the agreement of their
values with statistical means lends support to the con-
elusion that the majority of these stars have visual ab-
solute magnitudes near -0. 5 to -1. 0 at maximum light.
The classification suggests that there are a few of
higher luminosity that could be termed sup^rgiant
variables. (Author)
lYerkes Observatory, Williams Bay, Wis. J
NAVY WIDE PHOTO GUIDE RESEARCH, by Helmut A.
Abt. Final rept. on Contraa N6ori- 02054. 10 July 59,
Ip.
Order from LC mi$ 1 . 80, ph$ 1 . 80 PB 153 278
BEHAVIORAL SCIENCES
Human Engineering
Dunlap and Associates, Inc. , Stamford, Conn.
TRACKING TRAINING IV: DESIGN AND UTILIZA-
TION OF THE GENERAL VEHICULAR TRAINER, by
Hugh M. Bowen. Charles R. Kelley and Jerome H. Ely.
Rept. on Contract Nonr- 1908(00). 29 Aug 60, 59p.
5 refs. Technical rept. NAVTRADEVCEN 1908-00-4.
Order from LC mi$3. 60, ph$9. 30 PB 150 317
A design of a Oneral Vehicular Trainer (GVT) is given
in detail. The trainer is designed to accomplish the
preliminary training in vehicular control for trainees
who are in the early stages of training courses for
pilots, submarine helmsmen/planesmen, surface ship
helmsmen, land vehicle drivers, etc. The major char-
acteristics of the GVT are simulation of forward
movement through space as shown by an instrument
panel displaying vehicle motions and states in the ver-
tical and horizontal dimensions; simple and inexpen-
sive construction; variable dynamic characteristics
(lags, stability, responsiveness, speed, etc. ) able to
resemble a wide range of vehicular systems; integral
scoring circuits providing knowledge of results. Rec-
ommendations concerning utilization practice and the
design of a field evaluation test are given. An experi-
ment is reported which compared nine methods of
scoring. The nine methods all used the integral of ab-
solute error measure but had different dead-bands (no
error accumulated when deviation is + i volts from
zero) and different time delays (the scoring started i.
seconds after the start of the problem). It was con-
cluded that no advantage is to be gained from employ-
ing any dead -band, or any time delay. A discussion of
the major recommendations arising frcmi the series of
studies (of which this is the fourth) concludes the
report. (Author) (See also PB 146 878)
Rowland and Co. , Haddonfield, N.J.
A METHOD OF MAKING DIMENSIONAL MEASURE-
MENTS OF COMPLEX MOTIONS, by George E.
Rowland and Charles E. Kulp. Rept. on Contract Nonr-
2856(00). 31 Mar 60, 65p. 10 refs. R i C rept.
#60-1-2; AD- 240 350.
Order from LC ml$3.90, ph$10.80 PB 149 211
/
259
Using the method described, determination can be made
of the four dimensional coordinates of any given point
of interest. This ts accomplished through adjusting the
image size of a onle- camera motion picture photographic
view of a sphere aE> that it is reconstituted in actual
•ize. This restorltion erf correct projection size
■ImuJtaneousIy solves all the problems of parallax
which have previo(isly blocked practical photographic
measurements of this kind. Use of the method permits
photographic recording and resultant readout of the
envelope of space required for the execution of complex
motions. Processed data portraying the exterior dimen-
sions of the total ipace envelopes required by the
human for certain usks are present^. Although the
technique has beeij demonstrated using human bio-
mechamcal motioqs, there is no apparent reason why
the technique coul^ not be applied to mechanical
motions in genera
)
Per^nnel and Training
I
American Inst, (jar Research [Pinsburgh, Pa.]
AFFECTIVE AND! ACCEPTANCE FACTORS IN
SELECTION AND; UTILIZATION OF TRAINING AIDS
AND DEVICES, bVArmandN. Chambers. Rept. on
Contract N61 339-4?. 26 Nov 58, 53p. Technical tept.
NAVTRADEVCEN 9-11-1; AD-214 729.
Order from LCmttS. 60, ph$9. 30 PB 149 642
An attempt was m#de to identify some of the factors
other than training value which influence the choice
among available training aids, the amount of utilization
of various training aids, and the writing of require-
ments for training; aids by instructional personnel and
training supervisoi's. Individual interviews were con-
ducted with 21 instructors and 24 other personnel con-
cerned with Naval training where transparencies,
animated panels, models, cutaways, and mockups are
in use. Data indiqated that instructcx's prefer aids
which enibody realism, are readily procured, avoid
distraction, and pl^ovlde flexibility. They rate highly
the ability ctf a training aid to provide variety. To meet
these criteria, the^y prefer operational equipment,
transparencies, ct|arts, and animated schematics.
They neither like tlor use equipment panels. Films and
photographs also rjank low in their choice. Training
aids and devices «iere believed essential to classroom
teaching.
American Inst. fi>r Research, Pittsburgh, Pa.
A SURVEY OF CUEING METHODS IN EDUCATION
AND IN AUTOMATED PROGRAMS, by Leslie J.
Briggs. Rept. on (jontract AF 49(638)681. May 60,
44p. 14 refs Research rept. AIR-314-60-IR-106;
AFOSR TN-60-286; AD- 238 967.
Order from LC mi$3. 30, ph$7. 80 PB 153 460
This report releas^ for sale to the public 18 Jan 61.
This report discusses methods used by teachers and
writers of auto-inaructional programs in cueing or
prompting students| to maximize the likelihood of their
giving the correct responses to instructional exercises.
The use of direct v romixs versus less direct forms of
cueing is discussed and illustrated. The relative ab-
sence erf evidence on cueing technique from studies in
the experimental laboratory is noted. Teacher tech-
niques in starting with minimal cueing and proceeding
to more direa prompts are pointed out, and prompting
features of some training devices are described.
Crowder's intrinsic programming method is discussed
from the standpoint of cueing. Specific cueing tech-
niques used in "Skinner-type" programs by Holland
and others are illustrated and briefly commented on.
(Author)
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright-Panerson AFB, Ohio.
A BIBUOGRAPHY OF AEROSPACE MEDICAL DIVI-
SION REPORTS IN THE FIELDS OF ENGINEERING
PSYCHOLOGY AND TRAINING PSYCHOLOGY. 1945-
1960, comp. by Sandra A. Stevenson. May 60, 53p.
508 refs. AD- 243 253.
Order from arS$ 1.50 PB 171 332
A complete bibliography of the Memorandum Report,
Technical Report and Technical Note publications <rf the
Engineering Psychology Branch and the Training
Psychology Branch Is presented. This bibUography in-
cludes all published reports resulting from contract
and in-house research from 1945 to 1960. There were
additional reports emanating from the Psychology
Branches which were published in open professional
journals. These reports were not included in this bib-
liography. The references are grouped by functional
or subject-matter areas. Within an area, the refer-
ences are listed alphabetically using the authors'
names. In addition, in the Index, the reports are
referenced by author and by report number. (Author)
Dunlap and Associates, Inc. , Stamford, Conn.
RECENT INNOVATIONS IN METHODOLOGY FOR
TRAINING AND TRAINING RESEARCH, by Alfred F.
Smode and Kenneth W. Yamold. Rept. on Contract
Nonr- 2490(00). Mar 60. 92p. 202 refs. AO-235 806.
Order fromLC mi$5. 40, ph$15. 30 PB 147 306
Contents:
New wajrs of determining the requirement for training
Procedures for the analysis of task requirements
New ways of providing learning experience
Types of problems or tasks
Complex devices that provide opportunities for sys-
tem training
Establishing and/or controlling the working environ-
ment
New ways of measuring the progress and outcomes of
training
Observing and recording force activity behavior
Scoring and recording devices
Motor skill scoring
Analyzing data from learning studies
New ways of providing knowledge of results
Information feedback as a factor in learning
Motivational aspects
Knowledge of results and reinforcement
260
i
I
Educational Research Coi^. [Ombridge, Mass. ]
STABILITY OF INTEREST MEASURES AND THEIR
VALIDATION FOR SELECTION AND CLASSIFICA-
TION, by R. F. Schweiker. Rept. on Contract
AF 18(600)1358. May 59. 55p. 2 refs. WADC-TR-59-
36; AD-215 482.
Order from LC mi$3. 60, ph$9. 30 PB 153 631
This repon released for sale to the public 10 Jan 61.
To determine the suiubility of interest measures for
Air Force personnel procedures, two multiple -scale
interest measures, Activity Preference Report and
Opinion Inventory, were given to 16, 665 recruits en-
tering the Air Force, to 1, 465 erf the initially-tested
•Innen near the completion basic training, and to
1,043 of the initially-tested' airmen when completing
technical school for one erf five selected career fields.
Career Preference Items arid a Reenlistment Intent
Item were given in the first, two testings and measures
of satisfaction with the career field and the Air Force
•ere given in the third testing. Technical school
grades and aptitude indexes were obtained for the air-
men in the third testing. TTie interest measures and
die Reenlistment Intent Iteni indicated difference
among groups at the three faBs^c training bases and
among groups later assigned to the five career fields.
They also indicated that sortie changes occur during
basic training and technical school training. In a mul-
tifde regression analysis, the interest measures did
not provide useful prediction of school success, reen-
listment intent, or other indications of career satisfac-
tion. They are accurately measuring something of im-
portance, but additional analyses are necessary to de-
terrnine how this information can best be used by the
Air Force. (Author)
Human Resexirces Resea rch Office , George
Washington U. , Washington, D. C.
A FOLLOW-UP STUDY OF; EXPERIMENTALLY AND
CONVENTIONALLY TRAINED FIELD RADIO RE-
PAIRMEN, by George H. Brown and Robert Vineberg.
Rept. on Contract DA 49-106-qm-l. Sep 60, 33p.
3 refs . Technical rept . 65; AD-245 468.
Order from LC mi|3.00, p«$6.30 PB 152 788
Approximately 70 graduates) each of an experimenul an
a conventional Field Radio Repair course were recon-
Ed after about nine months' field experience to de-
Ine their relative proficiency at that time. The ex
nental course had emphasized recognition and cor-
ntetlon of the most common troubles in the most freq-
uently repaired items of equipment and provided the re
pairman with a systematic trouble shooting procedure;
it also incorporated "Functional Context Training"
which featured, for example, presentation of theoretica
material in a maintenance -oriented context. The exper
mental course had produced. graduates who were
markedly superior to the standard ccxirse graduates at
the time of graduation . At the lime of retesting, the rwc
groups of graduates were substantially equivalent in
their repair proficiency. It is concluded that althouglv.
the instruction received by the experimental graduates
«*t less oriented toward th^ry than was the standard
instruction, this did not place the eiqjerimental subjects
at any disadvantage as compared with the standard
graduates. (Author)
Human Resources Research Office, George
Washington U. , Washington. D. C.
ON-SITE TRAINING OF GUIDED MISSILE OPERA-
TORS, by Myron Woolman. Rept. on Contract DA 39-
106-qm-l. Aug 60. 148p. 9 refs. Technical rept. 64
and Suppl. ; AD-244 250.
Order from LC mi$7. 20, ph$22. 80 PB 152 580
The study was cexicerned with developing and testing a
method of training Nike IFC operators on site. In a
five-month field test, three experimental methods were
compared with conventional training. The principal ex-
perimental methexl- -Operational Context Training
(OCT)- -was incorporated in a Training Guide that in-
cluded (1) a step-by-step breakdown of all operator
procedures. (2) specific instructional techniques for
use by battery personnel without experience as instruc-
tors, and (3) a systematic method of evaluating train-
ees. Operators trained by the various methcxls were
compared by means of job -sample and written criterion
tests, and by other measures. Operators trained by
the OCT method were more proficient than those
trained by the other methods in the study; OCT-trained
e)peratorB were as proficient as school -trained person-
nel with greater on-site experience. (Author)
Naval Personnel Research Field Activity. San Diego,
Calif.
A FOLLOW-UP ANALYSIS OF THE NEW COMPOS-
ITE SYSTEM FOR SELECTING NROTC REGULAR
STUDENTS, by Bernard Rimland. Mar 60. 16p. 3 refs.
BuPers Technical Bulletin 60-8; AD-244 663.
Order from LC mi$2. 40. ph$3. 30 PB 152 626
An analysis was made of test scores and other Infor-
mation from the application files of 300 men chosen to
represent a random sample of applicants to the 1959
NROTC Regular Program. By comparing the scores on
the several selection instruments for the "selected"
group of 100 with the scores for the "non- selected"
group of 200. it was possible to assess the extent to
which each instrument had been usedbythecomminees
in making selections. The analysis showed that the
new selection procedures, thcxigh optional, had been
widely adopted by the State Selection Committees.
Some 80 per cent of the application files carried the
new Academic and Career Composite scores recom-
mended as part of the new procedures. A newly de-
veloped scale for facilitating the use of interviewer
judgements of career motivation made a significant
positive contribution to the 1959 selection program.
Also in line with the new recommendations, the over-
all interviewer's rating of the applicant, heavily over-
weighted by the Selection Committees in previous
years, was given a more moderate and appropriate
place in the selection program. The new selection
procedures are considered to be making a substantial
improvement in the quality of input to the NROTp pro-
gram and should be continued in use. (Author)
Personnel Lab. . Wright Air Ctevelopment Div. ,
Lackland AFB. Tex.
DEVQ.OPMENT OF SPECIALlTy OUTLINES FOR
COLLECTING JOB INFORMATION IN THE RAMO-
RADAR SYSTEMS CAREER FIELD, by Gordon E.
Cowan. Aug 60, 24p. 3 refs. WADD-TN-60-213;
AD- 243 826.
Order from LC mi$2. 70. ph$4. 80 PB »2 783
261
A study was made to investigate the feasibility of using
an instrument with standard functional work categories
to collect occupatisnal information across different
specialties of a maintenance career field and at two
skill levels. Spetialty Outlines were developed for the
5- and 7-skill lev^l for six AFSCs in the Radio-Radar
Systems career fif Id and administered to teams of pro
ficient NCO incumlients. The 7 -level outlines were
administered twlct with a five -week interval and the
5-level outlines w^re administered once. Analysis of
variance techniques were applied to estimates of the
percentage of time spent on each of 13 standard func-
tional work categdries. Each team of specialists was
interviewed to discuss the content and format of the
outline for their fitPSC. Results of the analyses and
interviews indfcatc that Specialty Outlines using stand-
ard functional work categories are (1) reliable instru-
ments, (2) adequate for use across different APSCs of
a maintenance caiieer field at both the 5- and 7 -level,
and (3) differentiate between the work activities of 5-
and 7 -level airmeh. (Author)
Personnel Lab. , iWright Air Development Div. ,
Lackland AFB, ifex.
FACTOR AhMLYlJlS OF WAF PEER NOMINATIONS,
by Lois Lawrence Elliott. Sep 60, 15p. 5 refs. WADD
TN-60-217.
Order from LC mi$2. 40, ph$3. 30 PB 153 506
A factor analysis of the intercorrelations of 30 peer
nomination variables, aptitude, age, and success or
failure for WAF irt basic training yielded seven factors
The three major factors represented dimensions of
leadership, heterosexual adjustment, and agreeable -
ness. The remaining dimensions were motivation,
emotional maturitV, neatness, and feminine interests-.
(Author)
PSYCHOLOGICAL
CLASSIFICATION
Personnel Lab. | Wright Air Development Dlv. ] - ^
Lackland AFB, "^ex.
TESTS AND THE SELECTION AND
OF AIR FORCE OFFICERS, by
Ernest C. Tupes 4nd Raymond E. Christal. Apr 57,
21p. 75 refs. Devtlopment rept. AFPTRC-TN-57-52;
AD- 126 383.
Order from LC m $2. 70. ph$4. 80 PB 153 572
This report releaied for sale to the public 4 Jan 61 .
Aptitude tests have proved highly effective as a means
of selecting office^ personnel. They are generally use*
in officer selection programs but are not yet fully ex-
ploited in officer classification. As appropriate instru
ments are developed, wider use can be made of apti-
tude tests in the cjassification of officers. Develop-
ment of motivatio^ and personality tests related to
proficiency in specific job areas may increase pre-
cision of officer c assification and, perhaps, add to
the effectiveness 6[ officer selection programs.
Tennessee U., Wnoxville.
DIMENSIONS OF AIRMAN MORALE, by Edward E.
Cureton. Rept. oi Contract AF 41(657)247. June 60,
" ' WAX) TN-60-137.
75p. 10 refs
Order from LC m*4.50. ph$12.30
PB 153 271
In an attempt to determine and measure aspects of air-
man morale, 167 questionnaire items were assembled
and administered to a thousand airmen. By cluster and
factor-analytic techniques, eight scales were derived,
one of them defined as a measure of General Morale.
Three of the scales are fairly independent of each
other, but closely related to the General Morale Scale:
satisfaction with the Air Force as a Whole, with Man-
agement and Communication , and with the Unit and its
Leadership. The remaining four scales are relatively
independent of all other scales: satisfaction with the
Immediate Supervisor, with the Air Force as a Mili-
tary Organization, with the Job, and with the Civilian
Community. The Supervision scale is the only one
clearly defined as measuring a uniquely identified
facet of morale. For the other scales , a different
approach in the analysis could yield another equally
defensible set. Technical appendixes give the analyti-
cal and statistical detail. (Author)
Psycholog)^
Adjutant General's Office, Washington, D. C
SYSTEMS RESEARCH- -OPPORTUNITY AND CHAL-
LENGE FOR THE MEASUREMENT RESEARCH
PSYCHOLOGIST, by Julius E. Uhlaner. July 60, I7p.
5 refs. PRE Technical research note 108. AD- 244 856.
Order from LC nU$2. 40. ph$3. 30 PB 152 757
Systems research is examined from the point of view d
the human faaors research scientist dealing with mili-
tary problems. The measurement research psycholo-
gist can use the systems approach to advantage, par-
ticularly where the objective is improvement of a total
operation through optimal balance of critical factors.
At the same time, he is in a position to influence de-
velopment of systems research methodology, coiKrib-
uting design and techniques for such objectives as
identification and definition of critical faacrs and the
development of a common metric with which to evalu-
ate man and machine performance. A suggested frame
work for human factors oriented systems research is
organized around three basic elements: (I) systems
components to be studied (independent variables), (2)
output or performance (dependent variables), and (3)
conditions or environment in which the system
operates. (Author)
Adjutant General's Office, Washington, D C
VALIDATION OF COMMON CORE PATTERN AN-
ALYSIS AND MECHANICAL KNOW!. EDGE TESTS
FOR MECHANICAL MAINTENANCE COURSES, by
William H. Helme, James B. Trump and David J.
Pitch. July 60, 20p. 4 refs. PRB Technical research
note 107: AD- 244 855
Order from LC mi$2. 40, ph$3. 30 PB 152 756
Two experimental tests. Pattern Analysis and Mechan-
ical Knowledge, developed under a joint Armed Ser-
vices program to provide common core classification
tests, were evaluated for Army use in classification
to three mechanical areas. The experimental common
core PA was less effective than the operational PA,
both singly and in combination with other Army Class!'
fication Battery tests. The Mechanical Knowledge Test
262
«M a promising predictor, particularly for motor
maintenance jobs. Definitive evaluation of MK suit-
ability for the ACS requires validation for additional
mechanical areas, as well as comparison with other
measures under development to improve differential
claaaification within the mechanical domain. (Author)
Air Force Missile Development Center, HoUoman
AFB, N. Mex.
COMPLEX AVOIDANCE BEHAVIOR IN THE CHIM-
PANZEE AND ITS APPLICABILITY TO THE STUDY
OP SPACE ENVIRONMENTS, by Richard E. Belle-
ville, Frederick H. Rohles^ Jr. and others. Sep 60,
20p. 10 refs. AFMDC-TR -60-27.
Order from LC ml$2. 40, ph$3. 30 PB 152 744
This report describes the concurrent development of
two types of avoidance behavior in the chimpanzee in
which a discrete avoidance task was super-imposed on
a schedule requiring continuous avoidance behavior.
The rationale for using these tasks for measuring the
behavioral effects of spacej flight Is presented. (Authoil
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
SOME FACTORS IN THE EMOTIONAL ADJUSTMENT
OF RADAR OBSERVERS IN JET FIGHTER INTER-
CEPTOR AIRCRAFT, by Joseph J. Reidy and
Horace F. Drury. Nov 53.i9p. ProJ. no. 22-1201-0000.
Special rept. no. I.
Order from LC mil 1.80, ph$ 1. 80 PB 153 325
The permanent assignment of each radar observer to a
specific pilot was an important factor in the signifi-
cantly better adjustment of the second group. The al-
ways desirable screening for size and body build in re-
lation to aircraft crew space in the selection of radar
observers is particularly important in climates where
beavy clothing must be worn for survival following
crash landing or bail-out aod where accessory survival
equipment must be carried attached to the parachute
during flight . Although the severe cold dlimate of the
theater appeared to have no effect gsi i£ on the results
noted, the buUdness of the clothing required and the
resultinR impairment of motion, excessive time
required for dressing and the inconvenience of having
to wear much of the clothing for long periods on the
ground while on standby foe alerts were constant
sources of annoyance and complaints .
Aviation Psychology Lab. , U. of Illinois. Urbana.
ISSUES IN THE USE OF AN ANALOG -DIGITAL
DATA SYSTEM FOR THE MEASUREMENT OF
TRACKING BEHAVIOR, by Carl E. Webber and Jack
A. Adams. Technical note on Contract AF 49(638)371.
Apr 60, 38p. 6 refs. AFOSR-TN-59-528; AD- 245 064.
Order from LC ml$3. 00. ph$6. 30 PB 152 703
Tracking data collected by an analog -digital data sys-
tem and processed with a digital computer is recom-
iHsnded as a solution for certain research restraints
Iniposed by the traditional methods of measuring track-
ing behavior. An experiment on system parameters
performed entirely on a digital computer, evaluated
■ainpllng rate and number of digits per reading of sim-
ulated tracking error functions for time on target
measures. The Sampling Theorem recommending a
sampling rate twice that of the highest component fre-
quency in the analog signal is sound for time on target
computations, but somewhat lower rates appear ac-
ceptable for many applications. Empirical tracking
data obtained with an analog -digital data system is
presented. (Author)
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright-Patterson AFB. Ohio.
JUDGMENTS OF THE RELATIVE FREQUENCY OF
TWO RANDOM SEQUENTIAL EVENTS: EFFECTS
OF DURATION OF OBSERVATION, by Dwight E.
Erlick. Rept. on Design Requirements for Decision-
Making Displays. Sep 60. lOp. 1 ref. WADD Tech-
nical rept. 60-673.
Order from OTS $0.50 PB 171 313
The purpose of this investigation was to determine tjie
effect that duration of observation has on one's ability
to tell which at two random sequential events has oc-
curred more frequently. Using a rate of four events
per second and observation durations ranging from
1 . 75 to 80 seconds, two specific conditions were
studied: (1) the effect ot having a constant observation
period repeated so that §s could anticipate the duration
of each observation, and (2) the effect of having a
highly variable observation time such that the observer
could not accurately anticipate when the time sample
would end. Using 75 per cent correct identification of
the more frequent event as a threshold measure, the
results indicate, for both presenution conditions, that
a smaller Increment In frequency erf one of the events
over the other was needed as the observation duration
increased. An asymptote was reached as the ratio be-
tween the more frequent and the less frequent event
approached 1 . 20. With a constant observation time,
the asymptote is reached between 10 and 20 secoiKis
duration, while with a variable observation time, it is
reached between 40 and 80 seconds. (Author)
Hughes Aircraft Co. , Culver City, Calif. '
OPERATOR PERFORMANCE IN STRIKE RECON-
NAISSANCE, by A. C. Williams, Jr. . C. W. Simon and
others. Rept. on Human Performance in Advanced Sys-
tems, Contract AF 18(600)1798. Aug 60, 8lp. 137 refs. f
WADD Technical rept. 60-521. S
Order from LC ml$4. 80, ph$l3.80 PB 153 387 I
The purpose, requirements, and constraints of the
tactical strike -reconnaissance mission are analyzed.
The properties and applications of various sensors and
their associated displays, the operator's task, vari-
ables affecting his performance, and the operator him- t
self were all considered in this analysis. Two experl- ^
mental studies were conducted. The first was a clini-
cal investigation of the effects of variations in display
resolution and scale factor upon operator performance
in target identification. The second was a quantitative
experiment to determine the feasibility of predicting
the identif lability of ur^gets on the basis of their visible
physical attributes revealed at various display reso-
lutions. The results suggest that such predictions are
possible. A bibliography of studies related to this area
16 appended. (Author)
263
Human Factor! Research, Inc., Los Angeles, Calif.
A STUDY OF INDIVIDUAL DIFFERENCES IN VIGI-
LANCE PERFoKmaNCE, by Donald N. Buckner,
Albert Harabedijan, and Janies J. KfcGrath. Technical
rept. no. 2 on Hunran Factor Problems in Anti-Subma-
rine Warfare. Ctontract Nonr- 2649(00). Jan 60. 50p.
15 refs. AD- 23k 897.
Orxler from LCkni$3.30, ph$7.80 PB 152 888
The statistical $nd practical significance of individual
differences between sonar operators in vigilance per-
formance, and fie reliability of individual differences
both within a wiitch and from one watch to the next
were determinep . The relationship between the per-
formances of the same individuals under alened and
ordinary watch fetandin^^ronditions was also investi-
gated. Fifiy-fofr men stood 2 one-hour watches a day,
4 days a week , tor 4 weeks . Half of the watches were
on a visual and half on an auditory vigilance task, and
the men were required to detect brightness or loud-
ness differences . A rapid decrement in detection
performance oq:urred between the pretest (alerted
condition) and tke beginning of the watch. This decre-
ment probably did not reflect a loss in the men's ca-
pacity to detectithe signals since perfornuince re-
turned abruptlyiand con^letely to the pretest level on
the posttest. Rather, it probably reflected a differ-
ence in the meifs set toward the tests as oppo'sed to
the watches . ln|lividual differences became larger as
the watch progrfessed. and were reliable both within a
given watch and) from one watch to the next . About
75% of the decrement in performance during the
watches occurred within the first 20 min. Men who
were visually a|id aurally more sensitive performed
the sonar detection task bener.
Lincoln Lab. , 'Mass. Inst, of Tech. , Lexington.
EXTENDING TllE SUCCESSIVE INTERVALS MODEL
TO THE MULltlDIMENSIONAL CASE, by William P.
Harris. Rept. dn Contract AF 19(604)7400. 14 Oct 60,
I2p. 2 refs. 58C-0015; AD-244 679.
Order from LC (ni$2. 40. ph$3. 30 PB 152 621
It is shown howfThurstone's Successive Intervals
method may be Extended to multidimensional data when
the subject responds to several attributes of a stimulus
on each trial, "the method requires that the subject
make simultanilpus judgments about N anributes of
each stimulus ii two or more categories per attribute.
The model says that the apparent magnitudes of the
anributes vary from trial -to-trial in an N-dimensional
multivariate normal distribution. This extension of the
successive intefvals model to many dimensions holds
promise to unccRrer some judgmental aspects of pattern
recognition behavior - - certainly mole ao than other
psychophysical hiethods.
Ohio State U. Research Foundation. Columbus.
ORIGINALITY 94 GROUP PRODUCTIVITY I. PRO-
DUCTIVE INDEl^NDENCE IN THREE NATURAL
SITUATIONS, bj Pauline N. Pepinsky. Rept. on Con-
tract Nonr-495(|5). 1959, 145p. 48 refs. AD- 231 067
Order from LC M7. 20, ph$22. 80 PB 152 913
indeper
Contents:
Productive independence on a university campus
Productive independence in a research institute
Productive independence in an architecturally planned
neighborhood
A conceptual transition to the laboratory
Personnel Lab. . Wright Air Development Div. ,
Lackland AFB, Tex.
A REVIEW OF SOME UTERATURE ON JUDGMENT
WITH IMPUCATIONS FOR JOB EVALUATION, by
Joseph M. Madden. Aug 60, 16p. 31 refs. WADD-TN
60-212.
Order from LC mi$2.40. ph$3.30 PB 153 llO
Jc^ evaluation has been described as a psychological
process closely resembling those which have been sub
jected to experimentation both in the laboratory and in
practical situations . It is based on the psychophysical
method of single stimuli . Predictions from previous
research indicate that the evaluation a job receives it
most reliable when it is judged in a group with other
jobs , and that the composition of this group influencei
the evaluation it receives . If the presence of these
context effects in job evaluation is verified, the next
step is to design an adequate procedure for their con-
trol. Determination of the optimal method of repre-
senting the job to the rater and an examination of the
effects of residual factors , such as familiarity of the
rater with the job being rated, may also suggest
changes in current job evaluation procedures . All of
these phenomena should be considered in their rela-
tionship to Air Force job-evaluation procedures.
(Author)
Psychological Lab. , U. of Southern California
[Los Angeles].
A F.ACTOR-ANALYTIC STUDY OF PROBLEM-
SOLVING ABILITIES, by P. R. Merrifleld, J. P Guil-
ford and others. Rept. no. 22 on Studies of Aptitudes
of High- Level Personnel, Contraa (N6onr-238(10)J.
Mar 60. 31p. 24 refs. AD- 237 752.
Order from LC mi$3.00, ph$6.30 PB 148 OW
A modified theory of problem solving was developed,
involving five phases: preparation, analysis, produc-
tion, verification, and reapplication . The study was
limited to six hypothetical component abilities, all
emphasizing aspects of the production phase. Tests ai
problems were restricted to the semantic or verbal
category. Twelve new tests were developed to investi-
gate the hypothesized abilities. Three additional new
tests were developed for use as criteria of success in
problem solving. They present problems in which the
solver's general task is to start with situational infor-
mation and goal information and to bridge the gap be-
tween the two. Eighteen marker tests of previously
known factors were included in the test battery. Ten
rotated factors were identified as previously known
dimensions, and a new factor was identified as conver-
gent production of semantic classes. The criterion
(problem- solving) tests had significant loadings on one
or more of four factors, all previously known. The
kind of test that seems most related to the criterion
tests was designed to measure abilities to work from
goal information. This suggests that the development
of a search model or anticipatory schema plays an
important role in solving problems of the kind included
In this study. There was no evidence of a unitary
problem- solving ability. Since much of the variances
264
of the problem- solving tests could be accounted for in
terms of known factors and no new factors seemed to
be needed, the hypothesis that problem solving can be
accounted for in terms of factors in the structure of
Utellect appears to be promising. (Author)
i
•Rutgers State U. , New Brunswick, N. J.
HOMEOSTASIS THEORY OF SMALL GROUPS. IV.
UGHT MANUFACTURING PERSONNEL, by F. K.
Berrien and William H. Angoff. Technical rept. no. 6
on Contract Nonr-404(10). Jan 60, 60p. AD-232 743.
Order from LC mi$3.60, ph$9.30 PB 152 889
Selected employees of two plants, A and B, manufactur-
ing identical items on machines of nearly the same de-
ilgn were respondents to a Likert-type attitude ques-
donnalre on two occasions separated by three and a
talf months. One week prior to the second survey, em-
ployees of Plant B were informed the plant would be
moved to a distant location. It was hypothesized that if
measures of Group Need Satisfactions remained essen-
tially unchanged on the second survey in Plant B, com-
pensatory adjustments would occur among variables
predicting G.N. S. Results showed that G. N. S. did in
taci remain unchanged in both plants. Few statistically
significant changes occurred among the predictor
variables, and none occurred that could be satisfac-
torily interpreted within the framework of the home-
osusis theory. It is concluded that future research
should be directed toward the discovery of conditions
that Influence the level of G.N.S. which is tentatively
conceived as akin to a perceptual constancy. (Author)
(See also PB 148 268)
School of Aviation Medicine, Brooks AFB, Tex.
PSYCHIATRY AND SPACE FLIGHT, by Bernard E.
Flaherty, Don E. Flinn and others. Sep 60. lOp.
23 refs. AFSAMrept. no. 60-80.
Order from LC mi$l. 80. ph|l. 80 PB 152 764
This paper discusses some of the emotional hazards '
that can be anticipated and their possible effect. Since
diese psychologic stresses ace intimately related to
the threatening environmental stresses, it seems worth-
while to review these factors at the outset.
Stockholm U. (Sweden).
A SIMPLE METHOD FOR FITTING PSYCHOPHYSICAL
POWER FUNCTIONS, by Gbsta Ekman. Technical
(scientific) note no. 1 on Contract AF 61(052)300.
26 May 60. 8p. 7 refs. AFOSR-TN-60-1085.
Order from LC mi$l. 80. ph$l. 80 PB 152 535
A method is described for fitting psychophysical power
functions of the form c(S-a)" to subjective scale values
on the ratio level If the stimulus consunt a is negli-
gible, the method may be used for fitting the function
tea subjective interval scale and locating the absolute
zero point of this scale. (Author)
Tennessee U . , Knoxville .
THE STATUS OF MORALE MEASUREMENT, 1959,
by Gerald H. Whltlock. Rept. on Contract AF
41(657)247. May 60, 33pi 73 refs. WADD-TN-60-136;
AD-243 825.
Order from LC mi$3.00, ph$6.30 PB 152 782
This review and critical analysis of attempts at morale
measurement presents the first phase of an investiga-
tion aimed at developing an effective means for measur-
ing morale among Air Force personnel. The uses of
morale measures as predictors and as criteria are
noted, and the implications of each usage for measure-
ment are discussed. The problem of scale dimension-
ality is analyzed, and studies are cited demonstrating
the confusion resulting from erroneous assumptions of
unidimenslonality. An analysis of low intercorrelations ^
among diverse morale n>easures emphasizes notions of
dimensional relevance and concept relevance . A review ^
of definitions of morale points out such problems as the '
equating of job satisfaction and morale, individual and
group references , and definitions for which no measure-
ment operations presently exist. The collection of
methodologies and conceptualizations which , in effect ,
constitute the body of morale theory, is reviewed with
particular attention to conclusions drawn from factor
analysis . These results give a basis for a more exact
and complete analysis of the dimensions of Air Force
morale. (Author)
BIOLOGICAL SCIENCES
Anatomy and Physiology
Aerospace Medical [Dlv. ] Wright Air Development
Div. , Wright -Patter son AFB, Ohio.
BIBLIOGRAPHY ON AERCW^DICAL RESEARCH WFTH
ABSTRACTS, ed. by Joan C. Rc*inette. Dec 59, 107p.
315 refs.
Order from OTS $2.50 PB 171 333
The major areas comprising the Laboratory's mission
are behavioral sciences, biomedical sciences, and
engineering as related to human faaors in aircraft de-
sign and survival equipment. The reports documenting
the first two areas are subdivided Into more specialized
categories: engineering psychology, training psychol-
ogy, bioacoustics, biophysics, and physiology.
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
BODY HEAT PRODUCTION AND SURFACE TEMPERA
TURES IN RESPONSE TO A COLD STIMULUS, by
John P. Meehan. Jan 55, I4p. 10 refs. Proj. no. 7-
7951, rept. no. 2.
Order from LCml$2. 40, ph$3. 30 PB 153 336
Metabolic rates were simultaneously measured with
multiple surface and deep body temperatures on an ex-
perimental group of Alaskan native subjects and a con-
trol group of Caucasian military personnel during a
standard exposure in a cold room. The initial or basal
metabolic rates of all of the subjects were found to be
at normal accepted values . The native subjects did not
have an elevated basal rate. On exposure to cold, the
native subjects showed the greater increase in meta-
bolic rate. This increase was due to greater shivering
on the part of the natives . During the cold exposure,
the native subjects kept their hands and feet warmer
than did the control subjects . Trunk skin temperatures
and mean body temperatures for the two subject groups
were not significantly different. The control group
developed the greater total loss of body heat. (Author)
265
Arctic AeromedjcAl Lab. , Ladd AFB. Alaska.
COMPARATIVE SWEAT RATES OF ESKIMOS AND
CAUCASIANS UNDER CONTROLLED CONDITIONS ,
by Kaare Rodahl and Donald W . Rennie. Mar 57, 21p.
16 refs. Proj. no. 8-7951, rept. no. 7.
Onierfrx>mLCn|i$2.70, ph$4.80 PB 153 341
Comparative swe*t rates and metabolic rates were
measured in Eskinxjs and Whites under three separate
conditions . The tvidence indicated a greater heat pro-
duction In the Esbmo group at rest and during standard
comparative exercises . In the "comfon zone" and un-
der conditions fatoring body heat storage, the Eskimos
responded by sweat activity which was greater than the
Whites' and whici) was in proportion to their increased
heat production. Body heat debt and heat storage under
the above conditions were the same for both groups ,
which Indicated tl»t the thermoregulatory "set" <rf the
Eskimo was the same as for the White. The average
skin temperature of the Eskimo did tend to be elevated
above the Whites' at all environmental temperatures
below 35° C. A high correlation existed between the
average skin terrperature and sweat rates of both the
£skinno and White groups . and the frequency -distribu-
tion of the data was the same for both. The fundamen-
tal difference In the groups from the standpoint of ther-
mal regulation appears to center upon the increased
metabolism of the Eskimo.
1
Arctic Aerome^ical Lab. , Ladd AFB, Alaska.
THE COMPARATIVE TOLERANCE OF NEGROES ANE
CAUCASIANS TO A STANDARDIZED COLD STRESS
AS INDICATED BY BODY TEMPERATURE AND
METABOLIC RATE , by Thomas Adams and Donald W
Rennie. Sep 57, 25p. 18 refs. Technical repc. 57-20
Order from LCfri$2. 70. ph>4. 80 PB 153 351
Although the Cai^casians had a significant increase in
heat production during the cold exposure, the metabo-
lism of the Negro was not significantly increased. It is
assumed that increased shivering activity among the
white subjects accounts for the difference in metabo-
lism between the two groups . It is postulated that the
warmer hands a»d fingers of the Caucasian subjects
caused a ntwre rapid rate of heat loss from this group
and that this increased heat loss stimulated shivering.
The implications of the comparative response of these
groups to cold 14 discussed from the viewpoint of oper-
ational efficiency in a cold environment, and the direc-
tion of future stv^dies is suggested.
Arctic Aerome^lical Lab. . Ladd AFB. Alaska.
THE CUTANEOUS PAIN THRESHOLD IN THE NA-
TIVE ALASKAN INDIAN AND ESKIMO, by J. Patrick
Meehan, Alice ti. Sioll, and James D. Hardy (Cornell
U. Medical Coll.). Dec 53. I5p. 9 refs . Proj. no. 22
1301-0002, rept] no. 9. „ .coo
Order from Lc(nl$2. 40. ph$3. 30 PB 153 328
As no significant difference in pain threshold was
found to exist bdtween the Indian, Eskimo, and White
subjects , it must be concluded that (I) in these groups
cultural differences are not such as to affect the pain
threshold as determined by this method; and (2) the
ability of the AUskan Indian and Eskimo to expose his
skin to extreme cold without inlurv is not associated
widi an elevation of this threshold. It is possible, how-
ever, that exposure to cold stimulation might reveal a
relative elevation of the "cold" pain threshold in the
Alaskan Indian and Eskimo as compared to the popula-
tions of warmer climates .
Arctic Aeromedical Lab. . Ladd AFB, Alaska.
THE EFFECT OF PROLONGED ARCTIC FUGHT ON
NIGHT VISUAL ACUITY, by Horace F. Drury and
Kaare Rodahl. Aug 52. I7p. 2 refs. Proj. no. 22-1201
0001. rept. no. I.
Order from LC miJ2.40. ph$3.30 PB 153 326
Light exposure during prolonged polar flights at high
altitude is not sufficiently Intense at any season of the
year to produce significant effects on subsequent ni^
visual acuity. There is a distinct possibility that a psr
tial acclimatization to altitude sufficient to bring about
improvement in night visual acuity n»y occur during
an exposure of 15 to 18 hours to a pressure altitude of
8,000 to 10,000 feet. The physiological and psychologl
cal stresses attendant upon prolonged night flights may
bring about a significant and perhaps serious decrease
in night visual acuity following extended missions.
Since these stresses are independent of exposure to
high light intensities . they may be expected to operate
at all latitudes .
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
EVALUATION OF GLYCINE IN FROSTBITE PRO-
PHYLAXIS, by William R. Beavers and Benjamin G.
Covino. Nov 57, I5p. 9 refs. Technical rept. 57-24.
Order from LCmi$2. 40, ph»3. 30 PB 153 353
Under many operational situations , military persooad
are unable adequately to Increase heat production by
muscle activity in response to cold stress . An ages
capable of increasing visceral heat production might be
useful in the prevention of cold injury. Glycine, an
amino acid with a hi^ specific dynamic action, was
given in 30 gm. oral doses to six young adult males.
The individuals served as their own controls when re-
ceiving 30 gm . glucose . In a 29° C . room 1 hour after
ingestion, glycine produced an average 9.2% increase
in resting metabolism. In a -17.8° C. (0°F.)cold
room 2 hours after ingestion of glycine, metabolism
continued higher and the subject had higher toe. fore-
head, and average body temperatures . No difference!
were noted in finger temperatures , but forefinger
blood flow was greater when glycine was Ingested.
Glycine may be of practical value in increasing heat
production under certain conditions . (Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
HIND UMB BLOOD FLOW DURING IMMERSON
HYPOTHERMIA , by Benjamin G . Covino and William I
Beavers. Jan 57, I4p. 20 refs. Proj. no. 8-7954.
rept. no. 2. , .
Order from LC mi$2. 40, ph$3. 30 PB 153 342
A marked vasodilaution was observed In the hind lin*
of dogs subjected to immersion hypothermia. An inidil
dilatation occurred at a rectal temperature of 35° C
while a second dilatation took place at a rectal tempeit
ture of 28 - 25° C. The primary response appeared
266
1 ;
due to the stimulation of sympathetic cholinergic di-
Utor fibers supplying arterio- venous anastomotic ves-
sels in skeletal muscle. This response could be inhib-
ited by atropinization and/or sympethectomy-acrenalec-
tomy. The secondary dilatation was unrelated to ner-
vous or local metabolic factors . This phenomenon was
correlated with an extremely low muscle and blood tern
perature, and so is believed due to the direct influence
of cold on the skeletal muscle arteriolar-capillary
circuit. (Author) j
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
HUMAN ACCLIMATIZATION TO COLD, by Kaare
Rodahl. Oct 57, 52pi 65 refs. Technical rept. 57-21.
Order from LC mi$3.60, ph|9.30 PB 153 352
Previous studies of human acclimatization to cold are
reviewed and compared with data from animal experi-
ments . Results from Eskimo studies are summarized
In terms of environmental exposure, activity, food in-
take, metabolic response, thyroid activity, evaporative
hMt loss, changes in blood and tissues , and physical
fiineas. The mechanism of general acclimatization to
cold is discussed and various aspects of local accli-
matization are considered. Finally, cenaln promising
areas of future research are suggested. (Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
UaVIDUAL AND RAQAL VARIATIONS IN A VAS-
CULAR RESPONSE TO A COLD SnMULUS, by John
P. Meehan. Apr 55, 13p. 4 refs. Proj. no. 7-7953.
rept. no. 1 .
Order from LC mi$2.^, ph$3.30 PB 153 338
■r
As experimenul precedure Involving the recording of
surface finger temperatures during a thirty minute ice
water immersion period, was performed on groups of
Caucasian. Negro and Alaskan Native subjects . The
average finger temperature for the last 25 minutes of
the immersion period, and the lowest finger tempera-
ture recorded, were used as the basis for comparing
the responses of the various subject groups . The Alas-
kan Native group maintained the highest finger tempera
tures during the immersion period, while the Negro
group maintained the lowest. The experimental data
indicate the possibility of a physiologic adaptation to
cokl on a racial as opposed to an individual basis . A
physiologic basis for the reporied higher percentage
incidence of cold inlurv. seen in Nejrro militarv
personnel engaged in cpld weather operations , is pre-
imted. (Author) \
^ .! I
Arctic Aeromedical Lab. , Ladd AFB. Alaska.
LIVER PHOSPHORUS METABOLISM IN THE COLD-
ACCLIMATIZED RAT, by John P. Hannon. July 60.
20p. 39 refs. Techni||ijept. no. 58-16.
*der from LC mi$2.1^ ph$3. 30 PB 152 695
Liver homogenates from control and 1 -month cold-
e«posed (5°+ l^C) rats were assayed for the P/0 ratios
charaaerisrlc of succinate and p-hydroxybutyrate oxl-
dKlons and for the level tof adenosinetriphosphataae
•alvlty. With both subsCrates a significant lowering of
*e P/0 ratio was observed In the cold-exposed group.
Measurements. of adenoslnetri phosphatase activity in
i
water homogenates showed that calcium and magnesium
had strong activating effects. Little difference was
found between control and experimental preparatioria
except where both ions were used simultaneously.
Here, the tissue from the cold-exposed group exhibited
a slightly Ipwer activity than the controls. Adenoaine-
tripboaphataae assays of homogenates prepared in
isotonic sucrose and measured at various tonicity
levels showed that both groups responded similarly.
However, slight differences between the control and
experimental preparations were noted when magnesium
was used as the activating ion. The data were dis-
cussed in relation to the high thyroid activity of the
cold- exposed animal. (Author)
Instltut fur Animalische Physiologie der J. W. Goethe
Universiui (West Germany).
INVESTIGATIONS ON THE FLOW GP BLOOD IN
CAPILLARIES, by Rudolf K. Zahn. Pinal technical
status rept. for I Oct 59-30 Sep 60 on Contract DA 91-
591-EUC-1302-OI-4171-60. [1960] 16p. 24 refs.
AD- 244 921.
Order from LC ml$2.40, pli$3.30 PB 152 690
Experiments with agents influencing the mechanism of
blood clotting showed a delay of onset of ultra-violet-
stasis with hepftrine. and an acceleration cf stasis with
is-otamlnesulfate and Tween 80. Furthermore heparine
and protamlnesulfate were shown to exert an antagonis-
tic influence on the onset of stasis so that intravacal
clotting is considered to be a major cause of ultra -
violet-susis. The endeavour to prove changes of per-
meability of the walls of blood vessels before onset erf
stasis by use of vital dyes yielded no results'. Hista-
mine. 5-hydroxy-trlptamlne and reserplne Injected into
the dorsal lymphatic sac failed to exert an influence on
the occurence of ultra-violet-stasis. Experiments with
weekly repeated administration of desoxy-ribo-nuclelc-
acld, desoxy-ribo-nucleasel and autoclaved desoxy-
ribo-nucleasel so far resulted In an Increased gain of
welj^t of the animals subjected to desoxy-ribo-nuclelc-
acld and aisoclaved desoxy-iibo-nucleasel. In the
chronic experiment autoclaved desoxy-rlbo-nucleasel
accelerates the onset erf stasis, whereas desoxy-ribo-
nucleic-acid delays It. Measurement of the permea-
bility of the web skin yielded no significant differences
between the different groups.
Institute of Andean Biology, Lima (Peru).
THE INFLUENCE OF HIGH ALTITUDES ON THE
ELECTRICAL ACTIVfTY OF THE HEART. ELEC-
TROCARDIOGRAPHIC AND VECTORCARDIOGRAPHIC
OBSERVATIONS IN THE NEWBORN, INFANTS. AND
CHILDREN, by Dante Penaloza, Raul Gamboa and
others. Aug 60. 2lp. 62 refs. AFSAM rept. no. 60-79.
Order from LC ml$2. 70. ph$4. 80 PB 152 763
Five hundred forty normal children were studied 350
at sea level and 190 in Morococha, 14, 900 feet above
sea level. The comparative study was made in children
of five age groups, ranging from newborn to 14 years.
In the newborn (both at sea level and at high altitudes)
the electrical activity of the hean showed similar char-
acteristics. Some weeks after birth there developed a
definite difference in the ECG of infants at the two ele-
vations. At high altitude, an accentuated right AQRS
deviation persists during infancy and childhood. In the
267
high altitudes, during the first weeks or months of life
the T loop shifts to a forward position and the T wave
becomes positiveiin the right precordial leads. In
healthy children of the high altitudes there exists a
nxxlerate degree of right ventricular hypertrophy. The
electrocardiographic and vectorcardiographic charac-
teristics of the hfalthy children living permanently at
high altitudes ar^ not comparable with those of the
normal children «t sea level. A high altitude environ-
ment IS an important source of electrocardiographic
and vectorcardiographic variability in healthy children.
(Author)
Oklahoma U . Mhool of Medicine , Oklahoma City .
HEAT LOSS FROM THE RESPIRATORY TRACT IN
COLD, by Paul Webb. Final rept. on Contract
AF 18(600)355. Apr 55. Up. AALproJ. no. 7-7951,
rept. no. 3. |
Order from LC iii$3.
.30, ph$7.80
PB 153 337
A new method fo^ the measurement of water vapor in
expired air has been developed and used in cold condi-
tions in Alaska. 'Additional temperature data were
gathered at the s^me time to supplement the informa-
tion from a prevfciust study. From this experimental
information a re4hstic assessment of respiratory
tract heat loss becomes possible.
St. Louis U. S<*KX)1 of Medicine, Mo.
REFINEMENTS Ui PHOTOELECTRIC PLETHYSMOG-
RAPHY, by Alric^ B Hertzman and Walter Ciszczon.
Rept. on Contrac^t AF 18(600)1043. July 60. 20p. 9 refs
Technical rept. 4o. 57-15.
Order from LC ilu$2.4a, ph$3. 30 PB 152 617
Circuits are described which permit convenient and
continuous calibDation of photoelectric recordings of
variations in tissue blood. content in terms of fractional
changes in photoelectric current. This procedure is
applicable to plefhysmograms and volume pulses
whether recorded by optical galvanometers or direct
writers. Drift in prolonged records may be eliminated
by photoelectric h»onitoring of the light bulb. An oscil-
lator which may ^x controlled by the light monitor has
been designed toi supply a constant AC voltage (at 10 kc)
to the filament of the Ught bulb. These arrangements
increase the convenience and dependability of apphca-
tlon of the technique of photoelectric plethysmography
to climatic expei Iments . (Author)
School of Aviation Medicine, Brooks AFB, Tex.
INTERNATIONAL SYMPOSIUM ON CARDIOLOGY IN
AVIATION [NO. 1) CONDUCTED AT THE SCHOOL
OF AVIATION KlEDICINE, 12-13 NOVEMBER 1959. by
Lawrence E. Laihb. ed. (1959) 429p. 383 refs.
Order from LCiiii$l 1.10, ph$65. 10 PB 152 460 \
Contents: I
Sect. 1. Aeroepice Flight and the Normal Cardiovascu-
lar System: Iitflluence of aerospace flight on the nor-
mal cardiovasdular system - stresses and effeas
Sect. 2. Cardiovascular Techniques: Phonocardiography
Current status bf vectorcardiography; Telemetering
physiological responses during experimental flights
Sect. 3. Cardiovascular Disorders in Aircrew person-
nel: Pathologic! findings in the cardiovascular system
of military flying personnel; The cardiovascular sys-
tem of the aging pilot; The problem of loss of con-
sciousness in flying personnel; The problem of ele-
vated blood pressure or hypertension in the pilot;
CardiovasciUar diseases in the flying population
Sect. 4. Electrocardiographic Studies; Royal Canadian
Air Force experiences in electrocardiographic evalua-
tion; The prognostic implications of the electrocardla-
gram; Electrocardiographic findings in 67, 375
asymptomatic individuals: Part 1: Incidence of ab-
normalities; Part 2: Supraventricular rhythms; Pan 3:
Ventricular rhythms; Part 4: Wolff-Parkinson-White
syndrome; Part 5: Complete left bundle branch block;
Part 6: Complete right bundle branch block; Part 7:-
A-V block: Part 8: Non-specific T-wave changes;
Part 9: Myocardial infarction; Part 10: Normal values
Sect. 5. Limits of Cardiovascular Normality for Flying
The National Program for Study of Cardiovascular
Disease
Technische Hochschule, Karlsruhe (West Germany).
MECHANICAL AND ELECTRICAL PHENOMENA OP
THE HEART ACTION, by W . Emsthausen and W. ».
Wittem. Final rept. on Contract AF 61(514)1063.
Mar 60, 40p. 13 refs . AFOSR TR-60-134.
Order from LC mi$3.00, ph$6.30 PB 153 037
The report covers the "elect romechanics" of the heart.
A new method for the simultaneous recording of motion
and voltage between two points on the hean' s surface
is described. Measurements on dog hearts recorded
with this method under various conditions are reported
(Author)
Tufts U. School of Medicine, Boston, Mass.
ALTERATIONS IN HEPATIC UPID METABOLISM IN-
DUCED BY ACCLIMATION TO LOW ENVIRON-
MENTAL TEMPERATURES, by E. J. Masoro. July 60,
23p. 22 refs. Technical rept. no. 59-25; AD- 244 757.
Order from LC ml$2. 70. ph$4. 80 PB 152 618
A review is made of the author's work on cold acclimi-
tion and its relation to hepatic lipid metabolism. Dau
on the mechanisms underlying the marked capacity of
the liver of the cold -acclimated rat to preserve hver
glycogen stores during fasting are presented. These
mechanisms were shown to be intimately associated
with hepatic lipid metabolism Information is also
given pertinent to the use of hepatic tissue of cold-
acclimated rats as a tool for the study of physiologic
regulation of intermediary metabolism. (Author)
Tulane U. , New Orleans, La.
CATALOG OF TRANSLATED MATERIAL IN SPACI
PERCEPTION, ed. by Ocil W. Mann. Rept. on Con-
traa hr7onr-434. TO. I. 15 May 55. 43p. 427 reft.
Joint Proj. rept. no. NM 001 IIOSOO.37, formerly
NM 001 063.01.37.
Order from LC mi$3.30, ph$7.80 PB 153 575
This report released for sale to the public 4 Jan 61.
This repori is a catalog of bibliographic materials In
the area of proprioceptive, vestibular function and
vision which have been translated from foreign lan-
guages. The catalog lists 427 items. The catalog is
arranged in the author -alphabetical format adopted by
the American Psychological Association. (Author)
268
University of Southern California. School o(
Medicine, Los Angeles.
HUMAN PSYCHOMOTOR PERFORMANCE USDER
VARIED TRANSVERSE ACCELERATIONS, by Richard
C. ICaehler and John P. Meehan. Rept. on Biophysics
of Flight, Contract AF 33(616)5407. Aug 60, 54p.
WADD Technical rept . 60-621.
Order from OTS $1.50, PB 171 304
Five male college students, 20 to 25 years old, were
exposed to transverse accelerations from front -to-
back up to 8 g and back-to-front up to 4 g on the USC
centrifuge to investigate human motor performance.
The results show that man can, with the proper con-
trols and properly loci^ed in the workplace, participate
effectively in aircraft control when exposed to rela-
tively high transverse accelerations. During front-to-
back acceleration, man can perceive a visual stimulus,
reach and adjust controls, e.g. , the horizontal lever,
toggle switch, and push-to-test button, regardless of
location in a mean time of 1 .0 second at 8 g. Controls
(wnnally more difficult to operate, the vertical wheel
and rotating kiK>b, require a mean time of 1. 5 seconds
at 8 g. For back-to-frbnt accelerations, the toggle
■witch, horizontal lever, and push-to-test bunon re-
quire a mean time of 0. 7 second at 4 g, whereas, the
vertical wheel and rotating knob require a mean time
of 1.0 second. (Author)
i
University of Southern California. School of
Medicine, Los Angeles.
RENAL RESPONSES TO POSITIVE ACCELERATIC*^.
by John P. Meehan. Re^. on Biophysics of Fll^t. Con
tract AF 33(616)5407. Sep 60, 20p. 12 refs. WADD
Technical rept. 60-637.
Order from OTS $0. 50 PB 171 343
The para -amino hippurate (PAH) clearances, creatinine
clearances and urine flows of young male subjects ex-
posed to positive acceleration have been studied. Ex-
posures at 3 g for 10 niinutes produced no consistent
changes in the above parameters from control values.
Longer exposures at 3 g produced a reduction of the
para-amino hippurate (PAH) clearance in some sub-
Jecta, no consistent changes in creatinine clearances,
and significant reductions in urine flow following
centrifugation. It is copcluded that positive accelera-
tion as used in the present experiments affects the
Udney primarily through mechanisms involving a re-
duction of the thoracic blood volume. (Author)
Washington U. , Seattl^. School of Medicine.
THE ROLE OF THE THYROID IN THE METABOUC
RESPONSE TO LOW TEMPERATURE, by L. D.
Ctrlion and A. C. L. Hsleh. Rept. on Contract AF
18(600)1467. May 57. ij^. 29 refs. AAL Technical
rept. 57-1. j
Order from LC mi$2. 4(1. ph$3. 30 PB 153 344
The requirenient for thjjroxin in chemical regulation of
heat production has been studied by testing the metabo-
lic response of curarized rats to cold exposure at var. ■
'ng periods after thyroid«:tomy. Sprague-Dawley rats
were kept at 5" C and 2^ C The metabolic response
to cold in curarized rat^ is not directly dependent
upon the anKXint of circulating thyroxin because the
response persists when th\roxin stores are depleted
Cold-adapted rats reduced their food ituake and lost
weight following thyroidectomy, but nuiintained a high
metabolism at 5° C. (Author)
Willow Run Labs. , U. of Michigan, Ann Arbor.
A STATISTICAL APPROACH TO THE PROBLEM OF
SPATIAL AND TEMPORAL INTEGRATION IN VISUAL
DETECTION, by W. M. Kincaid and A. B. Clarke.
Rept. on ProJ. Michigan, Contract DA 36-039-8C-
78801. Oct 60, 23p. 4 refs. 2900-57-T; AD-245 117.
Order from LC mi$2. 70, ph$4. 80 PB 152 605
A critical examination of an earlier formulation of
the effects of target size and shape upon visual
detection leads to a more sophisticatad approach,
which is also applicable to the more general problem
of the relation between the spatial -temporal character-
istics of a target and its detecubility. It is postulated
that the detection of a target involves a decision proc-
ess analogous to the testing at a statistical hypothesis,
using the most powerful test in the sense of Neyman
and Pearson. The determination at the most powerful
test in a given situation is equivalent to the solution of
a set of equations. A formal solution can be obtained.
(Author)
Biochamistry
Aviation Medical Acceleration Lab., Naval Air De-
velopment Center, Johnsville, Pa.
THE PREPARATION OF REDUCED CYTOCHROME
c BY MEANS OF ELECTRON -EXCHANGE RESINS,
by Herman W. Shmukler and Frederick G. Schappell.
Rept. no. 12 on Proj. MR005. 15-0002.7; Proj. TED
ADC RS-7045 (5915-A). 31 Aug 60, 9p. 6 refs. NADC-
MA-6031; AD-244 372.
Order from LC mi$l . 80, ph$l . 80 PB 152 470
By use of an electron -exchange resin (Duolite S-30) it
was possible to prepare reduced cytochrome c. The
extent of reduction and the purity of the product indi -
cate that it would be suitable for in vitro studies of
cytochrome c oxidase activity. The cytochrome c pre-
pared by this method was found to have a slower rate of
auto -oxidation than a similar preparation reduced by
dithionite while retaining its enzymatic activity as a
substrate for cytochrome c oxidase. The advantages of
this method in respect to the present means of reducing
cytochrome c (treatment with dithionite and hydroge-
nation using a platinum or palladium catalyst) are the
freedom from ionic contaminates either dithionite or
heavy metals and the elimination of the need for a
metal catalyst and the subsequent filtering involved.
(Author)
Aviation Medical Acceleration Lab. , Naval Air
Development Center, Johnsville, Pa.
X-RAY DIFFRACTION STUDIES OF CYTOSINE,
URACIL AND THYMINE, by Emma Fessenden. Rept.
no. 1 on Proj. MR005.15-O002.il. 30 Aug 60. 15p.
U refs. NADC-MA-6030.
Order from LC mi$2. 40. ph$3. 30 PB 152 740
269
x-ray dlffractioni patterns for three biological pyrimi-
dines are presented. Wherever possible the indexed
pattern has been completed. Cytosine monohydrate.
thymine and uracil all have been determined as belong-
ing to the monoclinic crysullographic system. The
system of cytosirie is not elaborated. Various forms of
cytosine are givefi in the literature with some degree
of uncertainty. Qytosines from several sourcea were
examined. By investigation with recrysttfllization and
by drying method^, the patterns for cytosine and cyto-
sine monohydrata were resolved. All patterns given in
the literature may be explained by varymg the ratio of
mixture of the rw|) compounds. Tlie pattern of uracil
was refined and i^idexed. The pattern of thymine was
confirmed, the u^it cell determined and the indexing
completed. (Author)
Washington U . Seattle. School of Medicine.
AN IMPROVED NETHOD FOR THE DETERMINATION
OF URINARY 171-KETOSTEROIDS, by Minoru Masuda
and Horace C. TTluline. Research rept. on Contract
AF 33(038)22916. Mar 53. lOp. 9 refs . AAL ProJ.
no. 22-1301-0002.
Order from LC n|i$ 1.80, ph$ 1.80 PB 153 327
A simple n>ethod of estinrvation of total neutral 17-keto-
steroids is given in which the final Zimmerman color
is extracted with famyl acetate. The extraction with
organic solvent l^ves behind in the aqueous layer the
non-ketonic interfering chromogens The definite re-
duction in titer b^ this method is comparable to the re-
duction in titer after micro-Girard separation and chro
matography. Purs l7-keiosteroids and urine extracts
show linearity ao:ording to Beer's Law with this
method.
Microbiology
Georgia Inst, oi Tech. , Engineering Experiment
Station, AtlanU
THE EFFECT OF LOW TEMPERATURES ON THE
SURVIVAL OF AIRBORNE BACTERIA, by T. W.
Kethley, E. L. Pincher, and W. B. Gown. Final rept
Mar 57, 63p. 17 refs. AAL proj. no. 8-7958.
Order from LC rAl$3. 90. ph$10. 80 PB 153 343
Results are reported for studies on various airborne
bacteria under varying condition* of relative humidity
at low temperatures. A complete description is given
of the special aeijosol cylinders devised for carrying
out these studies. Employing airborne bacterial parti-
cles dispersed from beef broth cultures, extensive
studies are reported for Serratia marcescens (ATCC
274, primary form), and Egcherichia coli (ATCC 10636)
for the range at temperatures SOPP to -iCPP. Prelimi-
nary studies are reported for Serratia indica (ATCC
4003), Microccoqus pyogenes var. aureus (ATCC 6538)
and Microccocus pyogenes var. albus (ATCC 9491). It
is concluded that ithe experimental bacterial particles
■CiKtted are very similar to those arising from natural
caiMes and that the findings are generally applicable to
many naturally occurring airborne bacteria. The very
low death rate observed for the experimental bacteria}
aerosols at low temperatures is consistent with pre-
vious reports of ihe presence of viable bacteria in the
upper atmospheres. It is further concluded that
although the death rate of airborne bacteria is very
small at low temperatures, the factors which determine
the fate of these organisms are similar to those oper-
ating at higher temperatures.
i r.- ..■ .
Materials Lab., Wright Air Development [Div.]
Wright-Patterson AFB, Ohio.
RESISTANCE OF MICROORGANISMS TO HIGH
VACUUMS, by Sam Bakanauskas. Rept. for July 58-
Apr 59 on Finishes and Materials Preservation.
Apr 59, I6p. WADC Technical note 59-142;
AD- 228 156.
Order from LC mi$ 2.40, ph$ 3. 30 PB 153 573
This report released for sale to the public 4 Jan 61.
A study was made to determine the effect of prolonged
dynamic vacuums on the viability at selected spore-
forming fungi and bacteria. The microorzanisms wq-e
exposed to pressures ranging from 1 x lO'^ to 5x 10"'
mm Hg for periods of 2, 4, 8, 16, and 32 days. Micro-
organisms used were: Aspergillus njger WADC 8,
Aspergillus flavus WADC 26, Bacillus globigii WADC
B5, pacilJus mvcoides WADC B8, and Bacillus cereus
WADC B6. With the exception of B. cereus WADC 56.
spores of all microorganisms remained viable after
32 days exposure. (Author)
Trinity Coll,. , Dublin (Erie).
TO INVESTIGATE THE VARIETY OF BACTERIAL
MUTANTS OCCURRING SPONTANEOUSLY AND
PRODUCED BY VARIOUS RADIATIONS AND CHEMI-
CALS, by G. W. P. Dawson. Final technical rept. for
1 Sep 59-31 Aug 60 on Contract DA 91-591-EUC-1171
Sep 60, 23p. 6 refs.
Order from LC mi$2. 70. ph$4- 80 PB 152 477
Studies at sponuneously occurring reverse muutiooa
in Salmonella typhimurium have been designed to ex-
plore the range of genetic changes that cause these re-
versions. To be able to classify reversions aa pre-
cisely as possible is a necessary preliminary to the
study of the response of genes to mutagens. Rever-
sions of the leucine requiring muunt leu 151 have been
chosen for deuiled study. A second line of Investiga*
tion is based on the expecution that there may be more
than one physiologically effective information pattern
of a gene. Reversions otf the site muunt tryptophane
A8 are being examined to discover whether any of diese
reversions arise by changes within the tryptophane A
locus but not involving a change in the A8 site.
Neurolog)r and Psychiatry
California U. , Los Angeles. School of Medicine.
NERVOUS CONTROL OF SHIVERING. SHIVERING
AS A RESULT OF BRAIN STIMULATION, by
Lucy Birzis and Allan Hemingway. June 57, l6p. 4 reft
AAL Technical rept. no. 57-10.
Order from LC mi$2. 40. ph$3. 30 PB 153 349
Electrical stimulation at 21 sites in the brain stem of
5 cats under light barbiturate anesthesia resulted in
270
the production of a tremor having the characteristics
of natural shivering. The positive stimulation sites lay
within the lesion -determined "shivering pathway" in
cbe midbrain and pons. The positive hypothalamic
stimulation site was located in the medial part of the
tuberal hypothalamus, between the mammillothalamic
tract and the fornix. (Author) (See also PB 146 618).
.! I
California U. , Los Angeles.
NERVOUS CONTROL OF SHIVERING. IL A DE-
SCENDING PATHWAY FROM THE PREOPTIC SHIVER
ING SUPPRESSOR REGION, by Lucy Birzis. Takio
Shimamoto, and Allan Hemingway. Rept. on Contract
AF 18(600)358. Mar 54. 7p- 2 refs. AAL ProJ. no.
22-1301-0009. rept. na 2.
Order from LC nU$l. 80, ph$l. 80 PB 153 330
There is a descending conduction pathway from the
riiivering suppression 'center' in the diencephalon ex-
toKling caudally at least through the medulla. Electri-
cal stimulation along this pathway suppresses shiver-
ing. One interpretation of these results might be that
central control of shivering is accomplished over this
route. Instead of acting on the site of origin of the
•diver ing impulses (presumably the posterior hypothal-
amus), the inhibitory influence may be exerted at lower
motor centers, perhaps at the ventral horn outflow, al-
though the conduction pathway In the conWias not been
investigated. Direct suppression of the ventral horn
cells innervating particular muscle groups would be a
means of obtaining the gratled response that is charac-
teristic of the shivering process. (Author) (See also
FB 153 349).
California U. ,'• Los Angeles. School of Medicine.
NERVOUS CONTROL OF SHIVERING. VL EFFEI -
ENT BRAIN DISCHARGE DURING SHIVERING, by
Lucy Birzis and Allan Hemingway. June 57. 19p.
9 refs. AAL Technical rept. 57-11.
Order from LC ml$2. 40, Rh$3. 30 PB 153 350
Action potentials associated with shivering have been
recorded from the brain stem of the cat using large
(25»< diameter) microelectrodes. The electrodes, from
which shivering action potentials were obtained, were
located within the efferent shivering pathway previ-
ously determined by lesion experiments. The rangeof
frequencies from these units was between 6 and 26 per
second and appeared as a continuous stream of im-
pluses having no rhythmic pattern. (Author) (See also
PB 153 330) •
Patbplogy
Army Chemical Research and Development Labs. ,
Army Chemical Center, Md.
THE COMPARISON OF THE BURN- PRODUCING EF-
FECTIVENESS OF SOME GASOLINE- BASE INCEN-
DIARY AGENTS, by M. J. Margovich. Sep 60, 31p.
5 refs. CRDLR 3024; AD- 243 348.
Order from LC mi$3. 00, phJ6. 30 • PB 152 599
Brooke Army Medical Onter, Fort Sam Houston, Tex.
THE INCREASE OF THE GRAM -NEGATIVE: GRAM-
POSITIVE ORGANISM RATIO IN BURN DEATHS
ASSOCIATED WITH SEPTICEMIA, by Wilfred T.
Tumbusch, John V. Butkiewicz and others. Rept. on
Radiation and Thermal Burns, Proj. no. 6-59-12-028.
Oct 59, lOp. MEDEW-RS-3-59; AD-243 989.
Order from LCmi$ 1.80, ph$ 1.80 PB 152 368
Surface and blood cultures from burned patients treated
at the US Army Surgical Research Unit during the past
six and one-half years have been reviewed. Since 1955,
there has been a gradual decrease in incidence of
Gram-positive organisms and a gradual increase in
incidence of Gram -negative bacteria cultured from
wounds and the peripheral blood. The clinical course
of patients who have died in the past twenty months with
Gram-negative septicemia has been described. (Author)
Kansas U. , Lawrence.
STUDIES ON THE INaDENCE OF TULAREMIA IN
ALASKA, by Cora Downs. June 60, 31p. 7 refs. Tech-
nical rept. no. 57-43; AD-244 756.
Order from LC mi$3. 00, ph$6. 30 PB 152 619
Chemical purification of the Ascoli antigen from in-
fected mice has been accomplished by methanol pre-
cipitation in the cold. Maximum recovery of active
substance occurred at 60% methanol concentration.
Paper electrophoresis and ultracentrifugation showed
that much of the crude Ascoli was made up of particu-
late nnaterial which gave unsatisfactory results in elec-
trophoresis and was not amenable to analysis by ultra-
centrifugation. Determinations for nonglucose amine
showed that alcohol precipitation concentrated this
component. Paper chromatography showed that crude
normal and crude infected Ascoli contained glycine,
proline, aspartic acid, leucine, glutamic acid, histi-
dine, alanine and methionine. The alcohol -purified
Ascoli contained glycine, glutamic acid, and alanine
only. Centrifugal ion of the crude infected Ascoli and
purified Ascoli at 60, OCX) rpm gave a gelatinous sedi-
ment which conuined a negligible amount of protein but
which was active both as a sensitizer and inhibitor in
the hemagglutination test and which protected mice
against challenge with fully virulent Pasteurella
tularensis. Chymotrypsin treatment of this gelatinous
material decreased nitrogen from 2. 17 mg/ml to 0. 2
mg/ml without decreasing the serological activity.
Further tests for the characterization of this antigen
are planned. (Author)
North Carolina State Coll. , Raleigh.
STUDY OF ALASKAN SCHISTOSOMES, by Reinard
Harkema. Rept. on Contract AF 18(600)187. June 53,
28p. 9 refs. AAL proj. no. 22-1401-0005.
Order from LC mi$2 . 70 , ph$4 . 80 PB 1 53 332
Schistosome dermatitis is a disease of place and the
infection of man is dependent directly upon exposure to
waters containing snails infected with the larval stages
of the schistosome. There are many opportunities for
personnel to become exposed to ^e cercariae. Many
lakes in the vicinity of Fairbanks are fairly attractive
for swimming and several of them are infested. Per-
sonnel in the field often bathe in any lake or pond avail-
able. There is the very definite possibility that such.
271
I
waters may be infected. Personnel can avoid infection
by staying out of th« water. A program of education in-
forming personnel 4f the hazards from swimming or
bathing in infested prater is the best method of prevent-
ing infection.
Science and Techiiology Div. , Library (A Congress,
Washmgton, D- d
AEROSPACE MEOiciNE AND BIOLOGY (FORMERLY:
AVIATION MEDICINE) AN ANNOTATED BIBLIOG-
RAPHY VOLUME III: 1954 LITERATURE, by Arnold
J. Jacobius, Roman Kenk and others. I960, 547p.
I,386ref8. j
Order from OTS $d. 00 PB 171 029
The change of title Wings into relief the fact that the
general subject 8C(|pe of the bibliography has been ex-
panded to include nfew areas of interest in space -
medical and space -[biological research. To the subject
fields heretofore covered by the bibliography new ones
have been added, aiich as Biological Rhythms, Biologi-
cal Orientation. Closed Ecological Systems, Physio-
logical and PsycholJDgical Effects of Heat, Cold, Isola-
tion, Restraint, an(d many others. References are ar-
ranged alphabetically by author; abstracts are inform-
ative; and full bibliographic information is provided.
Including foreign Api translated titles, volume and
issue numbers, plice of publication (if foreign), in-
clusive paging, full dates, and library call numbers or
other location sym^wls. While the bulk o* the publica-
tion is devoted to jpumal articles, reports, and mono-
graphs published fifing the year 1954, items published
in 1952 or 1953 no^ included in the preceding volumes
have been incorporated in this volume.
University of Sou them California . School of Medicine
LoS Angeles .
MAINTENANCE CF THE INTEGRITY OF THE
BLOOD VASCULAR SYSTEM. ITS RELATION TO
ANTICOAGULANTS AND BLOOD COAGULATION
MECHANISM, by Chester Hyman, Thonnas E. Nelson,
and Eli Castronovj. June 57, 42p. 14 refs . AAL
Technical rept. 51-9.
Order from LC mtt3.30, ph$7.80 PB 153 348
The purpose of thi^ investigation was to observe cer-
tain alterations injthe physiology of the blood vascular
wall during the development of pur|]Ura'in the throm-
bocytopenic and h)|poprothromblnemic rabbit, and thus
gain further knoWledge of the pathogenesis of the hem-
orrhagic diathesis associated with hemostatic dis-
orders . Alteration in vascular permeability to plasma
proteins was estimated by one of three different me-
thods: by observin J the rate of disappearance of dye-
labeled plasma protein from the blood, by determining
the rate of transfer of labeled protein to the thoracic
duct lymph, or by calculating the rate at whichxlye-
labeled protein pauses into the peritoneal cavity. It
was found that the i mechanism of vascular breakdown
following anti-pladelet serum is unlike that caused by
dicumarol. An increase in vascular permeability to
plasma protein dots not seem to be an integral step in
the development of thrombocytopenic purpura, but di-
cumarol purpura dan be directly related to increased
protein leakage, llthough the vascular injury resulting
from antiplatelet ! erum administration appears to be
due primarily to a direct vascular injury by the anti-
serum, the alterations in vascular integrity observed
with dicumarol under cenain experimental conditions
can be related to the resulting hypoprothrombinemia.
(Author)
Pharmacology and Toxicology
(Army Chemical Research and Development Labs. )
Army Chemical Center, Md.
COMPARISON OF SEVERAL METHODS USED BY
GASSING BRANCH FOR GOLLECTION AND ANALY-
SIS OF GB VAPOR IN AIR AT LOW CONCENTRA-
TION LEVELS, by Fred W. Oberst, Francis P.
McGrath and others. May 52, declassified 16 Apr 59.
23p. 10 refs. Medical Labs. Research rept. no. 111.
Order from LC mi$2. 70, ph$4. 80 PB 149 634
The object has been to evaluate and to make improve-
ments on several existing njethods for collection and
determination of low concentration of GB vapor dis-
persed in air. The results of this investigation show
that a wide range of concentrations of GB vapor in air
can be determined by proper selection of collection and
analytical methods. The colorimetric method using
Tetralin for collecting the sample is suitable in the
range of 2 to 50 mg/m^ while with Tetralin-isopropanol
in beaded tubes it is satisfactory between 0. 1 and
3 mg/m3. The fluorimetric method Is satisfactory in
the range of 0. 01 to 1 mg/m^ while the enzymatic
method may be used at levels ranging from 0. 0005 to
0. 02 n\g/m3. (Author)
Army Chemical [Research and Development] Labs.,
Army Chemical Center. Md.
METABOUSM OF 2-FORMYL- 1 -METHYL PYRI-
DINIUM IODIDE OXIME (2-PAM). by Sarah C. Kaiser.
Dec 59. lip. 6 refs. CWLR 2347; AD- 231 130.
Order from LC mi$2.40, ph$3. 30 PB 149 635
After intravenous injection of 2-PAM labeled with C*^
by N-methylation, the plasma level of radiocarbon
rises to a maximum at 10 to 20 minutes in the cat.
Thereafter, the label disappears from the blood quite
rapidly, so that by 2. 5 hours after injection of 2-PAM
only 0. 3% of the label remains. The excretion of label
after intravenous injection al 2-PAM appears to be
largely in urine, a mean cA 72^ of the C^^ injected at
2-PAM being excreted in the urine erf the mouse within
24 hours after the injeaion and 39% being excreted
within 2. 5 hours in the urine of one cat. Fecal excre-
tion by the mouse within 24 hours amounts to not more
than about 5%. Less than 0. 2% of the label appears in
expired air as C^*02- In the mouse, the label appears
to be secreted into the duodenal and jejunal segment of
intestine, in bile, and possible in pancreatic secretion,
and to be reabsorbed largely in the more distal seg-
ments of the intestinal tract. In the mouse, the liver,
duodenum and jejunum, ileum, kidneys, and empty
caecum and colon contain the greatest total amounts of
label. One experiment in a GB-poisoned cat yielded no
evidence of metabolic alteration of 2-PAM; in the
mouse, an important metabolic produa of 2-PAM is
probably N-methyl-pyridone-2. (Author)
272
Biomedical Lab. , Wright Air Development Lab. ,
Wright -Patter son AFB, Ohio.
CUMULATIVE EFFECTS OF BORANE TOXICITY AS
REVEALED BY A CLINICAL TEST, by Dwight F.
Miller, Anton A. Tamas and others. Rept. on Health
Hazards of Materials and Radiation. Aug 60, I4p.
9 refs. WADD Technical rept. 60-604.
Order from OTS $0. 50 j PB 171 309
A series of studies on various aspects of the toxicology
of the boron-derivative, high-energy fuels is pre-
sented. These studies, made possible by a new tech-
nique, supply information on the absorption and trans-
port of boranes in the body.; Evidence for the chronic
buildup of boranes in the body is presented. The
animal data is correlated with studies and observations
of accidental human exposures and the analytical tech-
nique is evaluated. (Author^
Rodiobiology
Naval Radiological Defense Lab. . San Francisco,
Calif.
OPERATIONAL SIGNIFICANCE OF BIOLOGICAL RE-
COVERY FROM CHRONIC IRRADIATION: A COM-
PARISON OF SEVERAL RECOVERY THEORIES, by
E. Shapiro. 16 May 60, 48p. 4 refs. Research and
development technical rept. USNRDL-TR-421;
AD- 238 299. }
Order from LC mi$3. 30. pH$7. 80 PB 153 589
This report released for sale to the public 6 Jan 61 .
Several theories that predict the way in which the body
recovers from chronic exposure to whole-body radia-
tion are applied to a typical operational situation.
Adaptations of the Schwarzchlld Law and Smith's
modification of the Blair thepry are considered. The
general post -attack situation is broken down into pre-
■helter. shelter, and post -shelter periods, and the
recovery from doses received during each of these
periods is computed according to each of the theories.
The dependency of certain operational parameters on
fholce of theory is investigated. Among the parame-
ters studied are shelter entry time, shelter residual
number (shielding factor), ghelter exit time, and
postshelter radiological redovery effort. The study
indicates that except in special cases the operational
fiarameters are relatively insensitive to the choice of
theory. (Author)
Public Health Service. Washington, D. C.
RADIOLOGICAL HEALTH DATA. VOLUME 1. NO. 9
Monthly rept. Dec 60, 56p. i
Order from OTS $1.00. $9.bo/yr
PB 161 371-9
Cements:
Section I. -Mi Ik
Public Health Service Mi Ik. Monitoring Program
Strontium-90 in Bovine Milk from Minnesota
Strontium-90 Content in Canadian Dried Milk Products
Radionuclides in Human Milk
Section II. --Air
Public Health Service' Radiation Surveillance Network
Naval Research Laboratory Radioactivity Measure-
ments
Argonne National Laboratory Air Data (April-June
1960)
Radionuclide Analysis of Cincinnati Surface Air
Section III . - -Water
Public Health Service National Water (Quality Network
Strontium-90 in Tap Water (April-June 1960)
Section IV . - -Other Data
External Gamma Activity (]\x\y 1960)
Strontium-90 Concentration in Bread Purchased in
New York City (March-June 1960)
Argonne National Laboratory Soil Data (May- -June
1960)
Environmental Levels of Radioactivity at Atomic
Energy Commission Installations
Strontium-90 Content of Animal Fodders
(See also PB 161 371-7)
»■
School of Aviation Medicine, Brooks AFB, Tex.
BIOLOGIC EFFECTS OF NUCLEAR RADIATION IN
PRIMATES, by Robert W, Zellmer and John E.
Pickering. Ai|g 60. 12p. 22 refs. Rept. 60-66;
AD- 245 179.
Order from LC ml $2. 40. ph$3. 30 PB 152 630
Macaca mulatta primates were exposed to the neutron
and gamma radiation of nuclear detonations as one
phase of an extensive animal program designed to yield
a better understanding of the biologic effects of ionizing
radiation. Afield test utilizing ionizing radiation from
nuclear devices was chosen to simulate as closely as
pos s ible the conditions of dose, dose rate, and radiation
distribution that have occured in human exposures. i
In both detonations the radiation dose required to pro-
duce death in 30 days for 50 percent d the animals was
determined. All animals were followed for acute radia-
tion effects, and where no mortality occured, they are
being followed for long-term effects such as cataract
production, bone marrow change, shortening of life
span, and carcinogenesis.
Zoology-
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska.
A SURVEY OF INVERTEBRATE DISEASE VECTORS
IN ALASKA, by John M. Geary. Nov 53, 37p. 23 refs.
Proj. no. 22-1401-0004, Research rept. no. 1.
Order from LC mi$3. 00, ph$6. 30 PB 153 331
A large gap exists in regard to present knowledge of
the externally parasitic invertebrates present in Alaska,
and little is known regarding the presence of disease
they may carry. That group of parasites, therefore,
was the center of activity of this project for two years.
Primary interest was directed towards fleas, which
might be expected to transmit endemic typhus fever and
sylvatic plague. There is also the possibility that bu-
bonic plague -carriers might be present. Although of
secondary importance as a vector, fleas can also trans-
mit Rocky Mountain fever. Considerable emphasis has
been placed on ticks, which in Alaska could be expected
to carry tularemia and Rocky Mountain sponed fever.
273
Wisconsin U (Madfcon].
STUDIES ON THE INTERNAL CLOCK REOJLATING
DAILY ACTIVITY RHYTHMS IN RODENTS, by
Patricia J. DeCourseV, Final rept and Patents rept.
on Contract AF 49(638)691. 24 Aug 6a 8p. 7 refs.
AFOSR-TR-60-119; AD- 244 958.
Order from LC mi$ll 80. ph$l. 80 PB 152 631
The study emphasize^ the adaptive features of the phys
iological time sense 0f rodents. A measure of the time
sense was obtained by recording the dally running ac-
tivity of rodents in wfieel cages, in consunt environ-
ment condltiora . A Retailed study of the rhythms erf the
flying squirrel indicated that the squirrels had intern-
ally regulated daily <||ythm8 of activity which in con-
sunt environmental tdnditions, drifted out of phase
with the natural day-night cycle. In artifi^al or natu-
ral day schedules th«y gradually resynchronized their
activity to the time cM darkness by means of a daily
rhythm of resetting Ijy light. Similar mechanisms were
found in most other liociurnal rodents tested. In diur-
nal rodent species a mechanism of activity synchroni-
zation also was found. This differed in important de-
tails from that of th^ nocturnal species. Such studies
have profound implioation for Air Force Research pro-
grams. Time sense has been repeatedly demonstrated
in man, and an undefstanding of its relation to sleep-
wakefuiness cycles, jdaily blood-glucose and tempera-
ture cycles and the Related daily efficiency cycles is of
fundamental imponarice when subjecting human sub-
jects to stress conditions requiring optim^ perform-
ance. (Author)
:hemistry
Naval Radiologlcar Defense Lab. , San Francisco,
Calif.
FLAME PHOTOMETRIC DETERMINATION OF Na, K,
Ca, Mg, AND Sr m SEA WATER, by M. Honma.
15 Sep 55, 16p. 20 rtfs. Research and development
technical rept. USNRDL-TR-62.
Order from LC tmU- 40, ph$3. 30 PB 153 571
This reptHt release^ for sale to the pubUc 19 Jan 61 .
i
In the determination of many alkali and alkaline earth
metals, conventional analytical procedures are boch
time-consuming andi difficult. Moreover, chemical
treatment is not feasible when many analyses for both
cations and anions are necessary from a small sample.
A rapid, flame photometric procedure was developed
by which Na.K.Mg, and Ca values are obtained directly
from small volumes, of sea water without chemical
processing. Hazard^ from radioactive fumes are
avoided by the use of auxiliary apparatus. The stron-
tium determination Is made in the presence of calcium
after chemical separation because of sodium interfer-
ence. The flame ph<)tometric results compare favor-
ably in accuracy with those from gravimetric proce-
dures and data available in the literature. Radiation
and interaction interferences have been accounted for .
(Author)
Inorganic Chemistry
Royal Inst, ot Tech. (Sweden).
NOTES ON THE PREPARATION AND ANALYSIS OF
HALOGENIDE-FREE RH0DIUM(I1D PERCHLORATE
(SULFATE SOLUTIONS, by Clara Berecki-Biederraaaa
Technical note no. 2 on Contract AF 61(052)181.
15 Feb 60, lip. 12 refs. AFCRL-TN-60-462.
Order from LC mi$2. 40, ph$3. 30 PB 152 773
A method is described for the preparation of halogenid»
free rhodium(III) perchlorate (sulfate) solutions. As
starting material, rhodium chloride or rhodium bro-
mide can be used. The halogenide was removed by
means of ozone, which oxidizes "free" (not complex-
bound) halogenide to halogen and Rh(III) to Rh(V); The
Rh(V) produced, being a strong oxidizing agent, also
reacts with the halogenide according to Rh(V) +- 2X "^
Rh(ia) + X2- Methods for the detection of halogenide-
ioos in rhodium solutions are given. (Author)
Royal Inst, of Tech. (Sweden).
NOTES ON THE PREPARATION AND ANALYSIS OF
RUTHENIUM (ID) AND RUTHENRJM (IV) IN SULFATE
MEDIUM, by Felipe Brito. Technical note no. 1 on
Contract AF 61(052)181. 15 Feb 60, 13p. 8 refs.
AFCRL-TN-60-461; AD- 245 503.
Order from LC mi»2. 40. ph$3. 30 PB 152 772
For equilibrium studies, pure solutions of ruthenium
(III) and ruthenlum(IV) perchloraies or sulfates are
needed. A survey is given of synthetic and analytical
methods reported in literature. Since none of them was
suitable for the purpose, new or modified methods were
worked out. For the preparation of ruthenium(IV) sulfate
solution, Ru04 was reduced with H2O2 in dilute H2SO4 and
the ruthenium(IV) cations separatedfrom complex anions
by a cation exchanger. For the preparation of ruthe-
nlum(IIO> RUO4 was reduced with SOj. the excess SOj
removed and the sulfito complex decomposed. Total
ruthenium was determined by reducing to metallic
ruthenium, using Mg metal, and then weighing. For de-
termining ruthenium(III) or ruthenium(rV). a redox ti-
tration method is proposed: a known excess of cerium
(IV) sulfate in ><'2 M H2S0^ is added, the RuO. formed
is boiled off and the remaining cerlum(IV) backtitrated
with lron(ID ♦ ferroin. For the determination of H, the
total analytical concentration of H*- , in purely catlonic
Ru(IV) solutions, the ruthenium may be either held back
in a H*- saturated ion exchanger or bound by adding
acetylacetone. The H* set free can In both cases be
titrated with standard NaOH. Concordant results were
obtained using these two methods. (Author)
Organic Chemi$tr)r
British Columbia U. (Canada).
VOLATILE FLUORO COMPOUNDS, by R. C Cavell,
H. C. Clark, and C. j. WilUs. Technical rept. no. 1
on Contract Nonr- 2659(00). July 59, 34p. 7 refa.
AD- 227 622. ^ ^.,
Order from LC miJ3.00, ph$6. 30 PB 149 683
274
A study was begun of the preparation and properties ot
the perfluoroalkyl derivatives of the Group III and IV
elements and the properties of volatile transition metal
fluorides. Trimethyltrifluoromethyltin (I) was prepared
from hexamethyldltin and an excess of CF3I. Compound
I decomposed readily in a vacuum at 150°C to form
(013)3 SnF and perfluorocyclopropane; treatment with
aqueous alkali at room tem^rature or H2O at 100°C
brought about rapid hydrolyj^is. Halogenation reactions
Involving I produced such ciiimpounds as
(CH3)2(CF3)SnBr and (CH3)l(CF3)SnCl, suggesting that
the strength of the Sn-C bond, not the electronegativity
of the organic radical determines the cleavage of alkyl-
or aryl-Sn bonds. CF3I waf allowed to react with Sn or
Snl; the only products were fluorocarbons having up to
9 C atoms. Reactions of perfluoroalkyl-Li derivatives
with Sn compounds produced no identifiable products.
Studies of the Infrared spectra of NbF5-NH3 complexes
Indicated that the structure .was that of a coordination
compound. i
Massachusetts U. [Amherst]. |
CHEMISTRY OF HYDRAZINE DERIVATIVES, by
Louis A. Carpino. Final re«. for 15 July 56-
15 Feb 60 on Contract AF 18(603)114. [1960} 3p. 5 refa
AFOSR-TR-60-24. >
Order from LC ml$ 1.80, pf^ 1.80 PB 149 687
The work of this contract has been concerned with a
study of the oxidative reactions of hydrazine deriva-
tives. The guiding hypothesis In this work has been that
oxidation of monosubstitutea hydrazines occurs through
derivatives of dilmide whereas oxidation of 1, l-dH-
•ubetituted hydrazines occurs through azamine inter-
mediates. A new method of 'converting certain 1, 1-di-
mbatltuted hydrazines to hydrocarbons was discovered
and the scope of the reaction delineated. New synthetic
routes to a wide variety ot hydrazines were developed.
Examination ot the Forster azotlzation reaction led to
the necessity of synthesizing representatives of a new
class of organic compounds, the 0-acyl and 0-arene-
sulfonylhydroxylamlnes. These unique hydroxylamine
derivatives promise to be useful amlnating agents.
i
(Jueen's U. , Belfast (Northern Ireland).
MECHANISMS OF THE OXIDATION OF AMINES,
byH. B. Henbest. Annual technical rept. for
I Oct 59-30 Sep 60 on Contract DA 91-591-EUC-1274.
[I960) 41p. 14 refs.
Order from LC mi$3. 30, phj7. 80 PB 153 085
1
Contents:
The reactions of tertiary amines with oxygen and with
ozone.
The oxidation of amines with alkoxyl radicals .
Reactions of amines in aquepus solution with polyva-
lent metal oxidants .
Rochester U. , N. Y.
A STUDY OF THE SYNTHESIS AND PROPERTIES OF
SOME CYCLIC UNSATURATED MOLECULES OF
THEORETICAL INTEREST,; by V. Boekelheide. Final
rept. for 1 Feb 53-28 Feb 5^ on Contracts DA 30-115-
ORD-421 and DA 30-115-ORD-723. [1958] I7p. 16 refs.
OCR rept. 770-...; AD-21 1536.
Order from LC ml$2. 40, phf 3. 30 PB 149 664
The following generalizations about aromatic character
in polycyclic systems can be made. There are no
simple rules, no magic numbers such as those of the
HUckel rule, which will allow one to predict aromatlclty
in this case. The number at f! electrons available may
or may not be Important, but this cannot be decided
without making a proper molecular orbital calculation.
Thus far for all of the cases investigated, the predic-
tions given by simple molecular orbital theory are in
qualitative agreement with the experimental facts.
Royal Holloway ColL , U. of London (Gt. Brit. )
BORON HALIDES AND DERIVED COMPOUNDS, by
Arthur Finch and G. Chainani. Annual technical status
rept. no. 1, 1 Oct 59-30 Sep 60, on Contract DA 91-
591-EUC- 1276-01-4096-60 (R i D 235). [I960] 23p.
11 refs.
Order from LC mi$2. 70, phH 80 PB 152 767
The preparation, esterification, and orthobaric pyrol-
ysls of the new cyclic boron compound, trlmethylene
chloroboronate, have been studied. A detailed scheme
representing the course of pyrolysis is presented; data!
for new compounds are listed. The new compounds 5
ethylene propyl boronate and trlmethylene propyl boron*
ate have been synthesised. Analytical data for these j
compounds and their solid amine complexes Is not com-f
plete; preliminary figures are In reasonable agreement*
with expectation. Some exploratory experiments with
Na/K alloy and halogen- containing boron compounds
have been made. (Author)
Southern Research Inst. , Birmingham, Ala.
FAR INFRARED SPECTRA OF SUBSHTUTED ARO-
MATIC HYDROCARBONS, by William S. Wilcox,
C V. Stephenson, and W. C. Coburn, Jr. Rept. for
1 June 58-31 May 60 on Experimental Techniques for
Materials Research, Contract AF 33(616)5855. Sep 60.
189p. 86 refs. W ADD Technical rept. 60-333.
Order from OTS $3.00 PB 171 300
The results of a fundamental study of the Infrared
spectra of substituted aromatic hydrocarbons from 2 to
35 microns are discussed. The purpose of this work
has been to explore the possibility of correlating the
absorption frequencies of substituted benzenes with
physical properties of the molecules or of their sub-
stltuents. Since the far infrared spectra (15 to 35
microns) exhibits a greater sensitivity to changes in
the substltuents bonded to the aromatic ring than the
rocksalt speara (2 to IS microns), the correlation
studies have been limited to the long wavelength region.
The materials, apparatus and techniques used In this
study are discussed In Appendix I. The far infrared
spectra of 94 substituted benzenes are given. (Author)
Ph)rsical Chemistry
Atlantic Research Corp. , Alexandria, Va.
SOUD-PROPELLANT SOURCE OF CESUM PLASMA,
by Lawrence W. Fagg and Raymond Friedman. Rept.
on Research on High-Pressure Plasma Production Tech-
niques, Contract AF 49(638)651, ARPA Order no. 6-58,
Task no. 11. 23 June 60, 4p. 2 refs. AFOSR TN-60-
701; AD- 239 696.
Order from LC mi$ 1.80. ph$ 1.80 FB 153 033
i^
275
An investigation of the combustion characteristics and
ion and electron density obtainable by burning mixtures
Of CsC104:Al and (:sN03:Al is being made.
Bonn U. (West Germany).
MASS SPECTROVtTRIC INVESTIGATIONS BY MEANS
OF A FIELD EMISSION ION SOURCE, by
H. D. Beckey and IWilhelm E. Groch. Rept. 4 c4 Final
rept. for July ST'-Apr 60 on Contract AF 61(514)1079.
AFCRC-TR-60-276; AD-245 445.
$3.60. ph$9. 30 PB 152 770
[1960] 51p. 17 ref^
Order from LC m
Contents: .
The photochemical formation and the photolysis of
nitrous oxide in the extreme ultraviolet, by
H. Schierholz
Photochemical forfnation of organic compounds from
mixtures of simple gases, by H. von Weyssenhoff
Intense light sources for the vacuum ultraviolet, by
E. J. Comes and E. W. Schlag
Mass spectrometrtc investigations by means of a field
emission ion source, by H. D. Beckey
Central Technical Inst. TNG. , The Hague
(Netherlands)
HIGH TEMPERATURE GALVANIC FUEL CELLS, ^by
G. H. J. Broers a<id M Schenke. Final rept. for 1 Jan-
31 Dec 59 on Conttact DA 91 -591 -EUC- 1023. Jan 60,
47p. AD- 234 912.
Order from LC mi$3. 30, ph$7 . 80 PB 149 675
An investigation vM)as made of a new type of high-tem-
perature cell electrolyte composed of about equal
amounts of non-sititered MgO and UNaCOs- A discus-
sion is given of vatrious techniques for pressing and
molding the electrolyte. Hydrogen, CO, and O were
galvanically utilized as fuel gases to a final concentra-
tion of less than 2|volume-':i^, at current densities of
20 A/sq cm. The 'life of the cells under continuous op-
eration ranged frdm 2 to 8 weeks, after which the
galvanic action ha^ not ceased. The main deterioration
was thought to be ti gradual loss in anode-elearolyte
contact, with som0 influence caused by carbonate
losses.
Chemical Engin^ring Lab. , Princeton U. , N. J.
CHEMICAL KINETICS AND COMBUSTION, by
M. Boudart. Reptj. on Contract AF 49(638)32. (1960)
25p. 38 refs. AFf)SR-TN-60-1150.
Order from LC tA%2. 70, ph$4. 80 ' PB 153 090
An invited survey paper, presented at the Vlllth Inter-
national Symposiifn on Combustion, September, 1^60.
Two familiar proi^lems are discuased: The possibility
of obtaining kinetit information from combustion
studies and the aopUcability of equilibrium chemical
kinetics to the bu^ of the reaaions in the flame.
(Author) j
(^lemical Engineering Lab. . Princeton U. , N. J.
STAGNATION OF A COMPRESSIBLE AND RELAX-
ING GAS AT A PlTOT TUBE: THEORETICAL AND
EXPERIMENTAL ISTUDY. by Stanley C. Li. Rept. on
Contraa AF 49(638)32. [1960] I79p. 117 refs. AFOSR-
TN-60-1151: AD-)46 601.
Order from LC mi$8. 10, pl427. 30 PB 153 091
A complete numerical solution of the Kantrowitz prob-
lem is given for a compressible gas and a Pitoc tube
following Griffith. The vibrational relaxation time al
sulfur dioxide has been studied over an extended tem-
perature range. (Author)
Cornell U. , Ithaca, N. Y.
CN STRETCHING BANDS IN THE RAMAN SPECTRA
OF SOME GROUP lb AND GROUP lib COMPLEX
CTVANIDES, by G. W, Chantry and R. A. Plane. Rept
on Contract AF 49(638)279. 22 Mar 60, 12p. 9 refs.
AFOSR-TN-60-330; AD-234 794.
Order from LC miW. 40, ph$8. 30 PB 149 6«1
The Raman spectra at solutions containing cuprous,
argentous and mercuric ions together with cyanide ioni
Indicate the presence of the dl-, tri and tetra coordi-
nated complexes. The speara from solutions conuin-
ing zinc and cadmium ions, respectively, with cyanide
ions show, on the other hand, only the tetra coordinated
complex. (Author)
Istituto di CSiimica Fisica dell'Unlversita, Pavia
(Italy).
DIPOLE MOMENT STUDIES OF DIPHENYLETHER,
DIPHENYSULFIDE ANl5 THEIR DERIVATIVES, by
Mario Rolla. Final technical rept. no. 2, 1 Jan-
31 Dec 59. on Contract DA 91-591-EUC-1016.
30 Jan 60, 59p. 23 refs. AD-234 916.
Order from LC miJ3.60. ph$9.30 PB 149 678
Electric dipole moments were determined for 6 dl-
phenyleiher (DPhE) and for 6 dlphenylsulfide (DPhS)
derivatives. Each compound had a nitro group attached
to the para position of one phenyl ring while the other
ring ha3a CI or Br atom or a methyl group attached to
the ortho or pieu position. The electric dipole mo-
ments were determined according to the dilute solution
method in benzene solution at 20° ♦ 0.05OC by means
of dielectric constant, density, and refractive index
measurements. (See also AD- 211 444)
Kentucky U. , Lexington.
N-SULFINYL AMINES. EFFECT OF STRUCTURE ON
THE ALCOHOL YSIS REACTION, by Walter T.
Smith. Jr. and Lowell D. Grinninger. Rept. on Con-
tract AF 49(638)49. Oct 60. 4p. 3 refs. AFOSR-TN-
60-855; AD-245 229.
Order from LCmi$ 1.80. ph$ 1.80 PB 152 746
The results are reported of a continuing study which
shows that a variety of N.-8ulfinyl -anilines react rap-
idly and completely with methyl alcohol.
Lund U. (Sweden).
EQUILIBRIUM STUDIES ON THE DISPROPORTIONA-
TION REACTION BETWEEN SOME DIALKYL DISUL-
.-FIDES, by L. Haraldsson. C J. Olander and ochers.
Technical note no. 3 on Contract [AF) 61(062)46.
1 May 60. lOp. 7 refs. AFOSR-TN-59-573; AD-2l7(W7.
Order from LC mi$l. 80. ph$l. 80 PB 152 478
The disproportionation equilibrium between two sym-
metric disulfides and the corresponding mixed one hM
m|$8.
276
been determined at 25° and at 60^^ by use of vaporphast
chromatographic technique. For diethyl disulfide in
mixture with dimethyl- and di-i -propyl disulfide, re-
spectively, the equilibrium constant is close to the
sutistically expected value. 4. For the pair diethyl -
and di-t -butyl disulfide, thp constant is 24. Within the
uncertainty of the experiments, the equilibrium con-
stant is temperature independent and thus AH is equal
torero. The strongly restricted internal rotation in
di-t-butyl disulfide is responsible for the high value of
the equilibrium constant. (Author)
f
i
Massachusetts U. , Amherst.
TOE SCATTERING OF LIGHT BY n -PARAFFIN
VAPORS, by Joseph Powers. Daniel A. Keedy. and
Richard S. Stein. Technical rept. no. 1 1 on Contract
Noiir-2151(0O). 23 July 59, U4p. 21 refs. AD -225 440.
Order from LC mi$3. 30, ph$7. 80 PB 149 631
Aji Improved apparatus for the measurement of the de-
polarization value of gases and vapors has been con-
structed. The parallel incident light beam transmitted
through the scattering volume eliminates the use of a
controversial convergence correction. A photomulti-
plier detection system improves the reproducibility of
the measurements. The depolarization values of the
gases and vapors measured in this study have the same
order of magnitude as the literature values. The dis-
crepancy between the experimental and the calculated
depolarization values must lie in the theory. Since the
variation of the depolarization values of n-pentane and
n-hexane with temperature over the range of tempera-
ture studied remained constant within the limits of
experimental error, no calculation of a Boltzman type
correction factor could be made. The results of the
calculation of depolarization values of n-hexane and
n-heptane are given in Table I for the cases a( rotation
and for the trans weighted refinement. (Author)
National Research Labs. , Ottawa (Canada).
A PHOTO-ELECTRIC DEVICE FOR THE MEASURE-
MEHT OF QUANTITY OF LIQUID, by R. Sandri.
Sep 60, 7p. Mechanical engineering rept. MI-822.
Order from LCmiJ 1.80, ph$ 1.80 PB 153 606
The report deals with a photo-electric device producing
an output voltage which is a linear function of the quan-
tity of liquid conuined in the measuring tube. After a
brief discussion of the useftilness of the device, the
principle of the measurement is explained. A detailed
description is then given at the optical system, its func-
tion and possible sources of error. Finally, the method
of calibration of the system is described. An accuracy
better than 1 percent of the maximum filling can be
attained. The apparatus can follow rapid changes of
^lantity of liquid. (Author)
Naval Radiological Defenae Lab. , San Francisco.
Calif.
THE ASSOCIATION OF C^ROUS ION WITH IODIDE,
BROMIDE AND FLUORIDE IONS, by Stanley W.
Mayer and S. David Schwartz. Interim rept. 7 June 49,
I2p. 12 refs. AD- 128(C).
Order from LC mi$2. 40, ph$3. 30 PB 153 588
This report released for sale to the public 19 Jan 61.
The distribution of Ce"*'^ between cation exchange resin
and solutions of sodium iodide, bromide, fluoride and
perchlorate has been measured. The constants for
ion-pair formation between Ce^^ and the halides have
been calculated. (Author)
Naval Research Lab. , Washington, D. C.
SYNERGISTIC SURFACE TENSION EFFECTS FROM
MIXTURES OF FLUORINATED ALCOHOLS WFTH
CONVENTIONAL WETTING AGENTS, by Marianne K.
Bernen and W. A. Zisman. Interim rept. 20 Oct 60,
18p. 27 refs. NRL rept. 5556.
Order from LC mi$2.40, phJ3.30 PB 150 619
Aqueous solutions of any single, conventional hydro-
carbon derivative have surface tensions which never go
below 26 to 27 dynes/cm, but certain synergistic mix-
tures of such wetting agents will depress the surface
tension of water to around 22 to 24 dynes/cm. This
Investigation has demonstrated that small quantities of
highly fluorinated, insoluble, alcohols, when added to
conventional wetting agents, become solubllzed in the
micelles of the latter and can thus lower the surface
tension of water well below a value obtainable by any
mixture of unfluorinated compounds. These low sur-
face tension values represent the closest possible pack
ing of the fluorinated alcohol when adsc»-bed at the
water /air Interface. Where the solubilizing agent is
not sufficiently water-soluble, an increase in the
solvent power of the continuous phase can be effected
by adding a mutual solvent; the fluoro alcohol can then
be solubilized to become effective in generating low
surface tensions. Under the best conditions synergistic
systems were produced having surface tensions of
15. 2 dynes/cm at 25°C if a perfluoroalcohol was used
^nd 19.9 dynes/cm if an (V-monohydroperfluoroalkyl
alcohol was used. (Author)
Physics Lab. , Wright Air Develc^ment Div. ,
Wright- Patterson AFB, Ohio.
RADIOCHEMICAL PRODUCTION AND FATE OF
FREE RADICALS, by Roger E. Rondeau. Rq>t. for
Mar- June 60 on Materials Analysis and Evaluation Tech-
niques. Aug 60, 28p. 31 refs. WADD Technical repL
60-544.
Order from OTS $0. 75 FB 171 310
This report represents an effort to interpret and corre-
late to a limited extent, the many physico-chemical
phenomena of radiation chemistry in terms of elemen-
tary free radical processes. (Author)
Rochester U. . N. Y.
THE FLUORESCENCE OF SULFUR DIOXIDE, by
Kenneth F. Greenough. Technical rept. no. 1 on Con-
tract Nonr-(668)15. 1 Feb 60, 6lp. 30 refs.
AD-232 410.
Order from LC ml$3. 90. ph$10. 80 PB 153 158
The fluorescence spectrum of SO2 was investigated. In
the gas phase, SO2 molecules raised to the second ex-
cited electronic state by absorption of 2700 to 3100 A
radiation undergo fluorescence transitions to the ground
state. Resonance fluorescence bands from 2800 to 3 100 A
superimposed on a continuous spectrum extending be-
yond 4000 A are both associated with transitions from
277
the zero and eaccitisd vibrational levels of the excited
state. Uo fluoreHence was observed from the first
excited electroniq sttte by irradiation ot SO2 mole-
cules with 3400 tq 3900 A light. The fluorescence
spect rum of solid 302 at 77° K excited by 2400 to 3500 A
radiation, is very similar to the gas phase spectrum.
The intensities of the transitions from the first excited
electronic state increase relative to those from the
second excited electronic state as the pressure of SO2
increases; this intensity change is ascribed to an en-
hancement of the internal conversion and thermal de-
activation procesies. The second excited electronic
state is more sensitive to self quenching than the first
excited electronic} sute, and the reverse is true for
quenching by the foreign gases, C02- H2, O2. and He.
Both excited electronic sutes are more sensitive to
self -quenching ih4n to foreign gas quenching. The
mean lifetime of «jhe first excited electronic state of
solid 502 ** ^"7° K is 0. 4 < ^<0. 6 msec; the mean life-
time of the second excited electronic state extrapolated
to zero SO2 presfliure is 0. 042 msec.
Sheffield U. (Gt.| Brit. ).
THE M(XECULAiR ARRANGEMENTS OF SOME
COMPONENTS Ot THE CHLOROPLAST, by
F. W. j. Teale. Final technical rept. no. 2, 1 Jan-
31 Dec 59, on PrUnary Fhocpchemical Processes in
Photosynthesis. Oontract DA 91-[591}-EUC-[1006].
20 Feb 60, 58p. $0 refs. AD- 234 401.
Order from LC n<$3. 60, ph|9. 30 PB 149 658
I
Chlorophyll fluorescence in chloroplasts is sensitized
by light absorbed t>y tryptophan residues in structural
protein. In vitro tneasurements with the model system
indole- chlorophyll suggest that energy transfer takes
place by resonance poupling at an intermolecular sepa-
ration at about 30: A in the chloroplast and does not in-
volve complex fortnation. The degree at chlorophyll
fluorescence quenching produced by a known fraction of
non-fluorescent chlorophyll molecules indicates the
migration al the siinglet excited state amongst some
275 different molecules prior to trapping. Comparison
with the observedl fluorescence polarization suggest
little preferred orientation In Chlorella. The photo-
oxidadon al chlorophylls in organic solvents 1$ pre-
vented by carotenbids, but pheophytlns are unaffected,
suggesting a possible carotenold- chlorophyll] inkage
through the magntslum atom. Hiosphollpids prevent
the dlmerizatton d chlorophyll in vitro. A complex
containing chlorot)hyll, fucoxanthol, and phospholipids
can be extracted from brown algae, with fluorescence
parameters similjsr to algae. (Author)
similfar to al
[Sheffield U. (Gt Brit )].
TEMPERATURE COEFFICIENTS OF ATOMS RECOM
BINATION, by Geerge Porter and J. Ashley Smith.
Final technical rebt. no. 2. 1 Jan-31 Dec 59. on Con-
tract DA 91 -591 -tUC-988. 14 Jan 60. 61p. AD-234 394.
Order from LC n*$3. 90. ph$10. 80 FB 149 659
nril$3.
The n^ethods desoribed in the report of December 1958
(FTR No. 1) have been used to obuin rate consunts
and temperature coefficients of recombination of iodine
atoms in the presence of various chaperon molecules.
A theory of atom recombination has been developed,
based on the equi^brium I ■*- M-^IM (1) where I is the
iodine atppi and M the chaperon molecule, followed by
I •»■ IM— ^12 "♦ M (2). The equilibrium constant ot (1) Is
calculated by statistical mechanical methods using the
experimenully measured "activation energy" to derin
the beat of formation of IM. The rate consunt of (2) is
calculated by means of collision theory. The calcula-
tions yield values of A in the equation k^ ■ ATe^E/RT
which are in fair agreen^ent with the experimenul
results for chaperon molecules whose rate consunts
differ by a factor of one thousand. The nature of the
binding energy in IM is considered and it is concluded
that charge transfer complex formation is probably of
principal importance. Preliminary attempts to detect
charge transfer spectra were unsuccessful in the gas
phase but transient spectra which are probably of this
type have now been observed in solution. (Author)
EARTH SCIENCES
Massachusetts U. , Amherst.
GEOMORPHIC STUDIES OF THE PROVINCETOWN
DUNES. CAPE COD, MASSACHUffilTTS, by H. T. U.
Smith (Master's thesis) and Curtis Messinger. Tech-
nical rept. no. 1 on Contract Nonr- 224 2(00). June 59,
79p. 58 refs. AD- 220 653.
Order from LC miM- 50, ph$12. 30 PB 149 638
Climatology and Meteorology
Air Force [Canibridge Research Labs. ] Bedford,
Mass.
EXAMPLES OF PROJECT TIROS DATA AND THEIR
PRACTICAL METEOROLOGICAL USE, by William K.
Widger, Jr. July 60, 109p. 9 refs. GRD Research
notes no. 38; GRD TN-60-470; AD- 245 132.
Order from LC mi$5.70, ph$I6.80 PB 152 684
This report released for sale to the public 6 Jan 61.
Selected pictures from the TIROS I meteorological
satellite are shown and In many cases are compared to
the concurrent synoptic maps. Examples of trans-
missions of TIROS data that were available for practi-
cal weather analyses are also illustrated. A brief dis-
cussion is given of the further research potential of
these data and of the Infrared meteorological data that
are expected to be obtained from TIROS II. (Author)
Air Force Cambridge Research [Labs. ) Bedford.
EXTREME VALUE STATISTICS IN METEOROLOGY:
A METHOD OF APPLICATION, by Irving I. Grln-
gorten. June 60, 72p. 25 refs. Air Force Surveys in
Geophysics no. 125; AFCRC-TN-60-442; AD-245 023.
Order from LC ml$4. 50, ph$ 12^30 PB 152 7«
While there have been several treatises on the appli-
cations of extreme -value theory to design and opers-
tiooal problems, this Survey Is written to present
simpler procedures with unbiased results. Most pre-
vious applications have used Fisher -Tlppetl distribu-
tions exclusively, which admittedly are limiting foriW
278
thst are reached asymptotically. Other distributions,
tlprefore, between the Gaussian and the Fisher -Tlppett
types are examined and applied herein. The relation of
amual extremes of meteorological parameters to their
hourly and daily distributions is also examined to see
what might be gained from short records, especially
the records of wind speeds. Tl»e latter require special
ti«atment because the annual extremes of winds do not
■ppear to be part of a larger homogeneous population
of daily winds. (Author) >
Air Weather Service, Scott AFB. UL
FORECASTERS • GU.IDE ON AIRCRAFT ICING.
1 Oct 60, 55p. 56 refs. Air Weather Service Manual
105-39. supersedes AWSM 105-39, Jan 53; AD-245 726.
Order from LC ml$3. 60, ph$9. 30 PB 152 977
The definitions of types and intensities of icing are
stated. The nature of the icing hazard, methods of com
batting it, and physical and operational factors in ice
formation are briefly reviewed. Data on distribution of
icing In the atmosphere with time and space, synoptic
situations, etc. , are summarized. A selection of non-
synoptic aids for Icing forecasting derived from various
onplrical studies is presented and their utility dis-
cussed. A suggested outline of steps for Integrating the
above information and aids into a synoptic forecast pro-
cedure for forecasting Icing is presented In the last
chapter. 1
Chicago U., 111.
BAHAMAS CIRCLE COMPUTATIONS. PART I. DE-
SIGN OF THE EXPERIMENT, by F. Baer and
J. Mlhaljan. Rept. on Contraa Nonr-212119. Jan 60,
1^. 2 refs. AD- 232 181.
Order from LC mi$2. 40, ph$3. 30 PB 152 905
Contents:
A program for computation on the Bahamas circle by
Ferdinand Baer
Smoothing of Irregularly spaced discrete data on a
circle by John Mlhaljan *
Cornell U. . Ithaca. N. Y.
WINTER M1CR0CLIMATF.S OF IMPORTANCE TO
ALASKAN SMALL MAMMALS AND BIRDS, by Harry
McClu re Johnson. Rept. 00 Contract A F 33(038)12764.
Mar 57. 147p. 50 refs. AAL Technical rept. 57-2.
Order from LC mi$7. 20, ph$22 80 PB 153 345
Winter microclimatic conditions at areas in the con-
tinental interior of Alaska, particularly near Fairbanks.
Alaska, and at areas on the Arctic Slope of Alaska were
measured and observed during the 1950-1951 and 1951-
1952 winter periods. The microclimatic and macro-
cllnMtlc conditions, consisting of changing fields and
diltributlons of quantities, were approximately deter -
■taod In the continental interior for a variety of habitat
tjipes at areas of valley lowland, adjoining hills, small
depressions, and the Cbena River channel. The deter -
nlnation of temperature fields was emphasized. The
microclimatic and macroclimatic conditions were ap-
proKimacely determined for a variety of microolimatic
•nd macroclimatic states a^d events In the several
main microclimatic zones. Concurrent with the deter-
minations of conditions of the physical environment ob-
servations were made concerning animal activity and
the biotic environment. An attempt was made to deter-
mine the response of these animals to conditions In the
several zones during the principal microclimatic states
aixl events. The subnivean stnall mammals were de-
pendent for survival upon the continuous existence of
the warm subnivean microclimates. The small birds
at times fed on seeds on the cold snow surface when it
had temperatures of -60° to -70Pf.
Hawaii Inst, of Geophys Ics , Honolulu.
NOTES ON THE METEOROLOGY OF THE TROPICAL
PAQFIC AND SOUTHEAST ASIA. ed. byC. S.
Ramage. Interim rept. on Contract AF 19(604)1942.
Dec 59, 176p. 40 refs. AFCRC TN-60-216;
AD-235 212
Order from LC ml$8. 10. ph$27. 30 PB 149 668
Included in the report are:
Relationship of general circulation to normal weather
over Southern Asia and the Western Pacific during the
cool season, pub. in the Jnl. of Meteorology 9:
403-408, Dec 52.
The cool-season tropical disturbances of Southeast
Asia. pub. In the Jnl. of Meteorology 12:252-262,
June 55
Non-frontal crachln and the cool season clouds of the
China Seas , pub. in the BuUetyi of the American
Meteorological Society 35: 404-411, Nov 54
Variation of rainfall over South China through the wet
season, pub. In the Bulletin of the American Meteoro
logical Society 33: 308-311, Sep 52
Diurnal variation of summer rainfall over East China,
Korea and Japan, pub. in the Jnl. of Meteorology
9: 83-86, Apr 52.
Hawaii Inst, of Geophysics, Honolulu.
NOTES ON THE METEOROLOGY OF THE TROPICAL
PACIFIC AND SOUTHEAST ASIA, by C. S. Ramage, ed
Interim rept. txi Contract AF 19(604)1942. June 60,
181p. 98 refs. Air Force Surveys in Geophysics
no. 126; AFCRC-TN-60-455.
Order from LC mlW.40, ph$28.80 PB 152 613
This report Is designed to supplement other texts on
tropical meteorology. It makes use of new observa-
tional material and accords the synoptic features of the
monsoons more attention than they have received In the
paSf . Hints on analysis, and the uses of auxiliary
charts and continuity are followed by a chapter on the
[Physical geography of the Pacific and a gazetteer de-
scribing the locations and environments of observing
stations . Chapter 3 tabulates monthly mean resultant
winds, steadiness and other derived data at standard
pressure levels for 34 sounding stations. Chapter 4,
which broadly considers the climatology of the region,
leads to more detailed discussions of the synoptic
climatology of the tropospherlc field of motion In the
central Pacific (Chapter 5) and of the synoptic clima-
tology of the China Seas and southeast Asia (Chapter 6).
The final chapters are devoted to tro{»cal cloud physics,
local effects and aerial weather reconnaissance.
(Author)
Included in the report are:
Relationship of general circulation of normal weather
over southern Asia and the western Pacific during the
cool seaton, pub. In Jnl. of Meteorology 9:403-408,
Dec 52
279
The cool- season tropical disturbances ot southeast Asia
pub. injnl. of Meteorology 12:252-262. June 55
Non- frontal orcein and the cool season clouds of the
China Seas, pyb. in Bull, ot the American Meteoro-
logical Societi 35:404-411, Nov 54
Variation of ratifall over south China through the wet
season, pub. |n Bull, of the American Meteorological
Society 33:308-311. Sep 52
Diurnal variation of summer rainfall over East China,
Korea and Jap in, pub. in Jnl. of Meteorology
9:83-86, Afr J2.
Imperial Coll. , London (Gt. Brit. ).
ACCRETION IH MIXED CLOUDS, by W. C Macklin.
Technical (Scie<itific) noce no. 8 on Contract
AF 61(052)254. July 60, 33p. 20 refs. AFCRC TN-
60-459.
Order from LC >ni$3. 00, ph$6. 30 PB 153 391
hii
The rate of acct^tion of ice and the nature and struc-
ture of the ice 4epo8ited on a body moving in a super -
cooled cloud is effected by the presence of ice particles
in the cloud; chgre are important implications to the
growth of hailscpnes. (Author)
Imperial Coll. of Science and Tech. , London
(Gt. Brit.)
THE DENSITY DP HAILSTONES COLLECTED FROM
A SUMMER STpRM, by W . C. MackJin. E. Sirauch
and F. H. Ludh m. Technical (scientific) note no. 7
61(052)254. June 60, 12p. 5 refs.
on Contract AF
AFCRC-TN-60-t458.
Order from LC
Measurements
made by immeri
liquids of varyiig
stones (mass 0.
gle storm rangdd
Some aspects o1
discussed.
mi$2.40, ph$3.30
(f
Imperial Coll
(Gt. Bfit.)
THE FALLSPE
Macklin and P
note no. 6 on
8 refs . AFCRO
Order from LC
Measurements
jects resembli
drag coefficieni)5
stones . It has
range from tho^e
depending on
ihe stone. (Autfior
ing
McGill U. (Camda)
TEMPERATURE
PB 152 775
the densities of hailstones have been
ing the stones in a series of chilled
densities . The densities. of 169
1 to 17.3 grams) obtained from a sixi-
-■ from 0.875 to 0.912 ± .003 g cm'"*,
the structure of the hailstones are
of Science and Tech . , London
iDS OF HAILSTONES, by W . C.
H. Ludlam. Technical (scientific)
Contract AP 61(052)254. June 60, 23p.
-TN-60-457.
mi$2.70, ph$4.80 PB 152 774
lave been made of the speeds of ice ob-
hailstones during free fall, and of the
of such objects and of natural hail-
l^en found that the drag coefficients
of spheres (about 0.45) to about U.8,
shape and surface characteristics of
)
AND WIND FREQUENCY TABLES
FOR NORTH AMERICA AND GREENLAND, VOL I
JANUARY-JUNE ed. by J. N. Rayner. Rept. on Con-
tract DA 19-1 29tqm- 1447. Aug 60. 278p. Araic '
Meteorology Research Group Pub. in Meteorology
no. 24.
Order from LC iniSll.IO, ph$42.60 PB 152 952-1
McGill U. (Canada).
TEMPERATURE AND WIND FREQUENCY TABLES
FOR NORTH AMERICA AND GREENLAND, VOL. U,
JULY -DECEMBER, ed. by J. N. Rayner. Rept. on
Contract DA 19-1 29-qm- 1447. Sep 60, 278p. Araic
Meteorology Research Group Pub. in Meteorology
no. 25.
Order from LC ml$ 11.10, ph$42. 60 PB 152 952-2
Naval Ordnance Test* Station, China Lake, Calif.
CURVED-EARTH HORIZONTAL- DISTAnCE CALCU-
LATOR FOR THE REDUCTION OF RAWIN- DETER-
MINED UPPER-WIND DATA, by Paul H. Miller.
15 July 60, 12p. NOTS TP 2513; NAVWEPS rept. 70W;
AD- 245 078.
Order from LC mi$2.40, ph$3.30 PB 152 6W
A calculator incorporating earth-cui'vature correcUoH
has been developed and constructed for use in the
reduction of upper -wind data. The calculator deter-
mines horizontal distances of a target at known altitudt
(up to 40 km) and elevation angle (6 to 45 deg). (Auttw^
Naval Ordnance Test Station, China Lake, Calif.
EVALUATION OF A METHOD OF CIRRUS FORE-
CASTING AT THE NAVAL ORIWANCE TEST STA-
TION, byD. L. Famham. 15 July 60, 18p. 7 refs.
NOTS TP 2528; NAVWEPS rept. 7104.
Order from LC mi$2. 40, ph$3. 30 PB 152 700
A practical and objective method of forecasting cirnia
cloudiness at the Naval Ordnance Test Sution, China
Lake, California, has been tested and evaluated. Re-
sults or using the method from October 1959 through
May 1960 are shown. It is concluded that the method
is accurate enough to use as a forecasting aid. (Author)
Naval Postgraduate School, Monterey, Calif.
THE CHURNAL TEMPERATURE WAVE IN A LAY-
ERED ATMOSPHERE, by Louis D. Megehee, Jr.
Master's thesis. 1959, 24p. 7 refs. AD- 230 565.
Order from LC mi$2.70, ph*4.80 PB 153 064
The partial differential equation for heat diffusion is
numerically integrated. A solution is obtained for the
diurnal temperature variation with a bounded coefficiw
of eddy diffusivity which varies periodically with time
and nonlinearly with height. The surface wave is^ rep-
resented by the sum of a diurnal and a semidiurnal bir-
monic wave. The results may be interpreted to apply
over a fairly broad range of diffusivity values and
height. With appropriate choices of the various param-
eters . reasonably good agreement is obtained betweei
theoretical and observational values of amplitude re-
duction and phase lag. (Author)
Naval Postgraduate School, Monterey, Calif.
A GRAPHICAL -NUMERICAL PREDICTION OF THE
1000-MB SURFACE WITH NON-ADIABATIC WARMINC
by Yeh-Chun Wang. Master's thesis . 1959. 48p. 6 reft
AD- 230 562.
Order from LC mi$3.30, ph$7.80 PB 153 063
280
A two- level graphical -numerical prediction model is ex
tended so as to incorporate some orographical and non-
adiabatic warming or cooling effects in a manner such
that almost no extra work is added. The model is ap-
plied to several cases where non-adiabatic heat ex-
changes are pronounced. The resulting prognoses show
• material improvement over a similar model which
omits the non-adiabatic influence. (Author)
Norske Meteorologiske Institutt (Norway).
SIGNIFICANCE OF REGRESSION EQUATIONS DE-
RIVED FROM SERIALLY CORRELATED DATA, AND
A PROCEDURE OF SELECTING OPTIMAL PREDIC-
TORS, by Jack Nord(f. Technical note no. I on Contract
AF 61(052)374. [1960] 2lp, 8 refs. AFCRL-TN-
«>-6i3. ;
Order from LC mi$2. 70, ph$4. 80 PB 152 769
The significance of statistical parameters derived
from serially correlated data is discussed and a
procedure of selecting optimal jjredictors is proposed.
It is suggested that this procedure will be more effi-
cient than some of those being in operational use.
(Author)
Pennsylvania State U. Mineral Industries Experiment
Station, University Park.
MONTHLY MEAN 50 MB AND 100 MB CHARTS PRE-
CEaNG THE IGY, by Hans A. Panofsky. Final rept.
Part 3 (of three parts) on Contract AF 19(604)2190.
Aug 60, 130p. 2 refs. AFCRC-TR-60-240 OH).
Order from LC mi$6.30, ph$19.80 PB 152 930
Mean monthly maps of the lower stratosphere for the
24 months immediately preceding the IGY, July 1955
through June 1957. In addition, 50-mb and 100-mb
charts are presented for the first two months of the
IGY.
Weather Forecasting Research Center, U. of Chicago,
lU.
AN EXPERIMENT IN COMPUTATION OF PREQPITA-
TION, by Kaare Pedersen. Scientific rept. no. 2 on
Contract AF 19(604)7230. Aug 60, 13p. 3 refs.
AFCRLTN-60-669; AD-246 419.
Order from LCmi$2. 40, iM3. 30 PB 153 046
In a recent paper Smebye (1957) showed that if the mean
vertical velocity through a column and the temperature
and humidity at a representative level were known,
fairly accurate values of the precipitation could be com-
puted. The purpose of the present paper is to try out
this procedure by using the vertical velocities routinely
pn^lded by the Joint Numerical Weather Prediction
Center, J. N. W. P., Washington, D.C.
1
I
Woods Hole Oceanographic Institution, Mass.
CLOUD PATTERNS IN HURRICANE DAISY, by Joanne
S. Malkus, Claude Ronne, and Margaret Chaffee. Tech
nical rept . «8 on National Science Foundation Grant
no. 7368 and Contract (Nonr) 1721(00). Jan 60, 65p.
10 refs. Ref. no. 59-63; AD- 232 742.
Order from LC mi$3.90, ph$10.80 PB 152 870
Data were collected on August 25, 26, and 27, 1958,
during the incipient, deepening and mature days of
Hurricane Daisy to provide a quantitative description at
cloud panerns and their role in storm dynamics and
processes. Nose camera films were taken at several
flight levels from which cloud maps were constructed
for each of the 3 days studies. Comparisons were made
of cumulonimbus structure, eye-wall formation, extent
and height of the cirrus shield, and location erf rain-
bands for all 3 days. The outstanding result of this
visual cloud mapping was the persistence of lines or
spiral bands of cumulonimbus in the same relative
coordinate position over 48 hr. (Author)
Frost Science
Army Snow, Ice and Permafrost Research Establish-
ment, Wilmene. 111.
BIBLIOGRAPHY ON SNOW, ICE AND PERMAFROST •
WITH ABSTRACTS. VOLUME XIV, ed. by Thomas E.
Hu^s. Jan 60, 252p. 999 refs. SIPRE rept. 12.
Order from OTS 13. 00 PB 171 190
Deutscher Wetterdienst, Hohenpeissenberg (West
Germany).
03SERVATI0NS AND ANALYSIS OF SNOW CRYS-
TALS FOR PROVING THE SUITABILITY AS AERO-
LOGICAL SONDE. II. SPECIAL STUDIES ON THE
SEQUENCE OF SNOW CRYSTAL TYPES, ON HOAR-
FROST CRYSTALS, by Johannes Grunow. Final rept.
for 15 Jan 59-15 Jan 60 on Contract DA 91-591-EUC-
1030, 01-1189-59. 15 Feb 60, 174p. 33 refs.
Order from LCmi$8.10, ph$27.30 PB 152 541
Each snowfall was submitted to a qualitative snow crys-
tal analysis. For each observation term the shares of
the different crystal forms contained in a snow sample
were ascertained and presented in their temporal suc-
cession. In order to bfing the results of these analyses
into relation with the Weather situation, cases with
warm front precipitation, cold front precipitation, and
also cold air and warm air in interplay were selected.
The synoptic analysis of these days was carried out by
weather maps and aerological cross seaions; and by
help of the T^-s diagram of Nakaya, the state of satu-
ration was brought into relation with the growing con-
ditions of the different forms of snow crystals as
known from laboratory investigations. The purpxjse of
these comparative investigations was to derive se-
quences (rf snow crystal types that can be considered
characteristic for certain weather situa'tions. From
the analysis of operations with only one certain crystal
type dominating, the particular weather situation of
such cases was derived. One case of dendrites, falling
from a thin cloud stratum, resting upon the place of
observation, offered the opportunity to study micro-
crystals in their generating zone. Special observations
of hoar-frost offered the opportunity to study the grow-
ing conditions of ice crystals under natural conditions
at the place of their origin. The different forms were
put down in a new morphological classification of hoar-
frost crystals in dependence on the temperature
ranges of their generation. (Author) (See also
PB 143 108)
281
'^ff'-
Geodesy
'^
Institute of Geodesy, Photogrammetry and Cartogra^y,.
Ohio State U. Refsearch Foundation, Columbus. ij
APPUCATION C»=1 DOUBLE FOURIER SERIES TO "
CC»«VriNG GRAJVITY ANOMALIES AND OTHER ;
GRAVIMETRICAL QUANTITIES AT HIGHER ELEVA-
TIONS FROM SURFACE GRAVITY ANOMAUES, by
Chuji Tsuboi. Reit. no. 2 on Contract AF 19(604)1963.
Oct 59, 2lp. Technical paper no. (7l6)-7; AFCRC-TN-
59-624; AD-230W8.
Order from LC mi$2.70, ph$4.80 PB 152 799
The double Fouridr series method was developed for
computing gravltylanomalies at higher elevations,
starting from glvan surface gravity anomalies. As an
example of its application, the method was used to
deduce gravity anomalies at an elevation of 15.9 km
above a portion a( Sweden. (Author)
Institute of Geodesy, Photogrammetry and Cartography
Ohio State U. Research Foundation, Columbus.
APPLICATION OP aiJJH'-AND OTHER SIMILAR
FUNCTIONS TO tCH^PUTING GRAVITY ANOMAUES
AT HIGHER ELEVATIONS. STARTING FROM GIVEN
SURFACE GRAVxhr ANOMALIES, by ChuJi Tsuboi.
Rept. no. 3 on CoiitraCT AF 19(604)1963. Oct 59, 22p.
Technical paper ii>. (716)-8; AFCRC-TN-59-625;
AD- 230 242.
Order from LC i4$2.70. ph$4.80 PB 152 800
The functions a'j{^ and (^^ *) were used for computing
gravity anomaliealat higher elevations, starting from
given values of siirface gravity anopialies. These rep-
resent 2 different I interpolation methods for evaluating
gravity aaomalieg| between given values. Also a hnear
interpolation metliod was tried. Gravity anomaly dis-
tributions at an efcvation of 46.7 km above the profile
no. 17 of Vening Meinesz across the East Indies as
deduced by the thi ee methods agree within several
milligals. (Autho^)
Geography
California U.
THE GEOGRAPHY
HONDURAS, by
tract Nonr- 222(1
Order from LC
^rkeley.
OF THE SAVANNAS OF INTERIOR
(^rl L. Johannessen. Rept. on Con-
1959. 293p. 210 refs; AD-231 473.
ijll. 10, ph$45.60 PB 152 892
)
nri
California U.
HISTORICAL
SOUTHWEST
Street. Rept. on
205 refs; AD-231
Order from LC
I erkeley.
EC )NOMIC GEOGRAPHY OF THE
PEIIINSULA OF HAITI, by John M.
i)niract Nonr- 222(11). 1960. 486p.
450.
nii$ll. 10. ph$74. 10 PB 152 893
282
Oceonography
Lament Geological Observatory. Palisades. N. Y.
UNDERWATER PHOTOGRAPHY AND CORE SAMP-
LING ON PLANTAGENET BANK, by John Ewlng and
Archie Roberts. Rept. on Contract NOb8r-64547 and
Technical rept. no. 1 on Contract Nonr-266(65).
Jan 60, 30p. CU- 1-60- Nonr 266(65); AD-234 110.
Order frtjm LC ml$2. 70, phK 80 PB 152 9Q(
Three series at underwater photographs and 4 core
samples were taken on the southwestern slope of
Plantagent Bank between^the crest and the 500-fathoni
contour, in the close neighborhood of 31° 57'N and65°
13'W. The Lamont multiple-shot model camera was
used. The light source was located about 5 ft above the
bottom and the camera about 8 ft. At this distance the
camera's field of view is an area about 6 ft x 4 ft.
The photographs are mounted so that the light source
is at the bottom. The ewing piston corer was used
with a 20-ft sampling tube. 1400 lbs in weight, with*
free fall of 10 ft. With this amount of weight and free
fall, this apparatus is capable of Uking a core as long
as 70-80 ft in normal ocean sediments. The longest
core obtained in this series was about 11 ft which give*
an indication of the type of bottom found on the bank.
(Author)
Marine Lab., U. of Miami, Coral Gables , Fla.
OCEANOGRAPHIC SURVEY OF THE TONGUE OP
THE OCEAN, VOLUME 1, by F. F. Koczy, F. Chew
and others . Technical rept. for 6 Aug- 26 Sep 58 on
Operation TOTO, Contract N 1 40(1 22)656 1 7B. 26 Sep M,
I69p. ML-2112.
Order from LC mi$7.80. phJ25.80 PB 153 625
This report released for sale to the public 18 Jan 61.
The TOTO is a "graben-like'^enrbayment on the Gre«
Bahama Bank. It is connected'with the Atlantic Ocean by
the northern entrance and by Northeast Providence
Channel. The slopes of the edge are rather steep, in
the upper 100-200 fathoms , and consist primarily of
coral rock . From about 200 fathoms to the deeper pan.
the slope is nx>re gentle and consists of calcareous
ooze: foraminifera , pteropods , and oolites; the bocton
is completely flat. The depth of the TOTO increases
gently from 700 fathoms at the Cul-de-Sac in the south-
em end to 1500 fathoms at the northern entrance. It IJ
suspected that sediment moves slowly in the TOTO to-
ward the Atlantic Ocean. Sedimentary material is sup-
plied primarily by restricted slides off the edge. Pre-
cipiution in this region reaches two maxima, in June
and in October; showers can be rather heavy during the
summer months . Winds are gentle during the summer,
but heavy winds can be expected from October to Marcli
The water masses of the TOTO are an integral pan of
the waters in the Atlantic Ocean east of the lahama
Islands. The surface water, to about 150 m.. is mark-
edly influenced by the water from the surrounding banto-
Submarine daylight measurements in the surface water
show the same clarity as is found in tropical waters of
oceanic origin. The general circulation in the TOT0i»
very sluggish and primarily wind-driven. Internal
waves and seiches have been detected and were most
pronounced during the winter time. Currents , measural
IB the TOTO, are from 0,2 k. loO.l k. /Dn the edge,
the maximum current is ().5 k. In the bights and creeks
the tidal current may reach 5 k. The TOTO can be char
•cterized as a small model-ocean. (Author)
Narragansen Marine Lab. , U. of Rhode Island,
Kingston.
MOLOGICAL PRODUCTIVITY PROJECT, by David M
Pratt. Annual progress rept. for 1 Jan-31 Dec 59 on
Contraa Nonr -396(03). Jan 60, 5p. Ref. no. 60-1;
AD- 235 398.
Order from LCmi$ 1.80, ^1.80 PB 152 907
Brief summaries of published work and current
progress in research on phytoplankton, epibenthos,
baaeria- plankton relationships, and special studies
of off-shore plankton. (See also PB 145 209)
Washington U. , Seattle.
COBB SEAMOUNT. A DEEP-SEA FEATURE OFF
THE WASHINGTON COAST, by Thomas F. Budinger
and Betty J. Enbysk. Technical rept. no. 60 on Con-
tracts Nonr-477(10) and Nonr-477(01). Mar 60. 89p.
117 refs. Ref. no. 59-6; AD-238 479.
Order from LC mi$4. 80. ph$13. 80 PB 148 426
Cobb Seamount is a deep-sea feature located 270 nauti-
cal miles west of Gray's Harbor, Washington
(46046. 4' N and 130P48. 8' W). The topography, geol-
rogy, biology, and hydrography of the mountain were
investigated by the research vessel. M. V. Brown Bear.
.^,200 mi of soundings. 34 bottom samples, 25 hydro-
graphic stations, and other observations were taken.
Tbia submarine mountain rises from a base at 1, 500
fathoms below the sea surface to within 18. 5 fathoms
of the surface and comprises an area of 240 square
naut mi. The average slopes of 12^ are indented by
lliree prominent terraces at 500, 100, and 45 fathoms.
Prom Che 45 -fathom terrace rises a l60-ft pinnacle
apparently composed of shells and characterized by a
flat top and 45° slopes. The hydrographic observations
Indicate that there are po anomalies in the water struc-
ture of current pattern which might be attributed to the
Influence of the mountain. A rotary current with both
■emidiurnal and inertial constituents was observed.
The geostrophic flow during four periods of observa-
tloos was 0. 1 knot setting southeast. The water mass
la dominantly Subarctic water mixed with 10-20 per-
cent Equatorial Pacific water. (Author)
Physics of the Atmosphere
Advanced Electronics Center, General Electric Co. ,
Ithaca, N. Y.
A DETAILED DESIGN STUDY FOR A TOPSIDE
lOKDSPHERIC SOUNDER. VOLUME I, by Leonard C.
Humphrey. Scientific rept. no. 1 on Contract
AF 19(604)7221, 15 Sep 60. 199p. 40 refs. AFCRL TN-
60-1125(0
Order from LC miW. 7p, ph$30. 30 PB 153 050
\
This report describes the investigations for the design
of a satellite- borne ionospheric sourKJer. The report is
divided in two volumes; the first describes the scientific
considerations which influence the measurements, the
various requirements of the equipment, their feasi-
oility. configuration in an instrumented satellite pai k-
age, and ground support complex requirements.
(Author)
Antenna Lab. , Ohio State U. Research Foundation,
Columbus, Ohio.
PRELIMINARY ANALYSIS OF METHODS FOR TEM-
PERATURE DETERMINATION AT ALTITUDES
ABOVE 120,000 FEET, by T. G. Hame, W. H. Peake
and others. Rept. on Temperature Measurements at
Altitudes above 120, 000 ft. Contract DA 36-039-8C-
84516. 25 May 60. 49p. 10 refs. Rept. 973-2;
AD-242 206.
Order from LC mi$3. 30. ph$7. 80 PB 152 669
An analysis is given of the feasibility of a variety of
methods for temperature determination at altitudes
above 120, (X)0 ft. It is concluded that several of these
methods (e. g. . rocket -grenade, falling sphere, pres-
sure instrumentation) are developed to the point where
they can yield accuracies of t5°K with an altitude reso-
lution that is typically of the or^r of 1 km, at altitudes
up to about 275, 000 ft. Between this altitude and about
400, OCX) ft, present methods (mostly based on pressure
measurements) are not satisfactory. Above 400, 000 ft.
proposed methods based on determination of kinetic
temperatures in the ionosphere are discussed, but
these methods are fully verified experimentally.
(Author)
Electrical Engineering Research Lab. , U. of Texas,
Austin.
SINGLE AND DUAL CAVITY MEASUREMENTS OF
GROUND AND AIRBORNE INDEX OF REFRACTION
FLUCTUATIONS AT 400 MCPS. by G. B. Walker.
Rept. on Contract AF 19(604)2249. 15 Sep 60, 45p.
6 refs. Rept. no. 6-38; ERD TN-60-975; AD-245 509.
Order from LC mi$3.30, ph$7.80 PB 152 951
This report gives the results of measurements of
variations in the index of refraction of the atmosphere
nuide at this Laboratory in February, April, and May
1960. Data were obtained by use of 403 mcps refrac-
tometers. These data include difference index of re-
fraction measurements as a function of cavity spacing,
single and dual cavity index of refraction as a function
of height on a 280 ft. tower, and single and dual cavity
index of refraction as a function of altitude on a light
aircraft. All data were recorded on an Ampex
FR-IOOA Magnetic-Tape recorder and a Brush re-
corder type BL-202. These data were later tran-
scribed on an Ampex 306-2 Magnetic Tape recorder to
perform power density spectra analysis. These power
density spectra are incliided. (A\ithor)
Ionosphere Research Lab. , Pennsylvania State U. ,
University E*ark.
THE EFFECTIVE RECOMBINATION COEFFICIENT
OF AN IONOSPHERE CONTAINING A MIXTURE OF
IONS, by S. A. Bowhill. Scientific rept. no. 141 on
Ionospheric Research, Contract DA 36-061 -ORD- 577.
15 Nov 60, 27p. 16 refs. AD-245 060.
Order from LC mi$2.70, ph$4.80 PB 152 697
A
283
The effective recombination coefficient of the normal
icnosphere may ^ evaluated from the nocturnal varia-
tion of ionization density; from the rate of change erf
ionization during a solar eclipse; or from the "slug-
gishness" of the ionization, as exhibited in its diurnal
.variation. Thes^ three methods are found to give
widely different tesults, at any one height in the iono-
sphere. It is sh^n that an ionoephere containing a
mixture of severjal ion species with different recombi-
nation coefficients^ gives adequate explanation of these
discrepancies, formulae are presented for the effec-'
tive recombinati^ coefficient for this model. A con-
sideration of existing knowledge of ionization processef
in the E-regpon $ugge8ts that the ions concerned may
be those of molecular oxygen and nitric oxide; the
laner being produced by ion-atom interchange between
nitrogen molecules and atomic oxygen ions. The
nocturnal E-reglbn should then consist primarily of
NO* ions. (Authfir)
Ionosphere Resbarch Lab. , Pennsylvania State U. ,
University Part(.
LOW FREQUENCY RADIO STUDIES OF APPARENT
IONOSPHERIC MOTIONS, by G. S. Sales. Scientific
rept. no. 131 on i Ionospheric Research, Contract AF
19(604)4563. 1 Abr 60, 21 Ip. 59 refs. AFCRC TN-
60-4«3; AD-245 661.
Order from LC iiu$9. 60. phJ33. 30 PB 152 6%
An investigation pf ionospheric motions using low fre-
quency radio wavjes is described. This work presents
the experimental' results of this program and the de-
velopment of a tfieory for the explanation of these ob-
servations. The jexperimental apparatus and the method
'of analysis used to obtain values of drift and random
velocities are discussed in detail. A study is made of
the sampling errprs associated with the computation of
correlation coefficients and this work is then applied to
specific problem^ associated with the analysis of mo-
tions In the ionosphere. The results are presented and
estimates of the Accuracy are given for the quantities
analyzed. Finally, a theory developed in terms of
hydrodyiuunic waves in the ionosphere, to explain the
observations of t^iis work and the work of other investi-
gators using medium frequency radio waves. (Author)
Naval Researcl^ Lab. , Washington, D. C
THE MEASUREMENT OF WATER-VAPOR DISTRI-
BUTION IN THE , STRATOSPHERE, by H. J. Masten-
brook and J. E. finger. 16 Nov 60, 38p. 18 refs. NRL
rept. 5551.
Order from LC riiJS. CO, ph$6. 30 PB 150 618
The development
integrated with a
: of a dew-point radiosonde has been
series of balloon flights extending
over a period of nwo years. This endeavor has sought
to establish the reliability of the instrument by an ap-
praisal of its performance and the consistency of the
flight data obtained. The instrument incorporates the
optical -electroni(J -thermal servo loop commonly used
in automatic dew-point instruments and operates to
control the tempep-ature at a mirror surface such that
a water or ice deposit is in equilibrium with the vapor
in the air being aimpled. The temperature uf the
mirror is measuied and telemetered to give the frost
point. Special atti^ntion has been given to problems
related to contamlination of the sample by extraneous
moisture and to condensate characteristics. The dau
from a total of eleven flights are included. The flight
data have been critically evaluated to point up problea
areas in the instrument and flight procedures and to
determine what flights have yielded valid data concern-
ing the water distribution in the stratosphere.
Upper Air Research Lab. . U. of Utah. Salt Lake
City.
CHARACTERISTICS OF LOW FREQUENCY ANTEN-
NAS FOR ROCKET APPLICATIONS, by Gayle Fred
Miner. Scientific rept. no. 4 on Contract
AF 19(604)2227 12 Aug 60. 58p. 15 refs. AFCRL-
TN-60-657; AD-244 708.
Order from LC mi$3. 60, ph$9. 30 PB 152 623
An investigation was conducted on rocket-borne dipole
antennas used for ionospheric research in the frequency
range of 3 to 12 mc. The description of a test facility
for measuring the impedance and field intensity of bal-
anced dipole antennas using a ground plane is given.
The facility allows the effect of the rocket body on an-
tenna performance to be included in the antenna meas-
urements. Results are given of an initial investigation
to determine the effect of dipole length on the* antenna
input impedance. Methods are discussed for the elec-
trical lengthening of a dipole antenna and for the elimi-
nation of the capacitive reactance component of the
impedance of a dipole of electrical length less than
Xj^- Experimental impedance data are presented for
the following three methods: (1) capacitive top -loading,
(2) base series inductance tuning, and (3) distributive
inductive loading. Field intensity measurements on a
base series inductance tuned antenna and a distributed
inductance loaded antenna at 7. 2 mc are given. The
construction details of a distributively loaded antenna
are given, including the use of ferrite materials to
allow an antenna to be tunedito a prescribed frequenqr.
The description and results of a saturation test per-
formed on the ferrite tuning core material are given.
(Author)
ENGINEERING
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
ESTlMATIhiC SOIL MOISTURE AND TRACTION-
ABILITY CONDITIONS FOR STRATEGIC PLANNING
PART I. GENERAL METHOD. PART 2. APPLICA-
TION AND INTERPRETATIONS, by C. W. Thomthwaitt
J. R. Mather and others. Mar 58, 62p. 19 refs.
Air Force Surveys in Geophysics no. 94; AFCRC-TN-
58-201; AD- 146 789.
Order from LC mi$3. 90. ph$10. 80 PB 153 884
This report released for sale to the public 19 Jan 61.
Soil moisture content is the nwst important factor in
determining bearing capacity, shearing strength, and
stickiness of soils; or, in other words, the traction-
ability of a soil. Knowledge of the balance between in-
coming precipitation and outgoing evapotranspiration
and surface and subsurface runoff provides infonnatitii
on the moisture content in the soil. A method is pre-
sented for computing soil moisture conditions by
284
means of a simple bookkeeping procedure utilizing
i^adily available climatic data. It is thus possible to
obtain detailed information on the water balance and
its distribution in the ground at any time in a desired
area on either a monthly or a daily basis. From a dis-
cussion of the factors affecting soil tractionability and
the influence of moisture on tractionability, it is pos-
■lUe to define different classes of the state of the
iround in physical terms, estimate their probability of
occurrence, prepare maps ctf monthly average soil
moisture conditions, and correlate these conditions
trith tractionability requirements. (Author)
Battelle Memorial Inst. , Columbus, Ohio.
CORROSION OF METALS IN SEA WATER, by
Frederick W. Fink. Rept. on Contract no. 14-01-
001-182. Dec 60, 62p. 152 refs. Office of Saline Water
Research and Development Progress rept. no. 46.
Order from OTS$ 1.75 PB 171 344
Contents:
Corrosivity of sea water: the nature of corrosion; cor-
rosive ions in sea water; conductance and salt con-
centration; oxygen and temperature; crevice and pit-
ting attack; velocity; heat transfer; stress; galvanic
couples
Problerns associated with heating sea water
Performance of metals in saline v>ater steel; cast iron;
wrought iron; alJrninum and its alloys; copper;
brasses and bronzes; cupro nickels; Monel; stainless
steels; titanium; special alloys.
Aeronautical Engineering
Aeroelastic and Structures Research Lab. , Mass.
hit. d Tech. . Cambridge.
AN EXPERIMENTAL INVESTIGATION OF STALL
FLUTTER OF A MODEL HELICOPTER ROTOR IN
FORWARD FLIGHT, by Norman D Ham. Rept. on
Cootract Nonr- 1841(58). 15 Mar 60, 47p. 8 refs.
Technical rept. 86-1; AD-236 709.
Order from LC mi$3. 30, ph|7. 80 PB 147 554
Stall flutter of a model helicopter rotor in simulated
forward flight was investigated. Stall flutter was found
to occur in all forwar(9 flight cases involving appreciable
blade stall, and consisted almost entirely of blade
motion in the torsional rnode. Stall flutter amplitude
was found to be dependent on such parameters as blade
chordwise C. G. position, blade torsional damping,
Uade torsional frequency, and the degree of stall occur-
ring over the rotor disc. The results of the study indi-
cate that more information Is required regarding the
tm'tlonal aerodyrtamic'dampingof stalled rotating blades
(Author)
I
AvcoCorp., Nashvi%, Tenn.
DESIGN, DEVELOPMENT AND FABRICATION OF A
UGHT WEIGHT AIRFRAME. Monthly progress rept.
■0. 5, Sep 60, on Contract DA 33- 008 -ORD- 1968.
(I960] 12p. AD-245 70;
Order from LC mi$2.'(0, ph$3. 30 PB 152 %7
In the explosive forming development, four experimen-
tal charges have been tried on explosive forining the
skins . These have proven unsuccessful due to a poor
weld at the seam of the cone shaped blank. A 7075 alu-
minum alloy material has been temporarily substituted
for X2020 material for explosive forming development
in determming placement of charge and tool tryout due
to the unavailability of X2020 material in small quanti-
ties . After establishing the basic parameters required
for explosive forming, final tests will be conducted
using X2020 material. Deuil parts fabrication is in
progress . All detail parts required for Unit No. 1 have
been completed with the exception of the formed skins.
(Author) (See also PB 152 343)
Bell Aircraft Corp. , Buffalo. N. Y.
SUPERSONIC AERC«LASTIC EFFECTS ON STATIC
STABILITY AND CONTROL. PART III. AEROELAS-
TIC INTERACTION, by Vincent W. Donato. Rept. on
Contracts AF 33(616)3577 and AF 33(616)6067. July 60,
371 p. 53 refs. WADC Technical rept. 58-95, Part III.
Order from OTS $5.00 PB 171 192
Static aeroelastic interaction equations are derived in
matrix form for wing-aileron lifting surfaces, consid-
ering the wing and aileron being independently flexible,
and the wing and aileron as a single structural assem-
blage. The equations are stated in general form so as
to accept Inputs in the form of aerodynamic and struc-
tural deformation influence coefficient matrices.
Closed form and series solutions for the equations are
presented. From these solutions expressions are de-
veloped for the flexible to rigid ratios of lifting pres-
sure, span loadings, and aerodynamic center locations.
Matrix expressions for the flexible to rigid ratio of
pertinent derivatives demonstrate the effects erf flexi-
bility on stability and control. Inertia effects are also
included. Sample problems illustrate the use of the
derived equations in an aeroelastic analysis. (Aishor)
Crysler Corp. , Detroit, Mich.
MODEL DESIGNATION VZ-6-CH SERIAL NO. 58-
5506. Final engineering rept. on Chrysler Aerial Re-
search Vehicle, Contract DA 44- 177 -tc -448.
29 Feb 60, 202p. 6 refs. AD-234 515.
Order from LC mi$9. 30, ph$31. 80 PB 153 624
This report released for sale to the public 10 Jan 61.
This report covers the design, fabrication, and teth-
ered flight testing of a two duct, vertical take-off
aerial research vehicle. Preliminary design work in-
cluded small scale wind tunnel testing, fuU scale static
test bed experimentation, stability analysis, and an
analog computer flight simulation. The ducted pro-
pellers of the. flight research vehicle were 8-1/2 feet
in diameter; the vehicle was powered by a 360 hp pis-
ton engine. Flight control was achieved by a system of
hinged vanes; the propeller blades were of a fixed
pitch, non -articulating design. Results of tethered
flight tests indicate that thrust was adequate to hover a
vehicle of 2200 pounds gross weight. Control was mar-
ginal about all three axes; control on the ground at the
moment of lift-off was inadequate, indicating that fur-
ther development work on the control system is re-
quired. (Author)
285
Curti 88 -Wright Corp. , Santa Barbara, Calif.
HYPERSONIC FRBE FLIGHT RESEARCH. PART II:
INVESTIGATIONS I OF HEAT TRANSFER AND AERO-
DYNAMIC STABIlilTY, by O. R. Burggraf. Rept. on
Contract A F 33(616)5104. July 60, 93p. 20ref8.
WADD Technical tiept. 59-708, Part 11.
Order from OTS $2. 25 PB 171 195
A series of eight ftee flight experiments have been
conduaed with iheJHTV-l Hypersonic Test Vehicle for
the purpose of stu^lying the aerodynamic heat transfer
characteristics a( blunted cones as well as the flight
dynamic charaaeijistics of the vehicle itself. The
vehicle, instrumentation system, and typical flight
conditions are disiussed briefly. Results of the flight
tests are discussejd, both with regard to heat transfer
and aerodynamic dharacteristics and with regard to the
limiudons of the nstrumentation system. (Author)
(See also PB 171 IN)
Directorate of P ight and All -Weather Testing,
W right -Patterso^ AFB, Ohio.
THE EFFECT OH FROST ON THE TAKE-OFF PER-
FORMANCE OF F-86 AND B-47 AIRCRAFT, by
Jerry Hanjian. Miy 56, 24p. WADC-TN-56-187.
Order from LC mj$2.70, ph$4.80 PB 153 630
This report released for sale to the public 12 Jan 61 .
This repon presents quantitative results of take-off
performance flighj tests on F-86 and B-47 model air-
craft with frost ort the lifting surfaces . No significant
change was found In the take-off performance of these
aircraft from the point of brake release through initial
climb under the variables of frost intensity and gross
weights tested duijing the winter season of 1955-1956.
Information of a qijalitative nature is also presented for
an RB-66A and B-12B aircraft. (Author)
Electronic Systefis Lab. , Mass. Inst, of Tech.,
Cambridge.
COMPUTERS FOR AIRCRAFT SIMULATION, by Mark
E. Connelly. Repi. on Contraas N5ori -07895 and
N61339-45. 15 Dei; 59, 115p. 124 refs.
Rept. 7591-R-2.
Order from LCmi$6.00, ph$18.30 PB 152 885
This report is thejconcluding work on a one-year study
of the equations ofj maion and the computing techniques
used in the aerodyhamics computer seaion of Opera-
tional Flight Trailers. A review of the characteristics
of basic 60 cpe, 4JX) cps, and DC analog computing
techniques is preinted with emphasis on the relative
applicability of th^se techniques to the unique require-
ments of the OFT problem. It is concluded that 400 cps
techniques would tive more than acceptable perform-
ance and would ofier substantial advantages with re-
spect to cost, 8iz«, maintenance and power consumed.
In conclusion, several suggestions are made concerning
OFT acceptance procedures, the matching of the OFT
to the actual airciiaft. and standardization. (Author)
cijaft.
Foster. John J. litfg. Co. , Costa Mesa, Calif.
STRESSKIN PROCtRAM (RESISTANCE WELDED
STAINLESS STEEjL HONEYCOMB SANDWICH PANEL)
by Plaul E. Harrlsbn and L. F. Elliott. Final rept. for
25 Apr 58-25 Sep 59 on Contract Noa(s) 58-659-c
24 Dec 59, 125p. 4 refs.
Order fr«n LC ml$6. 30, ph$19. 80 PB 149 718
Manufacturing research, development, and pilot- line
production of welded steel honeycomb core material and
composite sandwich panel, referred to In this report as
STKESSKIN, a trade name for an all- welded honey-
comb sandwich panel. Development at machinery and
equipment for producing STRESSKIN; specifically, face
sheet to core ribbon flange welding, node welding,
welding controls, node welding electrode tips, face
sheet welder elearode strips, flanged core ribbon
forming. Inspection at weld, cleaning stainless steel
panels, drying of panels, and stress analysis d paneli
All resistance welded honeycomb sandwich panels can
be manufactured with high quality and in quantity, at a
relatively low cost.
I . ■
McDonnell Aircraft Corp. , St. Louis, Mo.
UNLOADED ROTOR COMPOUND HELICOPTER.
UGHT VrOL TRANSPORT AIRCRAFT STUDY. Rept.
on Contraa DA 44-177-tc-588. 1 Feb 60. 136p. 73ref«.
Rept. no. 7064; AD- 232 716.
Order from LC mi$6.90, ph$21 .30 PB 149 666
This report gives the results of a design study c4 a
VTOL transport aircraft with a VTOL pay load of ap-
proximately two tons at 6000 feet 95^ out of ground
effect hovering, and with radii of action from 200 to 500
nautical miles. The study is centered around the XV-1
unloaded rotor type of VTOL aircraft which was exteti-
sively flight -tested by McDonnell and Air Force pilots
during 1955-57. Recommendations are made on light
VTOL transport requirements. A Justification of the
seleaion for unloaded rotor design parameters is given
A spectrum analysis for a gross weight range of 15,000
to 60, 000 pounds shows the effects of size on payload
and radius of of)eration. Also shown are the effects of
take-off atmospheric design requirements. The recom-
mended Army light VTOL transport of the XV-1 type
has about 30, 000 pounds design gross weight and can be
powered by any of three different gas turbines;
T58-GE-8, T55-L-7, or T64-GE-2. Given are dimen-
sional data, description of systems, performance,
flying qualities, structural approach, dynamics, and
weights. Some operational variables are treated.
Maintenance and operating costs are given for the
recommended aircraft. (Author)
Minnesota U. . Minneapolis.
SUPERSONIC SPEED FLUTTER ANALYSIS OF CIR-
CULAR PANELS WITH EDGES ELASTICALLY RE-
STRAINED AGAINST ROTA JION. by L. E. Goodman
and Jasti Venkata Raftayya. Rept. for Jan- Dec 59 on
Metallic Materials, Contract AF 33(616)6828. Aug 60,
85p. 22 refs. WADD Technical rept. 60-309.
Order from OTS $2. 25 PB 171 199
The flutter problem is formulated. In terms of small-
deflection plate theory, for a flat circular panel with
edges elastically restrained against rotation. The panel
is taken to be subjected to Isotropic tension or com-
pression in its middle plane. Linear piston theory is
used to predict the aerodynamic load on the vibrating
panel due to a supersonic compressible flow passing
its ijpper surface. Results of the analysis predict panel
thickness necessary to prevent flutter as a function of
air speed, elevation, and degree of edge fixity. Inves-
diitlons of aerodynainlc and structural damping effects
ud the influeiKe of ir^d- plane load are included.
(Author)
286
Northrop Corp. , Hawthorne, Calif.
EFFECTS OF TEMPERATURE-TIME-STRESS HIS-
TORIES ON THE MECHANICAL PROPERTIES OF
AIRCRAFT STRUCTURAL METALLIC MATERIALS.
PART II. STRESSED EXPOSURE OF 7075 -T6, by
C. D. Brownfleld and D. M. Badger. Rept. for May 58
Sep 59 on Materials Analysis and Evaluation Tech-
■iques, Contract AF 33(616)5769, continuation of Con-
tract AF 33(616)3028. Sep 60, 113p. 11 refs. NOR
60-16; WADC Technical i >pt. 56-585. Part II.
Order from OTS $2. 50 PB 171 328
A study has been made on tt>° problem of predicting
strength of a hardened metai alloy after subjection to
variable thermal and stress environments severe
enough to cause permanent loss of properties. Meth-
ods have been developied for predicting tensile ulti-
mate, tensile yield, and compressive yield strengths
of 7075-T6 aluminum alloy after single or multiple ex-
posure to various temperature and stress exposure
oooditlons. Test results have been used to establish
Ike validity of the Carton -Miller exposure parameter
to correlate residual strength after stressed and un-
atressed single multiple exposures. (Author) (See also
FB 131 520)
Princeton U., N. J.
AN EXPERIMENTAL INVESTIGATION OF HELICOP-
TER STABILITY CHARACTERISTICS NEAR HOVER-
ING FLIGHT USING A DYNAMICALLY SIMILAR
MODEL, by Robert M. Bennett and Howard C. Cur-
tlss. Jr. Rept. on ALART Program, Contraas DA 44-
177-tc-524andNonr-l$58(ll). July 60, 103p. 12 refs.
Aeronautical Engineering rept. no. 517.
Order from LC nfU$5.70, ph$16.80 PB 152 831
TWi report presents the results of experiments con-
ducted with a dynamically similar scale model of a
helicopter near hovering flight, to determine the quasi -
static stability derivatives in terms of fuselage varia-
bles. TTie stick-fixed transient response In two degrees
of freedom, horizontal velocity and fuselage pitch
Mgle. was measured. The apparatus consisted erf a
carriage -track system constraining the model to mo-
tion* in a vertical plane, and a positioning servomecha-
nlsm slaving the carriage to the horizontal motion of
the model. Longitudinal forces and pitching moment
■ere measured for small velocity Increments auout
hovering with the hovering trim control settings and
ftaelage attitude to determine static stability. Methods
far determining the significant stability derivatives
near hovering, the damtping In pitch (^/n/.^./) and the
»eIoclty stability ('"rt^ix ) from the dynamic data are
derived, applied and compared. A complete discussion
of the model and testing techniques used in the expert -
nents la included, as well as experience with down-
•Mh recirculation and pitch-lag oscillations encoun-
tered during the tests. (Author)
Princeton U. , N. J.
REQUIRED LATERAL HANDLING QUALITIES FOR
HELICOPTERS IN LOW -SPEED INSTRUMENT
PLIGHT, by Joseph H. Goldberg and Robert C.
Gangwlsh. Rept. of Contract DA 44- 1 77 -TC -524.
Feb 60, 42p. II refs. Aeronautical Engineering rept.
no. 496.
Order from LC miJ3. 30, ph$7. 80 PB 152 625
The reported investigation was conducted In order to
establish the requirements for, and factors influenc-
ing, the lateral handling qualities of helicopters. Fly-
ing qualities were studied using a number of appropri-
ate pilot subjects in a test program on a variable su-
blllty helicopter. Dynamic lateral characteristics
were varied over a broad range to define bases for
suitable handling qualities. Data on each configuration
were obtained in the form of pilot commentary and re-
lated helicopter stability and control characteristics.
Both visual and Instrument flight problems were con-
sidered, with test conditions limited to low -speed
level flight. Over forty different stability configura-
tions were tested by experienced helicopter test pilots.
A latter phase of the program was cotxlucted in a more
intensive manner by a single pilot after It was estab-
lished that reasonable consistency of results existed
within the pilot group. Testing iivpluded the recording
of detailed commentary as well as an over -all evalu-
ation represented by a numerical rating. Analysis of
test results indicated a number of areas of importance
in helicopter lateral handling characteristics. The
principal factors were found to be the damping of the
[Xitch roll oscillatory mode, spiral damping, and the
nature of control applications In turns. (Author)
Propulsion Lab. , Wright Air Development Center,
Wright -Patter son AFB, Ohio.
HOT GAS SURFACE EROSION STUDIES, by
W. H. Mitchell and J. N. Wherry. Rept. for Jan -
Apr 60. Aug 60, 22p. WADD Technical note 60-183;
AD- 241 779.
Order from LC mi$2. 70. ph$4. 80 PB 153 629
This report released for sale to the public 16 Jan 61.
The effect of Jet exhaust impingement on several sur-
faces was observed using a YJ85-GE-3 turbojet engine
for testing. The surfaces tested were sod. concrete, a
sand-dirt-gravel mixture, and sod covered with landing
mats. The velocities and temperatures of the exhaust
gas at the Impingement point were In the order of 425
to 1800 ft/sec and 450 to 1300°F with the nozzle height
ranging from 3 to 6 feet. The results Indicate that un-
prepared surfaces will not be usable for the range
tested. Sod covered with landing mats could be used on
a limited basis, and concrete probably could be used
for an indefinite period. (Author)
Wichita U. , Kansas.
SHROUCCD PROPELLER INVESTIGATIONS: SHROUD
AND CENTERBODY PRESSURE DISTRIBUTIONS OF A
SHROUECD PROPELLER WITH A 10-BLADED ROTOR
EXIT STATORS AND LONG CHORD SHROUD, by Ver-
non O. Hoehne. Rept. on Contract Nonr-201(01). Jan 60,
55p. 1 ref. Engineering rept. no. 213-10; AD-231 468.
Order from LC mi$3.60, ph$9. 30 PB 152 898
287
/
The static pressiire distribution on the surface of the
shroud and cent^body of a shrouded propeller model
was measured in the wind tunnel. The shrouded propel
ier model emboc|ied 10 propeller blades and 15 exit
stator vanes and was equipped with a centerbody or hub
having a hub-tip ratio ctf 0. 3. The model incorporated
3 interchangeably shroud inlets: 2 designed for static
and low speed operation, and one for high speed flight.
Only one of the static shroud inlets was tested during
this investigatioil. Pressure distributions were obtained
for a range of enernal advance ratios from approxi-
mately 0. 20 thrctigh 1 . 50, at angles of anack from
zero to 90° and ^th several propeller blade pitch
angles. Results jare presented as pressure coefficients
plotted against n^odel axial location in per cent of chord
at various consuMit values of advance ratio. (Author)
(See also PB 149 484)
Electrical
and Electronic Engineering
Admiral Corp. , Chicago, 111.
EVALUATION A^ DEVELOPMENT OF MIL-C- 14157
CAPACITORS FOR NUCLEAR RADIATION ENVIRON-
MENT, by E. R. Pfaff. Scientific rept. no. 5 on Con-
tract NObsr- 7761 2. (1960) 43p. 5 refs.
Order from LC nii$3.30, ph$7.80
PB 153 096
All capacitor unll s impregnated with uninhibited FS-5
and silicone gel c ielectrlc impregnant and the capaci-
tors with FC-43 (lielearic fluid constituting the gamma
group failed in le^s than 63 hours. Irradiated units
with Etherm "A" idielectric fluid and 4% Tertiary Butyl
Anthraquinone ex|ubited a slight improvement in the
seventy-five per pent failure point over the irradiated
standard 1% inhibited units. The control group units
with additional intiibitor had an appreciable improve-
ment in the severiy-five per cent failure point over the
1% inhibited units. The seventy-five per cent failure
point of the irradiated cross- linked polystyrene solid
impregnant capaditors occurred more rapidly than the
standard units. Post irradiation tests of Mylar indicate
that the Mylar is being damaged by hydrolytic degrada-
tion rather than oamma damage. This type of damage
can be improved py isocyanate treatment of Mylar.
Dielectric propenties of Monoisopropylbiphenyl dielec-
tric fluid have been improved by filtration. (Author)
Aero Geo Astro Corp. , Alexandria, Va.
A BROAD-BAND OMNIDIRECTIONAL ANTENNA
FEED FOR DUAL POLARIZATION, by D. M. Bowie
and B. R. Gross.
AF 19(604)5481.
60-1106; AO-215
Order from LC nr i$2. 70, ph$4. 80
Scientific rept. no. 2 on Contract
!6 Sep 60, 30p. 2 refs. AFCRL-TN-
194.
PB 152 728
A broad -band antenna feed suitable for low -silhouette
aircraft installation offering omnidirectional coverage
in azimuth separaltely for horizontal and vertical polar-
ization has been developed and tested, using an X-band
prototype structure. The near-field radiation charac-
teristics of the 3t|-ucture make it suitable either as a
radiator utilizing ja small external structure or as a
feed for radial su^-face-wave or reflective structures.
The design, whici was proposed earlier by Plummer
and others, provides for concentric arrangement of two
coaxial transmission lines supporting the modes usuiU)
used in separate feeds for the two polarizations. En-
ergy from the inner coaxial line, supporting the TEM
mode, and the outer line, designed to transmit the
TEoi coaxial mode, are transformed by means of a
toroidal splash plate and the ground plane into parallel
and perpendicularly polarized waves, respectively. A
mode -suppressor for use in the latter line has been de-
veloped, which effectively suppresses radial field coni-
ponents, thereby achieving separation of signals in tic
two transmission lines on the basis of polarization.
Radiation patterns for the feed in conjunction with a
circular ground plane of limited extent, with and with-
out a grounded dielectric layer are included. (Author)
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
OPTIMUM THRESHOLD FSK COMMUNICATION WTTH
DECISION REJECTION, by David Mtddleton. Apr 60,
6lp. 4 refs. AFCRC TR-60-137.
Order from LC ml$3.90, ph$10.80 PB 152 985
Optimum incoherent threshold detection of general FSK
signals in normal noise is examined, where the new
feature of decision rejection, as well as decision
acceptance, is used. Structure of the optimum thresh-
old system is given, and the error and rejection probi-
bilities associated with the Bayes risk are computed (ot
general signals and arbitrary baud lengths. It is shown,
in particular, that for the same error probabilities in
either state it is possible to have a smaller input sigml
level with rejection than without it, the rejection profai-
bilities being non zero, of course, with a consequent
reduction in information rate. Besides a detailed eiam-
ination of the binary rejection cases, the theory of the
multiple alternative deteaion process with decision re-
jection is also outlined. (Author)
Air Force Cambridge Research Labs. , Bedford,
THEORETICAL LIMITATIONS ON FREQUENCY AND
TIME DIVERSITY FOR FADING BINARY TRANS-
MISSIONS, byj. N. Pierce. July 60, 24p. 4 refs.
ERD TR-60-169; AD- 245 723.
Order from LC mi$2.70, ph$4.80 PB 152 984
It is theoretically possible to minimize the element
error rate in frequency-diversity or time-diversity
systems by proper chrtce of number of diversity
branches. The optimum number of branches is a func-
tion of both the total available SNR and the diversity-
combining method. This theoretical optimization hat
been carried out for two representative combining
methods. The results provide an upper bound on the
diversity improvement achievable with frequency or
lime diversity. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
OPTIMIZATION OF A STRIP LINE TRAVELING
WAVE LOOP DIRECTIONAL FILTER AS A BAND
REJECTION NETWORK, by Robert D. Standley.
1 July 60, 23p. 11 refs. USASRDL Technical
rept. 2133: AD- 242 485.
Order from LC mi$2.70, ph$4.80 PB 153 003
This report released for sale to the public 1 1 Jan 61.
288
All analysis of a strip line traveling wave Idop direc-
titUal filter is performed to optimize the device as a
band rejection filter. |A method for choosing the
optimum physical parameters is developed. Several
Illustrative examples are given to show that a consid-
erable difference exists between the optimum band
pass and optimum Iwnd rejection designs. A construc-
tion which does not require a solid dielectric base
material is suggested. (Author)
Bell Telephone l^bs.l, Inc., Whippany, N. J.
AN ULTRA-PRECISE STANDARD OF FREQUENCY, by
W. L. Smith. Interimtrept. no. 12, 10 July-9 Dec 59,
on Contract DA 36-039-sc-73078. 23 Dec 59, 37p.
Rept. no. 27480-K; AD-233 680.
Order from LC mi$3.00, ph$6.30 PB 149 722
This report includes {]) a discussion of the results to
date of a program to determine the effects of different
mounting arrangements on the acceleration coefficient
of frequency of 5-mc crystal units; (2) a discussion of
the mechanical and eleictrical design of two development
models for oscillators satellite application; and (3) a
description of the mechanical design proposed for the
final models of the satellite oscillator. Several crystal
units have been made \)^hich meet the requirements for
missile-borne apjplicatjons, using a three-point 90°
mounting with two points on the Z' axis. However, the
(tctors controlling the acceleration coefficient are not
nifflciently well known to assure reproducible results.
Two preliminary development models of the satellite
oscillator have been completed and tested for frequency
itsbility during vibration, shock, and static accelera-
tion. (Author) (See also PB 149 719)
Bell Telephone Labs. , Inc. , Whippany, N. J.
AN ULTRA-PRECISE STANDARD OF FREQUENCY,
bjfW. L. Smith. Interim rept. no. 13, 10 Dec 59-
9 Msr 60, on Contract DA 36-039 -sc -73078.
23 Mar 60, 28p. Rept. 'no. 27480-L; AD-238 443.
Order from LC mi$2. 70, ph$4. 80 PB 152 658
This report includes (1) a description of the mechanical
and electrical design of the final models of the satellite
oscillator; (2) a summary of the performance of these
oscillators during testing; and (3) the results of aging
tests on crystal units operating at temperatures below
SOIJC. Two final models ot the satellite 'oscillator op-
erating at 4. 9961 15 mc were completed, and tested for
frequency stability during mechanical ^ock, vibration,
«nd linear acceleratiory Performance of both units was
•ell within target requirements. Frequency drift rate
(hie to a ll^C change in ambient temperature was also
Mtisfactory. A 4. 996n5-mc crystal unit, sealed in a
■nail metal holder and* operated at 41°C, has shown an
Initial aging rate of less than 1 pp i09/day. A 5-mc
unit, sealed in a glass envelope and operating at 35°C,
his shown a total aging of about 2 pp 10^ during an
eijht-day run. (Author) (See also PB 144 300)
Birmingham U. (Gi. Brit. ).
CHARACTER RECOGNITION, by D. A. Bell. Final
rqx. for 1 Oct 59-30 S^ 60 on Contract DA 91-591-
EUC-1291. [1960] 2^. 6 refs; AD- 245 769.
CWer from LC mi$2. 7d, ph$4. 80 PB 152 926
Contents:
Correlation Detection of Five-Unit Code Signals.
Correlation Recognition of the Printed Numerals 0 to 9.
Mosiac Reader.
(See also PB 144 238)
Bureau of Naval Weapons, Washington, D. C.
AC AND DC VOLTAGE 10 TO 1000 VOLTS. BuWeps-
BuShips CaUbration Program. 25 Sep 58, 29p. Second-
ary Standards Lab. Measurement System Opieration
Procedure BE -05.
Order from OTS $0.75 PB 171 212
TTiis procedure describes the operation of a secondary
standard calibration system which is used to calibrate
dynamometer type Test Instruments by the reverse dc
method. This procedure normally applies to the cali-
bration of Test Instruments with accuracies between
0. 25% and 0. 5% of full scale. Test Instruments of
lesser accuracy than 0.5% at full scale should be cali-
brated by a less accurate system than that described
herein, if such is available.
Bureau of Naval Weapons, Washington, D. C.
AC- DC VOLTAGE INSTRUMENTS 10-lOOOV FULL
SCALE. BuWeps-BuShips Calibration Program.
25 July 60, 20p. Secondary Standards Lab. Instrument
Calibration Procedure AE-25.
Order from OTS $0. 50 PB 171 209
This procedure describes the calibration of dynamome-
ter voltmeters; it will verify correct performance of
the Test Instrument within the required tolerances.
Perform corrective action in accordance with the in-
struction manual and local laboratory practices. ^
Bureau of Naval Weapons, Washington, D. C.
AC VOLTAGE, 0.0001 TO 800 VOLTS 60 CPS.
BuWeps-BuShips Calibration Program. 19 Sep 58. 30p.
Secondary Standards Lab. Measurement System Opera-
tion Procedure BE -03.
Order from OTS $0.75 PB 171 213
This procedure describes the operation of a secondary
standard calibration system which is used to calibrate
ac voltage measuring instruments by the Thermal
Transfer method. This procedure normally applies to
the calibration of Test Instruments with accuracies be-
tween 0. 25% and 0.75% of full scale. Test Instruments
of lesser accuracy than 0. 75% at full scale should be
calibrated by a less accurate system than that de-
scribed herein, if such is available.
Bureau of Naval Weapons, Washington, D. C
CAPACITANCE, 0.1 TO 1050 ^^F DIRECT SUBSTITU-
TION METHOD. BuWeps-BuShips Calibration Program.
7 Aug 58, 17p. Secondary Standards Lab. Measure-
ment System Operation ft-ocedure BC-01.
Order from OTS $0. 50 PB 171 219
This procedure describes the operation of a secondary
standard calibration system which is used to calibrate
both fixed and decade-type capacitance units by the
direct substitution method using the Schering Bridge,
Parallel Mode. This procedure normally applies to the
289
measurement of dapacitance units with accuracies be-
tween 0.4% and 1^. Capacitance units of lesser accu-
racy than 1% should be calibrated by a less accurate
system than that ^escribed herein, if such is available.
This method doesj not give a direct measurement erf the
dissipation factor of the capacitance unit under calibra-
tion. The dissipation factor as read by the Capacitance
Bridge is the combined dissipation factors of the Pre-
cision Capacitor,
leads .
Test Instrument, and connecting
Bureau of Naval Weapons, Washington, D. C.
CAPACITANCE, 1 TO lOSOuuF SUBSTITUTION
METHOD I MCP^. BuWeps-BuShips Calibration Pro-
gram. 14 Aug 58^ Up. Secondary Standards Lab.
Measurement System Operation Procedure BC-02.
Order from OTS $0. 50 PB 171 220
I
I
This procedure describes the operation of a secondary
standard calibration system which is used to calibrate
both fixed and decade-type capacitance units by the sub
stitution method losing the Sobering Bridge. This pro-
cedure normally Applies to the measurement of capaci-
tance units with accuracies between 0.4% and 1%. Ca-
pacitance units ofj lesser accuracy than 1% should be
calibrated by a less accurate system than that de-
scribed herein, i^ such is available. This method docs
not give a direct tieasurement of the dissipation factor
of the capacitanca unit under calibration. The dissipa-
tion factor as read by the Capacitance Bridge is the
combined dissipation faaors of the Precision Capaci-
tor, Test Instrument, and connecting leads.
Bureau of Naval IWeapons, Washington, D. C.
CAPACITANCE. 100 >jjiF TO 1 >iF DIRECT METHOD
BuWeps-BuShips Cjalibration Program. 18 Aug 58, 16p.
Secondary Standaiids Lab. Measurement System Opera-
tion Procedure BQ-05.
Order from GTS $050 PB 171 221
This procedure df^scribes the operation of a secondary
standard calibrati^ system which is used to calibrate
both fixed and decbde-type capacitance units by the
direct method usi^g the Sobering Bridge. This proce-
dure normally applies to the measurement of capaci-
tance units with accuracies between 0. 4% and 1%.
Capaciunce units erf lesser accuracy than 1% should be
calibrated by a lens accurate system than that de-
scribed herein, if
such is available.
Bureau of Naval Weapons, Washington, D. C.
CAPACITANCE, 100 uuF TO 1100 ^lF DIRECTV
METHOD 60 CPS., BuWeps-BuShips Calibration Pro-
gram. 19 Aug 58,|l4p. Secondary Standards Lab.
Measurement Systpm Operation Procedure BC-04.
Order from OTS $6. 50 PB 171 22.3
This procedure de^ribes the operation of a secondary
standard calibraci^n system which is used to calibrate
both fixed and dec4de-type capacitance units by the
direct method using the Series Resistance Bridge
Method. This procedure normally applies to the meas-
urement of capacidance units with accuracies between
3% and 5%. Capacitance units ol lesser accuracy than
5^ should be calibtated by a less accurate system
than that described herein, if such is available.
Bureau erf Naval Weapons, Washington, D. C.
CAPACITANCE, 100 TO 1150>i>iF DIRECT METHOD
1 MCPS. BuWeps-BuShips Calibration Program.
15 Aug 58, lOp. Secondary Standards Lab. Measure-
ment System Operation Procedure BC-03.
Order from OTS $0.50 PB 171 222
This procedure describes the operation of a secondary
standard calibration system which is used to calibrate
both fixed and decade-type capacitance units by the
direa method using the Sobering Bridge. This proce-
dure normally applies to the measurement of capaci-
tance units with accuracies between 0. 4% and 1%.
Capacitance units of lesser accuracy than 1% should be
calibrated by a less accurate system than that de-
scribed herein, if such is available.
Bureau erf Naval Weapons, Washington, D. C.
DC CURRENT INSTRUMENTS 1.0 TO 200 AMPERES
FULL SCALE. BuWeps-BuShips Calibration Program.
26 Nov 58, 20p. Secondary Standards Lab. Instrumem
Calibration Procedure AI-02.
Order from OTS $0. 50 PB 171 210
This procedure describes the calibration of direa cur-
rent ammeters herein referred to as the Test Instru-
ment. A sample "Calibration Report" form has been
included at the conclusion of this procedure. The
Weston Model 901 DC Ammeter has been selected as ■
representative Test Instrument in the preparation of
the form. When calibrating other Test Instruments, the
sample report should be used as a guide. This proce-
dure nen-mally applies to the calibration of instrument!
with full-scale ranges from 1.0 to 200 amperes, and
with full-scale accuracies between 0. 2% and 0.75%.
Instruments of lesser accuracy than 0/75% full scale
should be calibrated by a less accurate system than
that utilized herein, if such is available.
Bureau of Naval Weapons, Washington, D. C.
DC RESISTANCE, 0.00001 TO 1.0 OHM. BuWeps-
BuShips Calibration Program. 6 July 60, lip. Second-
ary Standards Lab. Measurement System Operation
Procedure BR-04.
Order from OTS $0.50 PB 171 206
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to calibrate direc; current resistance instruments,
using the Kelvin Bridge. The Kelvin Bridge system
offers a means of measuring low valued four-terminal
resistors, largely free of the error contributed by lead
and contaa resistance. This is achieved by putting the
leads and contaas in series with high resistance in the
ratio arms; using a sufficiently low resistance yoke in
relation to the resistance value being measured; and
where accuracy requires, arranging the Ratio Box lead
resistance ratio to match the ratio being used. This
procedure normally aprplies to the calibration of Test
Instruments with accuracies between 0.05% and lOj^-
Test Instruments of lesser accuracy than l.OJ^ should
be calibrated by a less accurate system than that
described herein, if such is available.
290
Bureau of Naval Weapons, Washington, D. C.
DC RESISTANCE 0. 1 OHM TO 100 MEGOHMS.
BuWeps-BuShips Calibration Program. 2 Sep 58, 13p.
Secondary Standards Lab. Measurement System Opera-
don Procedure BR -03.
order from OTS $0. 50 PB 171 206
This procedure describes the operation of a secondary
itandard calibration system whi(± is used to calibrate
direa current resistan<^e instruments, using the
Wheatstone Bridge method. This procedure normally
tpplies to the calibration of Test Instruments with
accuracies between 0. 5% and 1 . 0%. Test Instruments
of lesser accuracy than 1.0% should be calibrated by
• less accurate system than that described herein, if
•uch is available.
Bureau of Naval Weapons, Washingtem, D. C.
DC RESISTANCE 10 OHMS TO 1.000,000 MEGOHMS.
BuWeps-BuShips Calibration Program. 2 Sep 58, lOp.
Secondary Standards Lab. Measurement System Opera-
tion Procedure BR -02.
Order from OTS $0. 50 PB 171 207
This procedure descrities the operation erf a secondary
Kandard calibration system which is used to calibrate
decade and fixed type, two terminal, direct current re-
•ietance instruments, u«ing an unguarded megohm
bridge. This system do^s not allow for the separation
ii measurement of the shunt leakage resisunce that be-
oomes significant beyond approximately ten megohms.
This procedure normally applies to the calibration of
Test instruments with a minimum ratio of 4:1 between
the applicable system phase accuracy and the Test In-
■rument accuracy. Test Instruments erf lesser accu-
racy should be calibrate(J by a less accurate system
then that described herein, if such is available.
Bureau of Naval Weapons, Washington, D. C.
rc VOLTAGE 0 TO 1000 VOLTS. BuWeps-BuShips
CaUbration Program. 21 Feb 58, lip. Secondary
Standards Lab. Measuretnent System Operation Proce-
dure no. BE -01. ;
Orter from OTS $0. 50 | PB 171 215
This procedure describes the operation of a secondary
•tUKkrd calibration system which is used to calibrate
direa current voltage measuring Instruments, by the
dc Potentiometric method. This procedure applies
normally to the calibrati6n erf instruments with maxi-
mum ranges not exceeding 1000 volts, and with accu-
ndes between 0. 25% an<! 0. 5% full scale. Instruments
of lesser accuracy than 0.5% full scale should be cali-
brated by a less accurate' system than that described
ktreln, if such is available.
kireau of Naval Weaporfe, Washington, D. C.
DC VOLTAGE 1.02 TO 1000 VOLTS. BuWeps-
Mbps Calibration Program. 27 Feb 58, 7p. Second-
try Standards Lab. Measurement System Operation
^ocedure BE-02.
Orter from OTS $0. 50 i PB 171 214
TWe procedure described the operation of a secondary
■■•dird calibration system which is used to calibrate
to«ct current voltage measuring instruments, using a
calibrated voltage source. This procedure applies
normally to the calibration of instruments with maxi-
mum ranges not exceeding 1000 volts, or ranges with
a minimum value of 1.02 volts, and with accuracies
between 0. 5% and 1 . 0% full scale. Instruments of
lesser accuracies than 1.0% full scale should be cali-
brated by a less accurate system than that described
herein, if such is available.
Bureau of Naval Weapons, Washington, D. C.
DC VOLTAGE INSTRUMENTS 1-1500 MV FULL
SCALE. BuWeps-BuShlps Calibration Program.
16 Oct 58. 16p. Secondary Standards Lab. Instrument
Calibration Procedure AE-01.
Order from OTS $0.50 PB 171 218
This prcK^dure describes the calibratiem erf direa cur-
rent milllvoltmeters herein referred to as Test Instru-
ments. A sample Calibration Report form has been in-
cluded at the conclusion of this procedure. The Weston
Mexlel 622 DC Mi 111 voltmeter has been selected as a
representative Test Instrument in the preparation erf
this form. When calibrating other Test Instruments,
the sample report should be used as a guide. This pro-
cedure applies normally to the calibration erf instru-
ments with full scale ranges from 1 to 1500 ntillivolts,
and with full-scale accuracies between 0. 2% and 0.75%.
Instruments of lesser accuracy than 0. 75% full scale
should be calibrated by a less accurate system tfem
that utilized herein, if such is available.
Bureau erf Naval Weapons, Washington, D. C.
DC VOLTAGE INSTRUMENTS 15-1000 VOLTS FULL
SCALE. BuWeps-BuShips Calibration Program.
3 Nov 58, 14p. Secondary Standards Lab. Instrument
Calibration Procedure AE-03.
Order from OTS $0.50 PB 171 217
This pr(x;edure describes the calibration of direa cur-
rent voltmeters herein referred to as Test Instrumenta
A sample "Calibration Report" form has been included
at the conclusion of this procedure. The Westinghcxise
Model PX-4 DC Voltmeter has been selected as a rep-
resentative Test Instrument in the preparation of this
form. When calibrating other Test Instruments, the
sample report should be used as a guide. This proce-
dure applies normally to the calibration erf instruments
with full-scale ranges from 15 to 1000 volts, and with
full-scale accuracies between 0.5% and 2.0%. Instru-
ments of lesser accuracy than 2.0% full scale should
be calibrated by a less accurate system than that
utilized herein, if such is available.
Bureau erf Naval Weapons, Washingtem, D. C.
DECADE RESISTORS 0.1 TO 100,000 OHMS PER
STEP (USING L&N 4232-Al BRIDGE). BuWeps-BuShips
Calibration Program. 2 May 60, 17p. Secondary
Standards Lab. Instrument Calibratiem Procedure
AR-06.
Order from OTS $0.50 PB 171 211
This prcxxdure describes the caUbration erf decade re-
sistors. This procedure will verify correa perform-
ance of the Test Instrument within the required toler-
ane:es. Normally, each recorded value is compared to
its tolerance and corrective aaion taken, if required.
II
n
291
before continuing the test. However, it is sometimes
desirable to delay the verification and corrective action
until several reilated values have been recorded. A
sample Calibration Report form has been included at
the conclusion ij/t this procedure. The General Radio
1432A has been I selected as a representative Test In-
strument in the I preparation of this form. When cali-
brating other Tfst Instruments, the sample report
should be used as a guide. This procedure applies
normally to thejcalibration of instruments with resist-
ance decades of|o. 1 to 100k ohms per step, and with
accuracies bet»»een 0. 05% and 0. 5%. Instruments of
lesser accuracy! than 0. 5% should be calibrated by a
lesa accurate s; stem than that utilized herein, if such
is available. Tl lis procedure covers the calibration of
Test InstrumenQs by measuring the dc resistance at
each step erf thedecade; it does not provide for the
measurement ol
resistance
the Test Instrument residual
Bureau of Navj 1 Weapons, Washington, D. C.
FREQUENCY RESPONSE 10 CPS TO 10 MCPS, 0.5
MV TO 5.2V A^ID AC VOLTAGE CALIBRATION DC
TO 10 MCPS, 0|.l TO 5.2 VOLTS. BuWepe-BuShlpe
Calibration Proi-am. 18 Jan 60, 29p. Secondary
Standards Lab. Measurement System Operation Proce-
dure BF-06.
Order from OTS
This procedure
Standards
to measure the
of indicating anc
lescribes the operation of a Secondary
calibration system which is used
I requency response and/or ac voltage
generating instruments.
Laboratory
a!
Bureau of Nav
INDUCTANCE.
BuWeps-BuShips
Secondary Star.<
tion Procedure
Order from OTS
$1.00
PB 171 216
Weapons, Washington, D. C
lO/iH TO 10 H DIRECT METHOD.
Calibration Program. 28 Aug 58, 23p.
idirds Lab. Measurement System Opera -
Bt-01.
$0.50 PB 171 208
This procedure describes the operation of a secondary
standard calibration system which is used to calibrate
both fixed and dacade-type inductance units, by the
direct method uaing an Inductance Bridge. This proce-
dure normally afplies to the calibration of Test Instru-
ments with accutacies between 1.0% and 2.0%. Test
Instruments at lesser accuracy than 2. 0% should be
calibrated by a less accurate system than that de-
scribed herein, If such is available. This system is
not suitable for t^e calibration of inductors with mag-
netic cores, sinde no provision is made for the deter-
mination erf the incremental inductance due to current
in the winding.
Bureau of Navall Weapons, Washington, D. C
STANDARDS INCtUCTORS, IOOjH TO lOH GENERAL
RADIO 1482 SERjIES (USING GR 1632A BRIDGE).
BuWeps-BuShips Calibration Program. 19 May 60. 13p.
Secondary Standards Lab. Cross-Check Procedure
CL-02. i
Order from OTS ^0. 50 FB 171 201
This procedure describes the cross-check of two like-
valued General R«dio Standard Inductors, 1482 series.
by the direct sub^itution method; it also applies to
similar standard inductors with accuracy and stability
specifications equal or nearly equal to the General
Radio 1482 series. Standard induaors of lesser
accuracy may be calibrated rather than cross-checked.
Bureau of Naval Weapons, Washington, D. C.
STANDARD RESISTORS NBS TYPE 1 OHM TO
100,000 0HX4S (USING LAN 4232-Al BRIDGE).
BuWeps-BuShlpe Calibration Program. 27 Apr 60, 12p.
Secondary Standards Lab. Cross-Check Procedure
CR-02.
Order from OTS $0. 50 PB 171 200
This procedure describes the cross-check of two like-
valued standard resistors: it also applies to similar
standard resistors with accuracy specifications equal
or nearly equal to those Usted. Standard resistors of
lesaer accuracy may be calibrated rather than
cross-checked.
Bureau of Naval Weapons, Washington, D. C.
VOLTAGE STANDING WAVE RATIO, X-BAND (8.20
TO 12.40 KMC) 1.01:1 TO 10:1. BuWeps-BuShips
Calibration Program. 13 July 60, 13p. Secondary
Standards Lab. Measurement System Operation Pro-
cedure HV-05.
Order from OTS $0.50 PB 171 201
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to measure the voltage standing wave ratio of X-band
instruments of 1" x 1/2" waveguide size (outside
dimensions).
Columbia U. School of Engineering, New York.
A CLASS OF OPTIMUM NON-LINEAR FILTERS FOII
QUANTIZED INPUTS, by Frank Tung. Technical rept.
T-2/N on Contract AF 19(604)4140. I July 60. 48p.
12 refs. CU-8-60-AF-4I40-EE; ERD TN-60-769.
Order from LC mi$3. 30. ph$7. 80 PB 152 254
Optimum non-linear filters belonging to Zadeh's claaa
?7j are considered. Anention is restricted to those
systems whose present output is influenced only by a
portion d the past input. The input signal consists d
a message and noise both of which are stationary ran-
dom processes. For this class of filters it is found
that only the second order probability density functiotu
of the message and the noise are necessary for obuin-
ing the optimizing integral equation. It is assumed thM
the amplitude of the input time series is bounded and
takes on discrete values at all times. Tliis assumption
is not too restrictive in practice since data supplied by
computers and devices using digital read-out are quan-
tized. By subjecting the joint probability density func-
tions to a few mild restrictions, it is found that the
optimizing integral equation reduces to a system of in-
tegral equations of the Wiener-Hopf type. By virtue of
the assumptions made, the Fourier transforms of the
kernels of these equations are rational functions. A
method is developed for the solution of this set of si-
multaneous integral equations and three examples are
given. (Author)
292
Cbmell-Dubllier Electric Corp., Indianapolis, bid.
RESEARCH AND DEVELOPMENT OF BATTERY
CHARGER PP-1451 ( )/G, by G. R Todd. Final rept.
for 28 Mar 56-28 Jan 59 on Contract DA 36-039-sc-
71226. [1959] 51p. AD-232 947.
Order from LC ml $3. 6^, ph$9. 30 PB 149-703
This report covers research and development and pro-
duction of prototype for a closely regulated, well
filtered, power supply for operation of various
communication gear, telephone switch boards, etc. ,
and for the purpose of charging batteries. The power
output is 28 VDC or 56 VDC at 1400 watts. Design was
successfully completed and prototypes were
constructed.
i
Curtlss- Wright torp. , Santa Barbara, Calif.
HYPERSONIC FREE FLIGHT RESEARCH. PART I:
INSTRUMENTATION EVALUATICffJ AND DATA
ANALYSIS, by R. W. Bogle and R. J. Magnus. Rept.
ooContraa AF 33(616)5(104. July 60, 45p. 9 refs.
WADD Technical rept. 39-708, Part I.
Order from OTS $1.25 ■ PB 171 194
Investigations of the reliability and accuracy levels of
the data -gathering system of the two-stage HTV-1 Hy-
personic Test Vehicle were conducted. Environmental
teats of the airborne magnetic tape recorder under ac-
celerations, vibrations, impacts and temperatures ap-
proidmatlng the free-flight environment of the HTV-1
provided a basis forXouantitative interpretation of the
•erothermodynamic c&ta and determination of the ac-
curacy level for the HTV recorder system. Results
Indicate that the electrical and mechanical performance
of the tape recorder and data- measuring system is
ndsfactory. The accuracy level of directly measured
quantities is approximately 2.5 percent. Similar re-
sults are obtained for Indirectly obtained quantities
that exhibit large changes in short time intervals. In-
*realy obtained quantities that vary slowly over rela-
tlrely long time interval^, for example heating rates
■ay result in errors of ibe order of 10% and in the
•orst cases, 45%. (Author)
Diamond Ordnance Fuze Labs , Washington, D. C.
■LIOGRAFHY OF NBS REPORTS ON PERFOR-
MANCE OF TELEMETRY TRANSDUCERS AND
CALIBRATION METHODS, by Joseph Pearlsteln.
U Oct 60, 5p. 44 refs. technical rept. TR-887.
Orter from LC mill. 80,. ph$l. 80 PB 153 496
Thia bibliography is a current list of reports that have
teen prepared by the Mechanical Instruments Section,
Instrumentation Division of the National Bureau of
teodards, under a program to determine the perform -
«sce of transducers used for telemetry and to de-
»elop testing and calibraiion tnethods for these devices.
(Author)
ttamond Ordnance Fuze Labs. . Washington, D. C.
COMPARISON OF A DUAL AND A SINGLE THRESH-
OLD METHOD OF DETECTION FOR A SCANNING
RADAR, by Joseph V. Cuneo. 14 Nov 50, 24p. Tech-
«*cal rept. TR-879. ^
Onler from LC mi$2. 70, ph$4. 80 PB 152 655
Two detection methods were experimentally compared,
using simulated returns of a scanning radar. The
single threshold method which employed a filter closely
approximating a matched filter was found superior to a
dual threshold method which utilized the occurrence of
a number of consecutive threshold crossings. The su-
periority of the single threshold method was not uni-
form but was found to be dependent upon the S/N ratio
of the radar return. Under the experimental conditions
described in this report, and for a given probability of
detection per scan, the single threshold method ex-
hibited an advanuge of 2 to 3 db over a 6 to 15 db range
of a signal-to-noise ratios. However, the advanuge of
the single threshold method was obtained at the cost of
considerable complexity in the instrumenution of a >
detection system. (Author)
Diamond Ordnance Fuze Labs. , Washington, D. C.
K-BAND RECIPROCAL FERRITE PHASE MODULA-
TOR, by Frank Reggia. 7 Nov 60. 14p. 7 refs.
TR-870.
Order from LC mi$2. 40, ph$3. 30 PB 152 581
A reciprocal ferrite phase modulator has been de-
signed for use at 23 to 25 kMc that makes use of small
magnetic fields for obtaining very large phase shifts.
It consists essentially of a Ni-Zn ferrite rod centrally
located inside a standard rectangular waveguide ex-
cited in the TEqi mode and a low -current solenoid for
producing the longitudinal control field. With a proper
choice of rod diameter and impedance matching ele-
ments, phase shifts greater than 600 deg/in. of effec-
tive length of rod and variations in transmitted power
less than 0. 2 db have been obtained with external con-
trol fields less than 50 oersteds. The zero-field in-
senion loss is approximately 0. 1 db/in. and the total
weight of the 3-ln. long modulator is 5 oz. These
characteristics, along with its simple geometrical
configuration, low operating power requirement and -^
small size, make this electrically controlled recipro- if
cal phase modulator especially suitable for rapid-
scanning microwave antennas. (Author)
Diamond Ordnance Fuze Labs. , Washington, D. C.
MINIATURIZED HIGH -PRECISION CRYSTAL OSCIL-
LATOR, by K. H. Sann. 10 Nov 60. 27p. 3 refs.
TR-878.
Order from LC mi$2. 70. ph$4. 80 PB 152 922
Missile guidance and control systems using frequency
standards offer a variety of possible advantages.
Quartz crystal oscillators used as frequency standards
are stable, and are sufficiently small and light in
weight to permit their consideration in missile sys-
tems. An analysis was made of the effects of compo-
nents on frequency stability of a highly miniaturized,
stable crystal oscillator. A laboratory model was
built that weighs 1 lb, occupies 20 in.^, and has a
short-term stability under laboratory conditions of
better than 10"'. The performance characteristics
promise, with further work, to lead to a miniaturized
frequency standard of 10'^ under the assumed dynamic
conditions. (Author)
293
East Coast Aetronautics . Inc., Pelham Manor, N. Y.
DEVELOPMENT OF A MODULAR SHELTER FOR
ELECTRONIC SYSTEMS, by Arthur Kenger. Final
rept. on Contrajct AR 30(635)4495. [I957y40p.
Technical rept .1 1 92 . 04; RADC TR-57-85; AD- 114 467.
Order from LC mi$3.00. ph$6.30 PB 153 273
A program for the design, fabrication and testing of a
modular shelte^ for uctical electronic systems was
undertaken at Ebst Coast Aeronautics , Inc. The aim of
the program wa^ to investigate and establish design cri-
teria for sheltefs incorporating techniques and mate-
rials applicable! to shelter requirements . In addition to
the above, the Results of the investigation were to be
used to design, jmanufactu re, and test a modular shel-
ter composed ol the feature techniques and materials
investigated, work on this program was not completed.
In view of this , Ithe following report is presented to
point out the deficiencies in the design in order to expc-
dfte future shelijer developments . In addition to the de-
ficiencies, a preliminary erection procedure is
presented .
Electrical Engineering Research Lab. , U. of
Illinois. Urbaiia.
DRIVING-POINt FUNCTION SYNTHESIS BY TRANS-
FORMATION OP THE BRUNE NETWORK, by Vempati
Gopaia Krishna ^urti. Interim technical rept. no. 16
onContract DA (11-022 -ORD- 1983. 15 Jan 60, 84p.
25 refs. OOR r4pt. 2207. 5 -E; AD-232 931.
Order from LC rni$4. 8a ph$l3. 80 PB 149 636
A new method of synthesizing driving -point immittaix:e
functions with ptssive linear elements and without
transformers is presented. The method is based on the
derivation of transformerless equivalent circuits for a
■ingle Brune cycle conuining a perfectly coupled trans-
former. The eq^ivalent circuits take the form of a
symmetrical bridge network containing 2 identical im-
pedance functions to be synthesized in the next stage.
A comprehensive list of these networks relating their
element values *ith those of the Brune network is given
The topology anq the number of elements in these.
bridge circuits depend on the turns ratio of the Brune
transformer. Pfom the point of reduction of the num-
ber of elements,! a transformer of turns ratio 2 or 1/2
is favorable. A paving of 2 reactive elements per
•uge, as compared with the modified Bott-Duffin pro-
cedure, is possible. For other cases, the networks
contain, for the large part, fewer elements than the
corresponding B<«t-Duffin bridge networks. In the reg-
ular Brune synthesis procedure, the minimum values
of the real part of a given impedance function along the
imaginary axis i» removed as a series resistance. If,
however, a resistance with a smaller value is removed
in series and thq remainder function developed on the
admicunce basid, a new Brune -type network is ob-
tained. The parameters of this new network, including
the transformer ratio, vary depending on the value of
the series resistance in the first step. A method using
this property is ^ven for obtaining desired conditions
in the Brune -typ^ network. Special synthesis proce-
dures for the practically biquadratic and bicubic func-
tion* are presented. (Author)
Electrical Engineering Research Lab. , U. d Illincit,
Urbana.
REAUZATICW OF LOOP- RESISTANCE MATRICES,
by Hing-Cheong So. Interim technical rept. no. 17 on
Contraa DA 11-022-ORD-1983. 15 Jan 60, 80p.
25 refs. OOR rept. 2207. 6-E; AD-232 937.
Order from LC mi$4. 50, ph$12. 30 PB 149 637
A pure resistance network G is said to be a coherent
realization of a symmetric, real nutrix M - [ajj] if (l)
M is the loop-resistance matrix of G for scn^e set of
loops [1) in G, and (2) there exist no 2 loops li and Ij k
[1] such that li and Ij agree in orientations in one re-
sistor Ra of G but oppose in orientations in another re-
sistor Rb of G. Incoherent realizations are resistance
networks which satisfy condition (1) but not condition
(2). Coherent realizations are mainly considered, al-
though incoherent realizations for third-order real
matrices are discussed.
Electrical Engineering Research Lab. , U. of
Illinois , Urbana.
SYNTHESIS OF RC LADDER NETWORKS WITH
SPEQFIED DRIVING-PaNT AND TRANSFER FUNC-
TIONS, by James R. Young. Technical note no. l6on
Contract AF 49(638)63. 9 Sep 60, 76p. 31 refs .
AFOSR-TN-60-1090; AD-244 369.
Order from LC mi$4.50, ph$12.30 PB 152 489
Necessary and sufficient conditions are stated for the
realizability of the shon-circuit admittance functions
and the open-circuit impedance functions of high-pasi
and low-pass simple RC ladders . Synthesis of these
simple RC ladders is accomplished through the use of
formulas which simultaneously reduce both driving-
point functions and the transfer function. It is shown
that double zeros of A and Aj ^22 occur when the open-
circuit impedance functions or the shon-circuft ad-
mittance functions , respectively, have noncompact
poles. Finally, the Fialkow-Gerst coefficient con-
ditions and the residue condition are shown to be suf-
ficient for the realization of the short-circuit admit-
tance functions or the open-circuit impedance func-
tions of a low-pass or high-pass modified simple RC
ladder. Shunt resistors or capacitors are added to the
conventional low-pass or high-pass simple ladder to
form a modified ladder. (Author)
Electrical Engineering Research Lab. , U. of
Illinois , Urbana.
TRANSFER FUNCTION SYNTHESIS BASED ON CAS-
CADED RC AND RL NETWORKS, by Donald Albert
Calahan. Technical note no. 15 on Contract
AF 49(638)63. 1 Sep 60, 128p. 23 refs .
AFOSR TN-60-1024; AD-244 368.
Order from LC mi$6.30, ph$19.80 PB 152 486
A method of partitioning transfer functions into RC snd
RL subnetwork functions is developed. It is shown
that the poles of any transfer function realizable by
cascaded RC and RL subnetworks are restricted by tbe
corvjition ^
j;arg Si<2
' m -«-i«. ,
294
?
u-A ,^ifVi ""• ' i,'
«bere the - Sj are the upper half plane complex poles .
Sufficient conditions are derived for the realization of
(X transfer function in the RC-RL form. A proce-
jite is also developed for maximization of the gain
constant of certain classes of transfer functions when
realized by this model . (Author)
Electron Tube Research Lab. , U. of Minnesota,
Minneapolis.
STUDIES ON BASE NICKELS FOR OX IDE- COATED
CATHODES, by W. G. Shepherd and D. E. Anderson.
Scientific rept. no. 8, 15 Jan- 15 Apr 60, on Contract
AF 19(604)3890. [1960] 97p. 17 refs. ERD-TN-60-796.
Order from LC mi$5. 40, ph$l5. 30 PB 152 735
A carbon-dispensing cathode base which throttles the
rate of carbon flow to a more useful value is described.
Cathodes, based on 0. 2% and 0. 08% Al-Nl alloys, have
now been operated at 1Q93°K in excess of 10,000 hours.
Stable emission levels of over 11 amps/cm^ continue to
be observed. Preliminary results are presented for the
re-evolution of free Sr from Ti, using Sr as a
tracer.
Electronics Research Lab. , U. of California,
Bfirlcc lev •
APPUCATION OF CORRELATION TECHNIQUES TO
ANTENNA SYSTEMS, by I. W. Linder. Rept. on Con-
tract N7onr- 29529. 11 Jan 60, 25p. 3 refa. Rept.
ao. 100: lER series no« 60, issue no. 267; AD- 235 198.
Order from LC mi$2.70, ph$4.80 PB 152 861
The development of the' optimum antenna and the exam-
ples chosen to illustrate the theory involved have been
iAended as initial considerations in the general prob-
lem of detecting a noisilike signal buried in a general
ndsy medium. This development has utilized only in
a general manner the extensive mathematical methods
which can be used to handle noise problems. In this
case a consideration of a spatial distribution of the
noise was combined with the correlation function of
random noise theory to arrive at an expression for
"best" antenna array. j[Author)
Electronics Research Lab. , U. of California,
Berkeley.
BOUNDS ON NATURAL FREQUENCIES OF LINEAR
ACTIVE NETWORKS, by C. A. Desoer and E. S. Kuh.
Rept. on Contract Nonr-222(74). 21 Mar 60, 30p. 5 refs.
Rept. no. 103; lER series no. 60, issue no. 271;
AD- 236 376.
Order from LC mi$2. 70, ph$4. 80 PB 147 314
Recent developments o{ new active devices have stimu-
lated circuit theorists to develop understanding of the
potentialities and limitations of linear active networks.
Research was concerned with the natural frequencies
(I.e. , the roots of the characteristic equation) of the
■etwork obtained by connecting the active device to fin
■rbitrary passive network. (Author) j
Electronics Research Lab. , U. of California,
Berkeley.
QUARTERLY PROGRESS REPORT, 1 OCTOBER-
31 DECEMBER 1959. Rept. on Contracts N7onr-29529
and Nonr- 222(53. 54, 57). 31 Jan 60, 28p. 4 refs.
Series no. 60, issue no. 27; AD- 235 450.
Order from LC nu»2.70, ph$4.80 PB 152 859
Contents:
Back- scattering from cones
Scattering from multiple targets
Scattering fields from anisotropic media
Microwave parametric amplifiers
Ferrite field-displacement device for slot coupling
control
Network theory
Electronics circuits research
Antenna arrays from a data- processing viewpoint
Information theory
Solar emission and absorption
Research in high temperature semicoiiductor devices
Magnetic amplifiers (See also PB 145 072)
Electronics Research Lab. , U. at California,
Berkeley.
STABILITY OF RANDOM LINEAR SYSTEMS WITH
MARKOV PARAMETERS (PART I), by B. H. Bharucha.
Scientific rept. no. 2 on Contraa AF 19(604)5466.
29 June 60, 35p. 10 refs. Series no. 60, issue no. 289;
ERD-TN-60-776; AD- 245 221.
Order from LC mi$3. 00, ph$6. 30 PB 152 741
The i-th moment stability of the random linear differ-
ential system with piecewise consunt parameters:
x^ A|cX, tic-i^ i< tic, k = 1, 2, ... is investigated
when the parameter process is (a) an independent
process, (b) a finite Markov chain. It is shown that
almost sure asymptotic stability is a consequence of
second moment asymptotic stability, whereas the
converse statement is false. (Author)
Electronics Research Lab., U. of California,
Berkeley.
STUDY OF CROSSED-FIELD AMPLIFIERS, by
J. R. Whinnery, C. K. Birdsall and others. Final rejK.
for 1 Ian 58-31 Jan 60 on Contract DA 36-039-sc-7498l.
(1960) 53p. 11 refs. AD- 240 766.
Order from LC mi$3. 60, ph$9. 30 PB 452 994
The completed fabrication of the second model of the
cjossed-field velocity analyzer is discussed. Prelimi-
nary measurements made to determine the plate char-
aaeristics for various heater voltages and the position
of the sampling slit relative to the center of the beam
as a function of the position of the movable cathode are
reviewed. A program to determine the dependence of
the noise figure on the parameters of a crossed-field
amplifier with laminar-flow beam was initiated to fol-
low up the promising preliminary results recently ob-
tained here. An analysis of the crossed-field potential
minimum is presented. The general form of the solu-
tion is derived. The coefficients in the general equa-
tions are defined after making certain simplifying
assumptions. A numerical example is examined to
295
study the possibility of an instability being caused by
the magnetic fielq. In large- signal work the beam
width was determined to be only one-half oi the pre-
viously assumed falue. The large-signal theory of
Sedin is shown to be verified for the case of low gain
backward- wave ainplification. Efficiencies as high as
62. 5^ are repcrttd. The effect of input signal level on
tbe phase shift thfough the amplifier is presented.
(Author) (See alsc PB 149 410)
Electronics Research Lab. , U. of California, Berkeley
SWITCHING AND MEMORY CRFTERIA IN TRANSIS-
TOR FUP-FLOPJ, by D. K. Lynn and D. O. Pederson.
Rept. on Ccntractj Noor-222(74). 2 Mar 60, 23p. 8refs.
Rept no. 101; IE|* series no. 60, issue no. 269;
AD- 236 377.
Order from LC ii*$2.70, ph$4. 80 PB 147 313
ft is well known tl)at the magnitude and length of the
minimum input trigger pulse is closely related to the
switching and meifiory aspects of the flip-flop. A study
of the relationshii^ is made in this report. Not all
energy or charge storage elements or mechanisms can
serve as the flip- Hop memory. A memory criterion in
terms of a simple physical argument has been estab-
lished to determine which storage elements provide the
necessary memorV function. Switching criteria and the
minimum amount of memory are determined from an
analysis of the initial conditions of the regenerative
switching action using piece- wise linear analysis tech-
niques. Prom this Information, estimates of maximum
repetition frequenpy are made. Capacitively and in-
ductively coupled flip-flops are used as illustrations,
and experimental results with the circuits are
presented. (Auth<|r) i
Electronics Research Lab.,
Berkeley.
SYNTHESIS OF
Olivares. Jr. R
153p. 24 refs. R
no. 265; AD- 233 1
Order from LC m
U. of California,
PORT RC NETWORKS, by J. E.
on Contract N7onr - 29529. 7 Jan 60,
. no. 99; lER series no. 60, issue
7.
. SO, ph$24. 30 FB 152 860
This report preseiits an attempt at determining the
necessary and sufljicient conditions that a matrix of
rarional algebraic functions is the immitance matrix
of a grounded RC oerwork. These networks are ana-
lyzed to determinel necessary conditions and powerful
methods for synthesizing them are developed. The re-
sults are then appijied to syrchesizing N-port RC: net-
works, devious i0rk by other investigators is re-
viewed. The probljem is then formulated mathemati-
cally in terms of tfce nodal admittance of a grounded RC
network for «^ich necessary and sufficient conditions
are well known. ?sM2cessary conditions on terminal im-
mittance matrices jare derived from the properties of
the nodal admittance matrix. Three related methods
for synthesizing si|ch networks are developed and
numerous illustradive examples are shown. These
three methods are a powerful means for synthesizing
grounded RC netwdrks of arbitrary structure with a
minimum number irf internal nodes. The results are
applied to the synthesis of balanced N-port RC networks
In which the restric :ion of a common ground is removed.
(Author)
Elk Electronic Labs. , Inc. , New York.
DEVELOPMENT OF RADIO INTERFERENCE MEAS-
URING SET AN/FRM-14( ) by Jacob Roeenbaum. Pint}
rept. for Aug 54-Oct 58 on Contraa DA 36-039-8C-
63113. [1958] 108p. 4 refs. AD-211487.
Order from LC mi$5.70, ph$16.80 PB 152 992
This report discusses the problems encountered and
the solutions achieved in the development of an ultra-
compaa, lightweight and portable RF interference
measuring set. Since ease of maintenance will deter-
mine the operational life of equipments, unit sub-
assemblies were employed permitting plug-in replace-
ment of parts and/or units reaching the end of their
useful Ufe. Since some of the data found In the Instruc-
tion Book Is helpful in achieving a better overall under-
standing of this equipment, the complete Instruaion
Book for the AN/FTIM-14( ) is included. (Author)
Fluid Dynamics Research Lab. , Mass. Inst, of Tedi.
[Cambridge].
A SMALL PIE2WELECTRIC MICROPHONE, by Erik
MoUb-Christensen. Rept. on NASA Contract NsG31-60.
July 60, lOp. Fluid Dynamics Research Group rept.
no. 60-3. AD- 244 588.
Order from LC mill. 80, ph$1.80 PB 152 603
This microphone was designed and constructed to fill
the need for a small microphone with a frequency re-
sponse in excess of 75 kilocycles per second. The dif-
ficult problem in the design of small piezoelectric mi-
crophones is the design of the terminal arrangement.
This problem was solved by designing the microphone
as a slight modification of a commercially available
coaxial jack. (Author)
General Electric Co. , Schenectady, N. Y.
INVESTIGATION OF VARIOUS ACTIVATOR -REPRAO
TORY SUBSTRATE COMBINATIONS, by J. H. Affleck.
Scientific rept. no. 9 on Contract AF 19(604)4093
6 Sep 60, lOp. 4 refs. AFCRL-TN-60-976; AD-244 484.
Order from LC mill 80. ph|1.80 PB 152 610
The thermionic constants and evaporation rates of sev-
eral refractory substrate -activator combinations are
reported and the results discussed. There is evidence
to show that tungsten carbide and tantalum have de-
sirable properties as the matrix element in a dispensei
rarhode. (Author) (See also PB 148 926)
(jeneral Electric Co. , Schenectady, N. Y.
TRANSMITTING BEAM TETRODE, TYPE Z-5192, by
J L. Wilson. Final rept. for 1 Jan -31 Aug 59 on Con-
tract DA 36 -039 -sc- 78275. 27 Nov 59, 104p.;
AD-231 626.
Order from LC mi|5. 70, ph|I6. 80 PB 149 694
Assembly and prtxessing of the Z-5192 tetrode is dis-
cussed. Results of the various tests are stated with the
proposed limits for each test. Probability curves and
histograms are presented which show the spread and
distribution of each characteristic test. A proposed
MIL-E-1 specification is included. (Author)
296
General Electric Co. ^ Syracuse, N. Y.
^ FEASIBILITY STUDV PF THE USE OF PHASE
SHIFT KEYING OVER, AN IONOSPHERIC SCATTER
TRANSMISSION CIRCUIT, by R. W. Swanson. Fin*l
rept. on Contract AF 1?( 604)4077. Mar 60, 225p.
23refs. AFCRL TR-60-131.
Order from LC mi|9.S}0. phi 34. 80 PB 152 958
A study, including implementation and field testing,
was conducted to determine the feasibility of a phase
shift keying (PSK) system and diversity reception for
^ tbe transmission of binary information over an iono-
tpberic scatter troismission circuit. The PSK equip-
oient designed and builf for this study operated at a fre-
quency of 49.6 MC wit^i dual equal-gain frequency
diversity, and it could transmit data at a rate of 11.1
or 55.5 nine-bit messages per second (nominal 100 or
500 bits per second). Two methods of obtaining both
bit and character timing information were implemented
and tested. Field testing of the PSK equipment was
carried out over the Natio.nal Bureau of Standards
Icosopheric Scatter Lipk between Havana, Illinois, and
Boulder, Colorado. Tl^ field results obtained demon-
strate Che feasibility of using phase shift keying as a
modulation technique for the transmission of binary
information over an ionospheric scatter path under
normal scattering conditions. The results of this test
program and a discus^on of them with the conclusions
and recommendations that can be made are included in
this report. (Author)
i
General Electric Co. . Syracuse, N. Y.
PERRITE MATERIALS FOR MICROWAVE FRE-
QUENCIES, byj. M. Blank, L. T. Piekarski and
others. Final rept. 1 5. Sep 57-30 Dec 59. on Contract
DA 36 -039- 8c- 74904 (i960] 172p. 10 refs.
Order from LC mi|8. 10, ph|27. 30 PB 152 660
This report released for sale to the public 29 Dec 60.
The study on low -power microwave materials was di-
rected toward learning to control the important param-
eters for achieving good microwave materials based on
magnesium ferrite aluminace compositions. Although
parameters concerned with batch preparation and firing
schedule were controlled, good reproducibility of the
desired properties wsf not achieved. Fine grain mag-
nesium aluminum ferrite samples having an average
grain size of less than|0. I ^were successfully pre-
pared by hot pressing techniques. The pressure -com-
position-temperature relationships at high temperature
for the wustite, magnetite, and hematite phases ^f the
iron oxide system were successfully explained by con-
sideration of the entropy of mixing of lattice defects.
The heat of mixing of t;he defects with the lattice was
assumed to be zero; tHis was verified experimentally.
Another helpful assumption was that the charge distri-
bution in a given phase is independent of the composi-
tion of that phase. The temperature coefficient of per-
meability of a standard, fired sample containing 34. 0
mol-% Fe203, 3. 0 Mn203, 50. 0 MgO and 13. 0 AI2O3
was about 40 times greater than that for a hot pressed
sample between 24° ar^d 1 lO'^. Strain gage equipment
which was developed fer measuring magnetostriction
of ferrites was capably of measuring differences be-
tween samples at values of 1 x 10"* to 2 x 10"8
inch/inch. This was adequate to show that one magne-
sium ferrite aluminatq sample, which had a narrow
resonance absorption Jinc width for microwaves at low
i 297
power levels, had small variations in magnetostric-
tion which appeared to be correlated with small varia-
tions in line width for a number of samples.
Granger Associates, Palo Alto, Calif.
ANTENNA AS-1019(XE-1)/TRD, by R. E. Hunter.
Quarterly progress rept. no. 3, 1 Feb-1 May 60, on
Contraa DA 36-039- 8C-84533. [1960] 14p. AD- 240 285.
Order from LC mi|2.40, ph|3.30 PB 152 671
The effort expended during this period was directed to-
ward the production of Unit #1 and the preparation of
that unit for testing. The antenna, its mast, and erec-
tion equipment were fabricated and assembled. A delay
was experienced due to failure of the vendor to deliver
the coaxial switch as scheduled, necessitating a slip in
delivery data of the first unit. Upon receipt of this iten%
fabrication was completed and preliminary tests were
conducted. (Author)
[Hermes Electronics Co. ] Cambridge, Mass.
OVERTONE MODE FILTER CRYSTALS; by F. Earle
Clark. Quarterly progress rept. no. 1, 1 Nov 58-
28 Feb 59, on Contract DA 36-039- sc-78242.
28 Feb 59, 24p. 2 refs.
Order from LC mi|2. 70. ph|4. 80 PB 149 708
Spurious modes in the vicinity of the third thickness
shear over-tone of AT-cut crystals have been found to V
be more closely spaced and to have greater amplitude ,
than corresponding modes associated with the funda-
mental resonance. Temperature tests have been per-
formed on resonances in 40 Mc third overtone crysMlf
Data are Included on 40 Mc third overtone crystals of
four different diameters ranging from . 250" to. 500"
Hermes Electronics Cb. , Cambridge, Mass.
OVERTONE MODE FILTER CRYSTALS, by F. Earle
Clark. Quarterly progress rept. no. 2, 1 Feb-
30 Apr 59. on Contract DA 36-039-8C-78242.
30 Apr 59, 41p. 1 ref. AD- 226 571.
Order from LC mi|3. 30, ph|7. 80 PB 149 709
New electrode panems have been designed which mini-
mize the amplitude of these modes. Dita are included
on 40 Mc third overtone crystals with three different
electrode designs. Comparisons of mode configurations
are also made at six different electrode orientations.
(Author) (See also PB 149 708)
Hermes Electronics Co. . Cambridge, Mass.
OVERTONE MODE FOSTER CRYSTALS, by F. Earle
Clark. Quarterly progress rept.- no. 3, 1 May-
31 July 59, on Contract DA 36-039- 8C-78242. 31 July 59,
35p. I i^. AD-228 396
Order from LC mi|3. 00, ph|6. 30 PB 149 710
Data are included on 40Mc third overtone crystals with
eight different electrode designs. Comparisons of
electrical parameters are also made. (Author) (See
also PB 149 709)
Hughes Researcih Labs. . Mallbu, Calif.
EQUIVALENCE lETWEEN CONTINUCXIS AND DIS-
CRETE ARRAYS^ by A. Ksienski. Scientific rept.
no. 3508/7 on Cofitract AF 19(604)3508. 15 Apr 6a
23p. 5 refs. AFC}RL-TN-60-1104. "'
Order from LC iii$2. 70, ph$4. 60 PB 152 841
iii$i
The radiation patterns produced by continuous excita-
tion distributionsiaixi discrete arrays are compared,
and the conditiont are derived under which one type of
source may be substituted for the other with negligible
errors. It is shoivn that the aperture lengths in both
cases should be tpe same but the element spacing is
dependent on the type of pattern desired. Examples
are computed to (temonstrate these relations for both
directive panern^ and shaped beams. (Author)
International Bu$iness Machines Corp., Kingston,
N. Y.
THIN-FILM QRCUIT FUNCTIONS, by W . N. Carroll,
R. G. Counihan and others. Quarterly progress rept.
no. 3. 1 Feb- 30 Apr 60, on Contract DA 36-039-sc-
S4547. [1960] 12()p. 18 refs. AO-240 819.
Order from LC n|i$6.00. ph$18.30 PB 152 672
The selection of t^e as table multivibrator as the sixth
circuit to be fabricated, factors affecting layout of thin-
film circuits , machined masks , inductor fabrications ,
and the results ofi several preliminary circuit fabrica-
tions are described. Factual data is presented on ther-
mo-compression bonds . Initial results of thermal stud-
ies include a plotiof calculated steady-state isothermal
lines in the substh>te on one circuit. Fabrication tech-
niques and initial jenvironmental results are discussed.
Results are given! of further studies on the epitaxial
deposition of silioon by the silicon -iodine disproportion
ating reaction in a closed tube. Included in these stud-
ies were experiments with an inverted reaction tube
which showed tha< convection currents make the major
contribution to detoosition. Also described are steps
taken to reduce substrate etching during normal depo-
sition. The feasi^lity of co-depositing desired impu-
rities with silicoil was investigated and experimental
results are given on 2 methods of introducing impu-
rities . A description is given of several experimental
methods for the fabrication of multiple- layer junctions
The measured characteristics of fabricated diodes are
presented. The six final circuits are described with
detail circuit andllayout information. Equipment uti-
lized for fabricating the experimental models is de-
scribed and the results of the first fabrication runs tab
ulated . Initial results are presented from the Investi-
gation into dielectric materials . (Author) (See also
PB 150 808)
k)nosphere Research Lab. , Pennsylvania State U. , .
Universitv Park.l
EXPERIMENTAL LAND THEORETICAL STUDIES OF
IONOSPHERE ECHO POLARIZATION OVER THE
SWEPT FREQUEtlCY RANGE 50-1000 KC/S, by a N.
Carlson. Scientific rept. no. 139 on kxwspheric
Research, Contract AF 19(604)3875. 1 Oct 60, 44p.
8 refs. AFCRC-TN-60-683. AD-245 388
Order from LC mi$3. 30, phf7. 80 PB 152 823
When electron dertsity gradients are low enough, the
echo from the N «iN„ level is found to change from
left-handed to rigi)t-handed when the wave frequency l»
increased, as predicted theoretically. The N = N^
echo appears near the middle d the frequency range
and it is left-handed as expected. These echoes often
overlap and interfere. When the overlap is slight,
regular interference fringes appear as radiofrequency
is Increased permitting a determination at the virtual
height separation that agrees with, and is much more
accurate than, the virtual height difference as
measured by the time elapsed between reception of the
echoes. With extreme gradients, the E- layer echo
polarization is found to change from left-handed to
right-handed and back to left-handed just once with no
measureable increase in group height. It is shown that
a simple ionosphere model- -a step function- -is adequate
for a qualitative explanation of these changes in sense
of rotation. It was found that the polarization of E-
layer echoes frequently varies unsystematically. An-
tenna site effects can be ruled out as a cause of this
and an explanation is offered that requires echoes that
are double because of either high gradients or hori-
zontal inhomogeneities. (Author)
tonosphere Research Lab. , Pennsylvania State U. ,
University Park.
RAY THEORY ANALYSIS OF LOW FREQUENCY
lONOGRAMS, by Arthur Brunnschweller. Scientific
rept. no. 140 on Ionospheric Research, Contract AF
19(604)3875. 1 Nov 60, 40p. 10 refs, AFCRC-TN-
60-684. AD-245 389
Order from LC ml$3. 00, ph$6. 30 PB 152 824
The formation of low frequency ionograms is discussed
in some detail and it is shown that ray theory (assum-
ing zero collision frequency) is sufficient to explain the
high echoes sometimes observed. The appearance of
interference fringes between overlapping echoes is alto
described and an explanation given. A promising but
not yet fully tested method for the reduction of low
frequency ionograms is presented, including a dis-
cussion of the "valley" ambiguity. (Author)
Laboratory for Insulation Research, Mass. Inst, of
Tech., Cambridge.
IONIC coNDucnvrrv of silver iodide pel-
lets FOR SOUD- electrolyte BATTERIES, by
J. N. Mrgudich. Rept. on Contract Nonr- 1841(10).
June 59, 23p. 17 refs. Technical rept. 138;
AD- 219 686.
Order from LC ml$2.70, ph$4.80 PB 149 726
Silver amalgram electrodes were found to provide
polarization-free contacts for the measurement of the
ionic conductivity of compressed Agl powder pellets.
Correlation of the conductivity data with X-ray diffrac-
tion studies established the presence of a deformed
hexagonal phase as an important factor in determining
pellet conductivity. Deformation can be induced by
co.-npres8ion. Preliminary evidence is presented that
hexagonal deformation can be Induced by proper con-
trol of preparation or by suitable thermal or mechani-
cal pretreatment of the Agl powder. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
AN ADDITIONAI. CO>SIDERATION IN THE DESIGN
OF TRAVELING WAVE RESONATORS, by
S. J. Miller. Rept. on Contract AF 19(604)7400.
26 Oa 60. 6p. 2 refs. 46G-0007; AD-246 186.
Order from LC mi$ 1.80, phS 1.80 PB 153095
296
In an unpublished note, .'Griemsmann examines the
build-up time of a traveling wave resonator. It is the
purpose of this communication to develop the expres-
giona for build-up tin e following the work of Griems-
mann and to apply these results to some known or
planned situation.
Lincoln Lab. , Mass. Inst, of Tech. . Lexingtcm.
CURRENT OPERATED DIODE LOGIC GATE, by
H. Reinecke, Jr. Rept. on Contract AF 19(604)5200.
21 July 60. 43p. 9 refs. Technical rept. no. 226.
Order from LC mi$3. 30, ph^. 80 PB 152 750
The realization of switching functions using current-oper-
iteddiode logic gates, which employ the direction of cur-
rent as the binary variable, is presented. Two realization
methods are discussed. The dual method consists of a
set of rules which are ^nalogous to the procedures em-
ployed for the realization of voltage- operated circuits.
The lattice method is based on the transmission char-
acteristics of a lattice network of four series-connected
diodes. Either method is capable of realizing any arbi-
trary transmission function, although the number of
diodes required may be different. Hybrid networ)cs.
which combine the advantages of both methods, are de-
scribed to illustrate the versatility of current -operated
techniques. Practical design procedures are included to
guide the designer in theapplication of the realization rules
A static multiplier, capable of simultaneously multiply-
irf two 4 -bit binary numbers, was designed and built to
denxxistrate the practicability of current -operated di-
ode logic gates.' Approximately 270 diodes were re-
quired to construct thejtwenty gates used in the static
multiplier. Dynamic tests of the assembled system in-
dicated a reliable capability of 333. 000 multiplications
per second. (Author)
Lincoln Lab. , Mass. Inst, of Tech., Lexington.
CURVED-EARTH COMPUTATIONS FOR AIRBORNE
EARLY WARNING AND CONTROL, by N. I. Durlach,
A. M. Carpenter, and M A. Herlin. Rept. on Contract
AF 19(122)458. 13 Jan j59, I64p. 13 refs. Technical
rept. no. 194; AD- 210 006.
Order from LC nu$7.80, ph$25.80 PB 149 741
In analyzing the performance of airborne radars, one is
frequently faced with a problem in which the earth's
curvature is a significant faa that cannot be ignored
without introducing seijious errors. This is panicu-
larly true when, as in the case of an airborne search
radar, an appreciable amount of energy is incident on
the earth's surface. This report is a collection of all
the formulas that the authors have found useful in mak-
ing curved-earth computations, and of all the graphs
that have resulted from these computations. Both exact
and approximate formi^as are dealt with in the report
and different formulas 'for the same functions are com-
pared graphically to illustrate their relative merits.
The choice of- f un<;tions considered has been determined
by two distina problems: (a) plotting coverage dia-
grams and (b) locating the position of an enemy aircraft
bjr using the earth's surface as a reflector.
Lincoln Lab.. Mass. Inst, of Tech., Lexington.
DESIGN AND ANALYSIS OF CIRCUTTRY FOR A
MATCHED FILTER SYSTEM, by William A.
Petersen. Rept. on Contract AF 19(604)5200.
25 Aug 60, 3lp. 5 refs. 25G-0001; AD- 244 771.
Order from LC mi$3.00, ph$6. 30 PB 152 629
This report is concerned with the circuit requirements
of a Matched Filter System. The filters are 600micro-
second, 100-tap, acoustical delay lines. Herein pre-
sented is a general description of the system, its re-
quirements, and the design considerations and detailed
analysis of the transistorized circuits devised to meet
these requirements. (Author)
Lincoln Lab. , Mass. InsL of Tech. . Lexington.
EFFECT OF HIGHER SPATIAL MODES ON PRE-
DICTED MULTI CAVITY KLYSTROJ PERFORMANCE,
by R. L. Pease. Rept. on Contract AF 19(604)5960.
25 July 60. 13p. 7 refs. Technical rept. no. 227.
Order from LC mi$2. 40, ph$3. 30 PB 152 948
Bers' single- nKtde theory of multicavity klystrons has
been formally extended to include higher spatial nxxles;
in addition, simple approximate expressions have been
developed to show the effects of hi^er modes on pre-
dicted values of electronic conductance and over- all
gain. Comparisons have been made between formal and
approximate theoretical expressions for electronic con-
ductance, and between these expressions and experi-
mental values. (Author)
Lincoln Lab. , Mass. Inst, erf Tech.. Lexington.
EFFECTS OF FEED DISPLACEMENT ON PATTERNS
OF PARABOUC-CYLINDER REFLECTORS, by
R. L. Pease and J. Pease. Rept. on Contract
AF 19(604)5200. 2 June 60, 31p. 5 refs. Technical
rept. no. 224; AD-245 618.
Order from LC mi$3.00, ph$6.30 PB 152 949
A calculation is made of the central- section pattern of
a parabolic -cylinder reflector fed by a line source dis-
placed from, but parallel with, the focal line. Approx-
imate but specific results are obtained in the regions
close to the principal maximum and far out from the
principal maximum. Beam deviation factors are cal-
culated for these two regions and are found to differ
from each other. The effect of changing the feed pat-
tern on the values of beam deviation factors is also
found. Rough estimates are made of the accuracy of
the present calculations and of the loss of gain due to
feed displacement. (Author)
Lincoln Lab. . Mass. Inst, of Tech. . Cambridge.
SOLID STATE DISPLAY PANELS WITH PHOTOCON-
DUCTIVE CONTROL, by R. R. Billups. J. Rothstein,
and W. L. Gardner. Jr. Rept. on Contraa
AF 19(604)5200. 26 May 60. 30p. 21 refs. Technical
rept. no. 223; AD- 243 854.
Order from LC mi$2.70, ph$4.80 PB 152 409
299
A solid state diselay panel is basically composed of
two elements: oii which detects the incoming signal
and controls the voltage division and the other, a light -
emitting layer, which produces a visual display.
Panels utilizing Wintered photoconductive (PC) layers of
CdS and CdSe as detectors and electroluminescent (El.)
layers for the oi<put have been built. The over-all
performance andl consequently the possible applications
of such solid sta^e display panels are determined by
the electrical ani optical characteristics of the com-
ponents and the Extent of the optical feedback between
them. A single i|nified theory has been developed
which accurately! describes the observed character-
istics ol these display panels. Possible applications
have been explored with some success, but at the
same time limitations have been uncovered which
emphasize the fact that further improvements in the
materials are needed. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
TRANSWORO aT PORTABLE WORD GENERATOR
FOR USE IN MEASUREMENT OF BIT ERROR DIS-
TRIBUTION, by' William G. Schmidt. Repc on Contract
19 Oct 6a 9p. 2 refs. 25G-0019;
AF 19(604)74(X).
AD-245 232.
Order from LC r*>i$l. 80. ph$l. 80
PB 152 721
The reliability ol any digital data communications sys-
tem is a function in part, of the bit error rate of the
system; the error distribution is usually obtained by a
comparison technique in \»#iich a "word generator" is a
prime piece of tejst gear. This paper describes a
transistorized wdrd generator which has been designed
and constructed for the specific purpose of replacing
the electron tubej models with small, highly reliable
transistorized ut^ts which would facilitate field meas-
urement of erroi] distributions. (Author)
Lockheed Electtonics Co., Metuchen, N. J.
RESEARCH DIRECTED TOWARD DESIGN AND
DEVELOPMENT I OF EXPERIMENTAL DATA PROC-
ESSING EQUIPMENT, by M. W. Woodruff. Interim
scientific rept. oil Contract AF 19(604)6104. htov 60,'
96p. 12 refs. ARCRL TN-60-1133.
Order from LCiii$5.40, ph$15.30 PB 152 935
This Laboratory Is unique in that it houses a complete
and complex data; processing system which is employed
as a facility for i|esearch in information processing and
human decision. Essentially, the laboratory is a simu-
lation facility designed for the purpose of conducting a
program of studies in the field of aerospace surveil-
lance on problemjs which may be experienced at any
command and corltrol level. In this way, by means of
controlled experihients, problems related to threat
evaluation, actio* selection, and decision making can
be explored. Th^ facility is capable of pursuing
further research in other areas, particularly with
problems of air traffic control, ground control inter-
rp»*« "'««RiIe launch, and other types of comnrwnd
and control systetns using various equipment coiapo-
nent configurations. This report describes the tech-
nical Improvements and engineering developments
which have contributed to improved operational relia-
bility and flexlbiity, and which have enhanced the sys-
tem capability to
(Author)
simulate operational problems.
Melpar, Inc., Falls Church, Va.
TELETYPEWRITER GROUP AN/GGA-2(XW-1) by
C. F. Nojtunik and T. K. Parks. Final rept. phase 2
on Contract AF 30(602)1555. 6 Mar 59. 172p. 10 refs.
RADC TR-59-53: AD-213 783.
Order from LC mi$8. 10, ph$27. 30 PB 148 282
This report released for sale to the public 28 Dec 60.
The equipment is a synchronous transponder error-
correctfng device to be used in conjunction with
standard Air Force teletypewriter communications
facilities. The report contains a detailed description
of the developed equipment, test procedures, results,
conclusions and recommendations for future develop-
ment aaivity. (Author)
Michigan U. Research Inst. , Ann Arbor.
NONLINEAR ANALYSIS OF CROSSED-FIELD AMPU-
FIERS, by Om P. Gandhi and Joseph E. Rowe. Tech-
nical rept. no. 37 on Contract DA 36-039- sc -78223.
June 60, 48p. 8 refs. 2820-4T; AD- 243 196.
Order from LC mi$3. 30. ph$7 .80 PB 1 52 995
A general two-dimensional large- signal theory has beta
developed for the magnetron forward- wave amplifier.
This theory accounts for the effects of a number of
variables, including magnetic field, beam position, cir-
cuit loss and space-charge forces. The above theory
has been used to analyze the planar injection-beam
magnetron amplifier under a wide variety of operating
conditions. The effects of magnetic field, space-charye
forces and stream thickness on the gain are calculated
and discussed. Tlie space-charge fields are calculated
from the three-dimensional Green's functions for elec-
trons in a rectangular box and these are then simplified
to the two-dimensional case. The variation of the
space-charge field in the magnetic-field direction is
needed to analyze magnetron amplitiers with biperiodic
circuits. Solutions of the general nonadiabatic equa-
tions are calculated and compared with the adiabatic
solutions. A particular nonlaminar stream model it
investigated. (Author)
Microwave Associates, Inc. , Burlington, Mass.
HIGH REPETITION RATE BROADBAND IXJPLEXER,
by Emanuel L. Horn. Quarterly progress rept. no. 6,
15 Nov 59-15 Feb 60 on Contract DA 36-039- 8C-78165.
[I960) 22p. AD- 241 916.
Order from LC mi$2.70, ph$4.80 PB 152 6M
Measurements of arc loss and recovery time have beet
continued at low repetition rates. Tests performed wlfli
a quartz wafer type encapsulated window yielded the
lowest arc loss achieved to date of 2. 3% but with a
corresponding recovery time of 46 microseconds. The
test results also indicate that for equal values of re-
covery time at equal gas pressures, the quartz wafer
encapsulated window is 1 . 2% lower in arc loss than an
encapsulated window containing medium density quarti
wool. An investigation was also performed to deter-
mine the distribution of the "mechanical" losses as
opposed to the discharge arc loss of a mourned encap-
sulated window. The tests show that the discharge arc
loss is only a fraction of the total losses measured.
(Author)
300
Microwave Lab. , Stanford U. , Calif.
THE CENTIPEDE HIGH -POWER TRAVELING -WAVE
TUBE, by M. Chodorow, A. F. Pearce, and D. K.
Winslow. Rept. on Contract AF 30(602)1844. May 60.
53p. 8 refs. M. L. rejjt. no. 695; RADC TN -60- 201.
Order from LC mi$3.60, ph$9.30 PB 152 937
The design details and performance characteristics of
■n S-band high- power traveling- wave tube are pre-
•ented. Instead of a helix, this tube uses a periodic
microwave structure for the purpose of reducing the
electromagnetic wave velocity in the interaalon region
The coupling between the sections of this periodic
structure is obtained primarily by the negative mutual
inductance of the reversed loops. The large number of
coupling loops was thcbasis for the name "Centipede"
This type of coupling provides for a fundamental com-
ponent with a forward group velocity and a cold pass-
band of approximately forty per cent. Typical results
of the tube performance on the first model of the centi-
pede are as follows: saturated half power bandwidth of
slightly over 500 Mc centered at 2900 Mc (or about
18 per cent); peak power output of three megawans;
peak efficiency of 30 per cent; saturated gain of about
26 db. These results were for a pulsed beam at 130 kv
with a perveance of 1.65 x 10"6. Curves of the cal-
culated impedance, the gain parameter C, and the
small signal gain based on beam parameters and cold
test measurements are presented as are curves of
measurements of the tube performance. (Author)
s
Microwave Lab. , Stanford U. , Calif.
DETERMINATION OF ELECTRODE SHAPES FOR
AXLALLY SYMMETRIC ELECTRON GUNS, by
Kenneth ]. Harker. Rept. on Contract AF 30(602)1844.
Aug 60, 23p. 13 refs. M. L. rept. no. 733^ RADC
TN-60-202. AD-246 012.
Order from LC mi$2. 70. ph$4. 80 PB 152938
The determination of the electrode shapes for an elec-
tron gun involves solving Laplace's equation subject to
specified boundary values of voltage and normal field
on an open curve. Past attempts to solve this problem
fv the case of axial symmetry by mathematical meth-
ods have met with considerable difficulties because the
problem is improperly set and leads to unstable solu-
tioi)8. Following Garabedian, we have reformulated
the problem in such a manner that it becomes properly
set and applied it to a curvilinear space-cliarge limited
flow gun. First, a conformal transformation is made
which maps the beam boundary into a coordinate axis.
The second step, which constitutes the essence of the
method, is accomplished by making an analytic con-
tinuation of Laplace's equation and its boundary values
into a fictitious complex domain. Laplace's equation,
which is elliptic in the real domain, is thereby con-
verted into a set of hyperbolic equations. This leads
to a stable scheme of computation by finite differences.
This method should find particular application to
curvilinear flow guns, where the use of analogs, such
•8 the electrolytic tank, requires the use of involved
experimental techniques. This method is very general,
however, being applicable to any configviration where
die boundary conditions are given through analytic
funaions. If one desires, these specifications for the
boundary conditions may be given implicitly, as, for
example, through a set of differential equations.
(Author) I
Microwave Lab. , Sunford U. , Calif.
GENERAL STUDIES IN HIGH -POWER MICROWAVE
CONCEPTS. Scientific rept. no. 24, 1 Apr-30 June 6(J,
on Contracts AF 19(604)1930, AF 49(638)415. and
AF 19(604)5226. Aug 60. 32p. M. L. rept. nc. 745;
AFCRL TN-60-974.
Order from LC nU$3. 00, ph$6. 30 PB 152 847
Contents:
Investigation of the behavior of velocity modulated
electron beams in long gaps
Electron beam parametric amplifier
Crossed -field electron guns
Electrostatic beam type parametric amplifier
Electron beam interaction with a plasma
Plasma parametric amplifier
Plasma diagnostic techniques ^ y
Plasma confinement \^
Plasma studies
Thermal plasma
Noise in plasmas
Harmonic generation in plasmas
Cesium plasma tube materials and techniques
Ferrite nonlinear resonance
Ferrlle frequency multiplication
Microwave Research Inst. , Polytechnic Inst, of
Brooklyn. N. Y.
INVESTIGATION OF A CIRCULAR WAVEGUIDE
PERIODICALLY LOADED WITH STRAIGHT WIRES,
by M. Ettenberg and T. T^mir. Rept. on Contract
AF 18(600)1505. 15 Oct 59, I6p. 11 refs. Research
rept. R -782-59; PIB-7ia. AFOSR TN -59 -1298;
AD-230 730.
Order from LC mi$2. 40, ph$3. 30 PB 152 652
The investigation of the properties of a periodically
loaded line is described. This line, consisting of a
circular guide with straight wires loading, is shown to
be suiuble for linear accelerators and traveling -wave
tubes. The determination of the propagation character-
istic and other pertinent measurements is described.
The results show that the structure exhibits a funda-
mental slow backward harmonic, similar to the prop-
erties of an anti-Karp line. A discufesion on the influ-
ence of various parameters indicates how an appro-
priate propagation curve may be designed by suitably
proportioning the geometrical dimensions of the struc-
ture. (Author)
Naval Air Test Onter, Patuxent River. Md.
EVALUATION OF IMPEDANCE PLOTTERS, by
W. S. Bartels and F. B. Brown. Rept. no. 1 (Final) on
Proj. TED no. PTR EL 9008. 29 Apr 58. 26p. 1 ref.
Serial ET315-127.
Order from LC mi$2. 70. ph$4. 80 PB 152 833
Z-G Diagraphs, type ZDU (covering the frequency
range 30-300 mc) and type ZDD (covering 300-2400
mc), were designed and manufactured to measure im-
pedance, admittance, reflection coefficient, and trans-
mission characteristics accurately and rapidly. This
report is an evaluation of the capabilities of the Z-G
Diagraphs for use as antenna test equipment.
301
Naval Ordnancte Lab. , White Oak. Md.
THE SELF IMPEDANCE OP A QRCULAR LOOP IN
A CONDUCTINC MEDIUM, by M. B. Kraichman.
17 Aug 60. 13p 3 refs. NAVWEPS rept. 7290.
Order from OT^ $0. 50 PB 171 353
Integral exprea^ions are derived for the radiation re-
aiatance and exaenval self inductance of a circular loop
inuneraed in a conducting medium. These expressions
are evaluated fc^ the case where the radius of the loop
is much smallef than a medium wavelength. The radia-
tion resistance ^nd external self inducunce are ex-
pressed in termis of their values in air plus a correc-
tion term due tq immersion. Values at the correction
terms are plotted as a function of a loop-wave param-
eter. (Author)
Naval Research Lab. , Washington, D. C.
A CLOSED aRjCUrr TV system for passive USE
AT NlOfT, byC. T. Hicks and C. M. Whitfield, Jr.
Interim rept. 23 Nov 60, 18p. 7 refs. NRL rept. 5557.
Order from OT^ $0.50 PB 161 968
Experiments were performed with a closed- circuit TV
system designed for applications involving nighttime
viewing. Various lenses and recently improved TV
camera tubes designed for low light levels can be used
In the system. Aero-Ektar 24-inch f/6 and 12-inch
f/2. 5 lenses caii be used with the RCA C-73410 image
orthicon tube, t^ RCA C-73477 inuige intenaifier
orthlcon tube, df the General Electric Z-5294 image
orthicoa tube, and a 10- inch -diameter Schmidt optical
system can be used with the C-73477 tube. Information
is displayed in final form on a 10-inch monitor screen
at a luminance l^vel adequate for conventional photog-
raphy or for viewing without the necessity of prior dark
adaptation of th4 eyes. The system was tested under
low Ught level conditions on rocket flights, outdoor
scenes, stars, tnd a resolution chart. The highest
sensitivity was (ibcained with the Schmidt collector and
the C-73477 tubt, visibility thresholds being about the
same as for a d^k-adapted eye with a 7 x 50 binocular.
Tlie use c^ storage would increase the sensitivity be-
yond that at the jdark-adapted eye. Under these moon-
ll^t to starlight conditions, the pictorial results indi-
cate that these rtew camera tubes have a sensitivity in-
crease of 20 to iOO over studio-cype camera cubes.
(Author)
Naval Researcl Lab. , Washington, D. C.
HARMONIC DISTORTION IN AMPLIFIERS, by
S. R. Swanson aiid W. C Long, Jr. Interim rept.
17 June 52, decUsslfled 15 Dec 53. 15p. 12 refs. NRL
rept. 3998. |
Order from LC ^$2. 40, ph$3. 30 PB 153 576
This report released for sale to the public 6 Jan 61 .
T
To correlate nortlinear distortion with the various
parameters in vtcuum-tube circuits and to determine
methods for redi^ing this distortion, a theoretical
analysis, supported by experimental measurement,
was made of amplifier and cathode -follower circuits.
The analysis sh<tws that under certain operating con-
ditions minimun^ may exist for the various harmonics
in a vacuum-tub^ circuit. These minimums do not
ordinarily occur for different harmonics under identi-
cal operating conditions. Although measurements wen
made using oAK5 and 6C4 tubes at audio frequencies,
the analysis is also valid for broadband amplifiers at
higher frequencies. Curves obtained experimentally
illustrate the relation between harmonic distortion aod
such parameters as plate voltage, grid bias, and load
realstance. For a linuted range of operating condi-
tions, second- or third-harmonic distortion will drop
from an average value of several percent to less than
0.01 percent. (Author).
Naval Research Lab., Washington, D. C.
INTERMODULATION DISTORTION IN AMPLIFIERS,
by S. R. Swanson. Interim rept. 4 Sep 52, declassi-
fied 15 Dec 53. 14p. 4 refs. NRL rept. 4037.
Order from LC mi$2. 40. ph$3. 30 PB 153 577
This report released for sale to the public 6 Jan 61.
Two components of the distortion produced in a wide-
band amplifier, such as a receiver multicoupler, are
considered for the case when the input contains signals
at two or more frequencies. These components erf dis-
tortion are combination frequencies and cross modula-
tion. The combination -frequency (also known as sum-
and-difference-frequency) signals appear at frequencie*
which are the sum and difference of the input frequen-
cies and their multiples. It is shown that the amplitude
of these signals is related to the amplitude of the
harmonic distortion produced in a nonlinear amplifier.
With two input signals of approximately equal ampli-
tude, the combination -frequency signals will be several
times greater than the corresponding harmonics.
Croas modulation or crosstalk is a result of the de-
pendence of the amplification of one signal upon the
amplitude of another signal in a nonlinear circuit, and
causes modulation from one carrier to appear on
another carrier. This effect is approximately propor-
tional to the third- harmonic distortion produced by the
interfering signal and is practically independent of the
amplitude of the signal being interfered with. (Author)
Navy Underwater Sound Reference Lab. , Orlando,
FU.
AN IMPROVED NOISE- MEASURING HYDROPHONE.
USRL TYPE H32, by Claude C. Sims. 18 Oct 60, l5pi
USRL Research rept. no. 52; AE>-244 882.
Order from LC nUj2. 40, ph$3. 30 PB 152 979
A replacement hydrophone for the type DT-99/PQM-1A
noise- measuring hydrophone is described. The sensi-
tive element consists of a PZTS ceramic cylinder wldl
metallic diaphragms and "O" ring seals. The direc-
tional characteristics, signal -to- noise ratio, and sta-
bility with time are superior to those of the type
DT- 99/ PQM- 1 A hydrophone. (Author)
New York U. Coll. of Engineering. N. Y.
DIGITIZED MAXIMUM PRINCIPLE, by S. S. L. Chaa|,
Rept. on Contract AF 49(638)586. July 60, 9p. 6 refs.
Technical rept. 400-14; AFOSR TN-60-600; AD-245 9*
Order from LC mi$l. 80, ph$l. 80 PB ISSOJ*
302
I
The maximum principle of Boltyanskii, Gamkrelidze,
tnd Pontryagin for minimal time or maximal range con
trol of nonlinear continuous systems can be readily ex-
tended CO sampled- data systems. This note states and
derives such a digitized version of the maximum
principle.
New York U. Coll. of Engineering, N. Y.
OPTIMUM DESIGN OF PASSIVE- ADAPTIVE LINEAR
FEEDBACK SYSTEMS WITH VARYING PLANTS, by
Piml E. Fleischer (Doccoral chesis). Rept. on Concract
AF 49(638)586. Aug 60, 15p. 12 refs. Technical rept.
400-16; AFOSR TN-6a-748; AD- 245 997.
Order from LC mi$2. 40, ph$3. 30 n 153 035
In designing a feedback control system involving a var-
iable (or incompletely known) plant the prime considers
don, besides obtaining a satisfaccory transfer function,
it to specify a system which is insensitive co plant var-
iations. Some procedures for obtaining insensitive de-
signs have been described in che liceracure, but chey
•11 resulc in syscems having large open loop bandwidths.
In the presence of instrument noise such systems would
tend CO produce an excessive noise output. In this paper
s minimizacion is carried out, where che confliccing re-
quirements of small sensitivity to plant variations and
Inaensitivity co mscrumenc noise are satisfied simulta-
neously. The solution is approximate, buc can be Justi-
fied in most physical situations. A mechod for itera-
clag the solution is alap described. (Author)
New York U. Coll. of Engineering, N. Y.
RELIABLE FAIL-SAFE BINARY COMMUNICATION,
by J. J. Metzner and K. C. Morgan. Scientific rept.
BO. 2 on Contract AF 19(604)6168. 10 July 60, 76p.
40 refs. AFCRL-TN-6D-791: AD-245 253.
Order from LC mi$4. 50, ph$l2. 30 PB 152 791
A new binary decision -fAflback system is described
which is very effective forhigh reliability transmission
when the channel is subject to fading, intermittent
strong noise bursts, or other changing conditions. The
results presented suggest that this problem can be
solved by employing long codes with feedback, correct-
ing only very small numbers of errors, and utilizing a
new technique which effectively prevents any type of
disturbance in the feedback channel from harming sys-
tem reliability. Tlie resulting system yields excellent
reliability, "fails safe" (an error probability of 10" 10
when the signal-to-noiae ratio falls to zero, for in-
Mince). and operates it a relatively high per -symbol
iflfbrmation rate. This approach is particularly effec-
thre in precisely those situations where less efficient
procedures fail - namely, when severe burst-type
Dolee or heavy fading is encountered. TT»e cost of this
performance, in terms of computing and storage re-.
«Mirements, is far les» than that of comparable unidi-
rectional systems. (Author)
Pacific Semiconductors, Inc. . Culver City, Calif.
IKTRINSIC -BARRIER TRANSISTOR TECHWQUES
(SILICON) by J. L. Buie. M. Millea. and R. C Neville
(>itrterly rept. no. 10. 15 Oct 59-15 Jan 60. on Con-
tract DA 36-039-sc-74887. (1960) 25p. 3 refs. PSI
wpt- no. 300ft 15-25-Q; AD-240 261.
(Wer from LC mi$2. 70. ph$4. 80 - PB 152 659
IXiring the past quarter photo-resist techniques have
been applied co the processing of silicon mesa transla-
tors. Procedures are given for the photo-resist tech-
niques. These are found adequate to produce one -half
mil transistor electrode structures. A useful tech-
nique for study of transistor defects is given. By this
means a defective spot or spots on-a transistor may be
observed by local melting of a temperature-aenaitive
wax. Impurity diffusion techniques are discussed.
Some changes in prior processes are discussed with
resulting overall improvement. Gold diffusion is also
described. This technique has been intrcxluced into the
diffusion processing in order to control lifetime in the
transistor and observe effects upon device perfor-
mance. (Author)
Physical Science Lab. , New Mexico State U. ,
University Park.
AN INVESTIGATION OF LOOP ANTENNAS AND A
FEASIBILITY STUDY OF ANTENNAS SUITABLE FOR
THE DOFL MISSILE CONFIGURATION, by G. E.
Johnson. Rept. on Contract DA 49-186-502-ORD-708.
1 Dec 59, 99p. 10 refs. AD- 234 629.
Order from LC mi$5. 40, ph$15. 30 PB 149 647
Loop antennas designed on the basis of mode theory
developed by Dr. >jlius Herman. Diamond Ordnance
Fuze Laboratories, were tested and compared with
predicted results. Agreement between calculated and
measured values of impedance is good indicating that
mode theory is useful in predicting impedance of thin
loop radiators. The theory also allows design of large
uniform current loops for omnidirectional linear an-
tennas useful in directton finding-, arrays, and null
seeking systems. Results of testing various antenna
configurations on ten-foot missile forms to produce a
pattern directed forward along a missile axis but with
an on-axis null and low back and side lobe level are
given. An optimum pattern Is produced by an array of
2 antennas exciting the missile body as a long wire
radiator at approximately 300 mc. (Author)
Raytheon Co. , Waltham, Mass.
DEVELOPMENT OF COMMUNICATIONS REFLEX
KLYSTRON TUffi C^K725/QK645, by Sidney S.
Taylor. Final rept. for 25 Mar 57-31 Mar 59 on
Contract DA 36-039-8C-73I97. [1959] 36p.
Order from LC mi$3. 00. ph$6. 30 PB 149 629
The cavity, cathode and reflector spacing, and much of
the internal structure of the QK422 was changed to meet
the specifications of the (^K725. The output section
and the tuning mechanism were redesigned to meet the
QKIC725 requirements. Shock and vibration tests were
taken. TUner hystersls was improved. Dimensional
and tuning limits were measured. The electrical,
characteristics of the tube were evaluated. (Author)
Raytheon Co. , Waltham. Mass.
DEVELOPMENT OF X-BAND PULSE -TYPE MAG-
NETRONS QK674, QK675, QK70S. by S. Beese and
R. Giuliano. ed. Quarterly engineering rept. #2,
19 Jan-1 May 59. on Contract DA 36 -039 -sc- 78 150.
[1959] 17p.
Order from LC mi$2. 40, ph$3. 30 PB 149 630
303
This project coiicerns the development of three rugged
ized miniature X'band pulse magnetrons each capable
of generating a ^ak power output of 60 watts. Each
tube is to be methanically tunable through the fre-
quency bands shown below QK7CI5; 8900 - 9100 Mc.
QK674; 9100 - 9000 Mc and QK675; 9500 - 9700 Mc.
Anode dimensio^ were established and operable mod-
els of all three tintypes were constructed. The hot test
and environmental tests results indicate that the tube
designs will be able to meet specifications.
Rome Air Dev<lopment Center, Griffiss AFB, N. Y.
RADC RELIABILITY NOTEBOOK. SUPPLEMENT I.
1 Sep 60. 215p. 48 refs. (RADC-TR-S8-111, Sup. 1].
Order from OT^ $3. 50 PB 161 894-1
This revision of Section 8 of the basic notebook
(PB 161 894) supersedes the original section. It in-
cludes sections jn reliability fundamentals; essential
premises associated with reliability evaluation; rales
for establishing (risk values; part failure character-
istics; electron tubes; semiconductor components;
resistors; capacators; stress analysis for capacitors;
transformers, magnetic amplifiers, inductors and
coils; rotary eloctrical devices; ccxinectors; relays
and switches; wire and cable; low population parts;
procedural routine for failure-rate sunrimation; inter-
pretation of total failure rate from system viewpoint;
reliability specification and proof; classification of
failures; matheitiatical and physical basis for reliabil-
ity stress analyiiis; thermal aspects of equipment de-
sign; and comparison of calculated and observed
reliabilities.
Scnotone Corp . , Elmsford, N. Y.
STUDY OF SEALED NICKEL-CADMIUM BATTERIES,
by Irwin M. Schulman and Paul Ritterman. Quarterly
rept. no. 3, 1 Jjne-31 Aug 59, on Contract DA 36-039-
8C-78249. [l95Vl63p. 12 refs. AD- 229 738.
Order from LC mi$3.90. phWO.80 PB 149 693
The life cycling program was continued using D her-
metically sealed cells with varying concentrations and
amounts of electrolyte. Results are shown of periodic
capacity tests n^de during the cycling program. Posi-
tive and negativfe plaques were processed for the ex-
periment which will test the effects of cobalt addition to
the positive plaies, lithia addition to the electrolyte,
and the varying lof ^gative /positive capciaty ratios.
Charge and disqhafge dau are presented for a 3 plate
cell (2 negative j- 1 positive) in a sealed chamber under
pure oxygen atnl at 10, 25 adn 50 psig and under the
ambient atm. A revised progr^pi for reaction mecha-
nism study is presented. (See also PB 145 802)
Stanford
APPUED
EMISSION TUBtS
ress rept. no.
039- sc- 84526.
AD- 240 959.
Order from LC
A vacuum c
nnental srjdv of
Research Inst. , Menlo Park, Calif.
RESEARCH IN MICROMINIATURE RELD
, by W. W. Hansen. Quarterly prog
1 Jan-1 Apr 69, on Contract DA 36-
i*iy60, 34p. SRI Project 2937;
mi$3.00, ph$6.30
PB 152 670
Performance and defects of the manipulator have been
evaluated, and remedial measures proposed. A vac-
uum of about 5 X 10 mm was obtained during the fini
pumpdown and suggestions for improvement are made.
An emitter* tip was successfully maneuvered into one
hole of a lOOO-mesh screen, but emitter stability was
insufficient to warrant a detailed determination of con
irol characteristics. Theoretical studies of tube char-
acteristics were extended, and deflection of electrode
structures due to electrical fields was estimated.
(Author)
Sylvania Electric Products, Inc. , Seneca Falls, N. Y.
THE DEVELOPMENT OF THE LOW-HEATER-POWEI
CATHODE- RAY TUBE SC-2751, by George R. Kautz.
Final rept. for 1 July 58-1 July 59 on Contract DA
36-039-SC-78135. [1959] 108p. Rept. no. PSDS9-4;
AD- 231 127.
Order from LC miJ5. 70. ph$l6. 80 PB 149 712
The methods and techniques of fabricating a low- power
heater- cathode assembly were satisfactorily worked
out to a degree where limited volume production can be
accomplished. Isolation of heater and cathode is the
nnajor problem in the manufacture of tubes incorporat-
ing the low- power heater assembly. However, it was
demonstrated that approximately 60% of the assembliei
can be made with heater- cathode leakage within satis-
factory limits. The SC-2751 tube appears to meet all
design characteristic specifications. Revisions made
in specifications have resulted in an improved tube for
face plate quality, anode insulation, and equipment
adaptability. Some revisions in inside bulb contour in
the CD region are necessary to completely eliminate
neck shadow. It is expected that modifications now be-
ing proposed will be a satisfactory solution to this
problem. The final design of this low- heater- power
assembly operates at 1 .5 v - 140 ma -and 750'^C cath-
ode temperature. This assembly, with appropriate
mounting, is interchangeable with standard heater-
cathode assemblies in all normal types of cathode- ray
tubes. I . .. •
Syracuse U- Research Inst. , N. Y.
THE REPRESENTATION OF NON-UNEAR NET-
WORKS, by J. Blackman. Scientific rept. no. 1 on
Time Response Characteristics of Linear Networks and
Transformation Methods in Network Synthesis, Contrao
AF 19(604)6142. Aug 60. Up. 2 refs. AFCRL TN-
60-995.
Order from LC mi$2.40. ph$3.30 PB 152 9i6
The main purpose of this paper is to prove a theorem
which provides a theoretical background for approxi-
mating the performance of continuous, non- linear,
single valued networks. To do this an appropriate
mathematical framework is supplied and, incidentally.
a theorem is proved which demonstrates that the well-
known convolution integral which describes the per-
formance of a linear network is the consequence of «
few very general assumptions.
hamber and micro- manipulator for experi-
field-emission tubes is described.
^
304
Technical Research Group, Somerville, Mass.
DEFOCUSING OF PARABOLOIDS FOR MAXIMUM
TRANSFER OF ENERGY TO A RECEIVER IN THE
PRESNEL ZONE, by Alan F. Kay. Scientific rept.
00. 131-2 on Contract AF 19(604)5532. 29 Apr 60,
lip. I ref. TRG-131-RS-2; ERD-TN-60-782.
Order from LC mi$2. 40, ph$3. 30 PB 152 776
For the generafcase of aperture antennas it has been
ibown how to design the amplitude and phase of the
aperture illuminations of the transmitting antenna and,
in the case that there Is one, of the receiving antenna
in order to maximize the ratio Pr/Pj of power re-
ceived to power transmitted. The optimum illumina-
dons are ones which may often be accurately approxi-
mated by paraboloidal reflectors with defocussed feede
This report is concerned with the validity of this ap-
proximation, i.e. to wfiat extent can defocussed
paraboloids realize nearly maximum energy transfer.
I I
r
Trans-Tech, Inc., Rockville, Md.
IMPROVED FERROMAGNETIC BODIES FOR USE IN
MICROWAVE DEVICES. Final rept. for 15 Dec 56-15
15 Jan 59 on Contract DA 36-039-sc-73124. (1959J 56p.
AD-213 228.
Onterfrom LCmi$3.6p, ph$9.30 PB 153 226
Tie nickel -cobalt-copper-aluminium ferrite system was
investigated as a general study of materials for the mi-
crowave region below 3, 000 megacycles per second.
Cenain compositions from this system were also in-
veitigated as a gyromagnetic ratio study. Polycrystal-
line yttrium iron garnet comprising slight variations
from stoichiometric proponions were investigated.
Calcium oxide-silicon oxide substitutions were effected
in yttrium garnet in the hope of lowering the sintering
temperature. The lead hath method of growing single
crystals of yttrium iron garnet was investigated. A
reproducibility study was conducted and the effects of
different amounts of imjyjrity in the magnesium -manga-
nese ferrite are presented . Flame spraying equipment
was assembled and nickel ferrite, nickel cobalt ferrite
and ynrium iron garnet were prepared and compared
CO materials prepared by ball-milling. An evaluation
of the materials designed and fabricated under the sub-
ject contract is presented, based on electronic
measurement of pertinent microwave characteristics
and other characterizing measurements . (Author)
Willow Run Labs. , U. of Michigan, Ann Arbor.
m.ECTROLUMINESCENT-PIEZOELECTRIC PLAT-
fANEL DISPLAYS, by S. Nudelman, J. Lambe and
ethers. Rept. on Proj. Michigan, Contract DA 36-
039-8C-788O1. Oct 60, 13p. 1 ref. Rept. no. 2900-
202-T; AD-245 182.
Order from LC mi$2. 40, ph$3. 30 PB 152 536
A display panel consisting of electroluminescent phos-
phors deposited on piezoelectric crystals has been fab-
ricated for the purpose of providing a controlled lumi-
nescent light spot. The scheme of operation provides
for light -spot generation by using the electric fields
generated at the piezoelectric-crystal surface, when
the crystal is driven by voltages applied at the reso-
nant frequency. The panel is made up of crystals con-
nected electrically in parallel, but resonating at dif-
ferent frequencies. Light -spot sweep movement over
i ^ SO.'j
the face of the panel and intensity variation are de-
rived by frequency and amplitude modulation of the
voltage applied to the piezoelectric crysul array. The
device can be used immediately in the development oi
computer switches, character displays, luminescent
dials, delay lines, and any displays requiring limited
electric -field bandwidths. After additional phosphor
research, it may have uses in the development of TV-
like displays. (Author)
Ordnance, Missiles, and Satellite Vehicles
Aeronautical Accessories Lab. , Wright Air Develop-
ment Center, Wright -Patter son AFB, Ohio.
VAPOR CYCLE COOLING SYSTEMS FOR SPACE
VEHICLES, by T. D. Moseley. Rept. on Aircraft Air
Conditioning. July 60, 27p. 1 ref. WADD Technical
note 60-161.
Order from OTS $0.75 PB 171 345
Investigation of vapor cycles using freon 11 and cycles
using water as refrigerants for space vehicle cabin
cooling at approximately 75<>F and electronic equipment
cooling at approximately ISO^F revealed similar per-
formance in the two refrigerants, but due to the high
compression ratios required, water was undesirable.
Optimum total radiator area for the combination of
vapor cycle systems with necessary power units re-
sulted at 250OF to 325°F radiator temperature for
cabin cooling and 270OF to 350°F for elearonlc equip-
ment cooling (temperatures were based on & power ef-
ficiency of 20 percent and heat rejection or radiator
temperature of 700OF). High power unit efficiencies,
high power unit radiator temperatures, and high cool-
ing system Carnot cycle efficiencies reduced radiatcn-
area. (Author)
Air Force Missile Development Center, HoHoman
AFB, N. Mex.
AERODYNAMIC MEASUREMENTS ON TWO ROCKET
SLEDS ON THE HOLLOMAN TRACK COMPARED
WTTH THEORY AND WIND TUNNEL RESULTS, by
Hans J. Rasmussen. July 60, 54p. 14 refs. AFMDC-
TR-60-22.
Order from LC mi$3.60, ph$9.30 PB 152 743
Measurements of pressure distribution and of free run
drag coefficients were conducted during checkout runs
of two liquid propelled rocket sleds on the Holloman
Track. Data were obtained on a vehicle of hexagonal
body cross section with a pointed nose (R§-2 sled) at
free stream Mach numbers up to M =1.1, and on a
vertical wedge slab configuration with rounded leading
edge and flat bottom and top surfaces (AJ 10-33 sled) at
free stream Mach numbers up to M > 1.5. The results
are compared with theory and wind-Hunnel measure-
ments. The over-all agreement between sled measure-
ments and wind-tunnel data is good, and the general
trend is the same in both sled and wind-tunnel results
The flow characteristics around both configurations, as
revealed by these measurements, are discussed in
detail. Blockage effects observed on tlie RS-2 sled In
the vicinity of slipper beams and sway braces empha-
size the need for proper angular orientation of slipper
beam fairings with respect (o the local flow direction
and Indicate that pway braces are highly undesirable on
supersonic sleds^ Discontinuities in the pressure field
on top and bottom of the vertical wedge slab nose were
observed at transonic speeds. They were attributed to
changes in local Mach number distriburton, which are
induced by crossTflow effects from the side surfaces.
Free run drag cofefficients are compared with design
assumptions and wind-tunnel results. (Author)
Army Chemical
Army Chemicai
Research and Development Labs. ,
Center, Md.
GRENADE. HANp, IRRITANT, CN-DM. EI7RI, by
Woodrow W. Re^ens and Kenneth G. Carlon. Aug 60,
16p. 2 refs. CRDLR 3019: AD-243 461.
Order from LC iiii$2. 40. ph$3. 30 PB 152 597
An experiment wits conducted to determine ways to im-
prove the siabiliijy of the N46 grenade. Various designs
were inve8tigate4,in an attempt to develop a suitable
item that^ould ^ree with the military characteristics.
The most appropl'iate design consists erf a standard
MIS grenade can i containing two thin- wall metal canis-
ters for the Irritant mixtures. The canisters are I. 95
inches in length tnd 2. 281 inches in outside diameter.
The grenade is assembled as described below. An
asbestos gasket ^s placed on the bottom of the grenade
can. Above this is placed the CN canister so that the
exposed surface faces the bottom of the grenade casing.
A polyethylene d|8c is placed on top of the canister fol
lowed by anocherj asbestos gasket. The DM canister is
then inserted witji the exposed surface facing the top of
the grenade. £n<>ugh asbestos gaskets are then placed
on the DM canisOer to ensure a tight fit when the gre-
nade is bealed. The grenade is functioned with the
standard M201AI grenade fuze. Preliminary testing of
the above design gave satisfactory burning performanct
and storage stability. Surveillance was conducted at
140**F and 160°F|. It was determined experimentally
that intimate blends of CN, DM, and fuel mixtures were
not stable at elevated temperatures. Physical separa-
tion of fuel-CN akid fuel- DM mixtures in the munition
was determined 7o be the optimum method for producing
a satisfactory stibie munition. (Author)
Army Chen\lca
Army Chemica
IMPROVEMENT
Research and Development Labs. ,
Center, Md.
STUDY FOR INCENDIARY SAFE
AND EQUIPMENT DESTROYER, M2A1, by Woodrow
W. Reaves and Jt)hn J. Blissel. Aug 60. I2p. CRDL
Special pub. 1-21. AD-243 614.
Order from LC i ru$2. 40. ph$3. 30 PB 152 596
This report covers work conducted to Improve the
storage, handling, and functioning characteristics of
the M2A1 incend(ary safe and equipment destroyer.
Formulations containing a resinous binder. Laminae
4116. were investigated. (Author)
:^i
Army Chemicalj Research and Development Labs.
Army Chemical] Center. Md.
THE TECHNICAL FEASIBILITY OF UTILIZING THE
M5 HC SMOKE ?0T FOR LAYING SMOKE SCREENS
FROM LIGHT-WlEIGHT AIRCRAFT, by Mitchell E.
Penn. July 60. Ul). 1 ref. CRDL Special pub. 1-20.
Order from LC r u$2. 40, ph$3. 30 PB 152 595
The object of the work described in this report was the
investigation of the feasibility of using the M5 HC sntoke
pot for laying smoke screens from lightweight Army
aircraft. Two kits, which allow an M5 HC smoke pot
to be dropped from low-flying aircraft or moving vehi-
cles or trailers, were developed. The E2 modificatico
kit for the vehicular-dissemination snK>ke pot consists
of two aluminum end plates, appropriate tie rods, andi
bouchon fuze (M201 Al). The E3 modification kit for tbe
aircraft- mounted snwke pot is similar to the E2 kit,
except for the addition of two bomb lugs with sway
braces. It is feasible to use low-flying lightweight air-
craft or moving ground vehicles to lay pyrotechnic
snwke screens using ajjpropriately nnxlified M5 HC
smoke pots. (Author)
Arnold Engineering Development Center [Tlillahoma,
Tenn. ]
DRAG AND STABILITV DERIVATIVES OF MISSOJ
COMPONENTS ACCORDING TO THE MODIFIED
NEWTONIAN THEORY, by J. Don Gray. Rept. on
ARO, Inc. , Contract AF 40(600)800 S/A 11(60-110.
Nov 60, 33p. 2 refs. AEDC TN-60-191.
Order from LC ml W. 00, ph$6. 30 PB 153 058
The modified Newtonian approximation for the pressure
distribution on bodies in hypersonic flow has been used
to derive expressions for the zero- lift drag and the
inllial slopes of the normal-force and pitching- moment
curves. From the general expressions developed. •
set of working graphs are presented for blunted cones,
truncated cones, spherical segments, and rounded-
shoulder cylinders. From these graphs and the
appropriate equations, also given herein, the dragand
static- stability derivatives of composite missile con-
figurations may be readily estimated. (Author)
Ballistic Research Labs. . Aberdeen Proving Ground.
Md.
AN ALIGNMENT CHART FOR THE DIRECT DETER-
MINATION OF GUN CHARGES IN INTERIOR BAL-
LISTIC CALCULATIONS, by R. C. Strittmater.
Aug 60. 7p. 1 ref. Memo. rept. no. 1299; AD-245 205.
Order from LC mi$l. 80, ph$l. 80 PB 152 732
An alignment chart has been developed which eliminates
the process of iteration when solving for the weight of
gun charges in interior ballistic calculations. (Author)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
THE EFFECT OF ATMOSPHERIC PRESSURE ON
THE REFLECTED IMPULSE FROM AIR BLAST
WAVES, by W. C. Olson, J. D. Patterson. II and
J. S. Williams. Jan 60, 19p. 10 refs. Memo. rept.
no. 1241; AD- 234 998.
Order from LCmiJ2. 40, ph$3. 30 PB 149633
Measurements are reported of reflected impulses In
air blast waves generated by explosive spheres (up to
one pound in weight) detonated under reduced ambieit
pressures simulating altitudes up to 100,000 ft. (8 mm
of mercury). Analysis reveals that the data scale
according to Sachs' law. (Author)
306
Ballistic Research Lajjs. , Aberdeen Proving Ground.
Md.
HYPERVELOCFTY IMPACT BY COLUSION OF TWO
PROJECTILES, by Walter K. Rogers, Jr. and Walter S.
Vikestad. Aug 60, 20p. Technical note no. 1337;
AD-245 209.
Order from LC mi$2. 40, ph$3. 30 PB 152 729
A high collision velocity was achieved by firing a steel
pellet from a small light-gas gun at a target disc fired
from a large smooth-bore gun. The technique exploits
tbe use of existing equipment to reach hypervelocities
in a range where' the need for impact data is urgent.
This report discusses the technique, instrumentation
and results of the experiment. Collisions were pwe-
dicted with reliability and precision. The experiment
demonstrates the feasibility of adding significant target
velocity to many hyperveloclty launching techniques.
(Author)
Bliley Electric Co. . Erie. Pa.
PRECISION CRYSTAL UNTTS FOR SATELLITE USE,
by J. M. Wolfsklll, R. T. Schlaudecker. and Robert
Mouck. Quarterly progress rept. no. 3, 1 Jan-
31 Mar 60, on Contraa DA 36-039-8C-84556. [1960)
23p. 5 refs. AD- 240 687.
Order from LC mi$2. 70, ph$4. 80 PB 152 673
The fabrication of sample crystal units is continuing
with the inclusion of 100 mc and 111 mc units, and the
utilization of the fifth, seventh, and ninth overtone
mode crystals. The most difficult of the requirements
to meet proved to be the stringent maximum effeaive
resistance levels and the tight frequency-temperature
stabihty characteristics demanded, although the aging
rate requirement also poses severe problems. It was
found possible to fabricate fifth mode crystals which
will meet the 25 ohm reiquirement, and also to make
seventh mode crystals which will meet their 35 ohm
value. The latter is true only if aluminum plating is
utilized. Only a few of the ninth mode units were pro-
duced which could meet the specified 45 ohm level. It
was found that achievement of crystal units which can
hold the required * 2 x 10"" frequency stability over the
(fiC to 55°C operating t«mperature range can be
accuxnplished only by individual selection. Investiga-
tion has indicated that some distortion of normal tem-
perature characteristics occurs when crystals are
mounted in the special dual channel mounting. This
was traced to variations in the solder mounting.
Studies were made to determine the practicability of
influencing drift characteristics to improve yield by
controlled variations in the mounting. Work was ex-
panded to include evaluation of a parallel field excita-
tion technique to achieve high stability. Necessary test
equipment for this phase of work is described.
Dynamic Simulations Lab. , Ordnance Tank-
Automotive Command, Center Line, Mich.
MATHEMATICAL MODEL AND DIGITAL COMPUTER
PROGRAM FOR VEHICLE FIRING STABILITY
ANALYSIS (ACTIVE SUSPENSION) by Carole M.
Fischer. Rept. on Contract DA 20-089-ORD- 39246.
12 July 60, 82p. 2 refs. Rept. no. RR-27; AD-245 581.
Order from LC mi$4. 80, ph$13. 80 PB 152 845
This report describes the establishment of a mathe-
matical model and digital computer procedure for con-
ducting comprehensive firing stability studies of
vehicle mounted weapon systems. Program results
include vehicle vibration, acceleration, velocity, and
displacement dau at any time increment during tbe
application of the gun filing force impact. (Author)
Electro-Optical Systems, Inc. , Pasadena, Calif.
ALL SKY SURVEILLANCE SYSTEM FOR SATEL-
LITE DETECTION, by Peter H. Escher and Gunnar P.
Mlchelson. Rept. on Contract AF 19(604)4565.
25 July 60, I7ip. 4 refs. EOS rept. 290-final; AFCRL-
TR -60-407; AD-246 037.
Order from LC miJ8. 10, ph$27. 30 PB 153 100
The feasibility of an electro-optical Sky Surveillance
System affording hemispherical coverage for the ac-
quisition and tracking of unannounced satellites is es- ,
tablished. A design employing a detector mosaic in )
configuration with a scanning telescope is advanced.
In its first version, the design will be capable of ac-
quiring and subsequently tracking unknown satellites
displaying a brightness equalling a third order of mag-
nitude star or better. For relatively small additional
cost the same design can be enabled to detect objects
of the fifth or sixth stellar magnitude by a simple nu-
merical increase of detector cells within the detector
mosaic and a corresponding increase of preamplifiers
and decision making discriminator circuits. The out-
puts of the discriminator circuits are sampled by an
electronic commutator. Output pulses announcing the
presence of a urget and identifying which of the indi -
vidual cells within the detector mosaic has made the
acquisition are telemetered to the ground togedier with
telescope position information. This data, which may
be presented on a conventional PPI scope, will furnish
vector information of a satellite, hence will make the
esublishment of its orbital trajectory possible.
(Author)
Jet Propulsion Lab., Calif. Inst, of Tech. , Pasadena.
RADIATIVE PROPERTIES OF SURFACES CONSID-
ERED FOR USE ON THE EXPLORER SATELLITES
AND PIONEER SPACE PROBES, by W. S. Shipley and
T. O. Thostesen. Rept. on Contract DA 04-495-ORD-
18. 15 Feb 60, 31p. 6 refs. Memo. no. 20-194;
AD- 236 593.
Order from LC mi$3.00, ph$6. 30 PB 153 885
This report released for sale to the public 19 Jan 61 .
Spectral reflectance data in graphical form and absorp-
tance-emittance data in tabular form are presented
for surface materials considered for use on the Ex-
plorer satellites and Pioneer space probes. The sur*
faces ranged from bare aluminum, titanium, and
stainless steel to painted coatings, coatings of Rokide
A, and anodized and plated coatings. A brief review at
the temperature control problem is presented as back*
ground information. (Author)
KearfottCo. , Inc., Little Falls, N. J.
STUDY OF TESTING OF CONTROL SYSTEMS
UNDER SIMULATED ENVIRONMEJ^S. by S. L. Spira.
Final rept. on Contract AF 29(600)2059. Ai^ 60.
263p. 105 refs. AFMDC-TR-60-19.
Order from LCmi$I 1.10. ph$41. 10 PB 152 778
307
^
This report includes an analysis of ihc environments
that can be expected during stco-age, transportation and
tACtical operation) erf advanced flight vehicles. The
study carries through into nnethods of simulating these
envlronmems and| determination at their deteriorating
effects on control: systems as they affect the perform-
ance and structurtkl reliability. Thus, the environ-
ments include thej natural surroundings to be encount-
ered as altitude, {various radiations, ionized layers,
solid part4cle8, timperature and gravity. The induced
surroundings of shock and vibration are discussed in
relationship to materials, assemblies, subassennblies
and components of systems as well as the total sys-
tems. Material fatigue has been analyzed from the
beat information Available. The test devices for
simulating the entironments have been reviewed to
determine their effeaivlty in evaluation of hardware.
These simulation tools include rocket sleds, shakers,
bouncers, vibratdrs, cemrifuges, and temperature -
altitude chamber^- (Author)
Lincoln Lab. , Kjlass. Inst, of Tech. , Lexington.
AMPLrrUDE CAilBRATION FOR REENTRY PHYSICS
PROGRAM: ARBUCKLE NECK RADARS, by B. C Kuhr
Rept. on Contrao
21G-0015.
Order from LC nii$3.30, ph$7.80
AF 19(604)7400. 19 Sep 60. 44p.
PB 152 759
ircrift
Lockheed Ai
ON THE ORBITAjL
SATELLITES, b]
on Physics. July
AD- 240 909.
Order from LC 4^2. 40. ph$3. 30
(O,
SATELLITE
on
no
nri
Corp. , Sunnyvale, Calif.
PERTURBATIONS OF MARTIAN
Leighton F. Koehler. Technical note
I5p. 4 refs. U^SD- 703029;
PB 152 939
Lowell TechDokgical Inst. Research Foundation.
Mass.
POLAR
MENTS, by Carliisle
others. Rept.
Scientific rept
May 60, 68p.
Order from LC
PROPAGATION MEASURE -
Dieter, Kenneth JCinnard and
NSF Grant no. Y/32. 48/272 and
1 on Contract AF 19(604)4156.
AFlCRL TN-60-647: AD-244 582.
$3.90, ph$10.80 PB 152 522
The satellite receiving station at Thule, Greenland
and the electronic} equipment used there for receiving
and recording sattllite signals are described in detail
in this report. Tbe location of the Polar Laboratory
and the difficulties encountered in the operation of this
Artie Field Statical are presented. A comparison is
made of the system designed at the Lowell Technologi-
cal Institute Research Foundation which is now in-
sulled at Thule ard the older system used prior to
May 1959. This Report contains a complete descrip-
tion o* the LoweU Technological Institute Research
Foundation systeth which was used for all 1958 Delta II
recording since May 1959. A jweliminary analysis of
the data obtained from ThuJe is presented with sug-
gestions for futurte work. Phenomena such as around
the world transmissions or "ghoet signals", scintilla-
tion, doppler effe(a and Faraday Fading are discussed
in terms of the existing Thule data. Finally, a
procedure is outlined for the determination of the
parameters of th« satellite orbit at the point c4 closest
approach. Quantifies, such as height of satellite,
time of arrival aftd distance from Thule are
calculated. (Autlior) 306
Naval Ordnance Lab. , White Oak, Md.
SMEAR-CAMERA TECHNIQUES, by T. P. Liddiard, Jr
and B. E. Drimmer. 18 Aug 60, 2lp. 20 refs.
NAVWEPS rept. 7289; AD- 246 590.
Order from OTS $0. 75 PB 171 352
The various photographic systems and techniques used
at NOL and other laboratories in conjunction with
rotating-drum and rotating-mirror smear cameras are
briefly discussed, and typical samples are shown of
records obtained by such means. These techniques
greatly increase the usefulness of such sweeping- image
cameras in detonation and shock -dynamics research.
(Author)
Naval Ordnance Test Station, China Lake, Calif.
PROCEEDINGS OF THE SUPERSONIC TRACK SYM-
POSIUM [NO. 3] [HELD ATI CHINA LAKE. CALI-
FORNIA, SEPTEMBER 25-27, 1956. by James P. Judin.
Seminar repts. and abstracts. [1956) 39p. STS-3.
Order from LC mi$3. 00, ph$6. 30 PB 153 867
This report released for sale to the public 19 Jan 61.
Contents:
Track operation aftd development
Flutter atxj structural stability
Instrumentation and measurements
Escape systems
Sled engineering and design
ISTRACON
I
Naval Ordnance Test Station, China I^ke, Calif.
TRANSIENT TEMPERATURE DISTRIBUTIONS IN
ROCKET MOTORS WITH COMPLEX CROSS SECTION,
by P. A. Longwell. 1 Dec 59. 59p. 1 ref. NOTS
TP-2521; NAVWEPS rept. 7098; AD- 245 486.
Order from LC mi$3. 60, ph$9. 30 PB 152 826
A numerical method of calculation of the transient tem-
perature distribution in propellant grains having com-
plex cross sections is presented. Calculations for two
shapes of internal burning grains are included as ex-
amples, and the temperature distributions during
assumecTcuring cycles are given. (Author)
Remington Arms Co. , Inc., Bridgeport. Conn.
DEVELOPMENT AND FABRICATION OF PERCUSSION
PRIMER FOR BAG LOADED WEAPONS, by R. A.
Sahlin and R. L. Bescher. Monthly progress rept.
no. 4, Aug 60, on Contract DA 19-020-ORD-5200.
14 Sep 60. 5p.
Order from LC mi$ 1.80, ph$ 1.80 PB 152839
During this period a field test was conducted in a
175 mm gun at Yuma, Arizona on two prinier designa:
(1) Plcatinny basic design utilizing screw machine
parts; (2) Remington second alternate utilizing a single
drawn case with an external percussion primer.
Remington developed wrap-around primer which pre-
vents primer leakage. This design provides a simpli-
fication in manufacture and reduction in cost. (See
also PB 152 259)
Remington Arms Co. , Inc., Bridgeport, Conn.
DEVELOPMENT AND FABRICATION OF PERCUSSION
PRIMER FOR BAG LOADED WEAPONS, by R. A.
Sahlin and R. L. Bescher. Monthly progress rept.
DO. 5, Sep 60, on Contract DA 1 9 -020- OR D- 5200.
13 Oct 60, 5p.
Order from LC nrU$1.80, ph$1.80 PB 152 840
During this period work has continued on two primer
designs: (1) Plcatinny basic design utilizing screw
machine parts; (2) Remington first alternate utilizing
t drawn body and a drawn combination container and
ignition element with a staked closure cup and roll
crimp. (See also PB 152 839)
Republic Aviation Corp. , Farmlngdale, N. Y.
COMPARISON OF SPECIAL PERTURBATION
METHODS IN CELESTIAL MECHANICS, by
Samuel Pines, Mary Payne, and Henry Wolf. Rept. on
QMtract AF 33(616)6449. Aug 60, 56p. 9 refs. ARL
Tlechnical rept. 60-281
Order from OTS $1. 50 PB 171 337
The object of the investigation is to critically compere
commonly used numerical methods for orbit compu-
tadon. From the many methods available thefollowing
three were chosen: Cowell's method, Encke's method
and the methodkof Variation of Parameters. Instead of
comparing the methods against each other, with the
attendant difficulty in deciding which of differing results
ii the r.iore accurate, they were all compared with an
exaa solution of the problem of two fixed centers of
gravitation. These three methods and the exact solu-
tion are described. The results of the comparison lead
clearly to the conclusion that the Encke method is
superior in all respects to the other two for a problem
for which the classical two- body problem is locally a
good approximation. For other problems, a modifi-
cation at this method is indicated, rather than use of
the Cowell method .of the Variation of Parameters
method.
Str others -Dunn, Inc., Pitman, N. J.
DEVELOPMENT OF OPTIMUM RELAY STRUCTURES
FOR GUIDED MISSILES. byH. J. Cullin and
J. W. Bentz. Quarterly progress rept. no. 14, 1 Mar-
31 July 59, on Contraa DA 36 - 039 -sc- 64655. (1959)
25p.
Order from LC mi$2.70, pM4. 80 PB 149 704
The main effort during this interval has been directed
toward the successful 15 ampere resistive load switch-
ing. Silver -cadmium -oxide type contacts have failed
to perform consistently on 15 amperes but they do
•how good results while switching a 10 ampere load.
Silver -molybdenum has also been tested as a contact
but the results were unsatisfactory. Copper heat sink
fixed brackets with a thin si Iver- cadmium- oxide |f ace
were tried in an effort to provide better conduction of
the heat away from the contacting surfaces. With the
results of this test it was reasoned that this was not
the main problem.
Watertown Arsenal Labs. , Mass.
lALLISTlC EVALUATION OF NICKEL STEEL
PLATE AT LOW TEMPERATURE, by Charles W.
Amos. July 59. I4p. 3 ref*. Technical rept. no. WAL
TR711.2/1.
Order from LC mi$2. 40. ph$3. 30 PB 153 062
Thia report released for s^le to the public 28 Dec 60.
Two 3/8" -thick 9% nickel steel alloy plates that con-
form to ASTM A353 alloy steel were subjected to bal-
listic shock impact with yawed caliber . 50 AP M2 pro-
jectiles at a temperature of -165°C. The limited bal-
listic tests indicated that this special nickel steel ex-
hibited good ballistic shock properties at considerably
lower temperatures than those where brittle behavior
occurs with heat-treated^steels of the types employed
for sundard homogeneous steel armor, and at much
lower temperatures than where brittle behavior occurs
with low alloy high strength structural steels. The
impact transition temperature of ASTM A353 nickel
steel alloy is approximately -190%. (Author)
Watertown Arsenal Labs . , Mass .
IN-MOnON RADIOGRAPHY OF SERGEANT MISSILE
MOTOR CASING, by Ernest H. Rodgers . Rept on
Development of Renxtte X-Ray Inspection System.
Oct 60, 14p. Technical rept. no. WAL TR 140.5/1.
Order from LC mi$2.40. ph$3.30 PB 152 988
Work on the in- motion radiography project was per-
formed in an attempt to reduce the delay time resulting
from the use of conventional radiographic techniques .
The successful conclusion of the project resulted in de-
creased setup time, decreased exposure and processing
time, ease of interpretation and considerable inspec-
tional cost savings . (Author)
Sanitation and Safety Engineering
Naval Research Lab., Washington, D. C.
A DRY CHEMICAL SYSTEM FOR CARBON DIOXIDE
REMOVAL FROM SUBMARINES, by S. H. Smith, Jr.
Final rept. on one phase of problem. 23 Nov 60, 8p.
6 refs. NRLrept. 5563.
Order from OTS $0.50 PB 171 046
A system has been developed at NRL for the optimum
utilization of packaged dry chemical CO2 absorbers, to
replace the current use of bulk quantities of loose ab- ^
sorbent. In thia system, a self-enclosed filter-blower f
apparatus holds five canisters, each with six [xxinds of
lithium hydroxide. Under normal conditions, the unit
will absorb the CO2 produced by 35 to 40 men over an
eight-hour period. The most recent version of this
unit is commercially designed and appears ready for
fleet use. A concurrent investigation was made of the
value of lithium hydroxide as compared with commer-
cial sodallme as a CO2 absorbent aboard submarines,
using the filter-blower apparatus. Lithium hydroxide
was found to be, as expeaed, substantially more
efficient as an absorber of C02> with a capability of
absorbing about 85 percent of its own weight in CO2,
as compared with atxxit 40 percent for sodalime.
(Author)
Naval Research Lab. , Washington, D. C
REMOVAL OF ORGANIC CONTAMINANTS FROM
AIR BY TYPE 13X MOLECULAR SIEVE, by
P. Gustefson and S. H. Smith, Jr. Pinal rept. on this
phase. 6 Dec 60, 19p. 10 refs. NRL rept. 5560.
Order from OTS $0. 50 PB 171 051
f-
ao9
The adsorption ^f low concentration* of n-decane,
methane, foenze»e. toluene, xylene, pyridine, aniline,
and nitrobenzeni on type 13X Linde molecular aieve
has been studied at influent concentrations of from 5 to
over 100 ppm and superficial linear velocities (veloci-
ties if no sieve were present to reduce the cross sec-
tion) of up to 30()0 cm /minute. The breakthrough weight
capacity at a flow rate of 2500 cm/minute for a repre-
sentative aliphatic compound (n-decane) was 10 wt-%of
the sieve and fofa mononuclear aromatic (benzene)
was 0. 35 wt-% it 25°C. Decreasing the flow rate of
the aromatic to BOO cm/minute increased the break-
through capacit]j to 2. 15^. Regeneration conditions
were also studi^. Water vapor readily displaces
organic adsorbsies (except high boiling polar com-
pounds) at rooiT^ temperature. Therefore, molecular
aieve with coad4orbed water may be reactivated by
passing dry air lat 200^ to 3250C in the same direction
of gas flow as that used during the adsorption cycle.
The coadsorbed water will displace the sorbed organic
compounds as H moves down the column, whereas the
organic materiiis would be pyrolyzed in place if the
here. (Author)
FOOD, HANDLING, AND PACKAGING
EQUIPMENT
water were not
Ship Buildihg
Etevid Taylor ] ifodel Basin, Washington, D. C.
MODEL EXPERIMENTS ON THE EFFECT OF A
BULBCXJS BOW bN SHIP SLAMMING, by Kazuo Oclii.
Oct 60, 35p. 6 teta. Rept. 1360.
Order from LC|mi$3.00. ph$6.30 PB 152 734
This report pre^nts the results of model experiments
to determine th* effect of a bulbous bow on ship slam-
ming. The experiments were conducted on two 5. 5-ft
models: one. thte MARINER, had a bulb whose area was
4 percent of the midship area: the other, the modified
MARINER, had the same principal dimensions as the
mArINER but h^d no bulb. Based on the experimental
results, a comparative evaluation is made of the effect
of the bulb on slamming. It is found that the differences
between the MAFINER and the modified MARINER are
not as large as bad been expected. The MARINER ap-
pears to be superior to the modified MARINER at
speeds less thati 1.5 knots (14.7 knots full scale) and
inferior to the rtKxlified MARINER at speeds above
2.0 knots (19.6 knots full scale). (Author)
Naval Engineering Experiment Station, Annapolis,
Md. I
A BIBLIOGRAPJfY AND ABSTRACTS OF REPORTS
ON RESILIENT MOUNTINGS, by Paul J. Shovestul.
25 Mar 59. 56p, 55 refs. E.ES. rept. 820052:
AD- 21 5 988
Order from LC mi$3. 60, ph$9. 30 PB 153 793
This report rek^ased for sale to the public 18 Jan 61.
This publicatioi^ is a bibliographical review of all
Engineering Ex^riment Station reports that have been
published to datp covering the development, investiga-
tion, and evaluation of resilient isolation mountings.
The publication provides abstracts of each technical
report issued Ci mcerning the isolation characteristics
of specific resilient nKHints.
»,».■■
.^' .'i'
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
WJTWTIONAL REQUIREMENTS OF TR(X>PS STA-
TIONED IN ALASKA, by Kaare Rodahl. June 55, lOTp
81 refs. ProJ. no. 7-7954, rept. no. 1.
Order from LC ml$5.70, ph$16.80 PB 153 339
A series of nutritional surveys , together with detailed
clinical, physiological and biochemical examinations
was carried out among a group of airmen and a group
of Infantry soldiers during the four seasons of the year
at Ladd Air Force Base in Alaska from 1950 to 1952.
Simultaneously, similar studies were made among (our
groups of Eskimos for comparison. Individual food
weighings showed an average gross consumption of
3,000 calories per man per day in the Air Force group
and 3,200 calories in the infantry group. These find-
ings are in striking contrast to figures previously pub-
lished for caloric requirements of troops stationed in
Alaska but are in agreement with studies among
Eskimos and trappers in Greenland.
MACHINERY, FABRICATION, AND
ACCESSORY EQUIPMENT
Engines and Propulsion Systems
AeroChem Research Labs. . Inc. , Princeton, N.J.
SOME NOTES ON HIGH SPEED MEDIUM PROPUL-
SION, by John B. Fenn. Rept. on Contract Nonr-
2773<0O). Mar 60, 20p. 10 refs. Technical memo,
no. 21; AD-238 972.
Order from LC mi$2. 40. ph$3. 30 PB 148 777
There is a class of propulsion engines which depend
upon the medium through which they fly for lian of
their working fluid. Under sonr>e conditions , they can
also derive some of their energy from this medium.
Air breathing engines are familiar members of this
class . This study explores some of the implications of
very high speed flight for these "medium propulsion"
devices . A simple analysis based on energy, mass and
momentum conservation is developed No dependeace
upon particular mechanisms or processes is presumad
The following conclusions are reached: (1) As flight
speeds are increased, the thrust yield per unit energy
carried aboard the vehicle rapidly reaches impracti-
cally small values . (2) The yield in thrust from ex-
haustible stored mass rapidly increases with flight
velocity. (3) In the range of achievable flight velociti«
simple mass addition to the exhaust stream without
any energy addition can result in values of specific im-
pulse comparable with the best chemical rocket pro-
pellants . (Author)
Air Force Inst, of Tech. , Wright -Patterson AFB,
Ohio.
THE FEASIBILITY OF THE NUCLEAR POWERED
ION PROPELLED SPACE VESSEL, by Donald McRae
Mixson. Master's thesis. Mar 57, 95p. 20 refs.
GNE [571-5; Technical rept. 57-4.
Order from LC mi$5.40, ph$15.30 PB 153 517
This report released for sale to the pubhc 16 Jan 61.
310
Tlie feasibility of the ion rocket is investigated in terms
of its destination (Mars) and in terms of the ratio of
payload to total ship masq. In order to achieve some
perspective, the capabilities of the ion rocket are com-
pared with those of chemical rockets. Assuming a
iQO-ton rocket under power for 114 days, it is deter-
mined that the ion accelerating potential must be
25,000 volts. With the ion acceleration efficiency
established, the output of the DC generators is known,
tnd the mass of these generators calculated -- assum-
ing the substitution of aluminum for the generator
copper. Once the input to the DC generators is known,
die heat transfer system ija investigated. The results
of these calculations show* that the 100-ton ship is
feasible. The results are'then scaled up for a rocket
of 3(X) tons total mass.
\
Biomedical Lab. , Wright Air Development DiV. ,
Wright -Patter son AFB, Ohio.
EFFE(JrS OF VARIOUS EXHAUST BLAST DEFLEC-
TORS ON THE ACOUSTIC NOISE CHARACTER-
ISTICS OF 1,000-POUND^THRUST ROCKETS, by
John N. Cole, Roben T. England, and Robert G. Powell
Rept. on Definition and Modification of Acoustic and
Vibrational Environments. Sep 60, 65p. 12 refs.
WADD Technical rept. 60-6.
Order from OTS$ 1.75 i PB 171 308
The sound field produced by rocket engines is affected
by exhaust blast deflectors used in test and launch site
operations. Whether or not these deflectors affect
only directivity of noise radiation or also affect total
acoustic power has been unanswered. Results of a
blast deflector study using a 1,000- lb-thrust solid
propellant rocket and scaled models of several types oi
deflectors are presented. Changes in acoustic power
spectra, directivities, and near-field sound pressure
level distributions derivec| from the study are included.
Evaluations of a number of model diffuser noise sup-
pressors designed for this 1,000- lb-thrust rocket and
limited informanon on the acoustic effects of firing
these rockets into water tanks with and without under-
water blast deflectors are reported. Results indicate
total power radiated can be ajppreciably reduced to
varying degrees with the different deflectors (maxi-
mum total power level reduction of 8 db). However,
almost all devices causedjincreases in the sound pres-
sure level at near-field positions where the missile
striKture itself is located! Additional modification of
the noise distribution at these near-field locations
would be desirable to benefit from the achievable total
PWL reductions. (Author)
Defense Metals Informal^ Center, Battelle
Memorial Inst., Columbus, Ohio.
ROCKET -NOZZLE TESTING AND EVALUATION, by
E. W. Ungar. [Rept. on Oontract AF 18(600)13751.
7 Dec 60, 17p. 3 refs. DN|IC memo. 77.
Order from GTS $0. 50 P3 161 227
This paper is concerned with the testing and evaluation
of nozzles for solid- prope(lant rocket engines. Repro-
ducibility of test results i4 discussed first. Then, the
general problem of simulation of nozzle exposure con-
ditions is covered. Finally, as an example of a
Emulation study, the results of a study uf small-scale
wazle aimulation are presented.'
Diamond Ordnance Fuze Labs. , Washington, ^D. C
STATUS OF DOFL FUEL CELL PROGRAM ON
1 OCrrOBER 1960, by H. F. Gibson. 24 Oct 60, 13p.
7 refs. Technical rept. TR-891; AD- 245 220.
Order from OTS $0.50 PB 171 050
The objective, a brief history, the organization, and
status of the DOFL fuel-cell program are given. The
program represents the current Ordnance fuel- cell
effort. The status of each of the different tasks is
indicated along with brief statements of recent findings.
References to details of the technical work are given
for each task. References are given also to some other
publications related directly to electrical vehicle
propulsion. (Author)
Hesse-Eastern Div. , Flightex Fabrics, Inc.,
Cambridge, Mass.
IMPROVEMENT OF HYDRODYNAMIC TEST MA-
CHINE FOR ROCKET MOTORS, PARTS 1 AND II, by
Paul V. Choate. Final summary rept. pts. 1 and 2 on
Contraa DAI 28-017-501 -ORD(P)- 1872. [1958] 181p.
AD-144 442.
Order from LC mi$8.40, ph$28.80 PB 153 272
Research was conducted to provide an improved ver-
sion of an established dynamic impact machine for use
as a test device in the modification of current and de-
sign of future unfired pressure vessels for use as
rocket motors; and to coixluct metallurgical studies on
3.5-in. rocket motor bodies (namely, the M-28A2
HEAT rocket) to ascertain the possibility of reducing
certain mechanical requirements presently incorpo-
rated in standard Ordnance drawirtgs. The hydrody-
namic test machine co.nsist8 essentially of an energy
source and a high pressure hydraulic system which
converts the energy released from the source into the
desired pressure-time cycle. The energy source (air
gun) consists of a single stage, piston-type air com-
pressor; an air storage tank ca[>able of withstanding up
to 125 psi air pressure: an acceleration tube or barrel;
a slug; and appropriate valves to control the flow of air
from the storage tank. Hydrostatic, hydrodynamic,
and static firing tests were completed with the M28
motor made during the modification program of the
hydrodynamic impact machine. This machine was
evolved into a laboratory instrument which, through
modification, may have the following uses other than
that for which it was designed: (1) pressure gage cali-
bration, (2) hydrodynamic test of shell cases, and (3)
test for strength of joint.
Jet Propulsion Lab., Calif. Inst, of Tech. ,
Pasadena.
MOLLIER DIAGRAMS FOR THE HYDROGEN-OXY-
GEN SYSTEM AND EXPERIMENTAL RESULTS OF
TESTS ON A ROCKET MOTOR OF 500- POUND
THRUST, by Dwight I. Baker. Rept. on Contract
DA 04-495-ORD-18. 4 May 59, 114p. 12 refs. Rept.
no. 20-127; AD- 228 095.
Order from LC mi$6.00, ph$18.30 PB 153 791
This repori released for sale to the public 18 Jan 61.
Th-' results are presented of experimental and analyti-
cal investigations of hydrogen and oxygen. Combustion-
product properties and performance data for various
311
mixture ratios ai|e given. Tests were conducted using
water-cooled motors, and test results on a 100- lb-
thrust motor areicompared with test results on a 500-
lb-thru8t motor. Chamber pressures to 839 psia were
obtained, and motors of 5.7- to l37-in. characteristic
length were used* MoUier diagrams which were pre-
pared from the theoretical data of hydrogen and oxygen
are included in i^. A. Corrections of the MoUier dia-
grams for recent
Plasma Propuls.on Lab. . Republic Aviation. Corp
Farmingdale,
OPTIMUM CAPAfclTOR
SPACE system:;
Neuringer, and
Nonr-2851(aO).
Order from LC
CHARGING EFFiaENCY FOR
by Philip M. Mostov, Joseph L.
inald S. Rigney. Rept. on Contract
Jan 60, 33p. II refs. PPL -TR -60-2.
iiii$3. 00, ph$6. 30 PB 152 749
[tor
12
data are given in App. B. (Author)
In space systems the efficient utilization of energy can
be critical. Many pulsed operation devices, e.g., a
plasma engine, involve charging a condenser periodi-
cally. The efficiency of energy transfer (>'*) to an ini-
tially uncharged condenser (C) when a DC source volt-
age is applied th rough a resistance (R), with inductance
(L) assumed zero, is shown limited to 50% even if R
varies arbitraril ^ during the charging process. If
L>0, ,/ can be r lade to approach 100% by charging in
a periodic mode and terminating at the end of the first
1/2-cycle. The requisite L, which is a function of R,
C, and charging Itime T, can be formidable and its
weight large. T<> provide guide lines in the selection
of practical volt4ge shapes, the Calculus of Variations
is used to dertvd theorems for the "perfect" time-
ahaped source v
live red energy.
< iltagfes,that optimize o when the de-
^, C and T are fixed. (Author)
Rocketdyne,
ANALYTICAL
R. H. Boden.
AF 49(638)649.
rept. 60-279.
Order from OTS
Cinoga Park, Calif.
SrUDIES ON ION PROPULSION, by
R((pt. for July- Dec 59 on Contraa
Aug 60, 77p. 30 refs. ARL Technical
Analyses ctf majfr
nents of the ion
Component
systems, thermal
electrode
namics, propella
working fluid foi
using low-thrust
tion of these
sign parameter
Space Sciences
delphia, Pa.
EXPERIMENTAl
ENTRY COAXlAjL
APPLICATIONS
and P. Gloersen
Oct 60, 23p. 4
R60SD456. AD-
Order from LC
The performance
plasma accelerator
$2.00
PB 171 305
problems associated with compo-
jocket engine system have been made,
studips include elearical power generation
power conversion, and accelerating
configiirations. Analyses of ion beam dy-
nt materials, radiation damage to
a nuclear power plant, and missions
vehicles are presented. Interpreta-
is made in terms of engine de-
(Author)
ana lyses
Lab. , General Electric Co. , Wiila-
PERFORMANCE OF A PULSED GAS
PLASMA ACCELERATOR AND
TO SPACE MISSIONS, by B. Gorowitz
Repc. Oil Contract AF 04(647)269.
s. Technical Information Series
788. V
i^i$2. 70, ph$4. 80 PB 152 959
2*5
of a pulsed gas entry coaxial type
has been evaluated by several ex-
perimental techniques. Impulse, kinetic energy, spe-
cif icimpulse. mass flow, and propellant species were in-
vestigated for single pulse operation of the accelerator
fired Into an oversize test chamber pumped down to a
pressure d 10*6 mm of Hg. Kerr Cell photography d
the luminous plasma exhaust indicated a high ratio of
unidirectional kinetic energy to thermal energy in the
plasma exhaust as demonstrated by the small a mount of
lateral spreading of the plasma in the oversize test
chamber. With 4500 joules stored in the capacitor bant
the performance of the accelerator is as follows: The
calorimeter measurements indicate that at least 25% of
the energy originally stored in the capacitor appears at
unidirectional kinetic energy in the plasma exhaust
(1 125 joules). The impulse delivered to the ballistic
pendulum under these conditions was 3950 dyne-seconds
The time-of -flight measurements indicate an average
specific impulse of 6000 seconds, in agreement wichthe
specific impulse deduced from the impulse and kinetic
energy measurements. Rotating mirror camera rec-
ords show that initial portions of the plasma emanate «
a specific impulse of 30, 000 seconds but that subsequent
portions emanate at a specific impulse of 6000 seconds
Sundstrand Turbo Div. . Sundstrand Corp. , Pacoima,
Calif.
STUDY OF TURBINE AND TURBOPUMP DESIGN
PARAMETERS. VOLUME I. A STUDY OF HIGH
PRESSURE RATIO RE-ENTRY TURBINES, by Hana
D. Linhardt. Rept. for 1 Feb 58-30 Jan 60 on Contract
Nonr- 2292(00). 30 Jan 60, 154p. 18 refs. S/TD No.
1735; AD- 232 635.
Order from LC mi$7. 50, ph$24. 30 PB 152 85<>-l
The design point analysis of two-stage, axial re-entry
type turbines is presented for the case of low weight
flow and high over -all pressure ratios. The optimum
pressure split between both stages is investigated ap-
proximately by evaluating the optimum performance
for two-stage re-entry turbines with equal heads or
equal pressure ratios In both stages. The optimum
efficiency for both pressure splits is analyzed and a
theoretical method of determining the detailed design
criteria is presented for each optimum design. The
method of analysis is substantiated by test of a two-
suge re-entry turbine designed according to the analy-
sis. Deviations from this analysis were found to be
caused by increased leakage and off -design perfonti*
ance of the second -stage nozzle. (Author) (See also
PB 150 834) I
Sundstrand Turbo Div., Sundstrand Corp. , Pacoima,
Cahf.
STUDY OF TURBINE AND TURBOPUMP DESIGN
PARAMETERS. VOLUME II. A. STUDY OF HIGH
PRESSURE DRAG TURBINES USING COMPRESSIBLE
FLUIDS, by Robert Spies. Final rept. for 1 Feb 58-
30 Jan 60 on Contract Nonr -229 2(00). 30 Jan 60, 61 p.
4 refs. S/TD No. 1735; AD- 232 636.
Order from LC mi$3.90, ph$10.80 PB 152 856-2
The simplified drag-turbine theory presented by Balje
(Trans. ASME, Aug 57, p. 1291) has been extended to
cover the case of a compressible gas in a turbine of
arbitrary area distribution. Conclusions regarding
superior jjerformance when an expanding channel is
used have been verified and areas of future invcstig**
312
dons indicated. The attainable efficiency of a large
pressure -ratio drag-turbine is high with values of 44
percent anticipated In future designs. (Author) (See
alsoPB 152 856-1)
Sundstrand Turbo Div. , Sundstrand Corp. , Pacoima,
Calif-
STUDY OF TURBINE AND TURBOPUMP DESIGN
PARAMETERS. VOLUME III. LOW SPECIFIC SPEED
TURBINES BASED ON TANGENTIAL FLOW THEORY,
by Michael Dubey. Final rept. for 1 Feb 58-30 Jan 60,
on Contraa Nonr- 2292(00). 30 Jan 60, 108p. 7 refs.
S/TD No. 1735; AD- 232 637.
Order from LC miJ5.70, ph$l6.80 PB 152 856-3
The tangential flow theory for drag turbines, as pro-
posed by D. H. Silvern, stipulates that a recirculating
flow mechanism for harnessing the energies available
in a working fluid can be expressed by Euler's equa-
tions, with minor corrections for friction forces. The
significant equations of Silvern' s theory are used to
design a test turbine which successfully demonstrates
that the desired flow pattern can be established. The
corresponding high efficiencies predicted by the analy-
sis are also attained. These turbine efficiencies are
considerably higher than (hat possible for single stage
axial flow, terry, or drag turbines operating at the
aame very low specific speeds. By using the loss co-
efficients inferred by the test data, an NgOg diagram
is derived indicating the maximum efficiencies attain-
able with optimized design parameters. The effects of
geometry ratios on performance are also discussed.
(Author) (See also PB 152 856-2)
Manufacturing Equipment and Processes
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
REVIEW OF SOME UNCONVENTIONAL METHODS
OF MACHINING, by Francis W. Boulger. (Rept. on
Contract AF 18(6QP)1375]. 29 Nov 60. 20p. 60 refs.
DMIC memo. 75.
Order from OTS $0. 50 PB 161 225
The portion of a review covering the principles and
applications of four electrical machining techniques, as
well as some information on chemical and ultrasonic
methods, is presented in this memorandum as an aid
to defense contractors in planning manufacturing
operations.
Microwave Research Inst. , Polytechnic Inst. ,
Brooklyn, NY.
DIES FOR FORMING FERRITE PARTS, by H. Hanft
and L. Silber. Rept. on Contract AF 30(602)2135.
19 July 60, 9p. 1 ref. Research rept. PlBMRI-831-60;
RADC-TN-60-199; AD- 245 072.
Order from LCmi$ 1.80, ph$1.80 PB 152 724
A method for making dies for compression molding of
ferrites is described. This technique lends itself to
shapes such as those with rectangular holes, which
camot be readily machined. (Author)
Naval Ordnance Test Sution [China Lake] Calif.
NICKEL ELECTROFORMING OF OPTICAL MIRRORS,
by R. A. Weinhardi. Interim rept. 2 Feb 53, declassi-
fied 24 June 55. 17p. 10 refs. Technical memo. 786.
Order from LC mi$2. 40, ph$3. 30 PB 153 883
This report released for sale to the public 19 Jan 61.
The general technique of electroforming is relatively
simple, consisting of plating a heavy deposit of metai
onto or into a suitable mandrel, and separating the
plated metal from the mandrel. The metal thus be-
comes the part desired, which may or may not require
subsequent machining. The process lends itself to the
production of parts having complex surfaces which
would be difficult or even impossible to produce by
other methods. In addition, it has the capability of re-
producing the surface finish of the mandrel to very
great accuracy. This feature makes possible the pro-
duction of metal mirrors.
Transport, Traction and Hoist Focilities
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
FIELD TEST OF CANADIAN SNOWMOBILE, by Jack
C. Green. Aug 49. 7p. Proj. no. 21-01-024.
Order from LCmi$l. 80, ph$ 1.80 PB 153 320
The purpose was to test the adequacy of the Canadian
Snowmobile (Mark II, Penguin) as a crash -rescue ve-
hicle under subarctic winter temperatures and terrain
conditions.
Naval Civil Engineering Lab. , Port Hueneme, Calif.
COMBINATION CARGO SLEDS, Y-F015- 11-235,
TYPE C, by J. J. Doman and D. Taylor. Final rept.
26 Oct 60, 20p. Technical rept. 091; AD-246 000.
Order from LC mi$2. 40, ph$3. 30 PB 152 942
A combination sled has been develc^ied for arctic use
which can be readily converted from a bobsled for loi^-
haul sled train operations to two fixed- runner sleds for
shon-haul operations. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
THE TUNDRA TRUCK, Y-F015-99-001, TYPE C,
by D. Taylor. Final rept. 30 Sep 60, 40p. 6 refs.
Technical rept. 094.
Order from LC mi$3. 00, ph$6. 30 PB 152 940
The Laboratory designed and tested a self-propelled
cargo vehicle combining amphibious and low-ground-
pressure capabilities for snow and swamp operations
in the arctic. The vehicle maneuvered easily in water
but failed on land. (Author)
MATERIALS
Fabric Research Labs., Inc., Dedham, Mass.
INVESTIGATION OF THE HIGH SPEED IMPACT BE-
HAVIOR OF FIBROUS MATERIALS. PART I: DE-
SIGN AND APPARATUS, by Chauncey C. Chu. Robert
313
J. Coskren, and Henry M. Morgan. Repc. for
15 Feb 59-15 Juna 60 on Air Force textile Materials.
Contraa AF 33(616)6321. Sep 60. 39p. 2 refs. WADD
Technical rept. 60-511. Part I.
Order from OTS^ 1.00 PB 171 311
A high speed imp^a test machine has been designed,
constructed, and talibrated to test parachute compo-
nents at high rates of leading. This instrument is
capable of rupturing materials of up to 10. 000 pounds
static breaking st|-ength at velocities of from 200 to
750 feel per secofd. The impacting force is applied by
a free flying missile launched by a gas gun utihzlng
either nitrogen ox; helium gas at nKxlerately low pres-
sures. The gun h^s a bore of 2.5 inches and fires
nuaalles weighing up to 10 pounds. Pertinent data are
atealned by mean* of multiple exposure photography
using a multimictoflash hghting source which provides
a maximum d fifteen separate flashes spaced at
predatermined intervals of between 10 and 10.000
microseconds. The resulting photograph records the
specimen and the impacting missile before, during and
after the Impact. Measurement of the distances be-
tween successive exposure yields information such as
the breaking strefigth. the extension to rupture, and
the energy abaori«l by the specimen. (Author)
Material Labs . 4 Puget Sound Naval Shipyard,
Brenrienon, Wa^h.
REINFORCED Pl+ASTIC COATINGS FOR THE PRO-
TECTION OF M^TAL SURFACES, by L. N. Schultz
Jan 60, 27p. 7 refs. Interim rept.
and M. E. Phelps
P-300-10.
Order from LC nli$2.70, ph$4.80
PB 152 862
Antifouling paints applied over plastic coated steel
panels have been
exposed for three years to full and
part time saltwater immersion. The effect of thif ex
posure on severa
resins with various surface treat-
ments IS describ<d. (Author)
Rock Island Araenal Lab. , 111.
HEAT FUSED CfRAMIC COATINGS FOR ALUMINUM
COMPONENTS Of ROCKET LAUNCHERS, by T. Rice
andT. Turner, i I Oct 60, 19p. 4 refs. Rept.
no. 60-3203. [
Order from OTS ^0. 50 PB 171 047
Ceramic coating^ containing lead-bearing and lead-free
frits have been prepared fronrcommercially available
frits, addition agents, and pigments and applied to
aluminum test pahels. The coatings have excellent
heat resistance, but are deficient in abrasion resist-
ance. No appreciable differences were noted between
the lead-bearing ind the lead-free formulations.
(Ai«hor)
Washington U. , {Seattle.
CHEMICAL PHYSPCS RELATED TO PHOTCXJRAPHY.
by William T. Siriipson. Rept. on Contract
AF 18(600)375. \^r 60. I38p. 225 refs. AFOSR-TR
60-43.
Order from LCnii$6. 90. ph$2l.30 PB 152 446
Summary of work
chemistry and
spectroscopy.
on the interweaving of quantum
e^(ierimental electronic state
Included in the report are:
Structures and .T-electron spectra. 111. Triphenyl-
methane dyes, pub. in the Jnl. of the American
Chemical Society 76:6293-6300. 1954
The unit-cell dimensions and space group of 1, 1" -di-
ethyl-2. 2' -pyridocyanine iodine, puh- in Acta Crys-
tallographica 8: 1 19. Feb 55.
Low resolution electronic spectrum of hexamethyl-
benzene with application to benzene, pub. in the Jnl.
of Chemical Physics 23:1146-1151. June 55
Low resolution electronic spectrum of crystalline
para -dimethoxybenzene with application to benzene,
puE~in the Jnl. of Chemical Physics 23: 1480-1485,
Aug 55
Polarization of the 1850 A. band of amides, pub. in the
Jnl. of the American Chemical Society 77:3929. 1955
Spectroscopic study of Wurster's blue and tetramethyl-
p -phenylenediamine with assignments of electronic
transitions, pub. in the Jnl. of the American Chemi-
cal Society 77:4454. 4461. 1955
Resonance force theory of carotenoid pigments, pub.
in the Jnl. of the American Chemical Society 77:6164.
6168. 1955
Classification of T-electron states, pub. in the Jnl. of
the American Chemical Society 78:3585, 3590. 1956
Calculation of bond eigenfunction matrix elements with
the vector model, pub. in the Jnl. of Chemical Phys-
ics 25: 1297-1298. Dec 56
Ckxipling strength for resonance force transfer of
electronic energy in Van der Waals solids, pub. In
the Jnl. of Chemical Physics 3:588-593. Mar 57
Polarized electronic absorption spectrum of amides
with assignments of transitions, put?, in the
American Oiemical Society 79:2375-2382. 1957
Theoretical electronic spectrum of the allyl system,
pub. in the Jnl. of Chemical Physics 27:20-23,
July 57
Electronic spectra of pyridocyanine dyes with assign-
ments of transitions, pub. in the Jnl. of the American
Chemical Society 79:4314-4320. 1957
Application of the Pariser and Parr method to dye ions
with amidinium resonance, pub. in the Jnl. of Chemi-
cal Physics 28:297-300. Feb 58
Consolidated variation perturbation theory, pub. in
the Jnl. of Chemical Physics 28:925-928. May 58
Formal HUckel theory, pub. in the Jnl. of Chemical
Physics 28:972-974. May 58
Electronic spectrum of 4. 4' -bis-dimethylamino
fuchsone and related triphenylmethane dyes. pub. in
Molecular Spectroscopy 3:363-380. Aug 59
HUckel theory. An effective Hamiltonian, pub. in the
Jnl. of Chemical Physics 31:1317-1319, Nov 59
Evaluation of one -center electron repulsion integrals
between certain ^-type atomic orbitals, pub. in the
Jnl. of Chemical Physics 32: 124-126, Jan 60
Metallic reflection from molecular crystals, pub. in
Reviews of Modern Physics 32:466-476. Apr 60
Calculation of delocalization contribution to infrared
intensity, pub. in the Jnl. of Chemical Physics
32:1747-1756. June 60
Fuels, Lubricants, and Hydraulic Fluids
Combustion and Explosives Research, Inc. ,
Pinsburgh, Pa.
THE THERMODYNAMICS OF PROPELLANT GASES,
by Stuart R. Brinkley, Jr. Final rept. , pt. 1 on Coa-
traa DA 36-061 -ORD-425. 30 Sep 56, 3i6p. 18 refs.
AD- 157 442.
Order from LC mi$3.00, ph$6.30 PB 149 665
1314
In Plsrt I methods for the calculations are developed.
b Pirt II an explicit program for these methods is
presented for the ORDVAC. a high speed computed
located at the Ballistic Research Laboratories,
Aberdeen, Maryland.
Consolidated Elearodynamics Corp. , Pasadena,
Calif.
AN ANALYZER FOR MOISTURE AND SOUDS IN
JET FUELS, by Michael Czuha. Jr. and Kenneth W.
(Jardiner. Rept. for June 59-May 60 on Aviation Fuels.
Contract AF 33(616)6588. Sep 60. 34p. 7 refs. WADD
Technical rept. 60-461.
Order from OTS $1.00 PB 171 303
A continuous analyzer for water in turbine fuels was
developed based on the absolute coulometric decompo-
■ttlan of the water. An optical method for determining
Mlpended solids using forward scanering of light was
also developed. The unitized instrument operates in
the parts per million range on both types of fuel
contaminants. (Author)
Fuels Research Lab. , Mass. Inst, of Tech.,
Cambridge.
EXPERIMENTAL STUDIES OF SUB- ATMOSPHERIC
(X3MBUSTI0N. by H. C. Hottel, G. C. WiUiams and
others. Rept. for 1 June 58-31 May 59 on Research to
Verify the Model Laws Related to Combustion at Low
Pressure, Contract AF 33(616)5746. Aug 60, 65p.
aOrefs. ARL Technical rept. 60-296.
Order from OTS $1.75 PB 171 306
Geometrically similar ramJet-type combustion cham-
bers of 1. 61-, 4.026-, and 6.065-inch diameter and
ieagths of 5. 25D and 4. 25D were operated at Reynolds
numbers ranging from 24^000 to 230, (XX) and pressure
terels from 0. 2 to 1.5 atmospheres with propane fuel.
Burner stability limits were satisfactorily correlated
by the parameter Ubo/P^^ as a function of air/fuel
ratio. Combustion efficiency was determined from
oqrgen consumption and was shown to be essentially
the same for scaled burners if the Reynolds number
•nd Damkohler's chemicaj parameter. U/P"''D, were
held constant; the pressure exponent, n, showed some
»arlation around an average value of 2. Deficiencies in
the scheme of modeling based on the two parameters
above are discussed. It is shown that wall heat losses,
in effect of pressure on turbulence level, and un-
scalable oscillatory phenobiena all tend to produce un-
sealed effects on burner stability and efficiency. In
puticular, inclusion of the two conventional parame-
ters alone and omission of the scaling of wall heat
kwaes can lead to efficiencies determined on the
"model" which are significantly different from those of
the prototype. (Author)
Jfctlonal Research Labs., Ottawa (Canada).
LUBRICANT BEHAVIOUR 'IN CONCENTRATED
(X3NTACT. THE EFFECT OF TEMPERATURE, bv
F. W. Smith. Aug 60, 33p. 13 refs. Mechanical Engl-
■Mrlng rept. MP- 17.
Cutler from LC ml$3. 00, ^$6. 30 PB 153 476
6?)erlments are described on the frlctional behaviour
<^a petroleum oil in the contact zone between a steel
roller and an aluminum one at 23^0 and betvireen steel
rollers and between tungsten carbide rollers at 230C,
lOO^C and 190^a The coefficient of sliding friction
decreases with increaiing temperature, (^litatively.
this is taken to itidicate that the frlctional force rep-
resents the shearing of a thick plastic film of lubricant;
quantitative agreement between experiments with steel
and with carbide rollers is poor. To explain disaccord
with other experiments in which the coefficient of fric-
tion increases with increasing temperature, it is pro- '
posed that mechanical instability of the lubricant film
may be a factor in extreme pressure lubrication. On
general physico-chemical grounds, it is suggested that
an intermolecular sliding process occurs at a shear
plane in typical concentrated contaa lubricant films at
low temperature and high stresses. TTie relationship
between such shear-plane processes and the Ree-
Eyring theory of non- Newtonian viscosity is discussed.
(Author)
Naval Ordnance Test Station, China Lake, Calif.
THE PREDICTION OF THE CRITICAL TEMPERA-
TURE OF PROPELLANT GRAINS, by Frank H. Conrad
and Paul A. Longwell. 4 Sep 60, 30p. 7 refs. NOTS
TP 2517; NAVWEPS rept. 7096. AI>245 485.
Order from LC mi$2.70, ph$4.80 PB 152 825
The critical temperature of a propellant grain may be
defined as that temperature imposed by the surround-
ings in some specified fashion above which the grain
will eventually explode or destroy itself due to "self
heating" or spontaneous combustion. The critical tem-
perature is a function of the thermal constants and
dimensions of the propellant grain and of the heat trans-
fer coefficients between the grain and the surroundings.
For a given propellant, the critical temperature is de-
creased by increasing the size of the grain and by de-
creasing the heat transfer coefficient to the surround-
ings. This report presents the information available
concerning the calculation of critical temperatures for
hollow cylinders in a fashion such that engineers work-
ing with propellants can easily make use of this infor-'
mation. For this work to be most useful on new pro-
pellants, experimental values of the heat generation
coefficient. Q, and the activation energy, E, should be
obtained for these propellants. (Author)
Plastics
Feltman Research Labs. , Plcatinny Arsenal,
Dover, N. J.
PROBLEMS OF WAVE PROPAGATION IN PLASTIC
MEDIA, by Julian L. Davis. Nov 60, 34p. 7 refs.
Technical rept. FRL-TR-12.
Order from LC mi$3.00, ph$6.30 PB 150 013
i
Some current investigations concerning the behavior of
plastic and viscoeiastic media subjected to externally
applied dynamic loads are discussed, with emphasis on
the analysis of a problem concerning wave propagation
in a bounded viscoelastlc medium. A brief survey of
some current problems in nonlinear wave propagation L
is given. This work is part of a program of basic re-
search on the physical and chemical properties of
polymeric materials being carried out in the Plastics
and Packaging Laboratory at Plcatinny Arsenal.
(Author)
1
315
Pelonan Resea^h Labs. , Plcatlmy Arsowl, Dover.
N. J. I
SEPARATION AKD SOLUTION PROPERTIES OP
GRAFT CX:)POLYMERS OF P-ISOPROPYLSTYRENE
AND METHYL METHACRYLATE. by David W. ^Levi
Oa 60. 24p. 16 tefa. Technical rept. FRL-TR^frST
Order from LC rti$2. 70. ph$4. 80 PB f^ 963
Evidence for grafting of polj^methyl methacryiate) to
autoxldlzed poly(|)-i8opropyl8tyrene) obtained earlier
froni aolubHity at»d fractionation behavior is sunima -
rized. An extraotion method was developed for sepa-
rating the graft aopolymer from the admixed homo-
polymer. Preliminary dilute solution characterization
at the separated fptdx copolymer samples by light
■canering and viecosity was carried out. When com-
pared with the hcmopolymers, the molecular weight -
visooaity relatioa and second virial coefficients furnish
excellent evidenqe that grafung was indeed accom -
plisbed. However, the dimensions of the graft copoly-
mers from light Scattering were anomalous. (Author)
Naval Research Lab., Washington, D. C
THE EFFECT CB? DIFFERENTIAL TEMPERATURES
ON THE FRACTURE TOUGHNESS OF STRETCH-
ORIENTED POLVMETHYL METHACRYLATE, by
H. L. Smith, W.IE. Anderson, andE. O. Cook.
Interim rept. 1 liov 60, Up. 7 refs. NRLrept. 5547.
Order from LCi^iS 2.40, ph$ 3. 30 PB 149 850
Stretch-oriented Ipolymethyl methacrylate (Plexiglas) is
known to have superior fraaure toughness over as-cast
material within (jertain temperature boundaries. It
loses toughness t»hen held at temperatures above the
glass transition temperature (approximately 200*^ to
225OF), and its Superiority over as-cast material Is
lost when fractuced at temperatures of approximately
20OF or lower, Jepending on the particular composition
d material. Th^ fracture toughness advantage of
stretch-oriented Imaterial oven as-cast material for
transparent airctafi enclosures is then limited to tem-
peratures above the brittle transition temperature, and
the plane is liimfed to speeds below that for which
aerodynamic heajting results in excessive skin tem-
peratures. The data show that stretch-oriented poly-
methyl meihacryllate may be used for finite periods of
time at aircraft speeds resulting in skin temperatures
somewhat above khe glass transition temperature, pro-
vided that such g|kin temperatures are coupled with
downward temperature differences in the thickness
direaion of the fiaterial. Stretch-oriented material is
also shown to retain a rwo-to-ooe margin in toughness
over as-cast material at skin temperatures down to
0°F when coupled with upward temperature differences
in the thickness direction of the material. (Author)
Plastics Technital Evaluation Center, Picatinny
Arsenal Doveij N. I.
RECENT DEVELOPMENTS IN CASTING RESINS AND
TECHNOLOGY ?0R ELECTRICAL ENCAPSULATION
APPUCATIONS. by Arnold M. Molzon.. Nov 60, 34p.
90 refs. PLASTTflC rept. 3.
Order from OTSJ$1.00 PB 171 034
Recent developments in plastic casting resins, proc-
essing techniquei, and test methods for electrical
encapsulation applications are summarized. Plastic
materials covered include epoxy, silicone, poly sulfide,
polyurethane, polyester, and hydrocarbon. Advance*
in electrical testing techniques have been largely due
to the use of sensing devices encapsulated in the resin
and the determination of parameters both during and
after resin hardening. Instrumentation has been re-
ported for determining the existence and magnitude of
thermal stresses in casting resins during and after
cure; thermodynamic properties, such as rate of poly-
merization, extent erf polymerization, and over -all
activation energies; and thermal properties, such aa
specific heat and second-order transition temperature.
Advances in encapsulation techniques have been made
in mixing and dispensing equipment, expendable mokls,
and kit -type packaging. The report lists resin sup-
pliers, suppliers of formulated material, and cheniicai
structure of encai>sulating resins and diluents.
(Author)
Thiokol Chemical Corp. , Elkton, Md.
DEVELOPMENT OF TE-60 PLASTIC PARTS AS-
SEMBLY, by H. G. Jones. Final rept. for 29 Aug 55-
31 Mar 59 on Contract AF 33(600)31 113. 24 Dec 59,
declassified. I73p. 35 refs. Rept. no. El 20-59.
Order from LC mi$8. 10, ph$27. 30 PB 153 620
This report released for sale to the public 10 Jan 61.
A program was conducted which demonstrated the fee-
sibility of constructing chambers and nozzles for solM
propellant motors from reinforced plastic materials.
The T-61 (Matador) booster was selected for this pro-
gram. A successful reinforced nozzle and chamber
assembly was made of fiber glass roving and epoxy
resin. This assembly weighed less than 600 lbs and
when loaded contained I, 450 lbs of T-35 (polysulfide)
propellant. The performance of this motor was ap-
proximately 106,000 lbs of thrust for 2. 6 seconds at
bCPV- Six firings were made; all were successful.
The firings were made at -30P. 60^ and I60°F and
included a drop test, a rough road test, and a temper-
ature cycle test. (Author)
Rubber and Elastomers
Institute of Rubber Research, U. erf Akron, Ohio
STRESS RELAXATION AND STRUCTURE OF HIGH
THvlPERATURE ELASTOMERS, by Maurice Morton,
V. R. Allen, and R. Dl Gates. Technical rept no. 7,
1 Dec 59-29 Feb 60, on Contract Nonr- 2573(00). [19W1
38p. 11 refs. AD-235 312.
Order from LC ml $3. 00, ph$6. 30 PB 153 17J
Sol-gel relations have been determined for the degra-
dation of sulfur vulcanizates of natural rubber by selec-
tive reduction of the sulfur crosslinks. The shapes of
these curves have been Interpreted in terms of network
chain entar^lements and crosslink density. Experi-
mental results add credence to the conclusions that
natural rubber vulcanizates degrade oxldati^^ly via
random scission of network chains. Sol-gel relations
during network formation have been used to calculate
the molecular weight between enunglements for uncrosr
linked natural rubber. The observed differences In fl«
reported values of this parameter have been attributtd
tea variable term which relates the effeaivenessrf the
■\
I
316
eotai^lement to chain flexibility. The determination of
H(lfae polymer solvent Interaction coefficient) for the
Vltron A-methyl ethyl ketone system by vapor pressure
measurements gave a negative value for v^ greater
than 0. 135. Degradation studies of Vlton A have shown
that crosslinking accompanies degradation when the
elastomer is exposed to high temperatures 2750C. ). A
poai-cure heat treatment (15-24 hours at 2(X)OC.)
rtMrds the rate of degradation of the vulcanizate
during subsequent heat aging tests. (Author)
Rock Island Arsenal Lab. , III.
ANTIRADS FOR NITRILE RUBBER, byj. W. McGarve>
22 Sep 60, 28p. 22 refs. Rept. no. 60-2856.
Order from LC mi$2. 70, ph$4. 80 PB 150 961
The mechanisms of radiation damage and protection in
organic materials were Investigated and a total of 118
different nitrile vulcanizates containing potential
antirads were evaluated in a screening program. Sev-
eral antirads were found which imparted a significant
degree of proteaion to nitrile rubber exposed to cobalt
60, gamma radiation. A good antlrad such as 1, ^-di-
phenyl-2-plcrylhydrazine imparted approximately ihc
same degree of radiation resistance to nitrile rubber a
is inherent in natural rubber. This investigation also
demonstrated the exlstance of certain structural corre-
lations by which it may be possible to selea or syn-
thesize new and even more efficient antirads. (Author)
Rock Island Arsenal Lab- ,111.
I>rrERNAL AND SURFACE TEMPERATURES OF
RUBBER EXPOSED TO DIRECT SUNUGHT, by
E. W. Bergstrom. 31 Aug 60, lip. Rept. no. 60-2561.
Order from OTS $0.50 PB 171 042
Surface and internal temperatures were measured on
rubber (SBR) discs which were exposed outdoors to
direct sunlight during the hot summer weather at Rock
Island Arsenal. It was found that the surface and in-
ternal temperatures of the rubber were In the range of
35 to 50OF. higher than lihe surrounding air tempera-
tures. This information should be of value in estab-
lishing specification requirements for rubber items
which will be exposed odtdoors in temperate climates.
(Author)
Rock Island Arsenal Lafc. , 111.
OZONE RESISTANCE OF SBR VULCANIZATES, by
E. W. Bergstrom. 31 Aug 60, 34p. 23 refs. Rept.
no. 60-2563.
Order from OTS $1.00 PB 171 043
TWa report summarizes. the results of various investi-
gations pertaining to the ozone resistance of SBR vul-
canizates. Results are reported for studies on, (1)
kwg term outdoor expo8(ire tests, (2) the correlation of
•ccelerated ozone test results with outdoor test results,
(3) the ozone resistance of SBR vulcanizates under dy-
namic test conditions, (4) the protection of SBR vulcani-
Utes exposed under constant load conditions, (5) the
protection of oil extended SBR from ozone attack, (6)
the protection of vulcanizates containing a 60/40 ratio
of SBR/natural rubber, (7) the compatibility of
N,N'-di-3(5 methyl heptvl)-p-phenylened{amine with
various nonelemental sulfur curing systems, and (8)
the staining characteristics of p-phenylenedi amine
antiozonants. (Author)
MATHEMATICS
Applied Mathematics and Statistics Labe. , Sunford
U. . Calif.
ASYMPTOTIC STOPPING REGIONS FOR SEQUEN-
TIAL TESTING WITH AN INDIFFERENCE REGION,
by Gideon Schwarz. Technical rept. no. 54 on Contract
N6onr-25140. 19 Jan 60. 13p. 1 ref. AD-231 229.
Ortler from LC mi$2. 40. ph$3. 30 PB 152 883
A family of tests is defined by a property that could be
used in the 2 -hypotheses problem to characterize the
Wald teat: For every test in the family, the a pos-
ceriori risk due to stopping and taking the more favor-
able action is a constant r along the boundaries of the
stopping region. The regions in the (n, Sn) - plane are
shown to grow, as r-*0, in all directions like - log r.
The asymptotic shape of Che regions is found explicitly
for this case and for a generalization to composite hy-
potheses. This generalization essentially covers the
case where there are 2 hypotheses separated by a true
indifference zone so that if the inean lies in the indif-
ference zone there is no loss attached to either termi-
nal decision. The asymptotic shapes are shown to be
valid for a whole class of r-families of tests. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
A CLASS OF TYPICALLY -REAL MEROMORPHIC
FUNCTIONS, by R. K. Brown. 1 June 60. 18p. 7 refs.
USASRDL Technical rept. 2121; AD- 242 517.
Order from LC mi$2.40, ph$3.30 PB 152 674
A Stieltjes-integral representation for a class of func-
tions which are typically-real and meromorphic in the
unit circle is developed. With this representation, new
and more direct proofs are obtained for several
theorems due to A. W. Goodman (Trans. Am. Math.
Soc. 81:92-105, 1956). New bounds for the coefficient
differences are established, and domains of variability
are derived for the derivatives of the functions.
(Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
TWO THEOREMS ON PATHOLOGICAL EXTENSIONS
OF DIFFERENCE FIELDS, by Albert E. Babbitt.
9 Aug 60, 9p. 5 refs. USASRDL Technical rept. 2145;
AD-242 982.
Order from LC mi$l. 80. ph$l. 80 PB 152 675
A difference field extension of a difference field F
which either is incompatible with some other extension
of F or is a monadic extension of F Is said to be a
pathological extension of F. It is known that a differ-
ence field admits a finitely generated pathological ex -
tension only if it admits a pathological extension of the
same type erf order zero. In this paper the following
generalization is proved- Let G be an extension of Fof
transformal transcendence degree at least 1 over F.
Then G admits a finitely generated patfiological exten-
sion only if there exists an element « in G such that •
generates a pathological extension of P of order zero.
(Author)
317
Behavioral Sciences Lab. . Wright Air Development
Div. , Wright- Patterson AFB, Ohio.
DISTRIBUTION- F IE E STATISTICAL TESTS, by
James V. Bradley.j Aug 60, 3«7p. 19 refs. WADD Tech-
nical rept. 6O-661I
Order from OTS 15. 00 PB 171 312
As a result of an Extensive survey of the literature, a
large number of distribution- free sutistical tests are
examined. Tests •re grouped togedier primarily ac-
cording to general type of nnathematical derivation or
type of statistical information used in conducting the
test. Each of the tnore important tests Is treated under
the headings: Rationale, Null Hypothesis, Assumptions,
Treatment of Tiefl. Efficiency, Application, Discussion,
Tables, and Sourcjes. Derivailors are given and mathe-
matical interrelationships among the tests are indicated
Strengths and weaknesses ot individual tests, and o*
distribution-free Jests as a class compared to paramet-
ric tests are discussed. (Author)
California U. , B erkeley.
ASYMPTOTIC BEHAVIOR AND UNIQUENESS THEO-
REMS FOR HYPERBOLIC EQUATIONS AND IN-
EQUALITIES, byjM. H. Procter. Technical rept. no. 9
on Contract AF 4^(638)398. Mar 60, 20p. ft refs.
AFOSR-TN-60-3a0; AD-235 217.
Order from LC nii$2. 40, ph$3. 30 PB 149 646
Inequalities of thJ form |Lu|$ci I uUc2 ||^^| *
C3 1^1 are cooajdered, where L - A - -J^j-and A is an
elliptical operatoi-.
California U , f erkeley.
HOMOTOPY-ABEMAN LIE GROUPS, by S. Araki,
I. M. James, and $mery Thomas. Technical rept.
no. 13 on Contradt AF 49(638)79. June 60, 7p. 8 refs.
AFOSR-TN-60-4i7; AD- 244 906.
Order from LCniil 1.80, ph$ 1.80 PB 152 606
rtiap
A topological gro^p
the commutator
The following theorem
Lie group is
(Author)
G is said to be homotopy-abelian if
of G X G into G is nulhomotopic .
Ti is proved: a compact connected
hom^opy-abelian only if it is abelian.
California U. , Berkeley.
LIE ALGEBRA COHOMOLOGY AND THE GENERAL-
IZED BOREL-W^IL THEOREM, by Bertram Kostant.
Technical rept. ilo. 16 on Contract AF 49(638)79. Sep
Sep60, 108p. 8iefs. AFOSR TN-60- 1061; AD-244 907.
Order from LC nd$5. 70, ph$l6.80 PB 152 607
Contents:
Cochain complexes defined by Lie algebras and
Hermitian struc tures
The I^placian in the case of a Lie summand
The spectral resolution of the Laplacian and cohomo-
logy for a famil f of nilpotent Lie summands
The generalized lorel-Weil Theorem
Wcyl's character formula and its extension to non-con-
nected groups
Synimet i ic comf lex spai fs X and a generalization of
a thf«5rem of F) resmann
CabforniaU, Berkeley.
ON DIFFERENCE METHODS FOR THE SOLUTION
OF PARTIAL DIFFERENTIAL EQUATIONS OF
MIXED TYPE, by Hajimu Ogawa. Technical rept.
no. 11 on Contract AF 49(638)398. Oct 60, 51p.
AFOSR -TN-60- 1026; AD-245 313.
Order from LC mi$3. 60. ph$9. 30 PB 152 715-1
This paper is concerned with the problem of solving
boundary and initial value problems for certain partial
differential equations of mixed type by finite difference
methods. FiUppov, in considering the Tricomi equa-
tion, used a maximum principle as a basis for prcving
the existence of the solution to a certain difference
equation. This solution was shown to converge, as the
mesh size tends to zero, to the solution to the boundtrjr
value problem for the Tricontl equation, provided thtt
the latter exists and is sufficiently smooch. In the firn
part of this paper, Fihppov's results are extended toi
more general mixed-type equation whose difference
approximation has a solution which satisfies a maxi-
mum principle. It is found that the conditions under
which the solution of the differential equation satisfieg
a maximum pjrinciple, as discovered by Agmon,
Nirenberg and Procter, are sufficient for the solution
of the difference equation to satisfy an analogous
principle, except near the parabolic line where addi-
tional conditions are required. (Author)
California U , Berkeley.
ON DIFFERENCE METHODS FOR THE SOLUTION
OF PARTIAL DIFFERENTIAL EQUATIONS OF
MIXED TYPE, by Hajimu Ogawa. Technical re{X.
no. 11. Part 2 on Contraa AF 49(638)398. Oct 60,
54p. 9 refs. AFOSR -TN-60- 1026, pt. 2; AD-245 313,
pt. 2.
Order from LC mi$3.60, ph$9.30 PB 152 715-2
Finite difference methods are employed for the solu-
tion of an equation which is hyperbolic in the interior
of a domain and parabolic on the line which carries the
initial data. As in the boundary value problem, a
maximum principle for a suitable difference equation
yields an approximate solution which converges to the
solution of the differential equation as the mesh size
tends to zero. Again it is found that the conditions
under which the differential equation has the maximum
property, as found by Weinberger and Protter, imply
that the difference equation has the properly, except
near the parabolic line. An existence theorem for the
solution to the boundary value problem for an equation
which is hyperbolic in the interior of a domain and
parabolic on a part of the curve carrying the boundary
values is proved. (See also PB 152715-1)
Carnegie Inst, of Tech., Pittsburgh, Pa.
SOME RESULTS ON TRANSFORMATIONS IN THE
ANALYSIS OF VARIANCE, by M. M. Rao. Rept. oa
Mathematical Techniques of Aeromechanics, Contract
AF 33(616)3878. Aug 60, 24p. 13 refs. ARL Technical
note 60-126.
Order from OTS $0. 75 PB 171 334
The square- root and the logarithmic transformations
are considered when the mean is large in each case, fc
the former the variance is assumed known, and in the
latter the corresponding assumption is that the coefB*
cient of variation is small but the variance is unknown.
318
In these cases, it Is shown that the usual normal theory
is applicable to test the hypotheses on means of the un-
transformed variables. Sufficient conditions for the
tppllcabi lity of the normf<l theory are presented for a
class of distributions depending on a finite set of
parameters with one parameter large, while the ocher^
if any, are relatively small, or are confined to a fixed
bounded set in the parameter space. (Author)
Columbia U. School of Engineering, New York.
THE LOSS OF INFORMATION DUE TO THE GROUP-
ING OF DATA, by Peter Frank. Technical repc. no. 6
00 Contract Nonr-266(55), 6 Jan 60, 25p. 3 refs.
AD- 231 843. ;
Order from LCmi$2. 70,: ph$4. 80 PB 152 896
Much of the theory of estimation is based on continuous
distributions where it is Assumed that observations are
real numbers: that is, they can be made with infinite
accuracy; this is a convenient mathematical approxi-
mation. In the actual world, two observations which
fall In the same interval (of real numbers) are identi-
fied: the observations have been grouped. The size of
the groupings has an effect of the efficacy of the statis-
tical procedures; also, the gproupings can be made part
of a statist I al design. In this report, size of group-
ings is analyzed by using Fisher's definition of
information.
Electronics Research Lab. , U. erf California,
Berkeley.
MONTE CARLO ESTIMATES OF BCCURSION PROB-
ABILITIES OF A GAUSSL^N PROCESS, by M. B. Free-
man. Rept. on Contract Noor-222(53). 30 Mar 60, 32p.
20 refs. lER series no. 60, issue no. 272; AD-238740.
Order from LC mi$3. (JO, ph»6. 30 PB 148 500
The probability that a certain Gaussian random process
ia greater than b throughout a time interval of length t
seconds Is estimated from observations of a high-speed
numerical model. The process is that characteristic
of a simple harmonic oscillator in Brownian motion.
(Author)
Harvard U. (Cambridge, Mass.]
BEST APPROXIMATORS WfTHlN A LINEAR FAMILY
ON AN INTERVAL, by J.' L. Walsh and T. S. Motzkln.
Rept. on Contract AF 49(638)574. July 60, 19p. 8 refs.
AFOSR TN-60-911; AD-244 395.
Order from LC mi$2.40, ph$3.30 PB 152 375
The purpose of the present note is to investigate the
behavior of functions p(x) of best approximatioti to a
given function f(x), where p(x) is supposed to belong to
a linear family P and where deviation is measured on
BcCSx Slbya generaUzed norm
|f(x) - p(xX| - j" r(|f(x)-p(x)|yw(x)dx
E
involving a transformejr r(t) and a weight funaion w(x).
This norm was recently Mudied In the special case
nOitP, p >0, w(x)s.l, and is now to be studied
more generally (but net including the case p < 1).
Harvard U. [Cambridge, Mass.)
ON THE CIRCLES OF CURVATURE OF THE
CURVES OF STEEPEST DESCENT OF GREENS
FUNCTION, by J. L. Walsh. Rept. on Cootraa
AF 49(638)574. Oct 60, 17p. 2 refs. AFOSR TN-
60- 11 38; AD-244 397.
Order from LC mi$2.40, ph$3.30 PB 152 369
A number of years ago the present writer pubUshed a
study of the tangents and circles of curvature ot
lemniscates and of the level loci of Green's function In
the plane. The present note Is complementary to that
previous study, and considers elementary geometric
properties of the curves of steepest descent, namely
the lines of force, or orthogonal trajectories of the
level loci of Greenes funaion. The method used is a
continuation of the previous methods, especially, use
of an integral representation of Green's function
essentially due to Hilbert. (Author) ^
Harvard U. (Cambridge, Mass.]
SERIES EXPANSIONS OF SOLUTIONS OF THE HEAT
EQUATION IN N DIMENSIONS, by D. V. Widder. Rept.
on Contraa AF 49(638)574. Aug 60, 37p. 4 refs.
AFOSR TN-60-912; AD-244 396.
Order from LC nil$3.00, ph$6.30 PB 152 376
This paper is an extension of a recent result by D. V.
Widder and P. C Rosenbloom concerning the expansion
of a solution u(x, t) of the heat equation, Uxx - ut , in
series of polynomial solutions. Whereas that result in-
volved two variables only, the present one permits an
arbitrary finite number of variables. It is found that the
polynomial solutions of the heat equation in n dimen-
sions are faaorable into polynomials In two variables.
The expansion problem may be considered as an Inves-
tigation i>f the space spanned by linear combinations of
these factorable solutions. (Author)
Harvard U., Cambridge,, Mass.
THE ZEROS OF INFRAPOLYNOMIALS WITH SOME
PRESCRIBED CCCFFICIENTS, by O. Shisha and
J. L. Walsh. Rept. on Contraa AF 49(638)574. July 60,
64p. 37 refs. AFOSR TN-60-54.1; AD-244 391.
Order from LC mi»3.90, ph$10.80 PB 152 371
The reports considers Infrapolynomials A(z)sao •*•
a|Z ■*•...-♦• anz" on sets S, with prescribed
an.«n-l. . an-y or a©, ai, . .., ak or both. The
main purpose here-is to obtain information on the
geometric location of the zeros of such polynomials.
Illinois U. (Urbana]
ON WEIERSTRASS PRODUCTS OF ZERO TYPE ON
THE REAL AXIS, by L. A. RubelandJ. P. Kahane
(Universite'de MontpelUer). Rept. on Contraa
AF 49(638)517. 15 July 60, 14p. 8 refs. AFOSR TN-
60- 807; AD-245 673.
Order from LC miJ2. 40, ph$3. 30 PB 152 972
Under the well-known restriction
oc
J * (ltr2)'^ log-t- |f(r)|dr < 00
319
on the rate erf groMth on the real axis of entire func-
tions of exponential type, the type of a produ« is the
sum of the types of the factors. It is shown here that
this is no longer t^ue if these restrictions are relaxed.
As a consequence
the "theorem of supports" for
certain generalized distributions falls to hold. (Author]
Institute for Flu d Dynamics and Applied Mathematics
U. of Maryland. College Park.
THE APPROXIMATION OF SOLUTIONS OF NON-
LINEAR DIFFERENTIAL EQUATIONS, by M. D.
George. Doctoral thesis-. Rept. on Ckxitract
AF 49(638)228. Ivfer 60, 16p. 4 refs. Technical note
BN-196; AFOSR-'tN-60-329; AD- 234 729.
Order from LC mi$2. 40, ph$3. 30
PB 149 730
Sufficient conditiotis are given for the convergency of a
sequence of operators to a given semigroup of non-
linear operators Hn a Banach space, with applications to
the approximation! of solutions of non-linear partial dif-
ferential equation I by finite -difference methods.
(Author)
Institute for Flu d Dynamics and Applied Mathematics
U. of Maryland, I College Park.
UPPER AND LOWER BOUNDS FOR QU/DRATIC
INTEGRALS, ANP AT A POINT, JFOR SOLUTIONS
OF LINEAR BOUfJDARY VALUE ^PROBLEMS, by
J. B. Diaz. Rept. pn Contract AF/49(638)228. June 59,
53p. 41 refs. Technical note BN-178; AFOSR-TN-
59-720; AD-219 6*5.
Order from LC ni^3. 60, ph$9. 30 PB 149. 729
An introduction ia presented to several methods for ob-
taining reliable, precise, numerically computable
upper and lower bounds for a large class of problems
of the general nat jre of those mentioned in the title.
For definiteness, lonly certain specific boundary value
problems are considered in detail, althouRh the same
procedures can b< easily seen to be applicable in more
general situations . (Author)
A method of Fourier
applied for a
in inverse scaneiling
Institute of Matl^ematical Sciences, New York U
(N. v.]
ON AN INTEGR/ijL
SCATTERING, b»
AF 19(604)3495.
rept. no. EM- 15!
Order from LC
EQUATION ARISING IN INVERSE
C. H. Yang. Rept. on Contract
\pr 60, 34p. 5 refs. Research
ERD-TN -60-756; AD-244 089.
.00, ph$6.30 PB 152 431
nri$3
transforms and double series is
solution erf an integral equation arising
Institute of Tecli , U. of Minnesota, Minneapolis.
PERIODIC SOLU^ONS OF SINGULAR PERTURBA-
TION PROBLEMSi by Edward R. Rang. Doctoral thesis
Technical rept. li. 1. 15 Sep 56-15 Sep 57, on Prob-
lems in the Theory of Ordinary Differential and Dif-
ference Equations. Contract DA 11 -022 -ORD- 2042.
9 Oct 57, 88p. 29iref6. OOR rept. 1469. 1; AD-146 632
Order from LC nii$4. 80. ph$13. 80 PB 149 644
Kansas U. , Lawrence.
A METHOD FOR THE SIMULTANEOUS APPROXIMA-
TION OF EIGENVALUES AND EIGENVECTORS OF
A REAL SYMMETRIC MATRIX, by Peter C. Patton.
Technical rept. no. 24 on Studies in Eigenvalue Prob-
lems, Contract Nonr -583(04). 1959. 74p. 11 refs.
AD-231 184.
Order from LC mi$4. 50, ph$l2. 30 PB 152 894
The results of many numerical experiments with an
IBM 650 computer on a new method for approximating
the eigenvalues and eigenvectors of a real symmetric
matrbt are described. Although the numerical method
is general in nature and could be applied to non-
symmetric or complex matrices, the error analysis la
valid only for the real symmetric case. The numerical
experiments were performed only on sixth and eighth
order matrices due to limitations imposed by the small
size and slow speed of the computer used. The deter-
mination of the minimum conditions under which the
method will produce correct answers is considered.
Matrices with given eigenvalues were generated on the
machine and then reduced in different ways to deter-
mine the best usage of the method. The numerical ex-
periments indicate that the method essentially doublea
the number of accurate digits of the eigenvalues and
elements of the eigenvectors at each iteration.
(Author)
Laboratory al Statistical Research, U. of Washington,
Seattle.
SAMPLE FUNCTIONS OF STOCHASTIC PROCESSES
WITH STATIONARY INDEPENDENT INCREMENTS,
by R. M. Blumenthal and R. K. Getppr. Technical
rept. no. 34 on Contract Nonr-477(ll). 18 Jan 60, 4(^.
10 refs. AD-231 424.
Order from LC mi$3. 00, ph$6. 30 PB 152 900
Let X - lX(t); r>Ol be a stochastic process in Rfj with
sutionary independent increments. Problems of the
foUowii^ type concerning the sample functions of X are
considered: (I) local HOlder conditions; (2) conditiooa
under which the > -variation of X over [0. 1] is finite
(or infinite); and (3) the relationship between dim Hand
dim X(E) when E is a Borel subset of [0, 1). If X is a
stable process of index •. then the behavior of the
sample functions relative to these 3 properties can be
described in terms of the single parameter a. Param-
eters of this type are defined and investigated for the
general class of processes. (Author)
Lincoln Lab , Mass. Inst, of Tech. , Lexington.
A PROGRAM FOR TESTING SEQUENCES OF RAN-
DOM NUMBERS, by Leonard Kleinrock. Rept. on Con-
tract AF 19(604)7400. 25 Oct 60, 27p. 2 refs.
51G-0O18.
Order from LC mi$2. 70, ph»4 80 PB 152 934
This report describes a program written for the TX-2
Computer, which is capaible of testing the randomness
of sequences of numbers. A sequence of numbers is
defined as random if the numbers in the sequence are
identically distributed independent random variables.
The program performs a series of tests on the se-
quence, and displays the results of these tests on the
console oscilloscope. A description of each test is
given, along with instructions on how to use the pro-
gram. A set of appendices is also given which pre-
sents a portion of the theory applicable to these tests.
(Author)
320
Lincoln Lab. , Mass. Inst, of Tech. , Lexington. •
A SURVEY OF THE SIMPLIFICATION OF TRUTH
FUNCTIONS, by Willard Draisin. Rept, pn Contract
AF 19(604)7400. 20 Oct 60, 18p. 21 refs. 22G-0054;
AD-245 231.
Onler from LC mi$2. 40, ph$3. 30 PB 152 723
This report presents a survey of the progress made in
Qnding a short mechanical procedure for reducing a
truth function to its simplest equivalent. The simpli-
fication of a normal truth function using methods devel-
oped by Quine and Pet rick is described in detail. The
application of these methods of simplification to truth
functions used in controlling systems is discussed.
(Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
WEST FORD COORDINATE CONVERSION PROGRAM,
hyW. R. Crowther. Rept. on Contract A F 19(604)7400
1 Nov 60, 7p. 21G-0026.
Order from LC mi$ 1.80, ph$ 1.80 PB 153 053
A program has been written to accept points in radar
coordinates and convert them to points in an earth -
centered non- rotating system. This program will be
used to modify the output of the Point Selection pro-
gram to an acceptable input of the Orbit Determination
program. The gain in timing and simplicity make such
a conversion advisable.
Michigan Sute U. [East Lansing].
A BIVARIATE TCHEBYCHEFF INEQUALITY FOR
CERTAIN CONVEX SETS, by Albert W. Marshall and
Ingram Olkin. Interim technical rept. no. 12 on Con-
tract DA 20-01 8-ORD- 14735. 20 Mar 59, 30p. 5 refs.
OOR rept. 1840. 9M; AD-211 948.
Order from LC mi$2. 70, ph$4. 80 PB 149 663
This paper Is concerned with obtaining a bound for the
probability that a two-dimensional random variable
falls in a certain convex set.
Naval O&dnance Lali. , White Oak, Md.
AN EXISTENCE THEOREM FOR THE EQUATION
»xn^U by James Conlan. 12 July 60, 24p. 4 refs.
Kttthematics Dept. rept. M-12; NAVORD rept. 6921;
AD- 245 565. i
PB 171 349
Order from OTS $0. ^5
This paper proves an existence theorem for a boundary
value problem for the partial differential equation
Uxy2 =f(x,y,z,u, ux, uy,uz, uxy.uxz.uyz) ■ The method
of proof is such as to lead directly to a simple scheme
for the numerical solution of such a problem. (Author)
Naval Ordnance Lab. , White Oak, Md.
ON CIALCULATION SOLUTIONS OF QUASI- LINEAR,
FIRST ORDER PARTIAL DIFFERENTIAL EQUA-
TIONS, by Avron Doughs. I Sep 60, 26p. 9 refs.
Mathematics Dept. rapt. M-I3; NAVWEPSrept. 7254.
Order from OTS $0.76 PB 171 350
A common means to dalculate solutions of non- linear
hgrperbolic partial difflerential equations, when shocks
•re present, Is to introduce Into an otherwise straight-
forward difference scheme special terms which might
represent the action of a fictitious tempering mecha-
nism, perhaps at some dissipative type. Experience
seems to Justify the use of such "tempered" schemes,
but proofs of convergence are largely incomplete or
lacking. In this paper, in the case of a simple type of
equation, we shall give convergence proofs for a class
of explicit tempering schemes including versions of
the von Neumann- Richtmyer and the Lax-Wendroff
methods. These results supplement those of a previous
paper devoted to tempering schemes of implicit type
(and to an explicit scheme with linear viscosity). (Author)
Naval Ordnance Lab. , White Oak, Md.
ON THE CAPACITY OF THE ICOSAHEDRON, by
James ConUn, J. B. Diaz, and W. E. Parr. 1 Sep 60,
Up. 6 refs. Mathematics Dept. rept. M-I4; NAVWEFS
rept. 7302.
Order from OTS %0. 50 PB 171 354
The numerical estimation of the capacity is one of the
chief examples of the actual application of variational
methods. The main purpose of the present report is td
obtain upper bounds for the capacity of a regular solid
by means of a simple trail function. (Author)
Naval Ordnance Lab. , White Oak, Md.
THE SOLLTION OF THE CHARACTERISTIC AND
THE CAUCHY BOUNDARY VALUE PROBLEMS FOR
THE BIANCHI ^ARTUL DIFFERENTIAL EQUATION
IN n INC«PEMCKNT VARIABLES BY A GENERAU-
ZATION OF RIEMANN'S METHOD, by H. M. Sternberg
(Doctoral thesis) and J. B. Diaz. 27 July 60, 192p.
14 refs. NAVWEPS rept. 7264; AD- 246 796.
Order from OTS $3.00 PB 171 351
This report deals with a generalization of a well known
method, due to Riemann, for the solution of hyperbolic
differential equations. A large class of partial differ-
ential equations, containing three, and more, independ-
ent variables can be treated by the techniques developed
here.
Naval Ordnance Lab. , White Oak, Md.
UPPEIf AND LOWER BOUNDS FOR THE CAPACI-
TANCE OF THE REGULAR SOUDS, by Wallace E.
Parr. 28 Sep 60, 104p. 21 refs. Mathematics Dept.
rept. M-15; NAVWEPSrept. 7318.
Order from OTS $2. 50 PB 171 355
Upper and lower bounds are given for the Dirichlet
integral, principally based upon an extension of a
method of G. PGlya and G. Szegb. Numerical bounds
are calculated for the capacitance of the five regular
solids. In particular, it is found that the number 1 . 3351
is an upper bound for the capacitance of a cube of
side 2.0, an improvement over all upper bounds pre-
viously known. (Author)
Naval Ordnance Test Station. China Lake, Calif.
FIRST AID FOR PET PROJECTS INJURED IN THE
LAB OR ON THE RANGE OR WHAT TO DO UNTIL
THE STATISTICIAN COMES, by R. M. McClung.
29 Jan 52, 59p. 11 refs. Technical memo. 1113.
Order from OTS $1.50 PB 171 327
321
The concept of coilfidence, the use and computation of
confidence and tolerance limits, and a method for de-
termining the sigrtificance ol the difference in two or
more sample meajia are discusaed in an elementary
manner. (Author) ',
Numerical Analyjsis Research, U. of California,
Los Angeles . I
CX>MPLETE SYSlteMS OF SOLUTIONS FOR A CLASS
OF SINGULAR EtllPnC PARTIAL DIFFERENTIAL
EQUATIONS, by feter Henrici . Technical rept.
on Contract DA 04-495-ORD-559. 1 Feb 60, 22p.
9 refs. AD-232 3t8.
Order from LC ni%2.70. phj4.80 PB 153 275
Reprint from Boundary Problems in Differential Equa-
tions; Proceedings of a Symposium conducted by Mathe-
matics Research Onter, U. of Wisconsin,
19-24.
20-22 Apr 59, p.
Princeton U. [N. J. I
ANALYTIC SPACES. PART 1. by Hugo Rossi. Rept. on
Contraa AF 49(6$8)692. Feb 60, 88p. 8 refs. AFOSR
[TNl-60-283; AD-r234 814.
Order from LC ^$4.80, ph$13.80 PB 149 649
Contents:
Irreducible varietjies
Nullstellensatz
The density thectrem
The regular poiiits
The singular sec
Coherence of shelves
The density theorem
Coherence of th^ sheaf of a ve riety
Abbildungsatz
Purdue U. , Lafayette, Ind.
GROUP COMMUtATORS OF BOUNDED OPERATORS
IN HILBERT SPACE. byC. R. Putnam. Technical note
no. 12 on Commutators on a Hilbert Space, Contract
AF 18(603)139. C^t 60, 6p. 4. refs. AFOSR -TN -60-7 1 8
AD-245 344.
Order from LCnjil 1.80, ph$1.80 PB 152 761
Various conditior* on operators A and B in order that
AD=OA. where 0=ABA-1B-1, implies AB - BA are
discussed. (Author)
Purdue U. , Lafayette, Ind.
A NOTE ON THE SPECTRA OF GROUP COMMUTA-
utnam. Technical note no. 13 on Com
rt Space. Contract AF 18(603)139
AFOSR -TN -60-744; AD-245 343.
ii$1.80, ph$1.80 PB 152 762
TORS, by C. R.
mutators on a Hi
Oct 6a 6p. 8 r
Order from LC
There are obuir
trum of ABA'^bH
(Author)
results on the location of the spec -
in case A commutes with AB - BA.
Rensselaer Poiy|echnic Inst. , Troy, N. Y.
LINEAR DIFFERENTIAL EQUATIONS WITH RAN-
DOM NONHOMOOENEITIES, by William E. Boyce.
AF 18(600)1586. 17 Dec 59. 12p.
29: AFOSR TN-.59- 1260; AD- 230 946.
Rept. on Contract
RPI MathRep no
Order from LC ml$2. 40. ph$3. 30
PB 153 382
A method Is proposed for dealing with the effects of
certain types at random perturbations In systems
governed by linear differential equations. When these
perturbations occur as a nonhomogeneous term tn the
differential equation, the solution is represented by
means of an integral Involving the random nonhomo-
genelty. both for boundary and Initial value problem!.
This integral can be commuted with the integrals rep-
resentit^ statistical moments. Several consequences
of this fact are discussed. (Author)
Syracuse U. , N. Y. v-
ITERATIONS WITH ERRORS, by Peter Frank. Re-
search rept. 28 on Contract AF 49(638)265. Aug 60.
I7p. 5 refs. AFOSR-TN-60-1095; AD-245 277.
Order from LC mi$2. 40. ph$3. 30 PB 152 736
Let M be a complete metric space, and T a transfor-
mation of M into itself. There are seven sections: (1)
M a complete metric space, no errors. A statement
of the contracting mapping theorem; (2) M a complete
metric space, bounded errors. Bounds for the accu-
mulated error. (3) M the real numbers, errors ran-
dom. Existence of a limiting distribution; (4) M a
Banach space, errors random. Existence of a limiting
distribution; (5) Markov processes and integral equa-
tions; (6) M a Banach space. T a linear transformatiaii
Characteristic functiona; (7) M the real numbers,
errors bounded. Bounds on the asymptotic bias and
mean square error.
Syracuse U., N. Y.
ON THE MEASURABILITY OF FUNCTIONS IN TWO
VARIABLES, by Mark Mahowald. Research rept. no.
29 on Contract AF 49(638)265. Aug 60. 8p. 4 refs.
AFOSR -TN -60- 1096; AD-245 278.
Order from LC mi$l. 80. ph$l. 80 PB 152 737
This report contains two sections, each essentially
independent of the other. In (1) the question of joint
measurability of a function of two variables given con-
tinuity in one and another condition is studied. The
main result is a general theorem on metric compact
spaces. (2) is concerned with the existence of a meas-
urable modification of a given stochastic process.
Necessary and sufficient conditions are obtained.
(Author)
University of Southern California (Los Angeles].
A NON-LINEAR EIGENVALUE PROBLEM FOR HAR-
MONIC FUNCTIONS, by John A. Ferling. Technical
rept. on Contract Nonr- 348(09). Mar 60. 11 refs.
AD- 237 809. ^
Order from LC ml$3. 60, ph$9. 30 PB 148 066
A non- linear eigenvalue problem related to the linear
problem is considered. In the linear problem, a func-
tion u ia to be found which is a regular harmonic fuac-
tion in a region D and which satisfies, on the boundary
of D. the condition (tju/^n) ■ -.AjU. where ^j is a real
poaitive parameter and n the inward normal. In the
non -linear problem, the boundary condition is replaced
by Ou/dn) - - A«(u) with f(u) being the sum of the
linear part u and a non-linear part g(u) = Au^ * u3h(u),
where A ia a constant and h(u) a continuously differen-
tiable funaion. Let AiP be the values of Ai for which
322
ibe Unear problem has solutions. The non-linear prob-
lem If investigated for values of the positive parameter
Tuear theAjP.
Washington U. , St. Louis, Mo.
C»^ REAL CHARACTERS OF CERTAIN SEMI-GROUPS
WITH APPLICATIONS. Jjy Allen Devinatz and
A. E. Nussbaum. Rep^)n Contract AF 49(638)218 and
National Science Foundanbn Grant NSF-G10715. June60,
2«p. 10 refs. AFOSR-TN-60-642; AD-245 119.
Order from LC miJ2. 70, ph|4. 80 PB 152 747
Washington U. , Seattle. Div. of Counseling and
Testing Services.
AN IBM TYPE 650 PROGRAM FOR COMPUTING
CORRELATION COEFFICIENTS BETWEEN PAIRED
VARIABLES, by Leon Muhlick, I*rem Shanker, and
August Dvorak. Rept. on Contract Nonr- 477(08) and
Public Health Research Grant M-743(C5). Mar 60, Up.
3 refs.
Order from LC mi$2. 40. ph$3. 30 PB 148 609
I
Wayne State U. (Detroit, Mich.)
PROBLEMS ON CONFORMAL MAPS OF RIEMANNIAN
AND KAEHLERIAN MANIFOLDS, by S. 1. Goldberg.
Rept. on Contract AF 49(638)14. July 60, 21p. 11 refs.
AFOSR TN-60-867; AD'244 303.
Order from LC mi$2.70, ph$4.80 PB 152 436
Some problems on conformal maps c^ Riemannian and
Kaehlerian manifolds ai|e studied. Let M*^ be a com-
pact and orientable Rieihannian manifold with metric g
on which there is defined an harmonic p-form a whose
coefficients ai| . . . !„ saliisfy the property (P):
l2-ip
•« 'Ji2.
H(m,p).
I m gjj. Such a space is called an
Computing Devices
International Business Machines Corp., Kingston,
N. Y.
QRCUITS AND COMPONENTS IMPROVEMENT PRO-
GRAM, ECPX 0002. Final rept on Contract AF
30(635)3130. 1 Jan 58. 52p. AD- 150 401.
Order from LC m43.60, ph»9.30 PB 153 274
(Contents:
Circuits and components improvement program
Transistor component evaluation and circuit design
Magnetic core and core circuit development
Seiniconductor component development and application
Printed circuits and components
Component reliability study
Tabulated results
Lincoln Lab. . Mass. Inst, of Tech. , Lexington.
GENDARE SYSTEM FUNDAMENTAL CONCEPTS OF
LOGIC AND STRUCTURE, by J. B. Williams, Jr. Rept
OB Contract AF 19(604)7400. 17 Oct 60. 20p. 22G-0042;
AD-245 234.
Order from LCmi$2. 40. ph$3. 30 PB 152 722
GENDARE (Generalized Dau Reduction) is a program-
ming system to provide data reduction services easily
and cheaply when large volumes of data are to be
processed. GENDARE design starts with the observa-
tion of logical redundancies in the class of programs
devoted to data reduction. On this basis the existence
of a general case for this program class is postulated,
assumptions made about the form of the inputs, and
determining characteristics discussed for the process-
ing to be performed. From this foundation the funda-
mental elements of GENDARE logic and structure are
developed as a natural consequence. (Author)
Moore School of Electrical Engineering, U. of
Pennsylvania, Philadelphia.
HUMAN FACTORS CONSUL RATIONS IN THE DE-
SIGN OF ELECTRONIC COMPUTERS, by R. O. Lucier
and E. J. Parker. Final rept. for 1 July 59-30 June 60
on Task B, Contr.act DA 36-039-8C-75047. 30 June 60,
53p. 8 refs. AD60UR1; AD-243 632.
Order from LC mi$3.60, ph$9. 30 PB 153 596
This report released for sale to the public 6 Jan 61 .
The necessity of considering the human element in the
design of computer equipment, especially in the design
of the operators' consoles for the FEELDATA equip-
ment family is discussed. The main text is- divided into
three sections, which are concerned with the design of
operators' consoles, the use of human factors by pro-
ducers of electronic compHJters, and the consideration
of the human component of man-machine relationships
in the area of ADPS. Several arguments are put forth,
one of which is the need to standardize various aspects^
of design in the control panels of consoles. Another
fact that the author points ouMi the problem of ADP
personnel - the growing neec^for programm'^rs and the
dwindling source of manpower, the high production of
computers and the inability to find enough personnel to
handle them. The appendix is concerned with various
aptitude and psychological tests administered to people
in ADPS. It discusses and compares the tests and the
results of such tests. (Author)
Moore School of Electrical Engineering, U. of
• Pennsylvania, Philadelphia.
INFORMATION RETRIEVAL AND THE DESIGN OF
MORE INTE LUCENT MACHINES, by Harry J.
Gray, Jr. and Edward J. Parker. Final rept. for
1 July 59-30 June 60 on Task E, Contract DA 36-039-
8C-75047. 30 June 60, 77p. 8 refs. AD60UR1;
AD-243 490.
Order from LC mlM.50, ph$l2.30 PB 153 597
This report released for sale to the public 6 Jan 61 .
Existing digital computers and data processing sys-
tems require exceptionally competent and Intelligent
people for their programming, operation, and main-
tenance. In order to reduce the requirements on the
personnel it becomes necessary to design the machines
so that they have more intelligence. The first effort
toward enabling the machine to make its own associa-
tions gave rise to the information pTOceaaing languages
of Newell and Simon. Our study of the operations in-
volved in human cognitive process has resulted in an
extension of the Newell-Simon Information Processing
Languages (IPL) to a multiple hst data organization
323
t
where each data itfm appears only once in an address-
able memory, yet the item has m it several descrip-
tOTS with control ikormation that place the data item
in several lists, aich a system has been shown to be
well-suited to inf^maiion retrieval problems. A
specification of a ^rallel-access information bank,
which may be more efficient than the multiple- list
system, has been previously prepared. Central to the
list machine and tie parallel-access information-bank
problem, is the prtoblem of descriptor recognition. In
this report, the pijoblem is defined and progress
towards its solutiqn is stated. (Author)
Moore School of Electrical] Engineering, U. <rf
Pennsylvania, Philadelphia.
LINEAR BOUNDED AUTOMATA, by John Myhill.
Rept. on Automatib Computation and Control Tech-
niques. Contract Af 33(616)5886. June 60. 29p. 6refs.
Rept. no. 60-22; WADD Technical note 60- 165.
Order from OTS jb. 75 PB 171 339
This report preserits a new concept, that of a linear
bounded automator^. Such automata can do more than
finite automata, biit cannot do as much as TUrlng
machines. A full 4lscussion of the concept is given,
followed by a prooj that all classes of tapes d a certain
kind are represenUable by linear bounded automata.
The report concludes with a proc* that all classes o#
tapes representatie by linear bounded automata are
primitive recursive. (Author)
Naval Research Lab. , Washington, D. C
A SEMICONDUCTOR BINARY COORDINATE CON-
VERTER, by M. F. Williams, A. F. Thomhill, and
W. A. Richards. jFinal rept. on one phase. 16 Nov 60,
I5p. 5 refs. NRu'rept. 5534.
Order from LC mtt2. 40, ph$3. 30 PB 149 297
The characteristics of a semiconductor binary digital
coordinate converter have been investigated. This
equipment conver(s 18-bit polar-coordinate data to 20-
bit rectangular -cdordinate data in three milliseconds.
The equations used are: X* /& sin ^ and Y" A cos <^.
Sine 6 and cosine!^ are obuined by the use of a rec-
ungular diode matrix and diode trigonometric function
Mbles; X and Y aie obtained by summing partial prod-
ucts in a parallel laccumulator type multiplier. The
converter occupiejs a volume of less than two cubic feet
and requires one kmpere at 20 volts and 200 milli-
amperes at 90 vo|t8. Methods of increasing the operat-
ing rate of the converter have been considered. (Author)
MECHANICS
Illinois Inst, of JTech. , (3iicago.
PLASTIC PRINClfLES OF MINIMUM ENERGY RATES
by Philip G. Hodgfe, Jr. Rept. on Contract Nonr 140604
Mar 60. I2p. 14^efs. DOMIIT rept. no. 1-11;
AD- 236 999. .
Order from LC n|i$2. 40, ph$3. 30 PB 147 310
Two new minimuip principles are proved for an
elastic/plastic material. (1) Among all compatible ve-
locity fields the alctual one minimizes the instantaneous
change in the potential energy. (2) Among all equilib-
rium stress rate fields which do not violate the yield
condition, the actual one minimizes the instanuneous
change in the complementary energy. (Author)
Institute for Fluid Dynamics and Applied Mathematics
U. of Maryland. College Park.
A NEW DECOMPOSITION FORMULA IN THE
THEORY OF ELASTICITY, by J. H. Bramble and
L E. Payne. Rept. on Contract AF 49(638)228. Sep 60^
15p. 7 refs. Technical note BN-218; AFOSR-TN-60-
1129; AD-244 833.
Order from LC mi$2. 40. ph$3. 30 PB 152 609
A new representation formula for the spherical com-
ponents <rf displacement in the theory of elasticity is
obtained. This formula may be used to reduce mixed
boundary value problems for the elastic sphere to
standard problems in potential theory. (Author)
Institute of Engineering Research, U. of Cahfornia,
Berkeley.
PROPAGATION OF AXISYMMETRIC WAVES IN AN
UNLIMITED ELASTIC SHELL, by A. Kalnins and
p. M Naghdi. Technical rept. no. 8 on Contract Nonr-
222(69). Mar 60, 21p. 15 refs. Series 131, issue 8;
AD- 238 156.
Order from LC ml$2.70. ph$4.80 PB 148 405
The propagation of axisymmetric stress waves in un-
^mited thin shallow elastic spherical shells is investi-
gated. In particular, a solution is obtained for an un-
limited shallow spherical shell subjected to a harmoni-
cally oscillating concentrated load at the apex. This
solution, ex&a within the scope of the linear theory of
shallow shells, has an outward propagating wave char-
acter in the entire range of forcing frequency. Appro-
priate expressions for the mechanical impedance and
the energy input are derived, and numerical results
are obtained for the axial displacement corresponding
to various forcing frequencies. (Author)
Institute of Mathematical Sciences, New York U. ,
N Y
A THEORY FOR THE SMALL DEFORMATIONS OF
CYLINDRICAL SHELLS. PART I. ROTATIONALLY
SYMMETRIC DEFORMATIONS, by Edward L. Reiss.
Rept. onContraa Nonr-285(42). July 59. 35p. 16 refi.
IMM-NYU 260; AD- 229 513. .
Order from LC mi>3. 00. ph$6. 30 PB 149 691
Mathematics Research Center. U. (rf Wisconsin,
Madison.
PLANE ELASTIC SYSTEMS, II. THE COMPLEX
STRESSES AND THEIR PROPERTIES IN THE ISO-
TROPIC CASE, by L. M. Milne -Thomson. Rept. on
Contract DA 11-022-ORD-2059. Dec 58, 4lp. 10 refs.
MRC Technical summary repc. no. 63.
Order from LCml$3. 30, ph$7.80 PB 149 756
The report which follows aims to describe and unify tte
properties of the two funaions of the complex variable
in terms of which the solution of plane problems may
be expressed in the case of Isocropic material under-
going infinltesinuil elastic deformation. As the report
324
in effect deals with plane geometry it is more con-
venient and intuitive to refer to the material as if it
were in the form of a thin plate. In so doing there is
no loss of generality, for one can proceed from this ■
case of generalized plane stress to the case of plane '
deformation by a mere change in the value of the
elastic constant.
Naval Ordnance Test Station, China Lake, Calif.
TRANSVERSE VIBRATIONS OF THIN RECTANGULAR
ISOTROPIC PLATES, by Ralph W. Claassen and Charles
J. Thorne. 18 Aug 60. 187p. 7 refs. NOTS TP 2379;
NAVWEPS rept. 7016.
Order from LC mi(8.40. ph$28.80 PB 152 632
A general method for the solution of boundary value
problems is illustrated by developing the formulas nec-
essary for determitiing the frequencies and nodal pat-
terns in the free vibrations of thin rectangular plates.
Numerical results are obtained for two frequently oc-
curring boundary conditions: clamped all around and
clamped on two opposite edges, free on two opposite
edges. Curves are given for the determination of the
"first" ten and eleven frequencies, respectively, and
their nodal patterns as a function of the ratio erf sides.
The parameter K, which determines the frequency an4
nodal patterns, is independent of Young's modulus,
density, thickness and Poisson's ratio in the first ex-
ample. In the second example Poisson's ratio of . 3 is
i»«i to determine K. K is expected to be only slightly
dependent on Poisson's ratio. (Author)
Pennsylvania State U. , fifiiversity Park.
RESEARCH AND DEVELOPMENT ON THEORETICAL
Alto EXPERIMENTAL STUDIES ON MECHANICS OF
METAL FORMING, by Ow^n Richmond, L. W. Hu,
and Joseph Marin. Final rept. on Contract DA 36-oi61-
ORD-435. 1 Sep 55, 80p. 20 refs.
Order from LC mi$4. 50, pli$l2. 30 PB 153 109
Experimental studies of the plastic deformation of a
Oat place compressed between flat plates, the plastic
indentation of a billet by a wedge and the plastic inden-
tation of a billet by a cone. Measurements were made
of the total applied load, total deformation, pressure
distribution on the die surface and strain distribution
within the billet. The test results were interpreted by
• plasticity theory which neglects the elastic deforma-
tions and assumes no strain hardening. The theory was
found to be suitable for the interpretations of the test
results obtained in this study.
Polytechnic Inst, of Brooklyn. N. Y.
ON THE DYNAMICS OF PLASTIC SPHERICAL
SHELLS, by R. Sankaranarayanan. Rept. on (Contract
AF 49(638)302. Sep ift, 23p. 9 refs. nBAL rept. no.
580; AFOSR-TN-60-1165; AD-244 945.
Order from LC mi$2. 70. ph$4. 80 PB 152 779
This paper discusses the behavior of complete spheri-
cal shells and simply supported spherical caps under
impulsive loading by uniform external pressure. The
pressure is assumed to be greater than the static col-
lapse pressures and to act for a short period of time.
The displacements of the shells are presented for par-
ticular values of the parameters of the problem.
(Author)
Aeroci)rnamics and Pneumatics
Arnold Engineering Development Center [Tullahoma,
Tenn.]
THE DESIGN AND EVALUATION OF A TRANSIS-
TORIZED CURRENT AMPUFIER WITH A BAhD-
WIDTH OF DC TO 100 KC, by W. M. Crouch. RepC.
on ARO, Inc. Contract AF 40(600)800 S/A 11(60-110).
Oct 60, 24p. 5 refs. AEDC-TN-60-194.
Order from LC mi$2.70, ph$4.80 , PB 152 843
Analog dau are transmitted from the operating wind
tunnels of the VKF to a magnetic tape system for re-
cording via co-axial transmission lines . To insure that
these dau, when rteeived by the magnetic tape system,
are accurate reproductions of the transmitted signal,
the co-axial lines must be properly terminated in a low
impedance. The amplifier which drives these lines
should have a response of dc to at least 100 kc m order
not to limit the data transmission below the capabilities
of the magnetic recording system. Both of these qual-
ities . low output impedance and the necessary frequency
response, are incorporated in the transistorized
current amplifier which is described in this report.
Design, performance, operation, and evaluation are
discussed. (Author)
Arnold Engineering Development Center [Tullahoma
Tenn.]
FORCE TESTS OF AN AGARD CALIBRATICHM
MODEL B AT M= 2.5 TO 6.0. by Jack D. Coats.
Rept. on ARO. Inc. Contract AF 40(600)800 S/A 11(60-
110). Oct 60, 30p. 7 refs. AEDC-TN-60-182.
Order from LC mi$2.70, ph$4.80 PB 152 S56
An AGARD Calibration Model B body-wing configuration
was tested in the 40-ln. sufiersonic wind tunnel (Tun-
nel A) of the von Karman Gas Dynamics Facility.
Force and moment coefficients were deteriTiiiled over a
range of pitch and yaw angles from -4 to HO deg at
Mach numbers from 2.5 to 6.0. The Reynolds number
range was from 2 x 10^ to 24 x 10^ i>ased on body
length. The lift and pitching- moment characteristics
(rf the 5. 8-in. -diam model used in these tests are in
good agreement with results obtained earlier on a 2-in.
model tested in the 40-in. tunnel and a 1.4-in. model
tested in the 12-in. tunnel at the von Karman Facility.
The forebody drag coefficients for the 5. 8-in. -diam
model are in general lower than those for the smaller
models. Variations in Reynolds number were not of
sufficient magnitude to produce turbulent flow over
more than 55 percent of the body length and produced
only small variations in the drag coefficients with no
effect on the lift and pitching- moment coefficients.
The rates of change of the location of boundary layer
transition with Reynolds number were identical to
those determined in the 12-in. tunnel and were influ-
enced by the presence of the wing. (Author)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
LIGHTNING STORM IN A SUPERSONIC WIND TUN-
NEL, by Anders S. Platou. Aug 60, 25p. Rept. no.
1113; AD-244 819L.
Order from LC mi$2. 70. ph$4. 80 PB 152 602
325
This is a study of in electrostatic charge which is gen-
erated in a supersonic tunnel when the air flowing
eirough the De Lavial nozzle conuins a considerable
amount of water vapor. If a pointed probe which is
electrically grounqed is mounted in the air stream a
purple glow exists on the tip of the probe. If the probe
is inaulAted from ground a positive pocentiAl of several
tticwi— ml volts accumulates on the probe. The amount
of charge which accumulates is a function of the humid
ity level of the air and the position erf the probe in the
nozzle. (Author)
Boh Beranek and Newman, Inc., Cambridge, Mass.
RESPONSE OF PLATES TO MOVING SHOCKS, by
Eric E. Ungar. R*pt. on Dynamic Problems In Fhght
Vehicles. Contract AF 33(616)6217. Aug 60, 37p.
ISrefs. WADD Technical rept. 60-445.
Order from GTS $1.00 PB 171 302
General expressions for plate responses to pressure
variations are derived in terms of generahzed coordi-
nates associated with the plate normal mode-shapes.
The expressions are then specialized for moving pres-
sure dlscontinuitiete, which correspond to shocks. The
responses of simple supported rectangular plates to
uniformly moving fcnd to slnusoidally and randomly
oscillating shocks are determined in detail for shocks
parallel to a pair <>f edges. The importance of the
mechanisms of tr^ce-maiching, force-resonsnace,
and moment-resortance, is established. (Author)
I
Catholic U. of Alperica, Washington, D. C.
ELEMENTARY MECHANICS OF TURBULENT FLUID
MOTION, by Max M Munk. Rept. on Contract
AF 49(638)516. MUr 60. I50p. 13 refs. AFOSR-TR-
60-6; AD- 235 018.;
Order from LC m^7.20, ph$22.80 PB 149 686
I
Order and system I in the happenings of turbulent fluid
motion was analyaed. A system of, turbulence mechan-
ics was establish^l having many good features. It is
complete in that tljere are enough equations in relation
to the unknown invtolved. The independent variables
from a harmonious and plausible system, which can
hardly be improved without enlarging it The equations
are expressed an(| very simple. Two principal coeffi-
cients are shown l|o be often constants. They are the
shear coefficient r/K/>and the rotation coefficient
S dU/dy/v/ They tillustrate the separation of the dy-
namic effects and Ithe diffusive effects taking place.
Results show that Ithe 2 principal turbulence effects
have little inclina^on to combine to Joint aaion. The
analysis was carried far enough for establishing even
the numerical information needed, although only
provisional, and Subject to revision and refinement.
The order of mag^tude of the major multipliers was
definitely established. (Author)
I
Cornell Aeronautjical Lab., Inc., Buffalo, N. Y.
HEAT TRANSFER TO SHARP AND BLUNT YAWED
PLATES IN HYPEHSONIC AIRFLOW, by J. G. Hall and
T. C. Golian. Reft, on Contract AF 18(603)10. Sep 60,
no. AD-1052-A-11: AFOSR TN-
9p. 5 refs. Rept
60-938
Order from LCmM- 80. ph$1.80
PB 152 947
The purpose of this note Is to report recent experi-
mental results for heat-transfer distributions over
sharp and blunt plates at yaw with zero angle of attack.
, • , I .,
Israel Inst, of Tech. , Haifa.
ON ROTATIONAL SUPERSONIC FLOW PAST THICK
AIRFOILS: TABLES, by A. Koganand A. A. Betser.
Final rept. on Contract AF 61(052)281. June 60, 78p.
I ref. AFOSR-TR-60-135; AD- 244 457.
Order from LC mi$4.50. ph$12.30 PB 152 479.
Certain shock wave parameters , which appear in the
calculation of pressure distribution on airfoils in a
supersonic rotational flow, are presented in tabular
form. The method underlying the use of the tables is
sunrunarized and discussed. A numerical example is
worked out in detail, illustrating the procedure to be
followed in the application of the tables . (Author)
National Research Labs. , Ottawa (Canada).
AERODYNAMIC SOUND AND PRESSURE FLUCTUA-
TIONS IN A SUPERSONIC BLOWDOWN WIND TUNNEL,
by R. Westley. Jan 60, 62p. 18 refs. Aeronautical rept
LR-274; 4P-244 858.
Order from LC mi$3. 90. ph$10. 80 PB 152 529
An investigation was made of the pressure flpctuations
in the settling chamber and working section and of the
exterior sound fields of the N. A. E. 5-inch supersonic
blowdown wind tunnel. Intense pressure fluctuations
were found in the settling chamber of the wind tunnel.
These fluctuations were a function of the flow condition!
at the control valve which suggested that they were
aerodynamic noise originating from the Jet of the con-
trol valve. Below a working section Mach number of 3,
the fluctuations in the working section were found to be
predominantly those which had been transmitted from
the settling chamber. The attenuation of the trans-
mission increased with Increase of working section
Mach number and at Mach numbers greater than 3 the
working section fluctuations became almost independent
of the fluctuations in the settling chamber. The sound
field surrounding the wind tunnel and the sound pressurt
levels at the exit of the exhaust diffuser were also
measured. (Author)
National Research Labs . , Ottawa (Canada).
DESCRIPTION OF THE SPRAY RIG USED TO
STUDY HEUCOPTERS IN FUGHT, byD. L. Bailey.
Sep 60, 21p. 1 ref. Aeronautical rept. LR-186A.
Order from LC mi$2.70, ph$4.80 PB 153 195
A description of the spray rig used to study icing on
helicopters in hovering flight. Details of operation,
instrumentation and the calculated performance are
given. (Author)
National Research Labs . , Ottawa (Canada).
THE STATIC AND FORWARD SPEED TESTING OF
A FLAPPED WING WITH BOUNDARY LAYER CON-
TROL FOR USE IN DEFLECnNG PROPELLER
SUPSTREAMS DOWNWARD FOR VERTICAL TAKE-
OFF. PART I, byB. Neal. July 60, 127p. 11 refs.
Aeronautical rept. LR-288.
Orderfrom LCmi$6.30. phJ19.80 PB 153 1«
326
Force and moment data ar^ presented for a four-pro-
peller model of a slipstreaqi deflection type VTOL
aircraft wing employing a ^'lotted forward flap to-
gether with a plain rear flap over which boundary
layer control air was blown. Tests were performed
out of ground effect both st4tically and at forward
speed for a wide range of ffap settings on a mobile
test rig that can be towed at speeds up to 50 ft ./sec.
The mobile test rig developed at this laboratory is
a useful tool for research ihto low speed flight and it
enables transition nnanoeuvres of VTOL aircraft to be
studied successfully. Useful improvements in the
perfornruince of slipstream deflection VTOL aircraft
can be made by the use of hbundary layer control over
the flap system. (Author) t
Naval Supersonic Lab. . Mass Inst, of Tech. ,
Cambridge.
INITIAL CALIBRATION OF THE HYPERCORE IN-
STALLATION AT M«7.6, by Jacques A. F. Hill.
Rept. on Contract Nonr- 1841(40). Mar 60, 35p. 6 refs
Technical rept. 437: AD- 239 875.
Order from LC mi$3. 00. ph$6. 30 PB 149 344
The Mach number and stagi>ation temperature distribu-
tions obtained in the calibration of a 12- inch diameter.
M>7.6 nozzle are presented. Model blockage limits
•re given for axisymmetric models at zero yaw and for
low-aspect- ratio wings at large angles of attack. Brief
descriptions are also given the (unconventional) tunnel
circuit and the nozzle design and fabrication processes
(Author)
Polytechnic Inst, of Brooklyn, N. Y.
HIGHER ORDER THEORY OF CURVED SHOCK, by
Ruben R. Chow and Lu Ting. Rept. on Aerodynamic
and Heat Transfer Problems in Hypersonic Flow, Con-
traaAF 33(616)6118. Aug 60, 30p. 11 refs. PIBAL
rept. no. 609; ARL Technical note 60-142.
Order from LC mi$2.70, pW4.80 PB 152 537
The next order conditions (of order of the reciprocal of
Reynolds number) across a two-dimensional shock have
been established to include the effects of heat conduc-
don, viscosity and the shock structure. These shock,
conditions involve the local shock curvature in addition
to its local inclination. Explicit resuhs have been ob-
tained for the corrections in the mass flux across the
shock, the stagnation enthalpy, the tangential compo-
nent of velocity and the normal component of momen-
tum flux. Numerical results are presented for Prandtl
number equal to 3/4. (Author)
Princeton U. . N. J.
THE ANOMALY IN THE APPLICATION OF PLK AND
PARABOLIC COORDINATE$ TO THE TRAILING EDGE
BOUNDARY LAYER, by Arnold Goldburg and
Sin- 1 Cheng. Rept. on Contract AF 49(638)465. Apr 60.
Up. 9 refs. Rept. 519; AFOSR -TN- 60- 650.
Order from LC mi$2. 40, ph$3. 30 PB 152 738
The application of the PLK method to the leading edge
of a flat plate predicted the well known optimum para-
bolic coordinate system for boundary layer analysis.
Ibe coordinate system applicable to the trailing edge
problem as predicted by the PLK method is found to dif-
fer from the conventional parabolic boundary layer co-
ordinates by an order of magnitude. (Author)
Princeton U. , N. J.
ON THE FLOW OF GASES UNDER NEARLY FREE
MOLECULAR CONDITIONS, by D. Roger Willis. Rept.
on Contraa AF 49(638)465. Dec 58, 92p. 21 refs. Rept
no. 442; AFOSR-TN-58-1093; AD- 207 594.
Order from LC mi$5.40, ph$15.30 PB 149 677
The present study is part of a program of theoretical
and experimental research in high speed gas dynamics.
Various methods of analysis of Boltzmann's equation
are discussed, with emphasis on those applicable when
the gas medium is sufficiently rarefied that conditions
are close to free molecular .
University of Southern California. Engineering
Center, Los Angeles.
HEAT ADDITION TO A ONE -DIMENSIONAL SUPER-
SONIC FLOW INCLUDING REAL GAS EFFECTS, by
Serge Albert Waiter. Rept. on Contract AF 40(600)857.
Sep 60, 33p. 3 refs. USCEC-R-73-201; AEDC TN-
60-180.
Order from LC ml$3.00, ph$6. 30 PB 152 557
The thermodynamic study of heat addition process in a
supersonic flow is presented, taking account of the
effects of dissociation and ionization; the only hypothe-
sis proposed is that the flow is in thermodynamic
equilibrium at each point. The specific mechanism of
the heat source is not given in detail in this paper, but,
it will be supposed that the heat added to the system is
steady and consunt per unit distance along the nozzle
axis. (Author)
Hydrodynamics, Hydraulic*, and Hydrostatics
Brown U. Div. of Applied Mathematics, Providence,
R. I
INVISCID MODES OF INSTABILITY IN COUETTE
FLOW, by W. H. Reid. Technical rept. no. 30 on
Contract Nonr-562(07). Jan 60. 27p. 6 refs.
Order from LC mi$2.70, ph$4.80 PB 152 857
An exaa solution is presented for the Invtscld modes at
instability in Couette flow. When the cylinders rotate
in the same direction, only one mode of instability is
present. It corresponds to the convectlve modes found
in the existing viscous treatments of the problem.
When the cylinders rotate in opposite directions, how-
ever, two types of insubility are present, the second
being of an oscillatory type. These results suggest that
although the "principle of exchange erf stabilities' may
be valid when the cylinders rotate in the same direc-
tion, it may not be valid when they rotate in opposite
directions. (Author)
327
Brown (J- Div. of Applied Mathematics, Providence,
R. I. I
THE STABILITY OF NON-DISSIPATIVE COUETTE
FLOW IN THE PRESENCE OF AN AXIAL MAG-
NETIC FIELD, b* W. H. Reid. Technical rept. no. 31
on Contract Nonr^562(07). Jan 60, 7p. 3 refa.
Order from LC m4$1.80, ph$1.80 PB 152 858
The effect of an axial magnetic field on the stability
characteristics ofjCouette flow in the limiting case of
zero viscosity anq infinite conductivity has been ex-
amined recently by Chandrasekhar, who showed that an
adverse gradient of angular velocity can always be
stabilized by a sutflciently strong magnetic field and
that the required Qeld strength can be derived from the
solutions at the reilated non- magnetic problem. Within
the framework ai the "small gap" approximation, the
non -magnetic problem has recently been solved ex-
actly, and this paAer, therefore, presents a deter-
mination of the magnetic field strength required to
completely stabilize the flow.
California Inst.
CAVITATING Fl
CULAR ARC HYI
Contract Nonr-2i
neering Div. rept.
Tech. , Pasadena.
>W PAST A CASCADE OF CIR-
IROFOILS, by A. J. Acosta. Rept. on
24). Mar 60, 40p. 8 refs. Engi-
no. E-79-2; AD- 237 442.
00, ph$6. 30 PB 147 535
Order from LC mtt3.
A linearized theory was presented of the cavltating
flow through a cascade of circular arc hydrofoils. Only
the case cA cavitiek of infinite length was treated. Nor-
mal force coefflclfnts are given for a range of stagger
angles and angles of attack for a camber of 16^. Com-
parison of the resbhs of the linear theory with an exact
theory for flat plale cascades indicates that the theory
ia limited to values of the stagger angle of about 60^,
at least for an ang^e of attack of 6^. Solidity is ob-
served to have a dominant effect on the normal force
coefficient, although, when the angle of attack is meas-
ured from the me^n of the entering and leaving angles,
the discrepancy frfam the results of isolated theories is
sharply reduced. No appreciable cascade effect occurs
up to about a soUd|ty of one half if the angle of attack is
■o determined. (Aiuthor)
David Taylor Moiel Basin, Washington, D. C.
A 36- INCH VARIABLE PRESSURE WATER TUNNEL,
by W. F. Brownell.I June 56, 78p. 9 refs. Rept. 1052.
Order from LC mi$4.50, ph$12.30 PB 153 574
This report released for sale to the public 6 Jan 61 .
A new 36-inch variable pressure water tunnel for the
David Taylor Moddl Basin is described. Design infor-
mation concerning the tunnel components, electric
drives, instrumenqation, auxiliary equipment and the
building is presented. (Author)
James Porrestal Research Center, Princeton, N. J.
TURBULENCE THEORY AND FUNCTIONAL INTE-
GRATION, by Gerald Rosen. Rept. on Contract Nonr-
1858(25). July 59. pp. 14 refs. ProJ. Squid Technical
rept PR-96-P. [
Order from LC mi$2. 70, ph$4 80 PB 149 689
An integral representation of the general solution to
the Hopf ^-equation is reported. Integral representa-
tions for the spatial correlation functions are derived
from the characteristic functional f . These exact re-
sults are ai^lied to Navier -Stokes fluid turbulence.
(Author)
Technische Hog&school, Delft (Netherlands).
UNSTEADY MOTION OP A FLAT PLATE IN A
CAVITY FLOW, by J. A. Geurst. Rept. no. 21 on Cos
tract N62558-2269. June 59. 42p. 18 refs. AD-225975.
Order from LC mi$3. 30, ph$7. 80 PB <i49 640
A flat plate is placed in a flow of an incompressible
non-viscous fluid with uniform velocity perpendicular
to the plate. Behind the plate a cavity with reentrant
Jet has formed. The jet is supposed to disappear on a
second sheet of the physical plane considered as a Rle-
mann surface. This artifice is used to represent with-
in the framework of potential theory the dissipation of
energy, that is observed at the rear end and in the in-
terior of the cavity. The reentrant-Jet model was pre-
ferred over the Riabouchinsky model, since the former
shows more resemblance to experimental observations.
When the plate performs an unsteady motion, the shape
and size oif the cavity will change. Assuming that the
deviation from the steady position is small in a certain
sense, this unsteady motion can be considered as a
^J^^rturbation of the original steady flow (linearization
of the unsteady effects). The stationary flow is first
treated, followed by an investigation of the unsteady
motion. (Author)
Statics, Kinematics, and Kinetics
Bolt, Beranek and Newman, Inc. , Cambridge, Mass.
FREE OSCILLATIONS OF EEXJE-CONNECTED
SIMPLY SUPPORTED PLATE SYSTEMS, by Eric E. ,
Ui^ar. Rept. on Contract Nonr-2322(00), 11 Jan 60,
40p. 3 refs. Rept. no. 721; AD- 231 848.
Order from LC mi$3. 00. ph$6. 30 PB 152 906
A simple semi-graphical method for calculating the
natural frequencies d 2-plate systems is developed,
where a 2-plate system is defined as one made up of 2
rectangular plates simply supported at all edges and
Joined at a common edge. Equations for the mode
shapes are given, b is demonstrated that at higher
modes the componeiu plates become effectively un-
coupled in general; the modes for which coupling is
mvst severe are indicated. Charts for easy deter-
mination d the aforementioned natural frequencies are
presented. One of these gives, as a by-product, the
natural frequencies d rectangular plates (of any di-
mensions) having one edge clamped, the remaining 3
simply supported. (Author)
Bureau of Naval Weapons, Washington, D. C
FORCE 0 TO 60,000 LBS. (APPROX.) TENSION
C»5lY. BuWeps-BuShips Calibration Program.
15 July 60, 34p. Secondary Standards Lab. Measure-
ment System Operation Procedure NF-02.
Order from OTS $0. 75 PB 171 203
328
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to calibrate static force sensing instruments.
METALLURGY
HANDBOOK OF SOVIET ALLOY COMPOSITIONS.
25 Aug 59. 258p. 386 refs.
Order from OTS $4. 00 PB 171 331
This handbook identifies Soviet metal and alloy desig-
nations and their corresponding composition ranges.
Although the applications of these materials are not
Mierally considered in this compilation, two groups of
■teels are segregated, i.e., special -purpose steels
and tool steels. The essential material is presented in
21 tables.
Aeronautical Materials Lab. . Naval Air Material
Center, Philadelphia, Pa.
EXPLORATORY INVESTIGATION OF X2020 HIGH
TEMPERATURE ALUMINUM ALLOY, by E. F.
Deesing and S. J. Ketcham. Apr 59, 26p. Rept. no.
NAMC-AML-AE 4195; Pt. 2: AD-217 102.
Order from LC mi$2. 70, ph$4. 80 PB 149 655
The X2U20 aluminum alloy Is theil^ally stable up to
250^. The alloy exhibits satisfactory resistance weld
Ing characteristics, however, considerable difficulty
was experienced in fusion welding the alloy by the con-
ventional heli-arc process. The alloy appears to be
ausceptible to intergranular corrosion when a delay
quench time of 10 seconds is exceeded. The alloy is
more compatible with magnesium in corrosive media
dian either 2024 or 7075 aluminum alloys.
Battelle Memorial Inst., Columbus, Ohio.
NOTCH SENSITIVITY OF REFRACTORY METALS, by
Albert G. Imgram, Frank C. Holden and others. Rept.
for 1 May 59-13 Mar 60 on Materials Application, Con-
tract AF 33(616)6291. Sep 60, 115p. 18 refs. WAE©
Technical rept. 60-278.
Order from OTS $2.50 PB 171 198
The tensile and notch tensile properties of four refrac-
tory metals, molybdenum, tungsten, columbium, and
untalum, and one alloy, Mo-0.5Ti, were Investigated
at five temperatures selected to encompass the brlttle-
to-ductlle transition. All specimen failures were
classified according to fracture mechanism. The notch
sensitivity of each material was evaluated by analyzing
the notch and unnotch tensile strength, the ductility
tjiransition, and the fraaure transition. (Author)
Defense Metals Informatibn Center, Battelle
Memorial Inst., Columbus, Ohio.
PRODUCnON AND AVAILABILFTY OF SOME HIGH-
PURITY METALS, by E. M. Sherwood and V. S.
Secrest. [Rept. on Contract A F 18(600)1375).
2 Dec 60, 48p. 109 refs. DMIC memo. 76.
Order from OTS $0. 50 PB 161 226
The preparation of metals of the highest purity requires
the combined use of a number of specialized techniques
Among the more important processing steps, purifica-
tion of halide compounds of metals and their decompo-
sition or reduction under carefully controlled condi-
tions, vacuum melting by arcs or electron bombard-
ment for consolidation, and final purification by zone
refining are potentially of the greatest utility. Many
improvements in these techniques are possible, and
further refinements in analytical methods will be re-
quired to evaluate high-purity metals of the future.
Electron-bombardment melting and zone-refining
equipment are the only types of general utility in the
preparation of high purity meuls. The chemical
processing equipment used is custom built and varies
widely with the process involved.
Illinois U. , Urbana.
PROTECTIVE COATINGS FOR REFRACTORY
METALS, by Clifton G. Bergeron, Victor J. Tennery
and others. Rept. for Sep 59-June 60 on Ceramic and
Cermet Materials, Contract AF 33(616)5734. Aug 60,
54p. 1 ref. WADC Technical rept. 59-526, Part II.
Order from OTS $1 . 50 PB 171 193
Various ceramic coating systems for tungsten metal
were developed and evaluated. These included silicide
coatings, ceramic crystals in a glass matrix, zirconia-
clad coatings, vapor -deposited SiO, and recrystallizing
glasses.^ The system considered protective for tung-
sten at temperatures of 3000**F or higher, from a
practical viewpoint, was a coating consisting of 35%
glass and 65% zircon. Tungsten wire specimens coated
with this glass-zircon coating were protected for ten
hours at 3000<'F . A study of the nature of the degrada-
tion of this coating tested at 3000°F as a function of
time was carried out based on microstructural obser-
vations and X-ray diffraction analysis of the reaction
products. (Author)
Metals and Ceramics Lab. , Wright Air Development
Div. , Wright- Patterson AFB, Ohio.
THE PRESENT STATUS OF RUSSIAN METALLURGY,
by George D. Haley. Rept. on Metallic Materials.
Sep 60, 13p. 19 refs. WAIX) Technical note 60- 197.
Order from OTS $0. 50 PB 171 307
Western observers, through recent visits to the Soviet
Union and by reviewing the increasing number of Russ
Russian technical publications, have indicated surprise
at the present advanced status of Soviet Metallurgy.
Russian advanced metallurgical technology has been due
to the socialization of this science. The government
has channeled vast resources, personnel, and facili-
ties into metallurgical research with the result that in
some areas Russian technology is superior to that of
the United States. Some forty- five thousand Soviet stu-
dents were enrolled in metallurgical curricula in 1958,
and in this year alone forty- five hundred well- trained
graduates entered industry. Many institutions are now
conducting vast research programs in very modern and
extensive facilities. The results of the Russian efforts
in this field have been outstandmg and greater progress
is expected; however, the price has been tremendous la
terms of funds, manpower, and effort. (Author)
329
Ferrous Metals
Defense Metals nformation Center, Battelle
Memorial Inst. ,1 Columbus, Ohio.
AVAILABILTTT AND MECHANICAL PROPERTIES OF
HIGH-STRENGTH STEEL EXTRUSIONS, by
R.J. Fiorentlno afid A.M. Sabroff. Rept. on Contract
AF 18(600)1375. t6 Oct 60, 63p. 7 refs. DMIC
rept. 138. I
Order from OTSi 1. 75 PB 151 097
Information on th^ availability and mechanical proper-
ties of high- strength steel extrusions is compiled. S^k
classifications of nigh- strength steels are considered.
Typical current ewrusion specifications are discussed,
and illustrative niechanical properties are reported.
Some anention is idevoted to anticipated future con-
sumer requiremetits . (Author)
Watenown Arsetial Labs . , Mass .
TOUGHNESS OF STEEL SHEET: THE ADVANTAGE
OF LAMINATINO, byS. V. Arnold. Oct 60, 24p.
3 refs. Technical rep*, no. WAL TR 834.21/2.
Order from OTS ^0.75 PB 171 0*4
Impact tests of si^iulated sheet prepared in various
gages by machinilg and grinding AIS 4340 steel bar
stock quenched ai|d tempered to 210,000 psi and
165,000 psi lensite strength values were conducted to
show the relation of impact energy to temperature,
gage and strt ngthi level . The data denvsnstrate a behav-
ior pattern whereby sheet of appropriate gage and
strength may be selected to assure ductile fracture in
tearing under im(tact loads . This panem also defines
the advantages to be realized over certain temperature
ranges by laminating, i.e. , using two or more thinner
sheets in place of a single sheet of the same aggregate
thickness. (Authcr)
Structural Metallurgy and Corrosion
Aeronautical Materials Lab. , Naval Air Material
Center, Philadelphia.
EVALUATION OP HIGH STRENGTM-HIGH TEMPER-
ATURE ALUMINlifM CASTING ALLOYS C355-T6I
AND XA-140-F, |y R. G. Mahorter. Jr. and W. F.
EmnKins. Final rCpt. on Bureau of Aeronautics ProJ.
TED NAM AE 4lt7. 6 July 59, 37p. 4 refs. Rept. no.
NAMC-AML-AE 11096.
Order from LC m|$3. 00. ph$6. 30 PB 152 463
Aluminum casting alloy C355-T61 was evaluated with
respect to tensile properties and found to be luperlor
to355-T51, A355-»T51. and 142- T77 for temperatures
up to 500OF and for times up to 100 hours. Another
casting alloy, XA140-F, was evaluated with respect to
tensile, fatigue ai<d creep properties. Tensile proper-
ties in the 4(X)OF k> 6OOOF range were found to be out-
standing when cctrtpared to other aluminum casting
alloys. The loss «f strength on long exposure to tem-
perature was small. Creep properties appear promi-
sing for a cast aluminum alloy. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
NOTES ON LARGE -SIZE FURNACES FOR HEAT
TREATING METAL ASSEMBLIES, by H. J Hucek,
A. R. Elsea, and A. M. HaH. (Rept. on Contract
AF 18(600)13751. 25 Aug 60, 9p. 5 refs. DMIC
memo. 63; AD- 242 530.
Order from GTS $0. 50 PB 161 213
The bottom -open gantry fyrnace using an endothertnic
protective atmosphere is the most frequent type of
installation for these large furnaces. This type of fur-
nace allows loading from or quenching into a pit below
the furnace without losing the protective atmosphere or
exposing the part to the air. Also, holding the parts to
be heat treated in a vertical position assists in reduc-
ing distortion during heat treatment. Thie endothermic
protective atmosphere is the most popular because it is
easy to control the carbon potential with this gas by
regulating the dew point. The dew point in the furnace
can be readily varied by regulating the mixture in the
generator and the flow of atmosphere through the fur-
nace. The regulation of the carbon potential of the fur-
nace atmosphere is extremely important in heat treat-
ing parts which require close control or elimination of
decarburization. An atmosphere which would be
neutral to a 0. 30 carbon steel could very readily de-
carburize a 0. 40 carbon steel. (Author)
General Electric Research I.ab. , Schenectady, N. Y.
RESEARCH AND DEVELOPMENT ON THE EFFECTS
OF HIGH PRESSURE AND TEMPERATURE ON VARI-
OUS ELEMENTS AND BINARY ALLOYS, by J. S. Kaa-
per, J. E. Hilliard and others. Rept. for June 58-
Oct 59 on Meullic Materials, Contract AF 33(616)5995.
July 60, 71p. 33 refs. W A DC Technical rept. 59-747;
AD- 244 767.
Order from GTS $2.00 PB 171 348
An investigation has been made of the effea of pres-
sure on the properties and kinetics of transformatioa li
various alloy systems. Many of the experiments were
exploratory and yielded no evidence for irreversible
changes with pressures of up to 100, OCX) atm at ele-
vated temperatures. However, a shift was observed 1«
the gamma loop of the iron-chromium system from
12. 5 to about 20 per cent chromium. Evidence for a
similar shift in the gamma loop of the iron-aluminum
■ystem was also found. Pressure heat treatment of a
tool steel gave a refinement of the austenite grain siie
and an improvement in the distribution of carbides. An
apparatus for x-ray diffraction analysis at pressures
up to 35, (XX) atm has been constructed, and observa-
tions have been made on the bismuth I to II transition.
In the kinetic experiments it has been found that pres-
sure markedly decreases the transformation rate of
austenite to pear lite and the precipitation rate in the
systems: aluminum -copper, copper-beryUium, lead-
tin, and gold-nickei. (Author)
Institute of Research. Lehigh U. , Bethlehem. Pa.
PLASTIC DEFORMATION AND FRACTURE OF
METALS AT HIGH RATES OF STRAIN, by
C. W. Curtis. Sutus rept no. 1, 28 Aug-30 Nov 54,
on Contract DA 36-034 -ORD- 1456. Sup. no. 1. (1954)
9p. 6 refs. AD-53 065.
Order from LCmi$ 1.80, ph$ 1.80 PB 153 882
This report released for sale to the public 19 Jan 61.
330
fffecx of a tapered cylindrical section on the behavior
^ an elastic strain puls^; The feasibility of changing
the magnitude and shape of an elastic pulse by channel -
[^ it from one uniform section of a bar to another hav -
ii^ a different cross-sectional area is being deter-
mined. By using colliding ^rs, the transmission
through a discontinuous change in cross section was
dbctlve in altering the magnitude but not the shape of
dw incident pulse. Preliminary results indicate that if
the change is made gradually by. means of a taper, the
shape as well as the magnitude of the pulse is altered
durii^ transmission. Propayation of plastic strain in a
jfUJJliX: Measurements were conducted to determine
whether rate of strain is an important factor in the prop -
agtiion of plastic strain in lead. Dispersion of a lon-
flnxHlP^' strain pulse in an elastic bap Equipment is
being constructed by using BaTi03 rather than resist-
ance strain gages to study the oscillations produced in
a long bar by reflection of an air shock from one end.
IrtfiilTflfTI of a strain pulse from a free boundary In-
vestigations are being made of a method in which a re-
strain gage is embedded in a block of lucite.
Naval [Weapons Plant] Washington, D. C.
METALLIC MIRRORS FOR MIRROR DECK LAND-
ING SIGHT SYSTEM; FEASIBO^ITY OF MANU-
FACTURING, by P. H. Austin and Wm. Lurie.
28 Apr 59, 33p. 23 refs. NGF-T-6-59; NAVORD rept.
6495; AD-216 736. *
Older from LC mi$3. 00, ph$6. 30 PB 149 739
An investigation was made of the mechanical, optical,
•od salt-spray corrosion- resistant properties of sheets
of 61 ST-6 Aluminum Alloy, Clad Aluminum Reflector
Metal, Haynes Alloy No. 25 (a cobalt -base alloy), and
Type 316 Stainless Steel, together with several inor-
fSolc protective coatings on the mirrors, to determine
the feasibility of polishing and forming them into
metallic mirrors having a 90-inch radius cylindrical
curvature, satisfactory reflective quality, and smooth
surface contour. TTie aluminum materials were badly
pitted by the cyclic salt- spray corrosion test. Haynes
Alloy No. 25 and Type 316 Stainless Steel polished toa
rcflecunce value of 65 and 72 percent, respectively:
both Successfully passed the salt-spray corrosion test;
however, after polishing, both were difficult to form
into the required curvature and still maintain satis-
factory surface contours.
Nitrogen Div., Allied Chemical Corp. , Hopewell, Va
NITROGEN TETROXIDE CORROSION STUDIES, by
C. W. Alley, A. W. Hayford, andH. F. Scott, Jr.
Rept. for June 59-June 60 on Finishes and Materials
Preaervation, Contract AF 33(616)6568. July 60, 64p.
WADD Technical rept. 60-384.
Order from GTS $1.75 PB 171 301
The corrosion rates of carbon steel, stainless steel
(304-L and PH15-7 Mo), aluminum (5086), and titanium
(75A and 6A1-4V) in dry and wet nitrogen tetroxide
*ere determined under static conditions oi exposure
•t -9**C to 740c. Carbon steel and aluminum were
•ttacked in proportion to water concentration and tem-
perature. Stainless steel 304-L and titanium were un-
packed, and PH 15-7 Mo only slightly attacked. Cor-
roaion by dry nitrogen tetroxide under flow conditions
••• negligible. Telflon was found to contribute to cor-
rosion of stainless steel and carbon steel under
certain conditions. (Author) 33^
Northwestern U. , Evanston, 111.
ON THE INTERNAL FRICTION OF COLD WORKED
AND QUENCHED MARTENSITIC IRON AND STEEL,
by T. Mura, J. O. Brinain, and I. Tamura (Osaka U.).
Rept. on Contraa AF 18(600)1598. 6 Sep 60, 19p.
18 refs. AFOSR TN-60-1121; AD- 245 089.
Order from LC mi$2. 40, ph$3. 30 PB 152 691
A theoretical explanation is given for the internal fric-
tion peaks which are observed at TtXfiC'^lSCPc for
cold worked iron and steels and for steels in the
martensitic condition. The theory for the peaks is
leased upon the addition of a term to the free energy in
order to account for the strain energy due to the inter-
action of an atmosphere and the line imperfections.
The linear standard solid was obtained from the nKxlel
in which dislocations are vibrating with an atmosphere
of carbide fH-ecipitates .
Westinghouse Research Labs. , Pittsburgh, Pa.
STRESS CORROSION CRACKING, by D. van Rooyen.
Technical rept. no. 2 on Contract Nonr- 2868(00).
19 Jan 60. lOp. 13 refs. AD-236 255.
Order from LC nii$l. 80, ph$ 1.80 PB 152 880
Nickel, even when stressed above its yield point, does
not crack in boiling 42% magnesium chloride solution.
Tests were made with compound specimens, consisting
of nickel bonded to stainleas steel which is susceptible
to cracking under the test conditions. Cracks initiated'
in, and propagated through, the steel stopped when
reaching the nickel boundary.
NUCLEAR PHYSICS AND
NUCLEAR CHEMISTRY
California U. , Berkeley.
NUCLEAR INTERACTIONS IN CARBON PRODUCED
BY COSMIC RAYS WITH ENERQES BETWEEN lOlO
AND IOI2 ev, by Luisa P. Hansen and W. B. Fretter.
Technical rept. nos. 45-46 on Contract Nonr-222(40).
Jan 60, 49p. 37 refs. AD-231 430.
Order from LC ml$3. 30, ph$7. 80 PB 152 916
High energy nuclear interactions in the range of ener-
gies lOlO -iol2ev were analyzed by means of a cloud
chamber in a magnetic field. Measurements of ioniza-
tion and momentum made possible the identification of
electrons and TT-mesons to about 20 Bev/c. The pri-
mary panicles were cosmic-ray nucleons and a possi-
ble fraction of pions, the target nuclei were carbon and
the velocities of the primaries were determined from
balance of momentum in the center of mass system. A
total of 41 events were analyzed, and the results com-
pared to previous experimental work.
Included in the report is:
Observations (rf solar flare radiation at high latitude
during the period July 10-17, 1959, Technical rept.
no. 46, pub. in Physical Review Letters 3:390-392,
15 Oct 59.
Naval Radiologiqal Defense Lab.
Calif.
San Francisco,
SaL ANALYSIS
F . M . To inovec
and development
AD- 234 743.
Order from UC i.
Y NEUTRON ACTIVATION, by
28 Jan 60, lOp. 4 refs . Research
•chnical rept. USNRDL-TR-3%;
.80, ph$l.80
PB 153 071
The use of the neiitron activation method of soil analysis
is discussed. Dati are presented which show the re-
sults of the analysiis of various soils . The analysis in-
dicates a large variation in chemical content can occur
in adjacent areas J Where interest exists only in the
gamma- ray emitting elements produced when the soil is
exposed to neutrons , this method is a rapid and inexpen
sive means of soil analysis . (Author)
Rock Island Ars^l Lab. , 111.
POLYMERIZATIC*^ OF STYRENE AND BUTADIENE
BY GAMMA RADIATION, by Stanley L. Eisler.
31A»«60. 13p. 9 refs. Rept. no. 60-2562.
Order from CTS $0. 50 PB 171 041
Conversion rates of styrene and butadiene monomers
to their polymers^ when exposed to gamma radiation,
are reported, as >re the molecular weights of the re-
sultant polymers. ' It was found in each case that both
the conversion ra^es and the molecular weights de-
crease as the doat rate increases. The irradiation of
solutions of styrefie in benzene provided similar re-
suits and in addit^ showed that concentration had no
appreciable effect on conversion rate, but that a de-
crease In conceitti'atlofi produced a decrease in molec-
ular weight. (Autl^r)
Washington U. . St. Louis, Mo.
THE CLOUD CHAMBER STUDY OF THE UNSTABLE
PARTICLES PRODUCED IN NUCLEAR INTERAC-
TIONS OF THE COSMIC RADIATION AT MOUNTAIN
ALTITUDE, by Medford Sherman Webster. Doctoral
thesis. Technical rept. no. 3 on Cosmic Rays, Con-
tract Nonr-816(09|). July 59, 141p. 61 refs.
AD- 225 104.
Order from LC nk%7.20. ph$22.80
PB 149 736
Contents:
Apparatus
Location of equipment
Description of tie cloud chambers
Triggering system
Cameras and photography
The geometry of Cloud chamber measurements
The viewing tables and apparatus
Determination of the space coordinates of a poi.it
Direaion cosinas of line segments
Projected scanefing angles
The physics of cllxid chamber measurements
Range
Ionization in thei drop- count and multiplate chambers
Scattering in th^ plates and gas of the chamber
Events
The scanning pt^ocedure
If- ^r decay in thfe gas
Charged V- decays
Neutral V-decajs
Heavy meson de cays at rest
An anomalous ev< nt
The decay of a stopped light meson
Properties of the established particles
Scattering with energy loss in the plate
The scattering in the gas of a 0. 27-Mev electron
Washington U., St. Louis, Mo.
THE POLARIZATION OF COSMiC RAY MUONS AT
SEA LEVEL, by Clarence Scott Johnson. Doaoral
thesis. Technical rept. no. 4 on Cosmic Rays, Con-
tract Nonr- 8 16(09). July 59, 93p. 31 refs. AD- 220 531,
Order from LC mi$5. 40, ph$15. 30 PB 149 737
The partial polarization of positive muons within a nar-
row range of velocities is studied. The partial polari-
zation of cosmic ray muons depends upon the shape of
the parent plon energy spectrum. Measurement of the
polarization at sea level Is a method of obtaining this
spectrum. The polarization was measured by stopping
the muons In a copper absorber, in which their polari-
zation is largely preserved, and observing the asym-
nr»etry of the muon decay electrons, which is interpreted
according to the 2- component theory of the neutrino
[Phys. Rev. 105:1671, 19571. The experimental resuJti
indicate that the positive muon beam stopfnng in a thin
absorber at sea level, is partially longitudinally polar-
ized. On the basis of the 2-component theory, the mag-
nitude of this partial polarization is found to be greaiet
than 21 ±2%. Assuming a power law for the parent ptcn
differential energy spectrum, the slope of this curve ii
found to be greater than 1 . 3 ±0. 3. In the absence of
external magnetic fields, copper deplorizes stopped
muons at a rate corresponding to a relaxation time of
steyeral ^jsec. The polarization at sea level with > - 2.5
i8% 32, while with Kabs * O-' the experimental result
becomes 0. 30.
Elementary Particles
Maryland U, College Park.
FINAL STATE INTERACTIONS AND |aX | » 1/2
RULE, by K. Chadan and S. Oneda. Rept. on ContraO
AF 49(638)24. Mar 60, 6p. 5 refs. Dept. of Physic*
Technical rept. no. 168; AFOSR-TN-60-303;
AD- 235 033.
Order from LCmi$ 1.80, ph$1.80 PB 149 733
Maryland U. , College Park.
K'-DEUTERON SCATTERING AND THE K"-NU-
CLECW SCATTERING LENGTHS, byT. B. Day,
G. A. Snow, and J. Sucber. Rept. on Contracts
AF 49(638)24 and AT( 40- 1)2504. Mar 60, 8p. 12 refs.
Dept. of Physics Technical rept. no. 167; AFOSR-TN-
60-354; AD- 234 684.
Order from LC ml$l . 80. ph$l . 80 PB 149 732
MaryUnd U. . College Park,
LIFETD^ES OF GE(»1AGNETICALLY TRAPPED
PARTICLES DETERMINED BY COULOMB SCATTER-
ING, by Robert C Went worth. Doctoral thesis. Rejt
on Contract AF 49(638)530. 1960. 108p. 70 refs.
AFOSR TN-60-288; AD- 235 186.
Order from LC mi>5. 70. ph$16. 80 PB 149 650
S32
Some aspects of the lifetimes to be expected for trapped
ftst particles, protons and electrons, in the earth's
magnetic field are Investigated. The scattering proces s
«as considered in detail for these particles as well as
the energy loss mechanism. The lifetimes determined
ky these mechanisms range from minutes to many
Marl depending on the particles scattered, their ener-
gies, and their distance from the earth. These calcu-
lations included only the scattering from the ionized
component of the earth's outer atmosphere, although
scattering from the neutral component can be added.
"Ibe problem of pure energy loss with scattering neg-
lected was easy to solve. The problem of pure
•catterli^ with no energy loss is more difficult. The
conclusion drawn from the analysis of this problem is
that the trapped particles random walk in their equa-
torial pitch angles as if they were always moving in a
oonsunt uniform density of scattering centers equal to
one half of the equatorial density. Although the density
of scattering centers is much greater near the trapped
particles reflection point, the effect of scattering is
much less than equatorial plane scattering. These two
ofiposing effects roughly cancel.
Syracuse U. , N. Y. i
THE ENERGY MSTRIBUTION OF ELECTRONS
FROM IONIZING COLLISIONS OF HEAVY PARTI-
CLES, by H. W. Berry. Rept. for 1 June 58-31 Aug 60
on Contract AF 33(616)5741. Sep 60, 59p. 14 refs.
ARL Technical note 60-144; AD-245 856.
Order from GTS $1.50 PB 171 335
The energy distribution of electrons from ionizing col-
lisions of ions and fast neutral atoms or molecules
with those of the parent gas has been measured for A,
He. N2. and H2. The energy of the incident particles
nuifed from 0. 30 to 3. 0 kev. The electron dlstribu-
tlona exhibit an initial rapid decrease followed by max -
ima or plateaus for A and He. For N2 and H2 the jrields
decrease nearly logarithmically. (Author)
I
Washington U. , St. Louis. Mo.
WTERACTIONS OF FASt >i-MESONS IN LEAD WTFH
SMALL ENERGY TRANSFER, by J. dePagter (Doc-
toral thesis) and R. D. Sard. Technical rept. no. 5 on
Cosmic Rays, Contract Nonr-816(09). Jan 60, 48p.
36 refs. AD- 233 706.
Onler from LC mi$3. 30, ph$7. 80 PB 152 911
With the Pb target material divided into 1. 27 cm slabs .
between hodoscoped Geiger tubes and surmounted by a
magnet cloud chamber, a study was made of the inter-
actions of fast /v~mesons in which at least one evapora-
tion neutron is produced and no additional charged par-
ticles emerge from the slab. The cross section aver-
age neutron multiplicity, am. Is (15. 2 1 2. 1) x 10-29
cm* per nucleon.
Instruments and Installations
IXiblln Inst, for Advanced Studies (Eire).
INTRINSIC CALIBRATION OF THE PHOTO-ELECTRIC
CONDENSATION NUCLEUS COUNTER MODEL 1957
Wmi CONVERGENT LIOTT-BEAM. by L. W. PoUak
•nd A. L. Metnleks. Technical (scientific) note no. 9
OB Contract AF 61(052)26. 1960, 61p. 10 refs. AFCRL-
TO-60-637.
Order from LC mi$3. 90, ph$10. 80 PB 152 768
The intrinsic calibration of the photo-electric conden-
sation nucleus counter Model 1957 with convergent
light- beam is based on a so-called 'e, E curve', where
E denotes the extinction for the concentration Z and e
that for the ctMicentration Z/2'18. The e, E curve is
w'ithln reasonable limits Independent of the particular
photo-electric counter Model 1957, the alignment and
type of the light-pencil whether divergent or convergent,
the size of the diaphragm directly above the photo-cell
and the speed of producing the over-pressure with fil-
tered air. The dilution ratio, however, for which the
e, E curve is valid, must be accurately known. The
ratio between any two concentrations read off from the
intrinsic calibration curve or calibration table based
on the e, E curve is also independent of the instrumen-
tal specification and of the absolute values taken as
basis for the calibration. The absolute values of the
calibration curve or table, of course, depend on the
factors mentioned. A convergent light -beam has been
used for this calibration and is strongly reconunended
in order to prevent 'scintillation' with very low con-
centrations and to ensure long- term agreement between
counters of identical construction. (Author)
Lockheed Aircraft Corp. . Marietta, Ga.
NEUTRON AND GAMMA FLUX MAPPING AT THE
RADIATION EFFECTS FAQLITY, by R. L. Gamble,
J. K. Grant and others. Kept, on Contract
AF 33(600)38947. Sep 59. 167p. 5 refs. Nuclear
rept. 60; AD- 228 483.
Order from LC mi$7.80. ph$2S.80 PB 153 790
This report released for sale to the public 19 Jan 61.
The 2200 m/sec neutron flux per watt of reactor powe|r
(neutrons/cm2 sec watt), the fast neutron dose rate per
watt (rads/hr wan in ethylene), and the gamma ray
dose rate per watt (ergs/gm sec watt in carbon) were
measured in the irradiation volumes around the radia-
tion effects reactor for several shield tank configura-
tions. Curves are given from which these quantities
can be obtained as a function of distance from the reac-
tor. A complete description is given of the instrumen-
tation and techniques used in making these measure-
ments as well as the the(n7 behind the techniques.
(Author)
Naval Radiological Defense Lab. , San Francisco,
Calif.
THE MODIFICATION AND CALIBRATION OF
LANDSVERK MOCCL L-62 CHARGER -REACCRS FOR
INTERCHANGEABILITY. by R. L. Lynn. 28 Mar 60,
22p. 2 refs. Research and development technical rept.
USNRDL-TR-408; AD-236 817.
Order from LC mi$2. 70, ph$4. 80 PB 153 622
This report released for sale to the public 16 Jan 61.
Landsverk Model L-62 charger-readers and their cali-
bration procedure were modified so that Landsverk
pocket chambers can be charged on any of the charger-
readers and subsequently read on any other of the
charger -reader 8 without introducing significant error
in the dose reading. The modifications were primarily
concerned with the establishment of an equal, constant
value, charging voltage for all the pocket chambers.
The introduction of an offset zero position for reading
Landsverk Model L-6S, 200-mr pocket chambers, to
333
compensate for th s negative readings of fully charged
200-mr pocket chiimbers was also accomplished. With
the modified L-6^ charger-readers, a constant value
of applied voltage on a pocket chamber will yield dose
readings repjroducible to better than 5 percent for con-
secutive readings made on different charger -readers.
TTiis value is compared with a discrepancy of about
15 percent for siitiilar readings on unmodified L-62
charger -reader 8. A precision of 1 percent can be
realized for consecutive readings made on any one
modified charger* reader. (Author)
Naval Radiological Defense Lab. . San Franci^o,
Calif.
A NINE-CHANN^ TIME ANALYZER FOR MEAS-
URING SHORT HALF -LIFE ACTIVITIES IN THE
MILLISECOND REGION, by R. A. Taylor. 19 Sep 56.
Up. 4 refs. Res^rch and development technical rept.
USNRDL-TR-llli
enter from LC nii$2. 40. ph$3. 30 PB 153 621
This report released for sale to the public 10 Jan 61.
A nine -channel tiine analyzer has been constructed and
used to measure fadiations from radioactive isotopes
whose half lives ^re of the order c4 magnitude of a few
milliseconds. It s operated in association with a Van
de Graaff generat sr. the beam of which is pulsed.
(Author)
Radioactivity
Air Force ^>ecifl Weapons Center, Kirtland AFB,
N. Mex.
_ FEASIBILITY OF USING REMOTELY CON-
TROLLED VEHKtLES TO DECONTAMINATE LARGE
PAVED AREAS, by Clayton L. Schlemm and Alexander
E. Anthony, jr. (fct 60, 88p. 8 refs. AFSWC TN-60-25
AD-245 017. I
Order from LC nriiK 80, ph$13. 80 PB 152 698
Studies were perfprmed to determine the feasibility of
using a remotely controlled vehicle to sweep and re-
move radioactive [debris from large paved areas. I'est
data were collected for comparison of the renrxxe oper-
ation and manual operation of the vehicle. The test
parameters inqlu^ed comparison of (1) decontamination
efficiency, (2) tii^e needed for decontamination, and
(3) sweeping patterns. A comparison of test parame-
ters has indicated that it is feasible to use a remotely
controlled sweeper to decontaminate an area. Approx-
imately the same decontanunation efficiencies were
obtained under rehiote and manual operation (approxl-
mately 99. 7 percent). The operating time for renxxe
decontamination was about twice that for manual. This
time can be reduqed as the area to be swept becomes
larger and the operator becomes more proficient.
These results were obtained on a snull area (approxi-
mately 3,000 square feet). The time lost was mostly
in turning around |and reorienting the vehicle at the end
d each sweeping pass on the contanunated area. The
driving patterns were quite different. Under manual op-
eration, the vehiqle is easily controlled and no sweeping
overlap is neceseltry. Under remote operation, there
was a tendency for the vehicle to drift. The operator,
attempting to correct this, had a tervdency to overstecr,
which resulted in n»re sweeping passes than were
necessary. Refinement of the renxjte steering mechu-
ism would correct this discrepancy. (Author)
Defense Atomic Support Agency, Washington, D. C.
GAMMA SPECTRA OF URANIUM- 238 FISSION PRO-
DUCTS AT VARIOUS TIMES AFTER FISSION, by
P. J. Dolan. May 59, 50p. 5 refs. DASA 526.
Order from LCmi$3. 30. ph$7. 80 PB 153 030
Calculated gamma spectra produced by Uranlum-238
fission are tabulated for various times after fission.
Similar tabulations are given omitting certain volatiki
and portions of their daughter products . The tabulated
data are also presented in graphical form. (Author)
Human Sciences Research, Inc., Arlington, Va.
AN INVENTORY OF ELECTED SOURCE MATE-
RIALS RELEVANT TO INTEGRATION OF PHYSICAL
AND SOCIAL EFFECTS OF AIR ATTACK, by Roben
D. Popper and William A. Lybrand. Technical note co
Contract AF 49(638)549. Oct 60, 518p. 191 refs.
HSR-RR-60/4-SE; AFOSR-TN-60-379; AD- 244 888.
Order from LCmi$l 1.10, ph$78.90 PB 152 821
The inventory is divided into three major sections: (1)
the problem includes studies or treatises dealing with
thermonuclear warfare and its effects; (2) societal
behavior under stress encompasses studies of World
War II bombing attack effeas, the effects of major
disasters on societal funaioning, and studies of indi-
vidual and small group reactions to stress; and (3)
analytic methods contains reports of analytic ap-
proaches used on aspects of the problem, or on simi-
lar problems, and a number of applications of analytic
models which seem to yield insi^s into the usefulness
of those types of models to the present research
program. (Author)
Massachusetts Inst, of Tech. , Cambridge, Mass.
APPLICATION OF WEATHER RADAR TO FALLOUT
PREDICTION, by Pauline M. Austin. Quarterly tech-
nical rept. no. 9, 1 Mar -31 May 60, on Contract DA
36-039 -sc-75030. 15 June 60. lip. AD-241 914.
Order from LC mi$2. 40, ph$3. 30 PB 152 661
The application of radar to the prediction of radioactlw
rainout resulting from a nuclear detonation is investi-
gated. The computational program for the effect of
rain on the fallout pattern for a selected wind field and
initial distribution of radioactivity is ready to be tested
with the addition of the final step, that of inserting i
standard shower in the region downwind of the detons-
tion. The programs for the first and second steps,
computing the trajectories of radioactive wafers and
summing at the ground, were completed and tested.
The accuracy of quantitative radar measurements for
both single and volume targets was studied, with par-
ticular effort directed towards the problems involved
with volume targets. A number of drop-size distribu-
tions were taken simultaneously with rain gauge and
radar data, and their effect on the signal was verified.
Consideration is being given to the effect of the finite
dinrtensions of the radar beam and the rain showers.
334
I i
Havtrl Radiological Defense Lab. , San Francisco,
Calif.
APPLICATION OF "THEORY FOR CLOSE-IN FALL-
OUT" TO LOW -YIELD LAND SURFACE AND
UNDERGROUND NUCLEAR DETONATIONS, by
A. D. Anderson. 12 Jan 59, 6lp. 10 refs. Research
ind development technical rept. USNRDL-TR-289;
AD- 234 359.
Order from LC mi$3. 90, ph$10. 80 PB 153 070
A fallout -prediction method should be based on all the
dynamics of the fallout process, but current prediction
oaodels do not provide more than generalized answers
because they do not accouijt for early-time dynamics.
A Theory for Close-in Fallout has been derived in a
recent attempt to account for the entire process. In
thia study, the new theory is checked by developing a
mathematical fallout -prediction model from it (the D
model). This model is used to predict fallout patterns
from 3 low -yield (about 1 KT nuclear weapons deto-
nated in Nevada. These patterns are then compared
with the measured test patterns and also with patterns
calculated with 2 other prediction models. Based on
these comparisons, it is concluded that the theory is
valid, at least for low-yield land-surface and shallow-
underground bursts. For underground bursts having a
llgnificant base surge, it is indicated that the D model
•ill have to be modified ta uke this effect into account
before successful prediction can be expected. (Author)
Naval Radiological Defence Lab. , San Francisco,
Calif.
INVESTIGATION AND CORRELATION OF SOME
PHYSICAL PARAMETERS; OF FALLOUT MATERIAL,
bjrW. Williamson, Jr. 28 Mar 57, 34p. 2 refs. Re-
•earch and development technical rept. USNRDL-
TR-152; AD-144 368.
Order from LC mi$3. 00, ph$6. 30 PB 153 068
This report released for sale to the public 6 Jan 61 .
An attempt has been made to correlate some of the
fundamental physical parameters of fallout material.
Parameters discussed are color and shape, activity,
tiU, weight, and density. The investigation revealed
a significant difference in density and aaivity in dif-
ferent types of fallout. (Author)
Nival Radiological Defense Lab. , San Francisco,
Calif. '
STATUS OF RADIOLOGICALLY PROTECTIVE COAT-
INGS FOR LAND TARGET SURFACES, by
W. L. Owen. 13 Nov 58, 50p. 10 refs. Research and
development technical rept. USNRDL--TR-277;
AD- 233 575.
Order from LC mi$3.30. ph$7.80 PB 153 570
This report released for sale to the public 4 Jan 61 .
It ii the purpose of this survey to examine the available
*at results and determine the status of protective coat-
i«p as applied to land target surfaces. The survey
cowered tests involving approximately 30 coating- sur-
'•ce combinations made up of approximately 20 coat-
lift and 12 surfaces. These combinations each had
WW subjected to at least one of three types of con-
tWilnant (dry, slurry and wet) and one of six separate'
decontamination procedures. Results from these tests
revealed only nine coatings exhibiting the capability to
appreciably improve decontamination effectiveness of
specific surfaces. With the exception of Navy 5H paint,
this capability was limited to the protection of asphalt
paving, concrete paving and wood sliding. Navy 5H
paint consistently provided substantial gains in the
effectiveness achieved on five different wall materials.
In general, it was noted that gains attributed to coat-
ings in most cases could have been duplicated or sur-
passed by the use of a more stringent decontamination
procedure on an unprotected surface. (Author)
Technical Research Group, Inc., Syosset, N. Y.
THE TRANSMISSION MATRIX METHOD FOR PENE-
TRATION PROBLEMS, by David Yarmush, Julius Zell,
and Raphael Aronson. Final rept. for Dec 58-Nov 59
on Contract AF 33(616)6081; Continuation of Contract
AF 33(616)3616. Aug 60, 299p. 5 refs. WADC TR-
59-772.
Order from OTS $4.00 PB 171 341
A practical machine method few computing transmission
and reflection of radiation by laminated slab shields is
described, making use of transmission and reflection
matrices. These are combined in a way which produces
a formal solution of the Boltzmann equation in slab
geometry. This result is applied by using representa-
tions in terms of energy groups and angular expansions.
Two codes for the IBM-704 which together carry out the
computation of the transmission and reflection matrices
are described and operating instructions are given.
Numerical results for gamma rays are presented. The
advantages of the transmission matrix method as com-
pared to other methods are discussed. Appendices are
included showing how in the Pj approximation the
method gives diffusion theory in a particularly simple
way and how it can be applied to other geometries.
(Author)
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Arctic Aeromedical Lab., Ladd AFB, Alaska.
ARCTIC SURVIVAL KIT, PASSENGER, by VolneyM.
Williams. Aug 57, 29p. Technical rept. 57-3.
Order from LC mi$2.70, ph$4,80 PB 153 346
This report concerns a newly developed survival item
that will provide passengers utilizing cargo-type air-
craft with a survival kit, which is immediately available
to then^ should bail out in the Arctic be necessary. At
the present time, passenger ball out is not feasible in
Alaska due to the probable inaccessibility of the cargo
survival bundles after para-descent. The standardi2»-
tion of the Arctic Survival Kit, Passenger will provide
the Individuals of the Alaskan Air Command with read-
ily available survival equipment of the type that would
be required by them, and which is considered to be an
improvement over the present cargo aircraft survival
kit. (Author)
33S
Quartermaster Field Evaluation Agency, Fort Lee,
Va. I
THE CONSTRUCTION OF INTERVAL SCALES FOR
MEASURING TH$ ACCEPTABILITY OF CLOTHING
AND EQUIPMENT IN FIELD TESTTS, by Lee E. Paul.
Jan 60, 6lp. 6ref9. Technical rept. R-4; FEA MRS
5901' AD- 231 043.
Ordei-from LCril$3.90, ph$10.80 PB 149 688
The purpose erf tlils research study was to establish
vaUd and reliable rating scales that are simple to ad-
minister, easy td score, and conform to psychological
and statistical principles which will permit the deter-
nnination of exaaj interpretation of test subject re-
sponses. The research study indicated that the 9- point
scales are more tellable than the 6-polnt scales and
provide more information on the items rated. The
6-point scales, however, can be used under certain
conditions, i.e. , where time is an important factor or
where only a roufh measure is needed. The specific
scales seem more sensitive to differences between
similar items an4 less subject to halo effect than gen-
eral scales. In general, attitude towards the Army has
bnle effect on itdm ratings. (Author)
PHYSICS
Armour Reseai^h Foundation, Chicago, 111.
CONVERSION Ot DIFFRACTOMETER FOR SMALL
ANGLE SCATTHRING, by Robert H. Bragg and
L. E. Copeland (jPortland Cement Association). Rept.
on Contraa AF 49(638)829. 1 Oct 60, 30p. 13 refs.
AFOSR-TN-60-lfi35; AD- 245 197.
Order from LC i|il$2. 70, ph$4. 80 PB 152 730
A Simple, rapid tonversion of a dlffractometer from
conventional difftaaometry to small angle scattering is
described. The Conversion consists of adding an attach-
ment which provides a much larger separation than is
usual between thi slits limiting the angular divergence
of the beam scat^red by the sample which reaches the
detector. Usablq measurements can be made down to
0. 10° 2 e The lattachment is inexpensive to construct
and can be installed and aligned in about 30 minutes.
Sample preparation requires only a few minutes and
both soUds and liquids are handled with equal facility.
Intensity data art obtained by means of manual fixed
count measurements and a complete panern for most
materials can b^ obtained in about one hour. The range
of intensity encoiintered in nriaterials e.g. , Magne-
site, colloidal grliphite, silica gel, and silica sols can
be as great as 1(F : 1. This makes possible comparlsot
of the experimer|tal curves with theory for bcch small
and large valuesjof the scattering vector. (Author)
Bureau of Naval Weapons. Washington, D. C.
MASS IN AIR 1 bRAM TO 30 KILOGRAMS DIRECT
WEIGHING METHOD. BuWeps-BuShips Calibration
Program. 8Junej60, 20p. Secondary Standards Lab.
Measurement Syktem Operation Procedure NM-03.
Order from OTS $0. 50 W 171 202
This procedure (^escribes the operation of a secondary
standards laboratory calibration system which is used
to calibrate Class T and lesser accuracy weights by
the direct weighing method.
J. G. Engineering Research Associates, Baltimore,
Md.
VIBRATIONS OF A THICK WALLED ELASTIC CYL-
INDER: A COMPARISON OF THE EXACT THEORY
WITH APPROXIMATE THEORIES, by Joshua E.
Greenspon. Technical rept. no. 2 on Contract Nonr-
2733(00). July 59, 21p. 24 refs. AD- 220 099.
Order from LC mi$2.70, ph$4.80 PB 149 682
Vibrations of an elastic cylinder as predicted by a
number of the approximate shell theories are com-
pared with the results of the exact theory. The mem-
brane theory of shells is rather accurate for predicting
frequencies and displacement rations of cylinders with
appreciable thickness. The theories which Include
rotatory Inertia and shear are accurate over most at
the wave length spectrum of the lowest branch. For
the very thick sheU (with [^"^^.tyrfi^us ' «• 5> °°»y ^
exact theory shows the full charaaeristics of the dis-
placement distribution. (Author)
Laboratory for Insulation Research, Mass. Inst, of
Tech. , Canibridge.
PROGRESS REPORT NO. XXV, Rept. on Contracts
Nonr- 1841(10), Nonr- 1841(50), AT(30- 1)1937,
AF 19(604)5482 and AF 33(616)5920. July 59. 86p.
54 refs. AD- 225 055.
Order from LC mi$4.80, ph$l3.80 PB 149 728
Contents:
Conduction and breakdown
Dielectric spectroscopy
Chemistry
Structure analysis
Single crystals
Ceramics
Magnetics
Magnetic resonance and magneto-opcics
(See also PB 144 445)
Electricity and Magnetism
California U. , Berkeley.
MATHEMATICAL ASPECTS OF ELECTROMAGNETIC
THEORY III, by Bernard Friedman. Technical rept.
no. 4 on Contract Nonr- 222(60). Jan 60, 44p.
Order from LC mi$3. 30. ph$7. 80 PB 152 8M
Contents:
Bessel functloQS
Field produced by a source In the presence of a
conducting wedge
Danish National Committee of URSI.
OBSERVATIONS OF ' WHISTl.ERS" AND VLF PHE-
NOMENA AT GODHAVN. GREENLAND, by Eigil
Ungstnip. Technical note no. 2 on Contract
AF 61(514)1309. 1 July 59, 4p. 5 refs. AFCRC TN-
59-469; AD-231 804. ^
Order from LCmiSl. 80. ph$ 1.80 PB 153 279
336
IXamond Ordnance Fuze Labs. , Washington, D. C.
THE MAGNETOSTATIC MODES OF A SMALL HOL-
LOW CYLINDER t)F FERRITE, by Clyde Morrison.
15 Nov 60, 18p. 5 refs. TR-881.
Order from LC mi$2. 40, ph$3. 30 PB 152 923
liagnetostatic modes are shown to exist in hollow
cylinders of ferrite. The field strength at which reso-
nance for each mode occurs is given and expressions
for power absorbed by the mode are derived. (Author)
Laboratoire de Ferromagnetisme, Instltut de
Physique, Strasbourg (France).
PREPARATION OF IRON PHOSPIQDES. IRON BO-
RIDES. AND THE STUDY OF THEIR DIFFERENT
MAGNETIC PROPERTIES, by M. R. Forrer. Final
technical rept. no. 1 , I Nov 58-1 Nov 59 on Contract
DA 91-591-euc-977-01-1095-59. [1960] 30p.
AD-230 071.
Order from LC mi$2.70, ph$4.80 PB 153 277
FejP, Fe2P, and FeP were prepared. All of these
compounds were ferromagnetic but only FeP demon-
strated ferromagnetism beyond room temperature.
Pe2B and FeB were prepa^red by melting in a high fre-
quency furnace. Fe2B had a ferromagnetic Curie point
at 74ClPC and a magnetic transition at 245°C. Experi-
mentation on a single crystal of Fe2B led to the con-
clusion that at 245°C the magnetocrystalline energy
«as rero. The saturation magnetization at room tem-
perature measured for polycrystalline FeB was 1 .02
Bohr magnetrons . The coercive force of FeB at room
temperature was 92 oer. This coercive force de-
creased in a quadratic function of the temperature lo-
i*rds zero for the Curie point at 309*\::. The-Curle
points of C03B and C02B were 485° and 155°C,
respeaively .
Laboratory for Insulation Research, Mass. Inst, of
Tech. , Cambridge.
TEMPERATURE AND SPACE-CHARGE EFFECTS IN
LIQUID HYDROCARBONS, by R. Coelho and M. Bono.
Rept. on Contracts Nonr-1841(10) and AT(30-1)-1937.
June 59, 14p. 8 refs. Technical rept. 137; AD-219 687.
Order from LC mi$2. 40, ph$3. 30 PB 149 725
Preliminary results on the residual d-c conduction and
^Mce-charge polarization in n-hexane and n-heptane
voder highly inhomogeneous field conditions (thin wire
ta coaxial cylinder) are presented. The gross features
of tbe current -voltage characteristics can be explained
by dissociation of polar impurities in the region of high
field strength. The depetxlence on polarity can be ex-
plained by space -charge distortion of the field. For
MfUlve wire, field emission appears, to occur from
the wire, surrounding it with a current -limiting space
charge.
Naval Ordnance Test Station, China Lake, Calif.
FURTHER STUDIES OF THE INFLUENCE OF LIGHT
ON FERROMAGNETISM, by Julian L. Thompson.
»Sep58. i9p. 4 refs. NOTS 2113; NAVORD rept. 6415
AD-211 397.
<^*r from LC mi$2.40, ph$3. 30 PB 149 654
The effect of light on ferromagnetism is largely due to
the red and near -infrared portions of the spectrum.
Thermal changes of permeability are shown to be appli-
cable to the detection of steady illumination. Domain
boundaries in thin ferromagnetic films are shown to
move under the influence of mechanical vibration, and,
light is believed to produce the same effect. (Author)
(See also PB 148 370)
Electronics
Armour Research Foundation, Chicago, 111.
SUPER POWER CATHODE STUDY, by Robert G. Pohl.
Final rept. no. 2. phase no. 2, 5 July-20Oct 60, on
Contract AF 30(602)2043. 20 Oct 60, 25p. 3 refs .
ARF 1146-6.
Order from LC mi$2.70, ph$4.80 PB 152 962
X-ray and electron diffraction studies of "nickelate"
cathodes show that cathodes that have been processed so
as to obtain high sputter voltages and high thermionic
emission do not contain the compound barium nickelate.
Rather the finished cathode consists of a matrix cathode
wherein barium oxide or other barium compounds are
distributed within a nickel matrix. The "nickelate"
phase of the processing Serves as a solvent permitting
solution of barium compounds into the nickel substrate.
Subsequent processing decomposes barium nickelate out
of existence. The finished cathode is a matrix cathode
possessing a more homogeneous distribution of constit-
uents than obtained in the customary sintered bariated-
nickel matrix cathode. A study of the darkening due to
ion bombardment of barlated nickel matrix cathodes
employed in high power klystrons shows an excess of
calcium in the darkened area, together with the for-
mation of tungstates and zirconates , with a resulting
loss of reducing Jtgent. zirconium. The experimental
procedures followed in constructing a test diode are
given. (Author) (See also PB 149 761)
Carnegie Inst . of Tech., Pittsburgh, Pa.
VELOCITY DISTRIBUTIONS IN DIRECT AND RE-
FLECTED ATOMIC BEAMS, by J. H. McFee (Doctoral
thesis) and P. M. Marcus. Technical rept. no. 1 on
Contraa Nonr -760(11). 8 Jan 60, I69p. 63 refs.
Ap-231 313.
Order from LC mi$7.80, ph$25.80 PB 152 882
Extensive and accurate measurements were made of the
velocity distributions in potassium atomic beams
emerging directly from an oven. At low source (oven)
pressures, the distributions were found to be highly
Maxwellian and were characterized by temperatures
which corresponded closely to the measured s6urce
temperatures. At high source pressures (mean-free-
path in sourcea^ source slit width) the velocity distri-
bution in the beam was found to be substantially defi-
cient in low velocity atoms, as compared to the Max-
wellian prediction. The atomic beam was scattered
(reflected) from various solid surfaces and the velocity
distribution at the scattered atoms was measured. The
surfaces investigated included polycrystalline Cu, W,
and Au. and cleavage planes of MgO and LiF single
crystals. Surface temperatures ranged from 50^*K to
337
2\(XPK. In the c^e of theCu. W, Au. and MgO sur-
faces, the velociti distributions of the reflected beams
were found to be f ighly Maxwellian. The temperatures
of the reflected- bjam distributions apparently corre-
sponded closely t< the surface temperatures, although
only in the case of the Cu surface was an accurate and
independent measiirement of the surface temperature
possible. The ex4hange of energy between the atomic
beam and these siirfaces was, essentially complete.
The reflection of K atoms from the cleaved LiF surface
was anomalous. The refleaed-beam velocity distribu-
tion was definitely non-Maxwellian, and the energy ex-
change between tile beam and the surface was found to
be incomplete (aptoroximately 70^ of the maximum
possible) for surf ice temperatures between 600°K and
900OK. (Author)
Electronics Resjsarch Lab. . U. of California,
Berkeley .
ELECTRON AND PLASMA BEAMS, by D. H. Sloan,
and others. Scientific repc. no. 8
(Interim annual rfpt. for 1959- 1960) on Contract AF
19(604)2270. 15 |une 60, 62p. 11 ref s . lER series
no. 60, issue no
284: AFCRL TN-60-971
Order from LC 4i53 90. ph$10.80 PB 152 960
Contents:
Electron optics
Cross -field gaseous tubes
Plasma investigations
Semiconductor ptjoperties of ionized gas
Interactions between electron beams and plasmas
Microwave Research Inst. , Polytechnic Inst, of
Brooklyn. N. Y-j
MICROWAVE PROBING OF A MEDIUM DENSITY
HYDROGEN PLASMA, by M. Ettenberg, M. Mentzoni
and T Tamlr. R^pt. on Contract AF 19(604)4143
refs. Research rept. PIBMRl-808-
)-988.
PB 153 069
31 May 60, 43p.
60; AFCRL -TN-(
Order from LC n4i$3. 30, ph$7. 80
A cw microwave |)eam ts propagated through a pulsed
discharge in hydii)gen of up to several hundred am-
peres peak current. The transmitted signal is the basis
for measuring th# attenuation coefficient and thereby
the electron density as a function of time, assuming a
collision frequency from the literature Measurements
have been made dp the decay constants of the afterglow
and it is possible! to assign an attachment frequency of
6 X I04 p sec-' t0 the major decay process in the pres
ence interval 1 -71 mm Hg The oscilloscope trace of
the transmitted signal sOTnetimes displays irregulari-
ties in the form c|f peaks artd overshoots which undergo
displacements om the time scale and changes in width
as the frequency Or electron density changes. Some
optical data have also been taken of the time depend-
ence of the total luminosity of the discharge as well as
of individual Balrier lines. Finally, a possible inter-
ference mechanism between a glass wave (surface
wave) and a dire<^t wave propagating diametrically
throt^ the cylinder is considered. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
ELECTTROMAGNETIC THEORY OF D. C. EFFECTS
IN FERROMAGNETIC RESONANCE, byH. J.
juretschke. Technical rept. no. 7 on Contract Nonr-
839(06). I Jan 60, 23p. 14 refs. AD- 235 288.
Order from LC nu$2.70, ph$4.80 PB 152 861
Electrical conduction in a ferromagnetic metal gener-
ally depends on the direction of the magnetization M.
If the average direction of M^ is fixed by an applied"
static magnetic field, Hq. a superimpbsed electromau-
netic field will produce two effects in the metal: (1) its
nruignetic field causes the magnetization to precess at
the applied frequency about its average direction, and
(2) its electric field excites oscillating conduction
currents . (1) These effects are coupled and will pro-
duce, anyjng other results, time- independent fields
and currents . D. C. effects accompanying ferromag-
netic resonance have been observed experimentally,
and are in qualitative agreement with the InterpreutiOB
The present report develops a more deuiled theory of
the effects to be expected on this basis .
Technical Research Group, Syosset, N. Y.
ON THE GREEN'S FUNCTION FOR A CIRCULAR
CYLINDER, by Stephen Barone. Scientific rept. no. 2
on Contract AF 19(604)3476. 13 Jan 60. 85p. 10 refs.
TRG-121-SR-2; AFCRC-TN -60-575
Order from LC mi$4. 80, ph$13. 80 PB 152 777
It is shown in some deuil how the Green's function for
a cylinder passes into the Green's function for a plane
as the radius of the cylinder becomes large. For the
case of a cylinder which obeys an impedance boundary
condition, the asymptotic evaluation of the Green's
function is carried out in deuil. A similar evaluatioa
is carried out for the case of a plane which obeys an
impedance boundary condition and a comparison be-
tween the two cases, plane and cylinder, is made.
Molecular Physics and Spectroscopy
Arnold Engineering Development Center (Tullahoma,
Tenn. ].
THE VISIBLE PLASMA FLAME SPECTRA OF ARGON
AND HELIUM, by W. K. McGregor, J. J. Ehrlich.
and J. D. Bratcher. Rept. on ARO, Inc. , Contract
AF 40(600)800. Dec 59, I6p. 5 refs. AEDC TN-59-134
AD- 229 965.
Order from LC mi$2. 40, ph$3. 30 PB 152 664
The electromagnetic spearum is being employed as •
diagiwstlc tool in research on the kinetics of gases a-
pandlng through nozzles. The spectra of argon and
helium plasma generated in an electric arc plasma
generator are reported. Tables are given of emissloa
lines detected in the range of 3000 to 7000 A using •
grating spectrograph; quantum transition data from
referenced sources are included for each emitted line.
The spectra are notable for their apparent freedom
from emissions caused by the gas stream conwmina-
tlon and for the distinct appearance of lines attributlfck
to loos. The dau obtained Indicate the utility of the
spectral data for gas stream diagnostics. (Author)
338
Battel le Memorial Inst. , Columbus. Ohio.
INVESTIGATION OF THE INFRARED ABSORPTION
OF SELECTED AROMATIC COMPOUNDS IN THE
lEGlON OF 2 TO 35 MICRONS, by R. J. Jakobsen.
Bafit. for 1 Feb 59-31 Jan 60 on Experimenul Tech-
■iques for Materials Research, Contract
AF 33(616)6140. Sep 60, 44p. 30 refs. W ADD Tech-
nical rept. 60-204.
Older fromOTS $1.25 PB 171 342
Oxnplete vibrational assignments have been made for
phenol, p-xylene. p-cresol. and hydroquinone. Infra-
red spectra of the selected para -substituted phenols
have been recorded over the 2- to 35 -micron range.
Wtth the aid of these infrared data and of Raman spec-
txt, most at the low -frequency vibrations have been
IMlfnnd The reliability of the assignments and the
tlgniflcance of the assignments are discussed, as well
u tbe determination of the modes of vibration. Corre-
lation studies of frequency with phjrslcal properties
lave been made for the assigned frequencies that are
■enaitive to the nature of the substltuent. (Author)
r ,
Massachusetts Inst, of Tech., Cambridge.
mON SERIES HARTREE-F(X:K CALCULATIONS, by
Richard E. Watson. Tochnical rept. no. 12 on Coa-
traaNonr- 1841(34). 1$ June 59, 264p. 26 refs. I
AD- 219 981.
Order from LC miSll.lO, ph$4l.lO PB 149 639
The results are presented of 76 analytic Hartree-Fock
(H-F) calculations for \TOii series atoms and ions.
Iron series elements refer to the first long period of
the periodic table. The period is involved with the
filling of the 3d shell, and starts with Sc (atomic
DO. 21) and ends with Ni (atomic no. 28). The ele-
ments which are included are Sc, Ti, V, Cr, Mn, Fe,
Co, and Ni. Results are also reported for singly and
iMve highly ionized Cu. These calculations extend the
knowledge of how the atomic 3d wave functions vary
with changes in atomic no. and state of ionization. The
analysis is restricted to the H-F calculations for iron
series atoms with non-closed shells. These cases
have an array of single and multi-detcrmlnantal wave
finctions which are eigenfunctions of the whole atom
quantum numbers. Necessary definitions are made
•nd the H-F equations are discussed. Methods for
solving the H-F equations are discussed with emphasis
on the Roothaan procedure. Results show that there is
good agreement between the analytic calculations and
the existing numerical solutions, and poor agreement
with the observed atomic muitiplets and iQ.iization
energies.
Massachusetts Inst, of Tech., Cambridge.
SOLID-STATE AND MOLECULAR THEORY GROUP,
b)r J. C. Slater. Quarterly progress rept. no. 33 on
Contraa Nonr-184K34). 15 July 59, 58p. 9 refs.
AD- 220 853.
Order from LCmi$3. 60, ph$9. 30 PB 149 680
Contents:
Htrtree-Fock Calculations for Mn**in Cubic Fields
Energy Bands In Iron
Symmetrized Plane Waves and Projection Operators
Self-Consistent Hartree-Fock Energy Bands
The Linear Chain
Interaction of a Hole with Mobile Lattice Ions In KCl
A Fortran Encoded Syntactic Unit Locater
An Integrated Operating System for a High Speed
Computer
Multi-Center Integral Programs for I.B.M. 704
Computer
Massachusens Inst, of Tech. , Cambridge.
SOLID-STATE AND MOLECULAR THEORY GROUP.
Quarterly progress rept. no. 35 on Contract Nonr-
1841(34). 15 Jan 60, 73p. 67 refs. AD- 232 049.
Order from LC mi%4. 50. ph$l2. 30 PB 152 863
Contents:
Multiplet structure In crystalline fields
The effea of crystalline fields on magnetic form
factors
The Mn**ion in crystalline fields
Approximate wave functions for atomic Be
Molecular calculations
Automatic coding, symbol manipulation and related
topics
Programs for evaluation of molecular Integrals: four
centered integrals
Condon-Shortley coefficients
Energy bands in iron
Band structure calculation
Energy band calculation
The linear chain
Interactions of a hole with mobile lattice ions in KCI
(See also PB 149 517)
Spectroscopy Lab. , Pennsylvania State U. , University
Park.
TEC3INICAL REPORT, JULY 1, 1958 -JANUARY 1.
1960. Rept. on Contract Nonr -656(1 2). [1960] ll5p.
57 refs. AD-231 151.
Order from LC ml$6. 00, ph$18. 30 PB 152 864
Contents:
Molecular constants of carbonyl sulfide and a coriolls
perturbation, by G. D. Saksena, T. A. Wiggins, and
D. H. Rank
A 5 -meter vacuum spectrometer for the near infrared,
by D. H. Rank, G. D. Saksena and others
Highly precise wavelengths in the infrared, by D. H.
Rank, G. Skorinko and others
Vibration -roution spectra of HCN, by D. H. Rank,
G. Skorinko and others
Precision measurements of the wavelengths of infrared
absorption lines with diffraction gratings, by
D. H. Rank
Pressure-Induced shifts of HCl lines due to foreign
gases, by D. H. Rank, W. B. Birtley and others
Pressure shifting of spectrum lines, some empirical
generalizations, by D. H. Rank, W. B. Birtley and ^
others
(See also PB 143 097)
Optics
Army Chemical (Research and Development) Labs.,
Army Chemical Center, Md.
THE FABRICATION OP PLASTIC INFRARED FILTER
WHEELS, by Hugh R. Carlon. [1 Apr 59] lOp. 2 refs.
CWL Technical memo no. 32-41; AD-213 702.
Order from LC mi$l . 80, ph$ 1 . 80 PB 149 641
A
339
The second of three technical memoranda dealing with
various optical miaterials used in the filter wheel modi-
flcaUon at the LOPAIR (Long- Path Infrared) toxic agent
alarm device. Since the modified LOPAIR instrument
utilizes a rotating filter wheel for wavelength selection,
various filler wh«el construction techniques were in-
vestigated in an attempt to construct a durable, inex-
pensive non- hygroscopic, easily duplicated wheel. The
plastic (polyethylene substrate) filter wheel evolved
during these inve^tigations is discussed in this report.
Fluorothene (poly-trifluoro-monochloroethylene) and
talc (Magnesium Silicate) are used as the basic filter
materials. Subsequent testing has shown the plastic
filter wheel to be! completely reliable. (Author)
Battelle-Institui}B. V., Frankfurt-am-Main (West
Germany).
PERFORMANCE OF WORK TO DEVELOP METHODS
FOR PRODUCTION OF INFRARED INTERFERENCE
FILTERS IN THt RANGE OF 4.5 TO 15 MICRONS
USING SEMICONDUCTOR MATERIAL AS INTERFER-
ING LAYERS, AJ^D DIFFERENT CARRIER PLATES,
SUCH AS SAPPHIRE, MICA ARSENIC TRISULFIDE,
OR SILVER CHLORIDE. Final rept. for 1 Dec 58-
29 Feb 60 on Coifract DA 91-59I-EUC-I0U. [1960]
43p. 24 refs.
Ch-der from LC rtii$3. 30. ph$7. 80 PB 149 657
Attempts were n»de to prepare these filters by evapo-
rating the interference layer onto the carrier plates
under vacuum, ijifferent combinations erf filter mate-
rials were employed in the examinations and the fol-
lowing parametefs were varied: material at the carrier
plate, material (|f the interference layers, number ctf
the interference
layers.
layers, thickness ot the interference
Block Associates, Inc. , Cambridge, Mass.
RESEARCH AN5 DEVELOPMENT TO PRODUCE AN
INFRARED SOURCE, by Merle J. Persky. Final rept.
I, Part 1 on Contract AF 19(604)2420. 31 July 60,
TR-60-294-1; AD-244 901.
113.00, ph$6.30 PB 152 714M
no
32p. 5 refs. GRI
Order from LC
A study of the feasibility of enveloping a flare with an
Infrared filter fdac use as an infrared signal augmenter
was performed, lit is shown that an intervening coaxial
air stream can tie used to protect an enveloping filter
from the flame at a magnesium flare. A number' of
successful feasibility demonstrations were made with
flare "RITA" sullied by Picatinny Arsenal. The flare
was enveloped bf a "pyrex" glass tube. One such
demonstration u^d a coaxial protective air velocity of
150 m. p. h. The' inside diameter of the tube was 3
inches. The assembly was 43 inches long. Also, it
was demonsrratad that such a system has a very low
ratio of visible to infrared emission. The maximum
ratio of visible t^ infrared energy over 99% ai the
spherical field at emission (excluding the exit) is ap-
proximately l/lO%. The ratio is greater than 1% only
over 7 x 10"5% d( the spherical field of emission. The
successful filter i was a grade of commercial architec-
tural black platel glass known as Pittsburgh Plate Black
Carrara whose apearal transmission is similar to
Corning 7-56. (Author) (See also PB 152 713)
Block Associates, Inc., Cambridge, Mass.
RESEARCH, DEVELOPMENT, AND CONSTRUCTI(»
OF ROCKET-BORNE RADIOMETERS, by Frits
Zernike, Jr. Final rept. no. 1, Part 2 on Contraa
AF 19(604)2420. 31 July 60, 12p. GRD-TR-60- 294-2;
AD-244 902.
Order from LC mi$2.40, ph$3.30 PB 152 714-2
This report describes two rockeiborne infrared radi-
ometers for use in observing the tail plume radiation
of an Aerobee Hi research rocket. The instruments,
mounted in two of the rocket's fins, were launched in
an Aerobee Hi at Holloman AFB, Alamogordo, New
Mexico, In June, 1959. The instruments were filter
radiometers, one using a lead sulfide detector to ex-
amine sections of the spectrum from 0.5 p. to 3^ the
other using a Barnes thermistor bolometer to examine
sections from 3nto 30^. The operation of the instru-
ments is described and some of the design considera-
tions are noted. (Author) (See also PB 152 714-1)
Block Associates, Inc., Cambridge, Mass.
THE DESIGN, CONSTRUCTION AND USE OF A
GROUND BASED INFRARED RADIOMETER FOR (X-
SERVATION OF SATELLITES, by R. Gelinas. Final
rept. no. 1, Part 3 on Contraa AF 19(604)2420.
31 July 60, 41p. 8 refs. GRD-TR-294-3; AD-244 903.
Order from LC mi$3.30, ph$7.80 PB 152 714-3
This report investigates the problem of the optimizatia
of signal to noise by means of optical parameters,
detector configuration, and signal chopping for cases c(
current noise, photon noise, and lattice noise limited
phoioconductors. In addition the problem of deteaor
choice for expected signal wavelength is explored. A
feasibility system is described having a 60" diameter
parabolic reflector with an InSb deteaor, 18 mm.
square, cooled to -196°C and slaved to Millstone. The
final system is expeaed to consist of a 60" diameter
Schmidt correaed spherical refleaor with an InSb strip
deteaor, scanned by a continuously moving belt along
the strip and cooled to -196°C. (Author) (See also
PB 152 714-2)
Block Associates, Inc. , Cambridge, Mass.
THE DESIGN AND CONSTRUCTION OF AN INFRA-
RED SPECTRO- RADIOMETER FOR OBSERVATION
OF THE EARTH FROM A HIGH ALTITUDE VEHI-
CLE, by Ronald R. Willey, Jr. Final rept. no. 1,
Part 4 on Contraa AF 19(604)2420. 31 July 60. I6p.
GRD-TR-60- 294-4; AD-244 904.
Order from LC mi$2. 40, ph$3. 30 PB 152 714-4
A prototype satellite interferometer spearo- radiome-
ter has been built in order to study the infrared energy
from the earth. The theory of the device, a rapid
scanning interference spearometer, and the construc-
tion of a suitable cam-driven scanning mechanism ia
discussed. More work is required to produce a scan-
ning drive which will withstand the environmental cflB-
ditions involved in satellite applications. (Author)
Included in the report is:
Rapid scanning interference spearometry, pub. injw-
of Optical Society of America, v. 50, no. 3, Mar 60.
(See also PB 152 714-3)
340
Block Associates, Inc., Cambridge, Mass.
RESEARCH, DEVELOPMENT, AND CONSTRUCTION
OF A ROCKET-BORNE SPECTROMETER, by Philip N.
Gallagher, Jr. and Frits Zernike, Jr. Scientific rept.
no. 1 on Contraa AF 19(604)5738. 1 Aug 60, 17p.
1 ref. GRD-TN-60-610; AD-244 900.
Order from LC mi$ 2.40, ph$ 3. 30 PB 152 713
This report describes two rocketborne prism spec-
trometers, the second instrument being a modified
version of the first. The instruments utilized a lithium
fluoride prism, a scanning slit, and a lead selenide
detector to exaxnin^^e spectrum from O.6/1 to 4 ^.
Synchronous reaification was employed to improve the
aignal-to-noise ratio. Desirable design improvements
auggested by the results of each instrument's operation
are discussed. (Author)
Institute of Optics, U. otf Rochester, N. Y.
A REFLECTOMETER FOR THE VACUUM ULTRA-
VIOLET, by Abbott Smith. Technical note b 4 on Con-
traa AF 49(638)433. 2 Feb 60, 13p. 3 refa. AFOSR-
TN-60-284; AD-234 920.
Order from LC mi$ 2.40, ph$ 3. 30 PB 149 651
A newly designed device for the measurement of abso-
lue refleaance in the vacuum ultraviolet region is
discussed. Notable features of this reflectometer are
compaaness and simplicity. The source and mono-
chromator with which the refleaometer is used are
also discussed. The system produces data in the
wavelength range 800 A . to 2500 A . at any angle of
incidence between 15° and 80*^. A sample refleaance
ciffve for a crystal of KCl is shown. (Author)
Naval Ordnance Test Station, China Lake, Calif.
BIBLIOGRAPHY OF ELECTRO-OPTICAL AND MAG-
NETO-OPTICAL PHENOMENA AND THEIR APPLICA-
TIONS, by J. M. Ruhge and D. Green. Dec 59, 49p.
516 refs. NOTS TP 2377; AD- 235 612.
Order from LC mi$3. 30, ph$7. 80 PB 149 643
The bibliography contains entries taken from the
Industrial Arts Index and from the book and technical
report files of the NOTS Technical Library, covering
the following topics: the Kerr elearo-optlcal effects;
magneto- optical effects; applications of plezoelearic
crystals, iconoscopes, orthicons, and vidicons; image
converter tubes; high-speed shutters; and the electro-
luminescent effea and its applications. The bibliog-
raphy is current as of February 1959. (Author)
New York U., NY.
A STUDY OF THE FA* INFRARED PROPERTIES OF
CRYSTALS, by J. H. Rohrbaugh. Scientific rept. «11,
I Mar-31 May 60. on Millimeter Wave Project. Con-
tract AF 19(604)2673; successor to Contracts W28-099-
•c-171, AF 19(122)4 and AF 19(6(54)1115. [i960) I4p.
I ref. AFCRC-TN -60-959; AD-244 601.
Order from LC mi$2. 40, ph$3. 30 PB 152 624
Contents; j"
The optical constants of NaCl - a comparison E|etween
theory and experiment
The spectrometer
(See also PB 149 172)
Physics Lab. , Wright Air Development Div. , Wright-
Patterson AFB, Ohio.
STEEL MIRRORS FOR A STREAK CAMERA, by
O. Van P. Sessoms. Rept. for Feb 59-Mar 60 on
Nuclear Effeas on Space and Re-entry Vehicles.
Aug 60, 13p. 4 refs. WADD Technical note 60-155.
Order from OTS $0. 50 PB 171 191
In the development of an ultra -high speed streak cam-
era it became necessary to produce small ferromag-
netic prisms, whose faces were optically flat mirrors.
This report describes the grinding and polishing tech-
niques used to prepare optically flat surfaces on steel
prisms and the problems encountered in this work.
Standard optical shop equipment was used; the tech-
niques employed wfere similar to those used in pre-
pared glass mirrors. (Author)
Solid State Physics
Armour Research Foundation, Chicago, 111.
PRESSURE EFFECTS IN LUMINESCENCE, by
L. Reiffel. Final rept. (including Technical note no. 4)
on Contract' AF 49(638)113. 16 Sep 60, 31p. 29 refs.
ARF 1099-15; TR 60-128; AFOSR-TN-60-1119;
AD- 245 196.
Order from LC mi$3. 00, phJ6. 30 PB 152 731
Abstracts of previous work under AFOSR sponsorship
are given. Equations required for estimates on the
magnitude of various pressure- induced effects are in-
cluded. The effects treated include: quantum efficiency
for a metastable state; mean life of a metaetable state;
lifetime of a thermally quenched emitting state; quan-
tum efficiency of a thermally quenched emitting state;
emission band position; emission band width; emission
from communicating levels; cross-over probability.
(Author) (See also PB 139 215).
Bell Telephone Labs., Inc., Whippany, N. J.
FUNDAMENTAL STUDIES OF THE PROPERTIES OF
NATURAL AND SYNTHETIC QUARTZ CRYSTALS, by
J. C. King. Interim rept. no. 12, 1 June-31 Aug 58 on
Contraa DA 36-039-8C-64586. 2 June 59, 28p. 14 refs.
Rept. no. 27424-K; AD- 227 100.
Order from LC mi$2.70, ph$4.80 PB 149 721
Further evidence of the segregation of imperfeaion In
synthetic quartz, according to growth direaions, was
found. The defea induced absorjxion at 50°K, for a
frequency of 5 mc, is nearly 2 decades higher ingrowth
along the -fX-axis relative to the absorption in growth
along the Z-axis within the same crystal. Changes in
the behavior of the 20°K acoustic absorpjtion as a func-
tion of strain amplitude were studied in a sample of
synthetic quartz. (See also PB 139 743)
Bell Telephone Labs., Whippany, N. J.
FUNDAMENTAL STUDIES OF THE PROPERTIES OF
NATURAL AND SYNTHETIC QUARTZ CRYSTALS, by
J. C. King. Interim rept. no. 14, I Apr-30 June 59, oa
Contract DA 36 -039 -sc- 64586. 1 Dec 59, 27p. 4 refs.
Rept. no. 27424-M; AD- 231 409.
Order from LC mi$2. 70, ph$4. 80 PB 149 723
341
The acoustic ab^pcion in synthetic quartz specimens
was measured a^ analyzed. A specimen designated
BTL Run 691 wafe grown hydrothermally on a Z-face
seed crystal in k D2O solution. No significant changes
were noted in thie SO^K relaxation absorption in resona-
tors made of thils material as compared with similar
synthetic quanij grown in an H2O solution. A Z -growth
synthetic re8on4tor specimen was subjected to several
annealing operations. First the specimen was annealed
in air at SOO^C ind then twice vacuum annealed at the
same temperatire. After each of these operations the
low -temperature acoustic absorption of the Z-growth
material was remeasured, and In every case the mag-
nitude at the 5(fiK absorption was diminished. Two
AT-cut synlhetii: quartz crystal resonators, one from
growth on a Z-r^inor rhombohedral seed sirrface and
the other from 4 Z-cut seed, where subjected to static
electric fields, perpendicular to their nujor surfaces,
while at an elevated temperature. The conclusion was
reached that field sweeping AT-cui blanks at 0. 45
kv/cm and 500°C does not effea the elimination of
loss-inducing costal defects. The acoustic improve-
ments in both Z*-face and Z-growth AT-cut crystals
after applying a
field of 2. 7 lev/cm suggested that for
higher fields ih< impurities are removed from the body
of the crystal, jsee also PB 149 721)
Bell Telephone Labs., Inc. , Whippany, N. J.
FUNDAMENTAL, STUDIES OF THE PROPERTIES OF
NATURAL ANDI SYNTHETIC QUARTZ CRYSTALS, by
J. C. King. Inteirim rept. no. 15, 1 July- 30 Sep 59, on
Contract DA 36-039- sc- 64586. 15 Jan 60. 29p. 11 refs.
Rept. no. 27424fN; AD- 233 826.
Order from LC |ni$2.70. ph$4.80 PB 149 724
The acoustic behavior of an Al-doped quartz specimen
grown on a z-m^or rhombohedral seed crystal was ex-
amined. Crystal unit X-203 was subjected to a total ex-
posure of about lO^r . Three modifications were noted
which were due [0 the irradiation: (1) in association with
a high density of^color centers, relaxation absorption
appeared at lOOfK; (2) the 50^ defect concentration
was reduced by b faaor of 6:1; and (3) a growth oc-
curred in the abteorption below 30°K, emerging as a
loss peak near i29K for all measured frequencies of
vibration. The icoustic loss in crystal 1-14 between
4. 2° and 80°K alter irradiation was determined. Down
to about 15°K. little difference was noted in the ab-
sorption in the frequency range which extended from 3
to 17 mc. A special crystal holder was constructed
which allowed a iquartz specimen to be x- irradiated at
77°K and allowed the measurement of its resonator
characteristics tohile warming to room temperature.
(See also PB 149 723)
Clevite Research Center, Cleveland, Ohio.
STUDY OF METHODS FOR IMPROVING THE QUAL-
ITY OF SYNTHETIC QUARTZ, by Danforth R. Hale.
o. 1, 1 Dec 58-28 Feb 59. on Contract
247. 26 Mar 59, 15p. 3 refs.
i$2.40. ph$3.30 PB 149 692
Quarterly rept.
DA 36- 039 -sc- 7
Order from LC
Five synthetic quartz crystals have been processed into
resonators for leaking electrical measurements on
them. Experimental synthetic growth has emphasized
high purity and I- cut seeds. Special feed sources undtr
investigation cojtiprise: quartz recrysiallizcd on the
Z-surface. supef-pure silicon metal, and silica gel.
(Author)
Electro- Optical Systems, Inc. , Pasadena. Calif.
investigation of composite or stacked
Variable energy gap photovoltaic solar
ENERGY CONVERTER, by J. W. Bums, W. Evans,
ajid H. Armstrong. Semiannual progress rept. no. 1,
1 Sep 59-1 >n 60 on Contract DA 36-039- sc- 85244.
8 Jin60. 48p. EOS rept. no. 4O0-2Q-1, ARPA Order
no. 80-59; AD-232 922.
Order from LC ml$3. 30, phf7. 80 PB 1 49 706
Progress is reported on the attainment at improved
photovoltaic sdlar cell conversion efficiencies by
means at the stacked or composite energy gap solar
cell structure. A theoretical analysis is given at the
performance at a composite photovoltaic solar energy
converter consisting of 2 separate cells d differing
energy gaps. A description is given of the experi-
mental determination of the optical transmission of
CdS and of the transmission-reflection characterlstlci
of a spectrally reflective mirror. An experimental
program is being conducted on the composite energy
gap solar cell employing a silicon solar cell, a spec-
trally reflealve mirror, and a high energy gap solar
cell. (Author)
General Electric Co. , Schenectady, N. Y.
INVESTIGATION OF ORGANIC SEMICONDUCTOR^k
by G. P. Brown and a Afterbut. Rept. for 1 JulySJ-
31 Oct 59 on Electrical and Electronic Materials,
Contract AF 33(616)5949. Sep 60, 83p. 78 refs.
WADD Technical rept. 59-469.
Order from OTS $2. 25 PB 171 3«
The specific resistivity as a function of temperature
has been determined for a variety of organic compoondi
including polyacrylonitrile, polyacrylonltrlle conuin-
ing additives, 1, l-diphenyl-2-plcrylhydrazyl, naphdii
lene and its 1-amino-, 1-nltro-, 2-methoxy-, and
2-phenyl derivatives, 1, 4-diphenyl-l, 3-butadlene,
l,8-dlphenyl-l, .3, 5, 7-octatetraene, and several
picrates. The resistivities were obtained onmaterlali
In various stages of purification, over a wide ranged
applied volta«s, in nitrogen and In air, and in the
solid and (wherever feasible) In the liquid state. A
zone refiner was designed and used in the purification of
several materials. A model for conductivity inorganic
compounds has been advanced. (Author)
General Electric Research Lab. , Schenectady, N. Y.
APPUCATIONS OF TUNNEUNG TO ACTIVE mODES,
by R. N.Hall. Scientific rept. no. 1 on Contract
AF 19(604)6623. 22 June 60, 5p. ERD-TN-60-780.
Order from LC mi$l . 80, ph$l . 80 PB 152 473
The variation of potential with distance in degeneratelji
doped p-n junctions at absolute zero has been calculne^
exaaly, and a simple but reasonably accurate approxi-
mation formula has been found. Preliminary rcsistintr
and Hall mobility data in GaP are reported. (Author)
Georgia Inst, of Tech. Engineering Experiment
Station. Atlanta.
QUARTZ CRYSTAL STUDIES AND MEASUREMENTS
PHASE I. MOTIONAL PARAMETERS. PHASE II.
EQUIVALENT ELECTRICAL PARAMETERS. PHAff
III. AGING OF QUARTZ RESONATORS, by IssacKop
342
J. E. Rhodes and others. Quarterly rept. no. 1, 1 Aug
1 Nov 58, on Contraa DA 36-039-8C-78910. [1958] 87p
3 refs. AD- 219 334.
(i-der from LC mi$4.80, ph$l3.80 PB 149 695
Keaearch was surted to increase understanding of the
behavior of quartz crystals as frequency control and
flter devices. The motional parameters of thickness
■hear modes of AT- and BT-cut quartz crystals are
itudied to: (1) nteasure as a function of the plate and
electrode size the motional capacitance and shunt
capaclunce on quartz crystal disks of the AT- and BT-
tjrpea in the range 1 to 10 mc; (2) measure the motional
c^MCitance of the inharmonic overtones as a funaion ol
the plate and electrode size, and to compare the func-
donal dependence of the motional capacitance on the
electrode size with the solution following from the
■train distribution of the mode; and (3) measure the
capacitance ratio and the shunt capacitance in its
variation with the variation ai the inharmonic overtones
The behavior of commercially produced crystals in the
conventional HC 6/U mounts was measured and com-
pared with previous and continuing measurements on
laboratory units. One hundred quartz crystal resona-
tors of type CR-19/U were obtained and one-third of
each group received was placed in a constant tempera-
ture oven at 85^0 for periodic frequency measurements
Forty-five aluminum plated resonators were fabricated
ia glass containers.
(>orgia Inst, of Tech. Engineering Experiment
Station, Atlanta.
QUARTZ CRYSTAL STUDIES AND MEASUREMENTS.
PHASE I. MOTIONAL PARAMETERS. PHASE II.
EQUIVALENT ELECTRICAL PARAMETERS. PHASE
m. AGING OF QUARTZ RESONATORS, by IssacKoga
J. E. Rhodes and others. Pinal rept. for 1 Atig 58-
28 Feb 59 on Contract DA 36-039-8C-78910. [19591
I13p. 1 ref. AD- 220 647.
Order from LC mi$6.00, ph$18.30 PB 149 696
Approximately 150 resonators fabricated here and
mounted in glass containers have been stored at 85%
■od periodically measured for frequency. Over one
hundred of these were base -plated with aluminum and
not overcoated to frequency. The crystal blanks of two
groups were heated to 450°C in vacuo, cooled to 250OC,
and coated with evaporat xl aluminum. Subsequently the
unite were baked out at 180°C for three hours at a pres-
sure of 5 X 10"^ mm Hg and sealed off. These units
rinwed drifts of less than 0. 5 ppm in test periods of 60
to 160 days. Aluminum plated units similarly fabri-
CMd and overcoated to frequency with evaporated
■kninum exhibited drifts o.ily slightly larger. Resona-
tor* plated with bimetal films of gold or silver then
«lth electroplated nickel exhibited positive drift vectors
•hereas those coated with aluminum plus gold exhibited
Mgttlve ones. (Author) (See also PB 149 695)
Gordon McKay Lab. of Applied Science, Harvard U. ,
Ciinbrldge, Mass.
nELECTRIC CONSTANT OF GERMANIUM AND
SILICC*) AS A FUNCTK)N OF VOLUME, by Manuel
Cirdona. Technical rept. HP-5 on Contract
Nair- 1866(10). 1 July 59, I40p. Ill refs. AD- 226 982.
Ortkr from LC ml$6. 90, ph$21. 30 PB 149 628
An attempt is made to enlarge the knowledge of the
pressure and temperature dependence of the physical
properties of Ge and Si. The pressure and temperature
dependence of the RF dielectric constant of very high
resistivity Ge and Si is reported. These results, are
compared with the known pressure and temperature ef-
fects on the baiKl structure. A description is given of
the pressure and temperature dependence of the IR re-
fractive index of high purity Ge and Si. The pressure
dependence of the vertical energy gap at the center of
the Brillouin zone for Ge is reported. An increase of
dE
this gap with. pressure at the rate g = (I. 3 ±0. 1 x
10 ev X cm^/kg is found. Measurements are de-
scribed of the electric susceptibility erf the free carriers
in heavily doped n and p-type Ge and Si, as a function
of temperature and carrier concentration. (Author)
Honeywell Research Center, Hopkins, Minn.
THE DUCTILE- BRITTLE TRANSITION IN IONIC
S(XIDS, by T. L. Jbhnston, R. J. Stokes, and C H.
Ll. Technical rept. no. 5 on Contract Nonr- 2456(00).
July 59, 20p. 9 refs. HR-59-474; AD- 220 587.
Order from LC mi $2. 40, ph$3. 30 PB 149 684
Pbllshed monocrystals of sliver chloride, sodium
chloride, lithium fluoride and magnesium oxide have
been shown to exhibit ductility transitions when loaded
by impact bending. The behavior of silver chloride
stood apart from that of the other solids in that the
temperature below which it cleaved without macro-
scopic deformation was less than 0. 1 T_ (where T„
is the melting point in degrees Kelvin), u is
emphasized that the ductility of ionic solids is ex-
tremely sensitive to strain rate of the presence of a
notch. (Author)
m
Honeywell Research Center. Hopkins, Minn.
EFFECT OF GRAIN SIZE ON THE DEFORMATION
OF POLYCRYSTALUNE SILVER CHLORIDE AT VAR-
IOUS TEMPERATURES, by R. D. Camahan. T L.
Johnston and others . Technical rept t»o. 7 on Contract
Nonr- 2456(00). Jan 60, 22p. 5 refs HR-60-412:
AD- 234 124.
Order from LC mi$2 . 70, ph$4 .80 PB 152 891
The effect of grain size on the stress-strain curve of
polycrysialline silver chloride has been determined at
liquid nitrogen temperature, -72°C and 26°C. It has
been shown that when pencil glide is the operative slip
mode (at -720C and 26*^), a change in grain size has
only a minor effect; indeed, the proportional limit is
independent of grain size at these temperatures . At
liquid nitrogen temperature, fewer slip systems are
operative atKl slip bands are quite straight. At this
temperature, the stress-strain curve is sensitive to a
change in grain size, the proportional limit and rate of
work hardening increase with a decrease fn grain size.
In addition, it has been found that when slip Is confined
to flat crystallographic surfaces as at liquid nitrogen
temperature, the ductility of polycrystals is limited by
cleavage which is nucleated by an intergranular crack,
in the upper temperature range, however, polycrystals
are ductile and finally neck down to a knife edge.
(Author)
3«3
Ulinois U. [Urbfna].
RESEARCH ON DIFFUSION AND IMPERFECTIONS
IN METALS, by JR. W. Balluffi. Final rept. on Con-
tract AF 18(6O3)J|06. 30 Aug 60, 13p. 6 refs. AFOSR
TR-60-130; AD- ^45 088.
Order from LC rmiJ2. 40, ph$3. 30 PB 152 683
Specific investigations include: (1) structural changes
in the diffusion z^ne during chemical diffusion; (2) the
effect of noo- equilibrium vacancies on the kinetics of
Kirkendall diffusion; (3) the Kirkendall effect in the
hexagonal close-backed phase of cadmium and mercury;
(4) the effect of simultaneous plastic deformation on
self- diffusion in |ilver; (5) the effect of a steady rate of
plastic deformatiton on chemical diffusion in copper-,
zinc alloys; (6) rijlative polygonization rates in a num-
ber of close- pact ed metals and alloys; (7) the deter-
mination erf diffusion coefficients in chemical diffusion.
Institute of Matfiematlcal Sciences, New York U.
N. Y
THE SOLimON OF THE FUNCTIONAL DIFFER-
ENTIAL EQUATtON FOR THE STATISTICAL EQUI-
LIBRIUM OF A CRYSTAL, by Robert M. Lewis and
Joeeph B. Keller.! Rept. on Contract AF 49(638)341.
Aug 60, 46p. 11 J-efs. Research rept. no. HT-6;
AFOSR-TN-60-9fc5; AD- 245 399.
Order from LC i^i$3. 30, ph$7. 80 PB 152 726
t'
The equilibrium fequation is solved in terms of a power
series in the ternperature and from it the results are
obuined. The fcfm of the solution was suggested by a
consideration of the asymptotic evaluation, for low
temperature, of ^he integral defining the generating
functional. Althdugh this is not a practical method of
obcalning the ser|es expansions, it has been carried
out for the first |erm of the partition function. This
consideration suggests that the expansions are asymp-
totic rather thaniconvergent.
<C«
Leicester U
INVESTIGATION
IN INSULATING
technical repi
DA 91-591-EUC
Order from LC
Brit.).
OF THE CONDUCTION MECHANISM
SOUEJS, by Walter Eric Spear. Final
np. 1, 1 Oct 59-30 Oa 60 on Contract
1269. Oct 60, 38p. 34 r els.
riii$3.00, phS6.30 PB 152 925
A pulse method n»s been developed for the study of
carrier mobihty and trapping effeas in insulating
solids. A study W the effeaive hole mobility fJ in
vitreous Se is defecribed. The dependence of the pulse
amphiude on applied field, specimen thickness d and
incident electron: energy V, is discussed. The applica-
tion of the experimental method to single crystals o*
monoclinic Se, KlgO and CdS is described.
Lincoln Lab.
ANTIFERROMAi
METER AND SI
G. S. Heller, J.
on Contract AF
82G-0023, AD-2'
Order from LC
Because of their
materials have
fass. Inst, of Tech., Lexington.
tNETIC MATERIALS FOR MILLI-
-MILLIMETER DEVICES, by
Stickler, and J. B. Thaxter. Rep».
(604)7400. 8 Nov 60, 26p. 24 refs.
992.
i$2.70, ph$4.80 PB 152 932
ligh internal fields, antiferromagnetic
uural resonant frequencies in the
millimeter and submillimeter wavelength region of the
electromagnetic spectrum. Since these normal modei
are circularly polarized and can be tuned by an applied
magnetic field, devices similar to the usual ferrlte
devices are possible at these high frequencies with tiw
application of relatively low fields. The dynamics of a
simple antiferromagnetic system are briefly reviewed
and the important quantities which characterize anti-
ferromagnetic devices are discussed. The figures of
merit for antiferromagnetic resonance isolators and
phase shift devices are derived. Experimental data oa
resonant frequency and line width, as well as a typical
non-reciprocal resotiance absorption trace showing a
reverse to forward loss of 10 to 1 in chromic oxide
at 140Mft1cp8 and at 77°K is presented. (Author)
Lincoln Lab. , Xtess. Inst, of Tech. , Lexington.
PHOTO AND THERMAL EFFECTS IN COMPENSATET
ZINC DOPED GERMANIUM, by Robert J. Keyes. Rept.
on Contract AF 19(604)7400. 21 Oct 60, 15p. 2 refs.
85G-0008; AD- 245 671.
Order from LC mi$2. 40, ph$3. 30 PB 152 973
At low temperatures zinc doped germanium exhibits
effects when the lowest zinc levels have been filled by
electrons from compensating antimony impurities, in-
ciuding negative photo-conduction, a discontinuity in
the temperature dependence of the sample resistivity,
and storage of free electrons produced by radiation of
greater energy than the semiconductor gap. A qualiu-
tive theory explains all the observations.
Lincoln Lab. . Mass. Inst, of Tech. . Lexington.
SOLID STATE RESEARCH. Quarterly progress rept.
for 15 July 60 on Contract AF 19(604)5200. 16 Sep W.
108p. 88 refs. AFCCDD-TN-60-1014; AD-243 927.
OrderfromLCmi$5. 70, ph$l6.80 PB 152 462
Contents: %
Semiconductor device design *
Chemistry
Materials research
Band structure of solids
Microwave and magnetic properties of solids
Magnetic materials
Magnetic films
Semiconductor components
Display techniques
(See also PB 153 251)
Materials Research Lab., Watertown Arsenal, Mass
ON THE CONTRIBUTION OF THE FERMI CONTAQ
TERM TO THE MAGNETIC FIELD AT THE NU-
CLEUS, by R. E. Watson and A. J. Freeman. Nov 60,
7p. 9 refs. MR L rept. no. 89.
Order from LC ml$1.80, ph$1.80 PB 152 854
The dominant source of the effective magnetic field at
the nuclei in ferromagnets was investigated for tranai-
tion element atoms and ions by means of a series of
spin (or exchange) polarized Hartree-Fock calcutatlona
Calculations were done for both free atom and crude
crystalline environments. The effeaive field is not
however large enough to overcome the positive con-
tributions of the outer electrons. (Authca:)
344
Metals Research Lab. , Brown U. , Providence, R. I.
ULTRASONIC ATTENUATION AND VELOCTTY
MEASUREMENTS IN SOLIDS, by Rohn Truell Final
i«pt. on Contract DA 19 -020-506 -ORD-3882. 1 Mar 59.
Mp. 15 refs. WAL 143/14-50; AD-217 993.
Order from LC mi$2. 70, ph$3. 80 PB 149 690
Megacycle ultrasonic methods constitute a tool for the
Hudy of the physical properties of solid materials In
the same way as do x-ray, electron, optical, and neu-
tron diffraction me^iods, thermal adKelectrical con-
ductivity methods, optical and microwave absorption
■■•■urements. The material presented is primarily
the story of what physical properties can be studied by
megacycle ultrasonic methods together with a discus -
•ion of the details of the methods that have been used.
Microwave Research Inst., Polytechnic Inst, of
Brooklyn, NY.
TRANSMISSION LINE FORMULATION FOR SEMI-
CONDUCTORS, by Herbert Kurss. Quarterly rept.
BO. 13, 1 July- 30 Sep 59, on Contract DA 36-039-8C-
730S2. 30 pec 59. 19p. Rept. R-523. 38-59;
PIB-453.38.
Order from LC ml$2. 40. phJ3. 30 PB 149 679
Pw plane wave scattering from a crysul plane, the
geometry of the scattered rays, the losslessness,
reciprocity, and symmetry constraints on the fields
far from the crystal plane are derived. The energy
band structure of a Kronig-Penny crystal is analyzed
vben (a) the crystal is semi -infinite (b) the crystal
contains a symmetric impurity.
Naval Ordnance Lab. , White Oak, Md.
TEMPERATURE DEPENDENCE OF THE GYROMAG-
>ETIC EFFECT IN UTHIUM CHROMATE FERRITE,
bjrR. S. Hebbert. 2 Jan 59. 14p. 6 refs. NAVORD
rept. 5765; AD-213 537.
Order from LC mi$2. 40, ph$3. 30 PB 149 738
Metsurements were taken of the gyromagnetism and
Magnetization of lithium chromate ferrite (Lio. sFei 25
Cr| 25O4) through a temperature region including
compensation points of both magnetization and spin.
Cenain qualitative predictions by Wangsness have al-
ready been verified: in the range 570C to 68°C the
direction of the Faraday rotation is rever.sed.
New York State Coll. of Ceramics, Alfred U.
DIELECTRIC LOSSES DUE TO DISLOCATICWS IN
SAPPHIRE, by D. P. Detwiler and N. M. Tallan. Rept.
ooContraa AF 49(638)87. 29 June 60, I77p. 69 refs.
AFOSR -TN- 60- 884.'
*der from LC mi$8. 10, ph$27. 30 PB 152 544
When the dielectric loss of Linde flame-fusion grown,
•ingle crystal, clear sapphire was studied at frequen-
ciea between 10^ and 10* cps and temperatures be
tween -160 and 400°C, dielectric loss maxima were
ohiVved. The loss process was more pronounced with
te optic axis in the direaion of the applied field than
•1th the optic axis perpendicular to the field. With
careful balancing of the bridge-guard circuit system
"■ed, no significant conduction loss was observed in
the temperature range studied. It is therefore sug-
gested that the conduction loss commonly observed in
the upper portion of this range for unguarded sapphire
samples is on the surface rather than in the bulk of
the crystal.
New York U. , N. Y.
STOICHIOMETRY AND ELECTRONIC PROPERTIES
OF PbTe, by Edward Miller, Kurt K. Komai-ek, and
Irving B. Cadoff. Rept. for 1 Dec 56-30 Sep 59 on
Solid State Research and Properties of Matter, Con-
tract AF 33(616)3883. July 60. 61p. 35 refs. WADC
Technical rept. 59-57(i supersedes WADC-TR-59-
570. Dec 59; AD-246 593.
Order from OTS $1.75 PB 171 356
Off-stoichiometric single crystals of PbTe were grown
by the Bridgman technique at a solidification rate of
0. 35 cm/hr. At this low solidification rate the crystals
were longitudinally segregated, the compositit)n at any
point corresponding to that dictated by the solidus curve
of the phase diagram. The phase diagram shows that •
PbTe has an off-stoichiometric melting point; the dif-
ference in coixrentration between the maximum melting
point and the stoichiometric point being 0. 002 atomic
percent, with the congruent melting point on the tellur-
ium rich side of the stoichiometric point. Stoichio-
metric PbTe is in equilibrium with liquid 0. 41 weight
percent rich in lead, the equilibrium temperature being
923. 2%. The solubility of boch lead and tellurium in
PbTe is restricted, the maximum lead and tellurium
excess being 5 x lO^^ atoms/cm3. Resistivity. Hall
coefficient, and thermoelectric power measurements
were made as a function of temperature on three slices
corresponding to stoichiometric, excess lead, and ex-
cess tellurium. The results obtained were analyzed
for the basic electronic parameters of the material.
The energy gap at absolute zero was calculated to be
0. 24 eV, and has a temperature variation of •♦-2. 5 x
10-^ eV/OK. The mobility ratio is 2. 2 -0. 15 and the
electron and hole room temperature mobilities are
1 170 and 500 cm2/volt-8ec respectively. The elec-
tronic effective mass was found to be 0. 22 m and the
hole effective mass 0. 29 m. (Author)
Northwestern U. , Evanston, III.
RESEARCH ON THE PYROELECTRIC PROPERTIES
OF SINGLE CRYSTALS OF CAOVIIUM SULFIDE AND
ZINC SULFIDE, by R. Frerichs apd W. Minkus. Rept.
on Contract AF 33(616)5625. Aug,60. 151p. 38 refs.
ARL Technical rept. 60-301.
Order from OTS $2.75 PB 171 338
This report describes the pyroelectric effect of a
cadmium sulfide crystal and determines the values of
its pyroelectric constant in the temperature range
-I950C and 72°C. This is the first time that the tem-
perature dependence of a pyroelectric constant has
been determined for a covalent typi crystal. The
method used to measure the response and to determine
the values of the pyroelectric constant are described.
The experimental error in the values of the pyroelec-
tric constant is estimated for each of tlie ambient tem-
peratures at which the effect was measured. A new
theory is developed to explain the temperature depend-
ence observed. (Author)
I
345
Physical Reseaiich Lab. , Space Tech. Labs. , Inc. ,
Loa Angeles, cilif.
SUPERCONDUCTIVE PROPERTIES OP VACUUM DE-
POSITED INDTUM FILMS, by Frederick W. Schmidlln,
Arthur J. Learn 4nd others. Rept. on Contract Nonr-
2542(00). [1960] I3p. 6 refs. PRL-9-18; AD-231 160.
Order from LC tAH4- 50, ph$l2. 30 PB 152 901
Contents: |
Sample preparation
Measuring apparatus and technique
Steady -state response to a direct current
Meaning d critical current
Evidence of joule heat
Dependence of oritical current on temperature
Dependence on fridth and thickness
Transient response to a suddenly applied current
Description at transition
Dependence of transition time on current and
temperature
Defiendence of trinsltion time on film geometry and
substrate I
Dependence' of col-nering and isochronous currents on
temperature ami their significance
Raytheon Co. , ^altham, Mass.
BETA SILICON (JARBIDE. by D. M. Warschauer.
Scientific rept. nb. 2 on Contract AF 19(604)6133.
15 Sep 60, 41p. 4 rets. AFCRL-TN-60-1103.
Orter from LC n^i$3. 3a ph$7. 80 PB 152 628
The kinetics of gaseous-cracking of SiCl4 and SiHCl4
in the presence df H2 to form SiC are discussed.
Looped silicon cdrbide crystals obtained with this
method o( gitwtWare described and illustrated. An
anempt to control nucleation density and growth rate
in the solution method by dilution with germanium has
been tried and abandoned. The effect of variation of
other growth parameters is reviewed. Progress with
Hall and resistivity measurements is discussed. De-
termination of thf temperature shift of the optical ab-
sorption edge in tubic material is almost complete.
Two papers recently given are appended because they
summarize the knowledge gained on some erf this work
to date. (Author) (See also PB 148 354)
Wayne State U .
[Detroit, Mich. ]
PREPARATION /iND PROPERTIES OF CUPROUS
OXIDE AND CUPROUS OXIDE PHOTOVOLTAIC
CELLS, by Dan trivich and Robert S. Toth. Technical
rept. no. 4 (Final) on Contract [AF 18(600)481).
Aug 60, 32p. 25 ^efs. AFOSR TR-60-125; AD- 245 116.
Order from LC rii$3.00, ph$6.30 PB 152 694
The electrodeposited cuprous oxide photovoltaic cells
were found to be much less efficient for energy con-
version than the Diermal cells but they were consider-
ably improved by' a sulfiding process. The mechanism
of the sulfide sen^tization was shown to be due to a
highly conduaing; surface film erf cuprous sulfide which
lowered the serias resistance of the cells. The elec-
trodeposited cupiious oxide had a very fine crystal size
but the same cryital structure as the thermal cuf>rou8
oxide. The resistance of the electrolytic cuprous oxide
was much higher than that of the thermal material, thu(
making it more sjsceptible to the sulfiding treatment.
The visible and infrared spectra of the two types of
cuprous oxide were similar except that the electrolytic
material had additional absorption bands at 3.04 and
6.05^. Ionic bombardment with hydrogen produced the
desired front Junctions on thermal cuprous oxide, and
in doing so reduced the top surface to copper. The re-
sulting cells had an efficiency of about 1% for the coo-
version of solar energy to electrical energy, consid-
erably greater than that of the back-wall cells. Efforti
were made to produce cuprous oxide in single crystal
form. A successful method was developed, using a
grain growth process at high tempierature . The elec-
trical conductivity of the single crystal cuprous oxide
was measured at high temperatures and various oxygen
pressures. At constant temperature, the conductivity
varied with the l/7th power of the oxygen pressure at
not too low pressures. At constant oxygen pressure,
the logarithm of the conductivity varied linearly with
the reciprocal of the absolute temperature, and from
these linear plots activation ener^es were calculated.
(Author)
Theoretical Physics
Avco-Everett Research Lab. , Mass.
MAGNETOHYDRODYNAMIC SHOCK WAVE IN A
COLLISION -FREE PLASMA, by F. J. Fishman,
A. R. Kantrowitz, andH. E. Petschek. Rept. on Con-
traa Nonr- 2524(00). Jan 60, 28p. 12ref8. Research
rept. 85: AD-232 911.
Order from LC miJ2.70, ph$4.80 PB 152 912
In high temperature low density plasmas collisional
relaxation becomes slow compered to other character-
istic times (collision free plasma). It seems likely that
under such circumstancessmore powerful dissipative
mechanisms would appear and the understanding of
these mechanisms is basic to the treatment of contain-
ment and flow problems. It is known that shock waves
propagating perpendicular to a magnetic field can be
much thinner than a mean free path, which implies dial
more powerful dissipative mechanisms must exist. An
attempt is made to identify the dissipative mechaniann
operative in a shock wave with randomized magneto-
hydrodynamic waves of large amplitude. The entropy
production process is the scattering of waves on wave*.
The typical wave mean free path is comparable to an
ion Larmor radius inside a shock front. The short
mean free path for this scattering process implies that
continuum magnetohydrodynamics can be applied in
many cases even when the interpjarticle mean free path
is quite large. Both the shock thickness and its depend-
ence on the Alfven Mach number obtained in this
manner are in agreement with MAST shock tube
experiments. (Author)
Brown U. Div. of Engineering. Providence, R. I.
THE EFFECT OF AN ALTERNATING ELECTRIC
FIELD ON ELECTRON Pl.OW IN AN INHOMOGE-
NEOUS PLASMA, by Lewis Wetzel. Rept. on Cortrad
AF 19(604)4561. Aug 60, 26p. 9 refs. Scientific rept
no. AF 4561/9; AFCRL-TN -60-994; AD-245 206.
Order from LC mi$2. 70. ph$4. 80 PB 152 742
It is shown that the interaction between an alternatinf
electric field and spatial inhomogeneities in a plasma
will produce perturbations of both the random diffusion
of the electrons and the alternating current excited in
the plasma by the applied field. The random diffusion
18 reduced in the direction of the field, the anisotropy
being of the order of UcAJa- where Uc is the average
energy gained by an electron from the field between
collisions, and Ug is the random energy of the elec-
tron. The a. c. current is altered by an additional tern-
proportional to the rate at which the gradient of the un-
perturbed electron density changes in the direction of
the applied field. Of interest here is the possibility of
induced currents transverse to the applied field. Nu-
merical examples indicate that these effects will usu-
ally be quite small, but may become significant under
auitable conditions. (Author)
Electron Tube and Microwave Lab. , Calif. Inst, of
Tfich P& sddc nfl
STUDY OF ELECTROMAGNETIC INTERACTION IN
PLASMAS, by R. W. Gould and D. G. Do*. Quarterly
progress rept. no. 1, 1 Dec 59-30 Apr 60, on Contract
DA 36-039-SC-85317; Continuation of Contract DA 36-
0»-8C-78230. [1960] 15p. AD-242 179.
Order from LC mi$2. 40, ph$3. 30 PB 152 996
Further design considerations for the cyclotron orbit
plasma oscillator are given including shaping of the
magnetic field to produce the desired electron trajec-
tories. Preliminary measurements on a hydrogen dis-
charge tube show that the necessary electron density of
lO^lcm'3 can be obtained with a discharge current of
.650 amp. and electron temperature of 120(XyK. The
construction of a PIG discljarge tube for high density
piasma generation is proceeding simultaneously.
<Author)
Michigan U. , Ann Arbor,
THEORY OF PLASMAS, PART I, by R. K. Osbom.
Rapt on Research on Particle Dynamics, Contract
AP 33(616)5585. Aug 60, 69p. 16 refs. ARL Techni-
cal rept. 60-274, pt. 1.
Order from OTS $1. 75 ( PB 171 336
This paper presents a portion of an attempt to develop,
in u-space, a unified theory of plasmas - the main
purpose being to localize points of difficulty or obscu-
rity encountered In the deduction of a description c*
luch systems. Within the context of non-relativistlc
particle dynamics, exact relations describing the parti
de and photon singlet densities a re deduced - the rela-
ttons for the particle densities being essentially those
developed earlier by Brittln. It is theii shown that the
relations governing the particle densities are crudely
reducible to Boltzmann's and/or Vlasov's equations in
the sense of certain reasonably clearly stat'ed, but ill-
evaluated, approximations. The relation describing the
photon singlet density is discussed in considerable
detail, and a reduction to the conventional equation of
Phtxon transtxjrt is accnmoMshfvi
Microwave Physics Lab. , Sylvania Electric Products,
Inc., Mountain View, Calif.
THE NONLINEAR INTERACTION OF AN ELECTRO-
MAGNETIC WAVE WITH AN ANISOTROPIC PLASMA
LAYER. PART I: THEORY OF HARMONIC GENERA-
TION, by R. F. Whitmer andE. B. Barrett. Scientific
rept. no. 2 on Investigation of Nonlinear Phenomena
Associated with Ionized Plasmas, Contract
AF 19(604)4083. 30 Aug 60, 36p. 13 refs. AFCRL-
TN-60-990; AD- 244 881.
Order from LC mi$3.00, ph$6.30 PB 152 633
The theory of electromagnetic wave propagation through
an anisotropic ionized layer, including the effects of the
nonlinear terms in the Boltzmann transport equation, is
presented. The method of solution of the nonlinear
equations involves an expansion of all of the dependent
variables in a Fourier series in time. The differential
equations describing wave pre agation are then solved,
for each frequency in the series, for plane wave propa-
gation, including all of the reflections within the plasma
layer . A solution in closed form has been obtained,
urxler small signal conditions, for the field at the h-th
harmonic in the Fourier series. A discussion of the
properties of the wave at the second harmonic frequency
as a funaion of the dc magnetic field strength, the
electron density, the electron-neutral particle collision
frequency, the field strength of the incident wave, and
the thickness of the plasma layer is given. (Author)
Plasma Propulsion Lab. , Republic Aviation Corp. ,
Farmingdale, N. Y.
POWER SUPPLY DESIGN PARAMETER STUDY FOR
ELECTROMAGNETIC DETONATIONS (PHASE I) by
K. M. Foreman. Rept. on Contract AF 49(638)552.
31 Aug 60, 21p. 9 refs. PPL-TR-60-3; AFOSR TN-
60-1198; AD-245 690.
Order from LC ml$2.70, ph$4.80 PB 152 955
The characteristics of an electrical power supply
suitable for electromagnetically induced detonations
are indicated. A parametric study of circuit constants
for a single simple R-L-C series circuit shows that
this type of pofwer supply is inadequate to provide for
all requirements of a propulsion device. However, a
suitable pulse of current for laboratory demonstration
purposes can be achieved with the following typical
circuit constants: L ■ 10*8 henries; C ■ 3 x 10"5
farads; R - 10'2 ohms. Directions for future studies
to satisfy practical energy release applications are
speculated upon. (Author)
Technische Hochschule; Stuttgart (West Germany).
DEVELOn^^ENT OF A DIAGNOSTIC CCVICE FOR
THE DETERMINATION OF MEAN EFFECTIVE TEM-
PERATURES IN PLASMAS USING SHOCK WAVE
MEASUREMENTS, by E. Hisam and W. Bez. Interim
rept. for 1 Jan-31 Dec 59 on Experimental Part, Con-
tract AF 61(052)199. Feb 60, 52p. 41 refs.
AD- 235 859.
Order from LC mi$3.60, ph$9.30 PB 153 626
This report released for sale to the public 16 Jan 61.
A description is given of the development of a diagnos-
tic plasma shock tube for the determination cA mean
effective temperatures in pulse discharges. The tem-
perature and pressure in such a discharge is to be
estimated from observations of the shock velocity in
the tube. Methods are described of measuring the
shock propagation velocity by using photocells. Re-
quired reproducibility of experiments is observed by
using an image converter with effective exposure times
ii
347
of approximately |0'' sec. The extensive electronic
equipment develoted for this diagnostic method is dis-
cussed in detail. KAuthor)
hermodynamics
Armour Research Foundation, Chicago, 111.
thermophysicAl properties of solid MATE-
1. elements (melting tem-
PERATURE ABOtE 1000°F), by Alexander Goldsmith,
Thomas E. Wate^an, and Harry J. Hirschhoni. Rept.
for 1 July 57-31 Aug 60 on Thermophysical Data Con-
solidation, Contrict AF 33(616)5212. Rev Aug 60,
735p. WADC Teclinical rept. 58-476, Volume I.
AD-247 193.
Order from GTS iS. 00 PB 171 329-1
This report released for sale to the public 3 Jan 61.
Thermophysical Property data, and their variation with
temperature, arq presented for a great number of
solid materials, tiased on literature published during
the period 1940-11957. Each reported value is shown
and annotated, ai|j recommended "most probable
value" curves ar^ given. Only those melting above
1(XX]^ are included. Properties covered include the
following: Melting point, Density, Latent heats,
Specific heat, Thermal conductivity. Thermal dif-
fusivity, Emi8si\^ity, Reflectivity, Thermal expansion.
Vapor pressure, |and Electric resistivity. (Author)
Arnold Englneei ing Development Center, Tullahoma,
Tenn
AN ANALYSIS
MEASURING HE
GASES, by J. C
Contract AF 40(
4 refs. AEDC T
Order from LC
SLUG-TYPE CALORIMETERS FOR
T TRANSFER FROM EXHAUST
'estkaemper. Rept. on ARO, Inc.,
1)800 S/A 11(60-110). Nov 60, 44p.
60-202; AD- 245 524.
i$3.30. ph$7.80 PB 152 966
Insulated-mass, klug-type calorimeters were investi-
gated for use in measuring convective heating prcxluced
by rocket exhaust gases which circulate in the base
region of a missile. The necessity of designing and
installing caloriraeters which do not alter the normal
thermodynamic conditions is discussed. Analysis is
made of various Sources of error in slug calorimeters,
particularly extraneous heat gain or loss. A numeric 1 1
method is used t<i compute transient temperature dis-
tributioiis in por«ie lain- cement-type insulation; con-
duction errors arte calculated for various insulation
configurations using these distributions. A method for
minimizing such
jrrors is described. (Author)
Florida U. Engipeering and Industrial Experiment
Station, Gainesuji
INELASTIC SCA
OXYGEN , by E
Technical rept
Ions , Contract
AD- 232 561.
Order from LC n|i$2.40. ph$3.30
He.
TERING OF NEGAllVE IONS IN
1. MuscWitz, Jr. and C. E. Baker.
9 on A Study of Negative Gaseous
-580(01). Dec 59, 20p. 15 refs;
PB 152 137
, no.
N<nr
Measurements at the inelastic cross sections for the
scattering of O* , O2' , H' , and OH' ions in oxygen gtt
in the ion-energy range 4-400ev are presented. An
improved collision chamber used for these measure-
ments is described. The results are interpreted in
terms of the possible types of inelastic collisions
taking place: (1) electron detachment, (2) electroij^t-
change, and (3) ion-molecule reaction. It is shown by
means of retarding potential analyses that the energy
of the electrons produced in electron detachment colli-
sions is considerably higher than thermal energy,
perhaps as much as several ev at the higher incident
ion energies . (Author)
Georgia Inst, of Tech. Engineering Experiment
Station. Atlanta.
THE TRANSPORT PROPERTIES OF A FULLY
IONIZED GAS. I. A QUANTAL STUDY OF DIFFU-
SION AND VISCOSITY CROSS SECTIONS FOR A
SCREENED COULOMB BOTENTIAL, by M. R. C.
McDowell and G. Peach (Royal HoUoway Coll. . U. of
London). Technical rept. no. 5 on Contract
AF 18(600)1524. 1 Sep 60, 61p. 32 refs. AFOSR-TN-
60-945; AD-245 157.
Order from LC mi$3. 90, phJlO. 80 PB 152 789
Bom's approximation and the Massey-Mohr approxima
tion are used to obtain quantum mechanical values of
the diffusion and viscosity cross section Qq and Q,' fat
a screened coulomb potential. The parameters are
chosen to represent an ionized gas with 10* < ru
ilOl8, ne being the electron density, and 5xlO^<Te
j^lO^ °K, Tg being the temperature. The scattering
phase shifts are also evaluated and compared with
those obtained from direct numerical integration of the
scattering equation. Bom's approximation to the phase
shift is used in a Fax^n-Holtsmark type analysis to
give more accurate values of the cross sections at lot
T and large ne- The results are used to discuss the
behavior of the electrical conductivity of a fully ionixed
gas. At high temperatures they are in close agreemoi
with earlier workers, but predict a different tempera-
ture dependence if (i-) is small. (Author)
ne
Massachusetts Inst, of Tech., Cambridge.
EVALUATION OF FREON 12 PROPERTIES AND Tlffi
GENERAUZED FLUID PROPERTIES NEAR THE
CRITICAL POINT, by P. C Calcaterra. Technical
rept. no. 3 on Contract Noar- 184 1(1 4). Mar 60, 39p.
6 refs. DSR no. 7484; AD- 242 361.
Order frqpi LC mi$3.00. ph$6.30 PB 150 036
To correlate the heat transfer charaaeristics of fluids
near and above the critical point, the values of the
fluid properties must be known over this range. This
report discusses in detail how the values of the density,
viscosity, thermal conductivity, and the specific heal
are evaluated for Freon 12 at 600 psia and over the
temperature range of 140^ to 400PF . Curves are pre-
.sented for determining the values of these properties
throughout the critical region for Freon 12 and for
fluids in general. (Author)
34t
Massachusetts Inst, of Tech., Cambridge.
HEAT TRANSFER TO FLUIDS AT SUPERCRITICAL
PRESSURES, by J. C. Chato. Technical rept. no. 4
(Final) on Investigation ot Fluids for Power Cycles,
Contraa Nonr- 1841(14). 31 Mar 60, 15p. DSR
BO. 7484; AD- 242 362.
Order from LC mi$2.40, ph$3.30 PB 150 035
(Contents:
Table ot enthalpies of Refrigerant- 12 at 610 psia.
Heat transfer results of experimental runs
Wave Propagation
Air Force (Cambridge Research Labs. ] Bedford,
Marss.
THE AIRBORNE SURVEY OF ICE CAPS AT RADIO
FRECJUENCIES, by Noel Stone. Aug 60, 20p. 10 refs.
ERD-CRRC-TR-I71: AD-245 724.
Order from LC mi$2. 40, ph$3. 30 PB 152 987
The theoretical feasibility of an aerial survey of ice
cap thickness is explored by computing (1) the scattered
field intensity from a snow-air surface, (2) the absorp-
tive transmission loss in snow and ice and (3) the net
return from the ground beneath the Ice. The air-ice
reflection loss is 10 db, the scattering loss, around
20 db. The absorption at 300 Mc is 0. II db. /meter in
ice, 0.035 db. /meter in snow. It is shown that an air-
craft may in theory make a survey under such
conditions. (Author)
Canterbury U. (New Zealand).
STUDIES OF PARTIAL REFLECTIONS FROM THE
LOWER IONOSPHERE, by J. B. Gregory. Final rept.
on Contract Nonr -2651(00). 1 Mar 60, lOp. 5 refs.
AD- 236 967.
Order from LC mi$1.80, ph$1.80 PB 147 558
Studies of partial reflections of radio waves at a fixed
frequency of 1 . 75 mc were carried out in 2 pro-
grammes. These programmes comprised an analysis
of a year's routine observations of the lower iono-
sphere, and the instrumentation of a method of meas-
uring the electron concentration of the lower iono-
qihere. Results are summarized. (Author) j
Center for Radiophysics and Space Research, ComeU
U., Ithaca, N. Y.
AN ANALYSIS OF THE EFFECT OF AN IMPOSED
MAGNETIC FIELD ON THE SPECTRUM OF INCO-
HERENT SCATTERING, by T. Laasperc. Scientific
rept. no. 4 on Contract AF 19(604)6158. 15 July 60,
79p. 19 refs. Research rept. RS 15; ARPA Order no.
106-60; AFCRL TN-60-790; AD-244 557.
Orderfrom LCmi$4. 50, ph$l2. 30 PB 152 523
The problem of incoherent scattering in the presence
of a constant external magnetic field is analyzed. It is
found that if the radar beam is directed normal to the
magnetic field, its presence can have a profound effect
on the spectrum of scattering. It is also found that tht-
gyromagnetic frequency of the charged particles plays
an important role in the whole problem.
Institute of Mathematical Sciences, New York U. ,
N. Y.
THE SHIFT OF THE SHADOW BOUNDARY AND THE
SCATTERING CROSS SECTION OF AN OPAQUE OB-
JECT, by S. I. Rubinow and Joseph B. Keller. Rept. on
Contracts AF 19(604)5238 and Nbnr-263(30). Sep 60,
25p. 6 refs. Research rept. no. EM-162; AFCRL-
TN -60-973; AD-245 623.
Order from LC mi$2.70, ph$4.80 PB 152 842
Because of the discrepancy in the proportionality con-
stant for hard cylinders that exists between the works
of Rice and Artmann, the shift for the circular cylinder
has been redetermined and it was found that a was the
same as for the parabolic cylinder as determined by
Rice. In addition, the shift has been determined for
circular cylinders for fields which satisfy an imped-
ance boundary condition.
Lincoln Lab., Mass. Inst, of Tech., Lexington.
MILLSTONE HILL RADAR STATION: LUNAR COM-
MUNICATION TEST SUMMARY, 1959, by Paul B.
Sebring. Rept. on Contract AF 19(604)7400. 30 Sep 60,
lOp. 2 refs. Rept. no. 30G-0011; AD-244 207.
Order from LC mi$ 1 . 80, ph$ 1 . 80 PB 152 466
This report summarizes the operating parameters and
the results obtained on several UHF "moon-bounce "
voice communication trials between the Millstone Sta-
tion and other activities having large steerable anten-
nas. As predicted, most multi-path distortion prob-
lems arising from the large physical size of the moon
were minimized by the use of single side-band trans-
mission. The series culminated in the very successful
test of a voice circuit from Millstone to the 250- foot
diameter radio telescope at the Jodrell Bank Experi-
mental Station in England. A voice -to- background level
ratio of 17 db was readily obtainable with better than
telephone quality. Simultaneous recordings of the
transmitted and reflected voice signal were made at
Millstone. Transmission from Jodrell back to Millstone
was accomplished over an excellent telephone circuit
which included the transatlantic cable. (Author)
Lincoln Lab., Mass. Inst, of Tech., Lexington.
TWIUGHT REGION PROPAGATION OF SHORT
RAMO WAVES BY MODES CONTAINED IN THE
NORMAL AIR, by T. J. Carroll and R. M. Ring.
Summary technical rept. on Contract AF 19(122)458.
31 Oct 58, 210p. 73 refs. Technical rept. no. 190;
AD-210 005.
Order from LC mi$9. 30, ph$31 .80 PB 149 740
An introductory history outlines the progress of the last
decade in understanding the weak but omnipresent and
useful fields of short radio waves well beyond the
horizon as guided wave modes contained in the dielec-
tric atmosphere by partial reflection. After an intuitive
exposition of the basic idea and main results, the
equations are briefly derived for the modes contained
in a horizontally stratified dielectric atmosphere above
a perfectly reflecting curved earth. The idealized
profile of refractive index is assumed to have essen-
tially the gradient determined by gravity and the gas
laws and to be terminated in free space above the tropo-
sphere or stratosphere.
349
Microwave Reseai-ch Inst. , Polytechnic Inst, of
Brooklyn, N. Y.
ON THE ELECTR<J)MAGNEnC PROPERTIES OF
WEDGES AND CONES WITH LINEARLY VARYING
SURFACE IMFEDAJ>JCE. by Leopold B. Felaen. Rept.
on Contract AF 19(604)4143. 14 Apr 60, 91p. 24 refa.
Research rept. R -736-59. PIB-664; A FCRL-TN -60-978
Order from LC nii|5. 40, ph$15. 30 PB 153 088
The electromagnetic behavior of wedge and cone sur-
faces having a linearly varying surface impedance (ad-
mittance) 18 analyzed. The impedance (admittance)
variation is such a| to render the resulting (two dimen
slonal) boundary v4lue problems separable. Alterna-
tive representationa of the formal Green's function so-
lutions are obtained and their different utility is em-
phasized. For certain reactive ranges of surface im-
pedance, a new type of surface wave is found to exist
which can serve asia model for the study of radiation
from a tapered surface wave antenna. An application
is made to the appiiaximate analysis of the radiation
properties of a surface of finite length having a linear
reactance taper, ii^serted between a feeding surface
waveguide with con^ant reactance, and a perfectly
conducting plane wlich serves as a termination. An
analysis of the scattering properties of a wedge with a
linearly varying surface impedance is also carried out
An asymptotic (far field) evaluation of the formal solu-
tion yields a deconlposition into geometric -optical,
diffraction, and transition effects, whose dependence
on the rate of surface impedance variation is made
evident. (Author)
Motorola, Inc., Bioenix, Ariz.
ELECTROMAGNETJIC PROPAGATION STUDY, by
John H. Thess. Fi^al rept. for 1 June 57-31 Dec 59 on
Contract DA 36- 039- sc- 74841 . [1960] 58p. AD-242 302.
Order from LC miJ3. 60. ph$9. 30 PB 152 993
This study covers ine investigation of the propagauonal
and meteorological jcffects on the accuracy of terres-
trial distance measurements obtained utilizing an inte-
grated electronic distance measuring system comprisin;
two Radar Set AN/RPN- 13(XE-2) equipments . The fol-
lowing modes of propagation were investigated both
fiieoretically and experimentally: (a) multipath propaga-
tion over land and water paths; (b) ground wave trans-*
mission supponed ^y a presenution of attenuation
ilieory; (c) propagation over obstructed paths including
a hill of large radiUs-of-curvature, a knife-edged moun
tain ridge, and a heavily foliated citrus orchard: (d) prop"
pagational linrutatio|is of operation over extremely long
ranges (139 miles ),|including a method for correction o^
propagation velocity utilizing intermediate weather dat.
and the use of circular polarization to reduce local
radar type echoes; and (e) transmission through rain.
(Correction ot propagation velocity along a path using
the average refracijive index, as calculated from air
temperature, presiure, and humidity measurements,
is greatly simplified by a nomogram which is included.
A nomogram for cajlculating the knife-edge shadow loss
is also included. (Author) (See also PB 149 371)
Natlo.-ial Bureau oQ Standards, Boulder, Colo.
(QUARTERLY RAOiO NOISE DATA. JUNE, JULY,
AUGUST 1960. by W. Q. Crlchlow, R. T. Disney, and
M. A. Jenkins. 4 N<^ 60, 68p. 11 refs. Technical note
no. 18-7.
Order from OTS $1
75
PB
See alsoPB
151 377-7
151 377-6
Oxford U. «jt. Brit. ).
ELECTRO-MAGNETIC RADIATION IN ANlSOTROnC
MEDIA, by Herwig Kogelnik. Technical note no. 6 an
Contract AF 61(514)1183. June 60, 72p. 54 refs.
AFOSR-TN-60-1042; AD-244 283.
Oitier from LC mi$4. 50, ph$l2. 30 PB 152 418
This report contains a brief survey of the material
constants of anisotropic media like ionized gases,
ferrites, etc. The cotiditions are studied which the
elements of the tensor material constants of lossy (and
lossless) media have to satisfy. Plane electro-mag-
netic waves in unbounded, lossy (and lossless) aniso-
tropic media are investigated. A general method is
presented of solving radiation problems in unbounded
(not necessarily lossless) homogeneous, anisotropic
media, which involves dyadic Green's functions and
their spatial Fourier transforms (which are defined).
The method is applied to the study of the waves ex-
cited by oscillating dipoles arranged in a plane in an
anisotropic medium - and particularly in a plasma.
The power radiated by an elementary electric dipole
(Hertzian dipole) in a lossless plasma is studied in
greater detail.
Plasmadyne Coi-p. , Santa Ana. Clalif.
INVESTIGATION OF THE PRODUCTION OF MILU-
METER AND SUB- MILLIMETER ELECTROMAG-
NETIC WAVES, by Ralph W. Waniek. Final rept. for
1 July 59-30 June 60 on Contract AF 19(604)5961.
1 Aug 60, nip. 2 refs. FR080-5961: AFCRL TR-
60-185; AD- 245 497.
Order from L(::mi$6.00, i3h$18.30 PB 152 929
The broad theoretical problem studied covers the pro-
duction of radiation by the deceleration of charged
particles (bremsstrahlung) in high magnetic fields.
After an introductory section detailing the charaaer-
i sties of the bremsstrahlung, a section is devoted to
the consideration of coherence problems in which the
importance of choosing proper conditions for injecting
the particles into the field is pointed out. The re-
mainder of the theoretical section is devoted to an in-
vestigation of the particular problem of choosing the
proper injection conditions. Two sealons dealing with
the forbidden zones and trajectories are preceded and
introduced by a section in which the necessary back-
ground theory is developed from first principles.
(Author)
Sindel S. p. A. , Rome (Italy).
.MICROWAVE INVESTIGATION OF THE DIELECTRIC
WAVEGUIM; PROPAGATION BY MAGNETO- IONIC
DUCTS, by D. Formato and A. Grtardinl. Technical
summary rept. no. 1 on Contract AF 61(052)145.
10 Apr 60, 39p. 5 refs. AFCRL TN-60-98i AD- 245 928
Order from LC mi $3. 00. ph$6. 30 PB 152 963
Magneto- ionic propagation In a cylindrical plasma of
circular cross-section has been investigated theoreti-
cally and experimentally in a straight and in a curvi-
linear geometry. The microwave signal transmitted
through a plasma generated from an RF discharge in
neon has been measured as a function of the discharge
power, of the magnetic field, of the gas pressure and
of the pitch angle of the helical winding, used as a
mode- selective input. The experimental results have
350
bMn explained' by the theory of the magneto- ionic prop-
aniion in a ionized medium with a plasma frequency
larger than the signal frequency. The theoretical re-
sults and their implications on the ionospheric inteiTsrc
tation of whistler atnKtspheric behaviour are also dis-
cussed. (Author)
Washington U. fSeattle] Coll. <rf Engineering.
TIB VARIATIONAL METHOD FOR EVALUATION OF
SCATTERING OF ELECTROMAGNETIC WAVES BY
OBSTACLES. I. THEORY, by Richard B. Kieburtz,
Akira Ishimaru. and Gedalia Held. Technical rept.
no. 45 on Contract AF 19(604)4098. Aug 60, 49p.
10 refs. AFCRL TN-60-961.
Order from LC ml$3. 30, ph$7. 80 PB 152 981
This report presents a generalized variational method
for calculation of equivalent circuits and scattering
coefficients for scattering of electro- magnetic waves by
obstacles. The method in this form can be applied both
to waveguide problems and to scattering of plane elec-
tromagnetic waves by obstacles In free space. The
development given here applies directly to waveguides
and to periodic infinite arrays of identical obstacles,
but the extension to single obstacles or finite arrays is
not difficult in principle, requiring only that the Green's
function be put into a suitable form. The fundamental
limitations of the variational method are clearly defined
from this new formulation. In particular, it is shown
how the \^ariational method may be used to calculate
scattering coefficients when nnore than one propagating
mode is excited by the obstacle, and how to obtain an
equivalent circuit representation of an obstacle without
symmetry along the direction of propagation. It is
shown that it is always possible to obtain both upper and
lower bounds on a parameter calculated from a varia-
tional expression, although in certain cases, one of the
bounds may be easier to obtain than the other. (Author)
RESEARCH METHODS. TECHNIQUES
AND EQUIPMENT
Cblumbia U. School of Engineering, New York.
ON ASSURING SAFETY IN DESTRUCTIVE TESTING,
by Peter Frank. Technical rept. no. 7 on Contract
Nonr- 266(55). 6 Jan 60, 7p. AD- 231 844.
Order from LC mi$I. 80. ph$l. 80 PB 152 897
The use q^ Items which are very dangerous If defective
is considered. The following procedure for deciding
whether to use the items is considered. A surveillance
sample d size Ng is tested; If none are defective, the
items (exactly N) are used; otherwise, none are used.
Wayne State U , Detroit, Mich.
RESEARCH IN MACHINE TRANSLATION. RUSSIAN
INTO ENGLISH: MATHEMATICAL TEXT, by Harry
H. Josselson and Arvld W. Jacobson. Rept. on Contract
Nonr -2562(00). (31 July 59] 50p. AD-226 834.
Onter from LC mi$3. 30. ph$7. 80 PB 149 685
Contents:
Linguistic problems associated with machine
translation
Logical problems
The itnmedlate constituent model
The transformation model
Computer considerations
Analysis of multiple meaning in mathematical text
Preparation of text for automatic data processing
information Theory
Lincoln Lab. . Mass . Inst, of Tech. . Lexington.
CONCEPTS OF AUTOMATIC DATA STORAGE AND
RETRIEVAL IN THE SIMPLEX SYSTEM. byC. W.
Uskavitch. Rept. on Contract AF 19(604)7400.
17 Oct 60, 67p. 12 refs . 22G-0053; AD-245 472.
Order from LC mi$3.90. ph$10.80 PB 152 78"'
Five guiding principles are inherent in the idea of a
Simplex system for the Field Army: (1) the system
should be independent of organizational structure; (2) it
must handle large quantities of information with mini-
mum delays; (3) it should provide service to as many
units as possible; (4) it must be easily modified; and
(5) the system must fulfill the operational requirements
of the Field Army. From these principles are derived
the more concrete, but general, concepts required for
design of the data storage and retrieval system. These
concepts include such ideas as minimum human inter-
vention, maximum utilization of all equipments . nxxlu-
lar construction, a common code for all information,
and special-purpose devices for such functions as error
correction and security coding. Although these concepts
are sufficient to provide a general conception of the sys-
tem, they are not detailed enough to show that imple-
mentation is feasible and, if feasible, which particular
implementation is best. Therefore, a set of "black
boxes" are postulated to provide an initial design of an
apparently feasible storage and retrieval system. Each
box is defined functionally in detail, and a possible im-
plementation technique is indicated . This design is not
proposed for implementation but has been derived as a
first step in the design process . By suitable study of
this initial design, seeking deficiencies and making im-
provements , a final design may hopefully be refined
which will provide the best system for the Field Army.
(Author)
t
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
ERROR STATISTICS ON DUAL DATA CIRCUITS
FROM KINGSTON, NEW YORK TO CAPE CANAV-
ERAL. FLORIDA, by E. J. Hofmann. Rept. on Con-
tract AF 19(604)7400. 20 Oct 60, 38p. 7 refs.
25G-0006; AD-245 991.
Order from LC mi$3. 00, ph$6. 30 PB 152 933
Both bit error rates and word error rates are shown,
and their temporal and amplitude characteristics are
examined. It is shown that dlgiul errors are of a burst
nature, both within a word and over many words. Dis-
tributions are given for the number erf bits in error in
a word error, duration of bursts, and the probability
of continuous error and error-free periods. Conver-
sion probabilities from mark to space and space to
mark are given. The effectiveness of simple parity as
an error -checking device is also evaluated. (Audxsr)
351
Phonographic Equipment
Army Signal Research and Development Lab. , Fon
Monmouth, N.J.
DARKROOM, PHOTpCRAPHIC, PORTABLE ES-29
(XE-3) by P. TownsJend. 14 July 60. 31p. USASRDL
Test rept. 1459, siipplement no. 1.
Order from LC mi$B.OO, ph$6.30 PB 152 564
Darkroom. Photogriphic , Portable ES-29 (XE-3).
formerly ES-29 (XH-1), which was modified and in-
stalled In a new shelter, has been subjected to a com-
plete series of acceptance tests and has been found
satisfactory for release for service tests . (Author)
Army Signal Research and Developntent Lab. .
Fort Monmouth, N.J.
EVALUATION OF ^OMM CONTINUOUS LAND PROC-
ESSOR, by L. D. doldfarb. 2 May 60, 20p.
USASRDL Test rep«j. 1479.
Order from LC miS2.40, ph$3.30 PB 152 565
The 70mm Continuojs Land Processor is a portable
film processing unij capable of rapid processing ex-
posed 70mm negatives from the cassette used in
Camera iCE-4 and piroducing either positive paper
prints or positive tiansparencies at a rate of two to
six feet per minute < Testing of the processor is dis-
cussed. In general the processor is in accordance
witii the Technical Kequi rements . (Author)
PHOJECTION SYS
CONDITIONS, by
USASRDL Test re
Order from LC mi
Army Signal Reseiirch and Development Lab. , Fori
Monmouth, N. J.
:M for high AMBIENT LIGHT
eter P. Paris. 25 June 59, 12p.
1473; AD- 220 673..
:. 40, ph*3. 30 PB 152 997
A projection systeni was tested which permits projec-
tion under high amlient light conditions. The system
is designed so that the screen reflects the ambient
light onto a mat abiiirbing surface thus preventing it
irom reaching the eNes of audience. The test showed
that with an added illumination of 200 footlamberts the
contrast of a projecied slide dropped only from I2:l^to
5:1. (Author) j
ITT Labs., Fort Wayne. Ind.
HIGH-SPEED IMAGE SHUTTER UNIT, by Louis F.
Mayle. Rept. on R^arch on Particle Dynamics, Con-
traa AF 33(616)614 J. Apr 60, 62p. ITT rept.
aerial 3029; WADD JTechoical rept. 60-216;
AD- 239 486.
Order from OTS $lJ75 PB 171 197
The description, theory, and operating procedure for
the High-Speed Image Shutter Unit are given. With this
equipment up to 12 pictures of a self -illuminating event
(i.e. an exploding wire or arc) may be taken sequen-
tially at extJ-emely fast exposures with no intervening
time between pictures. Pulsed image tabes are em-
ployed as electronic shutters. Timing accuracy, reso-
lution, and light sensivity are considered, and calcula-
tions are presented. Included are schematic and
wiring diagrams of the equipment, drawings for fabri-
cating the image tube housing and 5 photographs.
(Author)
MISCELLANEOUS
Naval Research Lab. , Washington, D. C
REPORT OF NRL PROGRESS. Feb 61.
Order from OTS $1.25, $10.00/year PB 171 315
Contents:
Articles:
The Determination of Gases in Metals, by G- A.
Picklo, Jr.
Structure of Vacuum -Deposited Gernuinium Films on
Amorphous Quartz, by J. E. Davey
Tropospheric Burdens of Gross Fission Products, by
L. B. Lockhart, Jr.
Scientific program:
Chemistry: Fnotodegradation of poly-«-methyl8tyrene
by near ultraviolet light in vacuum at 27*'C and
115°C. Characteristic functions and parameters in
the theory of hydrogen overpotential
Mechanics: Interpreting lower yield point plastic flow
in dynamic testing of mild steel. Beam deflection
problems solved by use of the loading diagram
Metallurgy and Ceramics: Refined optical techni'jue
and apparatus for high-temperature strain measure-
ments. Effect of hydrogen absorption and desorption
on the ultrasonic velocities and hardness of palla-
dium. Temperature dependence of the surface ten-
sions of liquid metals. Effect of interference ele-
meius on the determination of ferrous iron in iroo
compounds
Nuclear and Atomic Physics: Penetration of electro-
magnetic waves into ionized gases
Solid -State Physics: Mylar film dosimetry. Minia-
turized thermoluminescent dosimeter. Effect at
pressure on F -center luminescence
Souik): Comparison of deep sea velocity meter with
Nansen bottle operations during 1960
Supporting Techniques: A Beta Calculator for Graphic
Displays
352
ATOMIC ENERGY COMMISSION REPORTS
Reports may be purchased in accordance with instructions on the Inside front cover of the U S
GOVERNMENT RESEAJICH REPOR-re. As PB numbers are not indicated, order by series and number.
Tbese reports may also be consulted at any AEC Depository Library. A list of these libraries may be
obuined from the U. S. Department of Commerce, Office of Technical Services, Washington 25, D. C.
Reproduction in whole or part of any report listed herein is encouraged by the U. S. Atomic Energy*
Commission, subject to the approval of authors or originating sites. Genera J inquiries from the indus-
trial press about AEC-developed information should be directed to the Industrial Information Branch,
Atomic Energy Commission, Washington 25. D. C.
*I
Biolog)< and Medicine
Plftfa annual meeting at the bio-assay and analytical
chemistry groupr Gatlinburg, Tennessee from
October 1-2 1^59, by K. Z. Morgan and others.
Oak Ridge Nati nal Laboratory, Health Physics
Division. Oak Ridge, Tenn. Nov 60. 106p.
Order from OTS. $2.25. TID-7591 5^
The oriyn of life on earth and elsewhere. II, by
M. Calvin. University of California, Lawrence
Radiation Laboratory, Berkeley, Calif. Oct 60.
Contract W-7405-eng-48. 41p. Order from
OTS. $1.00. UCRL-9440
Chemistry
Uranium hexafluoride isotopic measurements using
an interpolative method, by G. F. Kauffman and
N. F. Cnristc^her. Goodyear Atomic Corpora-
tion. Portsmouth, Ohio. Nov 60. Contract AT-
(33-2)-l. 15p. Order from OTS. 50 cents.
GAT- 291
TTie chemistry, purification and metallurgy of
Plutonium, by C. A. Thomas and others. Metal-
lurgical Caboratory, Chicago University,
Chicago, 111. Dec 44. Decl. March 1, 1960.
S39p. Report consists of two books. Order
from OTS. Total price $5, 50.
MUC-JCW-223 (Book 1 & 2)
Crlttcal constants of dlphenyl and the terphenyls, by
H. Mandel and N. Ewbank. Atomics Internation-
al. A Division of North American Aviation, Inc. ,
Canoga Park. Calif, Dec 60. Contract AT(11-1)-
GEN-8. 33p. Order from 0T3. $1.00.
NAA-SR-5129
35.''
Lithium and lithium hydride chemical and physical
roperties. A literature search, hy T. P'. Davis.
ice of Technical Information Extension, Oak
Ridge, Tenn. Nov 60. 26p. Order from OTS
50 cents. TID-3558
NonequlUbrium thermodynamic theory for concen-
tratlon profiles in liquid extraction, by A. Hen-
nico ana T. Vermeulen. University of California.
Lawrence Radiation Laboratory, Berkeley, Calif.
Sep 60. Contract W-7405-eng-48. 56p. Order
from OTS. $1,25. UCRL-9415
Analytical methods in the beryllium program, by
J. M. Googin. Union Carbide Nuclear Company,
Division of Union Carbide Corporation, Y-12
Plant, Oak Ridge, Tenn. Dec 60. Contract
W-7405-eng-26. 12p. Order from OTS.
50 cents. Y-1324
Beryllium chip processing, by Z. L. Ardary and
others. Lmion Carbide Nuclear Company,
Division of Union Carbide Corporation, Y-12
Plant, OaV Ridge, Tenn. Dec 60. 44p. Order
from OTS. $1.00. Y-1328
Chemical Separations Processes for
Plutonium and Uranium
Salt-phase chlorination of reactor fuels. II. ARCO
process definition and scoping studies, by E.iA7
Vander Wall and others . Phillips Petroleum Co.
Atomic Energy Division, Idaho Falls, Idaho.
Oct 60. Contract AT(1 0-1)- 205. 43p. Order
from OTS. $1.00. * IDO-14525
Reprocessing of thorium -uranium fuels by liquid
metal extraction, by R. E. Johnson and l.D.
Chilton. Atomics International. A Division of
Nortfi American Aviation, Inc. , Canoga Park,
Calif. Dec 60. Contract AT(ll-l)-CTN-8. 19p.
Order from OTS. 50 cents. NAA-SR-5506
Controlled thermonuclear Processes
Stability of a diffuse hoi low -core toroidal pinch, by
B. R. Suydam. The University of California.
Loa Alamoe Scientific Laboratory, Los Alamos,
N. Mex. Oct 6<!). Contract W-7405-ENG-36.
17p. Order froin OTS. 50 cents.
LAMS-2477
Controlled thermoAuclear processes. A literature
search, by R. U Scott and S. F. LameTT Office
oi Tecimical Infbrmation Extension, Oak Ridge,
Tsnn. Nov 60. I04p. Order from OTS. ^2. 25.
TID-3557
Engineiering and Equipment
Thermoelectric rejfrigerator for the line recorder
mass spectrometer (llieoretical design), by"
P. L Davis. Goodyear Atomic Corpora tinn,
Portsmouth. Ohio. Nov 60. Contract AT(33-2)-
1. 24p. Order, from OTS. 50 cents.
GAT- 365
Health and Safety
Shock tube sttidies at the effects of sharp- rising,
long-duration overpressures on biolojg^cal sys-
tenM. Progress report, by D. R. Ridunona
and others. The Lovelace Foundation for Medi-
cal Education asd Research, Albuquerque,
N. Mex. Mar 99. Contract AT(29-1)- 1242.
30p. Order frotn OTS. 75 cents. TID-6056
Sixgi AEC air cleaning conference, July 7-9^ 1959
July 7-9.
jry Commi
Sponsored by Uj S. Atomic Energy Commission,
Division of Realtor Development, Washinton,
D. C. and Harvard Air Cleaning Laboratory, and
Health and Safety Division. Idaho Operations
Office. Idaho Falls, Idaho. 1959. 388p. Order
from OTS. $4.00. TID-7593
Further contributions on gross beta radioactivity
of biolo^cal and reUt^ samples at the Eniwetok
Proyjng Ground,^ 1952-1958, by k. Bonham"
University of Wfishington. Laboratory erf Radla-
dan Biology. Seattle, Wash. Dec 59. Contract
AT(45-l)-540. 41p. Order from OTS. $1.25.
UWFL-63
Instruments
Pressure and temperature instrumentation for dy-
namic measurements in the KEWB program. A
summary report, by S. P. Harris andC. F.
Bumpus, Jr. Atomics International. A DivisloB
of North American Aviation, Inc. , Canoga Park,
Calif. Nov 60. Contract AT(Il-l)-GEN -8.
77p. Order from OTS. $2.00. NAA-SR-4709
Design and construction of a unit for measuring
metal skin temperatures. Riasel: Theoretical
analysis and design for Sandia Corporation.
work performed from Fearviary 1956
ourii April I? ~
tion, Re^rch Department, Redwood City, Calif.
Coverin
Hi?
55^ Detroit Controls Corpora-
Dec 60. 47p. Order from OTS.
$1.50.
SC-4461(RR)
Interim report on development of design criteria
for relays. This report covers the period 1"
Febnjary to 31 March 1960. Oklahoma State
University, School of Electrical Engineering,
Stillwater, Okla. Oct 60. 66p. Order from
0T5. $1.75, SC-4466(RR)
Bibliography on semiconductor nuclear radiation
detectors, by J. L. Blankenship. Oak Ridge
National Laboratory, Instrumentation and
Controls Division, Oak Ridge, Tenn. Dec 60.
j 14p. Order from OTS. 50 cents. TID-3907
Isotopes — Industrial Technology
The technology and applications of large flssioo
product beta sources^ Radiation Applications
Inc. , New York, N. V. [1959?] 38p. Order
from LC. Mi $3. 00, ph $6. 30. NYO-2500
Study of the Industrial potential of radioisotopic
methods in the textile industry, April 1959 -"
'une I960, by L. Rebenfeld and H. J. White, Jr.
1^
'extlle Research Institite, Princeton, N. J.
July 60. Contract AT(30-l)-2365. 26p. Order
from OTS. 50 ccntsi NYO-2640
The development of a beta-ray particle size analy-
zer. April 1959 - Miy I960, by S. Z. Lewin
and odiers. Evans Research and Development
Corporation, New York, N. Y. Oct 60. Con-
tract AT(30-l)-2372. 42p. Order from OTS.
$1.25. NYO-2655
354
Potential applications of radioisotopes to the mining
Pittsburgh, Pa. Nov 60. Contract AT(30-1)-
2311. 233p. Order f ran OTS. $3.00.
( I NYO-2859
Tbt technology and applications of large fission
product beta sources Quarterly reportlor~
period ending March 31, I960. Radiation Ap-
plications Inc. , New York, N. Y. 1960. Con-
tract AT(30-1)-2186. 16p. Order from LC.
Ml $2. 40. ph $3. 30. TID-5869
111. Apr 60. Contract AT(ll-l)-712.
Order from LC. Ml $2. 40. ph $3. 30.
12p.
TID-5905
Ite applications of isotopes to industrial problems.
Progress report no. 14 for April 16 to May 16.
I960. byF. y. Rleke. University of Hilrign
Chicago Mktway Laboratories, Chicago, 111.
May 60. Contract AT(ll-l)-712. 17p. Order
fromLC. Mi $2.40. ph $3. 30. TID-5969
Isotopic ntethod for age determinations of industrial
products- Monthly progress letter for AprTT
1960, T. C. GregsonandL. B. Hangw r.nnti.
fsar Tire and Rubber Co. , Akron. Ohio. I960.
Contract AT(1 1 -1)-719. 3p. Order from LC.
Mi $1.80, ph$1.80. TID-6060
Study of the industrial potential of radioisotopic
medKxls in the synthetic detergent and soaFin
auBOT. Final report March 1 to November V
1959, by C. W. 5tanely. Office ol Isotopes
Development. U. S. AtonUc Energy Commission,
Washington 25, D. C. 1959. Contract AT(40-1)-
2514. 52p. Order from OTS. $1.25.
TID-6088
Gamma y aping in chemical plant instrumentation.
hyj. A. Williamson and F. M. Teetzel. Nation-
sl Lead Co. of Ohio, Cincinnati, Ohio. July 58.
30p. Order frotn LC. Mi $2. 70, ph $4. 80.
TID-6109
i
Rsdioisotope experiments for the chemistry currl-
Oiilum, by A. G. Schrodt and odhera Vfurl«.ar
Oiicago Corporation, Chicago, 111. Aug 60.
Contract AT(ll-l)-738. 162p. Order from OTS.
$2.00. TID-6374
Radioisotope ejqwrlments for the chemistry curri-
culum. Instructor notes. Nuclear-Chicago,
■ Corporation, Chicago, 111. Aug 60. Contract
AT(ll-l)-738. 60p. Order from OTS. $1.00.
TlD-6375
Industrial applicability of low level counting,. .<»».-
M. A. Greenfield and R. L Koontz. eVh.
Plesset Associates, Inc. , Los Angeles, Calif.
June 59. Contract AT(49-2)-1372. 54p. Order
from OTS. $1.50. WASH-1020
Metals, Ceramics, and Materials
Heat transfer fluids for fuel element cane, by L.
brewer. General Atomic Division, General
Dynamics Corporation, San Diego, Calif. Aug
59. Contract AT( 04-3)-314. 4p. Order from
LC. Mi $1.80, ph$1.80. AECU-4537
Corrosion of Inor-8 and Inconel dlssolver compo-
nents of the fluoride -volatility process, by F. W.
Fink. Battelle Memorial Institute, Columbus,
Ohio. Dec 59. 50p. Order from LC.
Ml $3.30. ph $7.80. AECU-4633
Study of factors Influencing ductility of iron
aluminum allov '
Monthly letter report no. 10
March 1 5, '1959 to 'iS£^
C. Perkins andj
!arch 1!
Nachman.
covering peri
I960, by P. C
University of Denver. Denver Research Insti-
tute, Denver, Colo. Feb 60. Contract AT-
(lH)-742. 4p. Order fromLC. Ml $1.80,
I*$l-80. AECU-4698
Low cycle fatigue of pressure vessel materials,
interim Teduilcal report no. 5, by G. Sachs
and others. Syracuse University, Metallurgical
Research Laboratories, New York, N. Y. Jan 60.
Contract AT(30-1)-2141. 47p. O rder from
LC. Ml $3.30. ph $7.80. AECU-4728
Studies of corroeion by molten zinc and cadmium
systems, byj. P. DeKany and others. Argonn
Nstional Laboratory, Argonne, 111. Oct 60.
Contract W-31-109-eng-38.
OTS. $1.00.
44p.
Order from
ANL-6243
Specifications and fabrication procedures for SM-
lA core U stationary fuel elements. Alco Prod-
ucts, Inc. , Schenectady, N. Y. May 60. Con-
tract AT(30-3)-326. 91p. Order from LC.
Ml $5. 40, ph $15. 30. APAE -Memo- 258
355
Fundamental alloy development suidles. Qyrterly
progress report no. 8 for August 1, 19y7-Octo-
ber^l, 1957, l|y C. E. Lundin and D. T. Klodt.
University of Efenver. Denver Research Insti-
tute, Denver, Colo. Nov 57. Decl. with dele-
tions November 4, 1959. 34p. Order from LC.
Mi ^3. 00. ph$6.30. AFEX-349<Del.)
Progress report no. 2 for
8, S R. -^ '
Phase diagram studies
April r- June yijSa ^T^T
Illinois Institute of Technology, Armour Re
F. Domagala.
search Foundation, Chicago. 111. July 58. Decl.
June 11, 1958. Contracts AF33(600)- 38062 and
AT(11-1)-171. 15p. Order from LC. Mi $2.40,
ph $3. 30. ' AFEX-420
Development of mttallic uranium fuel elements of
improved irradiation stability. Semiannual prog-
ress report no.' L Advanced Technology Labor-
atories. Division of American-Standard, Moun-
tain View, Calii. Dec 59. Contract AT(04-3)-
250. 45p. Or<Jer from LC. Mi $3. 30, ph $7 . 80.
ATL-A-104
Mechanical prcyerties of zirconium and zirconium-
uranium alloys containing tin, by A. D. Schwope
and others. Baltelle Memorial Institute, Colum-
bus, Clio. Sep 52. Decl. November 20, 1959.
Contract W-74(K-eng-92. 18p. Order from LC.
Mi $2.40. ph $).30. BMl-770
Ursnium migrattos in VO^-bearing cexainlcs. J.F.
ma others. Battelle Memorial Institute,
Quirk ar
Columbus, Otiq. Sep 53. Decl.
1960. Contract W-7405-Eng-92.
fromLC. Mi t2.70. ph $4.80.
T
February 16.
3(^. Order
BMI-862
Centrifugal casting of aluminum-uranium alloys,
by N. E. Daniel and others. Battelle Memorial
Institute, Columbus, Ohio. July 59. Decl.
February 8, I9p0. Contract W-7405-eng-92.
24p. Order frc^ LC. Mi $2.70, ph $4.80.
BMI-1363
Progress relating to civilian applications during
mly, 1960, by^. W. Dayton and C. R. Tipton
Jr. Battelle Mamorial Institute, Columbus,
Ohio. Aug 60. Contract W-7405-eng-92. 79p.
Order from Ort. $2.00. BMI-1455
Progress relating to civilian applications during
August, 1960, l»y R. W. Da>aon and C. R. Tip-
ton" Jr. Battelle Memorial Institute, Columbus,
Ohio. Sep 60. Contract W-7405-eng-92. 75p.
Order from OTS. $2.00. eMI-1464
OlS. $2.
Progress on the use of gas -pressure bonding for
fabricating low |coat ceramic, cermet.
fuel-cycle program, by S. J. Paprocki and othen.
Battelle Memorial Institute, Columbus, Ohio.
Nov 60. Contract W-7405-eng-92. 92p. Order
fromOT5. $2.00. BMl-1475
Analysis of the amount of preferred orientation by
x-ray diffraction line intensities, by D. A.
Vaupian^ Battelle Memorial Institute, Columbus,
Ohio. June 60. Contract W-7405-eng-92. Up.
Order from LC. Mi $2. 40, ph $3. 30.
BMI-X-156
Beryllium, by M. J. Whitman. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Mar 57. Decl.
August 14, 1959. Contract W-7405-eng-26.
25p. Order from LC. Mi $2.70, ph $4.80.
CF- 57 -3-92
Survey of anodizing processes for aluminum, by
H. L. Hols<^ple, Jr. Oak ^idge National Labor-
atory, Oak Ridge, Tenn. Aug 59. Contract
W-7405-eng-26. 9p. Order from LC. Mi $1. 8a
ph$l.80. CF-59-8-132
Temperature structure in the mic^lane spacer for
ECCR fuel rod, by L. G. EpeUnd J.K.T. Jung-
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Jan 60. 8p. Order from LC. Mi $1.80,
ph$1.80. CF-60-1-2
5-GFM in-plle thorium oixide slurry locydevelop-
ment, runs 14 through 16 in loop L-4-24S, and
filtration of thorium oxide slurry with sintered
filters, by J. M. Baker and others. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Mar 60.
21p. Order from LC. Mi $2. 40, ph $3. 30.
CF-60-3-39
Some renaarks on the contrlbutlcn of fissloo-prod-
uct cesium to the pressure buildup in UO9 fuer
elements, by M. W. Rosenthal and S. Cantor.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Mar 60. 9p. Order from LC.
Mi $1.80, ph$1.80. CF-60-3-81
Corrosion protection of stainless stgel piping by
titanium Inserts: Examination of titanium in-
serts, removed from lo<x) N after run N- 24,
by R. S. Greeley. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. Mar 60. 6p. Order
fromLC. Mi $1.80, ph $1.80. CF-60-3-156
Some experinnents on the accuracy of thoria slurry
samples, by R. P. Wichner. Oak Ridge Nation-
al Laboratory, Oak Ridge, Tenn. Apr 60. Coo-
tract W-7405-eng-26. 24p. Order from LC.
Mi $2.70, ph$4.80. CF-60-4-93
and dispersion uels. Phase 11 report on AEC
356
Corrosion in the Oak Ridge Research reactor core-
cooling system, by P.O. Neumann. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Apr 60.
17p. Order from LC. Mi $2. 40, ph $3. 30.
CF -60-4-97
Cladding survey for the enrico fermi reactor U-15
Wt. % Mo base diapers ion -type fuel element, 6y
M. M. Martin and R. J. Beaver. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Apr 60.
39p. Order fromLC. Mi $3.00, ph $6. 30.
CF-60-4-118
Examination of corrosion specimens from slurry
blanket mockup runs SM-6 through SM-9, by
R. B. Gallaher and others. OakRidge National
Laboratory, Oak Ridge, Tenn. May 60. Con-
tract W -7405 -eng- 26. 12p. Order fromLC.
Ml $2. 40. ph$3.30. CF-60-5-137
Relative effectiveness of decontamination of various
gtainless steel surface finishes, by E. E. Pierce.
Oak Ridge National Laboratory, Oak Ridge, Tenn.
Contract W-7405-eng-26.' 12p. Order from
LC. Mi $2. 40, ph $3. 30. CF-60-6-54
Vacuum casting of aluminiihi- silicon coating on
tuballoy [uranium]. Pinal report on a part of
P. A. no 3y-Mi:-54-S,"p S. 17. byb. IT
Schwa ru and L. Kurland. University of Chicago,
MeuUurgical Laboratory, Chicago, 111. Mar 45.
Decl. January 29, 1960. Contract W-7405-eng-
37. 27p. Order fromLC. Ml $2.70, ph $4.80.
CT-2751
Corrosion of construction materials, bonding mate -
rials, and uranium- -an electrochemical irivestl-
ition, by R. B. Hoxeng. University of Chicago,
sullurgical Laboratory, Chicago, 111. May 45.
Decl. January 28, 1960. Contract W-7405-eng-
37. 70p. Order frcMn LC. Mi $3.90, ph $10.80.
CT-3023
Corrosion of unbonded aluminum -jacketed slugs in
aqueous medium. Report on a phase of pr(5?lern
no. 391-ML-53-4: File serial no 22, t^ G. C.
English and others. University of Chicago,
MeuUurgical Laboratory, Chicago, 111. Jan 45.
Decl. January 30, 1945. Contract W-7405-eng-
37. 15p. Order from LC. Mi $2. 40, ph $3. 30.
CT-3047
Fabrication at uranium oxide fuel elements, by G.
R. Cole and others. E. I. du Pont de Nemours
It Co. Explosives Department, Atomic Energy
Division, Technical Division, Savannah River,
Laboratory, Aiken, S. C. Dec 59. Contract
AT(07-2)-l. 36p. Order from OTS. $1.00.
DP-430
Aqueous corroslOTi of aluminum at 260°C, by
V. Whatley. E. I. du Pont de Nemours 81 Co.
Explosives Department, Atomic Energy Division,
Technical Division, Savannah River Laboratory,
Aiken, S. C. Oct 60. Contract AT(07- 2)- 1.
12p. Order from OTS. 50 cents. EH»-521
The noble gas permeability characteristics of
graphite materials for use in gas-cooled reac-
tors, by A. B. Riedinger and L R. Zumwalt.
General Atomic Division, General Dynamics
Corp. , San Diego, Calif. Apr 60. Contract
^ AT(04-3)-314. 24p. Order from LC. Mi $2.70,
ph$4.80. GA-1361
Effect of environment on the creep- rupture proper-
ties of Inconel 71 3C, by J. C. BrcJcros. General
Dynamics Corporation, San Diego, Calif.
Oct 60. Contract AT(04-3)-187. 17p. Order
from OTS. 75 cents. GA-1629
Induction heated vacuum hot press, by E. W. Hoyt.
Vallecitos Atomic Laboratofyy Atomic Power
Equipment Department, General Electric Com-
pany, Pleasanton, Calif. Mar 60. Contract
AT(04-3)-189. 7p. Order from OTS. 50 cents.
GEAP-3331
A survey of new cadmium materials for possible
reactor application, by S. Siegel. Vallecitos
Atomic Labors toryT Atomic Power Equipment
Department, General Electric Company.
Pleasanton, Calif. Apr 60. Contract AT(04- 3)-
189. 19p. Order from OTS. 50 cents.
GEAP-3395
Fission gases, their measurement and evaluation,
by T. J. Slosek and B. Weidenbaum. Vallecitos
Atomic Laboratory, Atomic Power Equiptnent
Department, General Electric Qxnpany,
Pleasanton, Calif. Aug 60. Contract AT(04-3)-
189. 15p. Order fnwn OTS. 50 cents.
GEAP-3440(Rev.)
Short time corrosion tests of bronze, mild steel,
T-304 stainless steel and 2S aluminum in 10%
potassium tetraborate solution, by Y. B. Katay-
ama. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Dec 51. Decl. January 4, 1960. 4p. Order
fromLC. Mi $1.80, ph $1.80. HW-23022
Elimination of the cold outgassing period for the
casting qjeration. Final report, by R. A.
Carlson. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Jan 52. Decl. March 15, 1960. Contract W-
31-109-Eng-52. 7p. Order from LC. Mi $1.80,
ph$1.80. HW-23473
357
The formarion of ahemlcal film depoeits on alumin-
um surfaces, oy R. V. Andrews. General Elec-
tric Con^xuiy, Hanford Atomic Products Opera-
tioo, Richland, Wash. Feb 52. 199p. Order
from LC. Mi tS. 70, pb $30. 30.
HW- 23494 (Del.)
Preliminary report on the ultrasonic properties of
uranium, by D^ C. Worlton and E. c" Wood.
Hanford Works, Richland. Wash. Oct 52. Decl.
E)ecember 3, 1959, Contract W-31-I09-Eng-52.
31p. Order from LC. Mi %2. 70, ph M- 80.
HW-26CC3
Briquetting of madhined plutonium turnings for re-
cycle to the catting operation. Pinal report--
A study of die fabrication failures for zircooium
production test' 235- 6, by B. C. Chandler. Gen-
eral Electric do. FSnford Atomic Products Oper-
ation, Richlanc^, Wash. Nov 52. Decl. March
15, 1960. Contract W-31-109-Bng-52. lOp.
Order from LX!. Mi $1.80. ph $1.80.
HW-26141
Removal of graphiite f rom alinninum surfaces, by
R. L. DiUoaaidW. H. Hodgson. General
Electric Company, ^nford Atomic Products
Operation, Richland, Wash. jMne 53. Decl.
January 28. 19^. 4p. Order from LC.
Mi $1.80, ph $1.80. HW-28507
Some egectfl of scriations on slug quality, by R. L.
Knecht and J. W. Goffard. General Electric Co.
Hanford Atomic Products Operation, Richland,
Wash. Apr 54. Decl. January 29, 1960. Con-
tract W -31- 109-Eng-52. 8p. Order from LC.
Mi $1.80. ph $1.30. HW-31676
The gas contained in slug bond layer and blisters,
by F. A. Scott and H. J. Anderson. General
Electric Company, Hanford Atmnic Producu
Operation, Richland, Wash. June 54. Decl.
January 29, 19^0. Contract W-31-109-Eng-52.
4p. Order froai LC. Mi $1.80. ph $1.80.
HW-32156
The removal of nltkel from uranium, by R. L. D
Dillon. General Electric Company, Hanford
Atomic Producs Operation, Richland, Wash.
June 54. Decl. January 28, 1960. Contraa
W-31-109-Eng-!52. 5p. Order from LC.
Mi $1.80, ph$i.80. HW-32309
Hot press canning of thorium, by C. H. Blooms cer
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Mar 55.
Decl. March lj6, 1960. Contract W-31- 109-
Eng-52. 8p. 0rder from LC. Mi $1.80,
ph$1.80. HW-36169
Products Operation, Richland, Wash. May 55.
Decl. March 16, 1960. 28p. Order from LC.
Ml $2.70. ph $4.80. HW-36763
Flow stress recovery erf Zircaloy-2, by D. E.
Johnson. General Electric Company, Hanford
Atomic Products Operation, Richland. Wash.
Dec 55. Decl. January 8. 1960. 18p. Order
from LC. Ml $2.40, ph $3.30. HW-40312
Crystallite sizes (rfPu02 powders, by P. G. Pall-
mer. General Electric Company. Hanford
Atomic Products Operation, Richland, Wash.
July 56. Decl. March 7, 1960. Contract W-31-
109-Eng-52. 5p. Order frcrni LC. Mi $1.80,
ph$1.80. HW-44585
Recording surface coixtLtlon by replication, byJ.R.
Morgan. General Electric Company, "Ranford
Atomic Products Operation, Richland. Waah.
Jan 57. Decl. March 28, 1960. Contract W-
31-109-Bng-52. 21p. Order from LC.
Mi $2.40, ph$3.30. HW-48052
Design completion report; interlocking CCTitour
tooling system, by J. W. Nickolaus. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Oct 57. 9p. Order
from LC. Ml $2.40, ph $3.30. HW-53351
Post CCTiyletloo report--fuel ent^neerlng pilot plant
semlworks- -306 building, by S. M. Gill. Gener-
al Electric Company, Hanford Atomic Products
Operation. Richland. Wash. Nov 57. Contract
AT(45-1)-1350. 8p. Order from LC. Mi $1.80,
ph$1.80. HW-53616
Ceramic coatings on uranium, by D. W. Shannon.
General Electric Company, Hanford Atomic
Products Operation. Richland. Wash. Jan 58.
Decl. June 2. 1959. Contract W-31 -109- Eng- 52.
26p. Order from LC. Mi $2.70, ph $4.80.
HW-53666
Variable hydr
~-T5
~W.
lydrogen dingot test, by R. E. Olson and
Rathbun. General Electric Company.
Hanford Atomic Products Operation, Richland,
Wash. June 58. Decl. March 31. 1960. Con-
tract W-31-109-Eng-52. 17p. Order from LC.
Ml $2.40. ph$3.30. HW- 56391
Results of NaK capsule failures in hot water flow
tube, by J. W. Weber. ' General Electric Com-
pany. Hanford Atomic Products Operation,
358
RlchUnd, Wash. Sep 58. Contract AT(45-1)-
1350. 3p. Order from LC. Mi $1.80, ph $1.80.
HW-56588
Plutonium fuels development, plutonium metallurgy
operation quarterly report- -January, February.
March 195g by 0.' J. Wick. General Electric
Company, "Ranford Atomic Products Operation,
Richland, Wash. Sep 58. Contract W-31- 109-
Bng-52. 25p. Order from LC. Mi $2.70,
|il»$4.80. HW-57343
Alternate sieve plate materials for the "Zebra"
cartridge, by W. R. Hamilton and I. H. Klein
peter. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Dec 58. 6p. Order from LC. Ml $1.80,
I*$1.80. HW-58311
Plutonium fuels development, plutonium metallurgy
operation quarterly report- -July, August, Sep-
tember 195S by 0. I. Wick. 6enera[ Electric
Company. Hanford Atomic Products Operation,
Richland, Wash. Feb 59. Contract W-31 -109-
Eng-52. 26p. Order from LC. Ml $2.70,
ph$4.80. HW-59365
Partland cement grout vapor pressure- -temperature
test, by H. W7 Stivers. General Electric Com-
psny, Hanford Atomic Products Operation, Rich-
land, Wash. June 59. 12p. Order from LC.
Mi $2. 40, ph$3.30. HW-60556
Plutonium fuels development, plutonium metallurgy
operation quarterly report- -October, November,
gecember 1956 by 0. J. Wick. General Elec-
tric Conpany, Hanford Atomic Products Opera-
tion, Richland, Wash. Aug 59. Contract AT-
(45-l)-1350. 28p. Order from LC. Mi $2.70,
i*$4.80. HW-60996
Heat transfer testing, by D. R. Doman and others.
General Electric Company. Hanford Atwnic
Products Operation, Richland, Wash. July 59.
Contract AT(45-1)-1350. 7p. Order from LC.
Mi $1.80, ph$1.80. HW-60998
Specifications for requisition G-385923--Zircaloy-
4 fuel jacket tubing, by H. P. Oakes. General
Electric Company7 Hanford Atomic Products
Operation, Richland. Wash. Nov 59. Contract
AT(45-1)-1350. 6p. Order from LC. Mi$1.80,
I*$1.80. HW-61329
Evaluadion of fretting oorrosion of ZR-2, by R. J.
Lobslnger. General Electric Ccmpany, Hanford
Atomic Products Operation, Richland, Wash.
Feb 60. Contract AT(45-1)-1350. lOp. Order
fromLC. Mi $1.80, ph $1.80. HW-61915
Plutonium fuels development, plutonium metallurgy
operation quarterly report for January, February.
March 19W, by 0. J. Wick, dneraf Electric
Company, Hanford Atomic Products Operation,
Richland, Wash. 1959. Contract AT(45-1)- 1350
41p. Order fromLC. Mi $3.30, ph $7.80.
HW-61994
Preliminary Investigation of the transforniation rates
of plutonium- -uranlinn *lloya, by R. D. Nelson
ana J. M. Taylor. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Jan 60. Contract AT(45-1)- 1350, 19p.
Order from LC. Mi $2. 40, ph $3. 30.
HW-62073
Crackijig of irradiated uranium by rapid cooling, by
K. K. Merckx. General Electric Company^
Hanford Atomic Products Operation, Richland,
Wash. Oct 59. DecL February 3, 1960. Con-
tract AT(45-1)- 1350. lip. Order fromLC.
Mi $2. 40, ph$3.30. HW-62447
Protection (rf carbon steel from atinospheric corro-
aiop. Interim report no. 1, by L. D. Perrigo
and R. G. Moles. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Oct 59. Contract AT(45-1)-1350. 8p.
Order from LC. Mi $1. 80, ph $1. 80.
HW-62466
Addldonal teats on the corrosion of carbon steel
following the turco-4512 decontamination proc-
ess, by A. P. Larrick. General Electric Com-
pany. Hanford Atomic Products Operation,
Richland, Wash. Nov 59. Contract W-31 -109-
Eng-52. 9p. Order fromLC. Ml $1,80,
ph$1.80. HW-62690
Tlie irradlattxl rupture prototype (IRP^ design by
G. E. Neibaur and li. D. Stice. GeneralElec-
tric Ccxnpany, Hanford Atomic Products Opera-
tion, Richland, Wash. Feb 60. Contract AT-
(45-l)-1350. 12p. Order fromLC. Mi $2. 40,
Ph$3.30. HW -62701
Corroaion of type 202 stainless steel in high tem-
perature waoer, by A. P. Larrick. General
Electric Company, Hanford Atcxnic Products
Operation, Richland, Wash. Dec 59. Contract
AT(45-1)-1350. 8p. Order from LC. Mi $1 . 80,
ph$1.80. HW-62820
Deconttmination of the irradiated nqiture prototype
with peroxide- -carbonate and apaqe, by G. E.
Neibaur and R. D. Wack. General E lectric
Company, Hanford Atomic Products Operation,
Richland, Wash. Jan 60. Contract AT(45-1)-
1350. 9p. Order fromLC. Mi $1.80, ph $1.80.
HW- 63346
359
An initial study
I
at me wear
and
galling
.18 on ai
of various
hiel element 3 ugport materlala on autoclave3~
Zircaloy-2 byj. W. Weber. General Electric
Company rilanford Atomic Producta Operation.
Richland, Wash, Jan 60. Contract AT(45-1)-
1350. 7p. OrdirfromLC. Mi $1.80, ph$1.80.
HW-63730
Develownent of a <jeldlng proceaa for end cloaurea
on NPR and KEJ fuefelement, by T. B. Correy
and others. General Electric Company, Hanford
Atcwnic Product! Operation, Richland, Wash.
P«b 60. Decl. {with deletiona July 8, 1960. 5p.
Order from LC.| Mi $1.80. ph $1.80.
HW-63977(Del.)
A Btudy of tiie wear and galling of various fuel ele-
^ ment support mjterials on autoclaved Zircaloy"-
2. Interim report no. 2, by J. W. Weber. Gen-
eral Electric Company, Hanford Atomic Ehroducts
Operation, Richland, Wash. Mar 60. Contract
AT(45-1)-1350.
ph $3.30.
18p. Order from LC. Mi $2. 40,
HW -64075
Burst testing of irradiated Zircaloy nibing, by V. 1
Hanford Atomic Products Operation,
Mar 60. Contract AT(45-1)-
Richland, Waah
1350. Up. Or<ter from OTS.
50 cents.
HW
64168
Development of a j4elding process for spire-can fuel
elements, by G. R. Hanson. General Electric
Companyr Hanf(|rd Atomic Products Operation,
Richland, Wash, Mar 60. Contract AT(45-1)-
1350. 9p. Ord^r from LX:. Mi $1.80, ph $1.80.
HW- 64294
Uni<
lied to fuel clad-
ique fabrication tprocesses applied to fuel ciaa
mng materials, py S. H. Buan. General Elec
trie Company, Hanford Atomic Products, Opera-
tion, Richland, Wash. Mar 60. Contract W-31-
109-Eng-52. 2$p. Order from LC. Mi $2.70.
ph$4.80. I HW -64335
Novel ceramic fuej fabrication processes, by The
Staff of Ceramics Fuela Development, Hanford
Atomic Producta Operation, Hanford Laboratories
Operation^ Richland, Wash. Apr 60. Contract
AT(45-1)-1350. 50p. Order from OTS. $1. 25.
HW- 64629
Ziroaloy process cube monitoring, by P. J. Pankas-
kle. General Eiectric Company. Hanford Atomic
Products Operation, Richland, Wash. Apr 60.
Contract AT(45-l)-1350. 8p. Order from LC.
Mi$1.80, ph$i.80. HW-64731
Ultrasonic cleanint of fuel element components, by
C. A. Strand. General Electric Company,
1
Hanford Atomic Products Operation. Richland,
Wash. Apr 60. Contract AT(4501)- 1350. 5p.
Order from LC. Mi $1.80, ph$l.80.
HW- 64796
Pb-Sn alloy replacements for UO? denaity standards,
by J. A. diristensen. General Electric Com-
pany, Hanford Atomic Products Operation, Rich-
land, Waah. Apr 60. 7p. Order from LC.
Mi $1.80, ph$1.80. HW-64912
Ultrasonic grain size testing of Hanford fuel ele-
ments, py C. L. Frederick, Hanford Atopiic
Products Operation, Washingt n, D. C. May 60.
Contract AT(45-1)- 1350. I8p. Order from
OTS. 50 cents. HW-64971
Autoclave testing of Zircaloy-2, by R. A. Thiede.
Hanford Atornic Products Operation, Richland,
Waah, June 60. Contract AT(45-1)-1350. 5^.
Order from OTS. $1.50. HW-65350
A data recording system for the fuel core tester,
by G. L. Wafdkoeiter. Hanford Atomic Products
Gyration, Richland, Wash. June 60. Contract
AT(45-1)-1350. 19p. Order from OTS.
75 cents. HW-65756
Resonant frequency tester: A machine using meas- |
urement of frequency decay for quality evaluatioo i
of axial flow compressor Plades, by E. R. r
Taylor and others. Union Carbide Nuclear Com-
pany, Division of Union Carbide Corporation,
Oak Ridge Gaseous Diffusion Plant, Oak Ridge.
Tenn. June 60. Contract W-7405-eng-26. 38p.
Order from OTS. $1.00. K-1393
The diffusion of fission gases In metallic fuels, by
M.S. Reynolds. Knolls Atomic Power Labora-
tory, Schenectady, N. Y. Apr 55. Decl. May
3, 1960. Contract W- 31 -109- Eng- 52. 25p.
Order from LC. Mi $2.70, ph $4.80.
KAPL-1315
Grain refinement of cast beryllium, by A. E. Bibb
and S. M. Bishop. Knolls Atomic Power Labor-
atory, Schenectady, N. Y. Apr 58. Changed
from OFFICIAL USE ONLY June 17, 1960.
Contract W- 31 -109 -Eng -52. 19p. Order from
LC. Mi $2.70. ph$4.80. KAPL-1917
Controlled atmosphere differential thermal analysis
apparatus, by A. E. Bibb. Knolls Atomic Power
Uux>ratory, Schenectady, N. Y. Jan 60. Coo-
tract W-31-109-Eng-52. I2p. Order from LC.
Mi $2. 40. ph$3.30. KAPL-M-AEB-6
360
fjoodeatructive testing of Bj rfiS poison wire, by
A. J. Valachovic and R. C. HoIT Knolls
Atomic Power Laboratory, Schenecudy, N. Y.
Mar 60. Contract W-31-109-Eng-52. 23p.
Order from LC. Mi $2.70. ph $4.80.
: KAPL-M-AJV-1
Butt welding of copper to stainless steel sheet, by
D. B. Kittle and J. M. Gerken. Knolls Atomic
Power Laboratory, Schenecudy, N. Y. Feb 60.
Contract W- 31 -109 -Eng -52. IChp. Order from
LC. Mi $1.80, ph$1.80. KAPL-M-DBK-6
Brazing Inconel- shea ted thermocouples to Inconel
structural plugs and seal collars, by J. D. Carey
and A. J. ralmer. Knolls Atomic Power Labora-
tory, N. Y. July 60. Contract W-31-109-Eng-
52. 12p. Order from LC. Mi $2. 40, ph $3. 30.
KAPL-M-JDC-1
Fabrication of box section
flow test assemblies
Tohe-
bncation of box section type flow test assi
by welding, by J. M. Gerken and S. A . T<
gaard. Knolls Atomic Power Laboratory,
Schenecudy, N. Y. Mar 60. 14p. Order from
LC. Ml $2. 40, ph $3. 30. KAPL-M-JMG-13
Corroeion of aluminum in dilute aoueous solutiona.
by J. P. Howe. Knolls Atomic Power Laboratory.
Schenecudy, N. Y. [1948]. Decl. June 14,
1956. Contract W-31-109-Eng-52. 26p. Order
fromLC. Mi $2.70, ph$4.80.
I KAPL-M-JPH-20
Reaiupe of Inconel design Information, by G. C.
Wheeler, Knolls Atomic Power Laboratory,
Schenecudy, N. Y. Feb 60. Contract W- 31-
l09-Eng-52. Up. Order from LC. Mi $2. 40.
ph$3.30. I KAPL-M-NMA-1
Proceaa description for covering metal with a lamin-
ated ceramic coating, by R. E. Mistier and
odiera. Knolls Atomic Power Laboratory,
Schenecudy, N. Y. Dec 59. Contract W-31-
109-Eng-52. lOp. Order from LC. Mi $1.80,
ph$1.80. KAPL-M-REM-1
Fatigue tests of S3G fuel cell tube structure sections,
by S. Beiucher and G. L. Cutler. Knolls Atomic
Power Labdratory, Schenecudy, N. Y. Dec 59.
Contract W-39-109-Eng-52. 22p. Order from
LC. Mi $2.70. ph$4.80.
KAPL-M-SAB-l(Rev.)
The ARC welding of end cape to rectangular co-
extruded irradiation specimens, by w. A. Owcz-
arski and J. F. Bollinger. Knolls Atomic Power
Laboratory, Schenectady, N. Y. Jan 60. Con-
tract W-31-109-Eng-52. 23p. Order fromLC
Mi $2.70, ph$4.80. KAPL-M-WAO-5
The hot duetillty of Inconel BP-85 weld despos^ta, by
W. A. (^wczarski. Knolls Atomic Power Labora-
tory, Schenecudy, N. Y. Apr 60. Contract
W-31-109-Eng-52. 22p. Order from LC.
Mi $2.70, ph$4.80. KAPL-M-WAO-7
The feaaibllity of bubble testing rhombus and cluster
assemblies, by W. H. PappUi. Knolls Atomic
Power Laboratory, Schenecudy, N, Y. July 60.
Contract W -31- 109-Eng-52. Up. Order from
L. Mi $2. 40. ph $3. 30. KAPL-M-WHP-1 ,
I>evelc«)ment^ techniques for rolling uranium naet-
al, by D. E. Deutsch and others. Los Alamos
ScTentific Laboratory, Los Alamos, N. Mex.
Nov 50. Decl. with deletions January 28, 1960.
Contract W-7405-eng-36. 128p. Order from
LC. Mi $6.30, Ph $19.80. LA-1180(DeI.)
Welding of plutonium, by J. W. Anderson and others.
Los Alamos Scientific Laboratory, Loe Alamos,
N. Mex. May 58. Decl. March 13, 1959. Con-
tract W-7405-eng-36. 1^. Order from LC.
Mi $2. 40, ph $3. 30. LA-2220
The use of quartz tubes for sampling and casting
plutonium, by K. W. R. Johnson and J. W. Ander-
son. Los Alamos Scientific Laboratory, Los
Alamos, N. Mex. Aug 58. Decl. March 16,
1960. Contract W-7405-eng-36. I6p. Order
from LC. Mi $2. 40. ph $3. 30. LA-2250
The adaptation of new research techniques to miner -
al engineering problems, by K. BrBuer and others.
Massachusetts Institute of Technology, Depart-
ment of Meullurgy, Cambridge, Mass. Apr 60.
Contract AT(30-l)-956. 48p. Order from OTS.
^ $1.25. MI'IS-44
Literature survey on uranium monocarbide, by J. L.
Kane. Martin Company, Nuclear Division.
Baltimore, Md. July 59. 20p. Order from LC.
Mi $2. 40, ph$3.30. MND-2061
Coated particle inyeatigation. Pinal summary re -
art. Voluine 1, by D. Goslee. Martin Company,
uclear Division, Baltimore. Md. Apr 59. Con-
AT(ll-l)-589. 63p. Order from LC. Mi $3. 90,
ph$10.80. MND-AC-1755-1
Atomistic interpreution of radiation effecu in
meula, by A. Soein. Atomics International
Division, North American Aviation, Inc. , Can-
oga Park, Calif . Dec 59. Contract AT- U-l-
GEN-8. 34p. Order fromLC. Mi$3.0Q
ph$6.30. NAA-SR-4301
361
Finely dispergad phases in uranium -molybdenum
ternary alloys, by D. Kramer. Atotrdca Inter-
national, A bivlslon of North American Aviation,
Inc. , Caiioga Park, Calif. November 60. Con-
tract AT(ll-il)-GEN-8. 18p. Order from OTS.
SO cents. NAA-SR-5S07
Preparation of
faorlum-alumlnum alloys by direct
>ria reduction, by D. O. Raleigfa. Atomica
Internatlonai A Division of North American
Aviation, In^. , Canoga Park, CaUf . Dec 60.
Contract A'Itll-l)-GEN -8. 29p. Order from
OTS. 50ce4ts. NAA-SR-5689
The vapor presiiure of BeO, by T. A. Milne.
Atomics Interna clonal, A Division of North
American Aviation, Inc. , Canoga Park, CaUf .
Dec 56. 20p. Order from LC. Ml $2.40.
ph$3.30. NAA-SR-Memo-l795
Review o< llcer^ture on dtermal ejyansion of cerntet
components and metal-ceramic interface reac^
tions. by D. '). Klein. Atomics International.
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Jan 57. I4p, Order from
LC. Mi$2.*0. ph$3.30. NAA-SR-Memo-1837
Effect of e:qx)8i>ig uranium to santowax R at 350°F,
by H. E, Klline. Atomics International, Divl-
alon of North American Aviation, Inc. , Canoga
Park, Calif. May 57. 9p. Order from IjC.
Mi $1.80, pl^$1.80. NAA-SR -Memo- 1942
Rates of alloyiiy (rfSRB metal fuels with their
jackets ebayf ItffXTF, by R. S. Neymark.
Atomics Inteirnational Division, North American
Aviation, Inc., Canoga Park, Calif. June 58.
12p. Order from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-2835
Preliminary investigation of uranium compounds for
use as fuels in sodium graphite reactors, by W.
Robeon and A. Webb. Atomica International
Division, North American Aviation, Inc. ,
Canoga Park. Calif . Aug 58. 9p. Order from
LC. Ml$l.^ ph$1.80.
NAA-SR -Memo- 2995
Mechanical ass >inbly fabrication of oxide fuel ele-
n^ents, by E^ F. Cook. Atomics International
Division, North Annerican Aviation, Inc. , Can-
oga Park, Calif. Dec 58. 22p. Order from
LC. Mi$2.ro, ph$4.80
NAA-SR -Memo- 3299
Strength testftoti low-melting-point alloy seal, by
l.S. Kenne<ly. Atomic International. Dlvisli
HNPF-pressure build-up and
-ly aiva gas space require-
ments of the U-10 w/o Mo fuel elennents, by H. L
Sletten and A. Musso, Jr. Atomics International
Division, North American Aviation, Inc. , Cano-
go Park, Calif. May 59. 18p. Order from LC.
Ml $2. 40, ph$3.30. NAA-SR-Memo-3889
Investigation of y>por phase plating for cladding re-
actor fuels: Literature search, by J. Bodlne.
Atomics International Division, North American
Aviation, Inc. , Canoga Park, Calif. July 59.
14p. Order from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-4140
Production and fabrlcadon of UC by ARC melring,
by D. H. Turner. Atomics International DivislQi,
Na-th American Aviation, Inc. , Canoga Park,
Calif. Sep 59. I4p. Order from LC. Mi $2.40,
ph $3. 30. NAA-SR-Memo-4378
Compatibility of U-10 Mo with 304 suinless steel
at lOOC^, by R. S. Neymark. Atomics Interna-
tional Division, North American Aviation, Inc.,
Canoga Park, Calif. Feb 60. 7p. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR-Memo-4943
The diffusion of hydrogen through zirconium, by
K. A. Sense. Atomics International. Division
Ol North American Aviation, Inc. , Canoga Park,
Calif. Mar 60. 7p. Order from LC. Mi $1. 8a
ph $1 . 80. NAA-SR-Memo-5067
Resistivity of U-Mo alloy fuel rryasurements and
sundards test no. 2352, by G. A. Stone. Xtom-
ics International. Division of North American
Aviation, Inc. , Canoga Park, Calif. Apr 60.
5p. Order from LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-51S0
Materials for radiator-condenser ahell, by J. C.
sells. Atomics International. EHvision of
North American Aviation, Inc., Canoga Park,
Calif. Apr 60. I8p. Order from LC. Mi $2. 4a
ph$3.30. NAA-SR-Memo-5183
Elevated oemperature wear characteristics of Zir-
caIoy-2 and type 304 atainless steel in conttct
with Hastelloy-X, by J. A. Roberson. Atomica
International. Division of North Ane rican
Aviation, Inc., Canoga Park, Calif. Feb 60.
I3p. Order from LC. $2. 40, ph $3. 30.
NAA-SR-Memo-5252
itlbllity of UO2 and APM-M-2S7, revision of
R-4Z70, by K. Langrod. Atomics Internatibn-
R. S. Kenne<ly. Atomic International. Division
of North American Aviation, Inc. , Canoga Park,
Calif. Apr i9. lip. Order from LC. Mi $2.40,
ph$3.30. 1 NAA-SR -Memo- 3641 j^
Corn
al. Division of North American Aviation, Inc.,
Canoga Park. Calif. May 60. 7p. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR-Memo-5330 (Rev. A)
ABC safety mon
reactions, by
^
Cha
rll.
B and H.
Metal -water
Soodak.
Nuclear Developtnent Corporation of America,
White Plains, N. Y. [1956]. Decl. December
29,1959. 2lp. Order from LC. Mi $2.70,
ph$4.80. j NDA-15K-3
Determination of rf>e solution rate of metals in
Utfaium, by B. Minushkin. Nuclear Development
Corporation of America, White Plains, N. Y.
June 58. Decl. with deletions November 10,
1958. 40p. Order frwnLC. Mi $3. 30,
I*$7.80. I NDA-44(Del.)
Tbt preparation and properties of dispersion harden-
eo uranium powder products Quarterly techni-
cal report for the period ending June 30. 1959,
by W. Arbiter. Nuclear Devek)pment Corpora-
tlon of America, White Plains, N. Y. July 59.
Contract AT(30-l)-2303. 18p. Order from LC.
Ml $3. 00, ph$6.30. NDA-2II2-2
The preparation and properties of dispersion harden-
eg uranium powder products. Quartei
cal^ reyjrt for the period endingjeptember 36^
'■W
techni-
1959, by W. Arbiter. NuclearDevelopment
Corporation of America, White Plains, N. Y,
Oa 59. Contract AT(30-l)-2303. 31p. Order
fromLC. Mi $3. 00, ph $6. 30. NDA-2II2-4
Sponge fuel evaluation. Quarterly technical report
to the period ending December 31, 1959, by
J. M. KcKee. Nuclear Development Corporation
of America, White Plains, N. Y. Feb 60. Con-
tract AT(30-1)- 2303. 9p. Order fromLC.
Ml $1.80, ph $1.80. NDA-2116-5
Carbide fuel develomnetit . Progress report for
period of Septeniber 1 5, 1959 to January 31 ,~1960,
by A. Strasser and K. Taylor. Carboundum
Company, Niagara Falls, N. Y. Mar 60. Con-
tract AT(30-1)- 2303. 22p. Order fromLC.
Mi $2.70, ph$4.80. NDA-2145-1
SB report for
Carbide fuel development. Pr
~ February 1. 1966 to April 35", 1960, byTT
opment. Progret
Strasser and K. Taylor. Nuclear Develo|Hnent
Corporation of An»erica, White Plains, N. Y.
and Carborundum Company, Niagara Palls, N. Y.
June 60. Contract AT(30-l)-2303. 13p. Order
fromLC. Ml $2.40, ph $3.30. NDA-2145-4
Prediction of dimensional changes in uranium fuel
elements during irradiation--The elastic solu-"
iaoninterini report by P. R. Morris and R. N.
Thudium. National Lead Company of Ohio,
Cincinnati, Ohio. Sep 60. Contract AT(30-1)-
1156. 27p. Order from OTS. 75 cents.
NLCO-816
The application of the chip and shot methods to the
preparation of homogeneous alloys, by D. S.
kneppel. Nuclear Metals, Inc. , Concord, Mass.
Sep 58. Decl. March 31, I960. Contract AT
(30-l)-1565. 40p. .Order from LC. Mi $3. 00,
ph$6.30. NMl-1206
Texture of extruded zirconium and Zir(aloy-2
tubing, by V. Nerses. Nuclear Metals, Inc. .
Concord, Mass. July 60. Contract AT(30-1)-
1565. 35p. Order from OTS. 75 cents.
NMI-1222
texture
Preliminary attempts to produce randomly oriented
wrought beryllium ana their relation to tex
development, by F. M. Yans and P. Pointu
Nuclear Meuls, Inc., Concord. Mass. July 60.
Contract AT(30-1)-1565. 53p. Order from OTS.
$1.25. NMl-1225
Analysis of oxygen in beryllium, by A. R. Oilman
andS. Isserow. Nuclear Metals, Inc., Concord,
Mass. May 60. Contract AT(30-1)- 1565. 24p.
Order fromLC. Mi $2.70. ph $4.80.
NMI-1234
Fabrication devel(yment of beryllium-clad uranium-
3. 8% silicon, uranium -lOgt molybdenum, and
uranium - uranium monocarbide cermets, by ].
Greenspan. Nuclear Metals, Inc. , Concord,
Mass. Aug 60. Contract AT(30-1)-1565. 71p.
Order from OTS. $1.75. NMI-1236
Retention of uranium beta phase, by A. L. Geary
and V. Nerses. Nuclear Meuls, Inc., Concord.
Mass. Aug 60. Contract AT(30-1)-1565. 32p.
Order from LC. Mi $3. 00, ph $6. 30.
NMI-1237
A metallographic study erf the swelling of uranium
and uranium alloys, by A. Boltax and A. R.
Lumbert. Nuclear Metals, Inc. , Concord, Mass.
Aug 60. Contract AT(30-1)-1565. 78p. Order
from OTS. $1.75. NMI-1239
Preliminary survey of mechanical properties and
phase relationships in several peryllium binary
atloys for July 1 l958-June 30, 1959, by P. M.
Vans. Nuclear Meuls, Inc. , Concord, Mass.
Sep 60. Contract AT(30-l)-1565. 41p. Order
from OTS. $1.00. NMI-1240
Deforniation modes of single crysul uranium dlox-
ide from 700^ to 1900^C, by E. ]. Rapperport
and A. M. Huntress. Ffuclear Meuls, Inc. ,
Concord, Mass. Aug 60. Contract AT(30-1)-
1565. 29p. Order from OTS. 75 cenu.
NMI-1242
363
Fabrication of cUd masaive UO9 fuel elementa by
— hot extrusion. Monthly letter report for S>eptem-
ber. Nuclear Petals, Inc. , Concord, Mass.
73cr59. 6 p. Order from LC. Mi $1.80,
ph$l.80. NMI-2504
ot
The fabrication df clad masstve UO7 fuel elements
by coextrusioq. Cluarterly progress report no:
4ri5rPebruary. March, and April I96U, by
J. G. Hunt an4 P. Loewenstein. Nuclear Meuls,
tac! Concord Mass. June 60. Contract AT
(30-l)-1565. |24p. Order from LC. Ml $2. 40,
ph$3.30. ,,^ NMI-2510
Fundaroenul and applied researdi and deyelopinent
in metallurgy. Progreaa report Jor November
T95g Nucleir Metals, Inc. , Concord, Nlass .
1960. 20p. Order
,30. NMI-2a72
]iir^. Decl, May 18.
froooLC. Mi $2. 40. ph $3.
Fundamental and applied research and development
in meuUurgy. Progress report for ttecember
l95S. Nuclear Metals, inc., Concord, Mass.
P^59. Decl. May 18, 1960. 20p. Order
from LC. Ml $2. 40. ph $3. 30. NMl-2073
Fundamentol amt applied research and development
in meMllurgy. progress report for January 1959.
Nuclear Mewls, Inc., Concord, Mass. Mar 59.
Decl. May 1$, I960. 30p. Order from LC.
Ml $2.70, ph$4.80. NMl-2074
Fundamental and applied research and development
in metallurgy. Progress report for March 1959.
Nuclear Met#ls, Inc., Concord, Mass. May 59.
Decl. May i;8, 1960. 52p. Order from LC.
Mi $3.30. pri $7.80. NMl-2076
I
nenul aryl applied research and development
tietallurgy. Progress report for November
5. Nuc&r Metals, Inc., Concord, Mass.
Fundamental anid af
in metal
1959: . ^^
15Ii760. Colitract AT(30-1)-1565. 31p. Order
from LC. KJi $2.70, ph $4.80. NMI-2081
Fundamental and applied research and development
in mcMllura^. Progress report for December
1959. Nuclaar Metals, Inc., Concord, Mass.
1^5760. Contract AT(30-1)- 1565. 28p. Order
frcmi LC. Mi $2. 70. ph $4. 80. NMl-2082
:. ^*i$2.
Fundamental aitd applied research and development
In metalluriiv. Progress report for January 1960
Nuclear Melals, be.,- Concord, Mass. May 60.
Contract At(30-1)- 1565. 25p.
Mi $2.70, ph$4.80.
Order from LC.
NMI-2083
Fundamenul and applied research and development
— in metallurgy. Progress report for Februaj^
I960. Nuclear Metals, Inc., Concord, Mass.
May 60. Contract AT(30-1)- 1565. 36p. Order
fromLC. Mi $3. 00, ph $6. 30. NMI-2084
m
indamental and applied research and developmew
in metallurgy, progress report for March 1960
Nuclear Metals, Inc., Concord, Mass. June 60
Contract AT(30-l)-1565. 39p. Order from LC.
Mi $3.00. ph $6.30. NMI-2085
Fundamental and applied research and develc
:nt
indemental and applied research and developmen
"In metallurgy. Progress report for April 1960.
Nuclear Metals. Inc., Concord, Mass. June
60. Contract AT( 30-1)- 1565. 33p. Order
fromLC. Mi $3. 00. ph$6.30. NMI-2086
Evaluation of Zlrcaloy-clad U-2 <y/o Zr alloy tube
— no. 23. Extrusion no. 1&394. by U. F. Kauf-
man and R..G. Jenkins. Nuclear Metals, Inc.,
Concord, Mass. Feb 59. Contract AT(30-1)-
1565. 36p. Order from LC. Mi $3.00.
ph$6.30. NMI-4375
Evaluation of six Zircaloy-clad U-2 w/oZr alloy
tubes made for irradiation in the VBWR test_
T5c;pr5y P. P. Kaufman and w. J. Richmond.
N^ear Metals, Inc., Concord, Mass. June 59.
Contract AT(30-1)- 1565. 66p. Order from LC.
Mi $3. 90, ph$10.80. NMl- 4387 (Del.)
Coextrusion of Zircaloy-clad U-2 */o Zr rod for
— the EBR-1 Mark III core loading, by H. F. Saw-
y^T Nuclear Metals, Inc. , Cambridge, Mass.
Apr 58. Contract AT(30-1)- 1565. 53p. Order
from OTS. $1.25. NMl-4801
Development work on the fabrication of CP-5 fuel
— element tubes, by J. Wong. Nuclear Meuls,
Inc.. Concord, Mass. May 60. Contract AT
(30-l)-1565. 52p. Order from OTS. $1.25.
^ NMI-4852
Feasibility report for the fabrication of prototype
— Zircaloy-clad uranium fuel rod for Hanlord
THmTuc Products Operation by H. F. Sawyer.
Nuclear Metals, Inc. . Cambridge, Mass. Jan
58 35p. Order fromLC. Mi $3.00, ph $6.30.
NMl-FR-15
The development of uranium carbide fg_^""^|^r
fuel. First annual report May 1, l'>5^ to Apnj.
30. 1960, by H. 5. Ralish and others. Metal-
lurgical Laboratories, Olin Mathieson Chemical
Corporation, New Haven, Conn. June 60. Coo-
tract AT(30-l)-2374. 38p. Order from OTS.
$1.00. NY)-2688
364
Nuclear fuel research fuel cycle development pro-
gram. Quarterly progress report for AprlFl,
to June 30, 1966, by R. B. Holden andodiers.
Metallurgical Laboratories, Olin Mathieson
Chemical Corporation, New Haven, Conn. July
60. Contrcct AT(30-l)-2374. 22p. Order
from OTS. 75 cents. NYO-2689
The development and testing of homogeneous ceram-
ic fuels. Progress report for period September
1 -November 5), 1959, by G. Zuromsky. Com-
bustion Engineering, Inc. , Nuclear Division,
Windsor, Conn. 1959. Contract AT(30-1)- 2379.
24p. Order from LC. Mi $2.70, ph $4.80.
NYO-2742
A program to study the feasibility of and develop
an apparatus for the ultrasonic roll bonding^
fuel plates. Monthly progress letter. Taslc IV,
by R. K. Steele. Cornbustion Engineering, Inc. ,
Nuclear Division, Windsor, Conn. Dec 59.
Contract AT(30-l)-2379. Widi this is bound:
Progress report no. 4 covering the period Octo-
ber 16 to November 15, 1959, by H. L. McKaig
Jrl Aeroprojects Inc. , West Chester, Pa.
Dec 59. 15p. Order from LC. Mi $2.40,
ph $3. 30. NYO-2794
Final report on coating fuel elements, November 14,
1959. Nuclear Materials and Equipment Cor-
poration, Apollo, Pa. 1959. Changed from
OFFICIAL USE ONLY July 5, 1960. Contract
AT(30-l)-2264. 61p. Order from LC. Mi $3. 90,
ph $ 10.80. NYO-2801
Quarterly progress report for November 16, 1959
K) February 15, 19bO. Nuclear Materials and
Equipment Corporation, Apollo, Pa. 1960.
Changed from OFFICIAL USE CWLYJulyS, 1960.
Contract AT(30-1)- 2264. 2^. Order from LC.
Ml $3. 00, ph$6.30. NYO-2804
X-ray measurenwnt of twin faulting in FCC meuls,
by B. E. Warren. Massachusetts Institute of
Technology, Cambridge, Mass. 1959. Contract
AT(30 l)-858. 9p. Order from LC. Mi $1.80,
ph$1.80. NYO-4834
Ultraaonically accelerated dissolution of high-
temperature and corrosion -resistant metals, by
J. L. Straughn and W. B. Tarpley. Aeroprojecu
Inc., Westchester, Pa. May 58. Decl. March
16, 1960. Contract AT(30-1)- 1836. I6p. Order
fromLC. Mi $2.40, ph $3.30. NYO-7925
SolM-Iiquid equilibrium in the systems lithium hy-
dride-tiuniurn hydride and lithium hydride-
zirconium hydride, by C. E. Messer and Ira S.
l^evy. Tufts University, Medford, Mass. July
60. Contract AT(30-1)- 1410. 9p. Order from
LC. Mi $1.80, ph $1.80. NYO-8029
An X-ray diffraction study of the palladium-
iratures and
Mae land and
Medford,
Mass. Jan 60. Contract AT(30-1)-1355. I7p.
Order from LC. Mi $2. 40, ph $3. 30.
NYO-7551
The stabilization of aqueous suspensions of thorium
ox|^de . Progress report for November 1 , 1958 -
February 2$, 1960, by V. K. La Mer and others.
Columbia University, New York, N. Y. Apr 60.
Contract AT(30-l)-2267. 29p. Order from LC.
Mi $2.70. ph $4.80. NYO-8797
An approach to the study of solid sute bonding.
Final report for December 1958-Nobember 1959,
by R. K. Steele and J. Kozol. Combustion Eogi-
neering. Inc. , Nuclear Division, Windson, Conn.
1959. Changed from OFFICIAL USE ONLY
March 16, 1960. Contract AT(30-l)-2302. 44p.
Order from LC. Mi $3.30, ph $7.80.
NYO-8906
Quarterly progress report no. 2 coverin'
^ ry 16, 1960 to May 15, 1960. Nuclear
its
progresi
February 16, l*
Materials and E-^uipment Corporation, Apollo,
Pa. 1960. Contract AT(30-l)-2264. SC^.
Order from LC. Mi $3. 00, ph $6. 30.
NYO-9184
MeuIIuri
lUlIurgy division quarterly progress report for
period ending October 31, 1950, by E. C. Miller
and W. H. Bridges. Oak Ridge National Labor-
atory, Oak Ridge, Tenn. Feb 51, Decl. with
deletions October 19, 1959. Contract W-7405-
eng-26. 70p. Order fr<Mn LC. Mi $3. 90,
ph $10.80. ORNL-910 (Del. )
Meullurgy division quarterly progress report for
period ending January 31, I95C by E. C. Miller
and W. H. Bridges. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. June 51. Decl. with
deletions October 27, 1959. Contract W-7405-
eng-26. 73p. Order from LC. Mi $4.50,
ph $12. 30. ORNL-987 (Del. )
S?
Meullurgy division quarterly progress report for
riooenchng October 31, 1951, by W. H. Bridge
ridges. Oak Ridge National Laboratory, Oak
*^idge, Tenn. Apr 52. Decl. with deletions
Nobember 12, 1959. Contract W-7405-eng-26.
56p. Order from LC. Mi $3. 60, ph $9. 30.
ORNL-1161 (Del.)
Solid sute division semiannual progress report for
period ending August 31, 1955. Oak Ridge Nation
tional Laboratory, Oak Ridge, Tenn. Nov 55.
Decl. October 22, 1959. Contract W-7405-eng-
26. 36p. Order from LC. Mi $3.00, ph $6.30.
ORNL-1944
365
Metallurgy dlvlalcn gemlannml
rt for
tallurgy dlvlalCTi gemlaiutiMl progrcM rcpot
eiricxTending October 10. 1956. Ok Ridge
ational Latwratory. Oak Ridge, Tenn. 1956.
Decl, with deaetions November 4, 1959. Con-
tract W-7405'eng-26. 23lp. Order frcra LC.
h4i$10.20. pk$36.30. ORNL-2217 (Del.)
Electrole83 -plaibd brazing alloy , by P. Patriarca
and others, bak Ridge Nadooal Laboratory,
Oak Ridge, Tfenn. Mar 57. Contract W-7405-
eng-26. 13p, Order from LC. Ml $2.40,
ph $3. 30. ORNL-2243
The aolubility ol nitrogen and oxygen in lidiiuin and
methods of li]hi "' ~ " "
um purificationT by E. E. Hoff-
man. Oak Ridge National Laboratory, Oak Ridge,
Ttenn. Mar 6p. Contract W-7405-eng-26. 23p.
Order from LC. Mi $2.70. ph $4.80.
ORNL-2894
A failure analyal
mance of dis
for the low -temperature perfor-
.-Tsion fuel elementa, by J. R.
Eidge National Laboratory, Oak
Ridge, Tenn. June 60. Contraa W-7405-eng-
26. 36p. Oflder from LC. Mi $3. 00, ph $6. 30.
i ORNL-2902
Columbium cladi uranium carbide fuel element.
terly retert no. 2 for Auguat 1-bctqEer 31,
1959, by J. J. Finley and othera. Union Carbide
l^etaLa Comp«uiy. Niagara Falls, N. Y. Nov 59.
Contract AT(40-l)-2559. I7p. Order from LC.
Mi $2.40, ph, $3. 30. ORO-222
Fuel-bearing fiherglaa in aluminum base fuel ele*
ments. Quairterly report no. 2 for August 1,
19W to gtofer 31, m9, by R. H. Baskey.
Clevite Corporation, Mechanical Research Divl-
•ion, CleveUind, Oho. Nov 59. Contract AT
(40-l)-2557. 37p. Order from LC. Mi $3.00,
ph$6.30. ORO-224
Monthly progreas letter no. 6 for period November
1 19S4 t5 14ovember 30 1»59, by R. H. Baakey.
Clevite Corporation, Mechanical Research Divi-
sion. Clevelnnd. Ohio. Dec 59. Contract AT
(40-l)-2557. 4p. Order from LC. Mi $1.80,
ph$1.80. . ORO-226
Monthly letter report no. 1 1 coveringperiod Septem-
ber 15 to Ocopber 15, 1959, byj. O. Fleming-
Georgia Institute of Technology, Engineering Ex-
periment Station, Atlanu, Ga. Oct 59. Contract
AT(40-l)-24a3. 2p. Order from LC. Mi $1.80.
I)h$l,80. ORO-236
Columbium clad uranium carbide fuel element con-
Monthly letter report for November 1
tract. Montftiy letter report lor Novemner i
dirough Nov^nber 30, 1959. by J. J. Finley and
and others. Union Carbide Metals Company,
Niagara Falls, N. Y. 1959. Contract AT(40-l)-
2559. 2p. Order from LC. Mi $1.80,
ph$1.80. ORO-241
Monthly progress report no. 7 for period December
1 M9t5 December 31, Iffl, by R. H. Bask^.
Clevite Research Center, Cleveland, OHo.
Jan 60. Contract AT(40-1)- 2557. 3p. Order
from LC. Mi $1.80, ph$1.80. ORO-246
Monthly progress report no. 8 for period January 1,
196d to Ttmuary 31. 1960, by R. H. Baskey.
Clevite Research Center, Cleveland, Ohio.
60. Contract AT(40-1)- 2557.
LC. Mi $1.80, ph$1.80.
4p.
Feb
Order from
ORO-247
Synthesis and fabrication of refractory uranium
compounds . Quarterly report "O-' 2 covering
period September 1 to November 30, 1959, by
k. M. Taylor and others. Carborundum Ccm-
pany. Niagara Falls, N. Y. Dec 59. Contraa
AF(40-l)-2558. 21p. Order from LC.
Ml $2.70, ph $4.80. ORO-248
Monthly letter report no. 13 covering the period
frcan November 15 to December 15, 1959," by
J. D. Fleming. Georgfia Institute of Technology,
Engineering Experiment Station, Atlanu, Ga.
Dec 59. Contract AT940-l)-2483. 2p. Order
from LC. Mi $1.80. ph$1.80. ORO-250
Monthly letter report no. 14 covering period Decem-
— ber 15. 1959 to January 15, 1960 by J. D. Flem-
ing. Georgia Institite of Technology, Engineerlm
Experiment Sution, Atlanta, Ga. Jan 60. Con-
tract AT(40-l)-2483. 3p. Order from LC.
Mi $1.80. ph $1.80. ORO-251
Synthesis and fabrication of refractory uranium
compounds. Monthly process jepoft no. '5"tor
December 1 to Etecember 31 , 1959, by K.HCTi
Taylor axKl others. Carborundum Company,
NUgara Falls, N. Y. Jan 60. Contract AT
(40-l)-2558. 6p. Order from LC. Ml $1.80,
ph$l.80. ORO-254
r letter report no. 15 covering the pcrtod
I January 15 to February 15. 1960. byTTD.
aLng, deorgia Institute of Technology, Engi-
Monthly letter r<
^P"^ -r - . _ .
Fleming, deorgia Institute of Technology, Engi-
neering Experiment Station, Atlanta, Ga. Feb
60. Contract AT(40-1)- 2483. 2p. Order from
LC. Mi $1.80. ph$1.80. ORO-255
Columbium clad uranium carbide fuel element coq-
tract. Monthly letter report for December 1
through Decenaier 31 im by J. J. PI5Ry"*nd
odiers. Union Carbide Metals Company, Niagi-
ra Falls. N. Y. 1959. Contract AT(40-l)-2559.
366
^ Order fr«nLC. Ml $1.80. ph $1.80.
ORO-2S6
Columbium clad uranium carbide fuel element.
Quarterly report no7"
January 31, 1960, by
Union Carbide Metals
3 for November 1, 1959-
. J. J. Finley and others.
"Retala Company, Niagara Falls,
N. Y. Feb 60. Contract AT(40-1)- 2559. 30p.
Order from LC. Ml $2.70, ph $4.80.
ORO-262
Sptheaia and fabrication of refractory uranium
compounda. ^juarterly repon no. 3 for Decem-
ber 1, 1959 to Pebruair 29, 1960, by K. JXr~
Tkylor and others. Carborundum Company,
Research and Development Division, Niagara
Palla. N.Y. Mar 60. Contract AT(40-l)-2558.
19p. Order from LC. Mi $2. 40, ph $3. 30.
ORO-264
Syntfaeaia and fabrication of refractory uranium
compounds. Monthly progress report no. 7 for
March 1 through Marji 31 1960, by K. M;
Taylor and odiers. Carborundum Company,
NUgara Falls, N. Y. Apr 60. Contract AT
(40-l)-2558. 4p. Order from LC. Mi $1.80,
ph$1.80. ORO-267
Fuel hear
meats.
Iss in aluminum base fuel ele-
lonthlv progress letter no. 9 for period
jnmly profigrt
February 1, 1960 to February 29, 1960, by R. H.
Baskey. Clevite Corporation Mechanical Re-
search Division, Cleveland, Ohio. Mar 60.
Contract AT(40-1)- 2557. 4p. Order from LC.
Mi $1.80, ph$1.80. ORO-278
Fuel-bearing fiberglaa in aluminum base fuel ele-
ments. (ftiarterly report no. 4 for February 1.
1960 to April 30, 1966. by R. H. Baskey. Clev-
ite Corporation, Mechanical Research Division,
Cleveland. Ohio. June 60. Contract AT(40- 1 )-
2557. 26p. Order from LC. Ml $2.70,
I* $4. 80. ORO-300
Brittle fracture; ductile -brittle transitions, an an-
notated bibUop-aphy, byE. A. CernakandE.T.
Deigroeso. Pratt k Whitney Aircraft, Division
«f United Aircraft Corporaticn, Canel, Middle-
tcmn. Conn. Oct 60. Contract AT(ll-l)-229.
9lp. Order from OTS. $2.25. PWAC-301
ln^>Mtigation oi salta for use in uranium meul
PW-treatlng batfis, by S. R. Pocsik. TTie Dow
Uiemical Company, Rocky Flats Plant, Denver,
Ooio. July 60. Contract AT(29-1)- 1106. 22p.
Order from OTS. 50 cents. RFP-191
Plnenaionally stable alloyB Interim report, by
A. L Hiss and U.S. Kalish. Sylvania -Corning
Nuclear Corporation, Bayside, N. Y. Oct 57.
Decl. March 30, 1960. Contract AT- 30-1 -(XN-
366. 47^ Order from LC. Mi $3. 30, ph $7. 8a
SCNC-249
Technical
to
al Pf ogesB report for period July 1
August 31, 1957. sylvania -Coming Nuclear
Corporation, Bayside, N. Y. Dec 57. Decl.
Januarys, 1960. Contract AT- 30-1 -GEN -366.
20p. Order from LC. Ml $2. 40, ph $3. 30.
SCNC-254
Quarterly technical pr
ing peoember SiTT
as report for period end-
i7 . Sylvania - Corning
Nuclear Corporation, Bayside, N. Y. Mar 58.
Decl. Januarys, 1960. Contract AT- 30-[lI-
GEN-366. 61p. Order from LC. Mi $3. 60
ph $9.30. SCNC-261
Studies of strain wave prcyagation and associated
current output in bariiam dtanate, by J. W. Daily.
Sandia ^Corporation, Albuquerque, N. Mex.
Nov 59. 46p. Order from LC. Mi $3. 30,
Ph$7.80. SCnM-294-59(51)
The electrical behavior of exploding
vey of various materials, Dy T. ]. Tucker aiict
wires. A sur-
F. W. Nellson. SandiaCorporation. Albuquer-
que, N. Mex. Nov 59. Revised December 11,
1959. 122p. Order from LC. Mi $5.70,
ph $16.80. SCIM-334-59(51)
The thermal EMF of copper -conatanun thermo-
couples as a function ofjunction fabrication, by
J. U Hartley. Sandia Corporation, Albuquerque,
N. Mex. Dec 59. 18p. Onter from LC.
Mi $2. 40, ph $3. 30. SCriM-373-59(16)
The staking method of deforming metals and joining
parts, by R. P. Lewis. Sanma Corporation.
Albuquerque, N. Mex. Feb 60. 24p. Order
from LC. Mi $2.70, ph $4.80.
SCIM- 376- 59(25)
A determination of design strengths for 6061 -T-6
aluminum weldmentsT by D. W. Grobecker.
Sandia Corporation, Albuquerque, N. Mex.
Jan 59. Contract AT(29-l)-789. 37p. Order
fromLC. Mi $3.00, ph$6.30.
SCI>4-426-58(l6)
Physical properties of uraniuin slugs made by pow-
der naetallurgy, by J. L. Zambrow and H. H.
Hausner. Sylvania Electric Products Inc. . Bay-
side, N. Y. July 52. Decl. February 16, 1960.
Contract AT- 30-1 -GEN -366. 20p. Order from
LC. Mi $2. 40, ph $3. 30. SEP-95
367
Uranltnn-aluihlnum diffusion and aasocUted studies.
by S. Scorchheim and ]. Zambrow. Sylvania
Electric Products Inc. , Atomic Energy Division.
Bsyside, N. Y. Oct 52. Decl. February 16.
I960. Contract AT- 30-1 -GEN -366. 29p. Order
from LC. Mi $2.70, ph $4.80. SEP- 102
X
U quality testing program
report no.' I, by N.
Pri
Sylvania
SB
lectrlc
Uranium met _ _
Grossman.
Products, kiic. . Bayside, N. Y. Oct 53. Decl.
July 14. i960. Contract AT-30-1 -GEN -366. 84p.
Ortter froi^ OTS. 60 cents. SEP-l35(Rev.)
The fabrication erf tx>lIow cylindrical fuel elements
from uranjum powder, py J. Fugardl and others.
Technical Information Service. Oak Ridge Nation-
al Laboraipry, Oak Ridge, Tenn. [nd]. Decl.
April 20, I960. 27p. Order from 0T5. 30 cents.
SEP-157
Perforated wster fuel elements, by H. S. Kalish
• and ocher'sl Sylvania Electric Products, Inc.,
« Atomic Bafrgy Division. Bayside, N. Y. Sep 55.
Decl. De<)ember 15, 1959. Contract AT(11-1)-
229. 25p. Order from LC. Ml $2.70, pta $4.80.
SEP- 159
Hydrostatic pressing oi nrietal powders, by C. A.
Meyers anid W. G. Lidrasn. Sylvania Electric
Products. Inc. , Atomic Energy Division, Bayside.
N. Y. Sei^ 54. Decl. February 16. 1960.
Contract AT-30-1-BGN-366. 21p. Order from
LC. Mi $2. 40, ph $3. 30. SEP-180
Canning nickal-plated uranium slugs in aluminum.
ig nickql-pi
J. Storchrw
by J. Storichheim and others. Sylvania Electric
Products l^c. . Atomic Energy Division. Bayside.
N. Y. Jan|55. Decl. May 4. 1960. 31p. Order
from LC. i Mi $3. 00. ph $6. 30. SEP- 181
Monthly technical progress report for August 1956.
Sylvania Electric ft-oducta. Inc. , Atomic Energy
Division, fayside, N. Y. Oct 56. Decl. Febru-
ary 4. 196p. Contract AT- 30-1 -GEN -366. 2lp.
Order froi^ LC. Mi $2.70, ph $4.80. SEP-234
The self-diffuaion ot niobium— III. Final progress
report for July T7 1958 to January 1. 1959. by R.
Resnick aiid riiers. Sylvania Electric Products
Inc. . Res^rch Laboratories, Bayside, N. Y.
Mar 59. Contract AT(30-1)-2102. 14p. Order
from LC. JMi $2. 40. ph $3. 30. SEP- 252
Effect of hot aress cladding on mechanical properties
and micro»tructure of uranium plate, by W. R.
McDonell. Du Pont de Nemours (E. I. ) k Co.
Savaqnah Hiver Laboratory. Aiken. S. C. Dec 54.
Decl. February 16, I960. Contract AT(07- 2)- 1.
8p. Ordei
from LC. Mi $1.80,
ph$1.80.
TID-5382
Study of factors influencing ductility of iron-alumlj.
" Letter report no. 11, by F. C. Per
ns;
um alloys.
kins ana J. F. Nachman. University of Denver.
Denver Research Institute, Denver. Colo. Mar
60. Contract AT(ll-l)-742. 7p. Order from
LC. Ml $1.80. ph$1.80. TID-5626
A soitlstlcal description of distribution of phases.
Technical report no. 1. by D. E. Gucer. BIFovb
University. Providence, R. I. Feb 60, Contrao
AT(30-l)-2394. 2^. Order frwn LC. Mi $2.7|
ph$4.80. TID-5631
Phase equilibria studies of systems Involving the
alkali and alkaline earth metals. Report no. TV,
by F. A. Kanda and A. J. King. Syracuse UnivK
sity. Research Institute. Syracuse, N. Y. Mar
60. Contract AT(30-1)- 1910. 64p. Order fn»
LC. Ml $3.90, ph$10.80. TID-5691
lal expansioi
t. by F. A.
port, by F. A. Halden and others. Stanford Re-
search Institute, Menlo Park, Calif. Apr 59.
Contract AT(04-3)-115. 24p. Order from LC.
Mi $2.70. ph $4.80. TID-5722
Infornnal letter progress report, March 19|60. by
J. L. Zambrow. Sylvanla-Corning Nuclear Cor-
poration, Bayside. N. Y. Apr 60. Contract AT
30-I-GEN-366. 14p. Order from LC. Mi $2.40,
ph $3. 30. TID-5747
Zirconium hazards research. Summary report no.
3692, by J. A. Herickes and others. Bureau of
Mines, Pittsburgh. Pa. June 58. Contract AT
-(ll-l)-473. 31p. Order from LC. Mi $3.00,
ph$6.30. TID-5749
Fundamentals of glass-to-meul bonding. VIII. W«-
tability of iron by molten sodium diailicate. Tett-
nical progress report no. 8. by R. W. Cline an?
others' Mar 60. Contract AT(ll-l)-34. 30p.
Order from LC. Ml $2.70. ph $4.80.
TID-5754
Letter report no. 13. by D. W. Rudd. Metal Hydr-
ides Inc. . Chemical Research Laboratory. Bever-
ly, Mass. May 60. Contract AT(30-1)- 2298. 7p.
OrderfromLC. Ml $1.80, ph $1.80.
TID-5832
Diffusion in meuls. Progress report and publicatia
list, by D. Lazarus. University of Illinois,
UrBana, III. June 60. Contract AT(1 1-1)- 67.
53p. Order from LC. Mi $3. 60, ph $9. 30.
TID-5934
368
Growth of meul single crystals and the production
of high purity metals. I. Principles, techniques
and apparatus, by R. S. Davis and D. W. Batteau.
Flow Corporation, Arlington, Mass. Dec 59.
C&tract AT(30-l)-2049. 41p. Onter from LC.
Mi $3.00, ph$6.30. TID-5937
Burst-testing of large diameter Zlrcaloy-2 tvibiny
at 300^. Nuclear Materials and Equipment
Corporation, Apollo, Pa. Mar 60. Contract AT
(38-l)-200. 16p. OrderfromLC. Mi $2.40,
ph$3.30. TID-5940
Specialized otsting and forming of reactive metal
fhapes. fer log covered May 15, 1959 to October
15, 1959, by T. A. Hamm. Oregon Metallurgical
Corporation, Albany, N. Y. 1959. Contract W-
31-109-eng-52. 27p. OrderfromLC. Mi $2.70,
pli$4.80. TID-5951
Phaie equilibria, kinetic and thermodynamic studies
of some rare earth metal oxide ana nitride syB"^~
tenxs. Technical progress report, by L. Eyring
and others. State University of Iowa, Iowa City,
Iowa. May 60. Contract AT(ll-l)-72. 13^.
Order from LC. Mi $6.90, ph $21.30.
i TID-5956
Technical progress report, ftirt I. High-speed com-
puter program. Part II. Circuit re^jarch pro-
am. Part III. Mathematical mediods. Part IV.
i
witching circuit theory Part V. lUiac use a"n3"
Seration. Part VI. IBM 650 use and operation.
rt VII. General laboratory information. \Jtd-
versity of Illinois, Digital Computer LaEbratory,
Urbana. III. Nov 59. Contract AT(11-1)-415.
40p. Order from LC. Mi $3. 00. ph $6. 30.
TID-5972
Letter report no. 14 under AEC contract AT(30-1)
2298, byD. W. Rudd. Metal Hydrides, Inc.,
Chemical Research Laboratory. Beverly, Mass.
June 60. lOp. OrderfromLC. Mi $1.80,
Ph$l.80. TID-5982
Informal letter progress report, April 1960. Syl-
vania-Corning Nuclear Corf»ratinn, Bayside, N.
1960. 12p. Order from LC
Mi $2.40, ph$3.30.
TID-5985
TTiennal and structural studies of Ta-^H, Ta^D,
^1% DyCos and the Dy-H, "ft-fl, Ho-H, Yb-H
andlCCl-KBr systems. Annual report covering
flie^riod May 15 1959 to May 15, 1960 on amjli
cation of chemical thermodynamics and relatea
Phenomena to the study of alloy formation, lay"
w. E. Wallace. University of Pittsburgh. Pa.
June 60. Contract AT(30-l)-647. 35p. Order
from LC. Mi $3.00, ph $6.30. TID-6038
Absolute grain boundary energies in copper, by R. L.
Fleiscner. Massachusetts Institute of Technology,
Metals Processing Laboratory, Cambridge. Mass.
1959. Contract AT(30-1)-1310. 5p. Order from
LC. Ml $1.80. ph$1.80. TID-6120
Easy glide of lead single crystals, by R. L. Flelsche
Cher. Massachusetts Institute of Technology,
'■ Meuls Processing Laboratory, Cambridge. Mass.
1960. Contract AT(30-1)- 1310. 16p. Order
from LC. Mi $2. 40. ph $3. 30. TID-6121
Investigation of factors controlling the mechanical
properties of alloys. Seventeenth technical re-
port, by K. Kennedy and E. R. Parker. iJniver-
•Ity of California. Materials Research Labora-
tory, Berkeley. Calif. May 60. Contract AT
(ll-l)-34. 17p. OrderfromLC. Mi $2.40,
ph $3. 30. TID-6128
Summary technical report for the period January 1,
1955 to March 31, 1955, byj. w! Simmons.
National Lead Company of Ohio, Cincinnati, Ohio.
Apr 55. Decl. June 18, 1960. Contract AT
(30-l)-1156. 170p. Order from OTS. $1.10.
TID-10112
Production of high purity yttrium. Monthly progress
report for July 1 to August I 1958. Bureau
of Mines. Northwest Electrodevelopment Experi-
ment Sutlon, Albany, Oreg. 1959. Changed
from OFFICIAL USE ONLY July 31, 1959. Con-
tract AT(ll-l)-599. 9p. OrderfromLC.
Mi $1 . 80, ph $1 . 80. USBM-U-476
ment Station, Albany, Oreg. 1959. Changed
from OFFICIAL USE C»JLY July 31, 1959. Con-
tract AT(1 1-1)- 599. 1^. Order from LC.
Ml $2.40, ph$3.30. USBM-U-494
the Interior, Bureau of Mines, Region 1, Albany
Metallurgy Research Center, Albany, Oreg.
1960. Contract AT(ll-l)-599. 23p. Order from
OTS. $1.00. USBM-U-761
Current beryllium literature: A selected bibliog-
raphy, January 1958- August 1959, by Z. D. Lane.
University of California. Lawrence Radiation
Laboratory. Li»ermore. Calif. Sep 59. Contract
W-7405-eng-48. 33p. Order from LC. Mi $3. 00.
ph$6.30. UCRL-5705
369
iii
Eutectic-diffusion-boodlng of plate-type fuel ele-
ments containing ceramic tuel, by R. A. Wolfe
and others. Westinghouse Electric Corporation,
BettiA Atomic Power Laboratory, Pituburgb, Pa.
Oct 60. Contract AT-11-1_GEN-14. lllp.
Onter from OTS. $2.25. WAPD-211
Measurement
I the thermal conductivity of metal-
clad uranium oxide rods during irramation. by
I. Cohen and others. Westinghouse Electric
Company, Bectia Atomic Power Laboratory,
Pittsburgh, F$. Aug 60. Contract AT-U-ICXN-
U. 49p. Oider from OTS. $1.00.
WAPD-228
Oider
Interim report <^ miniature motor tube teats, by K.
Jackobson aod B. Rau. Westinghouse Electric
Corporation. Bettis Atomic Power Division, Pitts-
burgh, Pa, Oct 58. 34p. Order from LC.
Mi $3. 00, pH$6.30. WAPD-CTA(MEE)-615
Second interim report on testing of miniature niotor
tubes, by E. Rau and K. Jakobaon. Westinghouse
Electric Cor^wration, Bettis Atomic Power Divi-
sion, Pittsburgh, Pa. Nov 58. 17p. Order from
LC. Mi $2.40, ph$3.30.
WAPD-CTA(MEE)-645
An evaluation of
etch for Zir(;aloy-2, by 1^
the sulfuric acid -sodium nitrite
Kass.
w>^». .w. ^.^,^.~j -, -, -. Westin^KHise
Electric Corporation, Atomic Power Division,
Pittsburgh. P». Feb 54. Decl. March 28, 1960.
Contract ATr 11 -1 -GEN- 14, I3p. Order from
OTS. 25ceitts. WAPD-MDM-2<Rev.)
edts.
The extrusion Of a control rod cruciform shape from
Zircsloy-1. by ]• Haiapat/. Westinghouse Elec-
tric Corporation, Atomic Power Division, Pitts-
burgh, Pa. May 54. Decl. with deletions April
30, 1957. Qontract AT-ll-l-GEN-14. 8p.
Order from ^C. Mi $1.80, ph $1.80.
WAPD-MDM-6(Del.)
Bottom support welding feasibility
R. A. Cooper and A. v.
CSMl2^
rest report, by
test.
Smocer.
Includes appendix I: Procedure for welding PWR
core II bottom support welding mockup, by E. E.
Callen. Westinghouse Electric Corporation,
Atomic Pow4r Division. Pittsburgh, Pa. [1958].
36p. Order from LC. Mi $3. 00. ph $6. 30.
WAPD-PWR(RD2)378
Zirconium ingoits ARC melted from various types of
zirconium s^rap. by E. S. Foster and W. J. Hur-
ford. Westinghouse Electric Corporation, Atomic
Power Division, P nsburgh. Pa. Nov 51. Decl.
February 16, 1960. Contract AT-ll-l-GEN-14.
Production <rf plate from crystal bar hafnium, by
— W.J. HurfordandR. J. McClintick. Westing-
house Electric Corporation, Atomic Power Divi-
sion, Pittsburgh, Pa. May 53. Decl. with dele-
tions May 3. 1957. Contract AT-11-1-GEN~14.
Up. Order from LC. Mi $2.40. ph $3.30.
WAPD-RM-181(DeI.)
Further work on the diffusion of Krypton-85 from
uranium dioxide powder, by A. B. Auskern.
Westln^ouse Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburgh, Pa. Aug 60. Ow-
tract AT-ll-l-GEN-14. 12p. Order from OTS.
50 cents. WAPD-TM-225
Zirconium highlights. Westinghouse Electric Cor-
8p. OrcterlromLC. Mi $1.80
ph$1.80.
WAPD-RM
96
high
1, Be
poration, Bettis Atomic Power Laboratory, Pitta-
burgh, Pa. Jan 60. Contract AT-ll-l-GEN-14.
20p. Order from LC. Ml $2. 40. ph $3. 30.
WAPD-ZH-22
Uranium alloy newsletter no. 5, by D. W. Ullle.
Division of Research, Atomic Energy Commisaion,
Nov 53. Decl. February 16, I960. 35p. Order
from LC. Mi $3. 00, ph $6. 30. WASH-126
Uranium alloy newsletter no. 7, by D. W. Ullle.
Division of Research, Atomic Energy Commission.
May 54. Decl. with deletions December I, 1959.
6lp. Order from LC. Ml $3.90, ph $10.80.
WASH-l54(Del.)
Uranium alloy newsletyr no. 8. by D. W. Lille.
Division of Research, Atomic Energy ConumssioB.
Aug 54. Decl. October 7, 1959. 66p. Order
from LC. Ml $3.90, ph $10.80. WASH-155
Uranium alloy newsletter no. 12, by E. Epremian.
Division of Research, Atomic Energy Commissla.
Oct 55. Decl. March 30, 1960. 50p. Order
from LC. Mi $3. 60, ph $9. 30. WASH-199
Minutes of the sixth annual AEC welding committee
meeting, Oak Ridge National Laboratory, Septem-
ber 25-26, 1956. Division of Reactor Develop-
ment, Atomic Energy Conrunission. Apr 57.
Decl. November 23, 1959. Part I - 2l0p and
Part II - 276p. Order from LC. Total price
Mi $11. 10, ph $37.80. WASH -7 33 (Pt. I k2)
Thermoelectric nuclear fuel elen^ent progress re-
port no. 19, byC. R. Kilp and others. Westing-
house Electric Corporation, Atomic Power Depart-
ment, Pittsburgh, Pa. Feb 60. Contract AT(30-
^)-500. 23p. Order from LC. Mi $2.70, ^
ph$4.80. WCAP-1380
370
Thermoelectric nuclear fuel element Quarterly prog-
resa report- -January to March, 1960, by W. P.
Blankenship and others. Westinghouse Electric
Corporation, Atomic Power Department, Pitts-
burgh, Pa. Apr 60. Contract AT(30-3)-500.
58p. Order from OTS. $1.50. WCAP-1545
Dynamic screening corrosion tests of yankee mate-
rials of construction in high temperature boyated
water, by A. Krieg. Westinghouse Electric Cor-
poradon. Atomic Power Department, Pittsburgh
Pa. Jan 59. Contract AT(30-3)-222. 6lp. Or-
der from LC. Mi $3. 90, ph $10. 80.
YAEC-116
Atomic Power Department, Pittsburgh, Pa. Sep
59. Contract AT(30-3)-222. 68p. Order from
LC. Mi $3. 90, ph$10.80. YAEC-153
Fabrication of a silver-indium-cadmium alloy con-
trol rod for the yankee critical experiments, by
J. R. Dazen. Westinghouse Electric Corporation,
Atomic Power Department, Pittsburgh, Pa. Feb
60. Contract AT(30-3)-222. 25p. Order from
LC. Ml $2.70, ph$4.80. YAEC-156
Nuclear Explosions — Peaceful
Applications
Preliminary report operation HARDTACK, Phase II.
Summary report of strong motion measurements,
underground nuclear detonations, by W. M.
Adams and others. Defense Atomic Support
Agency and U. S. Atomic Energy Commission,
Washington, D. C. May 60. 80p. Order from
OTS. $2.00. lTR-1711
Peaceful uses of nuclear explosions. A literature
aearch, by H. E. Voress. Technical Information
Service Extension, Oak Ridge, Tenn. Apr 60.
ip. Order from OTS. SO cents.
TID-3522(3rd. Rev.)
Peaceful uses of nuclear explosions. A literature
search, by H. E. Voress. Technical Information
Service Extension, Oak Ridge, Tenn. Nov 60.
Up. Order from OTS. 50 cents.
TID-3522(4th Rev.)
CoBM)letion report project Chariot -Phase II,
ware program U. S. Atomic Energy Commission
Plow-
Cape •Thompson Area, Alaska. Holmes li Nar-
wr, Inc. . Los Angeles, Calif. 1959-1960.
Contract AT929-2)-20. 62p. Order from OTS.
tl.50. TID-5928
Completion report project Plowboy . Plowshare
- ram. Holnties and Narver, Inc. , Los Ange les ,
progra
Mr
■3ep60. Contract AT(29-2)-20. 30p.
Order from OTS. 75 cents. TID-6602
The community impact of peaceful applications of
atomic energy, by H. Sandbank. The American
Municipal Association, Washington, D. C.
Mar 60. 80p. Order from OTS. $1.00.
TID-8202
Excavation with nuclear explosives, by G. W. John-
son. University of California, Lawrence Radi-
ation Laboratory, Livermore, Calif. Nov 60.
Contract W-7405-eng-48. 30p. Order from OTS.
75 cents. UCRL-5917
Structural response and permanent displacement
measurements, by R. H. Sievers, Jr. and others.
Headquarters Field Command, Defense Atomic
Support Agency, Sandla Base, Albuquerque,
N. Mex. Oct 60. 218p. Order from OTS.
$3.00. WT-1708
Particle Accelerators and High-Voltage
Machines
Particle extraction III, by K. W. Robinson. Cam-
bridge Electron Accelerator, Mass. I^eb 59.
I3p. Order from LC. Mi $2. 40, ph $3. 30.
AECU-4509
Transient magnet response in the operation of the
A. G.. S. , byL. J. Laslett. Brookhaven Nation-
al Laboratory, Upton, N. Y. Aug 55. 26p.
Order from LC. Mi $2.70, ph $4.80.
BNL-4633
Linear accelerator drift tube support, by L J. Polk.
Brookhaven National Laboratory, Upton, N. Y.
Feb 56. lOp. Order from LC. Mi $1.80,
ph$1.80. BNL-4634
Estimate of radiation levels for the MURA 50 MEV
electron accelerator, by W. Smith. Midwestern
Universities Research Association, Madisoo.
Wis. Sep 59. Contract AT(ll-l)-384. 8p.
Order from LC. Mi $1.80, ph $1.80.
MURA-507
Use of an electrolytic tank, by C. D. Curtis and
R. E. Rothe. Midwestern UolversltleB Research
Association, Madison, Wis. Nov 59. Contract
AT(ll-l)-384. 15p. Order from LC. Mi $2.40,
ph$3.30. MURA-531
371
i
4
c
t
t
Magneto- gravitational effects
tors, by L '" ' ""
_^ in particle accelera-
W. Jones and A. M.
Sessler.
Wld-
western UAlversitles Research Association, Madi-
son. Wis. Apr 60. Contract AT(1 1-1)- 384. 8p.
Order froiti LC. Mi $1.80, ph $1.80.
MURA-537
Magnetic fie l(j calculatlona using distributed currenu,
by S. C. Spowdon. Midwestern Universities Re-
aearch Association, Madison, Wis. Jan 60.
Contract AT(ll-l)-384. Up. Order from LC.
Mi $2. 40, j)h $3. 30. MURA-553
High energy yutrino e^qperiments witfi a higti inten-
sity FFAG' accelerator, by K. R. SymonT Mid-
western Universities Research Association,
Madison, Wis. Jan 60. Contract AT(11- 1)- 384.
lOp. Orxktr fK> m LC. Ml $2. 40, ph $3. 30.
i MURA-554
Electromagn^c fields in a donut space, by W
N.
Wong. \<itlwe8tern Universities Research Asso-
ciation, Mfdision, Wis. Jan 60. Contract
AT(11-1)-: 84. 26p. Order from LC. Mi $2.70,
ph$4.80. MURA-555
Some notes q the kinematics of high energy nucleon-
idwe
nucleon collisions, by S. P. Rosen. Midwestern
Universities Research Association, Madison,
Wis! Mar60. Contract AT(11 -I)- 384. 30p.
Order from LC. Mi $2.70, ph $4.80.
MURA-563 4
Schwarz-Chrjatoffel tranflformations pertaining to
magnet e<j^8 or peelers, by L. J. Laslett. FTid-
western Uliversities Research Association,
Madison, Wis. Apr 60. Contract AT(ll-l)-384.
17p. Order from LC. Mi $2. 40, ph $3. 30.
MURA-567
Linear oscillttlons about off-center, fixed point
orbits, byM. M. Gordon. Midwestern Univer-
sitles Research Association, Madison, Wis.
[nd]. Contract AT(ll-l)-384. 1^. Order from
OTS. 50 cents. MURA-589
A neutrino beam design, by L. W. Jones. Mid-
western Utiiversities Research Association,
Madison, Wis. Aug 60. Contract AT(ll-l)-384.
lOp. Ord^r from OTS. 50 cents. MURA-590
rddr
Reiaxation ci^culatloo of integral scaling magnetic
fields produced by dlstribuoed currents, by S. C.
Snowdon. Midwestern Universities Research
Associatldi, Madison, Wis. Oct 60. Contract
ATXll-l)-te4. i2p. Order from OTS. 50 cents.
MURA-591
A proposal for the study of long-time association,
by G. Parzen. Midwestern Universities Re-
search Association, Madison, Wis. Oct 60.
Contract AT(ll-l)-384. 6p. Order from OTS.
50 cents. MURA-592
Quarterly
period 1
report of the laboratory director for the
period January 1 1960 to March 31. 1960. Mid-
western Universities Research Association,
Madison, Wis. June 59. 5p. Order from LC.
Mi $1.80, ph $1.80. . TID-5784
HI A current electron accelerator, by N.Chris tofiloi
iJniversity of California. Lawrence Radiation
Laboratory, Livermore. Calif. Jan 59. Changed
from OFFICIAL USE ONLY February 15, 1960.
23p. Order from LC. Mi $2.70, ph $4.80.
UCRL-5463-T
A radlofrequency separator for high-energy parti-
cles, by M. L. Good. University of Cali/ornia.
Lawrence Radiation Laboratory, Berkeley, Calif.
Oct 59. Contract W-7405-eng-48. 19p. Order
from LC. Ml $2. 40, ph $3. 30. UCRL-8929
ScHne problems in planning for future high energy
proton accelerators, by D. L. Judd. University
of California. Lawrence Radiation Laboratory,
Berkeley, Calif. Jan 60. Contract W-7405-eng-
48. 17p. Order from LC. Mi $2.40, ph $3.30.
UCRL-9WI
Physics and Mathematics
The mechanism al the direct interaction process at
Intermediate energies, by R. J. Griffiths and
R. M. Eisberg, university of Minnesota. Schoi
of Physics, Minneapolis, Minn. [1958]. 24p.
Order from LC. Ml $3.70, ph $4.80.
AECU-4311
Relativistlc self-consistent calculation for the iroa
atom, by S. Cohen. RAND Corporation, Sanu
Woiilca, Calif. June 59. Contract AT(1 1- 1)- 135.
24p. Order from LC. Mi $2.70, ph $4.80.
AECU-4342
Annual research report. Massachusetts Institute
of Technology, Laboratory of Chemistry and
Solid-Sute Physics, Cambridge, Mass. July S>.
69p. Order from LC. Mi $3.90, ph $10.80.
AECU-4348
Measurements of average heat-transfer coefficlena
for helium and hydrogen flowing in smooth tantiF
um tubes at high surutce temperatures, by tL[.
372
Newman. Loe Alamos Scientific Laboratory,
N.Mex. [19591. Contract W-7405-eng- 36. 26p.
Order from LC. Mi $2.70, ph $4.80.
AECU-4507
Ideal gas thermodynamic properties of detonation
products, by C. L. Mader. Loe Alamos Scien
tic Laboratory, Los Alamos, N. Mex. Sep 59.
206p. Order from LC.
Mi $9. 30, ph $31.80.
ABCU-4506
Tbermodynamic properties of detonation products,
by C. L. Mader. Loe Alamos Scientific Labora-
tory, Los Alamos, N. Mex. Apr 60. 57p. Or-
der from LC. Mi $3. 50, ph $9. 30.
AECU-4508(Suppl)
Finite amplitude stress waves in rocks, by D. R.
Grine. Stanford Research Institute, Poulter
Laboratories, Menlo Park, Calif. Oct 59. 64p.
Order from LC. Mi $3. 90, ph $10. 80.
AECU-4518
Technical progress report. Part 1 High-speed
ccanputer program. Part II. Mathematical
ethods. Part III. lUiac use and operation.
met ^
Part IV. IBM 650 use and operation. PaTTV.
General laboratory informatipn. University of
Illinois. Dlgiul Computer Laboratory, Urbana,
HI. July 59. Contracts AT(ll-l)-415 and Nonr-
1834(15). 22p. Order from LC. Ml $2.70,
|)l»$4.80. AECU-4531
Technical progress report. Parti. High-speed
computer program. Part 11. MadtenaticaTmeth-
o^. Part III. Illiac use and operation. Part IV.
BM 650 use and operation. Part V. General
laboratory information. University of Illinois.
Dlgiul Computer Laboratory, Urbana, 111. Aug
59. Contracts AT(ll-l)-415 and Nonr- 1834(15).
36p. Order from LC. Mi $3. 00, ph $6. 30.
AECU-4532
A fast hyperfragment produced by a heavy primary
cosmic ray. Dy U. Gamer ini and others. Univer-
sity of Wisconsin, Madison, Wis. [1959]. Con-
tract AT(ll-l)-64. 3p. Order from LC.
Ml $1.80, ph$1.80. AECU-4533
Diffusion in a temperature
^ adlcnt.
.oehler.
imperar
report no. 16, by J. S7 , _
Illinois, Urbana, 111. June 59. Contract AT(11-1)-
182. 1(^. Order from LC. Mi $1.80, ph $1.80.
Technical
University of
AECU-4534
j^ low energy photodisintegratlon of % and ^He
Md neutron -deuteron scattering,
Massachusetts Institute of Tedmology, Labors
photodis Integra
oeuteron scattering, by L. M. Delves.
te of Tec^ology, Laboi
tory for Nuclear Science, Cambridge, Mass.
[1959]. Contract AT(30-l)-2098.
from LC. Ml $2. 40, ph $3. 30.
18p. Order
AECU-4565
Research and investigation leading to methods of
enerating and delecting radiation in the 100 to
000 micron wavelength range of the spectrum.
Quarterly progress report iw- 15 for September
1 to December 1, 1959. by P. D. Coleman and
odiers. University of Illinois, Electrical Engln
neering Research Laboratory, Urbana, 111.
Jan 60. Contract AT(ll-l)-392. 6ip. Order
from LC. Mi $3. 60, ph $9. 30. AECU-4661
Low energy nuc tear physics. Second annual report
for the period February 1. 1959 to January 31,
1960, by P. S. Jastram. Ohio State University.
Research Foundation, Columbus, Ohio. Jan 60.
Contract AT(ll-l)-605. 122p. Order from LC.
Ml $6. 30, ph$I9.80. AECU-4675
The snap-II power conversion system. Topical re-
port no. 4. Turbine design and testing, by E. W.
Poulos and E. R. Furman Thompson Ramo
Wooldridge Inc. , Cleveland, Ohio. Jan 60. Coo-
tract AT- 1 1 - 1 -GEN -8 , 73p. Order from LC.
Ml $4. 50, ph $12. 30. AECU-4686
Time variation of thermodynamic parameters of a gas
in the regicw of a shock front. Progress report
no. Ill, by E. J. Eastmond and others. Bri^iam
Voung University, Provo, Utah. Nov 59. Con-
tract AT(04-3)-67. 59p. Or^r from LC.
Mi $3. 60. ph $9. 30. AECU-4687
The application of nuclear energy to agriculture,
Anniial report. Inter -Anaer lean Institute at
Agricultural Sciences. Turrialba, Costa Rica.
Mar 60. Contract AT(30-l)-2043. 50p. Order
from LC. Mi $3.30, ph $7.80. AECU-4731
Physics division summary report for July - Au;
1960, by M. Hamermesh. Argonne Nationa,
Laboratory, Argonne, 111. 1960. Contract W-
31-109-eng-38. 21p. Order from OTS. 75 cents.
ANL-6190
Thermal stresses in concentrically heated hollow
cylinders. Supplemenul data on coefficients ct
therniar" expansion, naodulus of eleastlcity and
poisson's ratio as functions of temperatvure, by
J. C. Heap. Argonne Natinaal Laboratory,"
Argonne, 111. Oct 60. Contract W-31-109-eng-
38. 38p. Order from OTS. $1.00.
ANL-6224
Bubble chaniber safety meeting, by J. M. Harrer.
Argonne National Laboratory, Argonne, 111.
June 60. Contract W-31-109-eng-38. 18p.
Order from OTS. 50 cents. ANL-6225
373
Multlgroup diffuaton theory formulation of die c«lcul-
ation (X the mean aqua re plowing down distance
in an infinite naedium. by B. ]. ToppeT. Argoone
Naciooal LaboratoryT Argonne, 111. Oct 60.
Contract W- 31 • 1 09-eng- 38. 1^. Order from
oris. SO cents. ANL-6226
Special lectures on d>e phys
tor analysis, liy P. J. Pe
al Laboratory, Argoone,
W-31-l09-cng^38. 40p.
91.00.
ical foundation of reac-
rsiani. Argoone Nation -
111. Oct 60. Contract
Order from OTS.
ANL-6227
The fission energetics at Th^^, by A. B. Smith and
ocfaers. Argonbe Natiooal Oburatory, Argoone,
111. Nov 60. (toatractW-31-109-eng-38. 20p.
Order from OUS. SO cents. ANL-6247
Reflector and prcMure vessel oaollng and thermal
stress analysia on the BM 650, by J. D. Love
and R. L. Catdn. Alco Products, Inc. , Schenec-
tady, N.Y. N^r 59. Contract AT(30- 3)- 326.
37p. Order fr^m LC. Mi $3.00, ph $6. 30.
APAE Memo- 184
Nuclear data tape program (fflM 704 Program NDTP),
by K. A. Paine. General Electric Co", Aircraft
Nuclear Propulsion Department, Cincinnati, Ohio.
Dec 57. Contracts AF 33(600)- 38062 and AT
(11-1)-171. 30p. Order from OTS. 75 cents.
APEX -574
Table of gamma -rttys emitted by radioactive nuclei.
Arranged in oiider of increasing energy, by E7~
der Mateosian and M. McKeown. Brookhaven
National Laboratory, Upton, N. Y. May 60.
24 p. Order ffom OTS. $3.00.
BNL 605 (T-177)
Neutron cross section evaluation group. Newsletter
no. 1, June 196lD, by R. Sher and S. Moore.
Brookhaven National Laboratory, Upton, Long
Island, New Yo^. June 60. 6p. Order from
OTS. SOoenui BNL-607 (T-178)
A study of Ae wln^ profile in the lowest 400 teet ct
the atmosphere. Progress report no. 6, January
16. l»y to May 15, ft60, byl A. Singer and
L. J. Tick. Bnxikhaven National Laboratory,
Upton, Long Island, N. Y. 12p. Order from
OTS. 50 cents. BNL-615 (T-184)
Neutron cross aeciion evaluation group. Newsletter
no. 2, October'1960, by S. Moore and others.
Brookhaven National Laboratory, Upton, Long
Island, N. Y. Oct 60. 8p. Order from OTS.
50 cents. BNL-634 (T-197)
Vapor pressure-of the Bl-Bilo system. P^^o<j^ 55>vcr-
ed: November 1, 1951 to September 30, 1952,
by R. L. Von Berg and W. A. Chantry. Cornell
University, Ithaca, N. Y. 1952. Decl. June 24,
1959. Contract AT- 30- 2 -GEN -16. 29p. Order
fromLC. Mi $2.70. ph $4.80. BNL-4I52
Preliminary desim report for the NMSR pressurized
water loop at 5rR, by L. T. Dudley and others."
Oak Ridge, National Laboratory, Oak Ridge, Tenn.
Oct 58. 4ip. Order fromLC. Mi $3. 60,
ph$9.30. .^. CF-58- 10-21
The fast flf«ioo factor, by G. R. Hoke. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Sep 59.
46p. Order from LC. Ml $3.30. ph $7.80.
, .. CF-59-9-6I
Tliennal ^frxk of HRT flanges, by P. P. Holz. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Sep 59. Contract W-7405-eng-26. 9p. Order
fromLC. Mi $1.80, ph $1.80. CF-59-9-114
I IBM-704 code for studying particle orbits In cy-
clotron fields, by H. C. Owens and T. A. Welton.
Oak Ridge National Laboratory, Oak Ridge, Tenn.
Nov 59. Contract W-7405-eng-26. 113p. Order
fromLC. Mi $6.00. ph $18.30. CF-59-11-3
EGCR coolant purlflcatloo. Treatnynt of buffer
helium fronii water or oil seals, by P. A. Haas
and C. D. Scott. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Jan 60. Up. Order from LC.
Mi $2.40. ph$3.30. CF-60-1-46. 2nd.
Bumiq) of beryllium by fast neutron reactions, by
A. M. Perry. Oak Ridge Nadonal Laboratory,
Oak Ridge, Tenn. Jan 60. 3p. Order from LC.
Mi $1.80. ph $1.80. * CF-60-1-56
Protection of space vehicles from meteorite penetn-
tion, by R. J. Hefner and P. G. Lafyatis. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Jan 60. 28p. Order from LC. Mi $2.70,
ph$4.80. CF -60- 1-67
Some conunents on the ioffe experiment, by A.
Simon. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Jan 60. Contract W-7405-eng-26.
13p. Order fromLC. Mi $2.40, ph $3. 30.
CF-60-1-72
[BM-704 Gaussian- integration routines, by M. P.
Lietzke. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Mar 60. 12p. Order from LC.
Ml $2.40, ph $3. 30. CF-60-3-48
374
Polflt, A 704 program for polynomial least s
fitting, byM. H. Lietzke and M. P. LietzKe.
res
Oak Ridge National Laboratory, Oak Ridge. Tenn.
May 60. 16p. Order from LC. Mi $2.40,
ph$3.30. CF-60-3-129
Progress repoi^ for July, August, September 1959
to the United Stttes Atoniic Energy Commission,
Columbia University, Pegram Nuclear Physics
Laboratories, New York, N. Y. 1959. Cootract
AT-30-1-GEN-72. SOp. Order from LC.
Mi $3. 30, ph $7.80. CU(PNPL)-199
Determ
termination of -^^ by comparison of yO;
and Pu^^^ with f g- for 0^' in a flux
for U
233
cal assembly, by R. Gwin and D. W. Magnuson
Oak Ridge National Laboratory, Oak Ridge, Tenn
Apr 60. Contract W-7405-eng-26. 16p. Order
fromLC. Mi $2. 40, ph $3. 30. CF-60-4-11
A simple formula for computing fission product
thermal cross sections and resonance integrals,
by C. W. Nestor. Oak Ridge National La&ra-
tory. Oak Ridge, Tenn. Apr 60. 1^. Order
fromLC. Mi $2.40, ph $3.30. CF-60-4-30
GAP: The IBM 704 ^id analysis program, by F. J.
Witt. Oak Ridge National Laboratory, Oak Ridge,
Tenn. May 60. Contract W-7405-eng-26. 18p.
Order from LC. Mi $2. 40, ph $3. 30.
CF-60-4-69
I,
Neutron thermalfzation and diffusion in pulsed media,
by S. N. Purohit. Oak Kidge National Laboratory.
Oak Ridge , Tenn. July 60. Contract W-7405-
eng-26. 45p. Order from LC. Mi $3. 30,
ph$7.80. CF-60-7-32
Time-dependent thermal -neutron energy spectra
in a monoatomic heavy gas, by S. N. Purohit.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. July 60. 36p. Order from LC. Mi $3. 00,
ph$6.30. ; CF-60-7-44
Progress report for April, May, June 1959 to the
United States Atomic Energy Commission.
Columbia University. Pupin Cyclotron LaEbratory
and George B. Pegram Laboratory, New York,
N. Y. 1959. Contract AT- 30-1 -GEN-72. 58p.
Order from LC. Ml $3. 60, ph $9. 30.
CU-194
trap criti- Nuclear elecarii
lie transitions in O^^, Ca^,
ments of the electromagnetic radiations frcwn
Intermediate image pair spectrometer naeasure-
iiectromagr
some light nuclei, by K. E. Eklund. Department
of Physics, Columbia University, New York,
N.Y. May 60. Contract AT(30-l)-GEN-72.
112p; Order from O're. $2.50.
CU(PNPL)-196
The neutrino- -a contribution to the memorial volume
to Wolfgang Paull, by C. S. Wu. Columbia Uni-
versityr Pupin Cyclotron Laboratory, and George
B. Pegram Laboratory, New York, N. Y. June
60. Contract AT- 30-1-GEN-72. 105p. Order
fromLC. Mi $5.70, ph $16.80. CU-197
clear elecoric jnonopole transitions in O^^, Ca^,
"Se^^ and Zr^", by U. Nessin. Columbia Univer-
sity, Department of Physics, New York, N. Y.
May 60. Contraa AT(30-l)-GEN-72. 93p.
Order from OTS. $2.25. CU(PNPL)-201
IBM 650 routine VI temperature distribution in fuel
elements, by J. C. Jensen. E. L du Pont de
Nemours li Company, Ejq)loelves Department.
Atomic Energy Division, Technical Uivisioo.
Savannah River Laboratory, Aiken, S. C. .
Sep 60. Contract AT(07 -2)- 1. 48p. Order from
OTS. $1.25. DP-512
Reactor stability, by D. S. St. John. E. L du Pont
de Nemours h Company, Explosives Department,
Atomic Energy Division, Technical Division,
Savannah River Laboratory, Aiken, S. C. Sep
60. Cootract AT(07- 2)- 1. 88p. Order from
OlS. $2.00. DP- 517
Long-w>.elengtfa beam inatabllity. M. N. Rosen-
bluth. General Atomic Division, General Dy-
namic Corporation, San Diego, Calif. Apr 60.
14p. Order from LC. Mi $2.40, ph $3. 30.
GA-1376
Safe
geometyies and tnass at assays be low five per
cent U^-^, byj. L. Feuerbacfaer. Cxxlyear
Atomic Corporation, Portsmouth, Ohio. May 59.
9p. Order fromLC. Mi $1.80, ph $1.80.
GAT-DM-769
IBM
program for fitting data to simple eroonec
curves of the form y = ab*, by T. B. Pattei
intial
curves "of the form y = ab*, by t. B. j^atterson.
Goodyear Atomic Corporation, Portsmouth, Ohio.
Nov 59. 4p. Order from LC. M^$1.80,
ph$1.80. GAT-DM-788
Likelihood ratio test, by D. L. Thomas. Goodyear
Atomic Corporation, Portsmouth, Ohio. Mar 60.
bp. Order fromLC. Mi $1.80. ph $1.80.
GAT-DM-821
Absorption correction calculation, by D. L. Th<»nas.
Goodyear Atomic C-orporation, Portsmouth, Ohio.
Apr 60. 13p. Order fromLC. Mi $2.40,
ph$3.30. GAT-DM-829
Performance -- two-phase pressure drop, burnout,
and hydraulic oscillation of an inclined tesT
375
section with net aoeam generaoon at 1000 PSIA.
by S. Levy and C. L. Swan. General Electric
Company, Atomic Power Equipment Department,
San Jose. Calif, iug 59. Contract AT(04- 3)-
189. PA#5. 25p. Order from OTS. 50 cents,
GEAP-3228 (Rev. 1)
Method for analyzing low -enrichment light-water
cores. Supplementary study related ^o BONUS
and nuclear superheat programs, by R. W.
Deutsch. General Nuclear Engineering Corpora-
tion. Dunedin. Fl$. Oct 60. Contract AT(40-1)-
2674. 43p. Ordear from OTS. $1.00.
GNEC-133
Physics Unit - Appliyi researcy subsection techni-
cal activities report for April 1953. by). E.
Faulkner and others. General Electric Company.
Hanford Atomic Ptrducts Operation, Richland,
Wash. May 53. Decl. March 3. 1960. 15p.
Order from LC. jMi $2. 40. ph $3. 30.
HW-27921
The resonance escape probabiliry of thorium slugs,
by G. W. Stuart. Jr. and R. K. Cole. General
Electric Compenjt, Hanford Atomic Products
Operation. RichUnd, Wash. Aug 54. Decl.
February 6, 1956^ 3p. Order from LC.
Mi$1.80. Dhll.lO. HW-32672
ph$l.lO.
The medwd trfsucccBSive generations, by G. W
Stuart and R. W. j Woodruff. Hanford Atomic
Products Operati<>n, Richland, Wash. Jan 55
Decl. August 18
1960. Contract W- 31 -109-
Eng-52. 38p. Oirder from OTS. 40 cents.
HW-33566 REV
Resonance capture (jf neutrons in naeul and oxide
General Electric
cylinders, by M. V. Davis,
dompany, Hanfotjd Atomic Products Operation,
Richland. Wash. ( July 55. Decl. June 10. 1960.
9p. Order from LC. Mi $1.80, ph $1.80.
HW-38235
Fading effect in Eastman NTA emulsion, by E. C.
Watson. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Mar 57. 5p. Order from LC. Ml $1.80,
ph$1.80. r HW-49444
Effects of in-reacti(^ test loops on PRTR (^ration
Peterson. General
and program, by R. E.
E lectr i c Compa ny , Hanford Atomic Products
Operation, Richland, Wash. Mar 59. Contract
W-31-109-Eng-52. 15p. Order from LC.
Mi $2. 40. ph $3. 30. HW-59691
Neutron age in graphite-water lattices, by D. E.
SimpsOTi. denetal Electric Company. Hanford
Atomic Product Operations, Richland, Wash.
Oct 59. Contract AT(45-1)-1350. 3p. Order
fromLC. Mi $1.80, ph $1.80. HW -62501
Equations of state for steain-water mixtares and
some representative applications analysis, by
W. J. Love. General Electric Company, Han-
ford Atomic Products Operation, Richland, Wash.
Apr 60. 23p. Order from LC. Ml $2.70,
ph$4.80.-. HW-62858 (Rev. I)
Statistical interr
models, by R.
tlon of data for alternative
Basmann and L. G. Waters.
General Electric Company, Hanford Atomic
Products Operation, Richland. Wash. May 59.
79p. Order from LC. Mi $4. 50, ph $12. 30.
HW-SA-1706
Fission product release from heated uranium
— (thesis), by R. K. Hilliard. General Electric
Company. Hanford Atomic Products Operation,
Richland, Wash. 1960. Contract AT(45-1)-
1350. 64p. Order fromLC. Mi $3. 90.
ph$10.80. HW-SA-1836
Coordinates for calculating vibrational frequencies
in chain molecules. byH. L. McMurry. ~
Phillips Petroleum Company , Atomic Energy
Division, Idaho Falls, Idaho. Aug 60. Contract
AT(10-l)-205. 50p. Order frcMn OTS. $1.25.
IDO- 16605
High-energy potential scattering, by P. J. Lynch.
Ames laboratory, Iowa State University of
Science and Technology. Ames, Iowa. Sep 60.
Contaact W-7405-eng-82. 151p. Order from
OTS. $2.75. IS-203
Report of the nuclear physics section for June,
July, August 1954. Knolls Atomic Power Labor-
atory, Schenectady, N. Y. 1954. Decl. Febru-
ary 24, I960. Contract W-31-109-Eng-52. 55p.
Order from LC. Mi $3.00, ph $6. 30.
KAPL-1210
Almost linearly optimum conibination of unbiased
estimates, oy M. Halperln. General fclectric
Company, Knolls Atomic Power Laboratory,
Schenectady. N. Y. Jan 60. Contract W- 31-
109-Eng-52. 9p. Order from OTS. 50 cents.
KAPL-2068
Digiul computation of space -time variation of neu-
tron fluxes, by E. L. Wachspress. General
Electric Company. Knolls Atranic Power Labora-
tory. Schenecudy. N. Y. Oct 60. Contract
W-31-109-Eng-52. 33p. Order from OTS.
$1.00. KAPL-2090
376
Mlcroacopic effects in multiphase n>ediums (neutron
getf-shielding), by C. H. Randall. Knolls Atom-
ic Power Laboratory, Schenectady. N. Y. May
60. Contract W-31-109-Eng-52. 136p. Order
fromLC. Mi $6.90, ph $21.30.
KAPL-M-CHR-2
SourcelesB surtup--a machine code for computing
low-source reactor startups, by D. B. MacMil-
lian. Knolls Atomic Power Laboratory, Schenec-
day. N. Y. June 60. Contract W-31-109-Eng-52.
23p. Order fromLC. Mi $2.70. ph $4.80.
KAPL-M-DBM-1
The constant-period approximation for numerical
solution of the spaoe- independent reactor kinetics
equations by D. B. MacMillan. Knolls Atomic
Power Laboratory, Schenecwdy, N. Y. July 60.
Contract W-31-109-eng-52. 8p. Order from
LC. Mi $1.80. ph $1.80. KAPL-M-DBM-2
H1Ij0--A steady state reactor analysis program, by
A. E. Kakretz and L. B. Shannon. Knolls Atom -
ic Power Laboratory, Schenectady, N. Y. Apr
60. Contract W-31-109-Eng-52. 108p. Order
fromLC. Mi $5.70. ph $16.80.
KAPL-M-DIG-TD-10
A stability analysis of the finite difference represen-
tation of the energy equation, by D. C. Maxwell.
Knolls Atomic Power Laboratory, Schenectady,
N. Y. May 60. Contract W-31-109-Eng-52.
55p. Order from LC. Mi $3.60, ph $9.30.
KAPL-M-DIG-TD-12
Effective thermal and epithermal fission fragment
absorption cross -sections, by E. C. Hansen and
C. R. Greenhow. Knolls Atomic Power Labora-
tory. Schenectady. N. Y. Oct 59. Contract
W-31-109-Eng-52. 19p. Order from LC.
Mi $2.40. ph$3.30. KAPL-M-ECH-3
An improved generalized analysis of fission frag-
ment poisoning- -thermal and resonance fission
framient cross sections, by E. C. Hansen and
C. R. Greenhow, Knolls Atomic Power Labora-
tory. Schenectady, N. Y. July 60. Contract W-
31-109-Eng-52. 43p. Order from LC.
Mi $3. 30. ph$7.80. KAPL-M-ECH-7
A probability distribution for random grouping of
items from a lot and its use in providing assur-
ance on the percent of defective groups, by M.
Halperln ana G. L. Burrows. Knolls Atomic
Power Laboratory, Schenectady, N. Y. June 60.
Contract W-31-109-Eng-52. I8p. Order from
LC. Mi $2. 40, ph$3.30. KAPL-M-GLB-2
Kare input, by J. A. Archibald, Jr. Knolls Atomic
Power Laboratory, Schenectady, N. Y. Apr 60.
Contract W-31-109-Eng-52. lOlp. Order from
-«-LC. Mi $5.70, ph $16.80.
KAPL-M-JA-6
Kare general mesh data, by J. A. Archibald, Jr.
knolls Atomic Power Laboratory, Schenecudy,
N. Y. May 60. Contract W-31-109-Eng-52.
25p. Order fromLC. Mi $2.70, ph $4.80.
KAPL-M-JA-7
Equations for the WOXX cross -section routine of the
kare system, by J. A. Archibald, Ir. Knolls
Atomic Power Laboratory. Schenectady. N. Y.
May 60. Contract W -31- 109-Eng-52. 6^.
Order from LC. Mi $3.90, ph $10.80.
KAPL-M-JA-8
Utilization of tapes in the kare system, by J. A.
Archibald. J r and others. Knolls Atomic Power
Laboratory, Schenectady, N. Y. June 60. Con-
tract W-31-109-Eng- 52. 16p. Order fromLC.
Mi $2. 40, ph$3.30. KAPL-M-JA-9
Flux peaking formulae for sonne two dimensional
systems, by J. H. Smith. Knolls Atomic Power
Laboratory, Schenecudy, N. Y. Feb 60. 13p.
Order from LC. Mi $2. 40, ph $3. 30.
KAPL-M-JHS-7
Bending stresses in a pressure vessel with an integ-
ral flat bead, by L. Deagle. Knolls Atomic
Power Laboratory, Schenecudy, N. Y. 1960.
Contract W-31-109-Eng-52, 19p. Order from
LC. Mi $2. 40. ph $3. 30. KAPL-M-LD-5
Distributed reactivity coefficiente in a I^A slab
core. Measurement and analysis, by N. E.
French and others. Knolls Atomic Power Labor-
atory, Schenectady, N. Y. Feb 60. Contract
W-31-109-Eng-52. 50p. Order from LC.
Mi $3.30, ph $7.80. KAPL-M-MLS-12
Model and equations for digital analysis of a mixed
natural and forced circulation power plant, by
A. J. Arker and T. R. Greene, Knolls Atomic
Power Laboratory, Schenecudy, N. Y. Mar 60.
Contract W-31-109-Eng-52. 43^). Order from
LC. Mi $3. 30. ph $7.80. KAPL-M-NPA-9
HFC
: An 1^4 704 digiul computer program to cal-
culate heat transfer dau obtained from out -of"
pile tests on fuel elements, by R. D. Burgess
and C. L. Gregory, Knolls Atomic Power Labor-
atory, Schenecudy, N. Y. May 60 . 97p.
Order from LC. Mi $5. 40, ph $15. 30.
KAPL-M-S3G-RES-70
377
Method for determiiiing fuel element »^^<^ *°"'
perature in the hot channel containing bulk ateam
walla film flanke ted with superheayd vapor, by
J. B. Kalinowsku Knolls Atomic Power Labora-
tory, Schenecudir. N. Y. Mar 60. Contract
W-31-l09-Eng-52. I7p. Order from IX.
Mi $2.40, ph $3..30. KAPL-S3G-M-RES-72
A aurvey of small qpre hydrogen moderated reac-
— tors, by W. B. Wright, Jr. Knolls Atomic Power
TlaBoratory, Schenectady. N. Y. Aug 55. Decl.
January 4, 1960. Contract W- 31 -109- Eng- 52.
I5p. Order frortLC. Mi $2. 40, ph $3. 30.
■ KAPL-M-WBW-1
Opacity of air at high
byl Kivelandfl.
altitudes and high tempera tvire,
Kivel and R. Mayer. Los Alamos Scientific
Laboratory, Loa Alamos, N. Mex. Aug 54.
Decl. June 6. 1^60. Contract W-7405-eng-36.
48p. Order froih LC. Ml $3.30, ph $7.80.
LA-1738
A gamma ray sensitive fuel level detector for a
homogeneous retctor, by D. M. Holm. Loe
Alamos Scientifiic Laboratory, Un^fersity of
California, Los Alamos, N. Mex. July 60.
Contract W-740$-ENG-36. 22p. Order from
OTS. 50 cents. J LA-2458
Proposed method o^ measuring thermal diffusivity
f. Ui^k r^r„r,^^«J..^o h«R. D. CowaH. Cos
ol meaaur
a jure, by"
fic Labon
at high tempera.^ w, w, .». ^.
Alamos Scientific Laboratory, University of
California, Los Alamos, N. Mex. Aug 60.
Contract W-740$-ENG-36. 48p. Order from
OTS. $1.25. L\-2460
On the continuum liidiation in ionized gases, by N.
Balazs. Princetion University, Project Matterhorn,
Princeton. N. J. July 60. -eontract AT(30-1)-
1238. 25p. Order from OTS. 75 cents.
MATT- 49
Baltimore, Md. Mar 60. Contract AT(30-3)-
217. 42p. OrdNr from OTS. $1.00.'
MND-P-2316
Nuclear 1 . 0 watt
Final re
•eport
Comp
power supply
Subtask 5.6,
for space application.
6^ by D. J. Knighton.
ubtask
Martin Company. Baltimore Md. June 60.
Contract AT(30r3)-217. 49p. Order from OTS
li 25 MND-P-2354
I
Curium fueled generators for lunar and apace mis-
aions. Prel^nijiary safety analysis report, by
C. 0. Riggs. iiartin Company, Baltimore, Md.
June 60. Contract AT(30-3)-217. 49p. Order
from 013. $1.50. MND-P-2366
13-watt curium fueled thermoelectric generator for
a alx-month apace mission. Final report
SubtaakS.B, by J. Bloom. Martin Company,
Baltimore, Md. July 60. Contract AT(30-3)-2l7.
45p. Order from OTS. $1.25. MND-P-2373
13-watt curium-fueled thermoelectric generator for
hard lunar Impact mis a ion. Final report ' S"S^
taiinrS, by J. Bloom. Martin Comi»ny, Balti-
more, Md. Aug 60. Contract AT(30-3)-217.
50p. Order from OTS. $1.50. MND-P-2374
Report on ahieldfng the MUBA high Intensity SOMev
electron accelerator, by J. H. Smith. Midwes-
tern Universities Research Association, Madison,
Wi8. June 58. Contract AT(ll-l)-384. I5p.
Order from LC. Mi $2. 40, ph $3. 30.
MURA-408
On Sturrock's perturbation theory, by W. N. Wong.
Midwestern Universities Research Association.
Madison. Wis. Jan 60. Contract AT(ll-l)-384.
17p. Order from LC. Mi $2.40, ph $3.30.
MURA-556
Measurenient of zero power frequency response of
theSRE, by J. G. Lundholm. Jr. Atomics Inter-
national. A Division of North American Aviation,
Inc. , Canoga Park, Calif. Nov 60. Contract
AT(ll-l)-GEN-8. 58p. Order from OTS. $1.25.
NAA-SR-3762
Measurement of ±e SRE power coefficients and re-
actor parameters utilizing the oscillation tech-
niques, by C. W. Griffin and J. G. Lundholm, Jr.
Atomics liternational. A Division of North
American Aviation, Inc. . Canoga Park. Calif.
Nov 60. Contract AT(ll-l)-GEN-8. :4p.
Order from OTS. $1.25. NAA-SR-3763
Calibration of the SRE shim rods by the oscillation
method, by C. W. Griff In and J . G. Lundholm,
Jr. Atomics International. A Division of North
American Aviation, Inc., Canoga Park, Calif.
Nov 60. Contract AT(11-1)-GEN -8. 25p. Order
from OTS. 50 cents. NAA-SR-3764
Numerical solution of quasi-linear equations, by
— E. R. Cohen and H. P. Flatt. Atomics Interna-
tional. A Division of North American Aviation,
Inc., Canoga Park, Calif. Oct 60. Contract
AT(ll-l)-GEN-8. 22p. Order from OTS. $1.00.
NAA-SR-5178
378
Aa enriched UOo ZrH critical aasembly, by M. V.
Davis and others. Atomics International. A
Divialon of North American lAviation, Inc. ,
Canoga Park, Calif. Nov 60. Contract AT(ll-i)-
OTN-8. 34p. Order from OTS. $1.00.
1 . NAA-SR-5610
Flux evaluation of MTR irradiated NAA-15 asaem-
bliea, by M. Roy. Atomics International. A
Division of North American Aviation, Inc. , Can-
oga Park, Calif. Apr 58. 3p. Order from LC.
Ml $1.80, ph$1.80. NAA-SR-Memo-2654
Bflect of temperature upon the energy absorption
in ^ P/8*"ic moderator-coolant in the CMRB,
by V. Keahishlan. Atomics International. X~
Envision of North American Aviation, Inc. ,
Canoga Park, Calif. July 58. ^. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR-Memo-2902
Energy abeorptlon In the coolant of a 555 Mw ther-
mal OMR, by V. Keehishian. Atomics Intema-
tional. A Division of North American Aviation,
Inc., Canoga Park, Calif. Nov 58. Sp. Order
from LC. Ml $1.80, ph $1.80.
NAA-SR-Memo-3245
Tlie Hemad code^ byB. L. Scott. Atomics Inter-
national. X~Dl vision of North American Aviation,
Inc. , Canoga Part, Calif. Aug 59. 12p. Order
from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-4220
Review of ultrasonic theory and application with re-
gard to feasibility of operation in organic re-
actors, by D. G. Lilja. Atomics International.
A Division of North American Aviation, Inc. ,
Canoga Park, Calif. Nov 59. 6p. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR-Memo-4595
Tliermionic nuclear fuels for direct conversion re-
actors, by S. M. Toy. Atomics International.
A Division of North American Aviation, Inc. ,
Canoga Park, Calif., Nov 59. 8p. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR-Memo-4692
Analysis of neutron slowing down from a finite plane
fission source for uniform and non-uniform
source distributions, by H. Alter. Atomics In-
temadonal. EN vision at North American Avia-
tion, Inc., Canoga Park. Calif. Mar 60. 21p.
Order from LC. Ml $2.70, ph $4.80.
NAA-SR-Memo-5081
Special heat transfer phenomena for supercritical
rtuids, by K. Goldmann. Nuclear Development
Corporation of America, White Plains, N. Y.
Nov 1 and 2, 1956. Decl. July 7, 1960. 18p.
Order from OTS. 50 cents. NDA-2-31
The transmission of gamma raya at slant Incidence
through slabs of various materiala In shielding,
by L. Pullman. Nuclear Development Corpora-
tion of America, White Plains, N. Y. Oct 56.
Decl. March 31, 1960. 109p. Order from LC.
Mi $5.70, ph $16.80. NDA-2056-6
Rem
imak. an WM-704 program tor neutron nioment
calculationB, by J. Certaine and odiers. Nuclear
Development Corporation of America. While
Plains, N. Y. Dec 59. Contract AT(30-l)-2303.
22p. Order from LC. Ml $2. 40, ph $3. 30.
NDA-2120-3
Decay at ^- weaoaa bound in die K-ahell of lirtt
nuclei, by H. Uberall. Carnegie Insitute ci
Technology, Pittsburgh. Pa. Feb 60. Contract
AT(30-l)-882. 43p. Order from LC. Ml$3.30,
ph$7.80. NYO-2239
Reaction p •*• P~~f *^ •♦• P + n with polarized proK>na,
by R. L. McIIwain. Carnegie Institute of Tech-
nology, Pittsburgh, Pa. May 60. Contract AT
(30-l)-882. 80p. Order from LC. Mi $4.50,
ph $12. 30. NYO-2240
Internal pairs following 'J" " capttire In -hydrogen,
by M. Derrick, and others, Carnegie Institute
of Technology, Pittsburgh, Pa. June 60. Con-
tract AT(30-l)-882. 26p. Order from LC.
Mi $2.70, ph$4.80. NYO-2241
Magneto-hydrodynamic shock structure without
collisions, by C. S. Morawetz. New York Uni-
versity, Institute of Mathematical Sciences,
New York, N. Y. Mar 60. Contract AT(30-1)-
1480. 65p. Order from LC. Mi $3.90.
ph $10.80. NYO-2885
A note on aignlficance of sums in floating-point
arlthnwtlc, by I. N. Rabinowltz. Princeton
University, Project Matterhorn, Princeton, N. J,
Nov 58. Contract AT(30-1)-1238. 3p. Order
from LC. Mi $1.80, ph $1.80. NYO-2389
A scheme for particle separation In high energy
beams, by H. M. Broay. University of Pemisyl-
vania, Philadelphia. Pa. Feb 60. Contract AT
(30-l)-2171. 6p. Order from LC. Mi $1.80.
ph$1.80. NYO-2180
Finite automata,
cognition and per cep-
trons, by H. i^eller. New York University.
Atomic Energy Commission Computing and
ata, pa
ttern recc
379
Applied Machtmadcs Center, New York, N. Y.
Mar 60. Contract AT(30-1)- 1480, 50p. Order
from LC. M| $3.30, ph $7.80. NYO-2884
ftopeaa report and budget propoaal, by J. M.
Miller. Columbia uJversity, New York. N.
June 60. Contract AT(30-l)-10l9.
from LC. Ml $1.80, ph $1.80.
Y.
6p. Order
NYO-7336
Natural alpha radioactivity in medium-heavy ele-
mentfl. Theaia, by R. D. Macfarlane. Carnegie
Inatitute of Technology, Pittsburgh, Pa. May 59.
Contract AT (30- 1)-844. I61p. Order from
OTS. $2.75. NYO-7687
Proposal for a sitm 11 plasma source. Technical
memo no. 59, by P. F. Chen. Princeton Univer-
sity, Project Matterhom, Princeton, N. J. Mar
58. Changed from OFFICIAL USE ONLY Febru-
ary 15, 1960. Contract AT(30-I)-1238. 32p.
Order from UC. Mi $3. 00, ph $6. 30.
NYO-8061
A propoaal for ajlinear plasma source L-2. Tech-
^
nical naemo no. 68, by F. Chen and othera.
Princeton Uniferaity, Project Matterhorn,
Princeton, N.J. Feb 59. Changed from OFFI-
CIAL USE ONLY February 15, 1960. Contract
AT(30-1)-123$. 52p. Order from LC. Mi $3. 60.
pta$9.30.
NYO-8a71
A theoretical an4 e^qgrimenul study of optical
fibers, by R. ). Potter. University of Rochester.
Inatitute at Optics, Rochester, N. Y. Apr 60.
Contracts ATCO-I)-875 and AF 33(6I6)-6171.
Il6p. Order from LC. Mi $7.20, ph $22.80.
1 NYO-9033
Conical refractiohs in crystal optics and hytlromag-
netlcs, by D. Ludwig. New York University,
Atomic Energy Commission Computing and
Applied Mathematics Center, New York, N. Y.
Apr 60. Contract AT(30-l)-1480. 2^. Order
from LC. Mi $2. 70. ph $4. 80. NYO-9084
On die kinetic thdory of steady gas flow, by L.
Sirovich. New Ycrk University, Institute of
Mathematical Sciences. New York, N. Y. June
60. Contract AT(30-1)- 1480. 75p. Order from
LC. Mi$4.5d, ph$12.30. NYO-9086
The
s sections on Ti*^, V^^, Cr^2_ q.
59
n croeg
and Cu"'Mronii 4 to 615 Mev, by H. Taketani and
W. P. Alford.
York, N. Y.
I7p. Order from LC. Mi $2. 40.
University at Rochester. New
une 60. Contract AT(30-l)-875.
ph$3.30.
NYO-9087
Metas table
and the aooma-
tas table smes of hyperfragmenta and it*
lous magnetic moment erf tne A-hyperon, _,
S. Iwao. University of Rochester, Rochester.
N. Y. June 60. Contract AT(30-l)-875. 9p.
Order from LC. Ml $1.80. ph $1.80.
NYO-9088
Pseudoacalar interaction in nuclear beta decay.
Thesis, by C. P. Bhalla. Oak Ridge National
Laboratory, Oak Ridge, Tenn. July 60. Con-
tract W-7405-eng-26. 188p. Order from LC.
Mi $8.40, ph $28.80. ORNL-29S0
Neutron activation croes -sections with 14.8 Mev
neutrons in the .
iHilT
>ns in tty region at the 28 -proton closed
ind (n. He"^) reactions with medium weight
■ Thesis, by I. L. Preiss. University of
nuclei. Thesis, by I. L. Preiss. University^
Arkansas, Fayetteville, Ark. Jan 60. Contract
AT(40-l)-277. 81p. Order from LC. Mi $4.80,
ph $13.80. ORO-235
Ionization and charge transfer croea sections.
Technical status'report no. 2, covering period
December 1, 1959 to February 29, 19&), by
E. W. McDaniel and others. Georgia Institute
of Technology, Engineering Experiment Stttion,
Atlanu, Ga. 1960. Contract AT(40-1)- 2591.
9p. Order from LC. Mi $1.80, ph $1.80.
ORO-253
Single -particle exciMtions of a degenerate electron
gas.' Technical report no. I6l" by A. J. Click
and R. A. Ferrell. University of Maryland,
College Park, Md. Dec 59. Contracts AT
(40-l)-2098 andNonr-1797(00). 35p. Order
from LC. Mi $3.00, ph $6.30. ORO-270
Multi-group analysis of nuclear reactors in three
space dimertsions, by F. B. Banan and others.
cJeneral Electric Comjxany, Knolls Atomic
Power Laboratory, Schenectady, N. Y. and
Flight Propulsion Laboratory Department, Even-
dale, Ohio. Apri 60. 167p. Order from OTS.
$3. 00. R59FPD936
The probability of coverage of point or spherical
targets by an effect spne
Albuquerque, N. Mex
from LC. Mi $2.40, ph $3. 30.
re. Sandia Corporation
June 53. 13p. Order
SC-2925(TR)
380
The electrical behavior erf exploding wires. Part I:
Experimental apparatus and techniques, by F. W.
Neilson and I. 6' McKinney. Sandia Corporation,
Albuquerque, N. Mex. Feb 60. 75p. Order
from OTS. $2.00. SCTM-8-60(51)
Notes on minimum energy trajectories, by D. R.
Morrison. Sandia Corporation, Albuquerque,
N. Mex. Jan 56. 7p. Order from LC. Mi $1.8a
ph$1.80. SCTM- 12-56(51)
Certtin nonlinear flows of magnetohydrodynamics,
by 0. G. Owens. Sandia Corporation, Albuquer-
que, N. Mex. Feb 56. Contract AT(29-l)-789.
18p. Order from LC. Mi $2.40. ph $3.30.
SCIM-19-56(51)
On a nonlinear differential equation arising In mag-
neto-hydrodynamics, by S. Bell. Sandia Corpora-
tion, Albuquerque, N. Mex. Feb 56. 16p.
Order from LC. Mi $2. 40, ph $3. 30.
SCTM-22-56(51)
fcmer requirements for sustaining vibrations.
Part II, by D. M. EUett. Sanma Corporation,
Albuquerque, N. Mex. Mar 54. Changed from
OFFICIAL USE ONLY October 30, 1959. 21p.
Order from LC. Mi $2. 40, ph $3. 30.
SCTM -29 -54(51)
A class erf casualty functions widi special applica-
tions to circular targets, by D. Young and others.
Sandia Corjaoration, Albuquerque, N. Mex. Aug
54. 21p. Order from OTS. $1.25.
i SCTM-32-54(51)
Determination of required component reliability
from system reliability requirements, by A. M.
Breipohl. Sandia Corporation, Albuquerque,
N. Mex. Mar 60. 71p. Order from LC.
Mi $3. 90, ph$i0.80. SCTM-63-60(14)
Ajpproximate solution of the free space antenna equa-
tion based on a determinaticn of the complex co-
efficients of the leading components of the cur-
rent, by C. W. Harrison, Jr. Sandia Corporation
Albuquerque, N. Mex. Feb 60. 12p. Order
from LC. Mi $2, 40, ph$3.30.
SCTW-53-60(14)
Report on microwave propagation characteristics of
U 12E tunnel, Nevada test site, Mercury, Nevada,
by J. F. Barham and S. A Ingham. Sandia Cor -
poration, Albuquerque, N. Mex. Nov 59. 40p.
Order from LC. Mi $3. 00, ph $6. 30.
SCTM-94-59(81)
Explicit symmetric flows of hydromagnetics. by
0. G. Owens. Sandia Corporation" Albuque rque .
N. Mex. June 56. 5p. Order from LC.
Mi $1^80, ph$l.80. SCTM-136-56(51)
Note on the numerical evaluation of integrals of the
form A" f (x)^ (x) dx, with particular reference
to the oetermination of the expectation of a func-~
tlon of a normally distributed random variable.
Sandia Corporation, Albuquerque, N. Mex.
Sep 53. 7p. Order from OTS. 75 cents.
SCTM -145 -53(51)
Power requirements for space communications, by
requl]
R. J. Thompson. Sandia Corporation, Albuquer-
que. N. Mex. July 60. 27p. Order from OTS.
75 cents. SCTM- 179-60(51)
An aid to printed circuit layouts using the IM>l-704
computer, by S. D. Stearns and R° A. O'Connell.
Sanaia Corporation, Albuquerque, N. Mex.
June 60. 12p. Order from OTS. 50 cents.
SCTM-201 -60(24)
Waveform effects in shock testing, by W. J. Sieger.
Sandia Corporation, Albuquerque, N. Mex.
Aug 60. 24p. Order from OTS. 75 cents.
SCTV-205-60(12)
Solution of the integral equation which determines
radar-cross-section for a scattering ground, by
R. A. Hessemer, Jr. and C. S. Williams, Jr.
Sandia Corporation, Albuquerque, N. Mex.
Sep 54. 1^. Order from LC. Mi $2.40,
ph$3.30. SCTM -207 -54(54)
Hi^-speed sequential gate control circuitry, by
L. Ehrman. Sandia Corporation, Albuquerque,
N. Mex. July 60. lOp.
SO cents.
Order from 015.
SCTM -239 -60(1 4)
photographic study of sources of spherical shock
waves, by ]. Todd. Jr. Sandia Corporation,
Albuquerque, N. Mex. Nov 54. 8p. Order from
from LC. Mi $1.80, ph $1.80.
SCTM -242 -54(51)
Vapor pressures of the rare earths, by L. C.
Beavis. Sandia Corporation, Albuque rque ,
N . Mex. Aug 60. 14p. Order from OTS.
50 cents. 801^1-256-60(14)
Characteristics of a free supersonic helium Jet
issuing normally from a flat plate, by A. Bedford.
Sandia Corporation, Albuquerque, N.Mex.
Aug 60. 48p. Order from OTS. $1.50.
SCTM -28 1-60(51)
A digital comparator, by N. A. Bourgeois. Jr.
Sandia Corporation, Albuquerque, N. Mex. Sep
60. 8p. Order from OTS. 50 cents.
SCTM-303-60(14)
Elementary theory of an RF probe in an ionized
medium, by C. W. Harrison, Jr.. and D. H.
Denton, Jr. Sandia Corporation, Albuquerque.
N.Mex. Oct 59. 9p. Order from LC. Mi $1.80.
ph$1.80. 5011.4-309-59(14)
381
Output formal contide rations for diglal automatic
data recording, by E. C. Dowling. Sandia Cor-
poration, Albuquerque, N. Mex . Feb 60. 55p.
Order from LQ. Mi $3. 60. ph $9. 30.
SCTM-3U-59(15)
A design of a merbiry-wetted co*xi>l awltdi, by
T. V. Harrouni Sandia Corporation, Albuquer-
que. N. Mex. Nov 60. 8p. Order from OTS.
SOcentB. SCTM-339-60(14)
Note on linear electro-opclc effecta and a Poas^ble
application to ^hock wave dUgnoetlcs, by H. G.
Baerwald. Sanilia Ujrporatlon, Albuque rque ,
NovjW. Contract AT(29-l)-789. Up.
Mi $2. 40, pta $3. 30.
50114-341-59(51)
N. Mex
Order from LC
Attributes sampling plana for asauring high lot re-
lubiUty, by B. E. Baker. Sandia Corporation.
Albuquerque. S. Mex. Dec 58. Contract AT
(29-l)-789. 3ip. Order from LC. Mi $3. GO.
ph $6. 30.
F. A. Hinchey
SCTM- 352 -58(51)
Cylindrical antemta theory, by R. H. Duncan and
New Mexico State University,
Physical Scienie Laboratory, University Park.
N. Mex. July j59. I05p. Order from LC.
Mi $5. 70. ph ^16.80. SCIW-367-59(14)
JulyB9.
ph^l6.
Basic radiation snudies. Quarter
no. 1 for the period from Novel
through
W.
ly progn
emoer I ,
ogreaa report
^ January
Laboratories, Inc
Contract AT(l
Ml $1.80. ph
V^
I960. Johnston (William H.)
, Baltimore, Md. 1960.
650. 7p. Order from LC.
TID-5612
Interactions of fa$t jt- mesons in lead with small
Jir Technica
energy transfe
dePagter and
St. Louis, Mo.
48p. Order f^m
re
"Was
port no. 5, by J.
mington University,
D. Sard.
Jan 60. Contract NONR-816.
LC. Mi $3.30, ph$7.80.
TlD-5642
Soft x-ray spectrp of metals and alloys. Final re-
port for tbe period July 1, 1951 --June 'Mi, Tm,
by C. H. Sha\« and E. L. Jossem. Ohio State
University, Research Foundation, Columbus,
Contract AT(l I -I)- 191. 64p.
Ohio. Dec 59
Order from LC. Mi $3.90. ph $10.80
TID-5643
Initial experimems on pressure drop for flow
throu^ eccentric annul!. TecHrical note~IX TN-
1-59 Parts {'and U, by T. Uiskind and others.
Nov 59. Contract AT(30-3)-187. 44p. Order
from LC. Mi $3.30. ph $7.80. TID-5670
Stripping effects tn the reactions C*^(He3,p)N^*
andCl2<He3,d)Ni^at 13. $Mev. by J. R.
Priest and others. Purdue University, Lafay-
ette. Ind. 1960. Contract AT (1 1-1) -122. 32p.
Order from LC. Mi $3. 00, ph $6. 30.
TID-5700
Magnetic compressional heating and cup confinement
..5a pUsma, by G. Schmidt and others. Stevens
Institute of technology . Hoboken, N. J. 1959.
I6p. Order from LC. Ml $2. 40. ph $3. 30.
TID-5701
Angular distributions
T^Mevand^^TS
i for ci^o<,P)N^^at 16.1-19-
r5gJi^2 2t U"9 Mev, by J. R
. Purdue University, Lafayer
Priest and others. Purdue University, Lafayette,
Ind. 1960. Contract AT(11-1)-1 22. 26p. Order
fromLC. Ml $2. 70, ph $4. 80. TID-5707
Final report of researches under contract NSori-
07806 and Noor- 1841(16). Summary of work
sponsored by ONR and AEC for period April 1,
T9igloMayl5, 1958. Massachusetts Institute
of Technology. Laboratory for Nuclear Science,
Cambridge. Mass. May 58. 106p. Order from
LC. Mi $5.70. ph $16.80. TID-5725
Decay of Sl^^, by E. L. Robinson and O. E. Johnson.
Pud'je University. Lafayette, Ind. 1960. Con-
tract AT(11-1)-122. 33p. Order fromLC.
Ml $3.00, ph$6.30. TID-5732
Separate carry storage adders. Report no. 97,
^y S. Takahashi. University of Illinois, Lngiul
Computer Laboratory, Urbana, 111. Mar 60.
Contract AT(ll-l)-45. 13p. Order from LC.
Mi $2. 40, ph$3.30. TlD-5739
Research and investigation leading to methodH of
gnerating and detecting radiation in the 100 to
%
P. D. Coleman and others. University of Illinois,
Electrical Engineering Research Laboratories,
Urbana. 111. Apr 60. Contract AT(1 1- 1)- 392.
90p. Order fromLC. Ml $4.80. ph $13.80.
TlD-5821
Plasma turbulence, by L. S. G. Kovas-tnay. Space
Technology Laboratories. Inc. . Riysical Researc*
Laboratory, Loe Angeles, Calif. Feb 60. Coo-
tract AT(04- 3)- 321. 23p. Order fromLC.
Mi $2.70, ph$4.80. TID-5825
An experimental study of close collisions of high
energy Mu-mesons with electrons, by R. F.
Deery. University of Washington, Seattle, Wash.
Apr 60. Contract Nonr-477(12). 99p. Order
from LC. Mi $5.40, ph $15.30. TID-5848
382
Oa the leptonic and non-leptontc decay-modes of k-
meson. Technical report no. 171, by J. C. Pati.
and others. University of Maryland, College 1,
Park, Md. and Wisconsin University, Madison,
Wis. Apr 60. Contracts AF49(638)-24 and AT
(Il-l)-30, AFOSR-TN-60-455. 37p. Order
fromLC. Ml $3.00. ph $6.30.
I TID-5887 (TN -60-455)
Bending of a thin cylindrical shell subjected toa line
loaa around a circumference, by H. R. Merk.
Pratt and Whitney Aircraft Division, United Air-
craft Corporation, Connecticut Aircraft Nuclear
Engine Laboratory, Middletown. Conn. June 59.
Contract AT(11- 1)- 229. 25p. Order fran LC.
Ml $2.70, ph$4.80. TID-5904
A boundary layer analysis of the kinetics of reaction
00 a flat plate. Interiiti report, by J. F. Wehner.
Johns Hopkins University, Baltimore. Md. May
60. Contract AT(30- 1)- 2334. 1 Op. Order from
LC. Mi $1.80, ph$1.80. TlD-5916
F-center growth in ICCl. by P. V. Carnegie Institute
ol Teduiology, Pittsburgh, Pa. Jan 60. Contract
AT(30-1)-1828. 103p. Order from LC.
Mi $5. 70, ph $16.80. TID-5932
Technical progress report. Part I. Hig^-speed
computer program. Part II. Circuit reseaFch
program. Part III. MathenMtical methods.
rt rv. Illiac use and operation. Part V. BM
650 use and operation, rart VI. General labora-
tory information. University of Illinois, bigital
Computer Laboratory, Urbana, HI. Dec 59.
Contract AT(ll-l)-4l5. 39p. Order from LC.
Ml $3. 00, ph$6.30. TID-5973
Technical progress report, fart I. High-speed
computer program. Part II. Circuit research
program. I^rt III. Mathematical methods.
Part rv. Illiac use and (»eration. Part VI. Gen-
Illiac use and operation
eral laboratory informatioru University of
Illinois, Digital Computer Laboratory, Urbana,
111. Jan 60. Contract AT(11-1)-415. 43p.
Order from LC. Mi $3.30, ph $7.80.
TID-5974
Technical progress report, j^rt I. High-speed
computer program. Part II. Circuit research
ram. Part III. Madiematical methods.
progra
Part I>
Jart rv. Illiac use and operation. Part V. 1^4
650 use and operation. Part VI. General labora-
tory information. University of Illinois, Digital
Computer Laboratory, Urbana, 111. Feb 60.
Contract AT(ll-l)-415. 36p. Order from LC.
Mi $3.00, ph$6.30. TID-5978
JMtc Studies in heat transfer and fluid flow. Quar-
terly progress report for period April 1. 1960
to June 30, 1960, by T. Diskind and others.
Columbia University, Department of Chemical
Engineering, Engineering Research Laboratories,
New York. N. Y. 1960. Contract AT(30-3)-
187. 88p. Order from OTS. $2.00.
TID-6035
The effects of intense gamma irradiation on electric
breakdown in helium. Final report, by H. C.
Shaw. Tracerlab, Inc., Richmond, Calif. Mar
60. 27p. Order from OTS. 75 cents.
TID-6234 (Rev. )
Tritium iproduction. Dependence of purity on neu-
tron dux, by C. M. Van Atu. University d
California, Radiation Laboratory, Berkeley,
Calif. Nov SO. Decl. March 24, 1960. lOp.
Order fromLC. Ml $1.80. ph $1.80.
UCRL-1026
Thermal conductivity of metal interfaces, by R. A.
Heckman. University of California. Radiation
Laboratory, Berkeley. Calif. Nov 50. Contract
W-7405-eng-48. I4p. Order from LC.
Ml $2.40, ph$3.30. UCRL-1052
ARC research progress report: Mirror machine
program, by R. F. Post. University of Califor-
nia. Radiation Laboratory, Livermore, Calif.
Oct 56. Decl. October 20, 1958. 30p. Order
fromLC. Mi $2.70, ph $4.80. UCRL-4795
Pyrotron high-energy experiments, by C. C. Damm
and F. S. Eby. University of California, Radia-
tion Laboratory, Livermore, Calif. Apr 58.
Contract W-7405-eng-48. 5p. Order from LC.
Mi $1.80, ph $1.80. UCRL-5046
Circuit dynamics of the pinch, by J. Killeen and
B. A. Lippmann. University of California, Law-
rence Radiation Laboratory, Livermore, Calif.
Feb 60. Contract W-7405-eng-48. 26p. Order
fromLC. Ml $3.00, ph $6.30. UCRL-5424-T
The satellite code: A nimrierlcal satellite Integra -
tion program for the IBM 704, by V. S. Smith
and others. University of California, Lawrence
Radiation Laboratory, LivernK>re, Calif. June
59. Contract W-7405-eng-48. 46p. Order
fromLC. Mi $3.30. ph $7.80. UCRL-5462
Electronic engineering design problems in fusion
research, oy V. l" Smim. University of Califor -
nia, Lawrence Radiation Laboratory, Livermore,
Calif. Aug 59. Contract W-7405-eng-48. 32p.
Order from LC. Mi $3.00. ph $6.30.
UCRL-5559
383
Toy top plaa ma Injector , by F. Coensgen and others
University of 'California, Lawrence Radiation
Laboratory, lerkeley, Calif. May S9. Sp.
Order from UC. Mi $1.80, ph $1.80.
UCRL-5603-T
Some aspects of high temperature plasma research
with the mirror machine, by R. F. Poet. Uni-
versity of California, Lawrence Radiation Labor-
atory, Liver^nore, Calif. Jan 60. Contract
W-7405-eng-48. 29p. Order from LC.
Ka$2.70. ph|$4.80. UCRL-5604-T
Electron-populaltton analysis and the dipole mcanent
of the LiH^r^*' excitea state, by A. M. Karo.
WW _
University ^ICalifornia, Lawrence Radiation
Laboratory, tivermore, Calif. July 59. Con-
tract W-7405-ieng-48. 2lp. Order from LC.
Mi $2.70. phj$4.80. UCRL-5628
Air core cryogei
and hirfi ener
Poet an
c magnet coils for fusion research
nuclear physics applications, by"
R. F. Poetar^C. E. Taylor. University of
California, Lawrence Radiation Laboratory,
Uvermore, Calif. Oct 59. 31p. Order from
LC. Mi$3.0(), ph$6.30. UCRL-5630-T
,0t. ph$6.:
Convergence of ^e quasi -chemical method for the
ising square fattice, by S. G. Brush. University
of Calirornia, Lawrence Radiation Laboratory,
Uvermore, Calif. Jan 60. Contract W- 7405-
eng-48. 6p. Order from LC. Mi $1.80,
ph$1.80. UCRL-5842-T
Thermodynamic jfunctions of a partially degenerate
fully Ionized ^s, by H. E. DeWitt. University
of California, Lawrence Radiation Laboratory,
Uvermore, Qalif. Aug 59. Contract W-7405-
eng-48. 56p. Order from LC. Mi $3.60,
ph $9. 30. i UCRL-5652
9-ZO0M--A one*dimensional, multigroup, neutron
diffusion theory reactor code for the IBM 709.
Part I. Theory and equations. Part II. Input
and operating instructions. Part III. Test prob-
lem, by S. pTbtone and others. University of
California, Lawrence Radiation Laboratory,
Uvermore, Calif. Aug 59. Contract W-7405-
eng-48. 55p. Order from LC. Mi $3. 60,
ph $9. 30. , UCRL-5662
Soine important^rameters of the plasma diode,
by R. Fox. Oliiversity of California, Lawrence
Radiation Laboratory, Uvermore, Calif. Nov
59. Contract W-7405-eng-48. 3()p. Order
from LC. Ml $2.70, ph $4.80. UCRL-5683
The high-energy lelectrostatic plasma gun, by R.
Fox" University of California, Lawrence Radia-
Laboratory, Uvermore, Calif. Nov 59. Con-
tract W-7405-eng-48. Nov 59. 45p. Order
from LC. Mi $3.30. ph $7.80. UCRL-5689
Ionization equilibrium equation of state. Part I.
Solution of equations, by C. A. Rouse. Univer-
sity of California, Lawrence Radiation Labora-
tory. Uvermore, Calif. Oct 59. Contract W-
7405-eng-48. Up. Order from LC. Mi $2.40,
ph $3. 30. UCRL-5695-T
Physics of the ion thrust system, by R. Fox. Uni-
versity of California, Lawrence Radiation Labor-
atory, Uvermore, Calif. Oct 59. Contract
• W-7405-eng-48. 19p. Order from LC.
Mi $2. 40, ph $3. 30. UCRL-57a7-T
The bumpy torus, by G. Gibson and others. Uni-
versity of California. Lawrence Radition Labor-
atory, Uvermore, Calif. Oct 59. Contract
W-7405-eng-48. lOp. Order from LC.
Mi $1.80, ph $1.80. UCRL-5738
Injection and trapping of high current electron
beams, by N. C. Christofiloe. University of
California, Lawrence Radiation Laboratory,
Uvermore, Calif. Jan 60. 4p. Order from
LC. Mi$1.80, ph$1.80. UCRL-5743-T
Gamma raya from ipelastic scattering of 14-Mev
neutrons on Pb~ , by E. Hallett and R. Jensen.
University of California, Lawrence Radition
Laboratory, Uvermore, Calif. Aug 59. Con-
tract W-7405-eng-48. 21p. Order from LC.
Mi $2.70, ph$4.80. UCRL-576e
Polarization in pion-nucleon scattering and the
second and mird pion-nucleon resonances, ~by
M. J. Moravcsik. University of California.
Lawrence Radiation Laboratory, Uvernnore,
Calif. Jan 60. Contract W-7405-eng-48. I6p.
Order from LC. Mi $2. 40. ph $3. 30.
UCRL-5831-T
Resonance absorption at neutrons in thick sheets
of molybdenum, by E. Goldberg and F. A.
Kloverstrom. University of California, Law-
rence Radiation Laboratory. Uvermore, Calif.
1959. 3p. Order from LC. Mi $1 . 80. ph $1 . 80.
UCRL-5864-T
A plasma cyclotron, by H. P. Furth. University
of California, Lawrence Radiation Laboratory,
Uvermore, Calif. Apr 60. (ip. Order from
LC. Ml $1.80, ph$1.80. UCRL-5911-T
Neutron diffusion theory programs and their appUca-
tion to simple critical systems, by S. P. Stone
384
and R. E. Lingenfelter. University of California,
Lawrence Radiation Laboratory, Uvermore.
Calif. May 60. Contract W-7405-eng-48. 35p.
Order from LC. Mi $3. 00. ph $6. 30.
UCRL-5913
Sttte of matter at high pressure, by B. J. Alder.
University of California, Lawrence Radiation
Laboratory. Uvermore, Calif. May 60. Con-
tract W-7405-eng-48. 24p. Order from LC.
Mi $2.70. $4.80. UCRL-5937-T
On die establishment of a teinperature function, by
W. Aron and L. Parker. University of Califor-
nia. Lawrence Radiation Laboratory, Uver-
more. Calif. 1960. Contract W-7405-eng-48.
9p. Order from LC. Mi $1.80, ph $1.80.
UCRL-5961-T
Measurement of average neutron energies for {^, n)
neutron sources, by W. N. Hess and A. R.
Smith. University of California, Lawrence Radi-
ation Laboratory, Berkeley, Calif. Apr 59.
Contract W-7405-eng-48. 17p. Order from LC.
Mi $2. 40, ph$3.30. UCRL-8617
ritnent on double scattering of antiprotons in
"^ Talkgf
August
University of California. Lawrence Radiation
Laboratory, Ba-keley. Calif. Aug 60. Contract
W-7405-eng-48. 17p. Order from OTS.
50 cenu. UCRL-9336
Enerin
nydr<
Meet
ogen
ing on A
Talk given at Research Progress
" til, IW. byB. C.\faglic.
On tbe double spherical harnxmics approximation,
by P. H. Wsckman. Westinghouse Electric
Corporation, Bettis Plant, Pittsburgh. Pa. June
58. 18p. Order from LC. Mi $2. 40. ph $3. 30.
WAPD-PWR-Ph-293
Cfa a numerical approxinMtion to the solution of the
OBe-dimensioattl, one-velocity transport eotiitlon
with isotropic scattering. Thiests, by U X.
Hageman. Westinghouse Electric Corporation,
Bettis Plant, Pittsburgh, Pa. Jan 59. 54p. Order
from LC. Mi $3.60, ph $9. 30. WAPD-T-706
Fast neutron penetration through reactor shields,
by N. Haronann and G. R. Tlopkins. Westing-
bouse Electric Corporation, Bettis Plant. Pitts-
burgh. Pa. June 59. 27p. Order from LC.
Mi $2. 70. ph$4.80. WAPD-T-783
PDQ-3 A program for the solution of the neutron-
Omus ion equations in two dimensions on the IBM-
fm, byW. R. Cadwell. Westinghouse Electric
Corporation, Bettis Atomic ?amer Laboratory,
Pittsburgh, Pa. May 60. Contract AT-U-l-
GEN-14. 5^. Order from OTS. $1.75.
WAPD-'I\I-179
ECESS: An IBM -704 program computing transport
equation coefficients for a ntonatoinic gas moder-
ator in the thermal energy region, by W. W.
Clendenin and G. R. Cu^pper. Westinghouse
Electric Corporation, Bettis Atomic Power Labor-
atory, Pittsburgh, Pa. Apr 60. Contract AT-ll-
l-GEN-14. 33p. Order from OTS. $1.25.
WAPD-TM-200
ART-04 - A modification of die ART program for
the treatment of reactor thermal transients on
the IBM-7Q4, by J. E. Meyer and W. D. Peterson.
Westinghouse Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburgh, Pa. July 60.
Contract AT-ll-l-GEN-14. 49p. Order from
OTS. $1.50. WAPD- 11^-202
TRIP-1 - A two-dimensional P-3 prom-am in X-Y
geometry for the IBM-704, by E. Gelbard and
others. Westinghouse Electric Corporation,
Bettis Atomic Power Laboratory, Pittsburgh, Pa.
July 60. Contract AT-ll-l-GEN-14. 21p.
Order from OTS. 75 cents. WAPD-TM-217
54 group library for P-1 programs, by A. F. Henry,
westinghouse Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburgh, Pa. Apr 60.
Contract AT-1 1-1 -CTN- 14. 118p. Order from
. OTS. $1.25. WAPD- 11^1-224
Mechanism of void formation test facility, by A. J.
Martenson and others. Westinghouse E lectr ic
Corporation, Bettis Plant, Pittsjjur^. Pa. Aug
59. Contract AT-ll-l-GEN-14. 28p. Order
from LC. Mi $3.00. ph $6. 30.
WAPD-V(FBE)-274
Report to the AEC nuclear cross sections advisory
roup, Argonne National Laboratory, September
froup, Argot
9-2l, 1960, by J. A. Harvey. Oak Ridge Nation-
al Laboratory, Oak Ridge. Tenn. Sep 60. 82p.
Order from OTS. $2.00. WASH-1029
Dust density versus time and disunce in the shock
wave, by M. G. Gordon and others. Chemical
Warfare Laboratories. Army Chemical Center.
Md. June 57. Decl. Sep 59. 52p, Order
from LC. Mi $3.30. ph $7.80. WT-1113
Radiation Effects on Materials
fuel
Irradiation testing of Enrico Fermi 'prototype
pins in the CP-5, 1957-1959, by M. A. Silliman.
and others. Atomic Power Develc^ment Associ-
ates, Inc. , Detroit, Mich. Apr 60. 56p. Order
from LC. Mi $3. 60, ph $9. 30. APDA-130
385
Calculations for
Irr>i
diatlon erf natural UO^-ThO
HgeTJatlc
(Reviaecl), by). W. Ullmann. Oak Ridge Nation-
al Laboratory J Oak Ridge, Tenn. June 59. 6p.
Order from LC. Ml $1.80, ph $1.80.
I CF-59-6-35
Irradiation effecty on UCa diaperaed in graphite.
(OkNL-M'I'R-ia-l), interim report no 1 by
J. G. Morgan ^ndM. F. Osborne. Oak Ridge
NatioiiBl Laboratory, Oak Ridge. Tenn. Aug 60.
1^. Order fDom LC. Mi $2. 40, ph $3. 30.
i CF -60-6-78
adiatioo o< 638 aluminum aamplea, by P. D,
Wright. Hanf(ird Works, Richland. Wash.
52,
Mi
Decl.
$1.80. phll
M4y 5. 1960.
80.
Aug
lOp. Order from LC.
HW- 25412
Summary erf HAPQ research and development pro-
gram on ceramic fuel naaterials, by M. J. Sander-
son. General Electric Company, Hanford Atomic
Products Operation. Richland, Wash. Dec 55.
Decl. May 6, 1960. Contract W-31-109-Eng-52.
4p. Orderfro^LC. Mi $1.80. ph $1.80.
HW- 40288
Examination of ttradiated uranium-magneetum nmt-
ri« fuel material. Interim report no. 2, by W.S.
Kelly. General Electric Company, Hanford
Atomic Produots Operation, Richland, Wash.
May 56. Decl. May 4. 1960. Contract W-31-
109-Eng-52. ^. Order from LC. Ml $1.80.
ph$1.80. 1 HW -42652
Organic recirculating ajpparatua 2. ORA'2 operating
history, Septeyiber l956-March 1957, by C. L.
Buckner. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
June 57. Decl^ February 25, 1960. 13p. Order
from LC. Mi |2.40, ph $3. 30. HW-50660
Summary of teatiag for the ELA!0-7 test loop, Janu-
ary 1, to December 31, 1958, by D. R. Doman.
General Electijic CompanyTTianford Atomic
Products Operation, Richland, Wash. Jan 59.
Contract AT(4$-1)-1350. 27p. Order from LC.
Mi $2. 70, phS4.80. HW-57883
Effect of reactor irradiation on Johns -Manvi lie
thermal insulation, by C. Mannal. Knolls Atomic
Power Laboratory, Schenectady, N. Y. Jan 54.
Decl. March?, I960. Contract W-31-109-Eng-
52. 15p. Ord^rfromLC. Mi $2.40, ph $3.30.
I KAFL-M-CM-35
Radiation damage' to non-metallic materials. A
literature aurviey. by E. M. Doss. Atomics
International. A Division of North American
Aviation, Inc., Canoga Park. Calif. May 57.
16p. Order from LC.
Mi $2.40, ph$3.30.
NAA-SR-Memo-1890
IrrsdiatioQ dams;
in metals fuels: A literature
ntle. Atomics International.
survey.
A Division of North American Aviation, Inc.
Canoga Park, Calif. Oct 57. Decl. June 60.
20p. Order from LC. Ml $2. 40, ph $3. 30.
NAA-SR-Memo-2156
'^y^-.
Production of fission gas in U-10 w/o moly fuel roda,
by R. H. Davidson Atomics Intematfonal. X~
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Apr 59. 5p. Order from
LC. Mi $1.80, ph$1.80.
NAA-SR -Memo- 3657
Transient heating of UC fuel elements in the KEWB
facility, bysTL. Gardner and S. G. Barnes.
Atomics International. A Division of North
American Aviation, Inc. , Canoga Park, Calif.
Sep 59. 22p. Order from LC. Mi $2.70,
ph$4.80. NAA-SR -Memo- 4333
Effects of radiation on massive uranium monocar-
bide, by H. Pearlman. Atomica International
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Dec 59. Contract AT- 1 1-1-
GEN-8. 16p. Order from LC. Ml $2.40.
ph $3. 30. NAA-SR -Memo- 4631
Data package, experiment AI-4, UOo ratcheting, by
B. M. Watson. Atomics International. A Divi-
sion of North American Aviation, Ur. , Canoga
Park, Calif. Dec 59. 42p. Order from LC.
Mi $3.30, ph $7.80. NAA-SR-Memo-4782
Investintlons in irradiated vitreous silica. Period
covered: March 2 i9'y -March 1 1<J60, by H.A.
Szymanski and D. Keiffer. Included ir~a paper I:
Color centers in aluminum oxide, by H. A.
S^^ymanski, andotheis. Caniaius College,
Buffalo, N. Y. Mar 60. Contract AT(30- 1 )-
1810. 26p. Order from LC. Mi $2.70, ph
ph$4.80. NYO-7396
Neutron irradiation effecta on minority carrier life-
time in silicon diodes, by B. Wickesberg. Sandk
Corporation, Albuquerque. N. Mex. Feb 60.
15p. Order from LC. Mi $2. 40. ph $3. 30.
SCTM- 56- 60(51)
Radiation tolerance of a selected group of coajtlal
cables, phases I. II, and III, by P. P. Proulx
and otbera. Sandia Corporation, Albuquerque,
N. Mex. Jan 60. 37p. Order from LC.
Mi $3. 00. ph$6.30. SClM-400- 59(16)
386
;nt loan contract AT(30-
1 and 2. Columbia University,
11959]. 19p. Order from LC.
Mi $2. 40, ph$3.30. TID-5641
Progress report on
- 0-l»l9, \<8ai~
New York. N. Y.
Radiation damage studies using the techniques of
electron -spin paramagnetic resonsanoe. Xnhual
progress report for May 1.
W^
iport for May 1 1959 through April
ough
1960, by P. J. Bray and A. 0. Williams, jr.
Brown University. Providence, R. I. Mar 60.
Contract AT(30-1)- 2024. 20p. Order from LC.
Mi $2. 40, ph $3. 30. TID-5644
The effect of gamma radiation on simulated lubricar-
ing systems and components. Final report, by
G. C. Lawrason. Southwest Research Institute
San Anantonlo, Tex. July 59. 33p. Order from
LC. Mi $3.00, ph$6.30. TID-5659
Effect of irradiation of solid catalysts. Quarterly
progress report no. 2, by H. C. Andersen aiio
P. N. Rylander. Engelhard Industries, Inc . ,
Newark. N. J. Nov 59. Contract AT(30-1)-
2402. 25p. Order from LC. Mi $2.70,
ph$4.80. TID-5984
Radioactive Waste
Idaho Chemical Processing Plant technical progress
report for October to December 1959, by J. R.
Huffman and others. niiUips Petroleum Company,
Atomic Energy Division, Idaho Falls, Idaho.
Aug 60. Coitract AT(10-l)-205. 25p. Order
fromOTS. 50 cents. IDO-14526
Idaho Chemical Processing Plant technical progress
report, radioactive waste disposal projects for
January -March 1960, byJ.R. Huffman and
others. Riillips Petroleum Company, Atomic
Energy Division, Idaho Falls, Idaho, Aug 60.
Contract AT(10-l)-205. 29p. Order from OTS.
50cenu, IDO- 14530
Stainless sttel process wastes: I. Removal of alloy
metals from waste solutions by mercury cathode
electrolysla, by M. E. McLain and D. W.
Rhodes. Riillips Petroleum Company, Atomic
Energy Division, Idahol Falls, Idaho. Sep 60.
Contract AT(10-l)-205. 12p. Order from OTS.
50 cents. IDO- 14533
Cyclotron irradiation of type 347 stainless steel w
welds in NaK at elevatei
Epp. Jr
temperatures, byT.A;
__^_^ ipei
and others. North American Aviation,
Atomic Energy Research Department,
Inc.
Downey, Calif. Jan 53. Decl. August 5. 1960.
Contract AT- 11- l-GEN-8. 45p. Order from
OTS. 40cenu. NAA-SR-74(Rev.)
A thermal problem associated with underground
storage "of radioactive wastes, by J. Crowelf
and F. L. Parker. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. (nd). Contract W-7405-
eng-26. 72p. Order from OTS. $2.00.
ORNL-3002
Radioactive waste processing and disposal. A litera-
ture search, by T. F. Davis. Official of Tech-
nical Information Extension, Oak Ridge, Tenn.
June 60. 92p. Order from OTS. $2.25.
TID-3555
Radioactivity statistics, by A. S. Goldin. National
Lead Coirifwny, IncT, Winchester Laboratory,
Winchester, Mass. Nov 60. Contract AT(49-6)-
924. Up. Order from OTS. 50 cents.
WIN -120
Reactors — General
Reactor physics measurements in treat, by F.
Kirn ana others. Argonne National Laborscorf,
Argpnne, III. Oct 60. Contract W- 31 -109 -eaf-
38. 52p. Order from OTS. $1.25.
ANL-6173
The reactor kinetics of the transient reactor test
facility (TTIEAT), by D. Okrent and others.
Argonne National Laboratory, Argonne, 111,
Sep 60. Contract W-3I-l09-eng-38. 65p.
Order from OTS. $1.50. ANL-6ir4
Study of die padted-bed fuel element concept, by M.
B. Rodin, and others. Argonne National Labora-
tory, Argonne, III. Aug 60. Contract W- 31 -109-
eng-38. 55p. Order from OTS. $1.25.
ANL-6193
Reactor development program progress report, by
N. Hilberry and others. Argonne National
Laboratory, Argonne, III. Aug 60. Contract
W-31-109-eng-38. 58p. Order from OTS.
75 cents. ANL-6215
Reactor development program progress report.
September 1960, by n" Hilberry and others.
Argonne National Laboratory. Argonne , 111.
Oct 60. Contract W- 31- 109-eng- 38. 72p.
Order from OTS. $1.75. ANL-6234
Reactor development program progress report for
November, I960, by N. Hilberry and (Xhers
Argonne National Laboratory, Argonne, 111.
Dec 60. Contract W- 31 -109-eng- 38. 63p.
Order from OTS. $1.75. ANL-6269
387
meas-
Cootrol rod theories evaluation based uf
urements of control rod worths in SM-I-2 re-
actor aasembheja, by J. W. Zwick. General
felectridj Compa|iy, Aircraft Nuclear Propulsion
Department, Cincinnati, Ohio. Apr 59. Con-
tracu ATCll-D-lTl and AF33<600)- 38062. 40p.
Order from OTS. $1,00. ' APEX-578
A 200-Mw (e) boilejr- superheater reactor prelimin-
ary design. Preliminary reference design for
the AEC program on nuclear superheat «velop-
roent. Prepare^ by General Nuclear Engineering
Crrporation, Dvinedin, Fla. and Combustion
Engineering, ,lnc
Contract AT(11
$2.75.
Windsor, Conn. Oct 60.
l)-795. 177p. Order from OTS.
GNEC-136
Thermal neutron flix measurement at the MTR -
ETR site, byC.'H. Hogg. Phillips Petroleum
Company, Atomic Energy Division. Idaho Opera-
tion* Office, Idaho Falls, Idaho. Oct 60. Con-
tract AT(10-1)-; 05. 43p. Order from OTS.
75 cenu. IDO- 16538
MTR
January"!
and others .
~Ru
ETR techni(^l branches quarterly report for
'~~- Mar^ 31, 1$60, by J. R. Hi5fman
llipe Petroleum Company, Atomic
Energy Division^ Idaho Operations Office, Idaho
Falls, Idaho. 1^60. Contraa AT(10-l)-205.
52p. Order froi^ OTS. $1.50. IDO-16633
Spert program revi^, ' by W. E. Nyer and S. G.
Forbes. Phillip$ Petroleum Company, Atomic
Energy Division,^ Idaho Operations Office, Idaho
Falls, Idaho. Ott 60. Contract AT(10-l)-205.
41p. Order froi^ OTS. $1.00. IDO-16634
Laboratory, Loei Alamos,
Contract W-7405|-ENG-36.
OTS. $1.75.
tific
N. Mex. Sep 60.
70p. Order from
LAMS -2469
Comparative study tf H2O and
for heterogeneouB pressuri/^ei
as moderators
reactors for
production of plutonium and useful power,~by
E. F. Weisner afid others. North American
Aviation, Inc., Atomic Energy Research Depart-
ment, Downey, ddlif. May 52. Decl. August 4,
1960. Contract iT-ll-l-GEN-8. 40p. Order
from OTS. 40 c^nts. NAA-SR-183
Performance of HN
"BylT
pump,
AT5ivii
iPP pr(
prototype free -surface sodium
W. ^u. Atomics International,
vision of No^h American Aviation, Inc. ,
Caooga Park. Cajif. June 60. Contract AT(11- 1)-
GEN-8. 26p. Otder from OTS
50 cents.
NAA-SR-4336
Standard cmerating procedure for the pool critical
assembly, by E. B. Johnson. Oak Ridge National
Laboratory, Oak Ridge, Tenn. (ndj. Contract
W-7405-eng-26. 28p. Order from OTS.
75 cents. ORNL-2449
Sulfex-TTiorex and Darex-Thorex processes for the
dissolution of consolidated Edison power reactor
fuel: Laboratory development, by L. M. Ferris
and A. H. Kibbey. Oak Ridge National Labora-
tory, Chemical Technology Division, Oak Ridge,
Tenn. (nd). Contract W-7405-eng- 26. .27p.
Order from OTS. 75 cents. ORNL-2934
Critical measurements on near -homogeneous. BeO-
moderated, ora Hoy -fueled svsteina, by F. A.
Kloverstrom and D. E. Kraft. University of
California, Lawrance Radiation Laboratory,
Livernwre. Calif. July 60. Contract W-7405-
eng-48. 18p. Order from OTS. 50 cents.
UCRL-5369 Pi. 2
Reactors — Power
VMR critical-assembly studies, by R. A. Egen and
others, Battelle Memorial Institute, Columbus,
Ohio. Dec 60. Contract W-7405-eng-92. 57p.
Order from OTS. $1.50. BMI-1482
Preliminary hazards evaluation of the isolated
coolant loops in the HWCTR, by L. M. Arnett
and others. E. I. du Pont de Nemours 8t Co.
Explosives Department, Atomic Energy Division,
Technical Division, Savannah River Laboratory,
Aiken, S. C. July 60. Contract AT(07- 2)- 1.
56p. Order from OTS. $1.25. DP-489
Calculation of reactor transients, by H. D. Brown
and D. Randall. £. I. du Pont de Nemours 81
Co. Explosives Department, Atomic Energy
Division, Technical Division, Savannah River,
Laboratory, Aiken, S. C. Aug 60. Contract
AT(a7-2)-l. 50p. Order from OTS. $1.25.
DP-490
?
Heavy water rnoderated power reactors progri
report for July 1960, by R. R. Hood and L.
ess
40
isakoff. E. I. du Pont de Nemours k Co. Ex-
plosives Department, Atomic Energy Division,
Technical Division, Wilnungton. Del. Oct 60.
Contract AT(07-2)-l. 29p. Order from OTS.
75 cents. DP- 525
•MW(E) prototype hig^-temperature gas -cooled
reactor research and devefoianent program.
Summary report for the period anuary I, 1959
epo
December 31, 1959 and quarterly progress"
388
report for the period October 1, 1959-E)ecember
31, 1959. Gaieral Atomic Division. General
Dynamics Corporation, San Diego, Calif. Sep
60. Contract AT904-3)-314. 185p. Order from
OTS. $3.00. GA-1235
Fast oxide breeder - stress considerations in fuel
rod design, by K. M. Horst. General Electric
Company. Atomic Power Equipment Department
San Jose, Calif. Mar 60. Contract AT(04-3)-
189.PAtl0. 31p. Order from OTS. 75 cents.
GEAP-3347
Nuclear superheat project second Quarterly progn
report for October-December 1959. General
Electric Company, Atomic Power Equipment
Department, San Jose. Calif. Sep 60. Contract
AT(04-3)-189. 178p. Order from OTS. $2.75.
GEAP-3371
ess
Nuclear superheat project fabrication, irradiation
and evafuatlon of superheat fuel element Sh-1
and Sh-2. by E. A. Lees and others. General
Electric Company, Atomic Power Equipment
Cteparunent. San Jose. Calif. Apr 60. Contract
AT(04-3)-189. 33p. Order from OTS. $1.00.
GEAP-3387
Nuclear superheat development program. Third
jTly ■ —
Combustion Engineering
quarte
jxTTiCHi development program. iTura
Ty progress report Januanr-March 1960.
ition Engineering, inc., Windaor, Conn,
and General Nuclear Engineering Corporation,
Dunedin, Fla. Sep 60 Contract AT(ll-l)-795.
I23p. Order from OTS. $2.50. GNEC-131
Los Alamos power reactor experiment No. 11.
LAPRE 11. by R. A. Clark. University of
California. Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. Apr 60. Contract W-
7405-ENG-36. 139p. Order from OTS . $2.50.
LA -2465
Quarterly status report of the LASL plasma thermo-
couple development program for tfte period e"r^
ing September 20 1960 The University of
California, Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. Oct 60. Contract W-
7405-ENG-36. 16p. Order from OTS. 50 cents.
LAMS-2473
Liquid fluidized bed reactor experiment. Final
report -Task 4.00, by M. R. Scheve. Nuclear
Division, Martin Company. Baltimore, Md.
Apr 60. Contraa AT(30-l)-2460. 136p. Order
from OTS. $2.75. MND-LFBR-2337
PM-1 nuclear power plant program 5th
March I. I960 to M
progress report
by F. Hittman.
chl 1960 to May 31. i»60.
Martin Company, Nuclear Divi-
quarterly
ay 31" 19<
sion. Baltimore, Md. July 60. Contract AT(30-
l)-2345. 193p. Order from OTS. $3.00.
MND-M-1816
Thermo-physical properties of irradiated poly-
vi coolants . Part I. Density and viscosity,
. J ^ A ' -_j _L rr— — -T*
enyl coolants .
Gercke and G.
fir
K. H. J. Gercke and G. Asanovich. Atc«nics
International. A Division of North American
Aviation, Inc., Canoga Park, Calif. Dec 60.
Contract AT(ll-l)-GEN-8. 51p. Order from
OTS. $1.25. NAA-SR-4484
Study of remote military
Station Antarctica for
er a
nited
lications Byrd
tates Atomic
Energy Commission, New York
iTEl
rations
Office, New York N.Y. Kaiser Engineers,
Division of H. J. Kaiser Company, Oakland,
Calif. May 60. (Revised July, 1960). Contract
AT(30-1)-2441. 88p. Order from OTS. $2.25.
NYO-9052
Study erf remote military power applications Pole
Station Antarctica for United States Atomic
Commission. New York Operations Office.
Ener
New
dm
ork, N. Y.
_^__ Kaiser Engineers. Division
J. Kaiser Company, Oakland, Calif. May
60. (Revised July, 1960). Contract AT(30- 1 )-
2441. 95p. Order from OTS. $2.50.
NYO-9053
An evaluation erf fossil superheat for nuclear power
plants, by W. H. Colquhoun and others.
EBASCO Services Incorporated. New York, N. Y.
Oct 60. Contract AT(30-l)-2524. 297p. Order
from OTS. $3. 50. NYO-9400
Hydrogenous reactor program quarterly progress
report for period ending April 30. 1960. byR.B.
Briggs and others. Oak kidge National Labora-
tory. Oak Ridge, Tenn. [nd]. Contract W-7405-
eng-26. 129p. Order from OTS. $2.75.
ORNL-2947
Molten-salt reactor progam quarterly progress
report for periods ending January 31. ar^ Apr 11
30, 1960, byH. G. MacPherson. Oak Rieige
Natio.TaI Laboratory, Oak Ridge, Tenn. (nd).
Contract W-7405-eng-26. 88p. Order from
OTS. $2.25. ORNL-2973
Gas -cooled reactor project quarterly progress re-
ort for period ending September 30. r96g7~5y
taff Oak Rieige Naticmal Laboratory. Oak Ric^.
Tenn. [nd]. Contract W-7405-eng- 26. 174p.
Order from OTS. $2.75. ORNL-3015
\
Economics erf nuclear power. A
selected literature, by W. E
_,raphy of
, , . _. Boat. Onieae erf
Technical Informatiem Extension, Oak Ridge,
389
Tran. Jan 60. |82p.
Order from OTS . $2 . 00.
TID-3089
Olio. July 55.
AT(30-1)-1156.
Fabrication at Yankee core I
fuel element.
te core 1 procotype
by M. D'Amore. Wesdnghouse Electric Corpor-
ation, Atomic Powder Department, Pituburgh,
Pa. May 60. Contract AT(30- 3)- 222. 52p.
Order from OTSi $1.25. YAEC-144
Decl. lune 17. 1960. Contract
183p. Order from OTS. $2.75.
NLCO-565
J."!
SOURCE INDEX
Semi-annual
I
progreci
30. 19610,
B report tor the
^^.
anua
n
1 to June 30. 19a0, by H. B. Walchli. Westing^
house Electric Cbrporation, Atomic Power De-
partment, Pittsbtirgh. Pa. Aug 60. Contract
AT(30-3)-222. a6p. Order from OTS. 50 cents
YAEC-186
^ettia technical review. Reactor technology, by
D. S. Griffin and others. We stinghouse Electric
Corporation, Bettis Atomic Power Laboratory.
Pittsburgh, Pa. June 60. Contract AT-11-1-
GEN-U. 92p. Order from OTS. $2.00.
WAPD-BT-19
TecKnolpgy — Feed Materials
Summary technical -eport for the period April 1,
1»55 to June 36 pSS, by J.~W
National Lead Company at Ohio,
;po:
m
Simmons.
Cincinnati,
Summary technical peport for the period January 1,
l»56toMarch31 1»56, by 1. W. SimJnons.
National Lead Company of Ohio, Cincinnati,
Ohio. Apr 56. Decl. June 18, 1960. Contract
AT(30-l)-ll56. I73p. Order from OTS. $1. 10.
NLCO-625
Summary technical report for the period October 1,
1956 to December 31, 1956. by J. W. Stmnaons.
National Lead Company ol Ohio, Cincinnati, Ohio.
[1956]. Decl. July 19, 1960. Contract AT(30-
1)-1156. I65p. Order from OTS. $1.10.
NLCO-660
Summary technical report for the period lanuary 1.
1957 to March 31, 1957, by J. W. Simmons.
National Lead Company of Ohio, Cincinnati,
Ohio. [1957). Decl. September 19, 1960.
Contract AT(30-1)- 11 56. 155p. Order from
OTS. 85 centa. NLCO-670
Fluorox proceaa: Production of UPf, in a fluidized
bed reactor, by C. D. Scott and others. Oak
Ridfce National Laboratory, Oak Ridge, Tain.
Oct 60. Contract W-7405-eng-26. 59p. Order
from OTS. $1.50. ORNL-2797
390
KBEBt
tut
fflNvnfttr
Source
ram
rBNiintel
Sourca
ram.
FBNvBftsL
nCSigon. DC.
Ariny Chemical Reaearch
antl tlevclapmem La'ia. .
Block Aaaoclatea, Inc. .
262
152 7S6
Cambridge. Maaa. (con.)
940
152 714-9
152 757
Army Chemical Cemer.
340
152 714-4
.' C
Md.
271
152 599
341
152 719
ktatm Corp .
CMcM°. >I>
772
149 694
2B«
153 096
177
149 695
906
152 595
Inc . Cambridge. Maaa.
326
171 902
MrawMd Electronic*.
■ 'A-
306
152 596
328
152 906
OHvrml Electric Co. .
' ;■ ; "
906
IS2 597
ktaM. N. Y.
283
153 060
999
149 641
BoMi U. (Weat Germany)
276
152 770
ImnO&o AUTO, Corp. ,
Army Signal Reaearch and
Brltlah ColunMa U.
MmalrU Vf.
iU
152 728
Develcpmem L.ab. , Fort
Mtmmouth. N. J.
2M
IS9 0n
(Canada)
274
149 683
Mre-Space laba. , North
317
132 674
Brooke Army Medical Cen-
ter, Fort Sam Houaton.
Anerlcaii Aviation. Inc. ,
1
917
132 675
Donvy. C«ll(.
257
152 846
3S2
952
152 564
192 965
Tex.
271
193 968
AaroClam Maaarch l.aba. ,
952
152 997
Brovn U. Dlv. of Applied
he., PrIncMon. N. J.
310
148 777
^
Mathematica, Providence.
Army Sno«. Ice and Perma
R. 1.
327
152 8S7
A«ra*lutlc and Structum
froat Reaearch Eatabllah-
328
152 B8
MaMrch Lab. , Maaa.
ment. Wllmette, 111.
291
171 190
kM. at Tech. , Camtorldca
285
147 SS4
Brown U. Div. of Engineer-
Arnold Engineering Develof
mem Center, TuTlahoma.
-
ing. Providence. R. I.
346
192 742
AarOMMlcal Acceaaorlea
Lab. , Wlfhi Air Davelop-
Tana.
306
153 068
Bureau of Naval Weapona.
■aal Cemer, Wrlght-
325
152 556
Waahlngton, D. C.
289
171 M9
PKteraon AFB. Ohio
305
171 345
325
338
152 843
152 664
171 212
171 213
Aaronauticil Material* Lab.
348
1.52 966
171 219
Naral Air Malarial Center.
290
171 20B
FMladelphU. Pa.
329
149 655
ARO. Inc.. Tullahoma,
171 210
330
152 463
Tami.
906
925
153 058
152 556
171 220
171 ni
Mraapaca Medical Div ,
375
152 849
171 222
Wrifhi Air Development
338
152 664
171 223
Olv. . Wright -Patteraon
948
152 966
291
171206
API. OMa
260
265
171 332
171 333
Atlamlc Reaearch Corp. ,
Alexandria. Va.
275
159 083
171 207
171 211
171 214
Mr Force Ca mbrklte Re-
•aarch 1 .ah* . Bedford.
171 215
Avco Corp. , Naahvllle,
171 217
278
278
284
152 684
152 701
153 884
Terni.
Avco'Everen Reaearch
285
' 152 967
292
171 218
171 200
171 201
288
152 984
I.ab.. Vteaa.
346
152 912
171 201
288
152 985
171 209
349
152 9r
Aviation Medical Acceler-
ation Lab. . Naval Air
328
171 216
171 2(8
Ur Force Inei. of Tech. ,
Developmem Cemer.
johnavflle. Pa.
336
171 208
Wrlfh-Paneraon AF^Ohlo
310
153 sr
269
152 470
269
152 740
Bureau of SMpa,
Waahmyon. O.C.
tk Force MlaaUe Develop-
289
171209
mtm Gamer, Holloinan
tft, N. Mm.
263
305
152 744
132 743
Avtaclon Paychology Lab. .
U. of nilnota. LTrbana
Balllatic Reaearch Laba. ,
263
152 709
290
171 212
171 213
171219
171 20B
Mr Force Special Weapon*
CaaMr. Klnland AFA.
Aberdeen Proving Ground.
171 210
Md.
306
149 639
171 220
N. Mn.
334
152 698
901
907
IS2 732
1.52 n9
171221
171 222
Ur Weather Service.
325
152 601
171 223
lean AF8. ni.
279
152 977
Banellc-lnetltut. Frankfurt-
291
171 306
171 207
Aatrlcan Inai. tor Reaaarch.
am Main (Weat Germany)
340
149 657
171 211
Pkiaburgh. Pa.
260
149 642
153 460
Baitelle Memorial Inat. .
Cdumbua. OMo
285
171 944
171 214
171 215
171 217
Imimm Lab. . Ohio State U.
329
171 198
171 318
laaearch Fcundatlon.
339
171 342
292
171 200
l^cluntxi^ Ohio.
283
152 669
Behavioral ISclencea L.ab. ,
171 201
171 201
AaUoch Collefe,
Wright Air Development
171 208
Yallo* Sprlnga. Ohio
263
171 S13
Dlv., Wright -Patteraon
171 216
AFB. Ohio
260
171 332
328
171 20S
ttfUmi Matheimtlca and
mOatica l.aha.. Stanford
263
171 919
336
171 201
318
171 912
CaltfamU Inat. of Tech. .
U., Calif.
317
1S2 S83
Bell Aircraft Corp. ,
Faaadena
328
147 535
teeik Aeromadical Lib. .
Buffalo. N. Y.
289
171 193
CaUfomta U. . Bertelay
282
152 893
LaMAFB. Alaaka
263
153 325
152 893
265
153 336
Bell Telephone Laba. , Inc. ,
318
149 646
266
153 326
Whlppany. N. J.
2*9
149 722
152 606
266
153 328
289
193 6S8
152 607
266
153 341
941
149 721
152 715-1
266
153 342
941
149 729
152 715-2
266
153 351
342
149 724
319
152 375
266
153 353
331
152 916
267
152 695
Biomedical Lah. , Wright
396
152 869
267
153 338
Air Development Dlv. .
267
153 352
Wright -Patteraon AFB.OMo 273
171 909
California U. , Loa At^e*
271
153 390
273
153 331
311
171 308
CalHomla U. , 1.0a Anoele*.
310
153 339
School of Madtdaa
270
153 349
313
153 320
Birmingham U. (Ol. Brit)
289
152 916
271
153 350
335
1^3 346
Bllley Electric Co. ,
Camerhury U. (No*
AnMur Reaearch Foun-
Erie. Pa.
907
152 679
Zealand)
345
147 558
teka. Chlcafo. Ul.
336
337
1.52 730
152 962
•lock Aaaoclate« bic. .
Carnegie Inet. Of Tech. ,
Plctabiirgh. Pa.
941
152 731
Cambridge. Maaa.
940
15J 714-1
318
171 394
M
171 329-1
940
152 714-2
997
152 882
I-l
Catholtc U. o( Anertca.
. D. C.
Cmmt for Mdloviiyaics
and Span Raaearch.
CsnMllU. . hten. N. "
Ccamd Taclarical Imt
T. N. O. , Tte Hafw
(Ndkn-Uada)
Eaclaaerlng
■ lT. n. j.
>u.. u
CtovtM R<
Cotaii
■rchCaaicT
OUo
U. Sckool of
mC Nmr Yorl
OSilM
I and Bxpl
Riiiirch. Inc. . nna
burilt. Pa.
Cooaciidaud Qaccrtr
dywamtca Corp. ,
- ■ CalM.
CaraaU Aerooautlcai Lai i
Inc., Buffalo. N. Y
Conall-DuMim^ Clactr^r
Corp. , tndlanaiiatla
ConailU. , Ithaca. N.Y
CanwUU. Madlcal
CoU. , New York
Chryalar Corp. ,
DaoroU. Mk:h.
Curtlaa- Wrlsta Corp. .
Saou Barbara, CaUf
326
949
27*
27«
27*
342
31 !S
3-26
InL 293
276
279
266
20
2H6
293
Dulah National Conuntitaa
ofUKSl
DmrU Tajrlor Modal Bask.
- - D. C. ^
I Alotrtc Support
A^ocy. WaatHaffoa,
).C. 334
MKala Inforina Ion
, Battalia Mem -
*. , Columtiua,
(mwclOaiiiMy)
Dianoad Ordaaaca Fu»
Lata., WaaWnyon. C
Olractorata <t PI1#« an i
AB-WaathBT Ta^UoL
^1^ raiiiiiaui AFB
bM(. (or
(Blra)
Advaaced
iac. . Scanrford, Coaa
336
257
310
321
311
313
329
330
2m
C. ?93
PwMndt SlinulaUcna L4b. .
Old— mil Tank-AmoiMotlve
Comnand, C«M«r Itn^.
Mch.
Eaat Coaai Ac
lac. . rallMin Mamr.
BducaclOMj Raaearch
144 686
151 .^23
149 675
153 090
153 091
152 906
149 692
fa» W Number
311
337
2i6
333
259
260
3or
294
261
Elacrrlcal Enflnaenng Ra-
aearch Lab. , U. of
Ollnda, Urbana.
Eloctrlcal Englnaaring Re*
aaarch Lab.. U. of
Taxaa. Auatln.
Elactro-OpUcal Syaiema,
Inc.. Paaadena, CalK.
Elsctron Tube and Micro-
wave Lab., Calif. Inat. of
Tech.. Paaadena
J
Eloctron Tube Raaearch Lab
*0
U. of MInneaaia,
2<n
152 254
MhBiaapaiU
319
152 S96
351
152 897 -
Electronic Syatema Lab.,
Maaa. Inai.afTech.,
Caninidfa
314
149 665
Electronlca Reaearch Lab.,
U. al CallfornU. Barkalar
171 303
152 947
149 709
149 681
153 345
153 328
153 624
171 195
171 194
153 279
153 726
152 734
153 574
1.53 080
161 227
161 22^
161 226
151 097
161 213
152 541
152 581
152 655
152 922
153 496
171 OSO
152 923
153 630
152 768
IV>317
147 30Pi
132 845
1S3 273
1S3 63I
Elk Elactronlc Laba.
New York
Fabric Reaearch Laba.
Deifiiam, Maaa.
Inc..
Inc.,
294
2«3
307
342
347
295
286
295
296
319
S3S
296
314
315
316
348
296
286
315
330
296
342
297
330
342
270
343
348
343
297
319
Havatl tiwt. of Geophynlca.
Honolulu 279
Feltaoan Reaearch Laba.,
PIcatlnny Araenal. Dower.
N. ].
Florida U. Engineering and
ladnatrial Expert mam
Station, Calneaville
Fluid Dynamic* Reaearch
; jh. Maa«. Inat. al Tech..
Cambridse
Poater. John J. Mfg. Ca,
Casta Mesa, Call!.
Fuel* Reaearch Lab.. Maaa.
Inat. of Tach.. Cambrida*
al Electric Co.,
Datrolt, Mich.
General Electric Co. ,
Schenectady, N. Y.
General Electric Co. .
Sjrracuae, N. Y.
General Electric Reaearch
Lab., Schenectady. N. ¥.
Georgia Inat. of Tech..
Br^pneering Experiment
Scattcn, Atlanta
Gordon MclUy Lab. of
/Uipilad Science, Harvard
U.. Cambridge, Maa*.
Graacn' Aaaoclacca.
Palo Alto, Calif.
Harvard U., Ca
Herme* Electronlca Co.,
Cambridfe, Maaa.
297
1-2
149 636
149 637
152 486
152 4*9
152 951
1.S3 100
149 706
152 996
1S2 735
152 885
147 314
152 741
1.52 »9
152 861
152 994
147 313
152 860
148 500
152 960
152 992
171 311
150 013
149 963
152 137
152 6CS
149 718
171 306
171 348
149 694
152 610
171 340
152 660
152 958
171 348
152 473
153 343
149 695
149 696
152 7W
149 628
152 671
1S2 369
1.52 371
152 375
152 376
149 668
152 613
149 708
149 709
149 710
SflUCt
Haaae-Eaatam DIv.,
Fllghtex Fabric*,lnc.,
Canbrtdfe. Maaa.
High Altitude Obaervatory,
Boulder. Colo.
311
258
Honeywell Reaearch Cemei;
Hopklna, Mian. 343
Hugtiea Aircraft Ca,
Oliver City, Calif.
Hughea Reaearch Laba.,
Ktelibu, Calif.
Human Factor* Research,
Inc., Loa Angelea. CaUf.
Human Reaource* Research
Office, George Washington
U., Waihlngion, O. C.
Human Sdencea Reaearch,
Inc.. Arlington, Va.
nilnol* Inat. of Tech.,
Chicago
niinda U., Urbana
263
298
264
261
334
324
319
329
344
280
267
ImDerlal Coll., London
(Ot. Brit.)
Inatliui Kir Animallache
Phyaioloaieder J.W.
Goethe Unlverelillt
(Weat Germany)
Inatitute for Fluid Dynamlca
and Applied Mathemailca,
U. of Maryland, College
Park 320
324
faiailtute of Andean Biology,
Lima (Pen* 267
laatltute of Engineering
Ra••arc^ U. of
CallfornU. Berkeley 324
Inatitute of Ceodeay. Photo-
grammetry and Carto-
p-aphy, Ohio State U.
Reaearch Foundation,
Cdumbua 282
Inatitute of Mathematical
Sclencea, New York U.,
N. Y. 320
324
344
349
Inatitute of Optica, U. of
Roctrater, N. Y. 341
Inatitute d Reaearch. Lehigh
U.. Bethlehem, Pa. 330
Institute of Rubber Research,
U of Akron, Ohio 316
institute of Tech., U. of
Mlnneaou. MtnneapolU 320
International Buainea* M*-
cMnea Corp., Kingston N. Y 298
lonoaphere Reaearch Lab..
Pennsylvania State U.,
Umverair/ Park 283
284
29«
153 272
152 946
149 684
152 891
153 3r
152 841
152 888
152 580
153 788
152 821
147 310
152 9n
171 m
152 683
152 774
152 775
1.53 391
152 (
149 729
149 730
152 601
152 763
148 406
152 799
152 BOO
152 431
149 691
152 723
152 842
149 651
153 812
153 173
149 644
152 672
153 274
152 697
152 696
152 823
152 824
larael Inat. of Tech.. Haifa 326 152 479
Uannodl Chlmlta Fialca
dell "Uplveralu. PavU
(Italy)
276
rrr laba.. Fort Wayne, Ind. 352
Reaearch
imorc, Md. 336
].G. Engineering Reaearch
Aasoclates, Baftlr
149 678
171 IW
149 68
^MM Fivrcstal Rssesrch
CaaMT, Prinoston, N.J.
k| Propulsion Lab., Calif.
^Mt. of Tech., Paaadena
U., Lawrence
KaarfoR Co., Inc.,
Uma Palla, N. ].
f—w i) U-. LexIngiLO
L^oratolre de Fsrromag-
natlame. Inatttut de
niyaiquc, Straabourg
(France)
Laboratory (or Inaulaiion
Raaaaii h tMm. Inat. of
Tech., Cambridge
Laboratory of Siatiailcal
Reaearch. U. of
Waahlngion, Seattle
Ltnnai Gedogloal Obser-
vatory, Paliaadea, N. Y.
UiMMarU. (a. Brit.)
UBOda Lab. . Maa*. Iimi.
of Tech., Lexington
I Aircraft Corp. ,
Mariana, Ga.
I n>b«ii1 Aircraft Corp..
Sanyvale, CalK.
I (lUiainl Electronlca Co.,
Mmchan. N. J.
Losall Techndoctcal Inat.
■rch Foundatian,
UadU. (Sweden)
McDonnell Aircraft Corp.,
St. Lonia. Ma
MeOUl U. (Canada)
328
307
311
271
320
307
276
337
298
336
337
320
282
344
264
298
299
300
308
320
321
323
344
349
351
333
258
30«
300
308
276
286
280
Marine Lab., U of Miami.
CenlQMiiss, Fla. '>82
Muryland l>)v Cdle^ Park 2.^8
332
MMaachuaatta Inat. of Tsch.,
Caa^ridr. Maaa. 334
339
348
349
Andisral 275
277
278
M**iichua«tu U.
UMsrial Lab* . PugetSound
Naval Shipyard.
Brsnarton, Waah. 314
ttaartala Lab. , Wri^ Air
Dsvelopmeat OH., Wright -
Htteraon AFB, Ohio 270
PB Number
149 689
153 8*5
153 791
152 619
152 894
152 778
152 746
153 277
149 776
149 728
149 725
1S2 900
152 908
152 925
152 621
153 095
149 741
153 409
152 629
152 750
152 948
152 949
152 721
1 52 759
152 934
152 723
153 053
152 722
152 462
152 932
152 973
149 740
1.52 466
1.52 7r
152 933
153 790
171 196
152 939
152 935
152 522
1S2 47*
149 666
152 952-1
1.52 952-'?
153 625
152 936
149 650
149 732
149 733
152 661
149 639
149 680
152 863
150 036
150 035
149 687
149 631
149 638
152 862
153 573
Sourca Paga
Materiala Resesrch Lsb.,
Watenown Araenal, Maaa. 344
Mathematic* Reaearch On-
ter, U. of Wiaconain,
Mad) eon
324
Melpar, Inc., Falla Church.
Va 300
Metal* and Ceramlca Lab.,
Wright Air Development
DIv.. Wright-Patteraon
AFB. Ohio 3K9
Metal* R
Brown U
rch Lab.,
Providence, R.I. 345
Michigan State U., Eaat
Lanaing 321
Michigan U.. Ann Arbor 347
Michigan U. Resssrch
bist., Ann Arbor 300
Microwave Asaoclatea.
Inc., Burlington, Maaa. 300
Microwave LaL., Stanford
v., Calif. 301
Microwave Phyaica Lab.,
Sylvania Electric Product*,
Inc.. Mountain View,
Calif.
Microwave Reaearch Inat.,
Polytechnic Inat. of
Brooklyn, N. Y.
347
301
313
338
345
350
Mlnneaoia U.. Minneapoii* ''86
Mlnneaota U. School of
Physics, Minneapoii* 258
259
Montpellier U. (France) 319
Moore School of Electrical
Engineering, t'. of Penn-
aylvania, rfdladelpMa
Moioraia, Inc.
Arlx.
PiKjenix.
Narrai
Marine Lab.,
arraganaen Marine
U. afRhode laland,
Kin^on
National Bureau of Standarda
Boulder, Colo.
National Reaearch Lshs.
Ottawa (Canada)
323
324
350
283
350
277
315
326
Naval Air Teat Center.
Patuxent River, Md. 301
Naval Civil Engineering
Lah., Pan Hueneme,
Calif. 313
Naval Engineering Exper-
iment Station. Annapolla,
Md. 310
Naval Ordnance Lab.,
White Oak, Md.
Naval Ordnance Test <:tstiat.
Chins Lake, Calif.
1-3
WWuntar
1S2 154
149 7S*
148 282
171 307
149 690
149 663
171 336
152 995
152 668
152 847
152 937
1S2*M
152 633
152 652
152 724
153 089
149 679
153 088
171 199
148 494
149 645
148 495
152 972
153 596
153 597
171 339
152 993
152 907
151 377-7
153 606
153 476
15? 529
153 195
153 196
152 833
152 940
152 942
153 793
.302
171 353
308
171 352
321
171 349
171 350
171 351
171 354
171 355
345
149 738
780
152 699
15-> 700
308
152 826
1 53 867
313
113 883
Sfliifift
P«»
nHa^SL
Naval Ortbiancc Test StaUon.
China Lake, Calif, (con. )
315
152 S25
Ui
l^^
337
149 654
341
149 643
Naval f>eraonnel Reaearch
Field Activity, San Diego,
CalK.
261
152 626
Naval Postgrsduate School.
Monterey. CalK.
280
153 063
153 064
Naval Radiological Defenae
Lab.. San Fr*nci*co. Calif.
m
1?3???
277
153 588
332
153 071
333
153 622
334
153 621
335
153 068
153 070
153 570
Naval Reaearch Lab.,
Waahington, D.C.
277
150619
284
150 618
302
153 576
153 577
161 968
309
171046
171 061
316
149 850
324
149 297
352
171 315
Naval ^uneraonlc Lab., Maaa.
Inst, of Tech.. CUmbridr
Nsvsl Wsapona Plant,
Waahmyon, D. C.
Navy Underwater Sound Ref-
erence Lab., Orlando, Fla.
New Mexico State U.,
Univeraity Park
New York State CoU. of
Oramica, Alfred U.
New York U.. N. Y.
New York U. Coll. of
Engineering, N. Y.
Nitrofm Oiv. AUIsd Chem-
ical Corp.. Hapewell, Va.
Norake Mateorologlake
Institutt (Norway)
North Carolina State Coll.,
Raleigh
Northrop Corp., Hawthorne,
CalK.
327
331
302
259
Northwestern U.
ni.
Evanaton,
341
345
302
303
331
281
271
2*7
331
34S
Anal yell
U. of California, Loa
Angelea
Ohio Sute U. Resesrch
Foutidstlon, C^umbus
259
264
Cklahoma U. School of Medi-
cine, OUahoma City 268
Oxford U. (Ck. BrU.) 350
Pacific Semlconductara, inc.,
(^Wer City. CalK. 303
RMuiaylvania State U.,
Univeraity Park 325
Pennaylvania State U. Mineral
Induatries Experiment
Station, Unlvereily Park 281
PennaylvaaU U., PMladelphU 257
259
Perkina Obaervatory.
Delaware. Ohio
Personnel Lab. Wrifhl Air
Development t3lv.. Lackland
AFB, Texaa 261
149 344
149 739
152 979
152 968
345 IS2S44
152 624
171 396
153 0S4
152 791
153 085
171 301
152 769
153 332
171 328
152 691
171 SU
322 133 275
152 171
152 913
153 337
152 418
152 6S9
153 109
152 930
152 834
152 171
152 783
\
lLtfl..Wrt#« All
OavrioRBMi Or., Laddind
An.
I (con.)
PImtcal RMMrch Lab..
^aca Tach. Lafaa., Inc.
U» AMriaa. Calif.
n^alcal Scteac* (.ab.. H
Mnico State U..
Untveraity Part
nnalca Lt/h .. Vrt0« Air
Danaloiinww Dly^ «r10i :
PattaraOB A*^. OMo
Plaama PranilsloB Lab.,
RapuUkc AvlattOB Corp.,
Parm^Ma. NY.
naamadvaa Corp., Santa
Ana, daUf.
naatles Tadnlcal Bvalu-
adOB Caatar, Araanal,
Dow. N. ].
rokytmetrnte laat. «( BrtwklK
N. Y.
m.
U.. M. I.
Prapdakai Lab., Wrt^ Afr
DrMlapnaiN Cantar,
iA»^nilo '"T
•aycho
Southern '~altfamla,
Loa An
ryblic Haaltb Sarrtca.
WaaMnyon. 0. C,
U^ LafB)«M. bid.
QuanermaateT Cield Cvali
ation AgeticY, Port Laa,
RavckaflB
COl, WUtham,
:ot Arma Ca, Inc
. Com.
' Polytaetailc hn t.
▼ror. ••• Y.
RaoBbltc Avtatloa Corv.,
Parntfn^la. «>. Y.
U.. N. Y,
Kock laland Araanal Lab.
BL
262
M4
S46
308
?T7
341
312
347
390
316
325
327
338
336
net
m
S?7
Vt.
?*4
273
322
336
275
aoi
346
30*
30*
yn
309
275
277
314
317
332
153 S06
153 572
153 110
152 401
144 647
171 310
171 141
152 744
152 955
152 929
171 aa4
152 779
152 537
152 868
152 730
152 625
152 tSI
149 649
149 677
\V>7i»
1.53 6^
148 004
161 371-9
152 761
152 762
149 688
153 085
14*629
149630
152 628
152 839
15* 840
153 38'
171 337
149 664
153 158
171 M7
130 961
171 0*2
171 013
171 041
SouTca fai
Rackanlyaa, Caao^ Park,
Calif. 312
Rome AIt OvwIoprimK C^n*
tar, GrifHaa AFi«. N. Y. 304
Rowland and Co.,
Haddoaflald, N. ].
Royal HollowavColl., U. of
LoHtoi 'Ot. %nt)
289
Royal Inat. of "^ech. 'Sweden)
Rutflara St«te U., Hew
Vnmawlck N. I.
«l. Loula School of V'edlclne.
Ma
School of Aviation Medicine.
Rrooka APR, ^e,.
Science and Technology ON.,
Library of Congreaa,
WaaUayon. D. C.
Sheffield U. '». Rrtl.)
275
348
274
•»65
■»68
165
■»68
?73
272
278
Slndel S. p. A.. Rome (Italy) 350
30*
275
iectric'o^ SdTadeiphia.1*. 312
SpectroBcopy Lah., Pennayl-
vanla State U., University
Pari!
Sonsiana Corp. , Elmaford,
W. Y.
Southern Feaearch Inat.,
Rirmlngharr, Ala.
Snca Sclancea Lab.. Genera]
•Hect
Stanford Reaearch Inat.,
»%nloPBrk. ^allf.
StockholfniJ. rsweden)
Struthera-Dunn. Inc.,
Pitman, N. I.
SondBtTWrf Turto Wv , Sund-
atraadCorp., Pacoima,
Calif.
Sylvania Electric Producta,
Inc., Senaca Palla. N. Y.
SyrwaiaeU.. W. Y.
Syracuae U. Reaearch Inat.,
V. Y.
'^aclnicai Reaearch Group,
Soarvrrfllc. »'aa«.
'Tacladoal Reaearch Group.
-iiiiim V. Y.
'^achnlache Hochechule.
Kartaruhe 'Weat Germany)
''achBlache Hochechule,
StuRgart 'Weat Certnany)
"Tachniache Hofaachool, Delft
(«letherlanda)
T
304
r
3*»9
3I|
313
30*
322
333
304
30R
3.35
338
■>68
347
328
1-4
P»NUH<)«T
171 30B
161 894-1
149 211
152 767
1.52 789
1.51 772
152 773
152 889
152 617
152 764
152 460
152 630
171 (B9
149 658
149 6S9
152 463
149 693
171 300
152 959
152 864
157 670
152 535
149 704
IS2 856-1
1S2 886-2
152 8S6-3
149 712
152 736
152 737
171 335
152 986
152 776
171 341
152 777
153 087
153 626
149 640
Soarca
: U., KnOKvllle
TMokol Chemical Corp.,
nkton. Md.
"Trana-Tech. Inc.,
Rockrtlle, NM.
Trinity Coll.. Dublin (Eire)
Tufta U. School of Medicine,
Baatoo. Vaaa.
Tulaaa U., Na« Orlaana. La.
Unlveralty of Southern
California, Loa Anfelea
Univertlty of Soiahem
California Engineering
Center, Loa Angeles
'Jnlveralty of Southern
CallfomU School of
Medicine, Loa Angeles
rami
263
268
305
270
268
268
322
269
272
Upper Air Research Lab.,
uTof Utah, Salt Lake City
Veterana Admlnlatratlon
Hoapttal, Long Beach. Calif. 271
WashingEon U., St. Loula. Mo. 323
331
332
333
Waahlnpon U., Seanle
Waahln^on U., Seanle. Coil,
of Engineering
WaaMr^on U.. Seanle, DIv.
of Counaellng and Teallng
Servicaa
Waahinglon U., Seanle.
SchooTof Medicine
WRtertown Araanal Laba.,
Maaa.
Wa
'ayne
v4ch
State U.. Detrctt.
283
314
351
323
269
270
309
330
323
346
351
Wanner -Cren Aeronautical
Reaearch Lab.. Lexlnyon,
Ky. 263
Weather Forecaatlng Reaearch
Center. U. of Chicago. PI. 281
Wcatlnghouae Reaearch Laba.,
Pittsburgh. Pa.
Willow Run Laba.. U. of
Michigan. Ann Arbor
Wlsconain U., Madison
Woods Hole OcssnogrspMc
Institution, Maas.
Yerkaa Obaervatory,
WUItamaRay, Wla.
331
269
306
274
281
259
153 271
152 782
316 1531
153 2M
152 477
152 611
153 S7S
148 086
327 152 557
171 30(
171 343
153 348
284 152 623
153 336
152 747
149 738
149 737
152 911
148 42*
152 44*
152'
148 *0»
153 344
153 3r
152 488
153 0*2
171 0*4
152 43*
152 644
149*85
152 74*
153 Mi
152 888
152*08
152 53*
152*31
152 810
153 r8
SUBJEa INDEX
jybiect
E&K
PPNVBfetr
5M'>J5ret
fsm.
PB Nuntwr
Subject
ram.
TLOmm
Aballan groupa
Antlferromagnet 1 s m
334
152 932
Bibliography (con. )
•-Theory
SIS
152 606
Antipersonnel weapona
--EftectWenees
--Rubber mouata
310
153 793
Accaleradon
271
152 599
257
153 727
■-Phyalologtcal effects
269
171 30*
Applied psychology
262
152 757
-Snow
281
171 190
171 343
Approalmste computation
319
152 375
--Space medicine
272
171 (B9
Aea^Nic%
AcryAc rcalna
--Soivcm eilractlon
336
149 612
320
322
149 730
152 894
153 275
- -Space perception
--Tralolng
-Tranaducera
268
260
293
159 575
171 332
153 496
316
149 963
Aptitude teets
Biolflglcal productivity
283
152 907
--Tsmpersture factors
316
149 850
--Effectiveness
261
152 626
Birda
Aerial ptatography
262
153 572
-Alaaka
279
153 345
"Aatarctic regtona
349
152 987
-Standards
262
152 756
Blaat aflacta
Aerial raconnaUsancc
Aquatic animala
-Slmulatloa
314
171 0*7
-Psychological (actors
264
153 387
"Nutrition
283
152 907
Blood
153 348
152 368
Aerial warfare
Arctic reglona
- -Coagulation
272
--8U>ll^gr»phy
263
334
153 387
152 821
--Physiological effects
Arctic sleds
267
153 352
--Pathology
Blood circulation
271
Aerodynamic data
--Design
313
152 942
--Temperature (actora
266
153 342
--Rsdu— f^
325
152 843
Argon
--Spertrographlc analysis
Blood dots
-Tables
326
152 479
338
152 664
- Inhibition
267
152 690
Aerodynamic heating
Aaroalaattc Interaction
327
285
152 557
171 192
--Teat methods
309
153 062
Blood volume
--Determination
268
152 617
Aeroioglcal sunde
Aaroapace
281
?72
152.541
171029
— Vlbrstlon
307
ISH 845
--'Motion
259
149 211
Apt. 8
325
152 556
--Arctic regions
780
153 063
Body temperature
"Oanalty
284
152 623
--Climatic tactora
265
153 336
"Puriflcailon
.*>•
171046
--Heat transfer
349
149 740
266
153 351
f
171 061
'80
1<3 063
Borel-Weil theorem
318
152 607
AlrMaai
280
153 064
Boron compounda (Organic)
--Msaaurement
306
149 633
--Moleture content
284
150 618
-Synthaaia
275
152 767
Aircraft
--Tetnperature
280
153 064
Boron halldea
--Ice lormation
279
152 977
Almoaphenc refraction
--Chemical reactiona
275
152 767
286
153 630
--Measurement
283
152 951
Boron hvdrldes
--Toalc effects
-- Mater lala
287
171 328
Atmoapherlc sounding
273
171 309
--StabUlty
285
171 192
--Instrumentation
283
153 060
Boundary layer
"Suparaonlc character-
Atmoepherlca
336
153 279
--Mathematical analvsis
Boundary laver control
327
152 738
Jatlcs
285
171 1«2
Atomic bomb exploelone
334
152 821
"Take-off
286
153 630
Atonic epectra
-- Effect Iveneaa
326
153 196
AirfoUa
"Dater ml nation
338
152 664
Broadband antennae
--hkxlel teat raaulls
325
152 556
Atomic structures
288
152 728
--Supersonic characier-
"Msthe mat leal analyais
339
149 639
Brune network
294
149 636
iatlca
326
152 479
Atoms
Bu ma
Airframes
--Chemical reactions
278
149 659
--Pathological effecta
--Production
271
152 368
"Development
285
152 967
--Ionization
339
149 639
271
152 599
-Mucrlals
330
161 213
Attention
Butadienes
Airplane panala
--Phvalologlcal (actors
Anitudes
264
152 8«8
-PalymeriMtlan
332
171 041
--Flutter
286
171 199
Cadmium aulfide cryatala
--Sandwich conat ruction
286
149 718
"Msaaurement
262
153 271
--Electrical ptopertlaa
345
171 338
--Supersonic character-
265
152 782
Calibration
let lea
286
171 199
Auiocnats
324
171 339
--Equipmetit
C:alori meters
336
171 20B
Aiaakan Indian
266
153 328
Aviation medicine
Alcoboia
- -Bibliography
265
171 333
"Analyais
348
152 966
"Chemlral effects
276
152 746
272
171 029
Cancra shutters
"Surface tenalon
277
150 619
Aviation gersonnel
--IVvelopfnefit
352
171 197
Atpkra
"Anitudes
762
153 '71
Cameraa
^Tli«»y
317
152 675
26S
157 782
--Equipment
352
152 565
318
152 607
--Claaaiflcation
261
153 631
Capaclunce bridge -
322
149 649
762
153 572
--Appkcatlona
289
171 219
Alkaline batterlca
-■Performance
262
153 506
290
171220
--Otvelopmeni
304
149 693
--Selection
261
153 631
171 221
AUaya
--Tenperkturc (actors
"Taadng equipment
"Teat methods
261
i. 53 631
171222
330
171 348
--Training
260
171 332
171223
330
171 348
8-47
286
153 630
Capacttora
"USSR
329
171 331
Backward wave amplifiers
--Callbratlor
289
171219
AkHHaam
--Development
295
152 994
290
171220
--■aaiatlacu
314
171 047
Bacteria
171 221
AkMtMMaUoya
--Detection
271
152 368
171222
"CtaUag
330
152 463
--Muuilone
270
152 477
171 223
"Machanlcal properties
287
171 328
Bacterial aeroeols
CapUlarlea
J30
152 463
270
153 343
--Blood circulation
267
152 690
"MKallurgy
Ahuniaum alloys
329
149 655
Bahamas circle
279
152 9QB
Carbon
Balancee
--Muclear reactiona
331
152 916
"Srraaees
287
171 328
-Calibration
336
171202
--Temperature (actors
287
171 328
Ballistic data
--Abaorption
309
171046
ftwlaaa
--Notnograptia
306
152 7S2
Carbc ships
--Motacular atnicturc
276
152 746
Banerles
--Model test reaulta
310
152 734
--OHidailan
275
153 085
--Appllcailons
29B
149 726
Cargo vehiclea
--Arctic regiona
Aaanaters
Banery chargers
313
152 940
"Calibration
290
171 210
- - Devel opment
293
149 708
152 9*2
AmIiIIiIiiis vehiclea
"Daaip
313
152 940
Beachee
--Maaaachuaetts
278
149 638
--Dealgn
Cathode rsy tubea
313
tSZM*
Amfitfl^s
--Devdopmeat
304
149 712
"Circuits
302
153 576
158 577
--Physical prc^rtles
BlSliogra-'hy
314
157 446
Cathodes (Electron.tubaa)
338
152 960
"Oealgn
325
1.52 M3
--Aerial reconnaissance
763
153 387
--Materials
295
•PI'S
AH/00A-2(XW-|)
300
141 2tl
--Aerlsl warfare
334
1 52 821
296
152*10
AH/PPN-iyXE-2)
3S0
1.52 993
--Aviatio.1 medicine
?6.»
171 333
337
1S2 9M
AN/PR Ml 4
296
152 992
27?
171 029
--Teal reaulta
304
152*7*
Aaslyals of vsrisnce
318
171 334
--Caating realna
--David Taylor Model
Baaln. Wsshlngton. D. C
316
171 094
C^auchy problem
321
171 951
AaUvtic functions
--Tbaory
322
149 649
. 257
153 726
Cavitation
--Meaaurement
328
147 535
Aaalytic spacaa
322
149 649
--Diamond Ordnance Fuse
Cavity reaonators
lahe., Waahlngton. D.C.293
153 496
--Deain
Calaatlar macbanica
298
159 OM
"Muhemailcal aaalyaia
299
152 949
--Human engineering
265
171 333
258
171 196
3CS
152 776
--lea
281
171 190
309
171397
"Marizailon
288
152 728
--Icoaoacopaa
341
149 643
C«itlpada
301
152 997
"SyKhaala
298
1S2 841
--Job analyaia
264
153 110
Cantiifugal pumpa
AflMiMa
--Optics
341
149*43
-Dealgn
SI2
151 8B6-I
**bi9adaiKe
301
152 833
- - Pet malroal
281
171 190
152 856-2
" Mathematical analyai*
295
152 861
--Photoelectric shuners
341
149 643
313
152 8S6-3
Aalosrroalve palnu
-Piezoelectric materUls
341
149 643
* * Pc 1 TorniAncc
312
152 856-1
"Taac raaulu
314
152 Ml
--Reasoning
264
153 110
152 866-2
1-5
Subteci
CawrllU^ puinpa (con.
- -hrformjKc (cok )
CaraaMc rnmtap
"Tmc raaulu
CaraMic naMrtala
-OMtiapnaM
Put W NumbeT
313
314
CkaiacMr rccopilcioi
Clwmieal element!
"DMcrnnliiaUcn
CbMMcal reactions
■ 'Temperature factor*
Ckamical varfare agema
""Ajaorptior
-•Cdorl metric analysii
' "Counter mcaaur—
"DMactlon
CmOrm
--niyaiaiofy
Clitoide lona
--Deternilfiailan
CMorcptiytU
"Phaochemlcal reactl4is
CHarofUm ^
Circular colla
m
era
--Accepcabfllty
--Military requtretnenti
Cloud chamber!
^-^icatl-a
--Aaalrals
--Ice formailon
Cctb Sea mount
Coabuatlon
--Aaalyala
Cofmnunlcatlon ajalai—
--Siaial to adae rado
"Ttaory
Camnutaiors
ClrcHKarjr a'
-call
"RKholofy
- 'niyalcaTfactora
Ctntia douda
--MeworologicaJ factor i
Chnlian detenae •yatenw
CUmaitc factors
275
2t»
274
m
■»7?
172
27?
339
2*7
174
27S
278
MB
267
272
2M
280
334
CnwBlii jam
"Amlymia
--Spectra
Coafta-fiiBl mapping
--Ttoary
Coirical bodlaa
--Haai tranadar
--RaOactlre eOecta
CoKrci ayatema
--Oaalgn
"Oavelopment
--Mathematical analjnli
--ScaWUty
* * 1 eat methofla
-Thaary
••T)mery
Coordinate conyener
Capolyinerlzaiian
--Cryatal acnictura
CarraUaon (uactiona
- -Appilcationa
--Oaiertrinattan
CoBmlc radlatldB
"Ceapnyaical (actor*
"Meaauremeiu
"NUdaar reactlona
--Phvalcal effacta
--PQUrizaUoD
r fla>
Ctwall a method
Croaaed field sn^iflara
Cryatal flliera
--Drrelnpiw
Cryatal oacUlatora
- -Circulta
--OMi»i
Cryatal airucture
--MMhamatlcal aaalyato
S36
336
331
'81
280
783
303
288
SOS
322
274
276
323
286
350
303
324
2«
2«
307
302
fit
374
316
946
346
2««
257
S23
333
259
331
258
259
331
331
332
327
328
348
332
309
300
297
293
789
152 856-3
171 193
171 047
336 149728
153 083
1S1936
IS3 57I
149 659
149634
149 634
149 635
149 641
157 763
ISUTTS
149 658
149 668
171 3S3
1S3 33S
IS3 348
132 460
152 700
152 821
279 153 345
149 688
149 688
149 736
15? 870
153:»9I
I48 4'»6
776 1*3 090
1*2 791
152 984
152 791
152 761
152 762
152 772
152 773
149 681
152 436
171 195
153 088
153 035
171 339
152 741
152 741
152 778
153 004
149 663
149797
149 963
157 6*4
15»694
15? 861
1*204
148 609
152 911
152 968
149 736
148 494
149 645
148 495
149 736
152 916
149 737
149 677
152 867
152 KS
152 789
149 650
171 337
152 995
149 708
149 709
149 710
157 922
149 7??
152 658
M5 149 679
Subfct
Cryatal at ructura (con. )
--Thaory
Cryatal units
--Development
Cryatala
--laical propertlea
- -Tnarmodynamic
fnfnximm
Cualaa
Curaoi
Curaai-aarTh computatlona
Curaad mirrors
--Corroalon
Cyanidaa
--Spectra
Cydic cooBounda
--Mdacular structure
--Spectra
--Synthaeia
Cylladars
- - ElectromagnaWc
propeniea
--Kkierlsls
"Maihemaiical snalyala
--Reflective effects
CyllBdrlcal shells
--Deformstioo
- -Streaaea
--VlbraUoa
Cylochroow c
--hiriflcatian
Dark adaption
Dau
--Proceaalng
Dau atorafe syatema
- -Circulta
--Coding
--Oaalgn
--Oevclapment
--Military reaulramama
Data tranamlaalan systems
--Qrcults
--Daairi
--Errora
Delay llnea
"Applications
Ocatruciive lestlng
Oeatructors
--M'AI
Oeuteriaia
- -Scattering
Dtasraptia
Dtalactrlc propertlea
- - Meaaurement
[)lelactrica
" -Oevalopfnem
--Mathennatlcal snalyala
--Rafractlve propertlea
DIaa
--Production
DMarance equatlona
DIflerence flelda
Difference method
DIflareaUal aquailona
--AapUcatlona
--Tlieory
Diffraction
--Mathematical aiMlyaia
'-Meaaurement
-'Theory
Diffuaion
' ' Mathematical anal yals
Diodes
"Aanllcationa
Dtpoie antennas
"Deaign
Directloa finding antennas
"Daal«i
Diaaaae carriera
'-Alaaka
OidpUy ayatema
--uarelopment
--Human engineering
DIveralty sysiema
' ' Developtnenl
Draa
--Matkamatical analyais
Dyaa
"Riyalcal propertlea
Early warning radar
systems (Airborne)
'-fcrformance
Earth
--Radlailan
Econotnic canditloaa
"Haiti
"Honduras
Ela«ic ahells
"Stresses
Elaatlcity
--Mathematical analyeia
i-6
339
307
341
344
260
299
331
276
77<
339
339
275
338
337
338
349
324
324
336
269
302
300
296
351
300
299
351
297
300
3*1
299
351
306
332
301
345
336
345
343
313
320
317
318
295
320
322
344
350
336
349
344
299
784
297
273
299
306
263
288
306
314
299
332
2S2
2«2
324
924
PB Number
152 863
152 673
152 624
152 725
153 460
149 741
149 799
149 681
149 664
171 342
171 342
149 664
152 777
152 923
152 777
152 842
149 691
149 691
149 682
152 470
161 968
152 935
147 313
152 787
152 935
152 409
152 7r
152 988
152 7?l
152 933
152 629
15? 897
152 596
149 732
152 833
152 544
149 728
152 544
149 628
152 724
149 644
152 675
152 715-1
152 715-2
152 741
149 644
153 3C
152 725
153 088
152 790
152 84?
152 60
152 750
1S2 629
152 671
159 331
152 409
152 536
171 313
152 984
153 068
1S2 446
149 741
149 650
152 893
152 892
148 405
149 691
1 49 756
El
iilUfiSL
' (con.)
Elaaiofnars
"Moiecular structure
--Siresaea
Electric batteriea
"Development
Electric discharges
"Physical factors
Electric fields
--niyalcal rffacts
Electric fillers
"Oesion
"DeveTopmrnt
Electric propulsion
"Inairu mentation
Electric relays
"Development
Blactrical equlpineni
"Calibration
Electrical networka
' -Mathematical analyais
-'hrformance
"Synt heals
Electrocardiography
"Teat reaults
Electrochemistry
Electrodes
- -Polarization
Electrolytic cella
- -Temperature (actors
Elaetromagnetic flelda
--Mat he mat lea] analyaia
Elactrofnagneiic theory
"Mathematical analyaia
Electromagnetic •avea
"Dl (fraction
'-Propagation
-RefMctlon
"Scanerlng
Electron beama
-Analyais
'-(}an(lgurstion
--Control
- -Electromagnetic effacta
Electron pins
"Design
Electron optica
Electron tube heacara
--Design
Elaaron tubea
"Life expectancy
Electronic circulta
- -Development
"EquipmetM
Electronic e<|uipfneni
"Coating
-"Development
-"Human engineering
-■Performance
Electronic ayatema
"Preearvation
Elect rona
--Denaity
"Electrical effacu
"Energy
'"Intenaity
Emoilona
"Psychological effects
Encapaulatlng technlquea
Encke* method
Equations of state
'- Determination
Errora
-Theory
EaUmaa
""Phyalology
Evaporation
--Meaaurement
Exhauat dlffuaera
-- Effect Iveneaa
Exhauat pases
- -Heat transfer
■ Phvsicsl effects
Excapnerr
Experimental data
-Siatiatical analyaia
Ezpinlvc chargaa
--Blaat
Expisure
"-PhyalolQtlcal effacta
Paae F» Numfrg
324 152 60»
316
316
311
325
342
299
292
311
309
292
294
295
304
294
29S
296
304
268
267
276
298
338
338
336
350
347
349
350
298
920
349
351
300
301
338
299
301
398
304
319
298
293
305
295
300
304
294
20
949
399
949
269
916
309
344
392
266
277
911
348
287
258
919
906
2«5
153 172
153 172
171 OSO
152 602
152 473
152 629
152 254
171 050
149 701
171 201
171 208
149 637
147 314
152 986
149 636
152 486
152 489
147 314
152 860
152 986
152 460
152 763
149 675
149 726
276 149 675
152 861
152 86«
152 869
153 088
152 633
152 987
152 418
152 929
152 963
152 993
152 823
152 824
152 431
152 842
152 981
152 99S
152 9)8
152 960
152 9M
152 938
152 9(0
149 712
152 896
152 672
149 708
171 345
152 859
152 935
161 894"l
153 273
152 697
152 SU
171 995
147 558
159 325
171 014 ,
171 997
152 725
152 796
159 928
153 941
199 601
171 901
152 916
153 629
152 996
152 M
149 699
153 996
Pue W Number
?sat ntJ^w^T
Bxpoaure (con. )
■-Fhyalolagical effecta(con.> 266
267
F-86
Paetor analyais
--Applicsilons
Parrltes
•-Applications
-- Elect romapietic
propertlea
•-Magnetic propertlea
-Molding
•-Propertlea
""Temperature factora
FcrrotTWgnrtic cryatala
"-Analysis
""Msgnetic properties
Ferromagnetic nuteriala
"'Applications
-- Development
"Magnetic propertlaa
--Theory
Parromagnetlam
- -Theory
Pleld einlsslan
' --Equipment
- ' Inst ru menisiion
PillM cabinets
"Dainoiltion
Plre coitrol
"Mathematical analysis
Ptsaion fragments
--Spectra
Flame pronagatlon
•-Analyaia
Flaaa
268
269
286
?62
264
?93
297
337
3*0
345
313
301
345
336
344
306
306
337
338
FlMt decks
•-Equipment
Pli^ simulstors
--U»velapmei«
Fluid floar
--Stability
••Turbulence
-•Vlacoaity
Flaida
Heat (ranafcr
Fluortinatrlc method
Fluorine cuiapuunda (Organic)
"Surface propertlea
"Syntheaia
Flutter
"Matheinatlcat analyaia
Flying platforma
""Daaign
Fourier series
--Applicailans
Fourier tranaforma
Free radicals
""Detection '
-"Spectrographir analyais
PraCRiency meters
"■rallbration
Frequency shift keyera
"-Mathematical analyaia .
Froatbtte
--Therapy
Fuel cells
Fuels
--Toaic effects
Functions
"Aaalyala
"Theory
(Samaa theory
""Appllcstlana
Gamma radiation
""Chemical effecta
-"Meaauretnani
--Penetration
"Reflection
Gaa dtachargea
"Analyaia
Qunom
"Analyais
"Mathematical analyaia
Oaa Ionization
•-Electrical factora
-Meaaurement
276
904
906
307
776
273
991
286
327
328
326
327
328
348
349
272
277
274
285
285
782
3?0
777
776
■>97
788
266
311
322
917
319
338
332
333
335
335
"Cottihustlon
--Thermodynamic
propertlea
Gandare system
3?7
276
327
333
348
348
776
914
979
159 951
152 695
153 338
153 392
152 618
153 337
153 344
153 630
1*8*06
148 004
152*81
1*2 660
1*2 929
152 418
149 798
152 724
152 847
149 798
149 728
152 854
159 226
153 226
153 277
152 868
337 149 654
152 770
152 670
15? 596
152 845
1*9 030
1*9 090
1'3 331
149 799
152 885
152 857
152 858
149 686
152 857
152 858
150 036
150 035
149 634
150619
149 683
147 554
159 624
152 799
157 431
171 310
15? 770
171 »I6
1*? 985
153 9*3
171 060
279 171 909
152 737
152 674
152 375
152 777
319 148 900
171 041
153 790
171 341
171 941
998 159 089
152 798
159 091
149 677
171 995
I5'> 789
157 137
1*9 010
149 665
IS? W»
Oeogrsptiy
"Haiti
"-Honduraa
Geotogy
Ormenium
--Dielectric propertlea
-"Impurities
- -niotoconductivlty
"'Tempersture factora
Qaciera
"Geophyaical effecta
Qydnea
--Phyaioio0ca1 effecta
Craft copolvmera
Gravity
--Determination
Gravity anotnaliea
Graan function
Graaada*
--Oa^a
'-E17in
-*M6
--StabUiiy
Group dyna mica
--^ycnologlcal factors
Gr
oup* (Ml
(Mathematlca)
Hall
-'Growth
"Phvalcal propertlea
"VeSocltv
Harnwnic functlois
"Determination
HsriTtonii.' oscillstors
"Siatiatical analyais
Hartree'Fock
Heart
' -Phyalology
Heart beat
--Meaauremeni
Heat e<(uatiar
Heat production (Biology)
"Meaaurement
Heat realstsnt alloya
--Mechanical propertlea
-•Metallurgy
Heat t ranafcr
--Determination
--Meaaurement
Hallcopler rotora
--Flutter
Hellcoptera
--Control ayatema
"Deaign
--Ice formation
--Lateral stability
•-Loigitudlnal atahllity
Helium
--Spectrs
"Spectrographic analysis
Heparin
--niyalologlcal effecta
High altitude
"Phyalcal effecta
--niyaioiogical effecta
High preaaure research
High speed rsmerss
--Appllcaiiana
-- Development
--Equipment
High apaad photography
"Applicatlona
High temperature reaearch
Hubert apace
Human engineering
"BlWIogrsphy
'-Military requlremeiKa
Hydrazine derivativea
""Chemical reactions
Hydrocarbona •
--Electrical propertlea
--(Dptlcal propertlea
--Spectra
Hydrofotla
--Cavitation
Hydrogen
-"Propellani propertlea
Hydroptunes
"DaaiBi
Hyperbaric aquations
--Theory
Hypersonic flow
--Boundary layer
--Heat tranafer
Hyperaonlc teat veMclea
--Aertalynamic
charscterlatlca
282
282
278
343
344
344
344
266
316
282
282
919
998
306
306
306
906
264
265
929
218
929
280
280
280
922
319
339
944
268
319
329
330
329
327
348
287
286
326
287
287
258
338
315
767
390
906
941
3S7
306
276
330
322
265
259
275
337
277
278
328
311
302
318
327
326
327
152 893
152 892
149 698
149 628
152 979
152 979
152 979
278 149 698
1 53 353
149 963
152 799
152 800
152 799
152 800
152 369
152 777
152 597
152 597
152 597
152 597
152 913
152 889
152 436
152 607
152 747
153 391
152 775
152 774
148 066
148 500
149 639
!*■> 854
768 152 460
153 087
152 376
268 153 397
171 198
152 463
149 655
152 557
152 966
285 147 554
152 625
149 666
153 195
152 625
152 831
152 946
152 664
267 I *2 690
171 306
15? 769
171 948
171 95?
171 191
171 197
171 952
149 675
171 348
152 761
152 762
171 333
149 211
149 687
149 725
149 631
171 300
147 535
153 791
152 979
149 646
1*2 597
152 947
152 597
286 171 195
SlibiiSt
Hyperaonlc teat vehiclea (con)
""Recording devlcea
Hypersonic wind tunnels
""Equlpmem
Hvperveloclty protectilea -
'-"Penetration
Hyperveloclty vehiclea
""Control ayatema
Hypothermia
"-Phyaloioglcal effects
Ice
--Ubiiography
--Radar analyaia
- -Thlckneaa
Ice cryatal*
- -Growth
Ice formation (Aeronautica)
""Meteoroioglcal factora
-"Simulation
Iconoacopea
"BIbllagraphy
Impact ahock
--Meaaurement
-Phyalcal effecta
Impact teatlng
Impedance
- - Meaaurement
Incendiary mixturea
--Effectlveneaa
- -Teat reaulta
Indium fllma
" "Superconductivity
Inaqauitlea
Infarmation theory
Pat f Number
293 171 194
327
907
281
949
949
spoiyn(
Infrared detecltira
-Deaign
""Equlptnent
--Signal to noiae ratio
Infrared equipmeiH (Airborne)
- -Development
Infrared filtera
""Appilcationa
--Development
--Materials
Infrared optical materiala
--Development
Infrared apectra
--Aialyala
Infrared wavca
- - Abaorptlon
- - Maaauremeni
Inatmctora
--Attttudea
InairunwKa
' -CallbratiOB
Integral equailona
Integral functlona
Interferometer*
"Applicatiaoa
Interior balliatic*
--Mathematical analyaia
International (jaophysical
Year
Ion beama
-'Application
Ion bombardment
"Appllcatiana
Ion exchange
-'Theory
Ion exchange realna
"Appilcationa
'.-Tnaory
Ian prtxwlaion
Ion rocJcet propulalon
279
326
941
311
307
314
301
303
271
906
346
318
308
909
951
919
307
399
340
340
341
340
340
999
940
341
339
339
340
260
289
290
291
292
328
396
320
319
940
906
258
281
906
950
312
393
277
269
277
312
310
149 344
907 152 729
192 778
266 159 342
171 190
152 987
152 987
280 152 779
152 977
159 196
149 643
159 272
152 729
171 911
152 899
149 647
1S2 599
182 596
152 901
149 646
159 CS4
153 085
152 7r
152 971
153 100
149 641
152 714-9
152 714-2
152 714-4
152 719
152 714-1
149 657
149 641
149 657
152 624
171 342
171 942
152 714-4
149 642
171 209
171 212
171 219
171 206
171 210
171 220
171 221
171 222
171 223
171 206
171 207
171 211
171 214
171 215
171 217
171 218
171 200
171 201
171 204
171 206
171 216
171 203
171 2(B
149 729
152 431
152 972
152 714-4
152 732
148 494
152 990
152 522
i-i 377-7
171 305
171 995
199 5«
152 470
159 588
171 906
159 sr
1-7
propa^Uoa
jobaMlri
-An
rau
-ApotlcaUona
-BOMlOfraptqr
-Mycfaoiaglcsl facwa
' 'rr manitolda
Kaatrowln problem
KIdMya
"Bood drcutadii
KljFatraM
fiUB fl Nttn<>eT
--T«M mthodi
-BnatoB
[■■■dint mata
--AffUcatlona
LMdHthtrMe
"Qactiical proparttaa
Laaxalaf
--T«a( mathads
Ll« grou^
un
"Aadlinla
--nqratcal aftacta
"fkvalotoglcaJ effecta
"Marlxation
"Scatiarlac
I lair acceleraiora
lam
jrrmem
* - Vainrlzailaa
UtWuin hydroKldea
--Api^icatlcna
""^
■leu
UoHUr
I afci k aan
"Tanparanira factora
"Taai reaulu
--Pkjralcal tactora
MacMaa iraaalatlona
- -laacrunnentatlan
lium oalda cryaula
MBMsaium oa
tn
in
349
MO
3(4
298
949
3M
297
34*
34a
331
sr
337
3t«
31^
31 «
310
761
264
264
323
276
299
294
S3»
331
2«7
2r
3SI
349
260
311
337
266
?77
277
301
26«
277
277
Mafltadc corea
- -Davaiapmeat
MapwUc flelda
--Maihemaiical analysla ]
--Phyatcal effect*
MaflMOc material*
-^SpecTra(rapMc analjrai i
majwHc iTwdea
MamyHf reaonaace
- -Theory
M^lietlc tapea
--Teat reault*
Mtgaato-hydrodynamic wa^ea
--AppUcatlciM
--Pro^apuian
Magneto- loBlc ducta
30S
339
315
SIS
341
351
343
329
344
349
344
337
aoaatroaa
' - uavtfflyoiant
! peraonnel
'Pai fui fnajice
-Teat mrthada
293
346
312
346
350
303
33«
261
261
14*736
I4«495
152 697
153 060
147 ssa
152 963
152 696
152 63
152 124
152 466
153 279
152 9sa
152 7*9
152 137
152 691
153 r7
153 277
171 306
'71 308
171 30S
14«777
1^2 7i3
I S3 no
153 no
153 436
153 091
M» 171 343
152 941
152 489
171 OM
149 739
153 639
153 639
149 68S
171 356
153 460
152 606
326 153 196
149 654
153 326
149 631
149 631
193 6S3
152 618
153 606
153 606
309 171 046
149 647
149 641
153 476
153 476
153 731
149 685
149 684
153 •»74
!<■» 854
15' «'>3
1^? 462
153 923
338 152
171 1^
152 742
152 749
152 912
152 963
149 630
153 960
153 788
IS2 783
Mammal I
-Alaaka
Marine Molocy
- -Pacific Oceaa
Mara
--Exploration
Maaa apactrometera
--Apiiilcatlana
Mathemailcal computer di
-Codlnt
-Prooeaalnf
i computera
rAapllcatlana
rClrciiiu
VOaalcn
'-Bqulpmeni
--Hamaii engineering
-Sciwiullng
--Theory
Mathematical logic
Mathematical oredlctian
--Appllcailona
Matrix algebra
--Apolicailona
Meaaure theory
Mechanica (Peraonnel)
--Teat methoda
279
283
283
WWyil^f
153 345
152 907
148 426
306 152 989
276 153 770
--[>Bcay
--Nuclear reactlona
--Ptlariiatlcn
etaboUam
- -aimatic faciflra
324
335
323
263
299
324
323
323
258
307
320
321
323
324
321
335
320
294
322
262
332
333
332
366
367
268
269
149 297
171 341
153 596
153 597
153 703
153 750
149 297
153 274
153 596
153 597
171 196
153 845
153 894
153 033
149 609
152 722
171 339
153 723
153 070
152 894
149 637
153 737
152 756
149 733
149 737
152 911
149 737
153 341
153 351
152 695
152 618
153 344
Metallurgy
-USSR
329
171 307
Metala
--Availability
329
161 336
--Corraelon
285
171 344
331
171 301
330
153 882
--Olflualan
344
152 683
--"racture
330
153 882
--Heat treatment
330
l6l 213
--MacMnlng
313
l6l 225
--Macbaaical propertiea
329
171 198
--Procaaatng
37^
153 109
--Prodactlon
329
161 226
Metaorolagtcal ballona
--Applicallana
258
148 494
259
148 495
--Plight paiha
280
152 699
Meteorolocical charla
--Northern hemiaphere
281
152 930
-GrecnUnd
280
152 952-1
152 952-2
--North America
280
I52 9S2-I
152 952-2
--Proceaalng
279
152 905
--Recording devlcea
-Siatlatlcal analyaia
280
152 699
278
152 701
280
153 064
281
153 769
-TaWea
280
152 952-1
152 9S2-2
--TranamlaaloB
278
152 684
Metaort^ioglcal radar
--Appllcatlona
280
152 774
334
152 661
Metaoroiagy
--AaU
279
149 668
157 613
--PacMIc Ocean
279
153 613
--Tropical regiona
279
149 668
157 613
Metric apace*
332
152 736
MicMgan
369
152 60B
SOR
152 536
Mlcraorfanlama
■-Vlabirity
270
153 573
MiCTopbonea
-Daalgn
Mlcroachnldl
296
259
152 603
153 278
Mlcrovave amplltlera
--Davelopment
300
152 995
Microwave equipment
301
152 847
--Calibration
292
171 204
--Development
393
153 581
--Material*
397
152 660
306
153 226
Mlcrovarc oadUator*
-DevelcpnKM 300 152 995
Mlcrtwave*
-Refraction 383 1S3 951
1-8
MUiury peraonnel
--Alaaka
--Nutrklon
Mtnlaiure electronic equlpntwrn
--Circuit*
--Dealcn
- - DeveTopment
Mirror*
--Electroformlng
- -Preparation
Mlaaile aotennaa
--Dealgn
Miaallc booatera
-Material*
Mlaaile peraonnel
--Training
Mlaaile tracking ayatema
-Itendbook*
Mlaailca
--Drag
--Electrical ayatema
- -Stability
Molecular aaaociatlon
-Energy
Molecular beama
•-Reflection
-Velocity
Molacular aleve
Molecular apectroacopy
Moiacular atructure
--Theory
Moieculc*
--Enerfy
Molller (Uagrama
Moon
-- Exploration
- - Reflective effect*
-Motion
Motion picture acreena
--Dealgn
Motor reactlona
--Msaaurement
Multipath tranamlaaion
--Appllcatiana
Naval aviation
- -Training devicea
Naval ordnance
-Teat facllltiea
Naval peraonnel
--Selection
Naval reaearch
Naval reaerve
NegMlve iona
I ayaiem
liolog;
-Phyaiology
310
310
298
296
293
313
341
303
316
261
261
306
309
306
276
311
257
349
358
3S2
263
288
260
308
261
352
261
348
270
271
Neutron fluxea
- -Meaauremen*
Neutrona
--Scattering
Newtonian theory
Nickel
-Bonding
- - Electrodepoaition
-Streaaea
Nickel alloya
--Aopllcatiana
--MKhanical propertiea
Night flight
--Viaual factora
Night televiaion
Niiropen ogtidea
- -Corroaive effecu
Noise (Radio)
--Analyaia
-- Meaaure ment
Non-deatructlve teating
--Applicationa
Non -linear differential equatlona
--Theory
Nuclear reactlona
--Mathematical analyaia
Nuclei
-Magnetic fielda
Nucleic aclda
--Analyaia
Nuntfier*
--Theory
Ocean bottom
--Atlantic Ocean
Oceanographlcal dau
•-Atlantic Ocean
Officer peraonnel
--Selection
Operatora (Mathemaiica)
--Tliaory
Optical Imaoea
- - Meteorological factora
Optica
--Bibliography
332
306
331
313
331
296
309
266
302
331
302
350
309
320
332
344
269
320
332
282
282
261
262
322
318
333
357
341
153 339
153 339
152 673
152 608
152 913
153 881
171 191
149 647
153 620
152 580
152 588
153 OU
149 701
153 OM
278 149 659
337
337
309
339
339
142 882
152 881
171 OBI
152 863
149 680
152 68S
153 091
153 791
152 846
152 466
171 196
153 997
153 744
152 984
149 642
153 867
152 636
171 315
152 626
152 ir
153 349
153 330
153 3S0
333 153790
149 732. '
153 0B8
152 888
153 88S
152 880
152 735
153 011
153 336
161 968
171301
153 576
153 577
151 377-7
152 988
149 730
149 733
152 1B4
153 740
152 894
152 736
152 908
153 625
152 626
153 572
152 761
152 7*2
149 646
152 747
152 834
149 643
Subject
Im.
PB Nunter
Subiest
Sam.
nnuatmr
Mjaa.
Bmi flNvBte
Or^aacc ateel
Planetary atmoapherea
Radar urpata
"Tenperatura factora
309
153 062
--Density
. 358
152 936.
-Detection
293
52 653
ftpalr conyaiada
Plaoeta
Radiation
-Conductivity
342
171 340
"Catalog
358
171 196
- -Chemical effecu
•277
71 310
■-Photochemical reactlona
276
152 770
Plasma (niyalca)
301
152 847
--Meaaure ment
340
52 714-3
-Seperatloo
309
171 061 ,
312
152 749
--Physiological effecta
273
152 630
Ortfaality
OliSe cathode*
264
152 913
152 959
■-Sourcea
258
49 645
338
152 664
Radiation countera
"Perlormance
295
152 735
152 960
-Calibratlan
333
52 768
Orimea
153 069
Radiation damage
"Maiabollam
373
149 635
346
152 742
- - Counter meaaurea
317
150 961
"Ciation
348
157 137
--Appllcatlona
--Electromapietlc factora
347
347
152 633
152 996
Radiation injuriea
- - Pathol ogy
273
153 589
-•Propellant propertiea
311
153 791
347
152 955
RadUtion metera
Onaie
157 996
--C:«libratlor
333
153 622
--Chemical effecta
317
171 043
350
152 418
--Performance
333
53 790
Mn threaholda
--Tsanerature factora
347
153 626
Radio equipment
"Meaaure ment
■»66
IM328
"Thaory
346
157 912
--Maintenance
261
152 7<i
M«a
347
153 626
152 78^--
"Davelopmeni
33*
1»S«70
171 336
Piper capacitor*
Plastic coatinga
296
IS2 99B
--Effect* of radlaUon
788
153 096
--Effectiveneaa
314
152 862
Radio receiver*
hrabdic anteiuiaa
Plaaticiiy
- - Equipment
--Senalilvlty
296
152 991
--Pocualng
305
153 776
--Theory
325
153 109
296
152 992
1 --Radiation
299
153 949
Plaatlca
Radio aipiala
fbnckute fabrica
--Application*
--wave rranamlaaion
316
153 620
--Oaicctlan
288
52 985
•-Teat methoda
314
171 311
315
150 013
--Dlatortion
302
153 576
Parachutea
Palncare-Llghthill-Kuo method
327
152 738
153 577
--Teating equipment
Partial differential equatlona
314
171 311
Polymerization
Radio wavea
- - Effscta of radiaUon
332
171 041
--Appllcatian*
284
152 696
--Theory
318
153 715-1
377
171 310
--Propagition
--Reflection
349
49 740
152 7IS-2
Poiynoinlala
349
47 558
319
152 376
--Theory
319
152 371
--Scanerlng
349
152 523
321
171 349
Potaaalum chloride cryatala
Radioactive analyaia
171 350
--Lumlneacence
341
152 731
--Appllcatiana
Radiochemiatry
332
153 071
i
171 351
Prscipltatlon
--MBaaurement
171 354
281
153 046
--Theory
277
171310
171 355
--Radar analyaia
334
152 661
Radio frequendea
322
153 275
Preaaure
--Standarda
389
49 722
hrtlde accelerator*
--Metallurgical effecta
330
171 348
52 658
"Performance
312
152 959
Preasurized cabina
Radiofrequcncy flltera
PkrUdea
--Coding
306
171 345
•Dealgn
288
53 003
"Denalty
347
171 336
Primatea
Radiography
--Ditermi nation
337
149 6V)
--Effecta of radiation
273
- 152 630
--AppI lotion*
Radltxagical contaminatlan
309
152 988
--Scattering
333
171 335
--Teating equipment
263
152 744
Rutlclaa (Airborne)
331
149 736
Primera
- -Counter meaaurea
273
61 371 -9
"Development
306
157 839
334
152 698
--niyalcal propertiea
335
1^068
309
152 840
335
153 570
--Precipitation
335
l«3 070
Printed circuit*
Radiological warfare
--Radioactivity
334
I«2t6l
--Development
323
153 274
--hychoioglca] effecta
334
52 821
335
1*3 068
Probability (Statiatlca)
317
1*2 883
Radkanetera
153 070
320
152 934
--Daalpi
340
152 714-2
Pwtlculaie filter*
"Appilcatlons
—Theory
295
152 741
152 714-3
--Appllcatlona
309
171 051
318
171 312
Radloaondea
RMatration praUema
335
171 341
320
152 900
--Appllcatlona
279
152 905
f9pttdea
321
149 663
Raman apectroacopy
276
149 681
"Molecular ainicture
314
152 446
171 327
Ramjet englnea
Rvaiafroei
ProBellant gralna
--Heat tranafer
- - Model leai reaulta
31S
171 106
"Hbliography
281
171 190
308
152 126
Rationa (Military)
taraoBoel
315
152 835
--Nutritive value
310
153 339
--tarformance
264
152 913
--Temperature
315
152 825
Rawinaonde dau
280
152 699
--Teat methoda
364
148 004
Prcpellanta
Reaction (Paychology)
--Training
268
147 305
--Combuation
275
153 033
-•MaiheinaUcal analyaia
265
152 535
tavpiratlon
--Thermodynamic propertiea
314
149 665
--Statlatlcal analyaU
264
52 621
"Maaaurement
266
153 341
Protective aheltera
--Teat methoda
263
152 744
Ntturbation theory
320
149 644
--Development
294
153 373
Reactora
--Appllcatiana
309
171 337
Protone
-Hasarda
333
153 790
nHse modulation
- -Scattering
332
149 732
RsalfMsflsoCa
327
53 557
--Equipment
293
152 581
Paychlatry
265
152 764
Raaaealf^
Haee ahlftera
PaycovTxxor teat*
--•Ulofraphy
264
53110
--Applicationa
297
153 958
--Phy«iologlcal factor*
269
171 304
—Thaory
264
48 004
ftenocoplea
770
152 477
Public health
RscoaniilBatlan ramjet englnea
310
48 777
fteayl ether
--Dlpole momenta
--Perindicala
273
161 371-9
RscoariAattOB reactlona
310
53 587
776
149 678
Pulae analvzera
278
49 659
Pkaajf aulflde
--Circuit*
334
153 621
Re-entry aerodyiumica
308
52 759
"dlpole momenta
276
.149 678
Pulae gmereiora
327
52 557
Anaphora
--Apolirailona
344
152 925
Re-entry turbinea
312
52 856-1
--Lumlneacence
3V
157 536
Pyridine*
52 856-2
Itaiphorua
--MetaSoliam
272
149 635
313
52 856-3
--Metaboilam
•>67
152 M5
Pyrlmldlne*
Ptaoelecirlc cclla
--X-ray analyaia
269
157 740
--Dealgn
Reflex klyatron*
341
49 651
"Appllratiaia
277
153 606
Quality control
307
153 100
--Theory
351
152 897
--Develtjpment
303
49 629
■ -Development
342
149 706
(>iartz cryatala
Refract onfwtera
•Materiala
346
152 694
--Electrical propertiea
343
149 695
--Applicationa
283
52 951
Phaoeleciric material*
149 696
Refractory materiala
—Applicationa
rtaoelectric abutter*
299
152 409
--Frequency meaaurenwtM
343
149 695
--Appllcatlona
296
52 610
149 696
Refriferanta
"Blbllograpby
Itegraphic Aim
"Proceaalng
341
149 643
"Oro»fth
342
149 692
--Heat traaafer
348
50 036
--Phyaical propertiea
341
149 721
349
50 035
352
152 564
149 723
--Vaporization
Reliability
306
71 345
152 565
342
149 724
Itaometry
(Quarts reaonatora
--Military requiremenu
304 1
61 894-1
—Appllcatlona
274 ■
153 571
--Freouency meaaurment
--Oaclllator circuits
343
149 696
Remote control ayateina
Itesyntheala
289
149 732
--Application*
334
52 698
— Anajyai*
278
1 49 658
152 658
Reeina
Hqvical chemlatry
314
152 446
RADC reliability noiehonk
301
161 894-1
- -Caating
316
71 004
52 596
rWaoelectric cryatala
Radar duplexera
- -Cocnbustion
306 1
--Appllcatlona
296
30R
152 603
152 536
--Drr«lopine«
Radar operatora
--Paychalogical factora
300
153 668
--Electrical propertiea
Reaialor*
316 1
71 084
-8lbllogr*phy
341
149 643
263
153 335
--Calibration
290 1
71 205
PUot*
Radar receivera
291 1
71 206
•■Training
259
150 317
--C^lbratlon
308
152 759
I
71 207
--Training devicea
786
l%-> 885
Radar refleciora
1
71 211
Hmtubea
--Teat reaulta
399
152 949
292 1
71 200
"Appllcatlona
776
153 091
Radar acanning
Respiratory ayatem
--Climatic factora
--Theory
293
152 655
268 153 337
It'
1-9
Subnet
Rhodium compcunds
--Sjmthesia
Rhythm
"Measure mem
Rlu
--Deeip
RockKCMee
"MuerUls
Rockai launcher*
--Mew aMecta
--CoatliHPi
Rocfcei motor noiae
' 'Couatarmeaaurea
Rockat motor nozzlea
--Teat reaulta
Rocket motort
—Performance
"Shock resiaunce
"Temperature
~Taai mathoda
"Taadaf equtpmeni
Rochai odBlxer*
"Corroalve effecta
Rockat pra|iellan(*
• -Thermodvnamic prop^rtlaa
Rocket propelled sleda
--Aarodynamtc charac^riatica
Rocket proputalon
--Theory
Pue. PB Number
r
Rodema
- -Phyaidocy
Rctor Uadaa
--Da-tclnc eyatema
Rubber
"Olnatlc factors
--EOacta of radiaUon
--Preaerratlon
--Storafe
- -Temperature facttva
Rubber mount a
- -MbUography
Ruiraaya
Rulhaniam
--Deter mi netlon
Sampling (Staclstlca)
--Appllcatlona
Sand
- -Stwrcea
Saadvlch paneia
"WehMng
SappMrea
"Cryatal atnicture
Satellite vehicle reeearcl
Satellite vehicle trajectotjtes
--Oeter ml nation
"Mathematical analyaU
--Phyalcal factors
Sataillce vehiclaa
--Appllcatlana
"Dttacdon
* ~ Bqulpciiani
--Surfacea
- 'Temnerature
"Tracking
S8R vulcanlzatea
SC-27'i
Scheduling
--Applicailona
Schtatoaofna
"Ataaka
ScMleran photography
--Applications
Schubert calctilus
SdantUlc reporta
"Mitacrapliy
Saa a^aar
--Aaalyals
- -Corroelye effects
--Desal I nation «
Selenium
-'Cryatal structure
SamtcoDductor*
--Appllcatlona
--Conductivity
--Crystal structure
--Develcpment
--Electrical propertlea
- -Materials
"Properties
Beqpwimil anslysls
"Appiicatlons
Sarisaai
Sarwa eipaoalona
--ApptlcaUflaa
274
274
340
2B4
316
314
314
SI I
311
311
StI
StI
331
311
306
310
310
312
274
326
317
317
317
317
317
310
287
274
3SI
27«
345
2S«
278
3oa
309
308
2S7
283
307
340
305
307
307
308
321
317
304'
tio
271
308
318
257
392
274
285
331
28S
324
344
345
344
342
346
342
346
317
3W
152 773
132 631
152 714-1
152 623
153 620
171 047
171 047
171 308
161 227
153 791
153 272
IS2 826
152 988
153 772
171 301
153 791
152 743
148 777
133 sr
171 306
152 631
153 195
171 0(2
ISO 961
171 0*3
171 0*2
171 or?
153 793
1«3 629
152 772
1«2 897
149 638
286 149 718
152 544
149 645
152 684
152 522
171 337
152 939
152 846
153 050
153 100
152 714-3
171 345
152 673
153 885
153 88S
!52 ■!■>?
153 053
171 043
149 712
1M 934
1«3 332
171 352
191607
153 726
171 315
153 571
171 344
149 739
171 344
344 152 925
149 297
152 925
149 679
152 462
152 473
152 628
149 706
171 340
152 694
1^2 883
1^7 988
319 1<2 376
Sheeta
"BoDiidary layer
--Cavltailan
--Deformation
--Heat transfer
--H)«lrodynamlc
characterlatlca
--Oadllatlafi
"Preaaure dlairlbutlon
--Tenalle propertlea
--Vibration
SMpa
-- Vibration
SMverIng
--InhlWtion
Shock oaves
--Measurement
--OscilUtion
--Photogrsphic analyais
"PropagBtion
--Reflection
--Theory
Shrouded propeller*
"Aerodynamic
characterlatlca
--Preaaure dtatrlbutlon
Silicon
--Dielectric propertlea
Silicon carbide cryatala
■Growth
Silicon cryatal*
--Applicaiian*
Silver chloride cryatal*
--Deformation
--Stresaea
--Tempersture factors
SUvar iodide
--Coaductlvliy
Simplex system
Sinpe cryatals
-Deformaiion
-•Electrical propertlea
"Fracture
--Cro<*th
"Msgaetlc propertlea
Skin
--Sensitivity
Smear cameraa
Smoke pot*
■"Effectiveneaa
--M5 HC
Smolce acreena
--Production
Snow
--Blbliogrsphy
Sno» cryauls
--Meteorological factors
SntMT veMdea
-Test reault*
Snowmobile
Sodium chloride crystals
--Deformstlon
Sodium Iodide crystal*
--Lumineacence
Soila
--Moiature content
--Radioactive analyai*
--TrafflcaMllty
Solar atmoaphere
--Spectra
Solar energy
"Atmilcationa
Solar flares
--Radiation
Sol ids
--Magnetic propertlea
•-Phyalcal properties
--Ttiiermodynamlc properties
--Wave ir*n*mi*aicn
Sonar peraonnel
--Performance
Sonar dgnal*
--Detection
Space chargea
--Electrical eftecta
--Electromagnetic effecta
Spaceflight
--Phyaioiogical effecta
- -Slimlatlon
-Theory
Space meolclne
-Bibliography
Space perception
--BltMlograpby
Space reconnai**ance
Spaceahlpa
--Propulaion
Spade
Spark machining
--Application*
I-IO
£UB PB Number
327
328
325
326
328
328
326
330
325
270
271
347
326
308
346
306
327
287
287
343
346
303
343
343
343
298
351
343
345
343
336
346
344
266
308
306
306
306
281
281
313
313
343
341
284
332
284
258
34?
331
344
345
348
345
264
264
337
301
268
265
263
308
268
307
310
312
334
313
152 738
149 640
153 109
152 947
149 640
152 906
171 30B
171 0(4
152 632
310 153 793
153 349
153 330
153 350
153 626
171 302
171 352
152 912
149 633
152 537
IS2 898
152 898
149 628
152 628
152 659
152 891
152 891
152 891
149 726
152 787
149 684
171 356
149 684
149 728
152 628
152 932
153 328
171 352
152 595
152 595
152 595
171 190
152 541
153 320
153 320
149 684
152 731
153 884
153 071
153 884
152 946
149 706
152 916
15? 462
149 690
171 329-1
149 690
152 888
152 888
149 725
152 938
152 460
152 764
152 744
152 939
272 171 029
153 575
153 100
148 777
153 587
152 749
152 959
IS2 fil
161 225
Subject
Spactrometera
--Appllcailana
-Oeaign
Spectroacopy
--Application*
Sphere*
--Elaatlcliy
--Sireaae*
Squid
SiaMlity
--Determination
Stainleaa ateel
--Fracture
--WekUng
Standing wave indicators
- -Testing equipment
Standing wave rstioa
--Meaaurement
Star*
--Photogr*phy
--Radiation
Scatiatlcal analyala
-Reliability
--Theory
Siatlatlcal function*
SiaiUclc*
--Function*
Steel
-Availability
--Enniaion
- - Heat t reat mem
--Internal friction
--Mechanical propertlea
-•Ten*lle propenle*
-USSR
Steroid*
--Determination
Stochaatlc proce**ea
Storm*
--Radar analyala
Strainers
--Applicatioaa
St real camera
Srreaa analyala
--Theory
Sireaakin
Structurea
--Elaaticlty
--Mechanical propertlea
Styrene*
--Poiymerlzation
Submarlnea
--Safety meaaurea
Submlnlature electronic
equipment
--Development
Sulfidea
--Diaproportlonment
Sulfur compound* (Organic)
--Molecular atructure
Sulfur dloxtde
--Lumlneacence
--Spectra
Sun
--Phyaical effecta
Superconductivity
- - Phyaical factora
Superpower cathode
Superaonic flow
-Meteorological factors
Superaonic wind tunnel*
"Acouulc propertie*
- ■Electric*' fscior*
■ ■Preaaure dlatribution
Surfacea
- -Coatlnga
Survival
--Arctic regioia
Survival kits
--Arctic reflona
- 'Development
Switching circulta
--Syntheala
Syatema engineering
"Theory
Tarpct recognition
"Visual factora
Taraeta
--Detection
Tchebycheff Inequality
Teaching machlnea
Telegraph signal*
-Coding
Telephone communlcetlon
ayaiema
--Circulta
Teleacopea
--Deaign
Teletype ayatem*
--Development
Televlaion equipment
-Deaign
iam fff "vrrtK
340
341
339
336
324
325
328
331
286
292
242
259
257
281
318
321
320
317
338
330
330
331
330
330
329
270
320
280
309
341
324
286
285
328
316
332
309
304
276
276
277
277
317
346
337
325
326
325
326
263
269
335
335
299
263
263
269
269
321
260
152 714-4
152 713
152 164
149 728
148 405
152 779
149 68*
306 153 058
152 880
149 718
171 201
171 204
153 278
152 834
152 769
171 312
171 327
152 400
152 8«S
151 0*7
151 097
161 213
152 691
151 097
171 044
171 331
153 327
152 900
152 774
171 OBI
171 191
149 756
149 711
171 192
152 906
149 963
171 0(1
PI 0(6
171 061
152 670
152 478
152 746
153 158
153 158
171 0(2
152 901
152 962
152 601
152 529
152 602
152 529
335 153570
153 325
153 344
153 346
153 346
152 750
152 757
153 3r
152 606
152 606
149 663
153 460
289 152 «6
3S1 152 933
259 153 278
300 148 281
302 161 468
TaiBPari
•-Dete
Subject
srature
Iter ml nation
ureinent
Taaaioraeter*
•'Calibration
Tarraatrlal ma^iatiam
'Aoalyal*
"Te*i reeult*
Tkermal radiation
--Abaorptlor
Thermlonjc emmiaaion
"Mathematical analyala
•-Maaaureinent
TMn fUma
--Appllcatlana
•-Propertlea
ThyrcM gland
--Phvaiologv
Time Interval countera
--Development
Tin compound* (Organic)
--Syntheala
Tiro* •
Timgirr of the ocean
Topoiagy
"Appllcatlona
Tolo
Tracking
--Equipment
--Training devlcea
Tracka (Aerodynamica)
--Development
Training
■-Bibliography
•-Piychologlcal factora
--Theory
Training devicea
--AaaTysl*
--Bftectlvene**
--Human engineering
Tranaducers
■-Bibliography
--Performance
--Teat methoda
Tranafer of training
Traaaforinatlona (Mathemaiica)
"Applicailona
•-Errora
Traaalator*
--Appllcatlona
--circulta
■- Development
Traaaltlon elementa
••Propertlea
Tranalatlona
••bdexea
fsat
PB Number
StWWt
Tranamlaalon llnea
Eae
PB NuirteL
Sublect
Vertical take-off planea (con)
tUR
PBNuirtier
283
152 «*9
--Mathematical analyala
345
149 679
--Performance
286
149 666
347
153 626
Tranaword
300
152 721
Vibration
Traveling wave lubea
--Theory
336
149 682
328
171 208
-•Deatv<
301
152 937
Vibration laolatora
347
'52 996
--Teat reaulta
310
153 793
332
149 650
- - Devel opnwnl
Trlaaer circulta
--l5eaign
295
152 995
Vlacoelastic materiala
Vlaual acuity
315
150 013
'96
149 694
296
147 313
--Arctic reglona
266
153 326
Vlaual perception
--Statistical analyala
307
l«3 885
--Appllcatlona
•>87
15? 800
269
152 606
795
15? 73«
Tropical cyclone*
-'Photographic *nalyais
Vlaual algnals
796
15? 610
281
152 870
--Detection
289
152 926
337
152 96?
--Radar analyala
■•SI
152 870
--Identification
263
171 313
Truth functions
321
152 723
Volimentera
298
152 672
Tularemia
--C^alibratlon
289
17120*
346
152 901
--Alaaka
271
152 619
171312
Tundra truck
313
152 940
171 213
269
153 344
Tunnten wire
■■Coatlnga
291
171 214
329
171 193
171 215
334
153 621
Tunneling current
Turbulence
342
152 473
171 217
171 218
274
149 683
--Theory
328
149 689
292
171 216
278
152 684
Turbulent boundary layer
Vorticea
282
153 625
--Mathematical analyala
326
149 686
--Mathematical analyala
326
152 479
318
152 606
Turbulent flow
Vulcanlzatea
322
149 649
••Mathemadcal analyala
328
149 689
--Deterioration
317
171 043
323
152 747
Ultra high frequency
--Stresses
316
153 172
294
149 636
communication syatema
Water tunnela
282
153 625
--Performance
Ultraatmic radiation
349
152 466
--Design
Water vapor
328
153 574
263
152 708
--Anenuation
345
149 690
--Meaaurement
284
ISO 618
259
150 317
Ultraaonica
Waveguides
--Appllcatlana
Ultravlolei radiation
313
161 225
■-Analyais
301
152 652
308
153 867
--Electromapietlc propertlea
301
152 652
-•Measurement
341
149 651
"Equipment
293
152 581
260
171 332
Ultraviolet spectra
Weather forecaating
''60
147 305
147 305
••Analysis
■»76
1 5? 746
--Teat reaulta
280
152 700
260
Underwater photography
••Atlantic Ocean
282
152 908
"Reflective effecta
350
153 088
'>60
153 460
Underwater aound equipment
Welerstraas producta
319
152 972
260
?»9
149 642
150 317
--r»|ibr*tian
30?
1 5? 979
Welds
Upner (tnTxiaphere
--Radiographic analyala
309
152 988
--'''emperature
283
152 669
Wetting agenta
--Effectiveneaa
293
153 496
153 496
UraniuiT^ isotopes
277
150 619
293
(Radioactive)
Whlatlera,
336
153 279
293
153 496
••Spectra
334
153 030
Wind
259
150 317
152 431
152 762
Urine
--Meaaurement
280
152 699
320
--Chemical analyala
270
153 327
Wind tunnel nozzlca
322
-■Excretion
269
171 343
--Calibration
327
149 344
323
318
152 436
171 334
Vactium fumacea
--Appllcatlana
330
161 213
*i^f.
326
153 196
332
152 736
Vacuum ayatema
Wounda
--Applicaiians
Van Allen radiation
270
153 573
--Analyais
271
152 368
300
lS2ni
152 639
258
149 645
X-ray diffraction analyala
299
Vapor cycle coaling
3as
171 345
'-Appllcatlona
269
152 740
303
152 659
Variable atari
330
171 348
--Claaalficatlon
259
152 171
Zinc
344
152 854
--Lurtilneacence
259
152 171
--Phyaical effecta
344
152 973
Vekua theorem
322
153 275
Zinc aulfide cryatala
?M
153 575
Vertical take-off planea
"Electrical propertlea
345
171 338
«oo
--Deaign
286
149 666
--Lift
326
153 196
I-ll
NUMBER INDEX
•««!»»
V»t*
4»L 7-7951, R-2
23,7-7951, R-3
AAL 7-7953. Rl
tU. 7-7954. R-1
*1L»-7951. R-7
JUL (-7954. R-2
ZS!*-79sa
AIL 21-01-024
Sl 22-1201-0000. SR-1
AAL22-ia0l-OOOl, Rl
AAL 22-1301-0002
AAL 22- 1301 -0009, R-2
AAL 22- 1401 -0004. RR-1
AAL 22-1401-0005
AALTR-57-1
AALTR-57-a
AAL TR- 57- 3
AALTR-57-9
AAL TR- 57- 10
AALTR-57-11
AALTR-57-IS
AALTR-57-aO
AALTR-57-21
AALTR-57-24
AALTR-57-43
AALTR-5»-16
AALTR-59-25
AD- 53 055
AD-114 4<)7
AO-126 3S3
AO-144 368 W
AD-144 442 111
AD-I46&32 SIO
AD-I4« 789 3U
AD-1S0 401 U3
AD-157 442 314
AD-J07 594 S>7
AD-210 005 949
AD-210 006 299
AD-2U 397 337
AD- 21 1487' 296
AD-2U 536 275
AD-211 948 321
AO-213 228 305
AD-213 537 345
AD-213 702 339
AD-213 783 . 30O
AD- 214 729 2eO
AD-215 482 261
AD-21S488 310
AO-216 73b 331
AD-217 102 329
AD- 217 993 345
AD-219 334 343
AD-219 685 330
AD-219 686 29t
AD-219 687 337
AD-219 981 339
AD- 230 099 336
AD-230 531 332
tP-iX 587 3«3
AD-2X) 647 343
AD-230 653 27*
AD- 220 673 3S2
AD-2X853 339
AD- 225 055 336
AD-225 104 331
AD-225 440 277
AD-225 975 32S
AD-236 571 297
«P>2a6 834 3S1
lO-Ob 962 343
AP-2r 100 341
ilD-227 622 274
AD-228 095 31 1
AD-221 156 270
AD-228 396 297
AD- 228 483 333
AD- 229 513 324
AD- 229 738 304
AD- 229 965 331
AD-230 071 337
AD-230 098 212
AD-230 242 282
AD-230 562 210
AD-230 565 , 280
AD-230 730 XI
AD-230946 322
AD- 231 043 336
AD- 231 067 264
AD-231 127 304
AD- 231 130 272
AD-231 151 339
AD-231 160 346
AD-231 184 320
AD-231 229 317
AD-231 313 337
AD-231 409 341
AD-231 424 330
AD-231 430 331
AD-231 430 2S2
AD-231 468 2*7
WMPiber
AD-231 473
AD-231 626
AD-231 804
AD-231 843
AD-231 844
AD-231 848
AD-231 897
AD- 232 049
AD- 232 181
AD- 232 388
AD- 232 410
AD- 232 561
AD-232 635
AD-232 636
AD- 232 637
AD-232 716
AD- 232 742
AD-232 743
AD-232 911
AD- 232 922
AD-232 927
AD-232 931
AD-232 947
AD- 233 147
AD- 233 575
AD- 233 680
AD-233 706
AD- 233 826
AD- 234 llO
AD- 234 124
AD- 234 359
AD- 234 394
AD- 234 401
AD- 234 515
AD- 234 629
AD- 234 684
AD- 234 729
AD-234 743
AD- 234 794
AD-234 814
AD-234 912
AD-234 916
AD-234 920
AD-234 998
AD-235 018
AD- 235 033
AD- 235 186
AD- 235 198
AO- 235 212
AD- 235 217
AO-235 288
AD- 235 312
AD 235 398
AC- 235 430
AD- 235 612
AD-235 804
AD- 235 806
AD- 235 859
AD- 236 255
AO-236 376
AD- 236 377
AO-236 460
AD- 236 593
AD-236 709
AD- 236 817
AD- 236 967
AD-236 999
AD- 237 442
AD- 237 752
AD- 237 809
AO-238 156
AD- 238 299
AD- 238 443
AD- 238 479
AD- 238 740
AD- 238 764
AO-238 765
AD- 238 967
AD- 238 972
AD- 239 486
AD-239 696
AD-239 875
AD- 240 261
AD- 240 285
AD- 240 3S0
AD- 240 687
AD- 240 766
AD- 240 819
AD- 240 909
AD- 240 959
AD- 241 779
AD- 241 914
AD- 241 916
AD- 242 179
AD- 242 306
AD- 242 302
AD- 242 3tl
AO-242 362
AD- 242 485
AD- 242 517
AD- 242 5X
AD- 242 982
212
AD- 243 196
296
AD- 243 253
936
AD- 343 348
919
AD- 343 461
931
AD- 243 490
331
AD- 243 614
964
AD- 243 632
399
AD- 943 719
279
AD- 913 825
922
AD- 243 826
277
AD- 243 854
3a
AD- 243 927
312
AD- 243 989
312
AD- 244 089
313
AD- 244 207
296
AD- 244 250
2S1
AO-244 283
963
AD- 244 303
346
AD- 244 327
342
AD- 244 368
294
AD- 244 369
294
AD- 244 372
293
AD- 244 391
296
AD- 244 395
33S
AD- 244 396
299
AD- 244 397
333
AD- 244 457
342
AD- 244 484
282
AD- 244 557
343
AD- 244 582
335
AD- 244 588
278
AD- 244 601
278
AD- 244 663
295
AD- 244 677
303
AD- 244 679
332
AD- 244 706
330
AD- 244 756
332
AD- 244 757
276
AD- 244 767
322
AD- 244 771
276
AI>244 819L
276
AD- 244 833
341
AD- 244 855
306
AD- 244 856
326
AD- 244 858
332
AD- 244 881
332
AD- 244 682
295
AD- 244 888
279
AD- 244 900
318
AD- 244 901
338
AD- 244 902
316
AD- 244 903
283
AD- 244 904
295
AD- 244 906
341
AD- 244 907
29<
AD- 244 921
260
AD- 244 945
347
AD- 244 958
331
AD-245 017
295
AD- 245 023
296
AD- 245 060
239
AD- 245 061
307
AD- 245 064
29S
AD-24S072
333
AD- 245 078
349
AD-245 0U
324
AD- 245 069
328
AD- 243 116
264
AD- 245 117
322
AD- 245 119
324
AD- 245 132
273
AD- 245 157
289
AD- 245 166
283
AD- 245 179
319
AD- 245 162
258
AD- 245 194
259
AD- 245 1%
260
AD- 245 197
310
AD- 245 205
352
AD- 245 206
275
AD- 245 209
327
AD- 245 220
303
AD- 245 221
297
AO-245 229
259
AD- 245 231
307
AD- 245 232
295
AD- 245 234
298
AD- 245 253
30«
AD- 245 278
304
AD- 245 313. pt. 1
287
AD- 243 313. pt. 2
334
AD- 245 343
300
AD- 245 344
347
AD- 243 396
283
AO- 243 399
350
AD- 245 999
348
AD- 245 445
349
AD- 245 468
288
AD- 245 472
317
AD- 245 485
330
AD- 245 486
317
AD- 943 497
300
260
271
306
323
306
323
292
265
261
299
344
271
330
349
261
330
323
276
294
294
269
319
319
319
319
326
296
349
308
296
341
261
342
264
264
271
266
330
299
325
324
262
262
326
347
302
334
341
340
340
340
340
316
316
267
339
274
334
276
293
294
263
313
290
344
331
346
318
323
278
348
299
273
305
288
341
336
306
346
307
311
295
276
321
300
323
303
322
318
316
322
322
296
296
344
276
261
351
315
308
330
Nwii>»r
AD- 245 500
AD- 245 503
AD- 245 504
AD- 245 509
AD- 245 513
AD- 245 524
AD- 245 565
AD- 245 575
AD- 245 581
AD- 245 607
AD- 245 618
AD- 245 619
AD- 245 623
AD- 245 666
AD- 245 671
AD- 245 673
AD- 245 689
AD- 245 690
AD- 245 703
AD- 245 723
AD- 245 724
AD- 245 726
AD- 245 769
AD- 245 788
AD- 245 856
AD- 245 928
AD- 245 991
AD- 245 992
AD- 245 996
AD- 245 997
AD- 246 000
AD- 246 012
AD- 246 037
AD- 246 186
AD- 246 394
AD- 246 419
AD- 246 590
AD- 246 593
AD- 246 601
AD- 246 678
AD- 246 796
AD- 247 193
AEDCTN-59-134
AEDC TN-60-180
AEDCTN-60-162
AEDC TN-60-191
AEDC TN-60- 194
AEDC TN-60-aD2
AeroChem TM-21
AFCCDD-TN-eO-l014
AFCRC-TN-58-201
ARCRC-TN-59-469
AFCRC-TN-59-624
ARCRC-TN-59-62S
AFCRL-TN-60-216
ARCRL-TN-eO-442
AFCRL-TN-60-459
APCRL-TN-60-455
AFCRL-TN-60-457
AFCRL-TN-eO-458
AFCRL-TN-60-461
AFCRi--TN-eO-462
AFCRL-TN-60-470
AFCRL-TN-60-483
AFCRL-TN-eO-575
AFCRL-TN-60-e06.
AFCRL-TN-bO-610
AFCRL-TN-60-613
AFCRL-TN-eO-637
AFC!U,-TN-60-647
AFCRL-TN-60-649
AFCRL-TN-60-652
AFCRL-TN- 60-657
AFCRL-TN-60-669
AFCRL-TN-60-663
APCR1--TN-60-684
AFCRL-TN-60-769
AFCRL-TN-60-776
APCRL-TN-60-762
AFCRL-TN-60-790
AFCRL-TN-eO-791
AFCRL- TN-60- 796
AFCRL-TN-60-959
AFCRL- TN-60- 961
AFCRL-TN-eO-971
AFCRL-TN-60-973
AFCRL-TN-60-974
AFCRL-TN-eO-975
AFCRL- TN-60-976
AFCRL-TN-60-997
APCRL-TN-60-966
AFCRL-TN-eO-990
AFCRL-TN-60-994
AFCRL-TN-eO-995
AFCRL-TN-eO-1103
AFCRL-TN-60-1104
AFCRL-TN-e0-ll25C)
AFCRL TN-60- 11 33
APCRL-TR-60-131
AFCRL-TR-60-137
AFCRL-TR-bO-l69
AFCJlL-TR-60-171
349
336
327
325
906
323
346
310
344
284
336
282
282
279
278
2*0
279
280
290
274
274
278
264
336
256
341
261
333
306
287
258
284
281
298
298
292
295
3DS
349
303
295
341
351
338
349
301
293
296
350
336
347
946
304
346
296
263
390
297
396
299
989
1-13
N
NmnbT
AFCRL-TR-60-185
APCRL-TR-aO-240. be.
AFCRL-TR-60-276 ^
AFCRL-TR-60-287
ak:rl-tr-»-2»4-
ArCRL-TR-«)-29«-:
APCRL-TR-60-294-:
Ai»CRL-TR-«)-2»4-
AFCRl,-TR-<iO-407
AFCRL-TR-eO-409
AFIT-57-4
AFMDC-TR-tO-I»
AFMDC-TR-60-22
AFMDC-TR-60-27
AFMDC-TR-60M
AK3SR-TN-M-1093
AFOSR-TN-59-52*
APOSR-TN-59-573
AFOSIl-TN-5»-7»
AFOSR-TN-59-lJtO
AFOSR-TN »-129«
APOSR-TN-«>-2«3
APOSIl-TN-«fr-3M
Ai>aiR-TN-«0-2M
APOSR-TN-40-2U
APOSR-TN-tO-aOO
AroSR-TN-60-303
APOSR-TN-60-329
APOSR-TX-60-J30
APOSR-TN-60-354
AFOSR-TN-60-379
AP0SR-TN-60-4J7
AFOSR-TN-eO-S41
APOSR-TN-AO-tOO
Ai>0SR-TN-(O-M2
AI>C6R-TN-«O-bS0
AFOSR-TN-aO-701
APO8R-TN-60-718
AFO8R-TN-60-744
APOSR-TN-60-74*
AFCRL-TN-M)-7S6
AFCRL-TN-eO-780
AFOSR-TN-60-807
AFOSR-TN-60-8S5
APOSR-TN-«l>-«67
AFOSR-TN-«0-8a4
AF08R-TN-W-9U
AFOSR-TN-60-912
AF06R-TN-«0-93a
APOSR-TN- 60-945
APOSR-TN-,60-96S
APOSR-TN-60-1024
AFO6R-TN-6O-1026.
AK)«-TN-60-l026.
AJ>OSJt-TN-«>-1042
Ai>06R-TN-60-106t
AFOSR-TN-60-lOU
AFOSR-TN-60-1090
APOSR-irN-iO-1096
AFOSK-TN-(iO-lll9
APOSR-TN-ftO-1121
APOSR-TN-60-n29
APOSR-TN-(iO-il3«
APOSR-TN-60-llSO
APOSR-TN-MMl(tS
Af>0SR-rN-M>-119«
Ai)OSR-TN-M>-123S
AFOSR-TN-60-6
AFOSR-TR-()0-24
AFOSR-TR-ftO-O
AI'OSR-TR-<)0-U9
AFOSR-TR-tO-lZS
APOSR-TR-60-128
APOSR-TR-(iO-130
AFOSR-TR -eO-134
APOSR-TR-(iO-133
AFFrRC-TN-57-52
AFSAM-(0-66
AFSAM-«0-79
AFSAM-bO-aO
AFSEC-TN-60-2S
A1R-3M-U)-|R-|06
AMRCPM-24
AMRC PM-25
AJlF-1099-15
AiU'-1146-6
ARL-TN-«)-l26
ARL-TN-eO-U2
ARL-TN-eO-l44
ARL-rR-()0-274,
ARL-TR-60-279
ARL-TR-tO-281
ARL-TR-60-296
ARL-TR -ftO-30l
ARPA Order 6-58, TaA II
ARPA Order 80-59
ARPA Order t06-60
ASRIX-2121
ASiUX-2133
ASJUX.-214S
ASROLT-1459,
ASROL T-1473
ASRDL T-1479
ASRL TR-86-1
Avco RR-85
AWSM-105-39
AWSM-105-39. \miX
wnr ceded
pt. 1
3S0
BBN-721
S3t
lXTR-194
399
3 281
BN-196
390
LLTR-223
s:
27ft
BN-318
3M
U- TR-224
237
BRL-1113
£
LLTR-226
ss
MO
BRl.MR-1241
LLTR-227
340
BRLMR-1299
SM
LMSD-31t 864
ISO
3«D
BRLTN-1337
»J
LMSD-703 029
300
340
BTL-27424-K
Ml
Lock NR-60
333
307
BTL-27424-M
S41
MAC-7064
286
U7
BTL- 27424- N
343
MEDBW-RS-3-59
371
Wt
BTL- 27480- K
M
ML-69S
901
ao7
8TL- 27480- L
m
ML- 733
301
30S
auMad-MROOS.
ML- 745
301
»3
15-0002.7, R-12
269
ML(UM>-2112
313
2S9
iMMad MR005.
MRC TSR-63
334
327
15-0002. 11. R-1
269
MRI R-523. 38-59
345
263
BuPns TB-60-8
261
MRI R-736-S9
350
27»
CAL AD- 1052- A- 11
326
MRL(OMRO)-89
344
3»
aTE-79-2
S»
MSEE-60-22
^
322
CRIXSP-1-20
306
MUPTR-167
»1
CRI3LSP-1-21
306
MUPTR-168
333
322
,CRDLR-3019
306
NAA-MD59-277
357
341
CRIXR-3024
ri
NAnr-MA-6030
369
au
CU-l-60
m
NADC-MA-6031
269
333
CU-8-60
393
NAMC-AML-AE-1096
330
31S
CWLRR-IU
373
NAMC- AML- AE-4195, pc.2
329
332
CWLTM-32-41
339
NATCET315-127
301
32D
CWLR-2347
373
NAVORD-5765
345
276
DA 33-008-ORD-I968. R-S 285
NAVORD-6415
^
332
DASA-526
334
NAVORD-649S
334
OMIC-M-63
30
NAVORD-6921
321
3lt
DMIC M-75
19
NAVTRAOEVCEN-9-U-l
260
319
OMIC-M-76
89
NAVTRADEVCEN-
303
DMIC-M-77
1809-00-4
^
323
OMlC-138
9O
.NAVWEPS-7016
s
SZ7
DOFL-TR-870
n
NAVWEPS-7094
6
275
DOFL-TR-878
93
NAVWEFS-7096
19
322
DOFL-TR-879
93
NAVWEPS-7098
0|
322
DOFL-TR-881
E
NAVWEPS-7104
:S
303
DOFI.-TR-887
n
NAVWEPS-7254
at
330
nOPL-TR-89l
11
NAVWEK-7264
'^
342
IXJ8«IT-1-U
:m
NAVWEPS-7289
tk
319
OSR-7484
M
NAVWEPS-7290
03
276
•9
NAVWErS-7302
321
323
LrrMB-597. Mifieraeded
257
NAVWEPS-7318
321
345
OTMB-1052
328
NAVWEfS SSL-AE-Ol
291
319
UIIrfB-llAO
§0
NAVWEBSSL-AE-03
291
319
LrrVB-1360
NAVWEPSSSL-AE-25
289
326
EGA- 192. 04
4IM
NAVWEPS SSL-AI-02
290
348
EeRl.-6-38
2§5
NAVWEPSSSL-AR-06
291
344
eES-820 052
Sd
NAVWEPS S.SI-BC-01
289
294
EM- 155
NAVWEPS S,SJ -BC-02
290
1 318
EM- 162
^
NAVWEPS SSL-BC-03
290
2 318
EOS- 290
NAVWEPS SSI -BC-04
290
3S0
EOS-400-2Q-I
983
NAVWEPS SSL-BC-05
290
318
ERL-99
IS
NAVWEPS SSL-BE -01
291
265
ERL-100
NAVWEPS SSL -BE -02
291
294
ERL-lOl
396
NAVWEPS .S.SI- BE -03
289
322
ERL-103
393
NAVWEPS SSL-BE -05
289
341
ES-29(XE-3»
352
NAVWEPS SSL-BF-06
292
331
ESL-MIT-7591-R-2
286
NAVWEPS SSI -BL-01
292
324
FDRC-60-3
296
NAVWEPS SSL-BR-02
291
319
FRL-TR-12
315
NAVWEPS SSL -BR -03
291
276
FRL-TR-13
316
NAVWEPS SSI -BR -04
290
325
CNE-57-5
310
NAVWEPS SSI -CL-02
292
347
CRO AFSC-94
284
NAVWEK SSI -CR-02
292
336
CRD AFSC-125
278
NAVWEPS SSL-HV-05
292
326
CRDAFSC-126
279
NAVWEPS SSJ ■NF-02
328
275
CRD RN-38
371
NAVWEPS SSL- NM-03
336
314
HR-59-474
3*3
NBSTN-18-7
330
274
HR-80-412
343
NCELR-091
313
346
HSR-RR-60/4-Se
334
NCEL R-094
313
341
HT-6
344
NM 001 1 10 500. 37
363
344
Hum RRO-TE-65
261
.NML Ref-60-l
3S3
268
Hum RRO TR-64
261
NOL M1)M- 1
331
336
IER-60-27
293
NOLMDM-13
331
262
IER-60-265
296
NOLMDM-14
921
273
IER-60-267
295
NOLMDM-15
267
IBR-eO-269
296
NOR-60-16
287
265
IER-60-271
295
iNOrS-2113
S7
334
lER-60-272
319
NOTSSTS-3
300
260
lER-60-284
338
NOTSTM-786
313
280
IER-60-289
295
MOTS TM- 1113
331
280
IER-131-8
324
NOrSTP-2377
3a
341
IMM NYU- 260
324
MOTS TP- 2379
S3S
337
lRL-131
284
NOrSTP-2513
330
318
lRL-139
291
NOrSTP-2517
919
327
lRL-140
298
Nai'STP-2521
300
333
IRL-141
283
NOTSTP-2528
280
347
1TT-M29
352
NRCC LR-186A
326
312
PLM-20-194
307
NRCC LR-274
336
309
PL R-20-127
311
NRCX LR-288
336
315
JRTH-137
337
NRCC MI -822
377
345
UR TK-138
391
NRCC W- 17
313
1 275
U,-21C-0015
300
NRL-9998
302
342
LL-21G-0026
331
NRL-4037
3D2
349
IX-22C-0042
323
NRL-5534
93«
317
0.-230-0054
331
NRL-5547
3t«
2S8
LI,-25C-00Ol
299
NRL-5551
3M
317
U.-25C,-00O5
3S1
NRL-5556
trt
152
LL-2W-0019
3DD
NRL-5557
m
352
LL-3DC-0011
349
NRL-.VyiO
309
352
LL-46C-0007
298
NRL-5563
309
2SJ
LL-51G-0018
XD
NSFC-7368
381
3«6
U.-58C-0015
264
.NSFC-10715
323
279
U.-82C-a023
344
NSFC-Y/32.48/272
sot
LL-85C-0008
344
NSL-437
87
279
LL TR-190
349
NWPW-T-6-59
81
Number
NYUTR-400-14
NYU TR-400-16
OORR-770-...
DORR- 1469. I
OORR-1840. 9M
OORR-2a07.5-E
OORR-2307.6-B
OSURF 716-7
OSURF 716-8
OSURF-823-l
miiii'-^
OTAC RR-27
PB
147 305
PB
147 310
PB
147 313
PB
147 314
PB
147 535
PB
147 554
PB
147 558
PB
148 004
PB
148 066
PB
48 282
PB
48 405
PB
48 426
PB
48 494
PB
48 495
PB
48 MO
PB
48 609
PB
48 777
PB
49 211
PB
149 297
PB
49 344
PB
49 628
PB
49 629
PB
49 630
PB
49 631
PB
49 633
PB
49 634
PB
49 635
PB
49 636
PB
49 637
PB
49 638
PB
49 639
PB
49 640
PB
49 641
PB
49 642
PB
49 643
PB
49 644
PB
49 645
PB
49 646
PB
49 647
PB
49 649
PB
49 650
PB
49 651
PB
49 654
PB
49 655
PB
49 657
PB
49 658
PB
49 659
PB
49 663
PB
49 664
PB
49 665
PB
49 666
PB
49 668
PB
49 675
PB
49 677
PB
49 678
PB
49 679
PB
49 680
PB
49 681
PB
49 682
PB
49 683
PB
49 684
PB
49 685
PB
49 686
PB
49 687
PB
49 688
PB
49 689
PB
49 690
PB
49 691
PB
49 692
PB
49 693
PB
49 694
PB
49 695
PB
49 696
PB
49 703
PB
49 704
PB
49 706
PBI
49 708
PB
49 709
PB
49 710
PB
49 712
PB
49 718
PS
49 721
PBI
49 722
PB
49 723
PB
49 724
PB
49 725
PB
49 726
PB
49 728
PB
49 729
PB
49 730
PBI
49 732
PB
49 733
PB
49 736
PB
49 737
PB
49 738
302
»3
275
3X
321
294
294
282
282
2S9
213
283
3D7
280
324
296
29S
328
285
349
264
m
300
324
283
238
259
319
323
310
259
314
327
343
303
303
277
30«
272
272
294
294
278
3»
328
33>
2tO
341
SB
at
318
303
322
332
341
3S7
329
3«0
278
278
321
■zn
314
288
279
27*
3r
27*
3*3
338
276
336
r*
Mi
351
33*
27S
33*
32*
3*5
334
342
304
29*
3*3
343
29J
3D9
342
297
297
297
3M
28*
341
289
341
342
337
298
338
3»
320
332
331
331
332
345
1-14
149 73»
181740
14*741
l«»*30
14*963
130013
l«03S
13D036
IS 317
lSO*il
1S*I9
UD961
131097
131 377-:
19137
18171
131 254
in 368
1«3»9
131371
131 373
132 376
133.409
131411
131431
131436
181446
131460
133 462
131463
133 466
133 470
131473
131477
131473
152 479
132 486
132 489
132 »3
152 Ui
132 339
132 333
132 538
152 537
132 341
152 544
132 536
132 557
152 364
132 S65
152 380
132 581
132 593
152 396
152 597
152 599
152*02
152*03
132*05
152*06
132*07
152*09
132*10
1S2 613
152 617
152 618
132*19
152 621
132 623
132 634
152 633
152 626
132 628
152*29
132 630
152 631
132 632
132*33
132 632
152*33
152 638
152 639
132 **0
132*61
132*64
132*68
152*69
132 670
132 671
132*72
152*73
132*74
132*73
132*83
132*84
132*90
152*91
132 694
132*95
132 696
132 697
132 69*
132*99
132 700
132 701
131703
SSI
3«9
399
334
316
316
313
349
3W
2S9
314
377
317
330
330
sa
399
393
371
919
319
319
319
299
3S0
330
933
314
268
9*4
330
349
269
343
370
376
336
394
394
306
349
336
365
^
3SI
343
333
337
332
352
261
293
306
5*
306
n
269
318
318
334
396
279
368
368
371
364
304
341
337
361
346
399
273
274
325
347
301
293
339
303
397
394
338
30O
283
304
297
294
307
317
317
344
373
967
331
346
367
3t4
IS
3S0
310
37«
363
Number
133 713
132 714-1
132 714-2
132 714-3
152 714-4
132 715-1
152 715-2
152 731
152 733
132 723
132 734
152 723
132 723
132 729
192 730
132 731
IS2 733
132 734
132 733
132 716
133 737
133 799
132 740
133 741
132 743
132 743
132 744
132 746
132 747
132 749
132 730
132 756
152 757
152 759
132 761
132 762
152 763
152 764
152 767
152 766
152 769
152 770
152 772
152 773
152 774
152 773
152 776
1 52 777
152 778
152 779
152 782
152 783
152 787
132 738
152 789
152 791
152 799
152 800
152 821
152 823
152 824
152 825
152 826
152 831
152 833
152 834
152 839
152 840
1S2 841
152 842
152 843
132 345
152 846
152 847
152 854
132 396-1
132 836-2
152 856-3
152 857
152 858 .
152 859
152 860
152 861
152 862
152 863
152 864
152 868
152 869
152 870
152 880
152 832
152 883
152 885
152 888
152 889
152 891
152 892
152 893
152 894
152 896
152 897
152 898
152 900
152 901
152 90S
152 906
152 907
9*1
MO
940
940
340
318
318
300
323
331
313
344
3sa
307
336
341
306
310
293
333
322
327
269
295
346
305
263
276
323
312
299
262
262
308
322
322
267
265
275
333
281
276
274
274
280
280
305
338
307
325
265
261
351
261
348
X3
282
282
334
296
298
315
308
287
301
257
308
309
393
349
325
307
257
301
344
312
312
313
327
328
295
296
295
314
339
339
338
336
281
331
337
317
286
264
265
343
282
282
320
319
351
287
320
346
279
328
283
Number
153 903
152 911
152 912
152 913
152 916
152 922
152 923
152 925
152 926
152 929
152 930
152 932
152 933
152 934
152 935
152 936
152 937
152 938
152 939
152 940
152 942
152 946
152 947
152 948
152 949
152 951
152 932- 1
152 932-2
152 955
152 958
152 959
152 960
1.^2 962
152 963
152 966
152 967
152 968
152 972
152 973
152 977
152 979
152 981
152 984
152 985
152 946
1 52 987
152 988
152 992
152 993
152 994
152 995
152 996
152 997
153 003
153 030
153 033
153 034
153 035
153 037
153 046
153 050
153 053
153 058
153 062
153 063
153 064
153 068
153 070
153 071
153 085
153 088
153 0B9
153 090
153 091
153 095
153 096
153 100
153 109
133 110
153 ISS
153 172
153 195
153 196
153 226
153 271
153 272
153 273
153 274
153 273
153 277
153 278
153 279
153 330
153 333
153 336
153 337
153 338
153 330
153 331
153 332
153 336
153 337
153 338
153 339
153 341
153 342
153 343
N<
232
333
346
264
331
293
337
344
289
3S0
391
344
331
320
300
258
301
301
308
313
313
258
326
299
299
283
280
280
347
297
312
338
337
330
348
285
259
319
344
279
302
351
288
288
304
349
309
296
3S0
295
300
347
332
2M
334
373
302
303
369
391
303
331
306
309
280
280
335
333
332
275
330
338
276
276
298
286
307
333
264
277
316
326
326
303
993
311
394
333
932
9r
399
996
919
363
366
370
366
371
373
271
365
368
367
310
96*
366
370
133 344
153 343
133 346
153 349
153 349
153 330
153 351
153 392
133 399
153 303
133 397
153 991
133 460
153 476
133 496
153 906
133 370
153 371
153 372
133 S7S
133 974
133 975
133 976
133 977
133 997
139 909
139 909
139 996
133 997
153 406
199 ilO
133431
133 «C2
15343*
153 633
133636
153 639
153 630
153 691
159 726
153 790
153 791
133 793
153 867
153 882
153 883
153 884
153 885
161 213
161 225
161 226
161 227
161 371-'
161 994-1
161 968
171029
171 034
171 041
171 042
171 043
171 044
171 046
171 047
171 050
171 051
171 190
171 191
171 192
171 193
171 194
171 195
171 196
1:1 197
171 198
171 199
171 200
171 201
171 202
171 203
171 204
171 205
171 206
171 307
171 208
171 209
171 210
171 211
171 212
171 213
171 214
171 215
171 216
171 217
171 218
171 219
171 220
171 221
171 222
171 223
171 300
171 301
171 302
171 303
171 304
171 305
171 306
171 307
269
379
993
372
370
271
266
267
266
322
263
280
260
313
293
262
333
274
262
270
328
268
302
302
3lO
277
273
323
323
277
316
331
333
285
282
347
287
286
261
257
333
311
310
308
330
313
284
307
330
313
329
311
273
304
302
272
316
332
317
317
330
309
314
311
309
281
341
285
329
293
296
298
332
329
286
292
292
336
329
292
290
291
291
292
289
290
291
289
289
291
291
292
291
291
299
290
290
390
290
379
991
9»
919
919
9t3
919
929
1-15
I7t 30S
171 J09
171310
171 311
171 312
171 313
171 315
171 327
171 32*
171 38»-l
171 331
171 332
171 333
171 334
171 33S
171 336
171 337
171 33>
171 339
171 340
171 341
171 342
171 343
171 344
171 343
i:i 348
171 349
171 3SO
171 3»1
171 352
171 353
171 354
171 :»5
171 356
rHSC-M-743<CS)
nB-453.38
n>-6*4
n»-7io
311
273
277
314
31*
263
3S2
321
2t7
3«S
329
2«0
266
31S
333
347
309
3*3
3)4
342
335
339
269
2SS
309
330
321
321
321
30S
302
321
331
345
323
3«S
390
3DI
PI»AL -609
PIBMRl- 7*2-59
niMRI-80«-«0
P1BMRI-S31-60
nMina P ROW- 3961
PLASTEC-3
ITL-TR-eO-2
PPL-TR-60-3
PRB TRN-107
PRBTRN-lO*
PRMSTU »-l8
PSl 3000:15-25-0
PSNS - ML P- 300-10
PU AEL-442
PU AEL-496
PU AEL-517
M A£l,-5l9
QPEAMRS->901
QFEA R-4
0ICK725-OQ645
RkC-60-1-2
R60SD4S6
RADC-TN-60-199
RADC-TN-60-201
RADC-TN-60-202
RADC-TR-57-85
RADC-TR-5«-lll.«
RADC-TR-59-53
RlAL-60-2561
RlAL-60-2562
RIAL -60- 2563
RIAL-60-2856
RlAL-60-3203
RPI Ma(l#ep-29
RS-15
S/TD-1735, V. 1
S/TD-173S. ».2
12
313
301
301
294
.1 304
300
314
322
349
312
312
Numbw BH
S/TD-1735. V.3 313
SEF-PSD59-4 SM
SlPRETR-12. ».14 m
SqukirK-96-P S»
sAl-2937 304
TCC-BI20-59 316
TED ADC RS-7045
(5915-A) 269
TBD MAM AE 4177, FR 330
TED-PTR-EL-9006. R-l 301
rRC-l2l-SR-2 33»
TRC-131-SR-2 305
UMNCR-25 2St
UMN CR-26 23»
UMNCR-27 23;
UMR|-2§20-4-T 300
UMRI-2900-57-T JM
UMRI-290O-2O2-T 305
U9CEC-R-73-201 327
USNRDL AD-I28(C) 277
USNIUX.-TR-62 274
USN1UX.-TR-I11 334
USNRDL-TR-152 335
USNRDL-TR-277 335
USNRDL- TR-2«9 335
USNRDL-TR-396 332
USNRDL- TR-40* 333
USNRDL-TR-421 273
USRL RR-52 302
UWER-213-lO 217
WADC-TN-56-H7 2*6
WADC-TN-59-I42 270
WADC-TR-56-5«5.pt.2 287
WADC-TR 58-95.PC.3 285
WADC-TR-58-476. V. 1 348
WADC-TR- 59- 36 261
WADC-TR-59-526. (K. 2 329
WADC-1R-59-570 345
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WADD-TN-60-136
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WADO-TN-60-155
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WADD-TN-60-165
WADO-TN-60-183
WADD-TN-60-197
WADD-TN-60-212
WADO-TN-eO-2l3
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WADO-TR-60-333
WAOO-TR-eO-384
WADD-TR-eO-445
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WADD-TR-60-511,
WADO-TR-eO-521
WADD-TR -60- 544
WADO-TR-60-604
WADD-TR-60-621
WADO-TR-60-637
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April 18, 196*" "'"T»'
Vol. 35, No. 4'*!^ » ««
CHEMISTWr
LiBRMRT
A monthly listing of
Government research reports
available to industry . . .
this issue:
iMechanism of Wear on Nonmetallic
Materials. (PB 171 474)
Qectron Physics of Traveling Wave Tube
Devices. (PB 171 414)
lialuation of Brazed Honeycomb Struc-
tures. (PB 171 408)
falaence of Environment on Ceramic
Properties. (PB 171 398)
||M Sinks: Materials. (PB 171 372)
Ugh-Pressure Research in Metals and
{Ceramics. (PB 171 025)
k Survey of Computer Programs for
Chemical Information Searching.
(PB 161 586)
llfractory Metals in Europe.
(PB 161 233)
Sliws-Corrosion Cracking: A Nontech-
• lical Introduction to the Problem.
(PB 151 103)
ods of Measuring Emittance.
(PB 161 228)
Complete list of printed report*
begins on page iii
Chemnoy
•UCt
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s
1
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BUSINESS AN!' 1-FFEN.^f:, ^FdVjft- Ai'V:'-.
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^.xfo'^uiS?' *"'""" CONTENTS- •"
* * ■ Page
PRINTED REPORTS AVAILABLE FROM OTS ANNOUNCED IN THIS ISSUE . iii
BBLIOCRAPHY 391
ASTRONOMY '. ///^'.V///^'.'.'.'.'.V/^'.V.'.'.'.'.'.'.'.'^ 391
Aatrophysica 392
BEHAVIORAL SCIENCES 392
Personnel and Training •!..'....*.'!!. i i !! i ! 393
Psychology .............'.'.'.'.'...'. 394
BIOLOGICAL SCIENCES 396
Anatomy and Physiology !.*!!!.*!!.'.*.'.'.'.'.*!.'.*.*.'.'!!!.'!.'.*.'! 397
Biochemistry !!!!!!!.!!!!.*!!!! 400
General Biology f 402
vflcrobioiogy !.'!!!.!!!!!!.'!!!!!!.*!! 403
Pathology !.!!!!!!..!!.!!!! 403
Radiobioiogy 404
CHEMISTRY '.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'. 40S
Analytical Chemistry !!!!!!!!!!!!! 405
c^gainic Chemistry !!!!!!!!!!!!!!!!!.'!!!!!!.'!! 405
Physical Chemistry ' ' 405
EARTH SCI ENCES '.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'. 411
Climatology and Meteorology .'..!.'!.*!.'.'.'.* 411
Oceanography ."!!.!!.'!!!!!!!.'!!!!!!.'!!!! 413
Physics of the Atmosphere 41 4
ENGINEERING \ '.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'. 416
Aeronautical Engineering !!!!!!.'!!!!!!!!!!!!!!!!!!!! 416
Civil Engineering ..'!!!!!.'!!!!!!!!!!!!!.'!!*!!! 420
Electrical and Electronic Engineering .....!!!!!!!!!!!!!!!!!!!!!!!!!!!! 420
Ordnance, Missiles, and Satellite Vehicles !!.!!!!!!! 435
Sanitation and Safety Engineering '.'.'.'. ! " 440
Ship Building 440
FOOD, HANIS.ING, AND PACKAGING EQUIPMENT '. ". 441
Food V.'.V.'.V.V. 441
Packaging _ 441
MACHINERY, FABRICATION, AND ACCESSORY EQUIPMENT 442
Engines and Propulsion Systems !.!.'!!! 442
Manufacturing Equipment and Processes 444
MATERIALS '...'.'.'.'.'.'. 445
Ceramics and Refractories : !!.!!.'!!!!!!!!!!.'!!!!!!!!!! 445
Fuels, Lubricants, and Hydraulic FluitJs !!'.!.'!.'!!!!.'!!.*!!.'!!!!!! 447
Leather and Textiles 443
MATHEMATICS , ' !!!.!!!!!!!!!!!!!!!!!!! 449
Confuting Devices 451
MECHANICS '..'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.'.v.'.'.'.'.'. 452
Aerodynamics and Pneumatics ."!.'!!!!!."!!!.'!!!!!.'!.'.'.'!.'!!.'.*!.'.' 454
Hydrodynamics, Hydraulics, and Hydrostatics !!!!!!!!!!!!!! 457
METALLURGY 458
Ferrous Metals !!!!!!!!!!!.'!!!!!!!.*!!!!.'!!!!!.'!.'!!! 459
Nonferrous (except light) Metajs !.!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! 460
Structural Metallurgy and Corrosion .'. 46O
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY '...'.'.'.'.'.'.'.'.'.'.'. 462
bstruments and Installations !!!.'!!!!!!!!!!! 463
Nuclear Reactions !.!!!.!!!!!!!!!!!!!!!!!!.!!.!!.! 463
Radioactivity 454
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT '.'.'.'.'.'.'.'.'.'.'.'.'.'. 464
PHYSICS ; ............'.'.'..'.'.'.'.'.'.'.'.'.'.'.'.'. 465
Electricity and Magnetism 466
Electronics !..!!!!.!!!.!!!! 466
Molecular Physics and Spectroscopy * 467
C^cs 468
Solid State Physics ^ 469
Theoretical Physics 472
Thermodynamics !!!.!! 474
Wave Prcmagation ' 475
RESEARCH METHODS, TECHNIQUES AND EQUTPMEhTr ..'. 476
Photographic Equipment 478
SOCIAL SCIENCES .v. ! ! ! . 478
Documentation ; T/N . . . 479
MISCELLANEOUS \ '..'.'. .'.WW. 480
ATOMIC ENERGY COMMISSION REPORTS 481
General, Miscellaneous, and Progress Reports 481
i
ft'>i-''.vv A
Ese
ATOMIC ENEROY COMMISSION REPORTS (con. )
Bloiogy and Medicine 482
Chemical Sepa|-acion8 Processes for Plutonium and Uranium 482
Chemistry 484
CmtroUed Thermonuclear Processes 486
Criticality Studies 486
Engineering and Equipment 487
Geology and Mlneralc^ 488
Health and Safety 488
Inatruments 490
Isotopes- -Industrial Technology 492
Isotope S«>ar8tion 493
Mathematics afid Computers 493
Metals, Ceran^cs, and Materials 493
Meteorology 499
Nuclear Explosions" "Peaceful Applications 499
Particle Accelerators and High- Voltage Machines 499
Physics ^ 500
Radiation Effe<:ts on Materials 506
Reactor Technology 507
Teclmoiogy- - Feed Materials 530
Waste Disposal and Processing 532
SOURCE INDEX
SUBJECT INDEX
NU\eER INDEX
I-l
1-5
1-13
/
U
PRINTED REPORTS AVAILABLE FROM OTS
ANNOUNCED IN THIS ISSUE
BEHAVIORAL SCIENCES
Research on psychological parameters of sound.
Feb 60. 65p. (PB 171 403) $1.75
Page
396
BBLIOGRAFHY
Antimony, bismuth, gallium, indium, selenium, and tellurium.
Sep 60. I6p. (OTS SB-438) 10 cents 991
Germanium and silicon. Sep 60. 21p. (OTS SB-437) 10 cents 391
Magnesium. Nov 60. 23p. (OTS SB-449 10 cents 460
Quartermaster Corps textile series reports (1942-1960).
Nov 60. 6p. (OTS SB-440) 10 cents 448
Semiconductors (Supplement to CTR-340). Sep 60. 20p.
(OTS SB-435) 10 cents 472
BIOLOGICAL SCIENCES
Gross and microcirculatory effects of tilting and acceleration
on the golden hamster. Sep 60. Sip. (PB 171 367) $2.25 398
Radiological health data. Volume 2, No. 1. Jan 61. 63p.
(PB 161 371-10) $1.00, $9.00/yr 404
Studies on the endolymphatic DC potential of the guinea pig's
cochlea. Aug 60. 12p. (PB 171 392) 50 cents 397
CHEMISTRY J
Amino oarboxylic amphoteric surfactants in alkaline cleaners.
9 Nov 60. 9p. (PB 171 128) 50 cents 407
Electroanalytical method for the determination of carbon and
hydrogen in organic compounds. Sep 60. 26p. (PB 171 409) 75 cents 405
Investigation of the chemical reaction between tungsten and
aluminum oxide. 1 Apr 60. 73p. (PB 171 373) $2.00 408
Mass in air 200 grams to 30 kilograms classes S-1 metric, P, and Q.
18 May 60. 28p. (PB 171 236) 75 cents 405
Molecular weight determination in the characterization ol polymers.
Sep 60. 28p. (PB 171 401) 75 cents 406
Thermochemistry and photochemistry of organic halogen compounds.
6 Sep 60. 98p. (PB 171 376) $2. 25 407
Thermodynamic analysis of solubility in liquid metal systems.
7 Dec 60. 24p. (PB 161 990) 75 cents 409
EARTH SCIENCES
— ' ' f,
Survey of spread -F. Nov 60. 72p. (PB 161 583) $1.75 415
ENGINEERING '
A. F. signal generator SG-21AJ and SG-21AA^. 12 Aug 60. 12p.
(PB 171 243) 50 cents 422
Airport runway and taxiway design: excerpts on typical configurations,
capacities, evaluation of design. July 60. 188p. (PB 171 370) $3.00 416
Audio frequency impedance measuring equipment OJ-1, OJ-2, OJ-3 and
general radio 650A. 25 July 60. 33p. (PB 171 245) $1. 00 422
Capacitors, fixed: General radio 505 series. 14 Sep 60. 23p.
(PB 171 239) 75 cents 422
Electron physics of traveling wave tube devices. July 60. 55p.
(PB 171 414) $1.50 425
Environmental factors influencing metals applications in space vehicles.
1 Dec 60. 49p. (PB 151 101) $1.25 437
Evaluation of brazed honeycomb structures. Sep 60. 321p.
(PB 171 408) $5. 00 418
iU
ENGINEERING (:on.)
;
Page
438
422
422
417
423
Exit taxiway locations. Sep 60. 24p. (PB 171 369) 75 centa 417
Extended Baler angle coordinate 8y3tem for use with all-attitude
aircraft simulators. Aug 60. 30p. (PB 17 1 404) 75 cents 418
Gas cycle cooling systems for space vehicles. June 60. 23p.
(PB 171 363) 75 cents
Generator, Timej Mark. Tektronix 180A. 18 Aug 60. I8p.
(PB 171 241) $0 cents
Heat procective ablative coatings for radoraes. Aug 60. 85p.
(TB 171 416) |2. 25 • • •
H«M sinks: Materials. 17 Aug 60. 32p, (PB 171 372) $1.00
Heterodyne freqitoicy meters 125 KC to 20. 000 KC. 17 Aug 60. 17p.
(PB 171 240) go cents •
Human factors inj design of automatic programming and recording
for trainers i(AN/ASG-15-Tl fire control system trainer).
Aug 60. 14p, (PB 171 419) 50 centa 436
Microwave attenuation. H-band (7.05 to 10.00 KMQ 0 to 50 DB.
28 June 60. 24p. (PB 171 228) 75 cents 423
Microwave attenuation. J -band (5. 85 to 8. 20 KMCPS) 0 to 40 DB.
18 Dec 59. 2^, (PB 171 225) 75 cents 423
Microwave attenUation, S-band (2. 60 to 3. 95 KMCPS) 0 to 40 [».
25 Feb 60. 33p. (PB 171 226) 75 cents 423
Microwave attenuation. X-band (8. 2 to 12. 4 KMCPS) 0 to 50 DB.
18 Dec 59. 23p. (PB 171 224) 75 cents 423
Microwave attenuation. X-band (8. 20 to 12. 40 KMC) 0 to 50 DB.
24 June 60. 2$p. (PB 171 227) 75 cents 423
Microwave frequency. G-band (3. 95 to 5. 85 KMCPS) 1" to 2"
waveguide siz^. 3 Sep 59. 19p. (PB 171 229) 50 cents 424
Microwave frequency, G-band (3. 95 to 5. 85 KMCPS) +0.0002%
1" X 2" waveguide size. 18 Dec 59. 25p. (PB 17r231) 75 cents 423
Microwave frequ^cy, J -band (5. 85 to 8. 20 KMCPS) +0. 0002%
1 1/2" X 3/4" (waveguide size. 18 Dec 59. 26p. 1^ 171 230) 75 cents 424
Microwave frequency, S-band (2. 60 to 3. 95 KMCPS) +0. 0002%
1 1/2" X 3" waveguide size. 7 Mar 60. 22p. (PB 171 232) 75 cents 424
Performance andi operation of the image isocon camera tube.
Apr 60. 27p. (PB 171 386) 75 cents 425
Research on high temperature complex component development.
1960. 77p. (f»B 171 380) $2. 00 427
R. F. Signal generator set AN/URM-26 or AN/URM-26B. 6 July 60. 32p.
(PB 171 246) tl.OO 424
Signal generator iAN/GPM-15. 12 Aug 60. 21p. (PB 171 244) 75 cents 424
Snow-compactioi^ equipment snow drags. 20 Oct 60. 37p.
(PB 171 375) il.OO
Standard laboratory procedures for sensitivity, brisance and subility
of explosives.! Jan 61. 45p. (PB 171 326) $1. 25
State-of-the-art burvey of delay techniques. Sep 60. 47p.
(PB 171 420) ii. 25
Study of pilot operational capabilities In the use of the FAA pictorial
position indicator and the Avion pictorial navigational display in the . , - '-
terminal areal Feb 60. 97p. (PB 17 1 368) $2. 25
Synthesis and purification of dielectric materials. Sep 60. 77p.
(PB 171 364) 12. 00
Test oscillator stet AN/PRM-10 8 Aug 60. 21p. (PB 171 242) 75 cents
Voluge standing [wave ratio, J -band (5. 85 to 8. 20 KMCPS)
1.00:1 to 10 :|l. 18 Dec 59. 17p. (PB 171 233) 50 cents 424
Voluge standing wave ratio, S-band (2. 60 to 3. 95 KMQ
1.00:1 to 10:1. 25 Feb 60. I6p. (PB 171 234) 50 cents 424
Voltage standing! wave ratio 3/8" coaxial, type N connector (100 to
1000 MQ. 2iAug60. I8p. (PB 171 235) 50 cents 424
FOOD, HANDLING AND PACKAGING EQUIPMENT
420
438
432
430
434
424
Individual alumiiium feeding containers. Part I. Engineering
evaluation phi se. Aug 60. 25p. (PB 171 418) 75 cents ..
Iv
441
MACHINERY, FABRICATION, AND ACCESSORY EQUIPMENT
Evaluation of numerically controlled machining of forging dies.
Sep 60. 80p. (PB 171 378) $2. 00 , 445
High -impact metal forming. 1957-1960. An annotated
bibliography. July 60. 40p. (PB 171 379) $1.00
Itiysical and mechanical properties of some high-strength
fine wires. 20 Jan 61. 21p. (PB 161 230) 50 cents
MATERIALS
Deterioration of textile materials by ultraviolet lighL . .
Oct 60. 160p. (PB 171 417) $3.00 448
Influence of environment on ceramic properties.
Oct 60. 30p. (PB 171 398) 75 cents 446
Investigation of diffusion barriers for refractory metals.
Aug 60. 59p. (PB 171 400) $1. 50 446
Investigation of the feasibility of utilizing available heat
resistant materials for hypersonic leading edge
applications. Volume IV. Thermal properties "^
of molybdenum alloy and graphite. Oct 60. 86p. (PB 171 390) $2. 25 445
Quartermaster Corps textile series reports (1942-1960)
Nov 60. 6p. (OTS SB-440) 10 cents 448
Refractory metal constitution diagrams. Oct 60. 197p.
(PB 171 391) $3. 00 r 447
Refractory metals in Europe. 1 Feb 61. bp. (PB 161 233) 50 cents 446
Research study to determine the phase equilibrium relations of
selected metal carbides at hi^ temperatures. July 60. 28p.
(PB 171 365) 75 cents 447
Spectrum and contour analysis of ultrasonic pulses for
improved nondestructive testing. Dec 60. 19p. (PB 171 186) 50 cents 445
Stability of ceramic materials at temperatures to 2000° C.
Sep60. 68p. (PB 171 405) $1.75 446
Vi^x>rization and physical properties of certain refractories.
Part I. Techniques and preliminary stixiies. Oct 60. 73p.
(PB 171 413) $2. 00 445
MECHANICS
Annouted bibliography and selected references on the
theory of elastic plates. Jan 60. 2:^. (PB 17 1 374) 75 cents 453
Determining air reactions on moving vehicles. Part FV.
Methods of aerodynamics: elementary bodies. Aug 60. 946p.
(PB 171 387) $10.00 455
Determining air reactions on moving vehicles. Part V.
Methods of aerodynamics: composite bodies. Aug 60. 236p.
(PB 171 388) $3. 50 455
Effects of time varying aerodynamic coefficients on
aeroelastic response. Apr 60. 109p. (PB^ 171 407) $2.50 454
Transient and nonlinear effects on high speed, vibratory
thermoelastic instability phenomena. Part I: Theoretical
consideraUons. July 60. I25p. (PB 171 415) $2.75 454
METALLURGY
Development of wrought beryllium alloys d improved properties.
Sep 60. 126p. (PB 171 389) $2.75 ' 46O
Effect of basic physical parameters on engineering properties of
intermetallic compounds. Aug 60. 34p. (PB 171 393) $1. 00 461
Effect of several geometrical variables on the notch tensile strength
of 4340 steel sheet heat treated to three strength levels.
Sep 60. 42p. (PB 171 396) $1.25 459
Effect of state of stress on the failure of metals at various
temperatures. July 60. 32p. (PB 171 366) $1.00 459
Effective stress concentration factors for flight vehicle materials
under various conditions during fatigue testing.
Oct 60. 161p. (PB 171 410) $3.00 ^ 461
V
MgTALLURGYCcjop.)
High -pressure re^rch in metals and ceramics. Sep 60. 77p.
<PB 17 1 025) $ft. 00 VA- • • V^-
Hydrogen embrittjement o< tiunium alloys. Oct 60. 49p.
(PB 171 394) U. 25 • • • • •
Magnesium. Novl60. 23p. (OTS SB-44^ 10 cents
Mechanical properties of beryllium. Sep 60. 37p.
<PB171 411) $1.00
Melting and castifg at the refractory metals molybdenum,
columbium, tatitalum, and tungsten. 18 Dec 60. 33p.
(PB 1 5 i 098) $1 . 00
Metallurgical appiication erf X-ray projection microradiography.
l2Aug60. 63b. (PB 171 381) $1.75 s
Partitioning and i^icrodistrlbutlon of interstitial alloying In
titanium. Sep 60. 42p. (PB 171 412) $1.25
Practical evaluation ot the standard stress -strain curves and
related properties. July 60. 27p. (PB 161 896> 75 cents
Preliminary design information on recrysuUized mo-0.5Ti aUoy
for aircraft and missiles. 16 Jan 61. I2p. . >. . >
(PB 161 229) Sb cents
Stress -corrosion 'cracking: a nontechnical Introduction to
75 cents 461
459
461
460
4S9
458
461
460
462
458
the problem. 6 Jan 61. 30p. (PB 151 103)
Tiunium -alloy fdrgings. 19 Dec 60. 89p. (PB 151 100) $2.25
Void formation aiid grain boundary sliding in aluminum -
magnesium so^id solution alloys. Sep 60. 37p.
(PB 171 399) il.OO
MISCELLANEOUS
Report of NRL Prtogress. Mar 61. (PB 171 316) $1.25, $10.00/ycar
459
460
480
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY
Hasp. Annual briefing no, 3. 15 Dec 59. Il2p.
Hi^ altitude sarnplmg program, I July 59. 33p. (PB 171 361) $1.00
Investigation ot the response of photomultiplier tubes. Aug 60, 18p.
(PB 171 402) i) cents
SPM (Stochastic process Method) equation for calculating the
spatial variatibn of neutron spectra. Sep 60. 158p.
(PB 171 397) ^3.00
PHYSICS
(PB 171 362) $2.50 464
464
463
Effect of gravity fcm free convection heat transfer. Part L The
feasibility of Using an electromagnetic body force, Aug 60
(PB 171 395) $1.50
Effect of temperature on the creep of polycrystalline aluminum by
the croes-slipi mechanism. June 60. 21p. (PB 171 360) 75 cents 470
Indium anlimonicfc for semiconductor -device feasibility studies.
Apr 60. 67p. (PB 171 406) $1.75 469
Infrared radiatio*i black body sources 50° C to 100° C. a0087 to
0.50 inch diameter aperture. 27 Apr 60. 40p. (PB 171 238) $1.00 468
Investigation of fftclors controlling properties of pressure-sintered
alkali halides, June 60. 24p. (PB 171 371) 75 cents 471
Measurements aid sundards in plasma-physics and astrophysics at
the National Bureau of Standards. July 60. 33p. (PB 161 560) $1.00 465
Mechanism of weiar on nonmeullic materials. Oct 59. 19p.
(PB 171 474) $0 cents 469
Methods of measiiring emlttance. 27 Dec 60. 2^.
(PB 161 228) $0 cents
Microwave propagation characteristics in germanium
10 Nov 59. 21p. (PB 171 377) 75 cents
Notes on the rel^onship of temperature and resistance
1 [)ec 60, 9p, (PB 171 187) 50 cents
Pressure measaflements 0 to 31. 5 in. Hg. 21 June 60. 21p.
(PB 171 237) 75 cenu
vi
IHYSICS (con. )
Semiconductors (Supplement to CTR- 340). Sep 60.
(GTS SB-435) 10 cents
^ge
RESEARCH METHCOS. TECHNIQUES AND EQUIPMENT
Change in apparent image size caused by motion during
photographic exposure. May 60. 18p. (PB 171 385) 50 cents
SOCIAL SCIENCES
Analytical and experimental study of a method for literature
search in abstracting Journals. Dec 60. 79p.
(PB 171 478) $2.00
Survey of computer programs for chemical information
searching. Feb 61. 87p. (PB 161 586) $2,25
472
478
479
479
For your convenience OTS order blanks (Form TS-37) are available
on request from the OFFICE OF TECHNICAL SERVICES.
vU
.•»VH ^'>' '^ T^
".?:y\ •>'*A ii'K'' "u ■■« •
( i t
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
OFflCE OF TECHNICAi SERVICES
Pages 391-532
April 18, 1961
BIBLIOGRAPHY
Banelle Memorial Inst. , Columbus, Ohio.
BIBUOGRAPHY OF THE UQUID-SOUD CYCLONE
1939 TO 1957, l^ O. F. Tangel, R. J. Brison, and
D. A. Jacobs. [19581 19p. 243 refs.
Order from LC miJ2.40, ph$3.30 PB 154 409
This report released for sale to the public 15 Feb 61 .
To facilitate the use of this bibliography, the entries
have been arranged into the following categories: (a)
Theory and design, fluid flow, efficiency determina-
tion, and effect of operating variables, (b) Applica-
tions: (1) In mineral processing, (2) In the pulp and
paper industry, (3) In the petroleum industry, (4)
Miscellaneous, including chemical and food processing,
(c) General, including review articles, bibliographies,
books, and articles general in nature.
Diamond Ordnance Fuze Labs. , Washington, D. C.
SEARCHING THE LITERATURE FOR TRANSDUCER
INFORMATION. PART 11. A SURVEY OF THE
FIELD, by J. Pearlstein. 1 Dec 60, 118p. 138 refs.
TR'898
Order from LC mi$6. 00, ph$18. 30 PB 153 505
A survey is presented of current knowledge with re-
spea to the availability, application, design, calibra-
tion, and testing of transducers. The references
covered are restricted to the following forms of litera-
ture: bibliographies, tutorial papers, surveys (includ-
ing state-of-the-art studies), guides, handbooks,
monographs, treatises, and comprehensive catalogs of
commercially available transducers. The items are
arranged under the following principal headings:
Transducers and Instrumentation in General; Commer-
cial transducers; Effeas, Principles, and Phenomena;
Basic Materials; and Measurands (quantities, magni-
tudes, or phenomena that maylbe measured, observed,
or sensed). Twenty eight tables pertaining to the use,
performance, and availability of transducers are
included. (Author) (See also PB 161 320)
Office of Technical Services, Dept. of Commerce,
Washington, DC.
ANTIMONY. BISMUTH, GALLIUM, INDIUM,
SELENIUM, AND TELLURIUM. Sep 60, I6p.
266 refs. OTS Selective Bibliography SB-438.
Order from OTS $0. 10 OTS SB-438
A bibliography of reports listed in the two OTS monthly
abstract journals: U. S. Government Research Reports
and Technical Translations. This bibliography in-
cludes reports added to the OTS collection during the
period 1950 to October 1960.
Office of Technical Services, Depl. of Commerce,
Washington, D. C
GERMANIUM AND SILICON. Sep 60, 2Ip. 360 refs.
OTS Selective Bibliography SB-437.
Order from OTS $0. 10 OTS SB-437
A bibliography of reports listed in the two OTS monthly
abstraa journals: U. S. Government Research Reports
and Technical Translations. This bibUography covers
repwrts added to the OTS collection during the period
1950 to September 1960.
ASTRONOMY
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
A COMPUTER PROGRAM FOR PROCESSING SIG-
NALS RECEIVED IN RADAR ASTRONOMY EXPERI-
MENTS, by P. L. Fleck, Jr. and T. J. Goblick. Rept.
on Contract AF 19(604)7400. 14 Oct 60, 21p. 6 refs.
34G-0005; AD- 245 549.
Order from LC mi$2. 70, ph$4. 80 PB 152 827
In 1958 and 1959, this laboratory attempted to obtain
radar reflections from the planet Venus. The received
data were analyzed on an IBM 7|I9 Data Processing ma-
chine. This report describes the General Detection
Program (which was written mainly in FORTRAN) that
was used for the data processing.
391
Astrophysics
CorneU U. Schooi of Electrical Engineering, Ithaca.
CORRELATOR FOR NOISE SIGNALS WITH APPLI-
CATION TO 200 MC/S POLARIMETER. by Kenji
Akabane. Technical rept. no. 3 on Contract Nonr-
401(27). 15 Jan 60„ 45p. 9 refs. Research rept. EE
^r ^n^L'S'mia. 30. ph$7. 80 PB 152 872
The principle of a inoise correlator that gives the am-
olilude o* the croep-correUtion function between two
noise signals Is diWrusstfd The amplitude of the cross-
correlation function is directly given by the output of
the correlator The minimum detectable cross-cor-
relation function i$ also calculated for the correlator.
One example of scalar observation by the 200 mc polar -
imeter Is illustraied. (Author)
Contents:
System analysis for human faaors
Concepts and approach to human factors In system
design
Identification and analysis of personnel functions
Identification and analysis of human performance
requirements
Human engineering in equipment design
Detection of error -producing designs
WorkpUce layout and equipment design
Design for maintenance
Design of Job aids
Design of physical environments
Development of the personnel subsystem
Job design and manning
Design of selealon and training procedures
Design of training aids and devices
Use of self-lnstrualonal devices
Evaluation of personnel proficiency
Human factors bookshelf
Maryland U. , Ciillege Park.
ARTIFICIAL MOE4FICATION OF TOE EARTHS
RADIATION BELt. by Fred Singer. R^pt. on Conn-act
AF 18(600)1038. (1958] 31p. 30 refs. AFOSR TN-58-952,
AD- 205 345. I ,cn-,o9
Order from LC n^%3. 00, ph$6. 30 PB 150 722
Presented at the rtlfth Annual Meeting of the American
Astronautical Society held in conjunction with the 125th
Meeting of the Anierlcan Association for the Advance-
ment of Science,
1958.
A/ashington, D. C, December 27-31,
Minnesota U. S<JhooI of Physics, Minneapolis.
TABULATION OP HIGH ALTITUDE RADIATION
DATA FOR THE I IGY PERIOD, by John R. Winckler.
Technical rept. i^). CR- 28 on 2. 12 Cosmic Ray In-
tensity at High Altitude, Contract [Nonr-710(19)I.
Apr 60. 199p. 1 tef. AD- 238 769.
Order from LC t|i$8.70. ph$30. 30 PB 148 496
This compendluni contains the numerical data obulned
on a series of high altitude balloon flights conducted
from Minnesota 4nd from a' bmited number of field
stations during t»^ IGY period. The normalized Ioni-
zation chamber rjates and the normaUzed Geiger
counter rates ar« given for all of the fUghts. The data
obtained during ascent of the balloon are given in
graphical form afid include also the ratio: (ion
rate/counter rat^) as a function of balloon pressure
height. The datai obtained at ceiling altitude are given
in tabular form ^eraged over l5-mln. intervals, ap-
proximately. Tl« geographic latitudes and longitudes
obtained partly from radio direction equipment (GMD)
but mainly from aerial camera photographs, are included
in the constant le4el portion of the data. (Author)
BEHAVIORAL SCIENCES
American Inst, for Research (Pittsburgh, Pa. 1
HUMAN FACTOHS METHODS FOR SYSTEM DESIGN.
by John D. Folley, Jr. . James W Altman (ed. ) and
^8. Rept. onContraaNonr-2700(00). 1960, 392p.
234 refs. AIR-2t0-60-FR-225; AD- 232 646.
Order from LC i^iiSl 1 . 10, ph$60. 60 PB 153 165
American Power Jet Co. , Rldgefield, N. J.
HUMAN ENGINEERING FACTORS AFFECTING
ARCTIC AIRCRAFT MAINTENANCE. DATA
SOURCES AND PROJECT BIBLIOGRAPHY. Rept. on
Contraa AF 41(657)41. Dec 57. 66p. 566 refs. Techni-
cal note AAL-TN-57-12. „ ..i ^^
Order from LC mi$3. 90, ph$lO. 80 PB 153 547
The scope of the current study of human factors affect-
ing arctic maintenance encompasses the basic mainte-
nance problem as modified by environmental stress.
Accordingly, data pertinent to the problem are of thr«
general sorts: (1) maintenance experience, (2) the
nature of the arctic problem, and (3) applicable psy-
diological and physiological factors.
Army Ordnance Human Engineering Lab. . Aberdeen
Proving Ground, Md.
STUDIES ON THE KINETIC DEPTH EFFECT AS A
MEANS FOR PRESENnNG THREE-DIMENSIONAL
INFORMATION: II. EFFECTS OF VARYING ANGLE
AND LENCTTH OF A TWO-DIMENSIONAL FORM, by
Charles Fried and James A. Meadows. Dec 60, 36p.
4 refs. Technical memo. 18-60. «.,.,.-,«
Order from LC ml$3. 00, phJ6. 30 PB 153 470
An attempt was made to correUte the amount of length
and angle changes of shadow projections of rotating
wire rods with the ease with which the depth impres-
sion of the Kinetic Depth Effect Is elicited. This at-
tempt was based on earlier findings of Wallach and
O'Connell. that the stimuli for the Kinetic Depth Effect
are length and angle changes of lines making up a mov-
ing form. The attempt was not successful as all
shadow transformations presented to the subjects in
this study produced the impression of a figure rotatlni
in space. Suggestion Is offered that further thought be
given to determining the stimuli for the Kinetic Depth
Effect lUuslon. (Author) (See also PB 146 160)
1- .
392
Personnel and Training
Adjutant General's Office. Washington, D. C
ABSTRACTS OF PRB RESEARCH PUBUCATIONS FY
I960, by Arthur J. Drucker and Emma E. Brown.
Aug 60. 28p. 47 refs. PRB Technical research
note 109.
Order from LC miJ2. 70, ph$4. 80 PB 153 440
Air Force Missile Development Center, Holloman
AFB, N. Mex.
HUMAN SCIENTIFIC AND TECHNICAL CAPABILI-
TIES AT HOLLOMAN AIR FORCE BASE, THfilR
ORIGINS AND DEVELOPMENT, by Theodore Saloutos
(U. of Callfarnla, Los Angeles). Sep 60, 129p.
Order from LC mi$6. 30, ph$19. 80 PB 152 686
Contents:
Part I: Development of Holloman Scientific and Tech-
nical capabilities, to July 1958
The government service, scientists and engineers,
and the problems of recruiting
The foreign-born scientists and engineers
The native-born scientists and engineers
Educational programs
Salaries of scientists and engineers
Expectations and frustatlons; An inquiry into the
problems of morale
Part II: Scientific and Technical capabilities July 1958-
June 1959
TTie office of the chief scientist
Dlreaorate of advanced technology
Directorate of aircraft missile test
Employees In miscellaneous categories
Educational backgrounds of 260 commissioned offi-
cers stationed at Holloman as of 30 June 1959
Applied Psychological Services, Wayne, Pa.
POST-TRAINING PERFORMANCE CRITERION DE-
VELOPMENT AND APPLICATION. A FURTHER
STUDY INTO TECHNICAL PERFORMANCE CHECK
LIST CRITERIA WHICH MEET THE THURSTONE
AND GUTTMAN SCALABILITY REQUIREMENTS,
by Arthur I. Siegel, Douglas G. Schultz, and Stephen
Benson. Rept. on Contract Nonr-2279(00). Mar iO,
85p. AD-234 691.
Order from LC mi$4. 8a ph$13. 80 PB 153 779
A test was made of the hypothesis that the technical
■kills involved in the work of aviation machinist's
mates are scalable in the same sense as are attitudes
and various psychophysical phenomena. Results in-
dicate that: (1) skills involved in the Naval rate of
aviation machinist's mate are scalable by the Thur-
■tone method of equal -appearing Intervals; (2) the
skills form a Guttman scale from the point of view of
the amount of inservice training required for achiev-
ing proficiency, (3) the Naval attitudes of the aviation
machinist's mate, as expressed in a self -report
questionnaire, do not relate strongly to proficiency in
the fleet; (4) the aptitude tests commonly administered
to all personnel entering the Navy correlate moder-
ately highly among themselves and with inservice
school success but had low correlations with job per-
formance as measured: and (5) It Is possible to use
•ttitudinal inventory scores effectively in combination
with other variables to predict post -training fleet
performance. (Author)
Arctic Aeromedlcal Lab. , Ladd AFB, Alaska.
SURVEY OF HUMAN ADJUSTMENT PROBLEMS IN
THE NORTHERN LATITUDES. CRITICAL FACTORS
UNDERLYING THE DECISION TO EXTEND OR NOT
EXTEND THE ALASKAN DUTY TOUR, by Frederick
H. Rohles, Jr. Nov 53, 48p. 6 refs. Proj. no. 22-
1301-0003. rept. no. I. series 2.
Order from LC mi$3. 30, ph$7. 80 PB 153 329
The ten most frequently reported reasons why the
single airmen did not desire to extend their duty tours
are presented in order of reporting frequency (l)lack
of recreation; (2) dislikes weather; (3) no feminine
companionship; (4) high prices; (5) job dissatlsfactioiu
(6) tour of duty too long; (7) dislikes city, (8) poor
base facilities; (9) cabin fever; andUO) desires state-
side duty. The ten most frequently reported reasons
for extending the duty tour given by the single airmen
are presented in order of reporting frequency: (1)
job satisfaction; (2) saving money, (3) general like of
Alaska; (4) likes outdoor activities; (5) has friends
here; (6) likes weather; (7) homesteading; (8) make
rank faster; (9) pioneer spirit; and (10) plans to get
married.
Arctic Aeromedlcal Lab. , Ladd AFB. Alaska.
A SURVEY OF REACTICW OF ARMY AND AIR
FORCE PERSONNEL, LADD AIR FORCE BASE,
TOWARD CERTAIN ASPECTS PERTINENT TO THE
EXPENSE OF THEIR INSTALLA'HON (POST EX-
ERCISE "DUTCH DOOR") by Anthony Debons. Spe-
cial project. Feb 51, 25p.
Order from LC mi$2.70, ph$4.80 PB 153 323
This report concerns the result of a survey pertaining
to personnel response to various aspects of the de-
fense program. It is an attempt to appraise: (a)
Personal evaluations of certain pertinent phases of the
defense program- (b) The extent of personal stability
in terms of acquired sense of security as related to:
(1) Leadership; (2) Equipment; (3) Training; and (4)
Knowledge of the defense assignment.
Personnel Lab. , Wright Air Development Div. ,
Lackland AFB, Tex.
FAMILIARITY EFFECTS IN EVALUATIVE JUDG-
MENTS, by Joseph M. Madden. Nov 60. I2p. 11 refs.
WADD-TN-60-261.
Order from LCmi$2. 40, ph$3. 30 PB 153 853
This report is one of a series dealing with rater bias
in job evaluation. It was found that the more familiar
the rater is with the job being evaluated, the higher
his rating is likely to be. This effect was observed
for five of the 14 job evaluation rating factors used:
Adaptability, Decision- Making, Managerial and
Supervisory, Menul Work, and Working Coodltions.
Methods are suggested for controlling the familiarity
effect in the Air Force job evaluation system. (Author)
Personnel Lab. . Wright Air Development Div. ,
Lackland AFB. Tex.
PREDICTION OF UNSUTTABILTTY DISCHARGES, by
Wayne E. Fisher, Joe H. Ward, Jr. and others.
Oa 60, 21p. 6 refs. WADD-TN-60-260.
Order from LCmi$2. 70. ph$4. 80 PB 153 852
393
An equation was Revised to provide recruiters with a
convenient devic«( for estimating the quality of a
prospective rccr^t from three predictors: age,
education, and apltitude score. This report describes
the development 9f the equation and illustrates its
effectiveness in flrediaing unsuitabiliiy discharges.
It provides a contenient dial computer for estimating
probability of un^uitafaility discharge. (Author)
Science Research Associates, Inc., Chicago, 111.
THE DEVELOPMENT OF COLLEGE ACHIEVEMENT
TESTS (FORMS 3 AND 4) FOR NAVY OFFICER
SELECTION BATTERY, by Jean Maier and Robert
ContraCT Nonr- 228 !((»). Apr 60.
19p. 1 ref. BuPe^s Technical Bulletin 60-3.
Order from LC rii$2. 40, ph$3. 30 PB 148 771
Two new Forms
of the Officer
Each of these
in four subject
matics, (c)
The new Forms
(If
Selea
Science
the acadiemic achievement section
ion Battery (OSB) were constructed.
Foi^ms (Forms 3 and 4) include sub-tests
natter areas: (a) English, (b) Mathe-
and (d) History and Social Studies,
irere to be comparable to Form 1 of
OSB, but improvements thought to
this section of th '.
Increase their ef iciency were made
Psychology
Arctic Aerome4ical Lab. , Ladd AFB, Alaska.
RELATIONSHIPS BETWEEN CERTAIN SCORES ON
THE MINNESOTA MULTIPHASIC PERSONAUTY IN-
VENTORY AND rrHE MINNESOTA PERSONAUTY
SCALE, by Eme|t L. McCollum. [1959] 2p.
Order from LC i^i$ 1.80. ph$ 1. 80 PB 153 322
I
The Minnesou Personality Scale morale scores and
the Minnesota Multiphasic Personality Inventory de-
pression scores Jaelded a correlation coefficient of
- .292, the Minn^ota PerscMiality Scale social adjust-
ment scores and the Minnesota Multiphasic Personal-
ity Inventory psythopathic deviate scores yielded a
correlation coefficient of - . 125, and the Minnesota
Personality Scal^
sota Multiphasic
scores yielded a
emotionality scores and the Minne-
Personality Inventory hypomanic
correlation coefficient of - .416.
Arctic Aeromeikical Lab. , Ladd AFB, Alaska.
TWO yrUDCES (pH TEMPERATURE AND MOTOR
ABILITY.' THE EFFECT OF TEMPERATURE ON
SERL\L-DISCRn^INATIVE RESPONSES. THE
EFFECT OF TIME AND TEMPERATURE ON
MOTOR ABILITY, by Frederick H. Rohles, Jr. [1952]
25p. 28ref8. PrfcJ no. 22-0601-0002, rept. no. 1.
Order from LC riii$2.70, ph$4 80 PB 153 321
For the adjustment period of thirty minutes, the best
performance in i^srms of speed and errors was ob-
tained by the grctJp which was retested at 60°. The
many variables ♦hich have to be considered in this
problem are: (1) temperature; (2) humidity; (3) air
movement --wind (4) exposure time; (5) degree and
type of activity; 16) clothing; (7) body temperature- -
both skin and reial; (8) vasomotor respcxises; (9)
basal metabolic rate; (10) diet; and (11) acclimatizatloi
and adaptation. These factors continually interact to
determine the heat balance of the organism.
Bryn Mawr Coll. , Pa.
BODY SPACE: TACTILE -KINESTHETIC SCHEMA,
by Robert S. Davldon. Technical note no. 1 on Con-
tract AF 46(638)726. 30 Sep 60, lip. 6 refs. AFOSR-
TN-60-1355.
Order from LC mi$2. 40, phJ3. 30 PB 153 424
The first of a series of psychophysical studies to de-
fine taaile -kinesthetic spatial relationships within
and around the body for normal subjects. The sub-
jects judged when two successive points touched on
one arm were phenomenally as far apart as those of
a standard on the other palm or on different pans o*
the arm. Non-linear relationships were indicated. A
change in position of the arm affected perceived dis-
tance. (Author)
Educational Testing Service. Princeton, N. J.
THE NEGATIVE HYPERGEOMETRIC DISTRIBUTION
WITH PRACTICAL APPLICATION TO MENTAL
TEST SCORES, by Frederick M. Lord. Rept. on Coo-
tract Nonr -2752(00). Apr 60, 22p. 11 refs.
AD- 237 968.
Order from LC mi$2. 70. ph$4 80 PB 148 018
A rarely mentioned distribution, negative hypergeo-
metric (H), is found from theoretical consideration to
be appropriate in cases for fitting observed distribu-
tions of test scores. Only the mean and variance of the
observed distribution are used for fitting, even though
the distribution be highly skewed. Six numerical ex-
amples fitting H to actual mental test data are pre-
sented for illustrative purposes. Properties of H are
outlined both from a theoretical and from a practical
viewpoint, with the hope of facilitating the general use
of this distribution. (Author)
Harvard Graduate School of Business Administration,
[Cambridge, Mass.]
THE EFFECTS OF AUDIENCES ON COMMUNICA-
TORS, by Raymond A. Bauer and Ithiel de Sola Pool.
Final rept. on Contraa AF 49(638)486. Sep 60, 146p.
AFOSR TR-60-129. _
Order from LC mi$7.20. ph$22.80 PB 153 287
This report deals primarily with various problems and
ideas suggested by, or related to. the "audience effea'
findings of the Zimmerman-Bauer experiment. The
personality questions and techniques for discovering
communicators' reference groups which had been
developed in the preliminary exploratory work were
tested in pilot studies conduaed at Wellesley in the
fall of 1958, and the spring of 1959. The personality
and reference group questionnaires, which were devel-
oped as a result of the pilot studies, were done in
preparation for a full-scale experiment on the inter-
personal variability in audience effect. This study w«i
an attempt to replicate the Zimmerman-Bauer finding
("audience effea") and to account for individual differ-
ences in memory by correlating degree of audience
effect with three factors: own attitude toward the
394
iscue, attitude of one's reference groups, and several
personality variables. In general, the results were
complex, and confusing. Although many of the studies
of the audience effect had found that communicators
attempted to "please" an audience, the theoretical
position outlined by Bauer had anticipated the possi-
bility that some communicators might oat want to
please an audience, and hence would remember more
d the unpleasant than pleasant facts. In order to test
this proposition, a full-scale experiment was con-
duaed at the Harvard Business School in spring 1960.
The findings of this experiment were positive. Degree
of "audience effect" was found to be related to the
subject's own statement as to how far one should go
toward "pleasing" a client. Studies are also reported
which represent attempts to: (1) investigate the effect
of professional training and experience in journaUsm
on the degree of "audience effect" shown; and (2)
explore the audience effea on creativity of writers.
(Author)
Human Factors Research, Inc. , Los Angeles, Calif.
AN EXPLORATORY STUDY OF THE CORRELATES
OF VIGILANCE PERFORMANCE, by James J.
McGrath, Albert Harabedian, and Donald N. Buckner.
Technical rept. no. 4 on Human Factor Problems in
Anti-Submarine Warfare, Contract Nonr -2649(00).
Feb 60. 59p. 16 refs. AD-234 087.
Onler from LC mi$3. 60, ph$9. 30 PB 153 126
Effort was directed toward ascertaining the types of
behavioral measures that would be promising predic-
tors of vigilance performance. Tests measuring cleri-
cal abilities appeared to be promising predictors of
the amount of decrement in detection performance suf-
fered by individuals during watch, but did not appear
to predict the overall performance levels. Perform-
ance on an auditory vigilance usk was more predict -
aUe from psychological test scores than performance
on a visual vigilance task. Qualiutive differences in
vigilance performance (sleeping vs. not sleeping on
watch) were more predictable from psychological test
scores than quantiutive differences in vigilance per-
formance. There was a significant correlation be-
tween brightness discrimination threshold and per-
formance on a visual vigilance task. Subjects detected
fewer signals when they reported feelings of tiredness
than when they reported feeling rested. Feelings of
restlessness increased from week to week during the
course of the experiment. The percenUge of signals
deteaed on watch was positively related to the amount
of sleep the subject obtained the ni^t before watch-
standing. The subjeas' general attitudes tofward the
experiment were not related to their performances on
watch. But, there was a significant relationship be-
tween task preference (auditory vs. visual) and task
performance such that performance was better on the
preferred usk.
Human Factors Research. Inc., Los Angeles, Calif.
THE PROBABILITY OF SIGNAL DETECTION IN A
VIGILANCE TASK AS A FUNCTION OF INTERSIG-
NAL INTERVAL, by Albert Harabedian, James J.
McGrath and Donald N. Buckner. Technical rept. no. 3
on Human Faacn- Problems in Anti-Submarine War-
fare, Contraa Nonr -2649(00). Feb 60. 35p. 20 refs.
AD-234 086.
Order from LC mi$3.00, ph$6.30 PB 153 141
Fifty-four students at the U. S. Fleet Sonar School,
San Diego, stood 2-1 hr watches a day, 4 days a wk,
for 4 wk. Half of the watches were on a visual and half
were on an auditory deteaion task. The subjeas' task
was to detect small intensity changes (signals) in an
intermittent light or tone, these changes occurring at
varying time intervals. Two signal rates were used, a
mean of 6 and of 30 signals per hr . Each subject stood
10 low signal rate watches and 4 hig^ signal rate
watches for each sensory mode. In this study, sensory
mode of signal presentation was ignored, but iniersig-
nal interval as the independent variable was treatec^
separately for the 2 signal rates. The intersignal /
interval was identified in 3 ways: the amount of time
elapsed since (I) the presenution of the previous sig-
nal, regardless of whether that signal was detected
(occurrence of the previous signal as the referent); (2)
the presentation of the last signal that was detected
(deteaion of the previous signal as the referent); and
(3) the presentation of the last signal that was missed
(missing the previous signal as the referent). (Author)
Illinois U., Uri>an.
SOQAL ADJUSTMENT AND INTERPERSONAL PER-
CEPTION, by Warren Smith, rev. by J. McV. Hunt.
Separate technical rept. no. 1 on Interpersonal Per-
ception and Interpersonal Relationships in Therapeutic
Counseling, Contract Nonr- 1834(11). 1 Feb 60, 85p.
125 refs.
Order from LC miM.80, phjl3.80 PB 153 168
This study was undertaken to investigate (1) whether
socially adjusted persons assume greater similarity
than do the socially maladjusted, (2) whether this
greater assumption of similarity is general and occurs
for a variety of other "persons ," or (3) whether the
degree of assumed similarity is a product of the de-
gree to which the judge accepts and feels warmth to-
ward the person judged. (Author)
Institute for Applied Experimental Psychology, Tufts
U. , Medford, Mass.
HEAD AND EYE TRACKING IN RESPONSE TO VE-
LOCITY AND ACCELERATION INPUTS, by Philip B.
Sampson, Edwin H. EDdn and others. Final rept. on
Contraa Nonr-494(l6). Apr 60. 52p. 21 refs.
AD- 237 445.
Order from LC mi$3. 60. ph$9. 30 PB 147 533
A study was conduaed to find out how well visual
tracking could take place when both the head and eyes
were free to follow moving targets and to discuss the
relevance of the findings to the notion of using the eye
as a control mechanism. The target used in this ex-
periment swung horizontally about the subjea at three
different velocities (30, 60, and 90P/sec) and three
accelerations (5. 20. and 45°/8ec. 2). The tracking \
error record obtained indicated that the eye was able
to track the urgets within the same tolerances re -
parted for eye tracking when the head was fixed. In
addition there was the suggestion that by permitting
both head and eye movements, higher velocities could
be tracked than by the eyes alone. A reasonably con-
stant head lead angle was found for the constant veloc-
ity inputs which varied with the magnitude of the input.
Various Implications of this finding were discussed.
An elearlc circuit analog was developed for part of
39S
and used to predla head and eye output in
to acceleration Inputs, using constants de-
rived from the vieloclty input data. The agreement be-
tween the obtain^ and tl^e prediaed function appeared
premising. (Author)
Author)
.
Mississippi SoUhern Coll. , Hattiesburg.
RESEARCH ON PSYCHOLOGICAL PARAMETERS OF
SOUND, by Robert W. Peters. Rept. on Contract
AF 33(616)3644 Feb 60, 65p. 83 refs. WADD Tech-
nical rept. 60-2K9; AD- 240 814.
Order from ar3$ 1.75 PB 171 403
Experlmenul approaches to the determination of
psychological parameters for complex sounds are dis-
cussed and relerant studies are summarized. The re-
sults o* a series of experiments which were conducted
treating the problem al parameters for complex sounds
are included in this report. The studies involved
language of auditory experience, scaling of auditory
stimulus sets on equal -interval scales, paired-com-
psrlsoBS scaling, scaling by direct magnitude estima-
tions, observer [generated scales, multidimensional
scaling of groupiB of sounds, and changes in auditory
perception under constant stimulation. The results of
the various studies indicated that the most promising
approach for the study of parameters of complex
sounds was the Multidimensional scaling model. In a
pure tone study this scaling model isolated the ex-
pected dimensions, {Mtch and loudness. In the scaling
of complex sounds, for several stimulus sets evalu-
ated, between three and six dintensions appeared to
emerge. (Authopr)
Psychological ^b. , U of Southern California
[Loe Angeles]
THE EVALUATION OF SELECTED INTELLECTUAL
FACTORS BY qREATIVE RESEARCH SCIENTISTS,
by Myron S. Alltn, J. P. Guilford, and P. R. Merri-
field. Rept. no.| 25 on Studies of Aptitudes at High-
Level Personnelt Contract Nonr-228<20) Apr 60,
4 refs. AD- 237 755.
Order from LChii$2. 40. ph$3. 30 PB 148 007
A new technique was devised for making a preliminary
survey erf the reilative importance of various intellec-
tual factors for creative research scientists as the
seientists themselves view those faaors. Twenty-
eight of the 46 kjiowti factors were selected by the in-
vestigators, eUtninating those thought to be of linle
importance or rplevance. A commonly worded defini-
tion and an exai^ple of a mental aaivity thought to in-
volve the factor were written fcr each faaor. These
28 factOTS were]rated by 35 well-recognized scientists
and engineers ipd by 50 non- scientists, as well as by
other special jqxxjps. In general, the factors were
rated in the same rank order by the two major groups,
with a correlatipn of .87. Differences in ranks for
some of the fact^s were marked only for a few factors
and for special ^oups. As a group, divergent-
production faacrs were not rated as high as expeaed
in either major group but soma of them were ranked
higher by the n<»i- scientist group. The scientists
rated factors in the product category of transforma-
tions highest, pirticularly the redefinition factors,
which are also in the convergent -production category.
It was concluded that the transformation factors de-
serve recogniti^ as potential contributors to creative
work. (Author)
Psychological Lab. , U. of Southern California
[Los Angeles]
THE STRUCTURE OF INTELLECT MODEL: ITS
USES AND IMPUCATIONS, by J. P. GuiUord and
P. R. Merrlfleld. Rept. no. 24 on Studies o< Aptitudes
of High-Level Personnel. Contract Nonr-228(20), con-
tinuation of Contraa N6onr- 238(10). Apr 60, 27p.
40 refs. AD- 237 754.
Order from LC mi$2. 70, ph$4. 80 PB 148 006
A resume is presented of the steps by which the con-
ception at the structure of intellea developed. More
rigorous definitions are presented for the new concepu
that arose in connection with the model. The model cf
the structure of intellect is now the source at ideas
for general psychological theory, and factorial inves-
tigations are directed toward testing whether unknowt
unique abilities that are prediaed by the model do, in
fact, exist as distinguishable unities. The theories of
learning and of thinking and problem solving, as
generated by the model, are discussed.
Rochester U. , N. Y.
SOME STUDIES OF THE INFLUENCE OF FILMS
ON MOOD AND ATTITUDE, by Vincent NowUs.
Technical rept. no. 7 on Research Program on Mood
and Attitude Change, Contract Nonr-668(l2).
6 Jan 60. I6p. 24 refs. AD- 23 1 247. •
Order from LC ml$2. 40. ph$3. 30 PB 152 881
A series of studies were reviewed in which documen-
ury films and similar materials were used to produce
chains in mood and in attitude. A theoretical discua
sion of mood was presented together with the results
of 7 factor analytic studies of the major dimensions of
verbal report of mood. A short Mood Adjective Check
list was found to be a useful instniment for quantify-
ing chains in mood as induced by films and other ex-
perimental operations. Concotniunt with changes in
mood were congruent changes ia- (1) readiness to
accept a reasonable recommendation which is part of
a mood-inducing communication, (2) attitude toward
a urget presented in an anger -arousing message,
(3) the desirability of consumer products, the evalua-
tion of certain affective goals, and the perceived
utility of the consumer products in achieving these
goals; (4) self -perception and person perception; and
(5) the subjective estinwile of the probability of un-
certain future events. These results cannot be ex-
plained on the bssis of mood theory in its present
status. With respect to the topic of this symposium,
they do suggest that this kind of communication can
have tremendous influences on the momentary emo-
tional and cognitive sute of the member of the audi-
ence, an influence which may be far beyond the intent
of the producer at the film. (Author)
BIOLOGICAL SCIENCES
Army Chemical Research and Development Lab«. ,
Army Chemical Center, Md.
THE EFFECT OF BORON HYDRIDES ON ISOLATED
CAT PAPILLARY MUSCLE, by Edmund F. Murtha.
Sep 60, 9p. 1 ref. CRDLR 3034; AD-245 202.
Order from LC mi$l. 80. ph$l. 80 PB 153 174
3%
TTie cardiovascular system is affected during intoxi-
cation with the boron hydride fuels of the HEF-3 and
HlCil-3 classes. This investigation was conducted to
determine whether or not these compounds can cause
a direct cardlotoxic effect. It was found that: (1) the
boron hydride fuels of the HEF-3 and HiCal-3 classes
can cause marked weakening of the isolated papillary
muscle of the cat; and (2) the direct cardlotoxic effea
of these compounds may be responsible for some of
the cardiovascular alterations which occur in intact
cats and dogs during boron hydride intoxication.
(Author)
Copenhagen U. (Denmark).
INFLUENCE OF THE CAUDATE NUCLEUS IN THE
MOTOR SPHERE (I); ANALYSIS OF THE UNTT
ACTIVrTY OF THE CAUDATE NUCLEUS (II); THE
ROLE OF THE CAUDATE NUCLEUS IN CONDI-
TIONED AVOIDANCE BEHAVIOR IN CATS (III), by
A. Mosfeldt Laursen. Final technical rept. for
1 Nov 59-31 Oa 60 on Contract DA 91-591-EUC-1314.
[1960] 12p. 14 refs.
Order from LC mi$ 2.40. ph$ 3. 30 PB 153 468
Michigan State [U.] East Lansing.
EDIBLE PLANT FIELD WORK FOR SUMMER OF
1954. by Quentin Jones . Dec 56. 31p. Technical note
AAL-TN-56-18.
Order from LC mi$3. 00, ph(6. 30 PB 153 524
The area covered was confined to the interior of
Alaska with panicular emphasis on the highlands and
active flood plains .
Anatomy and Ph)r$iolog/
Aerospace Medical Div. , Wright Air Development
DIv. . Wright -Patterson AFB. Ohio.
STUDIES ON THE ENDOLYMPHATIC DC POTEN-
TIAL OF THE GUINEA PIG'S COCHLEA, by
Edward A. Rice and Edward W. Shinabarger. Rept.
00 Acoustic Energy Control. Aug 60. I2p. 9 refs.
WADD Technical rept. 60-162.
Order from OTS $0. 50 PB 171 392
The effect of loud sound on the endolymphatic DC po-
tential was stixlled in both normal and hypoxic animals.
When the integrity of the cochlea wall was maintained,
the endolymphatic DC potential decreased 5 millivolts
with the onset of sound (1000 cps at below 140 db) and
recovered immediately when the sound was termi-
nated. At intensities of 140 db and above, the DC po-
tential irreversibly decreased. The effect of sound on
the DC potential survived the life span of the post
mortem microphonics. The positive DC potential re-
turned on terminating hypoxia. Oxygen deprivation re-
sulted in the DC potential decreasing before the
microphonics. The possible significance of these
findings to the physiology of hearing is discussed.
(Author)
Arctic' Aeromedical Lab. , Ladd AFB. Alaska.
CARDIOVASCULAR RESPONSE TO HYPOTHERMIA.
EFFECT OF COLD ACCLIMATIZATIC»4. by Benjamin
G. Covino and William R. Beavers. Jan 58, 17p.
12 refs. Technical rept. 57-27.
Order from LC ml$2.40, ph$3.30 PB 153 369
The process of cold acclimatization has been the basis
for numerous physiological investigations. Information
gathered from such studies is of obvious applicability
to individuals operating in arctic regions. The present
program was initiated in order to evaluate the effect of
prolonged cold exposure on the cardiac response to
acute severe hypothermia. The greatest hazard in pro-
found hypothermia is the occurrence of ventricular
fibrillation. In nonacclimatized control animals
rendered hypothermic, the incidence of ventricular
fibrillation was 9656- Following 1 to 4 weeks of con-
tinuous exposure to an environmental temperature of
from (f> to -40° C , the frequency of this fatal cardiac
abnormality was reduced to 9%. This beneficial effect
of cold acclimatization was not ascribable to a direct
effect on the hypothermic myocardium, since no cUf-
ference in ventricular fibrillary threshold was ob-
served between acclimatized and nonacclimatized
animals. Thus, extrinsic cardiac factors are believed
res[»nsible for the antlfibrlllary action of cold
acclimatization. (Author)
Arctic Aeromedica I Lab. . Ladd AFB, Alaska.
THE EFFECT OF PROLONGED COLD EXPOSURE ON
THE IN VTTRO RESPIRATIC^I AND ANAEROBIC
GLYCOLYSIS OF RAT UVER, by John P. Hannon.
June 57. 17p. 12 refs. Technical note AAL-TN-57-4.
Order from LC mi$2. 40. ph$3. 30 PB 153 545
Liver slices were prepared from rats that had been ex-
posed to cold (5 - IOC. ) for intervals of 2, 4, 6 or
9 weeks, and assays were made for respiratory rate
and the rate of anaerobic glycolysis. The results of the
respiration experiments indicated the first 4 weeks'
cold exposure was associated with increasing QO2
values, whereas exposure longer than 4 weeks was
associated with QO2 values that returned toward the
control value. The results indicated further that the
exact nature of the substances being metabolized in the
conventional tissue slice experiment was unknown. The
results of the anaerobic experiments indicated the rate
erf anaerobic glycolysis decreased progressively as the
duration of cold exposyae was increased. (Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
THE METABOLIC AND BODY TEMPERATURE
RESPONSE GP MEN TO AN ACUTE COLD STRESS
BEFORE AND FOLLOWING AN ARCTIC BIVOUAC,
by Donald W. *ennie and Thomas Adams. July 58, 30p.
36 refs. Technical rept. 57-37.
Order from LC ml$2.70, ph|4.80 PB 153 373
The nietabollsm and body temperatures of six subjects
were recorded during a standardized cold test before
and following a 24 -day arctic winter bivouac in order
to determine if any changes, which might be ascribed
to living in a cold environment, took place in their
thermoregulatory response. TTie body heat debt, total
body heat loss, tissue and environmental insulation
397
and blood flow to ( «rtain skin areas were estimated
from these data. Basal metabolism and thyroid func-
tion using l'^^ uptake were also measured in each sub-
ject before and following the bivouac. No change in
basal metabolism of I^^ uptake was noted in any sub-
ject following the field exposure. There were signifi-
cantly higher skin temperatures of the arms, hands,
lower legs, and fqet at the completion of the post -
bivouac test when icompared with the pre-bivouac
values. The temperatures of other skin areas and the
rectal temperature were identical from one lest period
to another. The warmer extremity temperatures indi-
cate a relatively Reduced vascular constriction in
response to cold iti the limbs of the acclimatized sub-
jects. Acclimatization to the degree of chronic cold
to which these meti were exposed was localized to the
beat distribution (Lnction of the peripheral
vasculature. (Author)
AraicAeromedjcalUb. , LaddAFB, Alaska.
HYPOTHERMIA, by Raymond J. Hock and Benjamin G.
Covino. Dec 56, I5p. Technical note AAL-TN-56-39.
Order from LC rT^$2. 40, ph$3. 30 PB 153 544
What is meant by jhypothermia? What is the reason
behind the increa^ scientific interest in this condi-
lion? How can hypothermia benefit us? These are
some of the questjons which this paper attempts to
answer.
ArCTic Aerome4cal Lab. . Ladd AFB, Alaska.
THYROID ACTIVITY IN MEN EXPOSED TO COLD,
by Kaare Rodahl 4nd Gisle Bang. Oct 57, 86p. 18 refs.
Technical repi. 57-36.
Order from LC nii$4.80, ph$l3.80 PB 153 372
An assessmertt his been made of the role of the thyroid
in man during thfl cold exposure usually encountered
during normal arttic living or operations and during
simulated emergency survival in the cold. The study
Included careful Clinical examination, estimates of
dietary iodine intjikes, environmental exposure, and
analyses of PBI a^ serum cholesterol. There appears
to be no real difference In thyroid uptake or urinary
elimination of 1 1 31, in the PBI ^ 31^ or in the conversion
ratio; and that th^re was no consistent seasonal differ-
ence in the PBI or* any significant difference between
the natives and the Whites. There was no real evi-
dence of any greater thyroid stimulation in infantrymen
engaged in extensive outdoor activities than in airmen
engaged in lndoo4 activities during the winter; nor was
there any eviden<ie of increased thyroid stimulation in
the Whites at the end of a 4-week severe cold exposure
The thyroid does|not play any significant role in human
acclimatization t^ the araic environment when the
cold stress is no^greater than what is normally en-
countered by soltjiers engaged in usual araic service
or by Alaskan Eilmos or Indians in the course of
their normal life or aalvities. (Author)
I
Armed Forces-WRC Comminee on Hearing and
Bio-Acoustics [Washington, D. C ]
THE EVALUATION OF AUDIOMETERS, ed. by Robert
W. Benson. Rept, on Contract Nonr- 2300(06). Mar 60,
54p. AD-234 693.
Order from LC n Li$3. 60, ph$9.
Contents:
Definitions and background information
Classes and types of audiometei-s
American standard specification for audiometers
Importance of accurate frequency calibration for
monitoring audiometry
Monitoring the accuracy of calibration of
audiometers
The listing of aildiometers by the AAOO
Pure tone audiometry is basic
Accessory equipment for special tests
Results of the working group review of available
audiometers
Shortcomings of audiometers
Characteristics at commercially available
audiometers
Index to individual audiometers
Index to group audiomete rs
Army Ordnance Human Engineering Labs. , Aberdeen
Proving Ground, Md.
THE EFFECTS OF EIGHT HOURS CONFINEMENT
IN MOBILE ARMORED PERSONNEL CARRIERS ON
SELECTED COMBAT RELEVANT SKILLS: STUDY 11.
by Samuel A. Hicks, Jimmy P. Scott, and Claude D.
Patton. Nov 60, 27p. 4 refs. Technical memo. 17-60.
Order from LC ml$2. 70, ph$4. 80 PB 153 469
Fony enlisted men were tested both before and after
confinement on tests designed to measure stamina,
eye -arm coordination, gross motor coordination, arm
steadiness, and rifle accuracy. The eight-hour con-
finement period resulted in losses in three areas. The
losses were statistically significant in two areas. Rec-
ommendations are Included for future research.
(Author) (See also PB 147 162)
Biomedical Lab. , Wright Air Development Div. ,
Wright-Patterson AFB. Ohio.
GROSS AND MICROCIRCULATORY EFFECTS OF
TILTING AND ACCELERATION ON THE GOLDEN
HAMSTTER, by Paul L. Yudkofsky. Rept. on Biophyslci
of Flight. Sep 60, 81p. 110 refs. WADD Technical
rept. 60-373.
Order from OTS $2. 25 PB 171 367
The heart rate, respiratory rate, blood pressure,
electrocardiogram, organ displacements, and micro-
circulation of the golden hamster were recorded and
correlated during a wide range of gravitational stress,
i.e. , from 1 to 60 positive g. The effects of various
anesthetics and hemorrhage on the observed responset
were determined. Lastly, the cardiovascular re-
sponses of the hamster to occlusion of the carotid
arteries were interpreting and necropsy examinationi
were performed to aid lit interpreting the recorded
physiologic data. Tilting from the horizontal to head-
up position elicited no pronounced physiologic re-
sponses in the test animal. The increased forces en-
countered during centrifugation elicit pronounced
effects which appear to be primarily compensated for
by increased heart rate. The microcirculation of the
hamster cheek pouch did not appear to actively enter
into the reactions to positive acceleration. Also, tl\e
cause of death at various magnitudes of acceleration
Is discussed. (Author)
30
PB 153 778
398
Callfamia U. , Berkeley.
SURVIVAL OF C-57 MICE AND SQUIRREL
MONKEYS IN HIGH AND LOW PRESSURES OF
OXYGEN, by S F. Cook and H. F. Leon. Rept. on
Contract AF 29(600)2017. Oct 60. 38p. 21 refs.
AFMDC-TR-60-21. _
Order from UC mi$3. 00, ph$6. 30 PB 153 409
•nie critical oxygen tension for C-57 mice lies be-
tween 624 and 528 mm Hg O2; for squirrel monkeys be-
tween 600 and 548 mm Hg O2. However, at 624 mm
Hg O2 monkeys appear nwre resistant than C-57 mice.
Widi low oxygen pressures the mice are slightly more
resistant. The lethal limit for monkeys Is near 94 mm
Hg Oo whereas mice can tolerate moderately well
pressures of oxygen as low as 84 mm Hg. Two differ -
oit toxic effects of high oxygen pressures are distin-
guished: (1) acute, referable to lung damage, and
(2) chronic, referable perhaps to disturbance of cell
enzyme systems. (Author)
Michael Reese Hospital, Chicago, 111.
THE REGULATION OF THE DISTRIBUTION OF THE
CARDIAC OUTPUT. I. BLOOD PRESSURE AND
BLOOD FLOW REGULATING MECHANISMS ELIC-
ITED BY INTRACRANIAL COMPRESSION. II. STUD-
IES ON CLINICAL MEASURES OF BLOOD FLOW
TO THE EXTREMITIES, by Simon Rodbard and Louis
N. Katz. Mar 58, 38p. 14 refs. AAL Technical
rept. 57-8.
Order from LC ml$3.00, ph$6.30 PB 153 365
Certain aspeas of blood pressure and blood flow regu-
lation were studied in animal experiments, utilizing
the stimulus of intracranial compression. These ex-
« periments elucidate mechanisms which act in concert
to provide a quantiutive blood pressure response to a
neurogenically determined pressure regjjlating stimu-
lus. They provide the basis for a hypothesis that a
pressure sensitive receptor is present inside the
cranial cavity. The need for a simple indirect method
for the estimation of the blood flow through extrem-
ities is apparent in the limitations erf present methods.
Two of the cardiovascular phenomena of the extrem-
ities, the oscillometric pulsations and the arterial
■ounds, were studied to determine if these might be
used to estimate the peripheral vascular efficiency.
Arterial sounds can be used to appraisd extremity
blood flow. The sounds heard during routine blood
pressure estimation are diminished when blood flow is
minimal, as occurs in the extremities of the aged or
after the application of a tourniquet. Increased blood
flow leads to the production of loud sounds. The
cUnical value of attention to the intensities of these
sounds is demonstrated.
North Dakota U. [Grand Forks].
- EFFECT OF COLD ON RENAL FUNCTION, by
William C. Nungesser. Rept. on Contract
AF 18(600)1136. Dec 56, 17p. 4 refs. Technical note
AAL-TN-56-37.
Order from LC mi$2. 40, ph$3. 30 PB 153 542
School of Aviation Medicine. Brooks AFB, Tex.
FLOW RATE RESPONSES OF THE HUMAN PAROTID
GLAND, by Ira L. Shannon and John R. Prigmore.
Sep 60. 14p. 39 refs. Rept. 60-85.
Order from LC ml$2. 40. ph$3. 30 PB 153 302
The present series of experiments was designed to
determine the parotid gland flow rate response to
certain stimulating agents, and to other methods of
exogenous elicitation. (Author)
School of Aviation Medicine, Brooks AFB, Tex.
SECONDARY OCULAR NYSTAGMUS AS A FUNC-
TION OF INTENSITY AND DURATION OF ACCEL-
ERATION, by George T. Hauty and G. R. Wendt (U.
of Rochester). Rept. on Contract N6ori- 126, TO. 1.
Apr 60, I2p. 34 refs. Rept. no. 60-29; AD-241 862.
Order from LC mi$2. 40, ph$3. 30 PB 147 778
Neither intensity nor duration o< stimulation was found
to be consistently related to the intensity and duration
of secondary nystagmus. Yet, total secondary nystag-
mic output was directly related to the prockict d in-
tensity and duration of stimulation and, moreover,
was roughly one -half that of the total joutput of the
preceding primary phase of nystagmus. These re-
sults. Interpreted in the light of existing knowledge,
suggest that the response characteristics of secondary
nystagmus are determined by activity occurring in the
vestibular nuclei complex. (Author)
/
University of Southern California . School of
Medicine , Los Angeles .
EFFECT OF CHANGES IN ENVIRONMENTAL TEM-
PERATURE ON STOMACH EMPTYING IN RATS, by
E. Geiger and J. J. Pinsky. Rept. on Contract
AF 18(600)549. [1956] Up. 8 refs. Technical note
AAL-TN-56-5.
Order from LC mi^2.40. ph$3.30 PB 153 511
Transfer of rats from room (22° C .) to either low
(3° C.) or high (37° C.) environmental temperature
immediately following a protein meal delays emptyii^
of the stomach. After adaptation to the changed sur-
rounding temperature, the stomach emptying was
found to be, again, similar to that observed at room
temperature. (Author)
Washington U . , Seattle . School of Medicine .
SMALL SAMPLE VOLUME INFRA-RED CARBON
DIOXIDE ANALYZER, by Allan C. Young and
W. A. Robinson. Rept. on Contract AF 33(038)422.
Dec 54, lOp. 4 refs. AAL Proj . no. 7-7951.
rept . no . 1 .
Order from LC mi$l .80, ph$l .80 PB 153 335
A compact CO2 analyzer using an interrupted infra-
red beam is described. The sample chamber has a
volume of 1 cc . Ninety per cent response requires a
time of 1/25 sec and a volume flow of 1 cc. (Author)
Wisconsin U. , Madison.
BLOOD GROUPS OF THE ANAQTUAVIK ESKIMOS.
ALASKA, by W. S. Laughlin. June 57, 20p. IJ refs.
AALTechnicaLrept. 57-5. ^
Order from LC mi$2. 40, ph»3. 30 PB 153 347
The presence of blood type B has been established in
the interior Eskimos of Alaska. The closest Eskimos
for whom data exists. Point Barrow, Nome, Bethel,
and Mackenzie River, all have varying frequencies of
399
B. The Indians d Alaska and the Mackenzie River
either lack B, or h$ve an extremely small amount,
moet likely attributable to admixture with Whites or
Eskimoe. The Anaqtuavik sample contains many re-
lated people; only aix persons are not known to be re-
lated to each other. The extent of relationship has not
been provided for (Xher groups with whom they may be
compared. The Anaqtuavik Eskimos fit within the
framework ol the ^festern Eskimos who have a rela-
tively coodauoiM distribution and high population den-
sity in cooupKlaoni with the central Eskimos. That
they retain blood g|:oup B and a high proportion of A is
contributing evideiKe to the fact that they have main-
tained direct and indirect contaas with other western
Eskimos. (Author
Biochemistry
Henry Ford Hospital, Detroit, Mich.
[CTUDES ON SUOaNlC DEHYDROGENASE] by Edna
B. Kearney and Tl*xnas P. Singer. Annual progress
rept. on Contraa fJonr- 1656(00). 10 Feb 60. 12p.
45 refs. AD- 232 663.
OrderfromLCmi^2.40, ph$3.30 PB 153 164
Contents:
Prosthetic group of mammalian succinic dehydrogenase
Purification and cctisiltution of choline dehydrogenase
Funaional interrelations of the respiratory chain in
liver mitochondria
Permeability factots in the assay of respiratory
enzymes
Recent studies on
On the multiplicity
luccinic dehydrogenase
(rf lactic dehydrogenases in yeast
Indiana U. Schood of Medicine. Indianapolis.
A SIMPLE BEAMiSPUTTER FOR THE ZEISS
FUNDUS CAMERA, by John B. Hickam. Sep 60, 4p.
AFSAM 60-87.
Order from LC m$1.80, phjl
80
PB 153 303
In the photographit method now being used to estimate
percent oxygen saturation of retinal venous blood, the
density ot the phonographic image of a retinal vein is
measured succesaively by red and by infrared light,
using first one filler and then the other. Greater con-
venience and accii^acy may be obtained by exposure
through red and iitfrared filters simultaneously; a
simple beam-splitter has been devised for this
purpose. (Author! i
Pittsburgh U. (Pal 1
A STUDY OF THt MECHANISM OF PHOTOSENSI-
TIZATION IN PHOTOSYNTHESIS, by Jerome L.
Rosenberg. Annuajl progress rept. for 1 Jan-31 Dec 59
on Contract Nonr^624<08). I Feb 60, lOp- I* refs.
AD- 232 419. ! ^, ^
Order from LC m^l. 80. ph$l. 80 PB 153 127
The fluorescence spectrum of chlorophyll in green
plants was observed. A monochromator, incorporated
Into a fluorescence apparatus, was tested by using it
to study interestiitg changes in the fluorescence of
alcoholic solutions of chlorophyll at low temperatures
and high concentrations. (Author)
Tufts (U. School ot Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contract AF 18(600)583. Dec 56, 7p. Tech-
nical note AAL-TN-56-20.
Order from LCmi$l. 80, ph$ 1.80 PB 153 526
Partial contents: Hepatic acetate metabolism.
Tufts [U. School of Medicine] Boston, Mass.
CONTINUING STUEXES ON THE METABOUSM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, 4p. Tech-
nical note AAL-TN-56-21.
Order from LCmi$l. 80. ph$ 1.80 PB 153 527
Partial contents: Hepatic acetate metabolism. Effect
of glucose on hepatic acetate metabolism.
Tufts [U. School of Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contract AF 18(600)583. Dec 56, 6p. Tech-
nical note AAL-TN-56-22.
Order from LCmi$l. 80. ph$ 1.80 PB 153 528
Partial contents: Lipogenesls and cholesterogenesis in
a liver homogenate system. Effect of pyruvate on
hepatic acetate metabolism.
Tufts [U. School of Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOUSM OF
FATTV ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contract AF 18(600)583. Dec 56, lOp. Tech-
nical note AAL-TN-56-23.
Order from LCmi$ 1.80, ph$ 1.80 PB 153 529
Partial contents: Lipogenesls and cholesterogenesis in
a liver homogenate system. Effect ot pyruvate on
hepatic acetate metabolism. Effect ot ketoglutarate on
acetate metabolism.
Tufts (U. School ot Medicine] Boston. Mass.
CONTINUING STUDIES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, 8p. Tech-
nical note AAL-TN-56-24.
Order from LCmi$ 1.80, ph$ 1.80 PB 153 530
Partial contents: Effect ot unlabeled acetate on hepatic
acetate- 1-cl* metaboUsm. Effeas ot ketoglutarate ob
acetate metaboUsm. Effea of NaCl on hepatic acetate
metabohsm. Effeas of glucose and pyruvate on
acetate metabolism. Effea of butyrate on acetate
metabolism. Upogenesis in Uver homogenate system.
400
-J4
Tirfts [U. School ot Medicine] Boston, Mass.
CONTINUING STUDIES Oti THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56. Up. Tech-
nical note AAL-TN-56-25.
Order from LC nii$2.40. ph$3.30 PB 153 531
Partial contents: Effea of pyruvate on hepatic acetate
njetabollsm. Effea of butyrate on acetate metabolism.
Effea c4 butyrate on glucose metabolism. Experi-
ments with liver homogenates.
Tufts fU. School of Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOUSM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, I2p. Tech-
nical note AAL-TN-56-26.
Order from LC nu$2. 40. ph$3. 30 PB 153 532
Partial contents: Effea ot short chain fatty acids on
hepatic acetate metabolism. Effea of Krebs cycle
intermediates on hepatic acetate metabolism.
Tufts [U. School of Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOUSM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, 12p. Tech-
nical note AAL-TN-56-27.
Order from LC ml$2. 40, ph$3. 30 PB 153 533
Partial contents: Effeas of Krebs cycle intermediates
on hepatic acetate metabolism. Effects of short chain
fatty acids on hepatic acetate metabolism. Studies on
the whole rat exposed to cold.
Tufts [U. School of Medicine] Boston, Mass.
CONTINUING STUMES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56. Up. Tech-
nical note AAL-TN-56-28.
Order from LC mi$2. 40. ph$3. 30 PB 153 534
Partial contents: Effea of short chain fany acids on
hepatic acetate meubolism. Comparison ot the
hepatic metabolism of butyrate and acetate. Acetate
metabolism in liver slices from rats exposed to
chronic cold.
Tufts (U. School of Medicine] Bdston, Mass.
CXKUNUING STUDIES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56. Up. Tech-
nical note AAL-TN-56-29.
Order from LCmi$2. 40, ph$3. 30 PB 153 535
hrtial contents: Inhibition ot hepatic metabolism by
abort chain fatty adds. Effea of butyrate and acetate
on propionate and glucose metabolism. Effect of
propionate and butyrate on succinate oxidation.
Metabolism in Uver prepared from cold-fasted rats. '
Studies on the whole rat exposed to cold.
Tufts [U. School ot Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOUSM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, 9p. Tech-
nical note AAL-TN-56-30.
Order from LCnU$ 1. 80, ph$ 1.80 PB 153 536
Partial contents: Metabolism in liver slices prepared
from chronic cold-fasted rats. Metabolism in liver
from cold-fasted rats. Upogenesis in the whole rat.
Cold exposure and diabetes.
Tufts fU. School ot Medicine] Boston, Mass.
CONTINUING STUDIES ON THE METABOLISM OF
FATTY ACIDS AND RELATED SUBSTANCES IN
ANIMALS EXPOSED TO COLD, by David Rapport.
Rept. on Contraa AF 18(600)583. Dec 56, 18p. Tech-
nical note AAL-TN-56-31.
Order from LC mi$2. 40, ph$3. 30 PB 153 537
Partial contents: Fatty acid metabolism in liver slices
prepared from chronic cold-fasted rats. Carbohydrate
metabolism in liver from cold-fasted rats. Effea ot
propionate on palmitate oxidation. Inhibition ot
hepatic glucose meubolism by short chain fatty acids.
Comparison ot metabolic patterns of propionate and
succinate. Cold exposure and diabetes. Fasting and
blood sugar.
Tufts [U. School of Medicine] Boston, Mass.
EFFECT OF COLD EXPOSURE AND FASTING ON
HEPATIC ACETATE METABOUSM. by E. J. Masoro.
Arthur I. Cohen, and Sylvia S. Panagos. Rept. on
Contraa AF 18(600)583. Dec 56. 12p. 13 refs. Tech-
nical note AAL-TN-56-32.
Order from LC ml$2.40. ph$3. 30 PB 153 538
A detailed study of the relationship between hepatic
carbohydrate content and acetate oxidation was
undertaken. In the present investigation the carbohy-
drate content of the liver was drastically reduced bf
fasting rats both at 25^0. and 0*>C. It was found that
acetate oxidation is greatly depressed by the lowering
of the hepatic carbohydrate level.
Tufts [U. School ot Medicine] Boston, Mass.
EFFECT OF EXPOSURE TO COLD ON SOME
ASPECTS OF HEPATIC ACETATE UTILIZATION,
by E. J. Masoro, Arthur I. Cohen, and Sylvia S.
Panagos. Rept. on Contraa AF 41(657)145. Dec 56,
I8p. 22 refs. Technical note AAL-TN-56-33.
Order from LC mi$2. 40. ph$3. 30 PB 153 539
Respiration studies on surviving tissue slices have
indicated that liver, heart, kidney, and skeletal
muscle are involved in the increased metabolic rate
associated with exposure ot animals to cold environ-
mental temperatures. Therefore, a study of the
metabolism ot a labeled compound by surviving tissues
should present a more complete picture of changes in
intermediary metabolism occurring under this con-
dition. Using C^^-labeled acetate, the pattern ot
hepatic acetate metabolism in the cold- exposed anintal
was investigated.
4M
Tufts [U. 1 Schocfl of Medicine, Boston, Mass.
THE EFFECT Of PROLONGED COLD EXPOSURE
ON HEPATIC LIPOGENESIS, by E. J. Masoro,
J. M. Felts, and Sylvia S. Panagos. Rept. on Contraa
AF 18(600)583. Djec 56. lOp. 12 refs. Technical
note AAL-TN-56-
Order from LCni$ 1.80, ph$ 1.80 PB 153 541
i6-p6.
nji$l.
The present repoft extends studies of hepatic
lipogenesis to ratb that have lived in the cold success-
fully for several iionths - " cold-adapted" rats. Liver
slices from thesel'cold-adapied" rats also showed
depressed Upogeiiesis, but the surprising finding is
that this reduction in fatty acid synthesis is not the
result at a curtailed hepatic carbohydrate metabolism.
Tufts U. School of Medicine, Boston, Mass.
EFFECTS OF SHORT CHAIN FATTY ACIDS ON
HEPATIC ACETATE METABOLISM IN COLD EX-
POSURE AND FASTING, byE. J. Masoro and Sylvia S
Panagos. Mar 58] 9p. 12 refs. AAL Technical
rept. 57-6.
Order from LC nii$1.80, ph$1.80 PB 153 363
Butyrate, isobutyiate, propionate, caproate, and
acetoacetate failed to reverse the block in acetate- 1-
C'* oxidation fou^ in liver slices from rats fasted at
0 to 2° C. for 24 hours. It appears that the ability of
glucose and pyruvate to increase the acetate oxidation
activity at these ijiver slices is related to a specific
step in carbohydrate metabolism rather than solely to
the fact that carbohydrates are excellent sources of
energy. (Author)
Tufts U. School of Medicine, Boston, Mass.
THE REGULATION OF HEPATIC ACETYL METABO-
USM BY SHORT CHAIN FATTY ACIDS, by E. J.
Masoro, J. M. P^lts and others. May 58, 22p.
22 refs. AAL Technical rept. 57-7.
Order from LC n^$2.70, ph$4.80 PB 153 364
Propionate, isobutyrate. and caproate inhibited all
phases of acetatejl-C^* metabolism. Although
butyrate suppressed acetate oxidation, the evidence
indicates that but; Tate increases lipogenesis from
It is apparent that fatty acids can exert a
Ion acetyl metabolism. (Author)
acetate
regulatory action
Tufts U. School W Medicine, Boston, Mass.
THE ROLE OF CARBOHYDRATE METABOUSM IN
PROMOTING FATTY ACID OXIDATION, by E. J.
Masoro and J. M. Felts. Rept. on Contract
AF 41(657)145. ^ov 57, 18p. 18 refs. Technical
note AAL-TN-57-|36.
Order from LC m i$2. 40, ph$3. 30
PB 153 548
In the experimentb reported in the present communi-
cation, the effea of carbohydrates on the oxidation by
liver slices of vatious fatty acids has been studied.
The resulting evidence Indicates that, while carbohy-
drate metabolism appears to be necessary for an
optimal rate erf fatty acid oxidation, it apparently is
not a function of the "sparking" aaion of oxalacetate
or other Krebs cjicle intermediates.
Tufts fU. 1 School at Medicine, Boston, Mass.
STUDIES ON THE METABOLISM OF FATTY ACIDS
AND RELATED SUBSTANCES tN ANIMALS EX-
POSED TO COLD, by David Rapport. Rept. on Con-
tract AF 18(600)583. Dec 56, 12p. Technical note
AAL-TN-56-19. ■■'.
Order from LC mi$2.40, ph$3.30 ! PB 153 525
Partial contents: Phosphate vs. bicarbonate buffer.
Hepatic acetate metabolism by rats exposed to cold.
Washington U. , Seattle.
METABOUC ALTERATIONS IN RATS WITH ADAP-
TATION TO LOW ENVIRONMENTAL TEMPERA-
TURES, by Walter H. Cottle. Rept. on Contract
AF 18(600)1467. Nov 58, 99p. 162 refs. AAL Tech-
nical rept. 57-12.
Order from LC mi$5. 40. ph$15. 30 PB 153 366
The metabolic changes resulting from prolonged ex-
posure to low environmental temperatures have been
studied in male albino rats. Following the initial ex-
posure to cold (5° C. ), animals showed a gradual in-
crease in heat loss, oxygen consumption, and food in-
take for 2 to 3 weeks. Metabolism at 28° C. (MR280)
was increased 20% after 2 weeks at 5° C After 2
weeks at 5° C. , MR 28° of thyroid-deficient rats
(thyroid-ectomlzed and given 2. 5 microgm. thyroxine
per day) was also increased. Determinations were
made of the metabolic rate of muscle, liver, and
kidney in vitro. Metabolic rates of rats paralyzed with
curare were measured at 30° C The differences be-
tween metabolic rates of cold -adapted and nonadapted
rats measured under these conditions resembled those
observed when metabolic rates of intaa rats were
measured at 28°C. The ability of curarized rats to
maintain body temperature when exposed to cold was
tested. Cold-adapted rats were able to increase heat
produaion without an increase in muscular aaivity
(chemical regulation), and maintained rectal tempera-
ture at or near its initial level. The increase in
chemical regulation with cold adaptation accounts
for the reduction in muscular activity which has been
found in rats in the cold after adaptation. It would also
account for the ability of the cold-adapted animals to
increase heat production to the high levels necessary
to withstand severe cold stress. (Author)
General Biology
Arctic Aeromedlcal Lab. . Ladd AFB, Alaska.
HELMINTH PARASITES OF ALASKAN MUSKRATS,
by Tommy T. Dunagan. Dec 56, 8p. 17 refs. Tech-
nical note AAL-TN-56-16.
Order from LCmlJ 1.80, ph$ 1.80 PB 153 522
Since it is known that there nrvay be considerable
variation in the parasites of muskrats from one local-
ity to another, the pjresent study brings this variation
and its interrelation with environment into better ligl*
by the obvious absence of certain particular species.
402
Arctic Aeromedlca 1 Lab. , Ladd AFB, Alaska.
JTUDIES ON THE PARASITES OF EDIBLE ANIMALS
IN ALASKA, by Tommy T. Dunagan. [19561 lOp.
Technical note AAL-TN-56-12.
Order from LCmi$ 1.80, ph$ 1.80 PB 153 518
This report is a systematic listing of species examined
lod parasites found. No effort has been made to
enlarge or explain any of the resulting conditions
caused by the parasite. No discussion of systematic
parasitology occurs. No ecological relations between
host and parasite have been outlined. A chart showing
(Ustrlbution of muskrat parasites has, hdwever, been
included to emphasize that such conditions exist .
Microbiolog)^
t .
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
HYDATID DISEASE IN ALASKA, by Thomas R. A.
Davis. (19561 23p. 41 refs. Technical note AAL-TN-
56-1.
Order from LC mi$2.70, ph$4.80 PB 153 507
The research effort on echinococcosis in Alaska is re-
viewed. The results of this strongly indicate that the
disease is wide-spread both on the Alaskan Mainland
and the Bering Sea Islands. Two etiologic agents have
been demonstrated and these have widely separated
epizootiologic and epidemiologic charaaeristics. On
the basis at the data presented it is concllided that
much field and laboratory investigations are still
necessary before a proper understanding of the signif-
icance at the disease and its control can be achieved.
(Author)
Araic Aeromedical Lab. , Ladd AFB, Alaska.
AN OUTBREAK OF INFECTIOUS HEPATITIS IN TWO
ARCTIC VILLAGES, by Thomas R. A. Davis. Dec 56,
15p. 15 refs. Technical note AAL-TN-56- 38.
Order from LC mi$2. 40, phJ3. 30 PB 153 543
The charaaeristics of an outbreak of infectious
hepatitis in the Araic is described. The relationships
between the geographic distribution of cases, the
human contamination of the sources of water supply,
and the explosive nature of the epidemic, are pro-
pounded as reasons for the conclusion that this
particular outbreak was the result of a fecal-oral
mode of transmission with water acting as the causa-
tive agent vehicle. (Author)
Pathology
Arctic Aeromedical Lab., Ladd AFB, Alaska.
ENDEMIC GaTER IN ALASKA, by Kaare Rodahl
and CIS le Bang. [1956] 9p. Technical not AAL-TN-
56-9.
Order from LC mi$ 1.80. ^shS 1.80 PB 153 515
Inland Eskimos at Anaktuvuk Pass and the mountain
Indians at Arctic Village. Alaska, had abnormally
high and rapid 1^31 up»kes, as high as 85 per cent
24 hours following the tracer dose. They had low uri-
nary eliminations, low salivary I^^^ concentrations
and low plasma and protem bound ll3l levels after
24 hours . This was associated with a high incidence
of thyroid enlargements and apparently low dietary io-
dine'intakes . These findings are typical of endemic
goiter as described by Stanbury and collaborators
(Harvard University Press , 1954) in the Mendoza
population. (Author)
Arctic Aeromedical Lab. , Ladd AFB. Alaska.
THE ISOLATION OF ENTERIC PATHOGENS AT
BARROW. ALASKA, by T. R. A. Davis, J. W. Cullison
and others. [1956] 7p. 8 refs. Technical note AAL-
TN-56-7.
Order from LC mijl. 80, ph$l. 80 PB 153 513
Investigation of the population of Barrow for Salmonel-
losis shows a relatively high incidence in all age-
groups. A seasonal variation is demonstrated with
about a 100 percent increase of isolations in the sum-
mer as compared to winter isolations. The implica-
tions of these findings are discussed. (Author)
Brooke Army Medical Center, Fort Sam Houston,
Tex.
ACLTE RENAL FAILURE: THE REDUCTION OF
MORBIDITY AND MORTALITY, by Paul E. Teschan,
Thomas F. O'Brien, and Charles R. Baxter. Interim
rept. on Traumatic Surgery and Siock. Dec 59, lip.
7 refs. Research rept. MEDEW-RS-5-59.
Order from LC mi$2. 40, ph$3. 30 PB 153 193
Prophylactic daily hemodialysis is technically feasible.
Morbidity in patients so treated is strikingly reduced
in contrast to past experience. The recurrent clinical
crises which were so common with conventional man-
agement in the past are virtually absent. It is antici-
pated that the clinical improvement during oliguria
which characterized the patients reported herein will
continue to occur in further patients treated with pro-
phylactic dialysis at a renal center. It is further an-
ticipated that as morbidity is lessened, a commensu-
rate reduction in general mortality of patients with
acute renal failure may also occur. (Author)
Brooke Army Medical Center, Fort Sam Houston,
Tex.
IN VITRO SENSITIVITY OF PSEUDOMONADS FROM
BURNED PATIENTS TO COUSTIN SULFATE, by
Charles D. Graber, Wilfred T. Tumbusch, and
Edward H. Vogel, Jr. Final rept. on Radiation and
Thermal Bums. Nov 59, 8p. 1 ref. Research rept.
MEDEW-RS-4-59; AD-246 505.
Order from LC ml$1.80, ph$1.80 PB 153 192
Bactericidal activity of colistin sulfate for Pseudo-
monas aeruginosa was acquired in routine tube sen-
sitivlty testing at levels considerably lower than with
polymyxin B, kanamycin and neomycin. Emergence of
pseudomonad resistance to this drug was not marked;
only 3 out of 25 strains required more than a threefold
titer Increase in antibiotic needed for cidal inhibition
following six serial transfers in sublethal concentra-
tion of colistin. (Author)
403
Brooke Army Medical Center, Fort Sam Houston,
Tex.
SEPTICEMIA IN M^N INJURY, by WllfredTumbusch,.
Edward H. Vogelj Jr. and others. Interim repc. on
Radiation and Thermal Burna. Oct 60, I6p. 14 refa.
Research rept. MEDEW-RS-6-60; AD- 246 507.
Order from LC iT|i$2. 40, ph$3. 30 PB 153 194
Data have been ptescnted which reveal that septicemia
is present at death in over 60 per cent of fatal burns.
These data also Suggest an increase in the clinical
importance of sefXicemia due to EseudomOQaa
aeruginosa in sevierely burned patients. While survival
from staphylococcal and a number of other types o*
septicemia has been attained, Pfffllt^^*""^" septlcenrUa
invariably has been fatal. Attention has been focused
on the similarity of the clinical course in patients with
gram- negative oafganism septicemia to endctoxemia.
Experiences wlih^ local and generaUzed Shwartzman-
like phenomena ifi severely burned patients have been
described. (Author)
National Library of Medicine, Washington, D. C.
LEPTOSHROSIS, A BIBLIOGRAPHY OF LITER-
ATURE 1957 - lf59. by Dorothy Bocker. Bibliography
no. 4 on Ccmmuilcable Diseases at World-wide Sig-
nificance. Nov 5t>, 42p. 319 refs. ^ , ,„ ^,
Order from LC mi$3. 30, phr. 80 PB 150 062
The references ^elected are In English, French,
German, ItalUnJ and Spanish; the period covered is
1957 - October 1*959. Earlier references are given In
some al the articles listed and are so indicated.
Radiobiology
Gustaf Werner j Inst, for Nuclear Chemistry (Sweden)
RESEARCH ON "LOCAUZED RADIO- LESIONS".
PART VI. RESTRICTED RADIO- LESIONS IN THE
C«PTH OF TH$ BRAIN PRODUCED BY A BEAM OF
HIGH ENERGY PROTONS, by Lars Leksell, Bttrje
Larsson and otters. Technical note no. 1 on Comract
Tl June 60, 21p. 9 refs. AFOSR TN-
AF 61(052)183.
60-1406.
Order from LC [ni$2.70, ph$4.80
PB 153 304
Restricted lesioiis were produced in the depth of the
goat's brain by (neans of cross-fire irradiation with a
narrow beam of high energy protons. The radlosurgi-
cal technique arid the histopathology o< the lesions are
described. It w^s possible to produce well circum-
scribed cerebri lesions of a type well suited for
physiological experimentation without danwging sur-
rounding nervous tissue. The method may also be
applied to iieurqsurgery in man. (Author) (See also
PB 146 312)
Conteots:
Section I. --Air ■
Public Health Service Radiation Surveillance Network
Public Health Service National Air Sampling Network
Naval Research Laboratory Radioactivity Measuremar
Canadian Radioactive Fallout Study Program
Section U. --Food, other than Milk
Survey at Radioactivity in Pood
Strontium -90 Concentration in Food Samples Taken ia
Sute of Alaska
Strontium -90 in Food
Strontium-90 Content in the MiUtary Diet in Peru and
Ecuador (1959)
Strontium-90 Co«ent In die Military Diet in Vietnam
(1959)
Strontium-90 Content in Diet in Various Countries
Section III. --Milk
Public Health Service Milk Monitoring Program
Strontium-90 in North American Milk
Cesium- 137 in People and Milk in the United States
Section IV. --Water
Public Health Service National Water Quality Network
Monitoring at Water Supplies Around the Nevada Test
Site
Section V. - -Other Data
External Gamma Activity (August 1960)
Argonne National Laboratory Soil Data
Strontium-90 Concentration in Human Bone From
Alaska
Strontium-90 Activity in Human Bone
Bnvimmental Levels at Radioactivity at Atomic Enero
Commission Insullations
Fallout Studies Interpretive Reports
(See also PB 161 371-9)
Radiobiological Lab. , U. of Texas, Austin.
EFFECTS OF CHRONIC LOW DOSE NEUTRON
IRRADIATION UPON PERIPHERAL BLOOD ELE-
MENTS IN THE MONKEY (MACACA MULAITA) by
Georges. Melville, Jr.. Robert J. Young and others.
Aug 60. 13p. 15 refs. AFSAM 60-60.
Order from LC ml$2. 40. phJ3. 30 PB 153 301
Twenty-four monkeys (Macaca mulatta) were divided
into four groups of 6 and exposed periodically to low
doses of neutrons from Po-Be sources. The irradiated
groups received 13, 28, and 55 rep total dose which
was divided into doses administered every 4 days for
40 exposures The cellular elements of the peripheral
blood, hemoglobin, and hematocrit values were
sampled and enumerated at intervals postirradiation.
These data were analyzed by analysis of variance. All
surviving monkeys have reestablished normal hema-
tologic values by the end of 24 weeks postirradiation.
There Is no indication of any incapacitating injury
under these experimental conditions. A significant
sutlstlcal result was found for reticulocytes, hemato-
crit values, neutrophils, and lymphocytes. Only the
hematocrit value changes are considered interpretable
in terms of the irradiation treatment (Author)
Public Health 3ervice, Washington, D. C
RADIOLOGICAL HEALTH DATA. VOLUME 2, NO. 1.
Quarterly rept. Jan 61, 63p. 7 refs.
Order from OTl $1.00 $9.00/yr. PB 161 371-10
404
CHEMISTRY
Analytical Chemistry
Bell and Howell Research Center, Pasadeita, Calif.
BLBCTROANALYTICAL METHOD FOR THE DE-
TERMINATION OF CARBON AND HYDROGEN IN
ORGANIC COMPOUNDS, by Herben S. Haber and
Kenneth W. Gardiner. Rept. for 15 June 59-14 May 60
00 The Chemistry and Pbysics of Materials, Contract
AF 33(616)6676. Sep 60, 26p. 2 refs. WADD Technical
rept. 60-415.
Order from OTS $0. 75 PB 171 409
The development and application of a rapid C-H ana-
lyzer is summarized. A prototype instrument was de-
veloped combining electroanalytical and gas chromato-
graphic techniques. Ten nrUnutes are required for a
complete analysis. Additional refinement of the appa-
ratus will be necessary to attain the specified accuracy
of 0. 356 by weight. (Author)
Bureau of Naval Weapons, Washington, D. C
MASS IN AIR 200 GRAMS TO 30 KILOGRAMS
CLASSES S-1 METRIC, P, AND Q. BuWeps-BuShips
Calibration Program. 18 May 60, 28p. Secondary
Sundards Lab. Measurement System Operation Pro-
cedure NM-02.
Order from OTS %0. 75 PB 171 236
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to calibrate mass in air. The system consists of the
Christian Becker BB-4 30 kg Large-Capacity Balance
and several sets of Class S weights totaling 30 kilo-
grams to be used as standards. Also included in the
system are Tare Weights totaling 30 kilograms. The
technique employed to make mass measurements Is the
Substitution Weig^iing method.
Mine Safety Appliances Co. , Gallery, Pa.
ANALYTICAL TECHNIQUES FOR ORGANIC COOL-
ANTS, by Eugene P. Meckley. [Rept. on Contract
Nobs-65426] 3 Jan 57. 37p. 31 refs.
Order from LC ml$3. 00. ph$6. 30 PB 154 408
Iblt report released for sale to the public 16 Feb 61.
Organic compounds such as blphenyl, Dowtherm A,
etc. are under Investigation as possible reactor cool-
tnts and moderators. In connection with the engi-
neering evaluation of such materials considerable ana-
lytical work Is necessary. As an aid to the members
participating in the organic coolants program these
techniques were compiled. Iitcluded In the report Is:
Antlysis of organic materials for traces of metallic
impurities, pub. in Industrial and Engineering
Chemistry 11:646-649. 15 Dec 39. .
Organic Chemistry
(Dates and Crellin Labs, of Chemistry, Calif, bift.
of Tech, Pasadena.
SMALL- RING COMPOUNDS XXDC A REINVESTI-
GATIDN OF THE SOLVOLYSIS OF CYCLOPROPYL-
CARBINYL CHLORIDE IN AQUEOUS ETHANOL.
>IS0MERIZATION OF CYCLOPROTYLCARBINOL, by
Marjorie C Caserlo. William R Graham and John
D Roberts. Technical rept. no. 7 on Contract Nonr-
220(26). Feb 60. 32p. 11 refs. Contribution no. 2554,
AD- 233 406.
Order from LC ml$3. 00, ph$6. 30 PB 153 156
Contrary to the reports of other workers. It was found
that the solvolysis of cyclopropylcarbinyl chloride in
S0% ethanol is attended by sutetantial rearrangement
- not only do the solvolysis products include cyclobutyl
and allylcarbinyl alcohols and ethyl ethers but cyclo-
propylcarbinyl chloride undergoes partial rearrange-
ment by "internal return" to cyclobutyl and allyl-
carbinyl chlorides. Nuclear magnetic resonance
spectroscopy has been used to demonstrate that
ccmslderable isotope -posit ion rearrangement takes
place under quite mild conditions in the reactions of
deuterium -labeled cyclopropylcarbinol and cyclo-
butanol with thlonyl chloride. Isotope -position
changes have been studied in the acid-induced iso-
merlzation of cyclopropylcarbinol. (Author)
Massachusetts U. , Amherst.
THE SCATTERING FROM PORTIONS OF SINGLE
SPHERULITES OF POLYETHYLENE OXIDE, by
Marion B. Rhodes and Richard S. Stein (Master's
thesis). ONR Technical rept. no. 17 on Contract
Nonr-2151(00). 29 Feb 60, i5p. 12 refs. AD- 244 443.
Order from LC mi$2. 40. ph$3. 30 PB 150 65f
Photographic light -scattering experiments were con-
ducted on 5- to 10-mm-diam spherulites of polyethyl-
ene oxide. By moving the sperullte sample relative to
the ligjit beam, patterns were obtained on scanning a
spherulite along a horizontal radius, a vertical radius,
and a 45° radius for Vy. Hh, and Hy polarization. All
the scattering patterns apparently have preferential
elongation in a direction tangential to the spherulite.
The intensity and elongation of the panem is greatest
when the direction of polarization is tangential. The
panem did not vary greatly with distance from the
center of the spherulite. The scattering patterns also
indicated that the local polarizability varies in the
radial and ungential direction of the spherulite in a
manner which is consistent with a fiber or plate like
structure for the spherulite; the long direction of the
fiber or plate is radial to this direction, and the great
est refractive index is perpendicular. An experiment
was designed to differentiate among the possible
causes for fluctuation in the scattering panem; it in-
volved obtaining patterns for various samples which
had been swollen with solvent having refractive in-
dices different from that of the sample. The solvents
used were methylphenyl ether, CCI4, acetone, prp-
pyiene glycol, cycloheoanone. nitrobenzene, and a
number of silicone fluids with a refractive index in
405
the I. 35 to 1. 55 ra ige, as compared to about 1. 46 for
a sample. Orienu(ional differences are the most
probable cause of ^canering; in highly ordered crys-
tals of polyethylene which exhibit ring structure, the
a and c axes are tatigential and rotate helically about
Che b axis with increasing radius.
New Hampshire Lj. [Durham]
ELECTROPHILIC DISPLACEMENT REACTIONS. X.
GENERAL AQD (IaTALYSIS IN THE PROTODEBOR-
ONATION OF ARgNEBORONlC ACIDB, by Henry G.
KuivilaandK. V. Klahabedian Rept. on Contract
AF 49(638)312. (I9|60l 24p. 22 refd. AFOSR TN-
60-1270.
Order from LC mii2. 70. ph$4. 80 PB 153 216
The kinetics of thejprotodeboronation of^-methoxy-
benzeneboronic acil in aqueous sulfuric, phosphoric
and perchloric acids, and in formic acid have been
studied. The rate constants in the first three acids are
correlated by the acidity function Hq, but they are con-
siderably greater it given values of Hq in phosphoric
acid than in the other two. In formic acid containing
I. 3% water and 4 (f^ ethylene glycol dimethyl ether
the rate constants ire not correlated by Hq- The pres-
ence of added sodlim formate in amounts which change
the acidity by a faator of ten does not change the rate
constant. indicatinR reaction with molecular formic
acid. The rate of protodeboronation erf the more re-
active 2, 6-dlemth4xybenzeneboronic acid in aqueous
perchloric acid up
not by stoichiomet :ic acid concentration. (Author)
New Hampshire I
to 2. 5 M is correlated by Hp, and
[Durham]
ELECTROPHILIC DISPLACEMENT REACTIONS. XII.
SUBSTITUENT EF 'ECTS IN THE PROTODEBORO-
NATION OF ARE? EBORONIC AQDS, by K. V.
Nahabedian and Heiry G. Kuivila. Rept. on Contract
AF 41(638)312. [l^j 36p. 21 refs. AFOSR TN-
60-1346.
Order from LC mi 13. 00, ph$6. 30 PB 153 215
Kinetic studies on fhe hydrolysis of nine areneboronlc
acids in aqueous sulfuric and phosphoric acids are de-
scribed. Dependence of rate on acidity has been ex-
amined in each caie, and activation parameters am)
solvent hydrogen iiotope effects have been determined
in certain cases. Conventional Hq plots reveal the
presence at two kifietically distinct regions separated
by the Ho range 5. D-5. 5. The behavior of activation
parameters and solvent isotope effects bear out this
dichotomy. Consideration of these facts coupled with
the effect of substijuents on reactivity leads to an in-
terpretation of the! data in terms of the existence of at
least two mechanisms for the reaction. (Author) (See
alsoPB 153 216)
Physics Lab. , Weight Air Development Div. ,
Wright -Patters on AFB, Ohio.
MOLECULAR WEIGHT DETERMINATION IN TTIE
CHARACTERIZATION OF POLYMERS^ by Richard M.
Lange. Rept. for Mar 59-Jan 60 on Non-Metallic and
Composite Mater iajls. Sep 60, 28p. 7 refs. WADD Tech-
nical rept. 60-357
Order from OTS $ i. 75
PB 171 401
Preliminary results are given on the determination of
the macro- structure of poly-(dimethyl-2. 2'-dimethylene
pimelate) prepared by solution polymerization to 40%
conversion. The physical methods used in this study in-
clude osmometry, light-scattering, viscometry and
fractioixal precipitation. Osmotic pressure measure-
ments on a sample at the whole polymer in toluene solu-
tion vielded a number -average molecular weight of 3.36
X lO' grams/mole. Light -scattering measurements on
the same system gave a weight -average molecular
weight of 2. 80 X ICr grams/mole. The heterogeneity in-
dex (Mw/Mn) at this polymer Indicates a broad distribu-
tion of molecular weights. A small sample at the poly-
mer was subjected to fractional precipitation techniq
with only partial success. Weight and number -average
molecular weights were obtained on two fractions.
(Author)
Purdue U , Lafayene, Ind.
THE METALATION OF DIPHENYLFERROCENYL-
CARBINOL, by Robert A. Benkeser. Walter P.
Fitzgerald, and Marvin S. Melzer. Rept. on Contract
AF 49(638)297. 10 Nov 60, 9p. 1 ref. AFOSR-TN-
60-1365; AD- 246 801.
Order from LCml$ 1.80, ph$ 1.80 PB 153 265
Triphenylcarblnol can be metalated with q." butyl lithium
and then carbonated to form the lactone of triphenyl-
carblnol-2, 2' -dlcarboxyl acid. A somewhat analogous
reaction which occurs with diphenylferrocenylcarbinol
is reported.
Physical Chemistry
Air Crew Equipment Lab. , Naval Air Material
Center, Philadelphia, Pa.
DESIGN CRITERIA FOR EFFIQENT FILUNG OF
UQUID OXYGEN CONVERTERS: DEVELOPMENT
AND EVALUATION OF, by Francis A. Florlo.
29 Aug 60, 19p. NAMC-ACEL-439; TED NAM AE-
51143; AD- 243 454.
Order from LCmi$2. 40, ph$3. 30 PB 153 354
A proposed method of filling liquid oxygen converters ll
presented and denwnstrated as being feasible in princi-
ple artd operation. Filling of 5. 10, and 25 liter Dewtr
flasks are performed under various service and design
conditions . In addition, effects of filling pressure,
component pre-cooling, and Dewar volume are also in-
vestigated. The total loss of liquid oxygen resulting in
transfers performed by the proposed method are ex-
tremely small and represent approximately .5 to 3.5
per cent of the total amount of liquid transferred . The
proposed method is offered as a possible substitute for
swndard Navy methods of filling liquid oxygen conver-
ters for air crew breathins. (Author)
Bonn U. (West Germany).
LABORATORY EXPERIMENTS ON FORMATION AND
OXIDATION OF HYDROGEN IN THE ATMOSPHERE,
by Wllhelm Groth. Final rept. for 1 Nov 58-31 July 59
on Contraa AF 61(062)128. 31 Aug 59, 17p. 17 refs;
AD- 227 279.
Order from LC ml$2. 40. ph$3. 30 PB 150 690
406
A liriit source was constructed for the investigation of
the photolysis of water vapor. A xenon discharge arc
of a pressure of about 50 mm in a thin wall quartz tub-
ing was used. Molecular hydrogen formed from water
vMwr in the presence of other gases was measured by
employing tritium as a tracer. A vacuum system was
constructed, allowing the separation of water vapor
from hydrogen to better than lO'O parts, and the count-
ing at trltlated hydrogen in a Geiger counter. All
measurements were carried out in a semi -quantitative
way and it was found that the li^t source and the tech-
nique of measuring small amounts of free hydrogen by
employing a tritium tracer can be used effectively for
further studies of the reactions involving hydrogen and
water. Self -decomposition of tritiated water vapor witli
and without addition of oxygen was measured and was
found to be negUgible under the particular conditions of
the experiments over periods of several months. The
photochemlcally Induced exchange of tritium between
tritiated water vapor and molecular hydrogen was
studied. The quantum yield of this exchange was found
to be under the conditions of the experiments of the
order of one and probably sUghtly larger than one. It
was possible to demonstrate the formation of free hy-
drogen from the phaolysis of water vapor in the pres-
ence of oxygen and to measure these amounts as a func
tion (rf oxygen pressure. The steady state concentra-
tions of H2 formed from water vapor by irradiation in
the presence of oxygen under the Influence of UV light
were found to be smaller than expected. Photochemical
oxidation of H2 by O2 under the particular conditions of
the experiments and at pressures of about one milli-
meter was found to have a quantum yield of the order ol
magnitude of one . (Author)
Calvin Coll. , Grand Rapids, Mich.
THE CATHODIC BEHAVIOR OF AgO IN ALKALINE
SOLUTIONS, by Thedfors P. Dirkse. Technical rept.
no. 10 on Contract Nonr- 1682(01). 30 Jan 60. 19p.
8 refs. AD-233 898.
Order from LC mi$2. 40, ph$3. 30 PB 152 871
A study has been made of the discharge of AgO in order
to determine why only a part of the discharge capacity
of AgO Is delivered at the potential of the AgO-Ag20
couple, and to determine the role of oxygen in this
process. The difference in discharge capacity of elec-
trodes produced by constant current and by constant po-
tential anodization has also been studied. A mechanism
involving the transport of Onions through the electrode
material and the reaction of these ions with the elec-
trolyte is presented. (Author)
Coating and Chemical Lab. , Aberdeen Proving
Ground, Md.
AMINO CARBOXYLIC AMPHOTERIC SURFACTANTS
IN ALKALINE CLEANERS, by A. Mankowich.
9 Nov 60, 9p. 2 r«f8. CCL *98.
Onler from OTS $0. 50 PB 171 128
A study was made oi amino-carboxyllc amphoteric sur-
factants in soak -type alkaline cleaners suitable for use
with aluminum and magnesium (nonferrous) aUoys as
well as with ferrous materials. Compounds were de-
veloped possessing the improved detergency" neces-
sary for the removal of asphalt and mineral oil sella.
The surfactant portion of such compounds may consist
of as little as 1. 0 percent of the partial sodium salt of
N-lauryl beta iminodipropionate plus 1.0 percent of a
polyethanoxy nonyi phenol (15-30 ethylene oxide mole
ratio). Galvanic corrosion tests using magnesium -
aluminum couples indicated satisfactory behavior c*
the aluminum, the anodic member of the couple, as
well as of the magnesium. The developed cleaners
meet all the performance requirements o< Fed. Spec.
P-C-436a (Cleaning Ccwnpound, Alkali Type) except
surface tension. (Author)
Colorado U. , Boulder.
THE THERMOCHEMISTRY AND PHOTOCHEMISTRY
OF ORGANIC HALOGEN COMPOUNDS, by R. Burk-
hart, H. B. Gottlieb and others. Final rept. on Con-
tract AF 49(638)241. 6 Sep 60, 98p. 68 refs. AFOSR-
TR-60-126; AD-245 663.
Order from OTS $2. 25 PB 171 376
Kinetic Study of the Photobromination of Trifluoro-
bromo Ethylene: A high -pressure. General Electric,
Model A-H6 mercury arc lamp was used as a light
source. The extensive induction period, before the
maximum rate was achieved, was increased when CI
was not removed from the Br by reaction with KBr.
When the incident light intensity was doubled, the in-
juction period was cut nearly 50%. An increase in
the amount of absorbed radiation by increasing the Br
pressure, instead of the incident light intensity, gave
only a small decrease in the induction period. The
reaction order for Br was 3/2. Phrtochlorination of
Trifluorobromoethylene: An interference filter trans-
mitting light at 424 A was used in connection with the
A-H6 lamp; the remaining experimental procedures
were similar To those in the previous investigation.
The kinetics of this reaction depended on the volume -
to- surface ratio of the reaction cell. Five reactions
were conducted to determine the dependence of the
rate on light intensity, 0. 56 and 0. 57 when the CI
pressure was 97. 9 and 68. 2 mm. respectively.
Flames Produced by Burning Fluorine -Containing Ole-
fins: A study was made of the flames produced by the
combustion of chlorotrifUioroethylene, CI, and O;
perfluoroisobutene, 1 , 1 -difluoroethylene, 1,2-di-
chloro-1. 2-defluoroethylene, and perfluorocyclobu-
tene. A study was made of the factors which influence
the intensity of the glow produced by the reaction of
chlorotrifluoroethylene with O. For the chlorotri-
fluoroethylene reaction with CI, the products of the
diffusion flame were CF3C1. CF3C12. CFC13, and
CF2C1-CFC12.
Cryogenic Lab. , Ohio State U. Research Foundation,
Columbus.
THE HEAT OF SUBLIMATION OF CARBON, by
P. Goodman, M. Nay and others. Rept. on Contract
W33-038-ac-17721. 1 Apr 49, 83p. 333 refs. AMC
Technical Intelligence rept. no. F-TR-2264-IA-1;
ATI- 114 680. _ ^ ^^
OrderfromLCml$4.80, ph$13.80 PB 154 056
This report released for sale to the public 15 Feb 61 .
The literature pertaining to the heat d sublimation of
carbon has been reviewed, and the various methods
which have been employed in an attempt to determine
this quantity are discussed. The experimental methods
used may be divided into two groups. The first group
407
*l
of data was obtained from the dissociation phenomena
of carbon monoxiide, and the second group from direct
measurements upon carbon. Both the experimental
evidence obtained from the spectrum of CO and the dif-
ferent interpretations thereof are given. The investi-
gations performefd by electron impact methods aa well
as the photodlssdciaiion at CO are also reviewed. The
second group of experiments was performed on carbon
at temperatures exceeding 2500°K. The results ob-
tained from the aartx>n arc, resistance and induction
heating methods,, and rate erf vaporization and effusion
methods are disdussed. A consideration of the mate-
rial presented in this review leads to the conclusion
that, aa yet, no v|nique value for the heat of sublima-
tion at carbon miy be given with certainty. (Author)
Prick Chemicalj Lab., Princeton U. , N. J.
CHEMICALLY INDUCED VIBRATIONAL EXOTA-
TION: HYDROXYL RADICAL EMISSION IN THE 1-3
MICRON REGION PROIXJCED BY THE H+-O3
ATOMIC FLAMS, by David Garvin, H. P. Broida and
H. J. Kostkowskij (National Bureau of Standards) Tech-
nical note no. 5 4n Contracts AP 18(603)134 and CSO
6«0-56-30. 24 A»g59, 24p. 18 refs. APOSR TN-
59-746; AD-226!73.
Order from LC r ii$2. 70. ph$4. 80 PB 150 923
A deuiled investigation has been performed in the 1 to
3 micron wavelength region on the radiation emitted by
the hydroxyl radical from a low pressure flame of
ozonized oxygen < tnd atomized hydrogen.
Prick Chemicali Lab. , Princeton U. . N. J.
ELASTIC CONSTfANTS AND INTERMOLECULAR
FORCES IN ICEi by C. Haas. Technical rept. no. [5)
on Contract Nonr- 1858(27). 27 Apr 60, 14p. 4 refs.
Order from LC rtu$2. 40, ph$3. 30 PB 148 021
The five independent elastic constants of ice have been
calculated in terms of two constants, the force con-
stants for stretching and bending the hydrogen bond.
The calculated elastic constants are all within 5 per-
cent of the observed values. The same force constants
also yield values for the lattice frequencies which
agree reasonably well with those determined experi-
menuUy. (Authqr)
(Authofr)
General Telephone and Electronics Labs. , Inc. ,
Bayside, N. Y. ,
INVESTIGATION I OF THE CHEMICAL REACTION
BETWEEN TUNQSTEN AND ALUMINUM OXIE«, by
R Wallace. J. Florio, and T. Polanyi. Final rept. on
Contract AF 19(604)4084. 1 AjfH" 60, 73p. 24 refs.
TR 60-204.6; ERD TR-60-168; AD- 243 898.
Order from OTS $2. 00 PB 171 373
A tungsten Knudsen cell - oven assembly operable at
2500 C in vacuun^ was assembled and set in operation.
Development stefja and performance data are reported
in detail. The coiiversion of a sixty degree ten inch
radius, Nicr-typ# gas analytic mass spectrometers to
a niachlne adapted for use in conjunction with a
Knudsen cell-ovefi assembly for the study of high tem-
perature chemic^ reactions between sollda, la re-
ported in detail. IDesign considerations and construc-
tional features are extensively discussed. The con-
version work is specific for an original instrument
having a 3.75" source chamber diameter and a down-
ward pointing ion source, however the design con-
siderations have more general applications. This
work constitutes the major preliminary instrumental
phase for the study of the reaction between tungsten
and alumina. The technological importance of this
reaction in the electronic industry is reviewed and a
short literature survey of pertinent studies presented.
The mass spectrometric method ot studying high tem-
perature reactions is discussed and the plan for con-
tinued work is reviewed in detail. (Author)
Institut Pasteur. Paris (Prance).
PHOTO -ACTIVATED PRODUCTION OP FREE RADI-
CALS FROM DIATOMIC MOLECULES AFTER AD-
SORPTION ON METALLIC SURFACES, by C M.
Moser. Annual technical rept. no. 1, 1 Oct 59-
30 Sep 60. on Contract DA 91 -591-EUC-l298-01-4l60-
60. [1960) 38p. 4 refs; AD- 246 741.
Order from LC mi$3. 00, ph$6. 30 PB 152 685
A detailed study of the potential curves for various
states of carbon monoxide using the simplest set of
atomic functions. Is, 28 and 2p on each center, dif-
ferent possibilities of extending and improving this
basis at the observed equilibrium distance for CO
(2. 1319 a. u.).
Institute for Fluid Dynamics and Applied Mathematics,
U. of Maryland, College Park.
ELECTRON DIFFUSION AHEAD OF SHOCK WAVES
IN ARGON, by H. D. Weymann. Rept. on Contract
AF 49(638)401. Mar 60, 18p. 7 refs. Technical note
BN-197; AFOSR-TN-60-334; AD- 234 795.
Order from LCml$2. 40, ph$3. 30 PB 149 731
Experlnf>ents with electrostatic and magnetic probes
were performed to investigate the electron diffusion
ahead of shock waves of M, » 8 to 12 in argon. Nega-
tive electrostatic signals of several volts were obtained
with pronounced fronts propagating with velocities of up
to several times the shock velocity. The current pro-
duced by the diffusing electrons was determined from
a measurement of the azimuthal magnetic field and
found to be of the onler of 10"5 amp for Mg • 12 .
Assuming that the electron flow velocity is approxi-
mately equal to the velocity of the electrostatic front
the nr>easured current corresponds to an electron den-
sity of n^ 10^ cm'^ at about 1 m ahead of the shock
front. (Author)
Institute for the Study of Metals, U. of Chicago. 111.
APPARATUS AND METHODS FOR LOW TEMPERA-
TURE HEAT CAPACITY MEASUREMENTS. TWE
HEAT CAPACITY OF STANDARD BENZOIC ACID,
by Arthur G. Cole, John O. Hutchens and others.
Technical rept. no. 3 on Contract Nonr-2121(13).
[1960] 37p. 11 refs.
Order from LC mi$3. 00, ph$6. 30 PB 1 53 765
An apparatus and methods for the measurement of low
temperature heat capacities of solids are described.
The methods of correcting the data for heat Inter-
change and for thermal gradients within the calorl-
metric system, as well as other necessary corrections.
408
gi« discussed. The heat capacity of a Calorimetry
Qj^terence standard sample of benzoic acid has been
nieasured in the tempeature range between 10 and
3(X)PK and the results are compared with data from
the National Bureau of Sundards and from other
laboratories. (Author)
latituto di Fislca, Unlversita di Padova (Italy).
IONIC MOBILITY AND RECOMBINATION IN LIQUID
HELIUM II. Final technical rept. for lX>ct 59- Oct 60
onContract DA 91-591-EUC-1290. [1960] I6p. 3 refs.
Orfer from LC mi$2. 40, ph$3. 30 PB 152 608
The research performed under this contract may be
devided into two general categories: investigation of
the properties of ions In liquid helium, and the uae of
helium Ions in experiments on the hydrodynamic prop-
erties of liquid helium. All the work was carried out
at temperatures in the helium 1 1 region, that is, below
2. 19°K. The behavior of the positive and negative iona
and their interaction with their solvent, liquid helium
*aa sttidied through measurements of the mobility and
the coefficient of recombination. These measurements
have been made at various temperatures and pressures
and by various means which will be enumerated below
and described more fully in the main body of the re-
port. The two experiments on the flow properties of
liquid helium will likewise be described briefly below
and more fully in the main report. (Author)
Kentucky U. [Lexington].
N-SULFINYL AMINES. TRANS -SULFINYLATION
WITH PRIMARY AMINES, by Walter T. Smith, Jr.,
WillUm K. Plucknen and Thomas L. Dawson. Rept.
onContract AP 49(638)49. Nov 60. 23p. 11 refs.
APOSR -TN -60- 854; AD-246 989.
Order from LC mi$2. 70, ph$4. 80 PB 153 451
The rates of reaction of N-sulfinylaniline with seven
primary aliphatic amines have been determined using
• gpectrophotometric method based on the absorbance
of li-sulfinylaniline at 320 n^ The trans -sulfinyla-
tlon reaction takes place in two distinct stages. The
dau indicate that the first stage is a first order ap-
proach to. equilibrium and that the second stage is first
oixler with respect to M-sulAnylaniline The rate of
the reaction is increased by increased solvent polar-
ity. Pyridine has a catalytic effect on the second stage
of the reaction. (Author)
■ Michigan U Coll. of Literature, Science, and the
Arts, Ann Arbor.
SPECTROSCOPIC EVIDENCE FOR GASEOUS
BENZYNE, by R. Stephen Berry, G. Nell Spokes and
R. Martin Stiles. Rept. on Contraa AF 49(638)538.
Oa60, 5p. 2 refs. 02878-2-P; AFOSR-TN-60-991;
AD-244 841.
Order from LC mill. 80. ph$ 1.80 PB 152 611
A volatile precursor of dlphenylene from the flash
photolysis of benzenedlazonium-2-carboxylate has been
detected. The short-lived Intermediaie Is tentatively
identified as benzyne (1, 2-dehydrobenzene). This
taalgnment follows a consideration of the source of
the species, its ultraviolet spearum, and the rapidity
with which it forms gaseous dlphenylene.
Naval Research Lab. , Washington, D. C
A THERMODYNAMIC ANALYSIS OF SOLUBILITY IN
LIQUID METAL SYSTEMS, by J. L. White. Pinal
rept. on one phase of the problem. 7 Dec 60, 24p.
33 refs. NRL rept. 5555. ^
Order from OTS $0. 75 PB 161 990
Binary liquid -metal solubility equilibria of the type A
(in solid or liquid pha8e)^A (in liquid B) are analyzed
in terms of the_fundamental thermodynamic solution
parameters AH^Cb and Affifig, the heat and entropy,
respectively, of Klution oTOfe Uquid solute at infinite
dilution in the liquid solvent. A general method for the
treatment of equUibrium solubility data is developed
and is termed the E ' -function method, in view at its
similarity to the standard J] -function method for the
treatment of vapor -preaaure dau. By the assumpcion
of subregular behavior of the liquid metal solution, the
£* -function method is applicable to moderately con-
centrated solution. Consideration is given to dewlls of
the application of the method to the three general states
of the solute phase: (a) pure solute A, (b) tennlnal so-
lution of B in A, and (c) intermetallic compound
AxBi .j|. The ^ ' -function method is applied to five
binary systems for which data are available in the lit-
erature: Mg-Pe, Pb-Nl, Bi-Be, Pb-Zn, and Pb-Cu.
The results are In close agreement with the results
published in the literature. (Author)
ftoyes Chemical Lab. , U. of lUlnols, Urbana.
A PROTON MAGNETIC RESONANCE STUDY OF
CRYSTALLINE POTASSIUM TRISOXALATORHO-
DIUMdll) HYDRATE, by A. L. Porte, H. S. Gutowsky,
and G. M. Harris. Technical rept. no. 29 on Contract
Nonr -1 843(1 3). 18 Arp 60, 19p. 15 refs. AD-237 062.
Ortler from LC ml$2. 40. ph$3. 30 PB 147 776
The broad -line proton magnetic resonance spectrum of
crystalline potassium trisoxalatorhodium(lII) hydrate,
K3Rh(C204)341/2H20, was Investigated in thetemper-
ature range 77OK-330OK. The spectrum at 77^ indi-
cates that some of the protons iii the crystal are not
present in water of crystallization and an analysis of
this same spectrum indicates that the compound should
be reformulated. The formula is not inconsistent with
the chemical reactions that the compound undergoes,
and it explains some properties which are not satis-
factorily accounted for by the previously accepted
formula. The absorption spectrum at 318°K substanti-
ates the analysis of the spectrum at 77**K and it also
indicates that the water of crystallization can be
grouped into at least three sets, the water molecules
in different sets having different d^rees of mobility.
(Author)
Noyes Chemical Lab. , U. of Illinois , Urbana.
TEMPERATURE DEPENDENCE OF THE CHLORINE
PURE QUADRUPOLE RESONANCE FREQUENCY IN
MOLECULAR CRYSTALS, by H. S. Gutowsky and
D. W. McCall. Technical rept. no. 20 on Contract
Nonr- 1834(13). 22 June 59, 22p. 19 refs, AD- 220 345.
Order from LC mi$2.70. ph$4.80 PB 150 921
The Cl^ pure quadrupole resonance frequency has
been observed in polycrysuUine CH2CI2. CHCI3,
CCI4, (CH3)3CC1 and CH3CCI3 at temperatures of
77*^ and abwe . In all cases t the resonance frequency
409
imown
decreases at higijer temperatures , in qualitative
agreement with Bayer's theory for the torsional
motions of the molecules . However, a quantitative
conqjarison of th(( theory with emeriment, including
Livingston's results at 4° and 20^, reveals signifi-
cant discrepanci^ which are discussed and attributed
mainly to the decjrease in torsional frequencies at
higher temperatures . The resonance was found to
"fade out" at temperatures below the transition points
in those solids, ici^. (CH^^CCl, and CH3CCI0.
where internal or molecular reorientations are la
to occur. In the ^her compounds the resonance was
observable up to the melting point . The origin of this
phenomenon is discussed briefly. (Author)
Pennyslvania Sute U. , University Park.
STABILITV RELATIONSHIPS AMONG THE RARE
EARTH ACETYUACETONES, by Igmar Grenthe and
W. Conrad Fernflius. Technical rept. no. 1 on Con-
tract Noor-65624 17 Feb 60. lOp. 12 refs.
AD-233 212. f
Order fromLC rli$l. 80. ph$l. 80 PB 153 157
Step-wise stoichlonietric formation constants have
been determined for the reaction between acetylacetonc
and the rare eartjhs including yttrium. "Hie measure-
ments have been knade at a temperature of 3(PC In an
aqueous perchloiiate medium of an ionic strength erf
0. 1 M. A plot of the logarithm of the first formation
constant against the ionic potential shows a linear re-
lation from La t(i Eu with a change of 0. 15 units in log
Ki between consecutive elements. After Gd the com-
plexity remains iearly constant with a total change in
log Kj from Tb to La of 0. 2 units. This relation be-
tween the ionic potential and log K has been compared
with the same reUtion for other rare earth complexes.
(Author)
Pennsylvania State [U. Coll.] of Mineral Industries
[University Park].
CHEMICAL PROPERTIES OF SOME OXIDE SUR-
FACES, by Dorothy P. Enright. 0. N. R. Technical
rept. no. 46 on (Jontract N6onr-269. T. 0. 8. Apr 52,
lOp. 3 refs. ATI*-159 367.
Order fromLC i|u$ 1.80. ph$ 1.80 PB 154 295
This report released for sale to the public 14 Feb 61 .
The reactivity of freshly dehydrated silica gel indi-
cates the presenae of surface ions which can donate
and accept electrt>ns and thus cause oxidation and re-
duction ph^nometia . This behavior of the silica sur-
face and of an alijmina- silica catalyst has been found
also in the reactjjvity of a partly oxidized graphite sur-
face. (Author)
Princeton U. , ^ . J
PARAMAGNETIC
RESONANCE ABSORPTION IN
PEROXO-DICOBALT COMPLEXES, by E. A. V.
Ebsworth and J. ~ -- - -
Nonr- 1858(27).
Order from LC rtJi$3. 00, ph$6. 30
Weil. Rept. on Contract
5 May 59, 33p. 35 refs. AD-218 013.
PB 149 648
l<^3>5^-
The paramagnetic resonance spectra of the ioni
-0-0-to(NH ) ]* and
•3 ^
[(NH ) Co "XiKNH ) ] were studied using vari-
ous solvents. Under appropriate conditions, 15 hyper-
fine lines can be resolved in the spectrum of each,
showing that the single unpaired electron must inter-
act equally with both cobalt nuclei. The derivative
spectra were not in general symmetric, and varied
with changes in the acidity, viscosity and temperature
of the solvent. These variations are Interpreted in
terms of anisotropy and relaxation effects. (Author)
Rensselaer Polytechnic Inst. , Troy, N. Y.
ALKALI METAL CARBONATES. PART IIL SOLID-
LIQUID PHASE EQUILIBRIA FOR MIXTURES OF
LITORJM, SODIUM, AND POTASSIUM CARBONATES,
by George J. janz and Max R. Lorenz. Technical rept
no. 5 on Contract Nonr-591(10). Apr 60. 21p. 15 refi.
AD- 236 206.
Order from LC mi$2. 70, phK 80 PB 147 045
The liquid- solid phase equilibria for the two binary
systems Li, Na/COo and LI, K/COo and the tenary
system Li, Na, K/d03 are reported. In the Li,
NB/CO3 system it appears that the compound LlNaCOs
melts incongruently at 500. 1°C at about 51 mol-%
Li2C03 and the eutectlc mixture at 500OC and 52
mol-%Li2C03. A compound, LIKCO3, congruenlly
melting at 504. 50C, and two eutectic mixtures at 42. 7
and 62. 0 mol-% Li2C03 melting at 498° and 4880C
respectively were found in the Li, K/CO3 system.
The ternary system is found to have one eutectic
mixture, melting at 3970C and of composition 43. 5,
31. 5, and 25. 0 moI-% LijCOj, NajCOg and KjOO,,
respectively. The values for the melting points aria
heats of fusion found in this investigation were 726°,
858°, 8980C and 10. 8. 10. 3, and 8. 5 kcal/mol for
Li2C03, Na2C03 and KjCOj, respectively. (Author)
Research Labs, for the Engineering Sciences, U. of
Virginia, Charlottesville.
IONIZATION YIELD OF LOW-ENERGY HEAVY ICWS
IN ARGON, by J. A. Phipps. L. C. Tow le and
R. A. Lowry. Rept. on Coniraa AF 49(638)22.
Oct 60, 20p. 6 refs. Rept. no. EP-4419-105-60U;
AFOSR-TN-60-1241; AD- 247 075.
Order from LC ml$2. 40, ph$3. 30 PB 153 356
A cylindrical ionization chamber with a differentially
pumped open window has been used to m2asure the
total ionization yield of low energy heavy ions stopped
in a gas. The ionization yield of protons in argon in
the energy range of 25 to 250 kev was determined
earlier. Recent results are presented on the ioniza-
tion yield of argon and nitrogen ions in argon gas in
the energy range of 25 to 100 kev. The average energy
per ion pair few argon ions increases rapidly with de-
creasing energy in the above range and at 50 kev it is
about three times the value for 200 kev protons. A
comparison of the ionization yields in argon of various
ions having velocities in the same region is presented.
(Author)
410
Stanford Research Inst. , Menlo Park, Calif.
ENERGIES OF THE GASEOUS ALKAUNE EARTH
HAUDES, by Daniel Cubicciotti. Technical note no. 7
on Contract AF 49(638)89. Nov 60, 6p. 10 refs.
SRI ProJ. 2024; AFOSR-TN-60- 1362; AD-247 244.
Order fromLC mi$ 1.80. ph$ 1.80 PB 153 314
EARTH SCIENCES
Alaska U. . College.
RESEARCH AND REPORTS ON AERIAL INTERPRE-
TATION OF TERRESTRIAL BIOENVIRONMENTS
AND FAUNA L POPULATIONS, by John L. Buckley and.
Wilbur L. Libby. Dec 57, 113p. 30 refs. AAL Tech-
inlcalrept. 57-32.
Order from LC mi$6.00, ph$18.30 PB 153 371
A study area of 91,445 square miles in Interior Alaska
was selected and 1 , 923 sample points were located on
serial photographs. The environmental type at each
point was identified from low altitude in a hght air-
craft. Of the points visited, 66.61 per cent fell in
Forest; 7. 28 per cent in Tall Brush; 13.47 per cent in
Dwarf Brush; 7. 12 per cent in Herb types; 2.76 per
cent in water; and 2.76 per cent on bare ground. These
major types were further subdivided and the percent-
age of each computed; a description of each type is in-
cluded. Annotated lists of the mammals, birds and
flshea of the study area were compiled, based on field
work of a four-man crew and on Uterature records.
Tables showing the environmental types in which each
of the mammals, birds, and the important species of
edible plants can be expected are included. (Author)
Dartmoudi Coll. , Hanover, N. H.
FIELD AND LABORATORY INVESTIGATIONS OF
LAKE, SHELF AND GLACIAL ICE, by J. B. Lyons.
Final rept. for 1957-1959 on Contract AF 19(604)2159.
1 Jan 60, lOp. 9 refs. AFCRC-TR-60-205.
Order from LC mi$l. 80, ph$l. 80 PB 153 480
This is a summary report covering a field investiga-
tion of perennially frozen Angiussaq Lake, Northwest
&eenland, as a possible year-round laixling site;
field investigations on T-3, with the objective of re-
lating surface geon^orphology and ablation character-
istics to the problem of stabilization of runways; and
investigations, at Lake Peters, Alaska, 00 the
strength characteristics of melting lake ice. (Author)
Pennsylvania State U. Mineral Industries Experiment
Station, University Park.
MODEL STUDIES OF SEISMIC ENERGY DISTRl-
mnw AROUND DIFFERENT TYPES OF SOURCE.
Qwrterly rept. no. 1 on Contract AF 19(604)7383.
30 Nov 60, 6p. AD-247 381
Ottter from LC mi$I. 80, ph$l. 80 PB 153 422
The purpose of these experiments is to compare,
through the use of models, the seismic pulses to tie
expected around different types of energy sources such
•I a fault displacement or an explosion. All experi-
ments are two-dimensional in character, structure
being simulated by variations in the thickness or
composition of the model. One objective of this in-
vestigation is to duplicate actual source conditions for
earthquakes as accurately as possible in order to
check whether assumed theoretical conditions for
which mathematical theory has been developed are
confirmed. (Author)
Climatology end Meteorology
Air Force Cambridge Research Laba., Bedford,
Mass.
PROGRESS AND PROSPECTS OF RADAR METEOR-
OLOGY, by David Atlas. Guenter Loeser Memorial
Lecture. 1957, 39p. GRD TN-60-63L
Order from LC mi$3. 00, ph$6. 30 PB 153 394
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
SOME CONTRIBUTIONS OF SMALL MAMMAL BIO-
CLIMATE STUDIES TO AIR FORCE NEEDS IN
NORTHERN REGIONS, by WiUiam O. Pruitt, Jr.,
Charles V. Lucier, and L. L. Hufman. [1956] 25p.
10 refs. Technical note AAL-TN-56-8.
Order from LC mi$2.70, ph$4.80 PB 153 514
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
ACCURACY OF TWO-THEODOUTE PILOT BALLOON
TRACKING METHOD OF MEASURING LOW-LEVEL
WINDS, by Ralph W. Armstrong. 22 June 59. 71p.
4 refs. USASRDL Technical rept. 2047. AD- 219 319.
Order from LC mi$4.50. ph$l2.30 PB 150 705
An investigation of the maximum error to be expected
in low-level wind-velocity measurements by the two-
theodolite balloon -tracking method was made, assum-
ing a maximum value for the theodolite angle errors
and that the error in time interval between theodolite
readings and in length of the base line can be made neg-
ligible. Results are presented chiefly in the form of
balloon horizontal displacement errors between theod-
olite readings (as a function of balloon position with re-
spect to the theodolite base line), since these displace-
ment errors can be divided by any selected time inter-
val between readings to give error in measured wind
velocity. (Author)
California U. , Los Angeles.
ANALYTICAL STUDIES OF NUMERICAL ERRORS
IN DYNAMICAL WEATHER PREMCTIOl, by
V^. Lawrence Gates. Final rept. for 1 July 58-
31 Oct 60 on Contracts AF 19(604)3886 and 4965.
31 Oct 60, 53p. 3 refs. AFCRL-TR-60-412.
Order from LC mi$3.60, ph$9. 30 PB 153 204
Contents:
The reduction of the oscillation phenomena (weak in-
stabiUty) of first -forward-then-centered time differ-
ences by a special starting procedure
The reduction erf truncation error by extrapolation '
techniques
The distortion of baroclinic inataUllty criteria by
finite differences
411
QilcagoU. fnt]
DESIGN OF A THUEE- DIMENSIONAL MESO-
METEOROLOGICAL NETWORK, by Tetsuya Fu]iw
and Henry A. ftrown. Quarterly technical rept. no. 4.
1 Jan- 30 Apr 60. oit Contract DA 36-039- sc-78901.
ri960l 132p. AD-242 802.
Order from LC mif6. 90. ph$21. 30 PB 153 232
Results at case stxidles of manerous networks in vari-
ous locations are oomblned In a discussion d the
observations necessary for the operation <rf a three-
dimensional mesoriieteorological network. Pour
obaervatlonal categories are considered: (1) surface,
(2) upper air. (3) tadar. and (4) photography. Each
category is discus led in terms of the elements
measured, optimum time and space resolution, accu-
racy required, and techniques for analysis. A model
network design Incorporating the above results is then
proposed. This Isi followed by a proposed practical
design for three different areas in the UScharac-
terized by coastalj plains, and mountainous environ-
ments. (Author)
Cornell U. MediUl ColL , New York.
MEASUREMENT OF THE RADIANT HEAT LOAD
ON MAN IN SUMMER AND WINTER ALASKAN
CLIMATES, by James D. Hardy and Alice M- Stoll.
Special rept. Novi53. 46p. 14 refs.
Order from LC mi$3. 30. ph$7. 80 PB 153 324
Radiant environmtotal temperature was observed to
range from >5I°G (♦■1240F) in summer to -19°C
(-IIOPP) in wlntei}. Heat load on man due to thermal
radiation is important, being equivalent to adding
10-20°C to thermometer (air temperature) reading in
summer and subtracting a similar amount in winter.
Climatic chambers used for testing field equipment
should be arranged to take into account these differ-
ences. Large changes in environmental radiant tem-
perature (10-40°C) occur that are not registered by
any presently used meteorological instruments. These
changes can be cdrrelated with alterations in water
vapor content and' air temperature o* the upper at-
mosphere. The radiant temperature may thus be use-
ful in studies of viteather. fAuthor>
Danish MeteoroU>gical ftist. , Charloctenlund.
INVESTIGATIONS ON THE DURATION OF SJN-
SHINE IN GREENLAND BY OPERATING 11 (ELEVEN)
SUNSHINE STATIONS, UTILIZING CAMPBELL-
STX)KES RECORDERS. FURTHER: MEASUREMENTS
OF SUNSHINE INTENSITY AT (PROVISIONALLY)
ONE SINGLE STATION IN GREENLAND, by Karl
Andersen. Final flechnical rept. for 1 Oct 59-
30 Sep 60 on Contract DA 91-591-EUC-1216.
31 Oct 60, 3p. I
Order from LCnt$ 1.8a ph$ 1.80 PB 153 093
Dllnois S»te witer Survey. Urbana.
STUDY ON INTENSITY OF SURFACE PRECIPI-
TATION USING RADAR INSTRUMENTATION, by
E. A. Mueller ail G. E. Stout. CMrterly technical
r«)t no. 9, 1 Ajr-30 June 60, on Contract DA
36-039-SC-75055. [1960] I9p. AD- 244 324.
Order from LC .^l$2. 40. ph$3. 30 PB 153 239
A toul dt 34 roll* d raindrop camera flbn was re-
ceived from the firee overseas installations during
the quarter. The Majuro installation was dismantled
and returned June 3. 1960. to Dllnois for refurbishing
and reinstallation. Operations at the other locations -
IndonesU and Alaska - were satisfactory during the
quarter. A tocal of 27 rolls of raindrop data film was
measured during the quarter. The preliminary calcu-
lation of the radar variables was accomplished as the
film was measured. A paper for the 187th National
Meeting of the American Meteorological Society at
Ei^ene, Oregon, was prepared. Both CPS-9 and
TPS- 10 radars were in routine operation during the
quarter. The CPS-9 was operated a total of 616 hrs.
No major maintenance difficulties were experienced
with either radar. (Author)
Intermountain Weather. Inc. . Salt Lake City. Utah.
CALCULATION OF INFRARED RADIATIVE FLUX
EMISSION OF THE EARTH PLUS ATMOSPHERE AT
VARIOUS LEVELS HIGH ABOVE THE EARTH, by
J. Vern Hales, Thomaa L. WiUiama, and Donald
Henderson. Final rept. on Contract AF 19(604)2418.
Aug 60. 65p. 21 refa. AFCRL-TR-60-406.
Order from LC ml$3. 90, ph$ia 80 PB 153 634
This work has proceeded in four phases: (I) CalcuU-
tion of the infrared radiative flux emission of the earth
plua atmosphere at a level sufficiently high that all
radiative gases are below the point of calculation, but
stiU so low that the earth is for aU practical purposes
an infinite plain below the point of calculation. (2)
CalcuUtion erf the infrared radiative flux emission of
the earth plus atmoaphere at various altitudes so high
that the sphericity of the earth becomes an imponant
consideration in the calculation. (3) Inasmuch as the
radiative flux calculations are extremely laborious
an effort has been made to reduce them to standard
procedures for manual operation or for calculation
using high speed computers, with the result that they
now can be accomplished quickly and almost auto-
matically as far as human labor is concerned. (4) In
orxler to check the accuracy of the Elsasser (1960)
charts being used and to permit the calculation of the
infrared radiative flux emission in various portions
of the Infrared spectrum, a technique has been de-
veloped of calculatli^ and using new radiation charts
developed for specific spectrum Intervals.
Lockheed Aircraft Corp. . Sunnyvale, Calif.
ATMOSPHERIC OZONE: ITS DETECTION, MEAS-
UREMENT AND EFFECTS, 1940 TO 1959. AN AN-
NOTATED BIBLIOGRAPHY, by A. A. Beltran.
I July 60, 63p. 154 refs. SRB-60-3; AD-241 588.
Order from LC mi$3. 90. ph$10. 80 PB 153 437
The sources consulted include the card catalog of the
Armed Forces Technical Information Agency, the vari-
ous catalogs of LMSD's Technical Information Center.
Meteorological Abstracts and Bibliography, Science
Abstracts, Section A - Physics, ASTIA Technical Ab-
stract Bulletin, and University of Pittsburgh, Scientiflc
Reprot No. 1 - The Spectra and Chemical Kinetics of
the Upper Atmosphere, A Literature Survej^ Vols. I
to VI. (Author)
412
MoGlU U. (Canada).
THE ARCTIC QRCULATION. A PRELIMINARY RE-
VIEW, by F. Kenneth Hare and S. Orvig. Supplement
to Final rept. on Contracts AF 19(604)1141 and
AF 19(604)1868. 30 June 58, 232p. 129 refs. Arctic
Meteorology Research Group Pub. in Meteorology
ao. 12; AFCRC TN-58-486.
Ordfcr from LC mi$10. 20. ph$36. 30 PB l50 723
This report is a review of the climatology of the
northern atmospheric circulation from sea -level up to
30 km. The treatment is mainly descriptive, and
makes no attempt to be a study bearing on the general
circulation problems at large.
Texas A. and M. Coll. , College Station.
WIND FIELD NEAR THE TROPOPAUSE. by
W.J. Saucier . K . C . Brundidge and others . Final
rept. on Contract AF 19(604)1565. Dec 58. 147P.
62 refs. Reference 58-26F; AFCRC-TR-59-222;
AD-2II4%.
Order from LCmi$7. 20, ph$22. 80 PB 150691
This rept. includes:
Summary of wind distrt^tlons In the jet streams of
southeast United Statesjlnvestigated by project jet
stream, by W . I. Saucier.
Clear-air turbulence and bumpiness , by Iver Dugstad.
A study of the duration of clear-air turbulence near
the jet stream and its relation to horizontal tempera-
ture gradients . by N . W . Cunningham .
Some new jet stream models , by K. C. Brundidge and
J. L. Goldman.
A further study of jet stream turbulence, by Tommy
E . Sanford .
Willow Run Labs. . U. of Michigan, Ann Arbor.
SCINTILLATION AND VISUAL RESOLUTION OVER
THE GROUND, by Frank R. Bellaire and Floyd C.
Elder. Rept. on Proj. Michigan. Contract DA 36-039-
sc-78801. Oct 60. 51p. 20 refs. Rept. no. 2900-
134'T; AD-245 118.
Order from LC mi$3. 60. ph$9. 30 PB 152 682
The scintillation, or the fluctuation in the intensity, of
the light from a constant target source, affects visual
resolution and therefore reduces the usefulness of
optical devices. The deterioration of visual resolution
due to scintillation can be caused by atmospheric con-
ditions near the ground and the character of the under -
lylnS ground surface. An experimental study is being
conduaed to determine the meteorological conditions
and other contributing factors which are significant in
producing scintillation and thereby reducing visual
resolution. In order to limit the number of variables,
the experiment has been carried out over level terrain
with a uniform ground cover and under relatively uni-
form weather conditions. Scintillation appears to be
primarily a function of the vertical temperature
gradient and the vertical motions within the ground
layers of the atmosphere. These faaors are inter-
related and are, furthermore, complicated funaions of
other meteorological parameters, the experimental
arrangement, and the character and roughness of the
ground surface. (Author)
Wisconsin U. , Madison.
LINEAR PREDICTION OF UPPER WINDS AFTER
STRATIFICATION, by Donald R. Johnson and Reid A.
Bryson. Scientific rept. no. 3 on Contract
AF 19(604)5191. May 60, 45p. 12 refs. AFCRC-
TN-60-467.
Order from LC ml$3. 30, ph$7. 80 PB 153 607
This study represents an initial inquiry Into the accu-
racy with which upper winds may be forecast using
simple stratification methods. Non- stratified climatic
prediction of the 300 mb winds over southern European
Russia was compared with non -stratified linear pre-
diction using upper winds at selected areas as pre-
dictors. After stratification of the data by groups of
Gross wetter types, stratified cllmatological forecasts
and stratified linear prediction were compared with
the initial results of no stratification. For the
methods used in this study we can conclude that while
the stratification used here does not give a better
cllmatological forecast, It does improve the results of
linear prediction. (Author)
Oc6anograph)f
Dartmouth ColL , Hanover, N. H-
UMNOLOGICAL STUDIES ON LAKES PETERS AND
SCHRADER, ALASKA, by John E. Hobble. Scientific
rept. #5 for July- Aug 58 on Contract AF 19(604)2159.
1 Mar 60, 53p. 33 refs. AFCRC- TN-60- 261;
AD- 234 481.
Order from LC mi$3. 60, ph$9. 30 PB 153 481
Umnologlcal studies of two Alaskan Arctic lakes are
presented which are located on the north slope of the
Brooks Range. (Author)
New York U. Coll. of Engineering, N. Y.
OPERATING PROCEDURES FOR COMPUTING ZERO '
AND ORDINATE CROSSINGS OF STATIONARY
GAUSSIAN NOISE USING AN IBM 650 CALCULATOR,
by Raymond G. Stevens. Technical rept. no. 2 on Con-
tract NC*s -72018. Aug 59. 26p. 4 refs. AD- 231 464.
Order from LC mi$2. 70, ph$4. 80 PB 150 060
The operation of a group of computer programs for
calculating estimates of U>e zero crossing distribution
of a random sutionary process is described. These
programs were developed and used for the calculation
of zero crossing distributions of ocean wave records.
For this purpose a comparison erf various methods of
zero crossing estimation was undertaken. While some
methods are obviously superior to others the entire
group of programs is included ao that similar comparl
sons can be undertaken if desired. The scope is lim-
ited to a description of the computer program opera-
tion, but a brief outline of the technique is included.
(Author)
Woods Hole OceanograpWc Institution, Mass.
BEACH STUDIES IN THE CAPE 000 AREA, by John
M. 2>lgler. Final rept. for Aug 53-Apr 60 on Con- .
tract Nonr- 1254(00). Apr 6a 73p. 23 refs. Reference
60-2a AD-236 811.
Order from LC mi$4. 5a ph$l2. 30 PB 147 311
413
C«pe Cod beaches become steep and full in summer
and are quite variible at other times. Variations in
beach eleratlon can be extreme. Sediment sampling
alcNV offshore profUes concludes that the deposition d
■edimeni Is confintd to a thin strip of sand next to the
coast and a mud r<)ne far offshore. These are sepa-
rated by a zone c* eroeion or non -deposition.
Woods Hole Oceanographic Institution. Mass.
OCEANOGRAPHlC DATA FROM ATLANTIS CRUISE
247. JANUARY-JUNE. 1959 FOR THE INTER-
NATIONAL GEOPHYSICAL YEAR OF 1957-58. by
Arthur R. Miller. Technical rept. on Contract Nonr-
2196(00) and National Science Foundation Grant
Y/9.5/80. Mar 6a 143p. 9 refs. Ref. no. 60-40;
AD-244 957. |
Order from LC xA%l. 20. ph$22. 80 PB 153 762
ProfUes of tempeijature. salinity, and oxygen and the
accompanying dati for sections accompUshed during
Cruise 247 of the Research Vessel ATLANTIS are re-
poned. Data frort shallow water off the mouth of the
Rio de la Plata an^ from ten other stations are also
included. Profile^ of density (sigma t) are included,
and approximate!^ 2400 bathythermograph slides are
reproduced. (Author)
ithoi
Woods Itole Oceanographic Institution. Mass.
PROCEEDINGS OT THE CONFERENCE ON AUTO-
MATIC DATA HANDLING FOR OCEANOGRAPHIC
OBSERVATIONS, WOODS HOLE, MASSACHUSETTS,
OCTOBER 8, ANP 9. 1959. Technical rept. on Con-
tract Nonr-2734<d0X Feb 60. 16p. 3 refs. Ref. no.
60-10; AD- 233 434. « ,eo .o^
Order from LC n|l$2. 40. ph$3. 30 PB 153 134
A conference wa^ convened to discuss the application
of automatic data handling techniques to oceanographic
observations. THe participants had Indicated either a
need for, or had particular interest in a truly flexible
and economical i»eans for the acquisition, recording
and reduction of » relatively large number of channels
of data. The WH()I data handling system was described
in some detail. The advantages of this and similar
type systems were discussed according to some of the
particular requixjements of the conferees. The areas
of discussion ar^ as follows: (1) a generalized de-
scription of data acquisition, storage, reduction and
analysis; (2) description of WHOI system: (3) inter-
range Instrumentation group sttndards, (4) extended
applications of \*HOI or similar systems; (5) data
acquis itioo over long time periods; and (6) sundardl-
zation. (Author)
Physics ol the Atmosphere
Cornell U . Sch »1 of Electrical Engineering , Ithaca ,
STUDIES ON PROPAGATION IN THE IONOSPHERE,
by H. G. Bookerl, D. Parley and J. Renau. Final rept.
on Contract DA i6-039-sc-78258. 30 Oct 59, 278p. 149
refs . Research ^-ept . EE 433. « . c« /«•
Order from LCtni$U. 10. ph$42. 60 PB 150 071
The theoretical investigation of electrostatic fields in
the ionosphere was completed. It was concluded that,
under certain conditions , significant electrostatic cou-
pling between the E and F regions of the ionosphere can
occur at all latitudes. However, the small scale elec-
trostatic fields created by irreguUr winds below 200
km are likely to be rather weak. It appears unlikely
that the strength, in the F region, of the irregular elec-
tric field could exceed 10"^ v/m. The possibility that
this electric field might create irregularities of elec-
tron density in the F region was examined. It was found
that irregularities could not be created near the geo-
magnetic poles, but that rather weak irregularities
(deviations of a per cent or two) might be formed at
loweu latitudes . A historical review of scatter echoes
is presented and the problems to be considered are
summarized. The types of frequently observed spread
echoes are illustrated and described. An explanation it
given for sporadic echoes . Frequently observed equa-
torial spread echoes can be explained on the basis of
backscaitered echoes from all directions . In a nrxjr-
phological study of spread echoes it Is shown that types
of spread echoes commonly observed In the northern
stations consist of supeiposltlon of overhead and ob-
lique specular reflections . The same type of spread
can be caused by the bifurcation of the F layer.
(Author)
Georgia U . Athens.
SPECTROGRAPHIC DATA OBTAINED FROM SO-
DIUM AND CESIUM CLOUDS IN THE UPPER AT-
MOSPHERE (I). SPECTRA OF ARGON OXIDE.
KRYPTON OXIDE AND XENON OXIDE (11). by
C. Dewey Cooper. Final rept. on Contract
AF 19(604)1562. 1 1 Dec 59, 34p. 21 refs. AFCRC
TR-59-[405) AD-231 895.
Order from LC mi$3. 00, ph$6. 30 PB 150 721
Spectrographlc evidence is provided for the resonant
scattering of sunlight by a sodium cloud which was
placed in the upper atmosphere at twilight. The rela-
tive intensity of the 5893A and 3303A sodium lines
provides conclusive results that the sodium twilight
flash results from resonant scattering of sunlight. In
similar experiments, cesium clouds radiate resonant
lines at 8525A, 4593A, 4555A. 3876A. and 3611 A.
When traces of ootygen are added to 1 atm of Ar, Kr,
or Xe and each mixture is excited in a discharge tube,
characteristic spectra appear near the 5577A
(ISfj - ^Dc) line. These spectra are associated with
rare -gas oxygen molecules which may be formed with
oxygen in the ^Sq or IDq «ate. Many of the rotational
lines of these bands were resolved, but the overlap-
ping of bands prevented a complete rotational analysis.
(Author)
Included in the report are:
3303 A emission from sodium ejected into the upper
atmosphere, by C. Dewey Cooper, pub. in the Jnl. of
Geophysical Research 63: 369-371. June 58
Spectra of argon, oxygen, and nitrogen mixtures, by
C. Dewey Cooper, pub. in the Physical Review 109:
2026-2028. IS Mar 58-
414
Ionosphere Research Lab. .Pennsylvania Sute U. ,
University Park.
IONOSPHERIC EFFECTS OF SOLAR FLARES.
11: IONIZATION MODELS, by A. P. Mitra. Scientific
rept no. 142 on Ionospheric Research, Contract
AF 19(604)3875. 1 Dec 60. 54p. 24 refs. AFCRL-TN-
60-691; AD-246 308.
Order from LC mi$3.60, ph$9.30 PB 153 197
(iirrent theories of flare ionization are reviewed with
particular consideration of Ld^and hard X-rays .
Models of flare produced ionization are then deduced
with reference to various height levels in the lower
ionosphere, constituents ionized and solar flare radi-
ations effective. Agreement with other workers is
reached with regards to very low height ionization
enhancements as being due, primarily, to hard
X-rays . Evidence Is given for a flash of LdL near the
start of a flare as being most effective near the base
of the E- layer. (Author)
Lincoln Lab. , Mass. Inst, of Tfech. , Lexington.
THE DISTRIBUTION OF ELECTRONS IN THE
UPPER IONOSPHERE FROM BACKSCATTER
OBSERVATIONS, by J. V. Evans. Rept. on Contract
AF 19(604)7400. 23 Nov 60. 21p. 44 refs. 3G-0002.
Order from LC mi$2. 70, ph$4. 80 PB 153 484
This report summarizes the methods by which infor-
mation has been obtained concerning the distribution «f
electrons above the level at the critical frequency of
the F2 region. Profiles of the electron density obtained
from rocket firings and by other techniques are com-
pared with some of the results obtained by PIneo et al
from observations of ionospheric backscatter at Mill-
stone Hill. It Is found that most methods yield prof iles
in which the electron density diminishes only as
rapidly or less rapidly than that in a Chapman region.
TTie results obtained by Plneo, however, always indi-
cate a more rapid decay than predicted by the Chap-
man theory. There is also a discrepancy between the
profiles obtained by Pineo et al when the telescope Is
(a) In the zenith, and (b) at an elevation of 15°. The
deoslty measurements do not agree for the region be-
ycod 400 Kms height. It is not yet possible to say if
the difference reported here, between the results of
backscatter experiments and the results of other
workers, reflects real changes in the shape of this
region which may be a function of time or latitude.
(Author)
MacDonald Physics Lab. . McGlll U. (Canada).
ON THE MEASUREMENT OF CLOUD TEMPERA-
TURES FROM THE GROUND BY INFRA-RED RADI-
ATION , by Walter Hitschfeld . Rept . on Contract
AF 19(604)2065. Oct 60. Up. 4 refs. Stormy
Weather Research Group Technical note MWT-4;
AFCRL TN-60-670; AD-246 048.
Order from LC mi$2.40. ph$3.30 PB 153 061
Systematic photographic observations have become
imponant means of studying the mechanisms involved
in cloud development . especially In cumulus . It Is
felt that these techniques could be augmented easily by
cloud temperature measurements , based on the infra-
red emission from the cloud drops . This note is a
discussion of a few such measurements , using a Golay
cell and a chopped beam.
National Bureau of Standards, Boulder, Colo.
A SURVEY OF SPREAD-F, by F. N. Glover. Nov 60,
72p. 109 refs. Technical note no. 82.
Order from OTS %l. 75 PB 161 583
Examples of spread- F forms occurring at different
latitudes are presented, illustrating the classification
of spread into range type and frequency type. The oc-
currence patterns of spread-F at different latitudes
are correlated with other geophysical phenomena.
Magnetic latitude and time within tfie suns pot cycle
appreciably affect the pattern of spread occurrence.
Instrumental techniques and their advantages for
spread studies are outlined. The principal theoretical
explanations of spread-F are summarized. A single
mechanism need not be postulated as responsible for
all types of spread occurrence or at all latitudes.
(Author)
Ohio State U. Research Foundation, Columbus.
INFRARED ABSORPTION BY MINOR ATMOSPHERIC
CONSTITUENTS, by Darrell E. Burch and [Xidley
Williams. Scientific rept. no. 1 on Contract
AF 19(604)2633. Aug 60. 158p. 24 refs. RF ProJ. 778;
AFCRL TN-60-674.
Order frtwn LC mi%l. 50, ph$24. 30 PB 153 283
The work has dealt with the infrared absorption of the
minor atmospheric gases nitrous oxide, carbon mon-
oxide, and methane. Samples consisting of these gases
alone and in binary mixtures with nitrogen have been
investigated over wide ranges of absorber concentra-
tion ^ and total pressure P. From the observed ab-
sorption for each band, it has been possible to present
curves showing total absorption J"A(w)di/ for various
values of absorber concentration as a function of equiv-
alent pressure Pg. which is a parameter that includes
the total pressure P and a small additional term pro-
portional to the partial pressure of the absorbing gas;
the magnitude of the additiotial term is also dependent
on the value of a "self -broadening coefficient. " defined
in the report and measured experimentally for each
absorption band. Another set of curves for each band
shows the total absorption for various equivalent pres-
sures as a function of absorber concentration. The
curves provide a basis for the prediction o* total ab-
sorption for any values of h and Pe Included in the
wide range of these parameters covered in the study.
Extensive tables included at the end of the report pro-
vide additional aj^rption data for use by other inves-
tigators who may be interested in atmospheric trans-
mission or in mbre general problems of absorption.
•ft
(Author)
Ohio State U. Research Foundation, Columbus.
INFRARED STUtHES OF THE ATMOSPHERE,
1954-1957, by J. H. Shaw, D. E. Burch and others .
Final rept. on dantract AF 19(604)1003. Jan 58, 81p.
85 refs. AFCRC-TR- 58-233; AD-152 546.
Order from LC mi$4.80. phH3.80 PB 150 697
This report released for sale to the public 9 Feb 61 .
The results of a 3-year program of investigating the at-
mosphere and atnxjspheric gases by Infrared techniques
are described. Studies have been conducted on the vari-
ations In abundance of atmospheric CO and of the abun-
dance of N20.at ground level. High- resolution spectra
415
I. 03.
of bands of CO2. O3. N2O. NO, C0H2 «nd NH3 have
been analyied. Measurements at the growth of single
lines of CO have >een made, and investigations of the
emission spectrum of the earth's atmosphere in the re-
gion ^to 2:^ and erf the spectrum of Mars in the PbS
region have been Undertaken .
Included In the re|)ort are:
The emission spectrum of the earth's atmosphere from
4^to 22n.. pub. In M^moires Soc. R. Lidge 18:42-47
Infrared evidence! for the presence of ozone in the
lower atmosphere, pub . in Jnl . of the Optical Society
of America 46:360-361, May 56
Thermal radiatiot from the atmosphere, pub. in Jnl.
of the Optical S^iety of Artierica 46:543-547, July 56
Absorption bands of N2O near 4.5n, pub. in The Jnl.
of Chemical Physics 23:1887-1888. Oct 55
Nitric oxide fundamental, pub. in The Jnl. of Chemical
Physics 24:399-402, Feb 56
Infrared emissioa spectra of the atmosphere between
I4.i<and 22.5»», pub. in Jnl. of the Optical Society
of America 47:227-229, Mar 57
Some comments on two articles by Taylor and Yates ,
pub. in Jnl. of the Optical Society of America
47:441, May 57
Combination baMv/^'iU, of acetylene , pub . in The Jnl .
of Chemical Physics 25:607, Sep 56
Infrared spectnjin and nxjlecular constants of carbon
dioxide. Part li y^of C^H:)2^^ sli I5u. Part II.
Levels lOOQ an^l OTOQ. lOol and 02oi couoled by
Fermi resonance , pub . In The Jnl . of Chemical
Physics 24:103-105, 1007-1008, 1956
Infrared emissior spectrum of the atmosphere, pub. in
Jnl. of the Optical Society of America 45:455-460,
June 55.
lylvania u! School at Medicine, Riiladelphia.
RADIANT TEMTCRATURE OF THE SKY AT HIGH
ALTITUDE, by g. T. Hammel. Special rept. Dec 54,
5p, 2rela. AAL, proj. no. 7-7951.
Order from LC fii$l. 80. ph$l. 80 PB 153 334
To obtain nwre fvidence upon the question of die mini-
mum radiant tei»perature erf the sky in the complete
absence at a water shield, the present study to meas-
ure the radiaM temperature at high altitude was
undertaken.
ENGINEERING
Aeronautical Engineering
Aeronautical llurbine Lab. , Naval Air Turbine Test
Station, Trent<^, N. J.
DETERMINATION OF CAUSES OF ENGINE FAIL-
URES INCURRED IN SERVICE OPERATION OF
F3H-2N AIRCRAFT. PHASE VII. OPERATING CHAR-
ACTERISTICS OF pi TURBOJET ENGINES WITH
WATER INGESTION AND UNDER IQNG CONDI-
TIONS. PART 4. EVALUATION OF Am-MCING
CHARACTERISTICS, by A. Kuah. Rept. on ProJ.
TED-ATTS-RAtP-2007. 1: Sep 60, 37p. 5 refa.
NATTS-ATL-47; AD- 246 410.
Order from LC mi$3.00, ph$6.30 PB 153 289
Airborne Instruments Lab. , Deer Park, N. Y.
AIRPORT RUNWAY AND TAXIWAY DESIGN: EX-
CERPTS ON TYHCAL CONFIGURATIONS, CAPAQ-
TIES, EVALUATION OF DESIGN, by M. A. Warskow.
H P. Galliher and others. Rept . on Contract
FAA/BRD-136. July 60. 188p. 11 refs. Repc.
no. 7601 -H-1. _
Order from OTS $3.00 PB 171 370
Airport operations at numerous civil airports have
been observed and measured. The data have been
analyzed to identify the elements important to airport
capacity and that cause delay to operations, and to
identify and evaluate aircraft spacing intervals. A
particularly interesting result of the field observatlOM
was the ability to document the so-called "pressure
factor "--that factor that evidences itself in higher
efficiency at higher operating rates. Controllers and
pilots, sensitive to the tempo o* the operation, reduct
the spacings and reaa more promptly to traffic con-
trol. Thus, as the airport operating rate increases,
the delay build-up is less pronounced than the in-
crease in the operating rate would indicate. It has
been found useful to study airports by analyzing the
delay to operations that results from various move-
ment rates rather than maximum capacity ratings
since, from a practical standpoint, operations at
maximum capacity are not observable. The multiplic-
ity of airport designs around the country have been
examined to determine which are typical. The mathe-
matical formulas developed have been applied to air-
pOTt configurations to determine which are typical and
will best satisfy general airport needs. A guide for
the application of the mathematical formulas is
provided that indicates how the operational elenfents
are selected and how compuutions axe made.
Bell Helicopter Corp. . Fort Worth Tot.
WADC RAPID PERFORMANCE PREDICTION
METHOD FOR COMPOUND TYPE ROTOCRAFT, by
Roben D. Foster. Rept. for May 55 -Oct 56 on Con-
tract AP 33(616)2895. Mar 59. 159p. 10 refs. WADC
Technical rept. 55 -4ia. AD- no 606.
Order from LC mi$7. 50, ph$24. 30 PB 154 406
This report released for sale to the public 16 Feb 61.
A method for rapid estimation of the flight performance
of compound type rotorcraft is developed. This method
makes extensive use of nomograms to avoid lengthy
computations. The method is based on familiar heli-
copter theory modified to include the effect at inter-
action between wings and rotors. A method for de-
termining the distribution of the load between the wln|
and rotot is developed and included as an integral part
of the method. Provision is also made for including
the effects of auxiliary power, or thrust, which may
be available in forward flight. Provisions are made
for calcuUting rate of climb, both venical and maxi-
mum, and rotor limited forward speed. The charts
are particularly useful for rapid assessment of new
designs, and in estimating the effect of varying design
parameters of both new and existing designs. Only
standard parameters are used. Sample calculations
for different types of rotorcraft are given. (Author)
416
Courtney and Co. . Philadelphia, pa.
HUMAN FACTORS CONSIDERATIONS IN THE DE-
9CN OF AIRPORT TRAFFIC CONTROL QUARTERS,
by Anthony W. Silvestro. John B. Kelly, and Douglas
Courtney. Interim rept. no. 2 on Preliminary Engl -
■eering Layouts, Contract FAA/BRD-89. 1 June 59,
TOp. Rept. no. 27.
Order from LC ml$3. 90, ph$10. 80 PB 150 920
Tber« are five Important assumptions underlying the
presentation of this report. Assumption (1) is that this
report is a human factors report as opposed to an engi
neerli^ repon. Assumption (2) is that the human fac-
tors considerations have been met by a fully nrKxlular
design. Assumption (3) is that we are preparing a de-
itfB in terms of a Clasa I airport. Assumption (4) Is
diat these recommendations cannot be considered flnal
until they have been placed in some simulated form.
Assumption (5) concerns the relation of these recom-
mendations to current and future TSOs. (Technical
Standard Orders) One of the basic reasons for carry-
ii^ out this project was to bring to current and hence
future TSO's full consideration of the human operator,
tt the same time incorporating the extensive experi-
ence and background that has led to the formulation of
the current TSOs. In order to establish a sensible
and acceptable compromise between equipment and
eiyineering requirements and the requirements at the
human operator.
Ei^neering Div. , Air [Materiel] Command [Wright -
Patterson AFB] C»uo.
CONFERENCES WITH M. HENRI COANDA IN PARIS.
FRANCE, by Carl E. Reichert. Memo. rept.
IS Mar 46, declassified 21 Dec 51, 13p. Serial no.
TSEAC4 -44621 -5-1; ATI-152 755.
Order frxwn LC ml$2. 40, ph$3. 30 PB 154 292
This report released for sale to the public 14 Feb 61.
Hlller Aircraft Corp. , Palo Alto, Calif.
VTOL DOWNWASH IMPINGMENT STUDY, VELOCITY
SURVEY, by A. Morse. Rept. on Contraa DA 44-177-
tc-500. Aug 60. 91p. 87 refs. Hiller rept. no. 60-15;
TRBC Technical rept. 60-58; AD-246 306.
Order from LC mi$5. 40, ph$15. 30 PB 153 083
b preparation for evaluating the effects and hazards of
operating VTOL aircraft from non- surfaced landing
areas, velocity surveys and flow pattern studies c4 an
air Jet impinging on a flat non-eroding surface were
conducted. A mobile test rig, mounting either a five-
foot diameter propeller, producing disk loadings of
1.73 Ib/sq ft to 7.7 Ib/sq ft, or a two- foot diameter
ducted fan, producing disk loadings of 15 Ib/sq ft to
145 Ib/sq ft, at height to diameter ratios from one
quarter to four and thrust angle inclinations of 0, 30
■ad 60 degrees, was used. Pltot and venturl tubes
measured velocities abova the surface from the Jet
centerline to 16 radii. Tuft boards indicated flow pat-
tttM. The ratio of the surface dynamic pressure to
the mean dua exit dynamic pressure was found to be
Independent of disk loading, and to be a maximum
■pproxlmately one diameter from the impingement
polM. For duct exit heights greater than six tenths of
the diameter the maximum surface dynamic pressure
Is approximately equal to the maximum dynamic pres-
sure that would be found in the same plane providing
no impingement surface was present. If the dua exit
is brought progressively closer to the ground plane
the surface dynamic pressure Increases more rapidly
than the Jet decay would indicate. At a height to
diameter ratio of 0. 25 the surface dynamic pressure
Is twenty-five percent greater than the maximum Jet
decay dynamic pressure. (Author)
Institute of Transportation and Traffic Engineering,
U. of California. Berkeley.
EXIT TAXIWAY LOCATIONS, by R. Horonjeff,
R. R. Read and G. Ahlborn. Rept. on Contract
FAA/BRD-4. Sep 60. 24p. 5 refs.
Order from OTS $0. 75 PB 171 369
Based on landing performance, the transport aircraft
types using the nation's airports are grouped into 3
classes. If the arriving aircraft are made up of all 3
classes of aircraft, the exit locations are virtually
independent of the proportion of each class to the
whole. The number of exits required depends on the
aircraft population. The location of an exit taxi way
need not be fixed at a specific disunce from runway
threshold because a certain amount of variation does .
not affect the acceptance rates a great deal. The moat
desirable exit taxiway locations for runway acceptance
for the 3 classes erf aircraft at sea level are: large
turbo jet transports, 5, 800-b, 000 ft. ; four-engine
propeller -driven transports and twin-engine turbo-jet
transports. 4,000-4, 200 ft. ; twin-engine propeller -
driven transports and the larger twin-engine general
aviation aircraft, 2. 600-2. 800 ft.
Lockheed Aircraft Corp. , Sunnyvale, Calif.
HEAT SINKS: MATERIALS, comp. by Maureen
Pearcy. Special bibliography for 1949-1960.
17 Aug 60, 32p. 88 refs. SB-60-29; AD-244 262.
Order from OTS $1.00 • PB 171 372
These 88 bibliographical references are concerned
with thermal conductivities of materials for heat sink
systems in spac^ and re-entry vehicles. TTie period
covered is 1949-1960. The materials include n)etala,
liquid metals, alloys, metal compounds, semicon-
ductors, ceramic materials, plastics, carbon, and
gases. Char aaeri sties studied are thermal and elec-
trical conductivities, IR photoconductivity, magnetic
and thermodynamic propertiea, and crystal structure.
References are also included for apparatus to meas-
ure thermal conductivity, thermal expansion, and
specific heat of metals, ceramics, and
semiconductors .
Lockheed Aircraft Corp. . Sunnyvale, Calif.
A STUDY OF CAUBRATION PROCEDURES FOR
HYPERSONIC, HIGH-TEMPeIiaTURE WIND TUN-
NELS, by S. E. NeiceandR. W. Rutowskl. Technical
note on Flight Sciences. July 60, 18p. 9 refs. LMSD-
703047; AD- 241 909.
Order from LC mi$2.40, ph$3.30 PB 153 435
Procedures for calibrating hypersonic, high-tempera-
ture wind tunnels, using measured reservoir and
stagnation- point quantities, along with a MoUier dia-
gram for equilibrium air, are described- The proce-
dures are espeoially applicable to spark-heated and
.417
reflected shock tvmnels. Three methods are consid-
ered for the estalilishment of the equilibrium state of
the reservcrtr and, stagnation region through the use of
different combinations of measured pressure, density,
•od heat transfer rates. The determination of the free
■Cr«am propertied, corresponding to the established
reservoir and stagnation conditions, is demonstrated
Certain simplifying asBumptions applicable to low-
denslty flows and wind tunnels employing very large
expansiooB to lowj free stream temperatures are
dlscuased. (Author)
Michigan U. Research Inst. , Ann Arbor.
AN EXTENDED EULER ANGLE COORDINATE SYS-
TEM FOR USE WITH ALL-ATTITUDE AIRCRAFT
SIMULATORS, b^ D. T. Greenwood. Rept. on Training
Equipment SimuKtors and Techniques for Air Force
Systems, Contract AF 33(616)5664. Aug 60, 30p.
Srefs. WADD Technical rep«. 60-372.
Order from OTS KO. 75 « i71 404
This report considers the problem dl finding a suitable
coordinate systefn for representing orientation. The
new extended Eu|er angle system is compared with
other coordinate systems (ordinary Euler angle sys-
tem, reversed EUler angle system, and quaternion
system), particularly with respea to the output varia-
bles and the amount of analog computer equipment re-
quired for aimul^tor representation. The extended
Euler angle system requires the most equipment but
has the advantage of being an all-attitude system with
outputs convenietJt for cockpit display. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
EFFECTS OF j|t-ENG1NE EXHAUST ON VIRGINIA
DIABASE CONCllETE PAVEMENT, by H. Tomita.
Final rept. 14"Nbv 60, 20p. 2 ref s . Technical rept.
R-089; AD- 246 389.
Order from LCJni$2. 40. ph$3. 30 PB 153 178
In coordination ilth a National Bureau of Standards'
study on the ref factory qualities of concrete, NCEL
conducted a stucfy to determine the resistance of
Virginia diabase) concrete to thermal shock from jet
aircraft operatic^ns . In simulated field tests , concrete
slabs and beams) were subjected to the exhaust of a jet
engine. The slabs spalled during the afterburner power
level of the firs< exposure cycle, with recorded surface
temperatures ofj900to 1000 degrees Fahrenheit. Sub-
sequent exposures resulted in no additional spalling .
The 6- inch by 64 inch by 24- inch beams showed no
spalling du/ing ihree cycles of exposure but suffered
reduction in fle:fural and compressive strengths. The
Virginia diabasd concrete did not possess the
necessary refrafctory qualities and flexural strength re-
quirements . Itsjuse is not recommended for jet air-
craft full -power* test areas . It is recommended that
simulated field <ests be conducted on small concrete
slabs and beam^ before a concrete is designated for
areas which wilj be subjected to severe jet-engine ex-
haust conditions!. (Author)
Naval Ordnance Test Station, China Lake, Calif.
ROCKET SLED TEST OF THE NA 39 SEAT-EJEC-
TION SYSTEM, by BUI Moore. 1 July 60, 184p. NOTS
TP 2536: NAVWEPS rept. 7566.
Order from LC mi$8. 40, ph»28. 80 PB 153 404
The purpose of these tests was to make a functional
checkout of the NA 39 escape system using Martin-
Baker seats, and to determine if the escape system is
adequate for safe recovery within the airplane per-
formance envelope. These tests proved that with
minor modificationa. the NA 39 escape system is ca-
pable of safe recovery within its perfonnance envelope
(Author)
Ohio State U. Research Foundation, Columbus.
EVALUATION OF BRAZED HONEYCOMB STRUC-
TURES, by Robert C McMaster, Anthony T.
D'Annessa and Henry W. Babel. Rept. for Jan 59-
May 60 on The Chemistry and Physics c< Materials,
Contraa AF 33(616)6364. Sep 60. 32lp. 53 refs.
WAIXD Technical rept. 60-393.
Order from OTS $5. 00 FB 171 408
A study was made of commercially-available nonde-
structive test methods for the evaluation of brazed
honeycomb structures. Surface- layer discontinuities
In bonding were deteaed reUably by X-ray, ultrasonic;
and thermal gradient tests. Internal discontinuities
were detectable only with penetrating radiation tests.
X-ray test methods evaluated Included: film radiog-
raphy, xeroradlography, direct fluoroscope, televi-
sion fluoroscopic systems, clear ostatic and photocon-
ductive- screen X-ray image amplifiers. Ultrasonic
test methods studied included: Immersion ultrasonic
tests with focussed transducers, contact ultrasonic
tests with resonance transducers, and contact ultra-
sonic tests with pulse -reflealon systems. Thermal
test methods evaluated included: thermal-flash proof
tests, tests with heat-repelled fluid coatings, tests
with thermographic phosphor coatings, test with color-
changing paint coatings, and tests with remote infra-
red sensing systems. Results of destructive tests oo
honeycomb parts confirm indications of bond condi-
tions of X-ray, ultrasonic, and thermal tests. Further
research and development are recommended for
xeroradlography, phoioconductive- screen television
systems, and thermal-gradient tests. (Author)
Princeton U. , N. J.
A REVIEW OF THE WING- SLIPSTREAM PROBLa*
WITH EXPERIMENTS ON A WING SPANNING A
CIRCULAR JET, by Frank W. Gobetz. Rept. on Coo-
tract Nonr- 18.58(14). Jan 60. 116p. 11 refs. Aero-
nautical Engineering rept. no. 489; AD- 233 722.
Order from LC ml$6. 00. ph$18. 30 PB 152 873
An attempt was made to examine and evaluate all
previous studies whose purpose was to investigate the
increase in lift of a wing Immersed In a slipstream.
Each oT the theoretical analyses is discussed to some
extent and the limited available experimental data are
compared with the theories. The experiments con-
ducted are described and the dau compared with what
Is considered to be the most promising otf the theoreti-
cal analyses. The correlation between the present d«B
418
tnd die theory formulated by Rethorst Is quite good and
indicates that at least some d the trends predicted are
correct. The appendix describes the integrating ma-
nometer which was designed for and employed in the
experimental program. (Author)
Princeton U. , N. J.
SYMPOSRJM ON GROUND EFFECT PHENOMENA,
A COMPILATION OF THE PAPERS PRESENTED
OCTOBER 21-23, 1959. Oct 59. 400p. 107 refs.
AD- 235 210.
Order from LC ml$ll. 10, phJ60. 60 PB 150 075
Rocketdyne [Canoga Park, Calif. )
SUMMARY REPORT FOR THE DESIGN OF AN ION
ROCKET RESEARCH DEVICE, by C. R. Dulgeroff and
D. J. Kerrisk. Rept. for 1 Jan 59-29 Feb 60 on Con-
traa AF 33(616)5972. Oa 60, 53p. 3 refs. Rept.
R-2241: ARL Technical rept. 60-290.
Order from LC ml$3.60, ph$9.30 PB 152 319
A bell jar vacuum system and a vacuum chamber used
for research on high current density ion souices are
described. Porous samples of nickel, graphite, tung-
sten, tantalum, and titanium carbide were tested for
ability to produce cesium ions by surface ionization.
Nickel and graphite were inadequate because erf reac-
tions with cesium vapor. Tungsten, tantalum, and
titanium carbide produced positive ions. Tungsten
produced current densities up to 12 ma/cm^, and has
ionization efficiency greater than 90 percent. Second -
try elearon emission studies wefe made to ensure
true current measurements. An analytical study of
arc type ion sources was made to determine types best
suited for high current density ion beams. (Author)
Sperry Gyroscope Co. , Great Neck, N. Y.
GYROTRON DEVELOPMENT (INCLUDING OPERA-
TION AND MAINTENANCE INSTRUCTIONS ON XG5
EXPERIMENTAL MODEL). Final er^neering rept.
on phase I, Contract NOa(s) 8846. Apr 49, declassi-
fied. 94p. 1 ref. Sperry rept. 5226-1129.
Order from LC mi$5. 40, ph$15. 30 PB 154 298
This repon released for sale to the public 10 Feb 61.
This report describes a new type of gyroscopic in-
strument - the Gyrotron. It gives the principle of
operation as well as a detailed mechanical description
of tbt Instnmient and a circuit description of its asso-
ciated amplifiers. Preliminary test results are listed
tnd various avenues for future research are dis-
cussed. Since the instrument is so radically different
from other gyroscopic instruments, chapters are also
included on its Installation, operation, and malnte -
nance. In two appendices, the discussion of some of
the considerations and problems concerned with the
Gyrotron is supplemented by mathematical analyses
tnd a description of balancing problems.
Vehicle Research Corp. , Pasadena, Calif.
DEVELOPMENT OF METHODS FOR PREDICTING
V/STOL AIRCRAFT CHARACTERISTICS, by Scott
Rethorst, W. W. Royce, and others. Final rept.
Phase 1 on Contract Nonr- 3099(00). 15 Apr 60, 199p.
10 refs. VRC rept. no. 5; AD- 244 736.
Order from LC ml$ 8.70, ph$ 30. 30 PB 150 742
This study contains analyses which enable a prediction
of optimum V/STOL performance characteristics . The
results of these analyses have been presented graphi-
cally to facilitate evaluation and to enable determination
of fruitful areas of development of V/STOL aircraft .
The charts produced have been cast in terms of load-
ings and dimensionless performance parameters so as
to broaden their applicability and generality. These
charts thus permit the evaluation, relative rating, and
estimation of performance trade-offs of V/STOL air-
craft configurations . In the course of this study, a
unique analysis has been performed which determines
the optimum size actuator disc area for forward
propulsion. It is shown that this area is relatively
small. The analysis also determines the optimum size
actuator disc area for hovering. This area is rela-
tively large. The present study has provided a resolu-
tion of this conflict through the concept of variable ac-
tuator disc area , which varies the propulsive disc area
between the near optimum cases for both hovering and
forward propulsion. The ratio of these disc areas thus
defined has been employed as a significant parameter
to illustrate the areas of major potential performance
improvement, and as a powerful tool for prediction of
the performance characteristics themselves . Analyses
of these considerations are presented in detail. The
performance of two example VTOL airplanes incorpo-
rating variable disc area is included. (Author)
Vought Astronautics Div. . Chance Voug^t Aircraft,
Inc. , Dallas, Tex.
IMPACT DISPERSION STUDY OF THE 609A VE-
HICLES ON THE WHITE SANDS MISSILE RANGE,
by M. L. Bamett and G. Tamower. Rept. on Contraa
AF 29(600)2404. Aug 60, I69p. in 2 v. 6 refs.
AST/EOR- 13081; AFMDC-TR-60-23; AD-245 443.
Order from LC mi$7. 80, ph$25. 80 PB 152 716
An Investigation was conducted of the feasibility of
using 609A vehicles at the White Sands Missile Range.
Range safety requires that all stages of any test ve-
hicle impact on the range. Two one-stage, one two-
stage, and one three -stage vehicles were studied. As
the result of these analyses, the following conclusions
have been reached. With the proper selection of a
guidance system, all of the vehicles studied can be
safely flown at WSMR. Unguided versions of the coo-
figurations studied are not compatible with range
safety requirements and so cannot be flown at WSMR.
The two one -stage vehicles require only a 609A-type
programmed attitude system. The rwo-stage vehicle
is marginal with a 609A-type system, but is satisfac-
tory with a radio cc»nmand or sophisticated inertial
system. The three-stage vehicle requires a radio
command or a sophisticated inertial system. Use of a
simplified programmed attitude system, in conjunction
with a radio command system produces an efficient,
economical, standardized configuration that can be
used all, or in part, as necessary, in all four vehicles
studied, (Author)
419
Civil Engin«ering
Arctic Aerom^cal Lab.. Ladd AFB. Alaska.
SOME STRUCTURAL AND THERMAL CHARACTER -
ISnCS OF SNO^ SffiLTERS, by Robert W. Eisner
and William O. pruin. [1956] 20p. 16 refs. Technical
note AAL-TN-H-U.
Order from LC mi$2. 40, ph$3. 30 PB 153 517
Snow shelters of various types have been described
with a considervion erf their adequacy for travel and
survival in extreme cold. With full utilization of sub-
nivean microcli|nate8 existing in arctic regions shel-
ters can be can|tructed which provide interior tem-
peratures considerably above that of ambient air with-
out artificial heating. Avoidance of the most extreme
ooadltlons o* ar«ic and subarctic climate is thus
possible. A siniple method is described for construa-
Ing snow shelters by artificially compacting loose,
unconsolidated mow. Observations on the thernial and
struaural characteristics of this type at shelter and oi
dome snowblocl^ shelters are discussed. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
SNOW-COMPAOTION EQUIPMENT SNOW DRAGS, by
J. B. Camm. Final repi. 20 Oct 60. 37p. 12 refs.
Technical rept R-109; AD- 246 003.
Order from oris 1.00 PB 171 375
Numerous typei and sizes of drags were tested and
evaluated durin| the development of the Navy's snow-
compaaion tecHniques. As techniques were developed
for constructing akiways, roads and runways on shal-
low and deep snow fields, two types of drags, along
with other special equipment, were found necessary to
produce good-quality compacted snow. A snow-level-
ing drag was naeded in the preliminary stages of con-
struction to levfcl and compact windrows left by other
equipment, to Spread and level shallow drift and light
snowfall, and t* remove slight surface irregularities.
A two-element, 925-pound wooden drag with metal
cutting edges was developed for this work. This sim-
ple drag was eflfeaive at speeds up to 500 feet per
minute and could perform light levebng on compacted
SHOW areas at i rate of 5. 3 acres per hour. The drag
was useful also in maintenance of compaaed-snow
areas and m leveling and spreading new snow and drift
around polar c^mps. Based on 1959 prices, the ap-
proximate cost I of this drag is $500 per unit. A snow-
flnishlng drag ^as needed in the final stage of con-
struaion to obtain a hard, smooth finish on compaaed
snow. Such a finish was necessary for successful
operation of aitcraft, cars, trucks and other wheeled
vehicles on the! compacted surface. A two-element,
2,830-pound steel drag with cyUndrical bonoms was
developed for this work. At a speed of 350 feet per
minute, this dcag could produce a good-quality finish
on 5. 3 acres of compacted snow in an hour provided
the working elements, or skids, were penetrating 1 to
2 inches into tHe surface. The drag was useful also in
ccmpressivelyicompacting and finishing new snowfalls
and drift on co<npaaed-snow areas and around polar
camps. Based
of tMs drag is
on 1959 prices, the approximate cost
H. 500 per unit.
Electrical and Electronic Engineering
Aero Geo Astro Corp. , Alexandria, Va.
RESEARCH ON SCANNING TECHNIQUES FOR
LARGE. FLAT COMMUNICATION ANTENNA
ARRAYS. Final rept. on Contract AF 19(604)5217.
31 Oct 60, 72p. 15 refs. AFCRL-TR-60-364.
Order from LC mi$4.50, ph$l2.30 PB 153 712
The program included both theoretical and experi-
mental projects intended to resolve problems associ-
ated with scanning in two principal planes. The basic
antenna was a large, flat array capable of being used
in the VHF or UHF region. The program stressed the
use of scanning of two-wire transmission line systemi
because of their inherent low cost. Scanning in one
principal plane was concentrated on techniques associ-
ated with two-wire transmission line, while a number
of approaches were considered for scanning in the
other plane. A rotating cam scanner, described in
some detail in this report, was developed for the scan-
ning of the two-wire transmission line, while two ap-
proaches appeared satisfactory for scanning in the
other principle plane. The two approaches considered
were the use of Fox-type phase shifters, that is.
routing phase shifters involving circular polarizaUon
within a transmission- line structure, and a multiple-
beam technique, in which step scanning is achieved by
switching from one beam to its neighbor. A detailed
examination of a novel multiple-beam technique is
offered; this is basically a problem of examining the
characteristics of the transmission- line network feed-
ing the array. It is concluded that a satisfactory low-
cost scanning system could be obtained using the
rotating cam scanner for one principal plane and
either of the other two techniques for the remaining
pUne. (Author) (See also PB 149 059)
American Electronic Labs., Inc.. Mladelphia, Pa.
DESIGN AND DEVELOPMENT OF CRYSTAL VIDEO
DETECTOR HOLDERS^ by Bernard Hainwwitz. Final
rept. for 1 May 57-31 July 58 on Contract DA 36-039-
sc-73259. [1958] 38p.
Order ft-om LC mi$3. 00, ph$6. 30 PB 153 227
The basic mathematics for the crystal is presented.
The reasons for using bias are discussed. The method
of design for the detector mount is presented. Tan-
gential sensitivity data is shown for the five final de-
tector nnounts. Drawings showing outline dimensioni
and weights for these nwunts are given. The selectka
of crystals for these mounts is discussed. (Author)
American Inst, for Research, Pittsburgh, Pa.
TEST MEASUREMENT REQUIREMENTS FOR 196(>«
GROUND ELECTRONIC EQUIPMENT. PHASE I. IW
NEED FOR NEW TYPES OF TEST DEVICES, by
Alan D. Swain. Rept. on Contract AF 30(602)1654.
Mar 58, 71p. 11 refs. A1R-244-58-FR- 177; RADC-Tl
58-22; AD- 148 606. „,e«^
OttlerfromLCmi$4.50, ph$12.30 PB 150 703
A review of prime and test ground electronic equipme*
currently being developed for use in the early 1960$
reveals that most present test measurement practice!
420
will be continued . A study of dau on the use of test
equipment by Air Force Specialty Classification 3- and
5- level maintenance mechanics at nwintenance sites of
the Airways and Air Communications Service shows
many liabilities in present test equipment. Unless
(ome substantial changes are made in current plans for
early I960 test equipment, these liabilities will prob-
ably continue. The following current difficulties are
anticipated. Test devices have limitations in operabil-
ity. Test devices frequently present information that
ii not immediately compatible with the maintenance ac-
tion required. There is also ample evidence of low
transferability of skill in the operation of different test
sets at a site, even though the sets may perform the
lame maintenance function. Tliere is also suggestive
evidence that one of the reasons that the 5-level me-
chanic does little fault location is because of the com-
plexities in using present test equipment for that pur-
pose. The following criteria were proposed for the so-
lution of the test measurement problem: (1) All test
measurement requirements expected in 1960-62 will be
accounted for. (2) There will be the smallest total num-
ber of different kinds of test equipment . (3) Items of
test equipment will have functional adapability permit-
ting the maintenance mechanic to fjerform with it those
operations that normally are done together. (4) Test
equipment "shells" will be human engineered for opti-
mal operabllity. (5) Information presented by the test
equipment will be compatible with the way the nuiinte-
oaoce mechanic will have to use the information.
(Author)
Antenna Lab. , Calif. Inst, of Tech. , Pasadena.
RADIATION FROM AN ELECTRIC DIPOLE IN AN
ANISOTROPIC COLD PLASMA, by Hans H.<i^uehl.
Technical rept. no. 24 on Contract AF 18(6(»)1113.
Oct 60, 57p. 13 refs. AFOSR-TN-60-1169; AD-246496
Older from LC ml$3. 60. ph$9. 30 PB 153 224
The general expression for the far-zone dyadic Green's
function in an anisotropic medium is presented. The
radiation erf an electric dipole in a cold plasma in con-
sidered. Expressions for the far -zone radiation from
• dipole for the case of weak magnetic field and low
planna density are derived. Expressions are also ob-
tained for the case of an infinite magnetic field.
(Author)
Army Signal Research and Development Lab. . Fort
Monmouth. N. J.
CASCODE DISTRIBUTED AMPLIFIER, by Clement A
Sktlaki. 1 May 59. 34p. 3 refs. USASRDL Technical
rept. 2043; AD-217 545.
Order from LC ml$3.00. ph$6. 30 PB ISO 704
thti use of triodes in cascode permits extremely wide-
knd amplification . A cascode amplifier, which em-
fkjrs 2C39A triodes as the active element, was con-
Sruaed and tested. Once the performance of this type
of active element is ascertained, the method of em-
|l0)ring the active element in a practical distributed
■■pllfier can be determined. A general procedure for
■yflthesizing constant resistance grid lines for dis-
tributed amplifiers employing cascode or pentode
•Oive elements is presented. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
COMPACT, Hiai POWER, COAXIAL DIRECTICWAL
COUPLER, by Robert D. Standley. 8 May 59, 15p.
2 refs. USASRDL Technical rept. 2041; AD- 218 970.
Order ft-om LCml$2. 40, ph$3. 30 PB 152 998
The directional coupler covered by this report was
designed to be used as a power monitoring device with
Radio Relay Set AN/MRC-71. A compact and rugged
component was developed by coupling a coaxial line to
a strip transmission line. The coupling was approxi-
mately 62.5 db and the directivity exceeded 16 db
over the required frequency range. Design procedures
are outlined. (Author)
Army Signal Research and Development Lab. . Fort
Monmouth. N. J.
A NEW SEMICONDUCTOR MICROWAVE MODULA-
TOR, by H. Jacobs, F. A. Brand and others. 16 May 6Q
28p. 9 refs. USASRDL Technical rept . 2114;
AD- 244 549.
Order from LC mi$2.70. ph$4.80 PB 153 001
Experiments have been conducted in which a semicon-
ductor rod of germanium is Inserted in a waveguide
parallel to the direction of the electric field. Upon ex-
[x>sure to light or the injection of minority current
carriers by means of a p-n junction, the conductivity
of the semiconductor is changed. The changes in con-
ductivity, in turn, cause variations in the absorption
of microwave energy. TTiis effect has been designed
into a device that c^ers the possibility of microwave
amplitude modulation. Experiments conducted at 9600
megacycles indicate llnle or no phase and frequency
modulation. Performance data and design information
relating to the role of the semiconduCTor lifetime, the
effects of various types of trapping centers, and other
electrical properties are described. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
PULSE SYSTEM THEORY APPLICATIONS II, by Kurt
Ikraih. 1 Mar 60. 73p. 2 refs. USASRDL Technical
rept. 2099; AD-246 075.
Order frtmi LC mi$4 50. ph$l2. 30 PB 153 000
The wave shapes of pulse train responses of various
filter networks under different operating conditions are
accurately formulated on the basis of mathematical
methods which are documented in USASEL Technical
Memorandum M- 1922 of Oct. 1957 entitled Pulse Sys-
tem Theory. A quantlutlve insight into the shortcom-
ings of ordinary Laplace Transform and Founer
Transform approach to pulse systems problems is
given on the basis of numerical examples whose prac-
tical implications are discussed. (Author)
Army Signal Research and Development Lab. , Pen
Monmouth, N. J
THE USE OF A NONLINEAR DEVICE IN THE
FEEDBACK LOOT OF AN EXPONENTIAL DELTA
MODULATOR, by H. Wolf. 25 July 60, I4p. 2 refs.
USASRDL Technical rept. 2141; AD-245 853.
Order from LCmi$2. 40, ph$3. 30 PB 153 004
421
Some experiment^ with exponential delta modulation
circuitry are disoissed. The results of the experi-
ments show that tie quality d ordinary exponential
delta modulation ijor speech can be improved by the
application of a n<)nlinear device in the feedback loop.
(Author)
Ballistic Research Labs . , Aberdeen Proving Ground.
THE DYNAMIC gHARACTERISTlGS OF PHASE-LOCK
RECEIVERS, by Keats A. Pallen, Jr. Jan 60, 74p.
34 refs . ARPA Satellite Fence Series no. 8 in the
series; Rept. no.; 1093; AD- 235 010.
OTderfromLCrr4$4.50, ph$12.30 PB 150 066
t
The characteristics required of a phase-lock tracking
receiver under adverse reception conditions are ana-
lyzed. It is shown that for constant sensitivity of the
phase-lock circuits , the use of a cross-correlation-
type AVC circuit is essential. It is also shown that
either the use of Extensive degeneration in the IF cir-
cuits or the use c^ common channels is essential for
minimizing phasej errors . The transfer characteristic
required for optirtium tracking characteristics is de-
rived, and a possible method of obtaining it described.
Several recomme»xJations on effective utilization are
made, and several problems requiring further study
are outlined. (Aiihor)
Ballistic Researjch Labs . , Aberdeen Proving Ground,
Md.
PARAMETRIC PRE-AMPUFIER RESULTS, by
K. H. Patterson.: Rept. no. 19 on ARPA Satellite
Fence Series . oit 60, 7p. BRL Technical note
no. 1354. AD- 24^ 550
Order from LCrfi$l. 80, ph$ 1.80 PB 153 494
The DOPLOC system is a special type of CW radar
operating at 108 U: . Developed specifically for the
quick detection of passive satellites it can, with one
transmitter and ^ne receiver, establish orbital paran>
eters immediately after a single pass . To achieve
maximum range linusually sensitive receiving equip-
ment is necessatkr. This requirement places consider
able emphasis on the noise- performance of the
DOPLOC receivers. Parametric pre- amplifiers , with
exceptional noisej figures , have been checked, both in
the laboratory ard in the field. A resume of the ex-
perience gained I rom these tests is presented .
(Author)
Boeing Airplane Co. , Seattle, Wash.
HEAT PROTECTIVE ABLATIVE COATINGS FOR
RADOMES. by J.J F. Cavanaugh and J. P. Sterry Rept
for July 59 -May do on Thermionic and Solid State Elec-
tronic Technologt, Contract AF 33(616)6683. Aug 60,
85p. WADDTecliiical rept. 60-507.
Order from OTS »2. 25 PB 171 416
An analysis was jnade of the thermally induced stresses
in a bare and coated alumina radome. The study indi-
cated that it would be structurally feasible to protect a
radome on an adronced interceptor agamst thermal
shock by using a^ ablative covering. Materials were
tested to determiie the effect of material thermal con-
ductivity upon hefct input rate to a ceramic radome.
An alumina radome was coated with a silicon carbide
filled phenol silane impregnated graphite cloth and
tested in a ramjet exhaust. (Author)
Bolt, Beranek and Newman. Inc. . Cambridge, Mass.
EQUIVALENT NETWORKS, by Richard D. Thomtoa
Scientific rept. no. 2 on Contract AF 19(604)7290.
23 Nov 60, 24p. Rept. no. 780; AFCRL-TN-60-1115;
AD-246 510.
Order from LC mi$2. 70. ph$4 80 PB 153 175
The question under consideration is how to find a sim-
plest electrical network equivalent to a desired net-
work. Four approaches are discussed: State-of-the-
art, exhaustive search, important special cases, and
considerations of network constraints. (Author)
Bureau of Naval Weapons, Washington, D. C
A. F. SIGNAL GENERATOR SG-21/U AND SG-
21A/U. BuWeps-BuShips Calibration Program.
12 Aug 60. lip. Secondary Standards Lab. Instrument
Calibration Procedure AG -51.
Order from OTS $0. 50 PB 171 243
The Test Instrument is a precision audio frequency
signal source which delivers signals of any of 26 fixed
frequencies between 10 and 500 cps. The frequencies
are generated by a rotating disc -photocell arrangemea
driven by a tunii^ fork stabilized oscillator.
Bureau of Naval Weapons, Washington, D. C
AUDIO FREQUENCY IMPEDANCE MEASURING
EQUIPMENT OJ-1, OJ-2, OJ-3 AND GENERAL RAEW
650A. BuWeps-BuShips Calibration Program. 25 Julyfift
33p. Secondary Standards Lab. Instrument Calibration
Procechire AZ-09.
Order from OTS $1.00 PB 171 245
Bureau erf Naval Weapons, Washington. D. C
CAPACITORS. FDCED: GENERAL RADIO 505 SERBS
BuWeps-BuShips Calibration Program. 14 Sep 60, 23p.
Secondary Standards Lab. Instrument Calibration Pro-
cedure AC-05 (Revision 1), Supersedes ICP 1252.
23 Jan 59. „^
Order from OTS $0. 75 PB 171 239
This procedure describes the calibration of General
Radio fixed capacitors. 505 series. The basic callbrt-
tion method utilized in this procedure is the compari-
son of the Test Instrument to the precision capacitor
or the standard decade capacitor, which has been pre-
viously certified to known values.
Bureau of Naval Weapons, Washington, D. C
GENERATOR. TIME MARK, TEKTRONDC 180A.
BuWeps-BuShips Calibration Program. 18 Aug 60. \W
Secondary Standards Lab. Instrument Calibration Pro-
cedure AG -47.
Order from GTS $0. 50 PB 171 241
This procedure describes the calibration of the Tektrtr
nix 180A Time Mark Generator. The Test Instrument
422
consists of a precision I mc crystal oscillator, plire
frequency dividing and multiplying systems. The fre-
quency dividing system produces marker pulses with
various spaclngs, which may be selected separately or
superimposed to form a timing comb, as well as ac-
curate trigger pulses which may be used to synchro -
nlie oscilloscope displays. The multiplying system
provides fixed -frequency sine wave output signals.
Bureau of Naval Weapons, Washington, D. C.
HETERODYNE FREQUENCY METERS 125 KC TO
20,000 KC BuWeps-BuShips Calibration Program.
17 Aug 60, 17p. Secondary Standards Lab. Instnmient
Calibration Procedure AF-21.
Order from OTS $0. 50 PB 171 240
This procedure describes the calibration of a related
gnup of heterodyne frequency meters, a partial list of
wfaidi Is given below.
Nomenclature
BC-221
SCR-2I1
Models
-A, B, C. D, E. F, J, K,
L, M. N, O. P. orQ
-C, D. F. J. K. L. M, N.
O, P. R, T. AA, AC. AF,
AG, AH, AJ, or AL
TS-164/AR (Identical to SCR-211-AC)
Bureau of Naval Weapons, Washington, D. C
MICROWAVE ATTENUATION, H -BAND (7.05 TO
10.00 KMC) 0 TO 50 DB. BuWeps-BuShlps Calibration
Program. 28 June 60, 24p. 1 ref. Secondary Standards
Lab. Measurement System Operation Procedure HA -07.
Order from OTS $0. 75 PB 171 228
TWb procedure describes the operation of a secondary
standards laboratory calibration system which Is used
to calibrate H-band microwave attenuators of wave-
guide size 5/8" X 1-1/4" (outside dimensions). Fre-
quencies of 7. 05, 9. 0, and 10. 0 KMc are used for cali-
bration in this procedure. If other calibration frequen-
cies are required, substitute as applicable. This sjrs-
tem utilizes the audio substitution method for attenu-
ator calibration in which audio attenuation is substl-
nited for RF attenuation. A constant audio output Is
maintained with the Test Instrument first removed and
then Inserted into the nUcrowave line.
Bureau of Naval Weapons, Washington, D. C
MICROWAVE ATTENUATION, J -BAND (5.85 TO
8.20 KMCPS) 0 TO 40 DB. BuWeps -BuShlps Calibra-
tion Program. 18 Dec 59, 23p. Secondary Standards
Lab. Measurement System Operation Procedure HA -03.
Order from OTS $0. 75 PB 171 225
Thla procedure describes the operation of a secondary
■tandards laboratory calibration system which Is used
to calibrate J -band microwave attenuators of wave-
guide size 3/4" X 1 1/2" (outer dimensions). This sys-
tem utilizes the RF substitution method for attenuator
calibration in which a Standard Attenuator Is adjusted
to maintain a constant RF output level with the Test
Instrument first removed and then Inserted Into the
microwave line.
Bureau erf Naval Weapons, Washington, D. C
MICROWAVE ATTENUATION, S-BAND (2.60 TO
3.95 KMCPS) 0 TO 40 DB. BuWeps -BuShlps Calibra-
tion Program. 25 Feb 60. 35p. Secondary Standards
Lab. Measurement System Operation Procedure HA -05.
Order from OTS $0. 75 PB 171 226
This procedure describes the operation of a secondary
standards laboratory calibration system which Is used
to calibrate S-band microwave attenuators of wave-
guide size 1 1/2" X 3" (outside dimensions). This sys-
tem utilizes the RF substitution method for attenuator
calibration In which a Standard Atteraiator is adjusted
to maintain a consunt RF output level with the Test
Instrument first removed and then Inserted into the
microwave line.
Bureau of Naval Weapons. Washington, D. C.
MICROWAVE ATTENUATION. X-BAND (8.2 TO 12.4
KMCPS) 0 TO 50 DB. BuWeps -BuShips Calibration
Program. 18 Dec 59, 23p. Secondary Standards Lab.
Measurement System Operation Procedure HA -01;
Supersedes MSOP 1851. 29 Aug 58.
Order from OTS $0. 75 PB 171 224
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to calibrate X-band microwave attenuators of wave-
guide size 1/2" X 1" (outside dimensions). This sys-
tem utilizes the RF substitution method for attenuator
calibration in which a Standard Attenuator is adjusted
to maintain a constant RF output level with the Test
Instrument first removed and then inserted into the
microwave line.
Bureau of Naval Weapons, Washington. D. C.
MICROWAVE ATTENUATION, X-BAND (8.20 TO
12.40 KMC) 0 TO 50 DB. BuWeps -BuShips Calibration
Program. 24 June 60, 25p. 1 ref. Secondary Standards
Lab. Measurement System Operation Procedure HA -06.
Order from OTS $0. 75 PB 171 227
This procedure describes the operation of a secondary
standards laboratory calibration system which Is used
to calibrate X-band microwave attenuators of wave-
guide size 1/2" X 1" (outside dimensions). Frequen-
cies of 8. 2, 9. 0, and 10. 0 KMc are used for calibra-
tion in this procedure. If other calibration frequencies
are required, substitute as applicable. This system
utilizes the audio substitution method for attenuator
calibration In which audio attenuation Is substituted for
RF attenuation to maintain a constant audio output with
the Test Instrument first removed and then Inserted
Into the microwave line.
Bureau of Naval Weapons, Washington. D. C.
MICROWAVE FREQUENCY. G-BAND (3.95 TO 5. 85
KMCPS) ±0.0002% 1" X 2" WAVEGUIDE SIZE. BuWeps
BuShips Calibration Program. 18 Dec 59. 25p. Sec-
ondary Standards Lab. Measurement System Operation
Procedure HF-06.
Order from OTS $0. 75 PB 171 231
This procedure describes the operation of a secondary
standards laboratory calibration system which Is used
423
to calibrate G-baiid microwave frequency meters of
waveguide size l"''x 2" (outside dimensions). This pro-
cedure normally Applies to the calibration of Test In-
struments with accuracies better than 0. 04%.
Bureau at Naval
MICROWAVE P
KMCPS) 1" X 2"
Calibration Progr
ards Lab. Measu
HF-04.
Order from OTS
Weapons, Washington, D. C
:QUENCY. G-BAND (3. 95 to 5j85
'AVECUIDE SIZE. BuWeps -BuShips
im. 3 Sep 59, 19p. Secondary Stand -
;ment System Operation Procedure
PB 171 229
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to calibrate G-baiid microwave frequency meters of
waveguide size I'ix 2" (outside dimensions). This pro
cedure normally allies to the calibration of G-band
frequency meters pf accuracies not better than 0. 04%.
Bureau of Naval Weapons, Washington, D. C.
MICROWAVE FREQUENCY, J-BAND (5.85 TO 8. 20
KMCPS)t 0. 0002% 1 1/2- x 3/4" WAVEGUIDE SIZE.
BuWeps -BuShips Qalibration Program. 18 Dec 59, 26p.
Secondary Sundarids Lab. Measurement System Opera -
tion Procedure HFl-05.
Order from OTS $|D. 75 PB 171 230
de^i
This procedure de^ribes the operation of a secondary
standards laboratory calibration system which is used
to calibrate J-banq microwave frequency meters of
waveguide size 1 li/2" x 3/4' (outside dimensions).
This procedure normally applies to the calibration of
Test Instruments With accuracies better than 0. 04%.
Bureau of Naval Veapons, Washington, D. C
MICROWAVE FREQUENCY, S-BAND(2. 60 TO 3.95
KMCPS) ±0. 0002%, 1 L/2" x 3" WAVEGUIDE SIZE.
BuWeps -BuShips Gplibration Program. 7 Mar 60, 22p.
Secondary Standartls Lab. Measurement System Op-
eration Procedure IHF -07.
Order from OTS $f). 75 PB 171 232
Tills procedure de^ribes the operation of a secondary
standards laboratc^y calibration system which is used
to calibrate S-bai
waveguide size 1
the system descril
calibrated by visi
quency with a
a dual -trace Osci
microwave frequency meters of
2" X 3" (outside dimensions). With
herein, the Test Instrument is
Uy comparing its resonant fre-
n harmonic ctf a stable oscillator on
•scope.
Bureau of Naval Weapons, Washington, D. C
R. F. SIGNAL GEIWERATOR SET AN/URM-26 OR
AN/URM-26B. BuWeps -BuShips Calibration Program.
6 July 60, 32p. Secondary Standards Lab. Instrumeiu
Calibration Procedlire GG-06.
Order from OTS $(.00 PB 171 246
irain
Bureau of Naval
SIGNAL GENERATXDR
Calibration Prog
Standards Lab
AG-52.
Order from OTS $0. 75
\^eapons, Washington, D. C
AN/GPM-15. BuWeps -BuShips
12 Aug 60, 2lp. Secondary
Instrument Calibration Procedure
PB 171 244
This procedure describes the calibration of the
AN/GiPM-15 Signal Generator Test Set which consists
of the SG34/GPM-15 Signal Generator, transit case,
and accessory cables. The -only item normally requir-
ing calibration is the SG34/Q>M-15 Signal Generator.
Bureau of Naval Weapons, Washington, D. C.
TEST OSCILLATOR SET AN/PRM-10. BuWeps-
BuShips Calibration Program. 8 Aug 60, 2lp. Second-
ary Staixlards Lab. Instrument Calibration Procedure
AF-48.
Order from OTS $0. 75 PB 171 242
Bureau of Naval Weapons, Washington, D. C
VOLTAGE STANDING WAVE RATIO, J-BAND (5. 85
TO 8. 20 KMCPS) 1.00:1 TO 1ft 1. BuWeps -BuShips
Calibration Program. 18 Dec 59, 17p. Secondary
Standards Lab. Measurement System Operation Pro-
cedure HV-02.
Order from OTS $0. 50 PB 171 233
This procedure describes the operation of a secondary
sundards laboratory calibration system which is used
to measure the voluge standing wave ratio of J -band
instruments of 3/4" x 1 1/2" waveguide size (outside
dimensions). This procedure utilizes the slotted line
technique for the measurement of voltage standing
wave ratio.
Bureau of Naval Weapons, Washington, D. C.
VOLTAGE STANDING WAVE RATIO, S-BAND (2. 60
TO 3.95 KMC) 1.0ft I TO 1ft I. BuWeps -BuShips Cal-
ibration Program. 25 Feb 60, I6p. Secondary Stand-
ards Lab. Measurement System Operation Procedure
HV-04.
Order from OTS %0. 50 PB 171 234
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to measure the voltage standing wave ratio of S-band
instruments of 1 1/2" x 3" waveguide size (outside di-
mensions). This procedure utilizes the slotted line
technique for the measurement of voltage standing
wave ratio. The Klystron and associated cavity used
herein covers the frequency range from 2. 4 to 3. 60
KMc. If suitable sig^nal sources become available, the
frequency range can be extended to 3. 95 KMc.
Bureau of Naval Weapons, Washington, D. C
VOLTAGE STANDING WAVE R/tTlO 3/8" COAXIAL,
TYPE N CONNECTOR (100 TO 1000 MC). BuWeps-
BuShips Calibration Program. 22 Aug 60, 18p. Sec-
ondary Standards Lab. Measurement System Operation
Procedure HV-06.
Order from OTS $0. 50 PB 171 235
This procedure describes the operation of a secondary
standards laboratory calibration system which is used
to measure the voltage standing wave ratio of 3/8 inch
coaxial instruments having type N connectors, and in
the frequency range from 100 Mc to 1000 Mc. Stngle-
ended instruments such as signal generators and ter-
minations or double-ended instruments such as atten-
uators, directional couplers, or filters having a VSWR
up to 1ft 1 can be calibrated with this system. This
424
procedure utilizes the PRD type 219 standing wave de-
tector in conjunction with a square-wave modulated RF
gtopal source, standing wave indicator, and associated
ccmponents for measuring voltage standing wave ratio.
CJtllfornia U. , Berkeley.
ELECTRON PHYSICS OF TRAVELING WAVE TUBE
DEVICES, by J. R. Whinnery, \X H. SJoan and others.
Rept. on Research on Physical Phenomena Affecting
the Characteristics of Electronic Components, Con-
tr«:t AF 33(616)6139. July 60. 55p. 10 refs. WADD
1>chnlcal rept. 60-471; AD-246 513.
Order from OTS $1. 50 PB 171 414
Ihe work described includes theoretical and experi-
mental studies on cold-cathode crossed-fleld dfevlces,
electron beams, fast-wave interaction with electron
itreams, solid-state and electron-beam parametric
amplifiers, backward- wave interaction with waves on
• ferrlte rod or in plasmas, large-signal effects in
traveling-wave tubes, and novel fast space-charge
wave devices. (Author)
California U. , Los Angeles.
EXTENSIONS IN THE SYNTHESIS OF THE OPTI-
MAL OR "BANG-BANG" NONLINEAR CONTROL
SYSTEMS. PART II: SYNTHESIS AND ANALYTIC
STUDIES OF OPTIMUM TYPE II NONLINEAR CON-
TROL SYSTEMS, by P. Chandaket and C T. Leondes.
Rept. on Contract AP 49(638)438. June 60, 62p. Dept.
of Engineering rept. no. 60-46; AFOSR-TN-60-960;
AD- 247 424.
Order frt>m LC miS3. 90, ph$10. 80 PB 153 438
Most of the work carried out thus far on the synthesis
of optimum nonlinear control systems of the "bang-
bang" or relay type has concentrated in the main on
systems wherein the controller is of the stationary
type. In this type of system, the controller depends
neither on the input nor on time. This report devel-
ops synthesis techniques for optimum nonlinear con-
trol systems of the quasi -stationary class wherein
the controller configuration depends on a knowledge
of certain information about the input to the system,
(n this way, the class of inputs for which system re -
sponse is optimum is significantly extended. (Author)
Ose Inst, of Tech , Cleveland, Ohio.
ELECTRIC ANISOTROPIC PROPERTIES OF THE
METALLIC-STRIP-TYPE PERIODIC MEDIUM, by
Nicholas J. Kolettls. Scientific rept. no. 17 on Con-
traaAF 19(604)3887. 30 Oct 60, 90p. 12 refs.
APCRL-TN-60-1127. AD-247 425.
Order from LC mi$4. 80, ph$13. 80 PB 153 417
The unbounded metallic strip type artificial dielectric.
•• an Isotropic medium, is reviewed and its electric
anisotropic character pointed out. The analysis uti-
lizes two approaches: First, the medium is analyzed
in terms of modes that propagate normal to the face
of the strips. In the second approach, a formulation
in terms oif modes that propagate parallel with the
face of the strips is employed. An analogy between
the problems for the three dimensional unbounded
•trip medium and a rectangular wav^uide loaded with
ibe medium is drawn. A computational program in
conjunction with an experimental one with typical strip
ipedium samples was undertaken. Theoretical and
experimental results obtained for phase constants and
equivalent relative permittivities justify the theoreti -
cal solutions that were derived.
David Sarnoff Research Center, Princeton, N. J.
PERFORMANCE AND OPERATION OF THE IMAGE
ISOOON CAMERA TUBE, by A. D. Cope and
H. Borkan. Rept. for Apr 59-Aug 60 on Research on the
Quantum Nature of Light, Contract AT 33(616)6497,
continuation of Contract AF 33(616)5728. Apr 60, 27p.
3 refs . WADD Technical note 60-123.
Order form OTS $0.75 FB 171 386
The Image Isocon is a television camera tube which
maintains a high signal nxxiiilation in the preseiKe of
excess scanning beam current. This results in a higher
signal-to-noise ratio and accommodation of a greater
dynamic range of light levels in a scene than can be
achieved with tubes employing orthicon scan. The price
paid for these improvements is a tube which requires
more complex electron optics and procedures of ad-
Justmeru than the image orthicon tube. Once adjusted
Che performance remains stable. Included in this re-
port are typical operating potentials and the camera re-
qjirements for operation of experimental Isocon tubes
beinffdeveloped under this and a related contract.
Daystrom Instrument, Archbald, Pa.
MODIFIED R-F SWTTCH QRC-29 (T), by John Qulnn.
Final engineering rept. on Contraa AF 30(602)1673.
8 Jan 59. 17p. RAIX: TR-59-15; AD-210 118.
Order from LC mi$2. 40, ph$3. 30 PB 150 698
The work was directed toward the development of an
experimental modified model of the Radio Frequency
Switch for a Wullenweber Antenna. The principal
modifications to the original design were concentrated
in an effort to improve the overall frequency response
of the system, and to that extent, the major redesign
was centered around the transformer and rotary cttoke
Joint sections.
\
Diamond Ordnance Fuze Labs. , Washington, D. C
THEORY OF TEM DIODE SWITCHING, by Robert V.
Garver. 20 Oct 60, 56p. 13 refs. TR-874.
Order from LC ml$3. 60, ph$9. 30 PB 153 579
The theory and technique for the design of a broadband
(100-t'o-l frequency range) TEM microwave diode
■witch are presented. A coaxial transmission line
■witch has been constructed that provides 26-db or
greater isolation and insertion loss ranging from
1 . 6 db to less than 1 db from 40 Mc to 4000 Mc. An
analysis is given of the switching action of one and of
two or more diodes as well as the biasing of the center
conductor of a TEM transmission line over broad fre-
quency bandwidths without interacting with the rf sig-
nal. The use of point-contact germanium, varactor,
and gold -bonded germanium diodes for T^M switching
is discussed. Some considerations of switching speed
and maximum power -handling capacity are given.
(Author)
425
Eagle- Picher Co^,,Joplin, Mo.
THE DESIGN AND DEVELOPMENT OF A HIGH AL-
TTTUDE RADIGSQNDE BATTERY, BA-347(XE-2)AJ.
by Georgp O. Archer and Edward P. Brogllo. Final
rept. for 28 May 59-1 June 60 on Contract DA 36-039-
8C-78327. [1960] |b7p. AD- 242 555.
Order from LC ml$3. 90, ph$10. 80 PB 153 231
The BA-347(XE-2i/U has been successfully designed to
operate at 130, 000 foci altitudes. A pressure tight
plastic case was cjesigned and tested. Problem areas,
involved poaitloniag the vent part to prevent freezing
and the selection of a suitable vent valve to operate in
conjunction with t|e battery case. Included in the re-
port are test dataj graphs, charts, and phocographs of
the battery. Asseinbly and detail drawings of parts
unique to this batttry are also appended. (Author)
Electronics Research Lab.,
Boston, Mass.
CAPACITY OF 2
Northeastern U. ,
2. 2-3 And 3-3 CHANNELS, by
Sze-Hou Chang and Eric Reid. Scientific rept. no. 4
on Contract AF 19(604)3053. 27 Sep 60, 77p. II refs.
AFCRL-TN-60- 11102.
Order from LC raiK 50, ph$12. 30 PB 153 722
The algebraic method of Muroga and the geometrical
method al 3iannoq are used to calculate the capacity
at 2-2, 2-3 and 343 channels. The geometrical mean-
ings of certain algebraic quantities are explored. In
particular the process of channel cascading is con-
sidered as a geonetrical mapping. The various ways
of cascading of 2-2, 2-3. 3-3 and 3-3, 3-2, 2-2 chan-
nels are then disoussed together with the decompo-
sition of 2-3 and 3-2 channels. The probabilities of
iiqxit symbols to Realize the theoretical capacity of a
3-3 channel are not always positive. In case negative
probability appeals, one input symixil must be sup-
pressed to realiz^ the actual capacity of the channel.
The condition undtr which this phenomenon occurs is
studied for a special class of 3-3 channels. Finally,
the effects on the capacity of a 2-2 channel when the
detection threshold is varied and when this channel is
provided with a mill- zone of detection are considered.
(Author)
Electronics Res^rch Lab. , U. of California,
Berkeley .
NOI^ IN BACKWARD- WAVE AMPUFIERS, by
H. Jory. Rept. o4 Contract AF 49(638)102. 25 July 60,
I76p. 49 refs. lEflR series no. 60, issue no. 298;
AFOSR-TN-60-1L71; AD- 247 353.
Order fr<in LC nii$8. 10, ph$27. 30 PB 153 400
The backward- wave amplifier, a type of traveling wave
tube, is studied fiom the point of view of the current
and velocity fluctuations which are present in the elec-
tron beam, and which produce electrical fluctuations
or noise in the output of the device. The work is con-
cerned with tubes] employing the tape-helix interaction
circuits and hoUo^w cylindrical electron beams nor-
mally found in backward-wave amplifiers. An analysis
is presented which demonstrates that this type of
ampUfier involveii an infinite "set of beam waves having
one phase variati( m in angle, but different radial
variations. The Relative coupling between the helix
and the various radially -varying beam waves is deter-
mined The relative excitation of the beam waves is
also calculated for typical noise pulses of finite width.
An experimental system designed to measure that pan
of the noise which couples to the backward-wave
amplifier is described. Measurements with two types
of operating conditions near the cathode are discussed.
The measurements of noise power are used to obtain
an estimate of the ration /S, where n is a measure of
correlation between current and velocity fluctuations,
S is a noisiness parameter, and the minimum noise
figure is proportional to (S-Tl). (Author)
• ■ • \. ■ i-j - . V • '
General Electric Co. . Owensboro, Ky.
INVESTIGATION OF THE EFFECTS OF ENVIRON-
MENT AND OF OPERATING CONDITIONS ON THE
REUABIUTY AND CHARACTERISTICS OF REUA-
BLE ELECTRON TUBES. VOLUME I, by W. S. Bowie.
Rept. on Study of Electron Tube Life, Contraa DA 36-
039-SC-42524. [19551 886p.
Order from LCmi$l 1.10, ph$I34.70 PB 154 484-1
This report released for sale to the public 17 Feb 61.
A study was made of the effeas of the environmental
factors, mechanical vibration and ambient tempera-
lure, and of the operating conditions, heater voltage,
heater cycling, plate voltage, plate current, plate diB-
sipatlon and pulse operation on reliable-type miniature
receiving tubes. The effect of these conditions on the
survival rate and on the change in the characteristics
was studied and the results presented in graphical and
mathematical form. The data so presented can be
used by designers erf elearonic equipment to enable
them to design for the highest reliability and the most
stable operation of the electron tubes. (AKhor) In-
cluded are data and graphs on the effects of heater
voltage, ambient temperature, and heater cycling.
Oneral Electric Co. . Owensboro, Ky.
[INVESTIGATION OF THE EFFECTS OF ENVIRON-
MENT AND OF OPERATING CONDITIONS ON THE
RELIABILITY AND CHARACTERISTICS OF RELI-
ABLE ELECTRON TUBES. VOLUME II. by
W. S. Bowie) Repi. on Study of Electron Tube Life,
Contract DA 36 -039 -sc- 42524. [1955] 917p.
Order from LC ml$ll. 10. ph$139. 20 PB 154 484-2
This report released for sale to the public 17 Feb 61.
Included are data and graphs on the effects of plate
current, plate voltage and plate dissipation; mechani-
cal excitation; and pulse operation. (See also
PB 154 484-1)
General Electronic Labs.. Inc.. Cambridge. Mass.
SPECIFICATION FOR METHODS OF EVALUATING
THE SUSCEFTIBIUTY OF FM COMMUNICATIONS
RECEIVERS, by D. BeauWen, E. Browne and others.
Rept. on Contraa DA 36-039- sc-78240. Sep 59. 29p.
Order from LC mi$2. 70. ph$4. 80 PB 153 241
This document specifies the method of testing fre-
quency-modulation communication receivers for their
susceptibility to Jamming. This method consists of
five standard tests, the results of which permit a good
426
appraisal of the performance of a receiver under
Jamming conditions. To facilitate rapid evaluation of
the test results, a method of assigning numerical
■cores to the various test results has been developed
and is included in this specification. (Author)
Haloid Xerox. Inc. [Rochester. N. Y.]
RESEARCH ON HIGH TEMPERATURE COMPLEX
COMPOUEm" DEVELOPMENT. Final rept. for
1 Apr 59-31 Aug 60 on Contract AF 19(604)5508. [1960
77p. 19 refs. AFCRL-TR -60-353.
Order from OTS $2.00 PB 171 380
This contract work resulted in the development of a
new microminiature concept, the RC circuit plate.
This plate is formed by depositing, without masks,
conductive, resistive, and dielectric materials on a
ceramic substrate. This is converted into an actual
RC circuit by applying a xerographic resist panern
and selectively etching the various layers. Associated
with the circuit plate is an interconnection scheme that
employs printed circuit techniques. This allows cir-
cuits to be assembled into modules and modules into
"super modules." thereby constructing complex equip-
ment without resorting to soldered wire conneaions.
Paralleling this development of a micro circuit concept
was the investigation of new materials for extreme
environment operation and new methods erf depositing
such materials. Results of this work included: (a)
development of electron bombardmeflt techniques for
the deposition of highly refractory dielectrics, (b)
formation of thin film capacitors by anodization and
chemical deposition and (c) deposition of conductive
films on ceramic substrates by electroless plating.
Utilizing several of the above techniques, a large num-
ber erf chromium resistors and SiO capacitors were
fabricated and tested. Information on cycling, thermal
■hock, and aging are given. Preliniinary work on
layout and formation of typical computer tyj)e circuitr;
was done. (Author)
Haverford Coll. [Pa.]
ELECTRONIC OBSTACLE AND CURB DETECTORS
FOR THE BLIND, by T. A. Benham. Summary rept.
for 1 Jan 53-30 June 60 on Subcontract no. 1 to Bio-
physlcal Electronics, Inc., Contract VIOOIM- 1900.
[19601 206p. 13 refs. AD-243 621.
Older from LC mi$9. 30, ph$31. 80 PB 153 lOl
An obsucle detector has been built and three units
field tested by blind people over a period of approxi-
mately one year. A portable laboratory model of a
curb detector has also been buUt and briefly field
tested. It still requires further development to be-
come a practical device. Both instrumentp range by
optical triangulation using light in the near infra-red
and a germanium photodiode light detector. Output to
the blind user is from a tactile stimulator mounted in
the handle. The obstacle detector, weighing two
pounds, is housed in a box, approximately 7" x T'
x 13" including handle. Its maximfum detection range
l» 9" but this can be reduced to 5' by depressing a
■witch in the handle. It operates for five hours per
charge from a rechargeable battery. The curb de-
tector will detect holes, down- curbs over 3". up-
curbe over 6" and low obstacles. A chopped incan-
descent light is focused on the ground by the upper of
two plastic Fresnel lenses. The diffuse reflection of
this li^t is imaged by the lower Fresnel lens on a
f>alr of photodiodes mounted side by side on a servo-
actuator. As the range changes, due to walking mo-
tion, (from 3' to 7') the actuator is positioned to pro-
duce equal light signals from both photodiodes. A
down -curb casts a shadow causing the light to be lost.
An up-curb reduced the range so the system cannot
follow, again causing the light to be lost. Light loss
is signaled to the user. (Author)
Hughes Research Labs., Malibu, Calif.
STRIP MAPPING BENEATH AIRBORNE RECONNAIS-
SANCE VEHICLE, by D. L. Bullock and O. R. Price.
Scientific rept. no. 3508/9 on Contraa AF 19(604)3508.
May 60, 29p. 5 refs. AFCRL-TN-60-1121.
Order from LC mi $2. 70, ph$4. 80 PB 153 3%
Institute of Mathematical Sciences, New York U. ,
N. Y.
ON ELECTROMAGNETIC EIGENFUNCTIONS IN
CLOSED CAVITIES, by H. Niemeyer. Rept. on Con*
traa AF 49(638)229. Aug 60, 46p. 10 refs. Research
rept. no. BR-34; AFOSR-TN-60-1103; AD-245 335.
Order from LC mi$3.30, ph$7.80 PB 152 727
Some asymptotic sutemenis about the elearomagnetic
eigenfunctions in closed cavities are proved. The be-
havior of the corresponding Green's tensors is in-
vestigated and to this result is applied a Tauberian
theorem for Laplace transformations which will yield
the asymptotic statements. (Author)
Jet Propulsion Lab. . Calif. Inst, of Tech. , Pasadena.
RBF-3 RECEIVERS, by F. H. Davis. Rept. on Con-
traa WO4-200-ORD-455. 26 July 48, 18p. 5 refs.
Memo. no. 4-29.
Order from LC mi$2. 40, ph$3. 30 PB 153 951
This report released for sale to the public 3 Feb 61.
The purpose of this report is to discuss steps taken to
improve the operation of the RBF-3 telemetering re-
ceivers. Five Navy RBF-3 FM receivers were used as
received from the Navy and were modified slightly to
receive the JPL telemetering channels. These re-
ceivers were well construaed, the parts easily ac-
cessible, and the limiting char aaeri sties good. It was
decided to attempt to improve their sensitivity and
signal-to-nolse ratio as much as possible and praai-
cable. The receivers at the present time approach the
theoretical maximum for sensitivity and operation. In
comparison with their original condition, they are
capable of receiving a minimum signal of 4 per cent
of the power originally required; or with a transmitter
erf fixed power and other conditions being equal, the
maximum range has been increased five times.
(Author)
Jet Propulsion Lab., Calif. Inst, of Tech., Pasadena.
A 217-219mc ADAPTER UNIT FOR USE WITH THE
RBF-3 RECEIVER, by Clifford I. Cummings. Rept.
on Contraa W04-200-ORD-455. 15 Sep 48, lOp.
2 refs. Memo. no. 4-43.
Order from LC mi$ 1 . 80, ph$ 1 . 80 PB 153 950
This report released for sale to the public 3 Feb 61
427
The contemplated dhange in telemetering frequency to
the newly authorized band in the vicinity of 218 mc for
use in fuure rocket firings has required careful con-
sideration of the RP transmission problem. If the
power output oi the telemetering transmitter is to be
kept snuU, so thatlthe weigtit of the power supply may
be kept to a minimum, a receiver of optimum per-
formance is necesaary. Redesign of the RF heiad from
a BC 1267-A IFF component (previous frequency range
157 to 187 mc) has been completed with good results.
This unit is cabled into the converter tube socket of an
RBF-3 FM recelvef , thus using all of the features at
this receiver with <he exception al the original RF
section. The RBF-S may be used at its original fre-
quency by merely iinplugging the adapter unit, replac-
ing the tubes al tt\e\ RF section, and retuning the first
IF transformer priory. With this arrangement,
limiting action is opined with a 5^v internal voltage
of a 50-ohm source
8 db. (Author)
and with a noise figure of about
Laboratory for Insulation Research, Mast. Inst, of
Tech . , Cambridgi .
PRINOPLES OF MODERN MATERIALS RESEARCH,
by A. von Hippel. Rept. on Contracts Nonr- 1841(10),
AF 30(635)2872 and AT(30- 1)1937. Mar 59. 25p.
37 refs. Technical rept. 136.
OrderfromLCmi|2.70, ph$4.80 PB 150 709
Quest for the 'Ideal Capacitor" Technical Breakdown
Strengtl^ Breakdown Phenomena in Alkali Halide
Crystals, Qualitativje Molecular Theory-
Lincoln Lab. , Mass . Inst, of Tech. , Lexington.
DETECTION OF SIGNALS IN NON-GAUSSIAN
NOISE COMPUTA-plON RESULTS FOR THE UNEAR
AND UMITING DETECTOR SYSTEMS, by James W.
McGinn. Rept. on Contract AF 19(604)7400. 7 Oct 60,
27p. 47G-0007; AQ- 246 779.
Order from LCnuS2. 70. pb$4. 80 FB 153 217
Some results are presented of the computation of prob-
ability functions fot the detection of pulse signals in a
noise background of time varying power . The results
are concerned withjthe linear and limiting detector sys-
tems described proviojsly. Probability functions are \
given on the reference for the two detector systems of
interest and the vaUies of parameters used in computa-
tion are specified . The results of computation in the
form of graphs of the probability functions are outlinec
and a brief discuss on is given at the results obtained.
(Author)
Lincoln Lab. , Matos. Inst, ai Tech. , Lexington.
EXPERIMENTAL AUTOCORRELATION OF BINARY
OODES, by D. F. OeLong. Rept. on Contract
AF 19(604)7400. 24| Oct 60. I2p. 47G-0006.
Order from LC mil2. 40, ph$3. 30 PB 152 974
In order fo get gooq range resolution from a long-
pulse radar, it is necessary to increase the bandwidth
of the pulse in somt manner. One technique, first pro-
posed by Siebert, i$ to subdivide the pulse into interval
0 or V according to some coding scheme. This report
gives the results of an experimental search for phase
codes with good aut|ocorrelation functions. Thus the
ambiguity fuiKtion tmly along the zero doppler axis
Lincoln Lab. , Mass. Inst, of Ttech. , Lexington.
PERTURBATION THEORY OF THE RECIPROCAL
FERRITB PHASE SHIFTER, by Kenneth J. Button and
Benjamin Lax. Rept. on Contract AF 19(604)7400.
1 Dec 60, 15p. 6 refs. 84G-0013. AD-247 290.
Order from LC ml$2. 40, ph$3. 30 PB 153 421.
A quantiutive comparison has been made between the
results at the perturbation theory analysis and the ex-
perimental observations. It has only been necessary
to consider the fundamental mode of propagation in a
waveguide conulnlng an equivalent dielectric slab and
to use as tiie perturbation the change In the diagonal
component of the ferrite permeability tensor as the
ferrite becomes magnetized. An explicit expression
for the phase shift has been derived. A simplified
form valid for ferrite specimens large enough to be
useful in the reciprocal phase shifter reveals the
principles of operation. This result shows that die-
lectric concentration of the microwave fields within
the ferrite produces a magnification of the perme-
ability change as the ferrite specimen becomes
magnetized in the small applied dc field. (Author)
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
SIGNAL PROCESSING IN RADAR ASTRONOMY.
COMMUNICATION VIA FLUCTUATING MULTIPATH
MEDIA, by R. Price and P. E. Green, Jr. Rept. on
Contract AF 19(604)7400. 6 Oct 60, 276p. 71 refs.
Technical rept. no. 234; AD-246 782.
Order from LC ml$ll. 10, ph$42. 60 PB 153 225
The detection and measurement of fluctuating urgets
that have appreciable depth are discussed. Although
stated in radar terms, the results are equally appli-
cable to communication problems in which the propa-
gation medium has significant multipath spread and
fluctuation rate. A signal received from such a urget
or channel is a perturbed version of the transmission,
in which frequency and time (delay) spreads have been
produced by multiple random mocbilation superim-
posed by the target (or channel) on the original modu-
lation of the transmission. Special cases of the deep
fluctuating target, namely the fluctuating point target
and the very slowly fluctuating deep target, are also
considered. (Author)
Lincoln Lab., Mass. Inst, of Tech. , Lexington.
AN ULTRASONIC RECEIVER FOR DETECTING
SIGNALS OF BATS, by A. Bertolinl. Rept. on Coo-
traa AF 19(604)7400. I Dec 60, 38p. 3 refs.
47G-0010.
Order from LC mi$3.00, ph$6.30 PB 153 697
A transistorized ultrasonic receiver for detecting
signals of bats has been built. It has a small signal
gain of 65 db with a bandwidth from 15 Kc to 200 Kc.
Some bandwidth selection within this frequency range
can be obtained with the use of plug-in filters built for
the purpose. Additional gain of up to 14 db can be ob-
tained, depending on the preamps used. (Author)
(v*0) is examined.
428
Lincoln Lab. , Mass. Inst, of Tech., Lexington.
A WIDE BAND ANTENNA. HAVING AXIALLY SYM
METRICAL PATTERNS. HIGH GAIN AND LOW
SIDE LOBES FOR ALL POLARIZATIONS, by K. J.
Keeping. Rept. on Contract A F 19(604)7400.
30 Nov 60, 33p. 1 ref. 46G-0008
Order from LC mi$3.00, ph$6. 30 PB 153 696
This report describes an antenna with its rear feed
which has circular symmetry about the axis of its
circular waveguide. It has equal E and H plane beam-
wldths of 0. 5° and the side lobe levels attained on the
test antenna were more than 20 db below that of the
main lobe. The performance of the antenna is com-
pered with theoretical results based on Huygen's
Principle. Due to the complicated nature of the pri-
mary pattern, it is difficult to define it accurately.
Therefore, a close approximation to the actual p>at-
terns was used and close agreement is obtained in the
poflitions and relative magnitudes c4 the first side
lobes- The main lobe, as predicted. Is in close
agreement with the measured pattern. (Author)
Litton Industries, Salt Lake City, Utah.
COAXIAL GAS DISCHARGE MiVICE, by L. D.
Yancey. Quarterly progress rept. no. 1, 19 May-
31 July 60, on Contract DA 36 -039- sc- 85 128; continua-
tion of Contract DA 36-039- sc -7 2403. [1960] 29p.
AD- 243 269.
Order from LC mi$2.70. ph$4.80 PB 153 245
An analysis of the fired VSWR erf the duplexer is pre-
sented. The effect of removing the "keep- alive" stub
and varying transmitter-to-antenna length is shown.
Prehminary redesign of the ATR tube is established.
(Author)
Lockheed Aircraft Corp. , Sunnyvale, Calif.
DESIGN AND CONSTRUCTION OF LARGE ANTEN-
NAS FOR RADIO ASTKOhiOMY, RADAR AND
CX)MMUNICATIONS, by George R. Evans. 28 June 60,
32^. 114 refs. SB-60-26; AD- 240 310.
Order from LC mi$3.00, ph$6.30 PB 152 719
A bibliography; sources checked were: Applied Science
and Technology Index (Industrial Arts Index), 1950-
date; ASTIA, through 1 June I960; California Institute
of Technology, Jet Propulsion Laboratory, CIT/JPLAI.
Literature Search No. 60: Radio Astronomy; Engi-
neering Index, 1950-date; Science Abstracts, Sections
(Electrical Engineering), 1955-date; Technical Infor-
mation Center, Lockheed Missiles and Space Division.
Lockheed Aircraft Corp. , Sunnyvale, Calif.
DIELECrRIC LOADED RESONANT SLOTS, by
J. W. Carr. Technical memo, on Physical Electronics.
May 60, 37p. LMSD-288264; AD-240 047.
Order from LC mi$3. 00, ph$6. 30 PB 152 693
Experimentally determined families of curves plotting
■kx resonant frequency versus (1) slot thickness-to-
wfckh ratio and (2) relative dielectric constant of the
slot loading material, are presented for half-wave
resonant slots. The role that the slot width-to-length
tatio plays in determining the slot resonant frequency
It demonstrated graphically. An example of how the
dua may be interpolated for design applications is in-
cluded and discussed. (Author) 429
Lockheed Aircraft Corp. , Sunnyvale, Calif.
REPORT OF THE JOINT MEETING ON SOLAR CELL
MEASUREMENT STANDARDIZATION BY THE WEST
COAST SUBCOMMITTEE OF THE AIEE SOLID
STATE DEVICES COMMITTEE AND THE SEMI-
CONDUCTOR PHOTODIODE TASK GROUP (28. 4. 6)
OF THE IRE SOLID STATE DEVICES COMMITTEE
AT THE STATLER-HILTON HOTEL* LOS ANGELES,
CALIFORNL^, 17-18 DECEMBER 1959. 29 Feb 60,
84p. 51 refs. LMSD- 288184.
Or^er from LC miJ4. 80, ph$13. 80 PB 153 645
Contents :
Solar cell standards aixl measurements
Laboratory light source and instrumentacioo
Definitions and ternunology
Literature survey.
New items of solar radiation equipment unlisted in
Eppley Laboratory, Inc. descriptive bulletins
A precision radiometer for the measurement of total
radiation in selected spectral bands
Representative solar radiation dau
Mallory, P. R., and Co.. Inc., Indianapolis, Ind.
UNIVERSAL POWER SUPPLY (VIBRATOR TYPE), by
Ralph Albon, Jr. and Kenneth Snnith. Final rept. for
15 May 56-31 Aug 58 on Contract DA 36-039-sc-
72370. 31 Aug 58, 54p. 9 refs .
Order from LC mi$3.60. phJ9.30 PB 150 689
This power supply is intended to operate beacons , tele-
metering units , and other related pieces of equipment.
Four different developmental designs were built and
tested before a final design was evolved. The latter
consisted of an aluminum housing about 3" in diameter
and 9" overall length within which was located printed
wiring cards to which the components were mounted.
Out-put voluges of 6.5, -22.5, 150, and 315 volts,
with adjustable controls, where necessary, were avail-
able at connectors nxxinted to one end of the power
supply. The battery was sealed from the circuitry sec-
tion to prevent possible damage from electrolyte leak-
age. (Author)
Microwave Associates, Inc.. Burlington. Mass.
HIGH REPETITION RATE BROADBAND DUPLEXER,
by Emanuel L. Horn. Quarterly progress rept. no. 7,
15 Feb-15 May 60, on Contraa DA 36-039-sc-78165.
[19601 14p. AD- 243 375.
Order from LC mi$2. 40, ph$3. 30 PB 153 229
The X-700 klystron was received and installed but
failed to function after less than 10 hr of operation at
or below its rated power output. Recovery time in-
strumentation was completed prior to the klystron
failure. Fabrication techniques were developed fbr
the quartz wafer type encapsulated window with results
which appear promising. Redesign of the tuned en-
capsulated element is progressing with satisfactory
initial results. Fabrication of a dual tube with high
power encapsulated input windows yielded an increase
in bandwidth over that previously chained. (Author)
(See also PB 152 668)
Microwave Reseaprch Inst.
Brooklyn, NY.
INVESTIGATIONS
MODULATORS. b>H
Polytechnic Inst, of
OF HlOi- POWER MAGNETIC
E. J. Smith and T. Kusuda. Pinal
rept. on Contract AF 30(602)1619. 22 July 60, 50p.
3ref8. Final rcptJ R-797-59; nB-725: RADC-TR-
60-228; AD- 247 22T.
Order from LC mii3. 30, ph$7. 80 PB 153 454
The results of invelstigations of high-power magnetic
modulators are surfimarized; the topics include: im-
provement of a twoi- megawatt experimental magnetic
modulator, evaluation of polyphase m'Odulators, and
studies of the flux -reset mechanism. An electrodeless
switch is described and the power capability of elec-
tromechanical pulsiers with solid conductors is ex-'
plored analyticallyi Finally the results of a study of
the operating characteristics of a hybrid pulse
generator are presented. (Author)
Microwave Lab., Stanford U., CaUf.
SOME EXPERIMEIfrS WITH A NEW TYPE OF
CROS^D-FIELD OUN, by T. A. Mldford and G. S.
Kino. Scientific rept. no. 25 on Contract
AF 19(604)1930. Aug 60, 33p. 11 refs. ML. rept.
no. 732; AFCRL-TK-60-1120; AD-247 593.
Order from LC miiS.OO, ph$6.30 PB 153 504
The construction a«d testing of a crossed-field gun
based on an exaa apace charge flow solution will be
described. All the characteristic parameters of a gun
of this type may bejobcained analytically. Experi-
mentally the gun w^s found to perform essentially as
predicted. This guti has a moderately high conver-
gence and produces a beam whose gross features give
a very good approximation to planar Brillouin flow.
Work by Anderson has indicated that crossed-field
beams produced by! a gun of this type may be some-
what less noisy thaji similar beams produced by other
types of guns. (Au^or)
^utfic
Motorola, Inc. , Qhicago, 111.
LOW FREQUENCYl ELECTRO-MECHANICAL FILTER
by a Niederman aitd Stanley P. Lapin. Quarterly
progress rept. no. ;7, 1 Nov 53-31 Jan 54, on Contract
DA 36-039- sc- 15536. [1954] 48p. 5 refs.
Order from LC miis. 30, ph$7. 80 PB 150 692
S3t5.
T
Theoretical and pr^limuiary experimental results on a
low impedance lattice filter, utilizing two crystals pex
section, are givei.. , Theoretical and experimenul in-
vestigations on a lc(w impedance ladder filter utilizing
one crystal per section are made. Progress on fabrica-
tion at low-inductai|ce 455 kc. crystals is described, in
eluding CT cut face
crystals. (Seealsci
STUDY OF PILOT
THE USE OF THE
CATOR AND THE
shear crystals and overtone X-cut
PB 140 567).
National Aviation paclllties Experimental Center,
Atlantic City, N.
OPERATIONAL CAPABILITIES IN
FAA PICTORIAL POSITION INDI-
AVION nCTORIAL NAVIGA-
TIONAL DISPLAY |N THE TERMINAL AREA, by
R. B. Fisher and J! A. Sunkes. Feb 60, 97p. Task
Assignment D- 2-521 3.
Order from OTS $2 25 PB 171 368
A preliminary investigation and analysis was conducteo
at NAFEC to determine the ability of a pilot to use a
-piaorial display of VOR/DME information and to
determine associated effects on communication work-
load. The terminal area was emphasized for this
investigation as part of an extensive Bureau of Re-
search and Development program also involving en-
route and high altitude utilization of pictorial displays.
The investigation and analysis provided information on
pilot ability to use pictorial displays for transition
from airways to airport instrument landing systems
and for airport departures to enroute airways as well
as for missed-approach and holding pattern
procedures.
National Bureau of Standards, Boulder, Colo.
INVESTIGATION OF STABILITY OF QUARTZ RE-
SONATORS AT LOW TEMPERATURES, by
P. A. Simpson and A. H. Morgan. Quarterly progress
rept. for 1 Feb- 30 Apr 59. 1 June 59, 25p. 2 refs.
NBS rept. 6062; AD- 219 846L.
Order from LC ml$2. 7a phH 80 PB 150 064
A continuation of some crystal aging tests at 13°C and
40°K is reported. Long-term measurements over a
period of 34 days show no aging to parts in 10^^ and
short -time (second-to-second) stabilities are a few ptrti
in 10^^ (Author)
Naval Ordnance Lab. , Corona, Calif.
COMPONENTS FOR A LOW -LEVEL PULSE -CODE
MODULATION TELEMETRY SYSTEM, by E. R. HiU
and J . L . Weblemoe . 11 Jan 60, 56p. 5 refs .
NAVWEPS rept. 5974; NOLC rept. 478.
Order from LC mi$3.60, ph$9.30 PB 150 707
Components for low- level commutation and coding of
instrumentation dau were Westigated for use in a
palse-code modulation telemetry system. The investi-
gation resulted in the development of solid-state cir-
cuitry that can: (1) commutate and code data from
source impedances up to 500 ohms with full-scale sig-
nal outputs of 50 mv, and (2) provide an eight-bit
straight binary code at a 250-kc clock rate without re-
sorting to amplification ahead of the coder. The systeir
was based on a design philosophy that involves a suc-
cessive-approximation method of data sampling and
coding, "nie pulse-code generator, which makes up the
coding portion of the design, includes a comparator,
pulse amplifier, and weighted -voltage generator, with
associated circuitry. Electronic-switch and saturable-
core ring-counter configurations are used in the com-
mutation circuitry. The circuits described in this re-
port, although specified for a PCM telemetry system,
may prove to be useful in tnany areas of instrumenta-
tion. (Author). 1^
Naval Ordnance Test Station. China Lake, Calif.
INSTRUCTIONS FOR OPERATION AND MAINTE-
NANCE OF THE MODULATOR. 4 -CHANNEL PCM
TIMING SYSTEM, by D. T. Duckworth. 15 Aug 60.
28p. 18 refs. NOTS TP 2519; AD-246 256.
Order from LC ml$2. 70, ph$4. 80 PB 153 084
The underlying principle of the PCM timing system is
pulse transmission of data; precise timing and con-
trol functions are derived by digital techniques and
430
sent to test-range instrument sites via a single-
carrier 9 -channel or 4 -channel pulse -code -modulated
UHF radio link. This report, one of a series on the
4rcbannel system, describes the modulator. The
modulator is used in the central station to commutate
the four individual intelligence functions into the
pulse-coded signal frame that is fed to the UHF radio-
Unk transmitter. (Author)
Naval Ordnance Test Station, China Lake, Calif.
INSTRUCTIONS FOR OPERATION AND MAINTE-
NANCE OF THE NOTS PORTABLE TIMING UNIT
(STU-1), by George R. Meuser. 15 Aug 60. 15p.
3 refs. NOTS TP 2531; AD-246 797.
Order from LC mi$2. 40. ph$3. 30 PB 153 221
The Supplementary Timing Unit. Model STU-l, is a
precision, free -running lOOO-cycle generator used as
an uncorrected time-base generator with recording
cameras located beyond the area serviced by the NOTS
range-timing system. The output of the timing unit
consists of lOOO-cycle pulses with every 10th pulse
broadened for aid in assessment. The output is of
sufficient amplitude and power to drive as many as
three NE-17 necm lamps. (Author)
Naval Research Lab. , Washington, D. C.
CRT TARGET DETECTABILITY WITH TRANS-
PARENT AND OPAQUE PHOSPHORS, by C. W. Iseley
and J. M. Carl. Interim rept. 23 Oct 59. 8p. 8 refs.
NRL rept. 5413; AD-229 180.
Order from LCmi$ 1.80. phJl.BO PB 143 302
Research is presented on cathode-ray tube (CRT) dis-
play problems arising from environmental illuminatioa
An investigation was made of the target detectability
characteristics of a transparent and an opac^je phos-
phor under moderate illumination conditions. The
method of fexperimentation which was used involved the
simulation of a radar B-scope presentation. Independ-
ent variables were CRT grid bias (pedestal amplitude),
receiver noise, and type of phosphor. Results indicate
that for each phosphor least signal strength is required
for detection when receiver noise is approximately
maximal. With at least moderately high gain, detect-
ability is approximately the same for a wide range of
grid biases. There is no significant difference in
detectability between the transparent and conventional -
phosphor tubes under these optimal conditions. (Authoi)
Naval Research Lab. , Washington, D. C.
WIND-INDUCED TORQUES MEASURED ON A
LARGE ANTENNA, by James W. Titus. Interim rept.
27 Dec 60, 49p. 7 refs. NRL rept. 5549.
Order from LC ml|3. 30. ph$7. 80 PB 150 319
The fluctuating torques applied by wind forces are an
important source of error in the servo systems re-
quired to aim large antennas for radar and radio as-
tronomy. As a step toward providing design informa-
tion for estimating and minitnizing these errors, direct
measurements were made of the wind-iixhiced torque
acting about the elevation axis of a 60-ft Kennedy para-
boloidal antenna. Torque was measured by a strain -
gage bridge and recorded on magnetic tape. Sixty runa
each of 33 minutes duration, were recorded. A mean-
squared torque spectral -density curve was obtained
for each run. A two-variable function of the form used
by Newton and others gives a good fit with these data.
The half -power frequency values ranged from 0. 029 to
0. 29 radian per second, with a median value of 0. 1 1
radian per second. A second comer frequency in the
vicinity of 2. 0 radians per second was also observed.
Peak torques were observed during certain runs, and
equivalent aerodynamic moment coefficients were de-
rived. Root -mean -square values of wind-torque varla
tion were obuined for all runs. (Author)
Nobel Inst, of Physics. Stockholm (Sweden).
A NEW SOLUTION OF THE FINITE RISE TIME
PROBLEM BY MEANS OF A DISTRIBUTED AMPLI-
FIER WITH AUTOMATIC GAIN CONTROL, by Bertil
Johansson. Technical note no. 1 on Contract
AF 61(052)118. 15 Dec 59, 8p. AFOSR TN-60-164;
AD- 232 064.
Order from LCmi$l. 80, ph$ 1.80 PB 150 720
In a distributed amplifier the output pulse is built up
by the addition of pulses from subsequent stages. If
this sum up is stopped when the pulses have reached
a certain pulse-height level then the output pulses will
have the same height and, what is essential in time
measurements, the same shape independent erf the
hei^t of the input pulse within a certain pulse -height
range. A distributed amplifier based on this principle
is described. It consists of 2 cascaded 5 tubes ampli-
fiers (rise-time 8 ns) and covers a pulse-height range
of 15 dB. By conveniently chosen combination of num-
ber trf tubes and cascaded amplifiers any desired
pulse- height range can be covered. The amplifier can
be built for fast as well as slow phosphors. (Author)
Office of Scientific Research and Development.
Div. 19.
A SYSTEM OF SHORT-RANGE COMMUNICATION
BY PASSING AUDIO- FREQUENCY ELECTRIC CUR-
RENTS THROUGH WATER, by Howard C. Hardy
(Moore School of Electrical Engineering, U. of
Pennsylvania). Final rept. (Pari IV) on Contract
OEM8r-922. June 45, downgraded 14 Feb 58, de-
classified 12 Jan 61. lOlp. 15 refs.
Order from LC mi$5.70. ep|18. 30 PB 153 954
This report released for sale to the public 1 Feb 61
Audio- frequency currents (speech or single tone) are
introduced into the water from a suitably design am-
plifier or oscillator and a transformer connected to
two elearodes in the water. When the currents flow
through the conducting medium, an alternating emf
will be found to exist between two other electrodes
placed in the water. The received signal is then am-
plified and heard in earphones. This kind of conrmiuni
cation is called UWT (underwater tel&graph or tele-
phone). Papers are included on: general theory of
propagation of underwater currents; operating and
maintenance instructions for underwater transceiver,
model C 105 and for underwater speech transceiver,
model C 4(K); tests of underwater transmission elec-
tric current reception; installation, operation and
maintenance of underwater speech transceiver, series
UWT-C 500 for Sleeping Beauty ^ II; and tests of
UWT installation in Sleeping Beauty.
431
rige Oonununlca^ions Engineers, Inc. , Washington,
Q C
PROJECT TEST RANGE, CC»JCLUSIONS AND
RECOMMENDATlONa Final rept. on Conlraa
AF 30(602)1756. jlme 60, 39p. 6 refs. PCE-R-7697A;
RADC TR-60-193J
Order from LC mi$3. 00, ph$6. 30 PB 153 609
i
A sinunary d woi^ on the establishment at a vhf iono-
spheric-scaner te^t range for use in the evaluation of
ionospheric- scatter equipment, systems, and oper-»
ational techniques, and in making studies leading to
selection at such equipment, system designs, and
techniques.
Plessec, E. H. , Associates, Inc., Los Angeles,
Calif.
THE U^ OF RAlJjAR AS AN IONOSPHERIC PROBE,
by Frances Richeyand R. S. Wehner. Scientific rept.
no. 1 on Contraa AF 19(604)6187. 11 Oct 60, 27p.
Urefs. C25-60(UM0; TR-103; AFCRL-TN-60-1134.
Order from LC mi52. 70, ph$4. 80 PB 153 498
An analysis has be^ made at the feasibility of using
radar as an icnosplieric probe to measure both elec-
tron density and cqllision frequency as a weil-resolved
function of space ahd time, the latter particularly to
follow changes in tpe ionosphere as the result of some
natural or artiflciall disturbance. It is shown that the
electron density measurement by means of back-
scattered radar return is perfectly feasible for a high-
powered, large diski, radar, and for enhanced densities
at ranges ever as j reat as 1000 km; for normal iono-
spheric densities tie range is considerably less with-
out pulse integrati< n or data processing. The tech-
nique of cross -moqulation is investigated for use in
determining electrtm-molecule collision frequency; it
is shown that the transfer of modulation at microwave
frequencies and nofmal electron densities is much too
small to be detectep; however, it is entirely possible
that cross -modulation techniques at lower frequencies
(1 - 10N4c) may prctve useful. This will be further in-
vestigated and repeated in a subsequent paper.
(Author)
Raytheon Co. , W4Itham, Mass.
QK324 PRODUCTION REFINEMENT AND QK702
DEVELOPMENT PtOGRAMS, by H. Morin. Quarterly
engineering rept. i^. 6, 15 July- 15 Oct 58, on Con-
tract DA 36- 039 -scj- 7 3206. [19581 24p.
Order from LC mi|2. 70. ph$4. 80 PB 150 699
The QK324 production refinement has been completed.
The results of QK3^ evaluation tests indicate that
there are no major design problems remaining on the
QiC324. The 20 QK$24 tubes built have met all at the
required specifications. Acceptance tests were con-
ducted on four (^762 prototype tubes.
Raytheon Co. . WoCtham, Mass.
STUDY OF PLATIffOTRON DEVICES, by Gerry'
PerloW and W. C. ft-own. Quarterly rept. no. 2,
1 Feb-1 May 59, on(QKS-779, Contract DA 36-039- $c-
1 ref. AD- 228 402.
78229. [1959] 26p.
Order from LC mi*. 70, ph$4. 80
PB 153 240
The pure water high pressure cooling system was as-
sembled and preliminarily tested. It was determined
that a 2.gal per min flow at a pressure at 1500 lb
could be maintained through a filtering system which
would take out any particles less than 3 microns in
diameter. Cold test equipment was assembled and
made ready for operation. Anode construction techni-
ques involving copper brazing of stainless steel were
developed and the construction of other subassemblies
advanced. (See also PB 148 550)
Rome Air Development Center, Griffiss AFB, N. Y.
A STATE-OF-THE-ART SURVEY OF DELAY
TECHNIQUES, by Joseph B. Brauer and Kenneth C.
Siiefvater. Sep 60, 47p. 37 refs. RADC-TR-60-146:
AD- 244 607.
Order from OTS$ 1.25 '*■ '^"^ PB 171 420
This report released for sale to the public 10 Feb 61
as PB 152 547.
A review is given of lmpx3rtant parameters of delay
devices, presently used techniques, future require-
ments <rf ground electronic systems, and potential new
mechanisms for achieving delay, primarily in the fre-
quency range above 1 mc. Carrier frequency tech-
niques employing propagation of both electromagnetic
and acoustic waves in solid and gaseous media are re-
viewed. Circulator and other techniques are discussed
as well as periodic delay and amplification struaurei.
(Author)
Rome Air Development Center, Griffiss AFB. N. Y
SURVIVAL OF GROUND ELECTRONIC SYSTEMS
FROM NUCLEAR ATTACK, by Dana A. Benson,
K. D. Kirk, and Stanley M. Ostergren. Oct 60, 50p.
13 refs. RADC-TR-60-159; AD-246 449.
Order from LC mi$3. 30, ph$7. 80 PB 153 206
This report discusses the planning, design, and fab-
rication of ground elearonic equipment systems. Its
purpose is to give a comprehensive understanding of
the factors that must be considered in providing equip-
ments and systems with survivability. The general
aspects and basic approaches to the survival problem
are presented. The mathematics and probability
theory have been simplified, but for a given applica-
tion they may be expanded to include all the related
possibilities, combinations and Influence factors.
(Author)
Stanford Electronics Labs. , Stanford U. , Calif.
ANALYSIS OF NOISE -PRODUCING MECHANISMS IN
SOLID-STATE DEVICES, by D A. Linden. Rept. 00
Contract Nonr-225<44). 8 Feb 60, 262p. 43 refs.
Technical rept. 1551-3; AD- 235 651,
Order from LC ml$ll. 10. ph$41. 10 PB 153 169
Methods of analyzing fluctuation phenomena In semi-
conductor devices are studied with the three-fold aim
at presenting a unified treatment of the several techni-
ques, of exploring their interrelations, and at clari-
fying the assumptions on which they rest. The presen-
tation Is addressed to the electronics engineer, and
stresses concepts and methods familiar to him through
hit studies of network theory and communication
432
theory. Three major analytical approaches are dis-
cussed. The thermodynamic method is based on the
calculation of ensemble fluctuations by means of sta-
tistical mechanics. The Fokker- Planck approach
starts with the dynamics d the process Expressed in
terms of transition probabilities, and yields a differ-
ential equation governing the development, in time, of
conditional probabilities or probability densities. The
Lat^evin procedure consists of augmenting a phe-
nomenologlcal equation governing macroscopic oc-
curences with noise sources whose responses simu-
late fluctuation effects. A consistent point of view is
achieved by regarding the phenomenological equations
as results of averaging the equations governing con-
dltioftal probabilities; the insertion of noise sources
then assumes the status of an approximation designed
to restore the detailed knowledge lost in the averaging
process. (Author)
Stanford Electronics Labs. , Stanford U. , CmM.
THE LARGE -SIGNAL PROPERTIES OF MICROWAVE
CIAVITY-TYPE PARAMETRIC CIRCUITS, by
p. A. Olson. Rept. on Contract AF 33(616)6207.
8 Feb 60, 99p. 26 refs. Technical rept. no. 315-1;
AD- 234 179.
Older from LC mi$5. 40, ph$15. 30 PB 147 244
A study is made of the large-signal propenies - pri-
marily the saturation characteristic and phase re-
sponse - of microwave cavity-type parametric cir-
cuits. Negative -conductance -type amplifiers and fre-
quency converters employing semiconductor diodes are
ccoaldered. A second -order theory is developed and
calculations are made of the large -signal behavior of
the parametric circuit when used as an amplifier, as a
frequency converter, and as a limiter Large-signal
experiments were performed, on both a parametric
amplifier and a frequency converter, to test the pre-
dictions of the theory. Results of the meaaurementa of
gain and phase as a function of signal level are pre-
sented. The agreement with theory is good. A limiter
circuit, consisting of two stages of parametric fre-
quency conversion, was tested as a phase -distortion-
less microwave limiter. The limiter provided an out-
put which was constant to within 1 1 db over a range of
input greater than 50 db; and had 10 db gain at small
signals. (Author)
Stanford Electronics Laba. , Stanford U. , Calif.
PARAMETRIC AMPLIFICATION WITH SOLID-STATE
MATERIAL AND WITH ELECTRON BEAMS, by
G. Wade. Rept. on Contract AF 33(616)6207.
23 Nov 59. 23p. 14 refs. Technical rept. no. 303-1.
Order from LC mi$2. 70, ph$4. 80 PB 150 716
Microwave parametric amplifiers involve a tendency
for oscillations to be excited in a dynamical system
when an energy storage element of the system is
caused to vary in an appropriate fashion. Parametric
amplification can be obtained with solid-state mate-
riala and electron beams. This paper summarizes
diaracteristlcs and attainments.
Stanford Electronics Labs. , Stanford U. .Calif .
A STUDY OF THE ITERATED TRAVELING- WAVE
PARAMETRIC AMPLIFIER, by C. V. BeU. Rept. on
Contract AF 33(616)6207. 8 Feb 60, 109p. 32 refs.
Technical rept. no. 316-2; AD- 234 191.
Order from LC m«5.70, pl4l6.80 PB 147 243
This study was undertaken to determine a gain and
noise theory for the traveling-wave parametric ampli-
fier. The model that is analyzed is a uniform trans-
mission line which is periodically loaded with para-
metric diodes. The diodes constitute the variable ele-
ments. Across each diode is fed a large pumping
voltage which produces a time-varying capacitance.
The loss due to the diodes is included as a shunt con-
ductance. The analysis is used to determine the noise
figure of the device. The thermal noise due to die
diodes is included in the derivation. All other sources
atncAae within the amplifier are neglected. The analy-
sis shows that certain phase conditions must be satis-
fied for maximum gain and bandwidth. It is also shown
that the reverse gain of the amplifier can be mini-
mized by a proper choice of the pump phase. An ex-
perimental amplifier is described. The amplifier was
designed for a signal frequency of 1 . 7 kMc and a pump
frequency of 3.4 kMc. The measured gain was 5.0 db
with a bandwidth of 270 Mc. The double -channel noise
figure was 1 .'2 db (corresponding to a single -channel
noise figxu-e of 4. 2 db). The measured values of gain
and noise figure are in good agreement with the theory
(Author)
Stanford El(«?ftronics Labs. , Stanford U. . Calif.
THE WAVES ON A FILAMENTARY ELECTRON
BEAM IN A TRANSVERSE -FIELD SLOW -WAVE QR-
CUIT, by A. E. Siegman. Rept. on Contract
AF 33(616)6207. 1 June 59, 33p. Technical rept. no.
157-1; AD-217980.
OnJer from LC ml$3. 00. ph$6. 30 PB 150 715
The waves on a filamentary electron beam in a longi-
tudinal dc magrt^c field, and their interaction with a
transverse -flew slow -wave circuit, are studied in de-
tail. All quantiftes are expressed in terms of circular
polarization, with the circuit fields having arbitrary
polarization. The beam is found to carry 4 waves: a
positively polarized negative -energy slow cyclotron
wave, a n^^tlvely polarized positive -energy fast cy-
clotron wave, and two synchronous (P = Pe) waves, one
with positive polarization and positive energy, oiiewith
negative polarization and negative energy. The coupling
of these waves to the circuit is described both in the
manner of Pierce's longitudinal traveling-wave-tube
(TWT) analysis and in a coupled-mode description.
(Author)
Stoddart Aircraft Radio Co. , Inc. , Hollywood, Calif.
STUDIES, ANALYSES. AND COMPARISONS FOR A
TRANSISTORIZED AND MODERNIZED ANAJRM-6
TEST SET ANA^M-106(XN-1). Final rept. for
11 Mar 57-11 June 58 on Contraa NOb8r-72677. [1958]
74p.
Order from LC ml$4. 50. ph$12. 30 PB 150 712
433
The purpose of thif contract is to modernize and
transistorize the design ctf the AN/URM-6 equipment
and to Incorporate las many of the latest developmente
in the art at interference measurement as practicable
(Author) j
[Thompson] Rami Wooldridge, Inc. , Inglewood,
Calif. '
BALLOON TELEKtETRY, by G. A. McDaniel. Rept.
on Contraa AF 18^600)1190. 6 May 57, 9p. I ref.
Rept. no. GM-TMtl62; AFBMD Doc. na 7-4059;
AD- 217 243.
Order from LC mJ$l. 80, ph$l. 80 PB 153 235
A 45 foot long teth^ed aerodynanvic balloon with a lift
capacity of approiclmately 160 pounds could be used to
raise an omni-dlractional telemetry receiving antenna
and battery operate pre-amplifier to a height of about
3, 000 feet. The trtans miss ion line to the ground would
be used as the tethjering line. An isotropic antenna at
3,000 feet altitude 'would provide impact telemetry
coverage over a radius of about 30 miles. (Author)
University d Souibem California. Engineering
Center, Los Angales.
PLASMA PARAMETRIC AMPLIFIER, by Jim Y. Wada
and Zohrab A. KapTielian. Technical note on Contract
AF 49(638)522. S*^ 60, 57p. 10 refs. USCEC rept,
79-202; AFOSR-TN-60-126I; AD- 247 170.
Order from LC mip. 60, ph$9. 30 PB 153 446
The theory and application of plasmas as nonlinear
reactance element^ in parametric amplifiers are pre-
sented in this pape^. , The feasibility of parametric
amplification is defnonstrated by use of a quadrupole
cavity model containing a plasma column. Analytical
expressions for ch^ power gain and noise figure are
derived for the casle in which the signal and idling fre-
quencies are suffiqiently separated and for the degener
ate case in which ttiese two frequencies are equaL
The results and tl^lr limiucions are discussed in
some detail. (Author)
Upper Air Lab
BIAXIAL POINTING
J. of Colorado, Boulder.
CONTROL, by Fred WUshusen.
Final rept. on Contract AF 19(604)1724. [1960] 53p.
(AFCRLl-TN-60-645; AD- 247 034.
Order from LC mii3. 60, ph$9. 30 PB 153 442
This report is wrltien to give those flying the instru-
ments and other interested people a better understand-
ing of the operation, capacity, and limitations of the
rocket -borne solar pomting servo and of its progres-
sive development a|id present status. The pointing
■ervo is a device designed for attachment to an Aero-
bee type rocket to continually point an instrument at
the sun during the rocket flight. The device is a bi-
axial servo system in which sensors, or eyes, detect
any error in pointi4g and feed this information to both
azimuth and elevation drives to correct the error. All
of the various comaartments are discussed in detail.
Washington U. , Seanle. Coll. of Engineering.
SINUSOIDALLY MOCXJLATED WAVE GUIC«S FOR
TRAVELING- WAVE ANTENNAS, by AUra Ishimaru.
Technical rept. no. 46 on Contraa AF 19(604)4098.
Sep 60, 47p. 9 refs. AFCRL-TN-60-1117.
Order from LC mi$3. 30, ph$7. 80 PB 153 555
The sinusoidally varied waveguides produce the waves
whose amplitude and phase are modulated along the
surface. One wall of the guide is replaced by sinusoi-
dally varied impedance. The spacing between walls is
also varied sinusoidally. The Floquet's theorem
yields the relations between each harmonic and the
propagation constant. The periodic structure is also
studied in terms of the generalized kL - ^L diagram
which Includes the leady as well as the slow waves.
The successive approxiination method is applied to
yield relatively simple expressions for the aperture
field and it is shown that by suitable choice of various
parameters, the desired amplitude and phase of the
aperture field can be obtained. (Author)
Westlnghouse Elearic Corp. , Baltimore, Md.
RADIO TRANSMITTING EQUIPMENT, MODEL R-lx.
VOLUME I. Final development rept. , vol. 1,
1 Aug 53-30 Sep 56, on Contract NOb8r-63455. [1956)
91p.
Order from LC mi$5. 40, phJ15. 30 PB 150 710-1
The report Includes information on the following: (1)
Design and development of a LF (low frequency) R-lx
(2) Design and development of a HF (high frequency)
R-lx. (3) Operational evaluation of a LF and a HF
R-lx. (4) Envlronmenul evaluation of a LF R-lx.
Volume 1 contains development reports for 1 Aug 53-
31 Mar 55.
Westlnghouse Electric Corp. , Baltimore, Md.
RADIO TRANSMITTING EQUIPMENT, MODEL R-lx,
VOLUME 2. Final development rept., vol. 2,
1 Aug 53-30 Sep 56 on Contract NObsr- 63455. [1956]
193p.
Order from LC mi$8. 70, ph$30. 30 PB 150 710-2
Development reports for 1 Apr 55-30 Sep 56.
(See also PB 150 710-1)
Westlnghouse Research Labs. , Plnsburgh, Pa.
SYNTHESIS AND PURIFICATION OF DIELECTRIC
MATERIALS, by W. C. Divens, D. H. Hogle and
others. Rept. for 1 July 59-30 June 60 on Electrical
and Electronic Materials, Contract AF 33(616)5979.
Sep 60. 77p. 4 refs. WADC Technical rept. 59-337,
Part II.
Order from OTS $2. 00 PB 171 364
Progress on the program of preparing purer, improved
dielectrics for use as electric insulation at SOO^C is
described. Boron nitride was prepared with superior
properties to any reponed. Hot pressed nitride discs
show properties which are anisotropic. Anodized alu-
minum cotlde films have good dielectric properties at
50CPC are polarity sensitive, and have resistance de-
crease with increasing field. Electrode metal adhesior
to anodized oxide films was improved by silicon moo-
oKlde evaporation in a vacuum, on to which gold was
434
evaporated without releasing the vacuum. Aluminum
oatide films formed by hydrolysis of aluminum iso-
propoxide had inferior dielectric properties for oxide
niade by this method. Boron phosphide was synthesized
by two means: (1) direct reaction of the elements,
boron and phosphorus, and (2) by reaction of boron
trichloride, phosphorum and hydrogen. (Author) (See
alBoPB 161 366)
Wisconsin U. , Madison.
SURFACE WAVE, ANTENNA AND MICROWAVE
FILTER ENGINEERING STUDY, by Elmer H. Scheibe
Quarterly progress rept. no. 1, 1 Sep- 30 Nov 59 on
Contract DA 36-039-sc-78326; Continuation of Con-
tract DA 36-039- sc-77990. 31 Dec 59, 17p. 10 refs.
AD- 243 871.
Order from LC ml$2. 40, ph$3. 30 PB 153 242
Research is concerned with the theory and design of
constant input Impedance microwave branching filters.
A considerable part of the first period was devoted to
equipment modifications. A deuiled study of the
sli^le and double stage pass filters off the Tee was
made. The single and double stage pass filters will
form part of the complete constant input impedance
branching filter. (Author)
Ordnance, Missiles, and Satellite Vehicles
Aeronautical Research Lab. , Air Force Research
Div , Wright -Patterson AFB. Ohio.
FERRY OPERATION WITH ELLIPTIC SATELLITE
ORBITS. byC. A. Traenkle. Technical rept. Nov 60.
43p. 5 refs. ARL Technical rept. 60-319.
Order from LC mi$3. 30, ph$7. 80 PB 152 321
For special applications, a manned space station may
be put intentionally into an elliptic satellite orbit of
high numerical eccentricity. The problem of setting
up a ferry service to such a station brings in additional
variables, as compared with the fundamental circular
satellite orbit, namely the position angles of the bodies
In their common orbit plane. The control and naviga-
tion of the process is represented by characteristic,
non-dimensional parameters, arranged in two sets:
the geometrical group, giving the shape of the ferry
ellipse (major axis, eccentricity), and the kinematical
group, giving the constellation angle at the Instant of
firing, the transfer time and the velocity boosts. For
the final coincidence adjustment of the ferry with
respect to the station, two additional procedures of
Vernier control are developed by generalizing the case
of the circular satellite orbit: the correction method
by full ferry cycle transit, giving high propellant econ-
omy, and the short arc correction, to be applied if a
•bon transfer time is required. The characteristic
parameters of the process vary sinusoidally about the
mean values, to be compared with the corresponding
ones of a circular satellite orbit ctf mean radius.
(Author)
Aeronautical Research Lab. , Air Force Research
Div., Wright -Patterson AFB; Ohio.
LAYOUT OF SATELLITE FERRY OPERATION, by
Carl A. Traenkle. Rept. for 3 July-28 July 60. Oct 6a
32p. 5 refs. ARL Technical rept. 60-313.
Order from LC ml$3. 00, ph$6. 30 PB 152 320
The layout and basic mechanics of a ferry service to
a manned space station, moving in a circular orbit is
analyzed, by deducing the pertinent relations for the
control and navigation of the process. These include
the characteristic parameters for the transfer ellipse,
the velocity boosts, the constellation angle at the mo-
ment of firing of the ferry and the time interval for
the transfer. The final coincidence adjustment Is
made by an additional Vernier control, for which two
procedures are devised; the correction method by full
ferry cycle transit, distinguished by its propellant
economy, and the short arc correction, characteristic
for small corrections and short transfer time. The
results are expressed in dimensionless parameters
and represented in charts of wide applicability.
(Author)
Aeronutronlc. Newport Beach, Calif.
SPACE VEHICLE EPHEMERIS AND DIFFERENTIAL
CORRECTION PROGRAM UNIFIED THEORY, Rept.
on Project Space Track, Contract AF 19(604)5885.
14 June 60, 48p. AFCCDD-TN-60-34.
Order from LC mi$3. 30, ph$7. 80 PB 153 744
This report traces the development of a differential
correction theory for lunar and space probes. To
overcome the singularities inherent in differential
processes with conventional two-body descriptions of
the path, as the eccentricity passes throu^ unity in
either the parabolic or rectilinear sense, a unified
formulation of the two -body equations was developed.
The differential correction procedure Is based upon
an ephemeris, Integrated in Encke form by special
perturbations, and upon differential expressions de-
rived from the unified two-body equations. The report
Includes experimentation with simulated range, range-
rate, azimuth, altitude, right ascension and/or decli-
nation data to evaluate the performance of the result -
ing IBM 709 proffram. (Author)
Air Force Missile Development Center, Holloman
AFB. N. Mex.
CIRCULAR TRACK -CHAMBER. A PROPOSED
FACILITY FOR TESTING MAN-MACHINE-SYSTEMS
UNE«R CONDITIONS OF SPACE FUCMT AND
LUNAR HABITATION, by Hubert C. Feder. Oct 60,
29p. 4 refs. AFMDC TN-60-14.
Order from LC mi$2. 70, ph$4. 80 PB 153 408
The circular track -chamber, as proposed, combines a
100-foot diameter circular track and a 100-foot dlam-.
eter hemispherical vacuum chamber into one compos-
ite test facility. The purpose at this facility is to test
the compdtibility of man-machine systems. The
anticipated test procedure encompasses the simultane-
ous and continuous testing of most of the parameters
of a complete space flight history from launch through
planet life to re-entry and recovery. The facility will
handle payload-load factor products up to 2,000,000
pounds and can accommodate a crew of 20 men living
and working in a planetary environment. (Author)
435
Allied Research Associates, Inc., Boston, Mass.
LAUNCHING OF AIRBORNE MISSILES UNDER-
WATER. PART VL MISSILE RESPONSE TO WAVE-
INDUCED SUBMAtlNE MOTION, by Theodore R.
Gootknan and Theodore P. Sargent. Rept. on Contract
Nonr- 2343(00). 29 Feb 60, 37p. 9 refs. DDcument no.
ARA-720; AD-233 061.
Order from LC m«$3. 00, ph|6. 30 PB 153 161
The technique d generalized harmonic analysis is em-
ployed to derive expressions for the trajectory re-
sponses d a slender missile resulting from random
initial conditions. The random initial conditions arise
from motion d the launching submarine induced by
waves of a confused sea and a swell. The submarine
is considered to b^ a hovering, slender body d
revolution.
Army Signal Mi8$ile Support Agency, White Sands
Missile Range, h|. Mex.
TITLES AND ABSTRACTS OF SELECTED ARTI-
CLES CONCERNING THE MOTION OF ROCKETS
AND ARTIFIQAL SATELLITES, by James S. Bethel.
Sep 60, 37p. 109 refs. Missile Electronic Warfare
rept. no. 1033.
Order fnm LC mi^3. 00. ph$6. 30
PB 153 182
Titles, sources, and abstracts of selected periodical
articles related to the motion of rockets and anificial
satellites are listed. Articles in this collection ap-
peared in major soiencific and engineering journals
durii^ Che period 1.945-1960. (Author)
Ballistic Researcfi Labs . , Aberdeen Proving Ground,
Md. I
THE APPUCATION OF RADIOACTIVE TRACERS TO
aiAPED CHARGE UNERS, by M. K. Gainer. Jan 60,
23p. 5 refs. Memd. rept. no. 1242; AD-234 866.
Order from LC mii2.76, ph$4.80 PB 150 068
Radioactive tracerf have been used to study the contri-
bution of different tegments of a shaped charge liner to
the penetration of steel targets by the jet for confined
and unconfined rouitds . It was concluded that the effect
of confinement is tp produce a steady sute collapse
over all but the bale region of the liner, and that non-
steady state coUaple cakes place over nearly the entire
liner when unconfiited . (Author)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md. '
THE EFFECT OF i STRONGLY NONUNEAR STATIC
MC»^NT ON THB COMBI>JED PITCHING AND
YAWING MOTION OF A SYMMETRIC MISSILE, by
Charles H. Murphy. Aug 60, 52p. 10 refs. Rept.
no. 1114; AD- 247 V\.
Order from LC mii3. 60, ph$9. 30 PB 153 425
The usual quasi -linear solution of the nonlinear pitch'
ing and yawing motion of 8ymm3tric missiles depends
on the assumption {hat the static moment is very close
to linear. In this rpport the Thomas-Reed perturba-
tion technique which originated in astronomical prob-
lems is described Ind applied in detail to the special
problem of almost
strongly nonlinear
circular motion. The influence of
static moments on the existence of
limit motions is determined for three examples d
nonlinear monnents. Refinements d the quasi -linear
methoda are obtained whfbh are in good agreement
with the exact theory. Thejequatlons derived in the
report can be applied to more general motions and
such apDlications are indicateoT (Author)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
A METHOD OF SOLUTION FOR THE DETERMINA-
TION OF SATELLITE ORBITAL PARAMETERS
FROM DOPLOC MEASUREMENTS, by R. B. Patton, Jr.
Rept. no. 7 on ARPA Satellite Fence Series. Sep 59,
63p. Memo. rept. no. 1237; AD- 231 388.
Order from LCml$3.90, ph$10.80 PB 150 724
An extraction is presented d a more comprehensive
report (BRL Memo Report No. 1220) which describes
the overall effort and progress in the development of
the DOPLOC passive detection and tracking system. A
description is included d a method d solution for ob-
taining orbital parameters from doppler dau only. It
consists of applying successive differential correc-
tions, obtained by a lease squares creacment, to a set
of initial approximations for the orbital parameters.
While the method is direaed specifically to DOPLOC
data, it is sufficiently general to be applied to any type
of satellite tracking data if minor modifications are
introduced. Addendums present the results obtained
when the method of solution was applied to DOPLOC
measurements for revolution no. 4 of Explorer VI and
revolution no. 322 of Discover VI, respectively. The
orbital parameters, which were determined for
Discover VI, agree very well with those published by
Space Track. (Author)
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
A SUMMARY OF PHOTOGRAMMETRIC RESEARCH
AT THE BALUSTIC RESEARCH LABORATORIES, by
Dirk Reuyl. Mar 60, 17p. 17 refs. Technical note
no. 1304; AD-234 894.
Order from LC mi$2.40, ph$3.30 PB 150 070
The summary of photogrammetric research at the
Ballistic Research Laboratories, is concerned with the
following: (1) examples of application d the p)hoto-
grammecric mechod to specific ordnance problems and
ics use as a standard of calibration for tracking sys-
tems; (2) basic analytical studies of the general phcto-
grammetric problem and development of techniques of
measurement and data reduction; (3) development of a
precision photogrammetric system, comprising BC-4
ballistic camera and synchronization instrumentation;
(4) establishment of a research facility for the evalua-
tion of photogrammetric instruments and systems; and
(5) the need for new metric cameras of high light
gathering power for application to problems in space
projbe and satellice research. (Authc^)
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright-Patterson AFB, Ohio.
HUMAN FACTORS IN DESIGN OF AUTOMATIC
PROGRAMMING AND RECORDING FOR TRAINERS
(AN/ASG-15-T1 FIRE CONTROL SYSTEM TRAINER),
by Allan M. Swve. Aug 60, 14p. 1 ref. WADD Techni-
cal rept. 60-558; AD- 243 967.
Order from OTS $0. 50 PB 171 419
436
A description is given of the Fire Control System
Ttainer, AN/ASG-15-T1 for B-52 gunners. This
trainer features an automatic recording system and an
automatic programming system. The parameters used
in recording the studeitt performance are: (1) reaction
times, (2) critical target ranges, and (3) a weighted
error score displayed in numerical form. Automatic
programming is accomplished through the use of
motion picture films which control a television presen-
tation to the student. Automatic recording is accom-
plished through use of a series of timing devices. The
ASG-15 demonstrates the sophiscicacion thac can be
achieved with relatively simple and inexpensive train-
ing equipment. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
ENVIRONMENTAL FACTORS INFLUENCING
METALS APPUCATIONS IN SPACE VEHICLES, by
J. M. Allen. Rept. on Contract AF 18(600)1375.
1 Dec 60. 49p. 34 refs. DMIC rept. 142.
Order from OTS $1.25 PB 151 101
Metals will be used extensively both in the vehicle
struaure and in the supporting and auxiliary equip-
ment that is used for space flight. This report de-
scribes Che specialized environments which are im-
posed on metals and the possible consequences of
these environments. In general, the specialized
environments are identified with (1) the natural en-
vironment of space, (2) the entry into an atmosphere,
or (3) the power -conversion system utilized by the
vehicle. (Author)
Diamond Ordnance Fuze Labs., Washington, D C.
ACCELEROMETER MEASUREMENTS AND PRO-
JECTILE PARAMETERS, by H. J. Rosenberg.
17 Nov 60, 32p. 4 refs. Technical rept. TR-857.
Older from LC ml$3. 00, ph$6. 30 - PB 152 917
The limitations of an accelerometer in themeasure-
tnent of projectile acceleration, velocity, and dis-
placement are discussed. The design limitations of
the instrument, the errors of the associated inte-
gration process, and the presence of vibration and
gravity cause the accelerometer reading to deviate
from the true value. (Author)
Diamond Ordnance Fuze Labs. , Washington, D. C
DEVELOPMENT OF A SPLIT IGNITER FOR INITI-
ATING GASLESS INLAYS, by Ira R. Marcus.
14 Nov 60, 39p. 13 refs. Technical rept. TR-875.
Order from LC mi$3. 00, ph$6. 30 PB 152 654
An investigation has shown that burning time dlsper-
ik»s in UMNOL gas less delay mixtures can be caused
by the A-l-A igniter used co Initiate diem. The mech-
anism of this igniter effect is not understood but tests
have shown chac when A-l-A is used in the input posi-
tion, it can penetrate die delay mix and ignite it below
itt surface. A-l-A igniter does not cause time dis-
persions when it is used in the output position, to
transfer ignition from the delay co Che nexc element in
the fuze train. A split input igniter made of two dif-
ferent compositions of zirconium, barium chromate.
and superfloss powders has been developed to elimi-
nate the penetration and thus reduce the time disper-
sions attributed to A-l-A. One of these composicions
is suicable as an output igniter. Complete specifica-
tions for manufacturing these igniters are included.
(Author)
Diamond Ordnance Fuze Labs. . Washington, D. C.
LONG PERIOD CURPISTOR-C»ODE TIMERS, by
John O. Thayer. 29 Nov 60, 17p. 7 refs. Technical
rept. TR-895.
Order from LC mi$2. 40, ph$3. 30 PB 153 478
Relaxation-type oscillators for timing purposes have
been developed that provide useful output pulses at
races from one pulse per mlnuce co three pulses per
day. Methods of accumulating these pulses to produce
time delays of up to 1 year are discussed. The pri-
mary oscillator components include a curpiscor, a
mylar or polyscyrene capacicor, an XD-IC cold-cath-
ode diode, and a resisdve compensating device. IXie
to the current-regulating curpistor, the variations in
timer pulse repetition rate are relatively independent
cf changes in the low-current battery supply voltage.
Supply voltage changes of up to 1 30 percent cause a
curpistor current change within il percent. Time
variations caused by temperature changes between
-40OC and 55°C are within kb percent for the longest-
period timers tested. Applications for this device
include (a) single delay device, (b) generator for an
electromechanical or magnetic core accumulator for
use in fuze timing, (c) other long-period timing de-
vices. (Author)
Feltman Research Labs. , Picatlnny Arsenal,
Dover, N. J.
DETERMINATION OF BEST SPOTTING COMPO-
SITION FOR OBSERVATION OF HONEST JCHIN, by
John E. Andrews, Jr. and Leo J. Frey, Jr. Nov 60,
40p. 16 refs. Technical rept. FRL-TR-17.
Order from LC mi$3. 00. ph$6. 30 PB 150 097
Out of 9 spotting compositions and 3 explosives tested
in the laboratory, spotting composition 580 (40%
atomized aluminum, 60% barium nitrate) was chosen
as relatively safe to handle and use. It withstood a
40-foot drop test when packed and did not detonate
when exposed to a fire. Field tests showed that 3
pounds of spotting charge wUl provide 95%detectiOTof
the smoke and flash at 15 miles (kj a bright hazy day.
The bomb-type (spherical flash) vehicles used In these
tests were found to be only half as efficient as
standard-type spotting devices (which produce a coni-
cal flash). For reliability, two spotting devices, ISO©
apart and each confalning a 1. 5-pound charge, were
used in the final design. Of the various types of
Instrumentation normally used to observe the Honest
John (binoculars, battery command scopes, and aim-
ing circles), the M65 battery command scope was
found most efficient for detecting the flash and smoke,
and the binoculars were found least efficient. Static
test results substantiated the following relationship
between weight of charge and total integral light:
Total integral light - KiWK2. Values were obtained
for Kj and Kj for each spotting composition tested.
(Author)
437
Fehman Reaearph Labs. , Picatimiy Arsenal,
Dover, N- J.
HANDUNG PROftRTIES OF THE MONOPROPEL-
LANT SYSTEM to/40 ETHYL NITRATE /n- PROPYL
NITRATE, by Daniel R. Satriana, Frank]. Masuelli.
and Ernest F. Siavenson. Nov 60, 20p. 13 refs. Tech-
nical repc. FRL-TR-18; AD-247 121.
Order from LC nti$2.40, ph$3.30 PB 152 316
The monopropell^nt system 60/40 ethyl nitrate/n- pro-
pyl nitrate was si^bjected to various tests. In short-
term stability tests, no brown fumes were noced in 30
hours at 96% or in 64 hours at 65%. Compatibility
with various metals, sealers, polyethylene, and rubber
was found to be satisfactory at ambient and elevated
temperatures. However, some propellant was ab-
sorbed by the poltethyiene and, at the elevated tem-
perature, a film tormed on the brass and aluminum
samples. The autjo- ignition temperature and the flash
point of the propellant were 192°C and 65% respec-
tively. Propellanij sealed in 37 mm cartridge cases
neither detonated {nor burned in the 40-foot drop test.
When subjected t0 . 30 caliber rifle bullet fire, it
burned but did noc detonate. Propellant sealed in pipe
bombs detonated qhree times in three trials when im-
paaed with a . 30 jcaliber rifle bullet. No action was
observed in frictipn sensitivity tests. Electrostatic
sensitivity tests ifidicated that serious hazards might
exist in the handlijng of large quantities of the mono-
propellant. Thixdin, nitrocellulose fibers and ball
po<wder are satisfactory gelling agents for the mono-
propellant. The tfurning rate was decreased 1/3 by' the
use of the nitrocellulose and the ball powder and wa^
increased 7 time^ by use of the Thixcin formulation.
(Author)
Picatinny Arsenal,
Feltman Researi:h Labs
Dover, N. J.
AN INTERPRETATnON OF THE
EXPLOSIVES, by
Dec 60, 13p. 2 t
Order from LC nnl$2.40. ph$3.30
SENSmVTTY OF
Rufus C. Ling and Werner R. Hess.
Technical rept. FRL-TR-21.
PB 153 111
An attempt is ma
data on the basis
the explosive mi
probability is cL
active sites amon
ternal energy
biliiy of ignition i
to interpret explosive sensitivity
if the distribution of active sites in
um. It is assumed that the ignition
ly controlled by the population of
the crystallites affected by the ex-
ce. An expression for the proba-
u established and discussed.
Picatinny Arsenal,
Feltman Research Labs.
Dover, N. J.
STANDARD LABCJRATORY PROCEDURES FOR
SENSITIVITY, BRJSANCE AND STABILITY OF EX-
PLOSIVES, byArAurJ. Clear. Jan 61, 45p. Tech-
nical rept. FRL-1[R-25.
Order from OTS $|l . 25 PB 171 326
The deuiled procedures given in Picatinny Arsenal
Technical Report No. 1401, Rev 1 (PB 116 184) for
standard laboratory tests to determine the sensitivity,
brisance, and stability of high explosives, primes,
pyrotechnic compqsitions, and propellants have been
reviewed and revised to bring the methods up to date.
Accordingly the directions for several of the proce-
dures have been mpdified wherever necessary to in-
clude details whicn have been found to be important.
Procedures which ^re either obsolete or seldom used
have been omitted. (Author)
Flight Accessories Lab. . Wright Air Development
Div. , Wright -Patterson AFB. Ohio.
GAS CYCLE COOLING SYSTEMS FOR SPACE VB-
HICLES, by T. D. Moseley. Rept. on Aircraft Air
Conditioning. June 60, 23p. 3 refs. WAIX) Technical
note 60-66; AD-245 325.
Order from OTS $0. 75 PB 171 363
This study was to determine the conditions when gaa
cycle cooling systems require the smallest radiatora,
and to compare these requirements with a passive cool-
ing system. For a one kilowatt cooling load, the power
unit's radiator temperature was held constant at IfXPf
while the cooling system's radiator temperature waa
varied from 58 to 950^. Cooling systems providing
temperature control for both cabin and electronic
equipment compartments were considered. Air and
hydrogen, representing low and high specific heat
gases respectively, were evaluated. Radiator size de-
creased with an increase in radiator temperature, ex-
cept when the radiator area required for a power unit
to drive the cooling system was considered. Since the
smallest radiator was obtained with the simple passive
cooling system, gas cycle cooling systems were con-
sidered undersirable for space vehicle applications. ,
(Author)
jet Propulsion Lab. , Calif. Inst, at Tech. ,
Pasadena.
THE TEMPERATURE OF AN ORBITING MISSILE,
by A. R. Hibbs. Rept. on Contract DA 04-495-
ORD-18. 28 Mar 56, 23p. 3 refs. Progress rept. na
20-294.
Order from LC ml$2. 70, ph$4. 80 PB 153952
This report released for sale to the public 2 Jan 61.
The successful operation at radio equipment carried
In an orbiting missile requires fairly close control
over the temperatures to which the equipment Is sub-
jected. This temperature Is controlled by two factors.
First, the temperature al the outer shell of the
missile depends on radiative transfer between the
missile and its environment (sun, earth, and empty
space). Second, the temperature of the equipment in
side the missile depends on heat transfer from the
shell (directly by radiation, and through the structure
by conduction). The analysis presented shows
(1) how the average temperature of the outer shell can
be controlled (for a given missile shape, orientation,
and trajectory) by a correct choice of surface coat-
ings, a^ (2) that that the limits of temperature vari-
ation al the enclosed equipment can be held to within
a few degrees d this average shell temperature by
adequate insulation. Numerical calculatlcms are pre-
sented which indicate the necessary characteristics of
the coating and Insulating materials. (Author)
Lincoln Lab. , Mass . Inst, of Tech. , Lexington.
SOME RESULTS OF ESTIMATING SATELUTE ELE-
MENTS FROM MILLSTONE -HILL AVERAGED DATA,
by Hans. D. Fridman. Rept. on Contract
AF 19(604)7400. 2 Nov 60, 32p. 3 refs. 22G-0039;
AD-246 781.
Order from LCmi$3. 00, ph$6. 30 PB 153 220
The Millstone Hill site of the Lincoln Laboratory is a
tracking facility from which raw radar data and data
438
averaged over intervals of time were obtained . In order
to make use of the raw radar data averaged over a num-
ber of time intervals a programming facility that calcu-
lates the satellite orbit parameter from the known posi-
tion and velocity of the satellite at a given time of
observation was constructed. The system by which the
radar data on the satellites was acquired, the tech-
niques by which the data has been filtered and smoothed,
and the programming system that made use of this data
to evaluate the technique of estimation are described.
(Author)
Lincoln Lab. , Mass. Inst, of Tech., Lexington.
WEST FORD ORBIT DETERMINATION, by A. A.
Mathlasen. Rept. on Contract AF 19(604)7400.
2 Nov 60, 19p. 21G-0028; AD-246 777.
Order from LC mi$2.40, ph$3.30 PB 153 219
The IBM 7090 West Ford Orbit Determination program
accepts geocentric coordinate data, from which it
determines the orbit parameters (semi-major axis,
eccentricity, argument of perigee, inclinatior, longi-
tude of ascending node, epoch of nodal crossing) ex-
isting, and presumed constant, during the time inter-
val of the data. These parameters are then made
available to other programs. (Author)
Lincoln Lab. , Mass. Inst, of Tech., Lexington.
WEST FORD STATISTICAL ORBIT PREDICTION
PROGRAM, by W. R. Crowther. Rept. on Contract
AF 19(604)7400. 2 Nov 60, 6p. 21G-0027, supersedes
210-0019; AD-246 778.
Order from LC mi$1.80. ph$1.80 PB 153 218
A program was written to perform statistical predic-
tion of orbit parameters. It accepts many sets of
orbit parameters and determines a least mean squares
fit of each parameter to a polynomial with time as its
variable. The polynomial may be chosen to be a con-
BUnt, linear, or quadratic by a control card. (Author)
Lockheed Aircraft Corp. , Sunnyvale, Calif.
INTERPLANETARY MANEUVERS USING RADIAL
THRUST, byC. M. Petty. Technical rept. on Mathe-
matics. Aug 60. 23p. 4 refs. LMSD-703036;
AD-241 227.
Order from LC mi$2. 70, ph$4. 80 PB 153 055
Basic Interplanetary maneuvers are considered, with
emphasis placed on simplicity in Instrumentation.
First, a general theory of radial thrust is developed
geometrically, since it reveals a proper perspective of
the opportunities and limitations of the theory. The
special case of constant radial thrust acceleration is
treated in detail. Finally, an example of a Martian
capture maneuver is given where the initial portion of
the maneuver has constant radial thrust acceleration
•nd In the terminal portion the thrust acceleration
varies to maintain constant radial speed. The asso-
ciated characteristic velocity and other parameters
are computed. (Author)
Naval Ordnance Test Station, China Lake, Calif.
RANGES FOR TRAINING AIRCRAFT HLOTS IN
SPECL^L-WEAPON-CEUVERY TECHNIQUES, by
Everett B. Hill and Elaine Nowak. 1 Sep 60, 42p.
NOTS TP 2343: AD-246 254.
Order from LC mi$3. 30, ph$7. 80 PB 153 086
This report describes instrumentation designed and
developed for aircraft ranges ueed in training pilots in
low-level speclal-weapon-delivery techniques. Range
operating procedures, raige personnel requirements,
and instrumentation costs are discussed. (Author)
North Carolina State Coll. , Raleigh.
THE APSIDAL MOTION OF THE ORBIT OF AN
EARTH SATELUTE, by Raimond A. Struble.
Technical memo. no. 3 on Contract DA 36-034-ORD-
2733. Mar 60, 12p. 14 refs . OOR rept. 2125. 6-M.
Order from LC mi$2.40, ph$3.30 PB 150 702
Using the equations of motion for an earth satellite de-
veloped previously, a study of the motion of the line of
apsides of an orbit is presented. Though this study rep-
resents but one aspect of a general theory of motion
now in preparation, the results are sufficiently novel to
warrant this singular announcement.
Physical Research Lab. , Space Tech. Labs. , Inc. ,
Los Angeles, Calif.
INSTRUMENTATION FOR MAGNETOAERODYNAMIC
HEAT TRANSFER, by Richard W. Ziemer. Rept. on
Thermonuclear Propulsion Research, Contract
AF 04(647)309. 8 Sep 60. 39p. 16 refs.
STL/TR - 60- 0000- 09290 .
Order from LC mi$3.00, ph$6.30 PB 152 829
An experimental technique is described for directly
measuring the stagnation point heat transfer rate to an
aerodynamic model in an electromagnetic shock tube.
The application to measuring the reduction in aerody-
namic heating by magnetoaerodynamic means is
specifically considered. The development of the in-
strument is discussed, and the successful results of
preliminary experiments are reported. It is concluded
that the technique is practical for magnet oaerodyrjanUc
heat transfer measurements and that the present
apparatus could be used to study radiative heat trans-
fer from ionized gases. Recommendations for future
research are presented. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
A REALISTIC APPROACH TO PROBLEMS OF OPTI-
MUM ROCKET TRAJECTORIES, by Samuel E.
Moskowitz and Lu Ting Rept, on Contract
AF 49(638)445. Oct 60, 18p. 3 refs. PIBAL rept. no.
625; AFOSR-TN-60-1342: AD-247 226.
Order from LC mi$2. 40, ph$3. 30 PB 153 388
This report suggests an approximate method foranaly
zing problems of optimum rocket trajectories in a
plane for which the vehicle experiences minimum
flight time or attains maximum altitude. Included
within the scope of this report are such questions as
an expedient form of the governing equations entering
Into the functional, when the maximum values of lift
and drag forces are significant. (Author)
439
PouJter Lab«. , gtanford Research Inst. , Menio Park,
Cam. I
LUMINOSITY yrVCHES OF HIGH VELOCITY IM-
PACT, by D. D. I^eough. Final rept. on Contract
AF 19(604)5572. 112 Oct 60, 25p. 12 refs. SRI ProJ.
no. GU-2858; AFCRL-TR-60-415.
Order from LC nii$2. 70, ph$4. 80 PB 153 316
An experimental investigation of the light associated
with the impact o( high velocity microparticles is
described. A system capable d producing velocities in
the range erf 4-5 rtxm/psec and ot observing the impact
effeas by means othar than terminal observation has
been achieved. Multiplier phototube results indicating
the energy associ^ed with the phenomenon at varying
pressures are reported. A short duration pulse con-
sisting of a fast rise portion followed by an appropri-
ately exponential decay is observed. All work was
performed in an anr atmosphere ranging in pressure
from atmospheric! to* 16^ A possible source of
luminosity is disoussed briefly. The velocity range of
calibration erf a nrKicrometeorite deteaor has been ex-
tended, with the result that the impinging particle
momentum vs detector microphone output is found to
be linear. (Authoi)
Space Sciences I ab. , General Electric Co. ,
Philadelphia, Pal
LUNAR TRAJECnORY STUDIES AND AN APPLICA-
TION TO LUNIK nil TRAJECTORY PREMCTION, by
A. Petty and I. Ju^kevlch. Scientific rept. no. 1 for
15 July 60 on Contract AF 19(604)5863. July 60, 109p
12 refs. AFCRL-rN-60-1132; AD- 247 577.
Order from LC miS5.70. ph$16.80 PB 153 492
The study covers ^ee relatively closely connected
areas. These arei (1) Design of a fast, accurate, and
efficient computer; program for computation of lunar
trajectories. (2) An application of the resulting com-
puter program to An error analysis of specific lunar
trajectories and ta the determination of some actual
trajectories. As s^ example the trajeaory of
LUNIK in has bee|i considered in detail. (3) Tracking
program (determliiation al initial conditions to be used
in the equations of|motion). (Author)
Sanitation 1 and Safety Engineering
Araic Aeromedldal Lab. , Ladd AFB, Alaska.
CONTINUATION OF FACTORS AFFECTING WATER
PURIFICATION, b) Lester Baribo. Dec 57, lOp.
Technical note AAL-TN-57-5.
Order from LC mill . 80, ph$l .80 PB 153 546
The work has been extended to determine the effect ot
pH on the disinfecting action of chlorine, iodine, and
colloidal silver. The effects of various other faaors
affecting the action of colloidal silver are also
reported. (Sec alsd PB 153 519)
Arctic Aeromedicil Lab. , Ladd AFB, Alaska.
FACTORS AFFECTING FIELD WATER PURIFICA-
TION, byL. E. Batibo. Dec 56. I6p. Technical
rept. AAL-TN-56-13.
Order from LC mi$2.40, ph$3.30
This study was begun to determine what physical and
chemical factors are important to sterilization of water
under field conditions in Alaska.
Ballistic Research Labs. . Aberdeen Proving Ground.
Md.
DEVICES FOR REDUCING BLAST EFFECTS IN
VENTILATING SYSTEMS, by William J. Taylor,
Wesley E. Curtis, and Robert O. Clark. Feb 54, de-
classified 5 Aug 57. 36p. 6 refs. Technical note
no. 869; AFSWP no. 730.
Order from LC mi$3.00, ph$6.30 PB 154 406
This report released for sale to the public 15 Feb 6L
Results of shock tube tests on ten model ventilator
designs are reported showing their relative effective-
ness in reducing the passage of air shocks. A muffler
type ventilator is described which is the most efficient
of the designs tested In preventing the passage of air
shocks into ventilating systems and reducing the high
velocity air flows. (Author)
i
Ship Building
David Taylor Model Basin. , Washington, D. C
ON THE STRUCTURAL DESIGN OF THE MIDSHIP
SECTION, byM. St. Denis. Oct 54, 108p. 29 refs.
Rept. C-555.
Order from LC mi|5.70, ph$16.80 PB 153 953
This report released for sale to the public 8 Feb 61.
A consistent and integrated procedure is presented for
carrying out systematically the structural design of the
midship section of a naval vessel. The report is writtea
in two parts. In the first part the problem is considered
in a general manner and the specific theories and
methods used in the procedure are introduced. In the
second part an illustrative example is worked out for u
idealized vessel embodying the simplest possible struc-
ture sufficient to illustrate all the points discussed.
(Author)
David Taylor Model Basin, Washington, D. C.
SEADAC THE TAYLOR MODEL BASIN SEAKEEP-
ING DATA ANALYSIS CENTER, by Wilbur Marks and
Paul E. Strausser. July 60, 53p. Rept. 1353;
AD-245 156.
Order from LC ml $3. 60, ph|9. 30 PB 152 689
The Taylor Model Basin Seakeeping Data Analysis
Center (SEADAC) is described. The methods for
preparation, analysis, and storage of data are outlined.
Coirfldence In the system is demonstrated by compari-
son at SEADAC compuution of the spectral density of
certain seakeeping events with numerical calculation
al the same data. The limitations at the SEADAC are
listed and changes that will improve the system's ef-
ficiency and extend its capabilities are suggested.
(Author)
PB 153 519
440
Nitlonal Research Labs. , Ottawa (Canada).
A SIMPLE APPROACH TO THE MATHEMATICAL
SHIP FORM, by P. A. Hamill. Sep 60. 22p. 2 refs.
lylechanical Engineering rept. MB-225.
Older from LC mi$2. 70, ph$4. 80 PB 153 632
Current work on mathematical ship forms is de-
scribed. Available solutions of the problem of fitting
• nirface equation to an arbitrary ship are compli-
cated and of limited use. It is desirable that analyti-
cal forms be introduced in the design stage, to pro-
vide a concise description of the hull and also to as-
sist in the design. A very simple process, whereby
certain initial design conditions are mathematically
(aired, is developed and tested on the forebody of a
fine form. The resulting surface would be acceptable
ta a ship hull. It is suggested that this approach to
•hip design nf>ay offer considerable advantage and
■bould be pursued further. (Author)
Naval Research Lab. . Washington. D. C
SHOCK DESIGN OF SHIPBOARD EQUIPMENT. PART I.
DYNAMIC DESIGN -ANALYSIS METHOD, by R. O.
Belsheim and G. J. O'Hara. 16 Sep 60, 59p. 8 refs.
NRL rept. 5545; AD-243 497.
Onter from LC mi$3. 60, ph$9. 30 PB 149 520
A design -analysis method is presented for the calcula-
tion of the shock response of naval shipboard equip-
ments which are not installed on non-linear shock or
vibration mounts. It is essentially a simplified model
analysis method where the design shock inputs have
been empirically obtained from realistic underwater
C3q>loflion tests, as reinforced by information obtained
from theoretical and laboratory studies. The method
allows variations in the complexity of atialysis depend-
ent upon the importance classification of the equipment
by the Navy. Differing energy-absorption capacities
for different geometries and loadings, when some plas-
ticity can be allowed, is permitted by the use of an
effective yield stress as the failure criterion. Several
simple numerical examples are worked out in detail
closely following the step-by- step procedure outlined
(complete with appropriate formulas) in the main body
of the text. (Author)
FOOD, HANDLING, AND PACKAGING
EQUIPMENT
Food
Alaska U. , College.
THE AVAILABILITY OF EDIBLE PLANTS AND
ANIMALS TO THE SURVIVOR IN THE ARCTIC AND
SUBARCTIC, by Wilbur L. Libby. Rept. on Contraa
AF 41(657)28. Dec 56, lOp. I ref. Technical note
AAL-TN-56-34.
Order from LC mil 1.80, ph$ 1.80 PB 153 540
TUs note is designed to inform workers in the sur-
vival fields that this project is underway, of the means
by which it is being accomplished, and to elicit criti-
dams of the methods being employed. The objectives
of the project are to determine the amount of each
environmental type in Interior Alaska, and to deter-
mine the plant aind animal composition of these types
on a qualitative and quantitative basis with particular
emphasis on the availability of survival food.
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
NUTRITI(»4AL SURVEY AT ANAKTUVUK PASS, by
Horace P. Drury, Miriam Hall and others. Dec 56.
9p. 4 refs. Technical note AAL-TN-56-17.
Order from LC mi$L 80, ph$l. 80 PB 153 523
The inhabitants cf Anaktuvuk Pass eat substantially the
same number of calories with almost exactly the same
percentage of fat, and have about the same cholesterol
iqtake as the inhabitants of Ladd Air Force Base.
hfoWever, the Eskimos eat much more protein and
much less carbohydrate.
Araic Aeromedical Lab. , Ladd AFB, Alaska.
RECONSIDERATION OF PEMMICAN AS AN EMER-
GENCY RATION, by Horace F. Drury. [1956] 5p.
2 refs. Technical note AAL-TN-56-6.
Order from LC mil 1.80, ph$ 1.80 PB 153 512
The undeniably adverse effects of pemmican alone are
due to low blood sugar. This can be alleviated by the
periodic administration of very small doses of carbo-
hydrate. The amount of sugar normally consumed in
coffee or tea would make an appreciable difference. It
should be possible to formulate a satisfactory emer-
gency ration based largely, but not exclusively, on
pemmican comix>sed of dehydrated meat and fat. When
wrapped simply in foil, this should have a caloric
density almost double that of any currently standard
ration. (Author)
Packaging
Naval Supply Research and Development Facility,
Bayonne, N. J.
TRANSPARENT PACKAGING, by S. Stambler, C. Katz
and S. Gordon. 3 May 60, 79p.' Engineering rept.
no. 2.5082; AD-246 081.
Order from LC miH SO, ph$12. 30 PB 153 198
This report presents the results of a study to evaluate
transparent films for packaging applications. It was
determined that no one film could be used as an all
purpose military barrier material. Four mil low
density polyethylene and laminations of mylar and poly-
ethylene may be used as additional military barrier
materials and provide the added property of trans-
parency. Performance requirements based on the
needs of the military supply system were developed
for transparent films. (Author)
Thompson. John I., and Co. , Washiigton, D. C.
INDIVIDUAL ALUMINUM FEEDING CONTAINERS.
PART I. ENGINEERING EVALUATKW PHASE. Rept.
for 1 Mar -25 Mar 60 on Equipment for Life Support in
Aerospace, Contract AF 33(616)7080. Aug 60, 25p.
22 refs. WADD Technical rept. 60-522(1); AD- 246 377
Order from OTS 10.75 PB 171 418
441
An evaluation was hiade of materials and techniques
for fabricating a'fqod container to be used in space
flighr. Requlremeics were tqr a 6- ounce rectangular
aluminum container, and associated equipment: a
mouthpiece, and q<iick opening, expelling, and hand
sealing devices. A comprehensive literature search
supplemented by personal interviews in industry and
other interested activities surveyed the present state-
of-the-art in the fcjod conning, container fabricating,
and related indu8ti:ies. It was concluded that after
further design 8tuc)y, complex reaangular, aluminum
containers and associated equipment can be produced
using present mat^ials and techniques. Pure alunU-
num alloys are the best container materials; impact
extrusion the most, promising process; and brazing
and resistance weltiing the heat methods for Joining
thin- walled aluminiim components. Many protective
coatings are available to prevent chemical reaction be-
t<veen the container and its contents. Quick opening
devices can be adopted from industry-developed
openers. Plastics are available for the mouthpiece.
Specific materials and techniques for the associated
equipment require 'further design study. (Author)
MACHINERY, FABRICATION, AND
ACCESSORY EQUIPMENT
Franklin Ins. Laos, for Research and Develo{»nent,
Philadelphia, Pa.]
PERTURBATION ANALYSIS OF THE STABILITY OT
SELF-ACTING, GAS- LUBRICATED JOURNAL BEAR-
INGS, by Vittorio Castelll and Harold G. Elrod, Jr.
Interim rept. on extract Nonr- 2342(00). Feb 60,
30p. 21 refs. Repri.no. I-A2049-II; AD-234 380.
Order from LC mli2.70, ph$4.80 PB 153 128
The dynamics ot a gas- lubricated Journal bearing are
studied by using Reynold's equation and the Lag^rangian
equations ot motloq. This system of equations is then
linearized by the perturbation method. The stability
of Che bearing is then investigated by studying the
location in the conrplex plane of the roots of the char-
aaeristlc determiriant of the solution of the system of
governing equationfe. (Author)
George Washlngt(Jn U. , Washington, D. C.
DETERMINING THE SEE OF AN OCEAN SHIPPING
PIPELINE MEETING A TIME-PHASED MILITARY
REQUIREMENT SCHEDULE UNDER CONVOY CCW-
DmONS, by Ralpt:^ B. Hunt and Erling F. Rosholdt.
Rept. on Logistics Research Project, Contraas Nonr-
761(05) and (06). 1(7 Feb 60, 34p. 1 ref. Serial
T- 113/60; AD- 232 656.
Order from LC mlS3. 00, ph|6. 30 PB 153 145
Consideration was given to the size of an export ocean
shipping pipeline needed to meet a time-phased mili-
tary lift requiremetit schedule under conditions re-
quiring the ships to sail in convoys. The resulting
algorithm and tables that are presented are intended
for manual computation use. The algorithm minimizes
the choice ol alternatives that must be made to es-
tablish the magnituiles at the ship pipeline require-
ments through the (ime-phasing operation. The logic
of the decision rul^s represents a. difficult oroblemfo!
computer programming short al a brute force ap-
proach and is a suJ^Ject for future work. (Author) ^2
Engines and Propulsion Systems
Aerojet-General Corp. , Azusa, Calif.
CHARGED- OOLLaO PROPULSON SYSTEM, by
R. B. Edmonson, C. B. Kretschmer, and L. B.
Becker. Quanerly rept. no. 1 on Contract
AF 49(638)656. Nov 60, I7p. Rept. no. 0290-01-1;
AFOSR-TN-60-1454.
Order from LC mi$2. 40, ph$3. 30 PB 153 441
Research is summarized on the electrostatic spraying
of microscopic droplets of oil. The research is di-
rected toward an undersunding of the mechanisms of
charge accumulation and electrostatic spraying in high
electrical fields. This understanding is necessary for
subsequent adaptation of the phenomenon to use in high-
efficiency, low-thrust propulsion applications . The
work has been directed primarily to the measurement
of charge-to-mass ratios and particle size distribu-
tions . Effective spraying of Octoil with an additive of
tetra-n-butvl ammbnium has been attained at a pres-
sure of 10*"-mm Hg utilizing a porous non- conductive
element for feeding the liouid propellant oil mixture.
(Author)(See also PB 146 178)
Air Force Missile Development Center, HoUoman
AFB, N Mex.
RELATIVISTIC TREATMENT OF ROCKET PROPUL-
SION WITH FAST PARTICLES AND PHOTONS
TAKING INTO CONSIDERATION NUCLEAR DATA,
byT. Foel8che(U. of Frankfurt-Main). Mar 59, 26p.
6 refs. AFMEX: TR-59-4; AD- 209 328.
Order from LC mi$2.70, ph$4.80 PB 150 719
Only normal maner is available in sufficient amounts,
and it reacts with a maximum mass conversion factor
of only 9/1000 for nuclear -physical reasons. This
fact limits the end velocity of a rocket to a few tenths
of the velocity erf light, so that relativlstlc velocities
and an essential time dilatation cannot be attained.
Ballistic Research Labs . , Aberdeen Proving Ground,
Md.
AN EXPERIMENTAL STUDY OF COMBUSTION IN-
ST ABlUTY IN SOLID ROCKET PROPELLANTS.
PART II, by Leland Watermeier. Sep 60, 67p.
18 refs. Rept. no. 1116. ,
Order from LC miJ3 . 90 . ph$ 10 . 80 PB 1 53 493
Double base and composite rocket propellant slabs
were burned in a transparent - walled vessel which
was vented to the atmosphere through a nozzle. The
propellants were burned at chamber pressures of
200-800 psi . Pressure waves nornwl to the burning
surface were produced by a siren at frequencies of
100- 1400 cps. Photographs and pressure records re-
vealed an increased burning rate in double base pro-
pellant as the resonant frequency of the chamber was
approached. In aluminized pro{>ellants , the burning
aluminum panicles agglomerated on the surface and
left as globules whichbroke up the normal flame zone.
(Author) (See also PB 143 263)
Dynamic Analysis and Control Lab. , Mass. Inst, of
Tech. , Cambridge.
FRICTION DRAG ON BLAC«D DISCS IN HOUSINGS
AS A FJJNCTION OF REYNOLDS NUMBER, AXUL
AND RADICAL CLEARANCE AND BLAC« ASPECT
RATIO AND SOLIDITY, by Robert W. Mann and
Charles H. Marston. Rept. on Contract AF 49(638)289.
31 Dec 59, 16p. 7 refs. Rept. no. 124; AFOSR TR-
60-95: AD- 244 482.
Order from LC mi$2.40, ph$3.30 PB 152 525
Extra losses from partial acknission operation of a gas
turbine occur both in the nozzle flow arc and away
from it . The latter have been related to the theory of
Quid flow over a rotating disc expressing a dimension-
less moment coefficient as a function of Reynolds num-
ber. By direct measurements of drag torque, the
moment coefficient has been determined over a range
of Reynolds number from 2. 0 x 10* to 4. 5 x 10^ for
•everal aspect ratios, axial and radial shroud clear-
ances, and solidities. Losses increase with increasinj
aspea ratio. Small increases from minimum practical
clearance have little effect, but blade pumping losses
become severe at radial and axial clearances of the
order of half the disc radius. Typical changes in
■olldity have only small effects on losses. (Author)
Michelson Labs. , Naval Ordnance Test Station,
China Lake, Calif.
A NEW RESEARCH TOOL: THE TRANSPARENT
SOLID-FUEL ROCKET MOTOR, by Henry T. Sampsoa
Oct 60. 9p. Technical Article 7; NOTS TP 2458.
Order from LC mi$l. 80, ph$l. 80 PB 153 286
This article describes a new device by which the burn-
ing pattern of a solid-fuel rocket motor can be ob-
served directly during motor operation, and correlated
with pressure and thrust data also taken from the fir -
ing. The information derived by this tool's use, cou-
pled with knowledge of propellant geometry and pres-
sure and thrust information, will aid the design engi-
neer in correlating conventional theoretical motor-
design parameters with actual performance of a test
motor.
Naval Ordnance Test Station. China Lake, Calif.
COMPARISON OF EXPERIMENTAL AND THEORETI-
CAL PRESSURE DISTRIBUTION CAUSED BY GROUNC
INTERFERENCE EFFECTS ON HORIZONTAL -
WEDGE TEST-TRACK SLEDS, by D. Philip Ankeney.
15 Aug 60, 28p. 5 refs. NOTS TP 2533; NAVWEPS
rept. 7564; AD-245 484.
Order from LC ml$2. 70, ph$4. 80 PB 152 790
Aerodynamic pressure on the underside of two tran-
sonic horizontal -wedge rocket -propelled test sleds is
predicted by simple one -dimensional 'choking theory'
The theoretical prediction is compared to telemetered
pressure data from the two sleds. Good agreement be
tween theory and experiment is obtained despite the
simplifications of the one -dimensional theory. The
problem of obtaining shock -wave attachment in order
to decrease the pressure loads is discussed, and the
beneficial effect of 'bleed area' in promoting shock
attachment is noted. Sled aerodynamic shapes de-
signed to avoid ground interference of choking effects
>re discussed. (Author)
Naval Ordnance Test Station, China Lake, Calif.
THE THEORETICAL COMPUTATION OF EQUILIB-
RIUM COMPOSITIONS, THERMODYNAMIC PROPER
TIES AND PERFC«MANCE CHARACTERISTICS OF
PROPELLANT SYSTEMS, by H. N. Browne and Mary
M. WilUams. 8 June 60, 59p. 7 refa. NOTS TP 2434; *
NAVWEPS rept. 7043; AD- 246 591.
Order from LC ml$3. 60, ph$9. 30 PB 153 181
A computer prograhi has been developed for the cal-
culation of the high temperature thermodynamic prop-
erties and performance characteristics of propellant
systems. This report is a summary of the methods
and equations used in the program which will handle a
maximum a< 12 chemical elements and 70 combustion
products. Flame temperature, chemical composition,
enthalpy, entropy, specific heat ratio and molecular
weight of both the chamber and exhaust, frozen and
shifting equilibrium specific Impulse, boost velocities,
relative boost velocities, thrust coefficient, charac-
teristic velocity, and exhaust gas velocity are com-
puted. The assumptions made, the limitations im-
posed, and the inpu data required for the solution of a
specific problem by use of this program is discussed
in detail. The appendices provide a working guide for
those using the program. (Author)
Naval Ordnance Test Station, China Lake, Calif.
TRANSIENT BEHAVIOR OF ROCKET SLEDS AT
THE TIME C»? STARTING, by D. PhiUp Ankeney.
1 Sep 60, 86p. 12 refs. NOTS TP 2532; NAVWEPS
rept. 7563.
Order from LC mi$4.80, ph$13.80 PB 153 290
An experimental study of the transient response of a
rocket sled having a vertically malaligned center of
gravity and being subjected to sudden thrust by the
ignition of a rocket motor was undertaken. Experi-
mental vertical -force reaction data were obtained from
strain-gage-instrumented front skids of the rocket
sled. The experimental data are compared with the re-
sults from a two-degree-crf-freedom theoretical sled
model which had nonlinearity introduced by skid gapw.
The theoretical model was evaluated on a Mid-Century
analog computer and reproduced the major features at
the experimental data during the transient response
period of 0. 2 sec, representing 2(^ of the burtiing time
of the motor . The theoretical sled model study was cai-
fined to the lowest harmonics of the translational and
pitching motions and their coupled effects . (Author)
Physical Research Lab. . Space Tech. Labs. , Inc. ,
Los Angeles, Calif.
THE STRUCTURE OF AN ELECTROMAGNETICALLY
DRIVEN SHOCK, by Vernal Josephson and Richard W.
Hales. Rept. on Thermonuclear Propulsion Research,
Contract AF 04(647)309. 15 Sep 60, 33p. 9 refs.
STL/TR -60-0000- 1931 3.
Order from LC mi$3. 00, ph$6. 30 PB 152 830
A diagnostic study of shocks produced by an electri-
cally driven conical shock tube shows that high velocity
(30-lOOcm/^sec) ions are accelerated out ahead of the
luminous shock front by high electric fields generated
by "sausage" instabilities in the conical discharge tube.
Further, the hig^ velocity luminous front is produced
by the sequential pinching of the hot ionized gas along
the axis at the discharge tube, in contrast to ' cyrrent
loop" driven shocks in conventional T-tube discharge
configurations. (Author)
443
Manufacturing Equipment and Process**
METAL CUmNO BIBLIOGRAPHY, 1943-1956. I960.
Iv. 18000 refa.
Order from American Society at Tool and Manufactur-
ing Englneerg, 10700 Puritan Ave. , Detroit 38. Mich.
$20.00 I
Supplements 1954 ibibliography by O. W. Boston cov-
ering period 1864tl943 and compiled for purpose o<
reviewing present: state erf the art. Informative ab-
straas provided fbr 5593 seleaed references, foreign
and domeatic, and arranged in 15 major sections by
cutting process. Covers chip forming operations, with
subsections relatitig to Theory, Experimental Tests
and Techniques, and Shop Praaice. Author and de-
tailed subjea indexes provided. (Author)
Army Signal Research and Development Lab, , Fort
Monmouth, N. J.
FERRITE SPHERE GRINDING TECHNIQUE, by John L.
Carter, Edward V. Edwards, and Irving Reingold.
1 June 58, 9p. 3 rffs. USASRDL Technical rept. 2049;
AI>225 462. ■• !
Order from LC n^$l. 80, ph$l. 80 PB 150 706
A unique method ifx accurately and rapidly grinding
small ferrite spheres is described, A standard metal-
lurgical grinder was modified in a manner which enable
the grinding at samples that are spherical to within
0.001 inch. The procedure described makes it unneces
sary to resort to the conventional technique at tumbling
the samples in a Hollow grinding wheel by means d an
air stream. (Aut)K)r)
Carnegie Inst, df Tech. , Graduate School of Indus-
trial Administration. Pittsburgh, Pa.
BUDGET CONTROL AND COST BEHAVIOR, by
Andrew C. Stedry. ONR Research memo. no. 63 on
Planning and Control of Industrial Operations, Con-
tract Nonr- 76001. May 59, 76p. 85 refs. AD- 220 282.
Order from LC nrii$4. 50, ph$l2. 30 PB 150 713
The relations chac might exist between individual per-
formance and aspiration levels and the relations that
might also exist between these variables and the kind
of external goals tvhich are represented by a budget of
the kind commonly employed in management practice
were investigated. Experimental results indicate that
an Implicit budget (where the subject is not told what
goal he must attajn) produces the best performance,
closely followed t|y a medium budget and a high budget.
The low budget, >4hich was the only one which satisfied
the criterion of "Attainable but not too loose" resulted
in performance significantly lower than the other
budget groups.
iifc
Dttense Metals formation Center, Battelle
Memorial Inst. , Columbus, Ohio.
PHYSICAL AND MECHANICAL PROPERTIES OF
SOME HIGH-CTRENGTH FINE WIRES, by D. A.
Roberts. [Rept. (in Contract A F 33(616)7747]. 20Jan61.
21 p. DMIC memo, 80.
Order from OTS 10. 50 PB 161 230
Hi{^-strengdi fine vrires are at Increasing Interest to
the Department at Defense and to defense contractors
and subcontractors as possible materials at construc-
tion in rocket-nxxor cases, pressure vessels, aircraft
cable, high-temperature parachute cloth, and ocber
applications. In spite of this increasing Interest, only
relatively little, widely scaaered information has bea
available. The dau in this memorandum cover wires
o€ 0.010- inch diameter or smaller having tensile
strengths in excess at 250, 000 psl. No effort was
made to evaluate the merits of the different types at
wire for specific applications or to appraise the va-
lidity at the test dau. Copper-base and precious-
metal alloy wires are not included.
Lockheed Aircraft Corp. , Sunnyvale, CaUf .
HIGH- IMPACT METAL FORMING, 1957-1960. AN
ANNOTATED BIBLIOGRAPHY, by A. A Beltran.
July 60, 40p. 130 refs. Special Bibliography SB -60- 25;
LMSD- 703045; AD-241 995.
Order from GTS $1 . 00 PB 171 379
Although explosive forming Is the prime concern ct
this bibliography, articles and reports on hydrospark
farming, electro- discharge machining, impaa extrud-
ing, and the shooting of bolts into metals have been in-
cluded. The sources consulted include the card cata-
log of the Armed Forces Technical Information Agency
the various catalogs at LMSD's Technical Information
Center, and the publications listed below: (1)
Aero/Space Engineering; (2) Banelle Memorial Instl-
tuie. Defense Metals Information Center - Bibliogra-
phy on Explosive Metal Working, Memo No. 51,
7 April 1960; (3) Banelle Technical Review; (4) Crerar
Metals Abstraas; (5) Battelle Memorial Institute, De-
fense Metals Information Center - Selected Acces-
sions; (6) Engineering Index; (7) American Society for
Metals - Review of Metal Literature; and (8) Armed
Services Technical Information Agency - Technical
Abstract Bulletin. (Author)
Princeton U. , N. J.
ECONOMETRIC ANALYSIS OF THE UNITED STATES
MANGANESE PROBLEM. Technical rept. no. 4
(Final rept. pt. 2) on Contract Nonr- 1858(02).
15 Mar 60, 91p. 19 refs. Econometric Research Pro-
gram research memo. no. 14; AD- 237 728.
Order from LC mi$5. 40, ph$15. 30 PB 147 534
Effort was directed towards the determination of the
lowest-cost policy which would provide the United
States' economy with the required quantities of a
certain strategic material, manganese. This pohcy
should enable the requirements to be met over a given
period at time and in view erf various possible politicsl
situations. The faaors taken into account in deter-
mining such a policy were: the various types erf alloys
and the quantities erf them that will be required by the
steel industry, the availability of foreign ores and the
circumstances under which they can be brought to this
country, the availability erf (lower grade) domestic
bres and the various techniques of upgrading them, the
conditions governing the policy of stockpiling ores,
and the various political situations that might arise
during the ten-year period. Two models are pre-
sented which dealt with the manganese problem: a
non- stochastic model which covered a 6 yr period of
"limited war." and a preliminary stochastic model
which took into account possible changes in the politi-
cal situatlan. A description of a more comprehensive
itocfaaatic model and the results obtained from it are
also presented. (Author) (See also PB 143 225)
S^li^ield Armory, Mass.
ULTRASONICS IN THE CHROMIUM PLATING PROC
ESS AND IN COPPER PLATING OF TITANIUM, by
G. Pributsky and W. M, Kisner. 25 Jan 60, 27p.
6 refs. Technical rept. SA-TR16-1116; AE>-246 631.
Ofder from LC ml$2. 70, phK 80 PB 153 223
An investigation was made to determine the effect of
ultrasonic vibrations on the appearance, the adhesion,
and the corrosion resistance of subsequent chromium
plating. An investigation was also made to evaluate
the effect at the use of ultrasonic vibrations during the
electrodeposltion of copper on titanium. Chromium
plated drill rods were ultrasonically irradiated in di-
lute chromic acid in order to passivate the base metal
In tbe pores and cracks at the chromium plate. These
rods were evaluated in a salt spray cabinet. No im-
provement in the corrosion resistance erf the speci-
mens was evident. In all instances the application of
ultrasonics did not prove beneficial. Test procedures
are described and results discussed. (Author)
Watertown Arsenal Labs . , Mass .
DEVELOPMENT OF HIGH WELD-JOINT EFFIQEN- ,
QES IN A WORK -HARDENING STAINLESS STEEL,
by William P. Hatch, George M. Orner, and Warren C.
Malatesta. Oct 60, 68p. 6 refs . Technical rept. no.
WAL TR 648.4/1; AD- 246 835.
Older from LC mi$3.90, ph$10.80 PB 153 263
Work-hardened stainless steel sheet materials are
attractive for missile work because their propenies
include high strength in conjunction with corrosion
resistance and relatively good low-temperature tough-
ness characteristics . A project was initiated with the
objective of making single thickness bun-weld joints
having tensile and yield efficiencies approaching 100%
by cold-working of the weld joint. Techniques involv-
ing cold work at sub-zero temperatures were utilized
to obtain the desired Joint efficiency with tensile fail-
ures occurring in the base metal in 1/16" full-hard 301
stainless steel. Excellent ductility was exhibited in the
immediate vicinity of the fractures with this material
in the high- strength ce>ndition . Additional study of
notch sensitivity is recommended in connection with
any plans for structural applications of this type erf
ibeet material .
Wyman-Gordon Co. , North Grafton, Mass.
EVALUATION OF NUMERICALLY CONTROLLED
MACHINING OF FORGING DIES, by A. H. Swift and
W C. Brunner. Final technical engineering rept. for
Dec 57-Mar 60 on Contract AF 33(600)36176. Sep 60,
Wp. AMC Technical rept. 60-7-667a.
Order from OTS $2. 00 PB 171 378
MMWrlcally controlled machining of forging dies
Pnvlded a superior finish and greater accuracy as
compared to conventional methods erf die sinking. The
continuing development of programming techniques.
specifically the mode of communication between the
human element and the machine, to translate drawing
information into control tapes which direct the tool
aided in moving from simple shapes to more complex
configurations. Seven die blocks were programmed.
Six blocks machined were production forging dies
capable of producing finished forged parts. Former or
blocker dies, which have blended or "faired" surfaces,
were not attempted. Operational problems posed no
particular difficulties after the normal break-in period.
MATERIALS
Watertown Arsenal Labs. , Mass.
SPECTRUM AND CONTOUR ANALYSIS OF ULTRA-
SONIC PULSES FOR IMPROVED NONCCSTRUCTIVE
TESTING, by Otto R. Gericke. Dec 60, 19p. 2 refs.
Technical rept. no. WAL TR 830.5/1.
Order from OTS $0. 50 PB 171 186
A novel technique for obtaining the ultrasonic anenua-
tion/frequency relationship in a single operation Is
suggested and investigated. This new method employs
ultrasonic pulses which contain energy over a wide
band of frequencies, and uses a spectrum analyzer to
detect the frequency dependence of ultrasonic anemia -
tion. (Author)
Ceramics and Refractories
Avco Corp. , Wilmington, Mass .
THE VAPORIZATION AND PHYSICAL PROPERTIES
OF CERTAIN REFRACTORIES. PART I. TECHNI-
QUES AND PREUMINARY STUDIES, by A. A.
Hasapis, M. B. Panish and C. Rosen. Rept. for
1 Oct 59-31 May 60 on Material Thermal Properties;
and Materials Analysis and Evaluation Techniques ,
Contract AF 33(616)6840. Oct 60, 7^. 12 refs .
WADD Technical rept. 60-463, Parti.
Order from OTS $2.00 PB 171 413
The heat of vapcMization of Rh was found to be 129 K
cal/mole in the fange of 2051 to 2205OK by a Knudsen
effusion technique. Interactions between Th02, AI2O3,
and W have been' studied. The viscosity of fused a02
is 104,44 poises at 2560^0 and that of AI2O3 is 13
poises at 2200^0. A continuously nnonitored effusion
apparatus , a null-point effusion apparatus , an oscilla-
ting cup viscometer, and a sessile drop apparatus have
been constructed and calibrated. (Author)
Bell Aircraft Corp. , Buffalo, NY.
INVESTIGATION OF THE FEASIBILITY OF UTILIZ-
ING AVAILABLE HEAT RESISTANT MATERIALS
FOR HYPERSONIC LEAWNG EDGE APPUCATIONS.
VOLUME IV. THERMAL PROPERTIES OF MOLYB-
DENUM ALLOY AND GRAPHFTE, by I. B. Fieldhouee,
J. I. Lang (Armour Research Foundation) and
H. H. Blau (Arthur D. Little, Inc. ). Rept. for July 58-
July 60 on Ceramic and Cermet Materials, Contract
AF 33(616)6034. Oa 60, 86p. 4 refs. WADC Tech-
nical rept. 59-744, Vol. IV.
Order from OTS %2. 25 PB 171 390
445
The purpose of this contraa was to investigate the
feasibility o^ utilUzing available heat resistant mate-
rials in the fabrication of leading edges for hypersonic
boost-glide vehicles. This particular volume jjresents
the results of nueasurements of the thermal conductiv-
ity, specific be^t, linear thermal expansion, and emit-
tance of a 0. 5% titanium alloy of molybdenum, a nd of
siliconized AT] graphite as a function of temperature.
Emittance meadLarements were made on coated and
uncosted materliUs. (Author)
/
Defense MMal4 Information Center, Battelle
MemoriaMnst i , Columbus, Ohio.
REFRACTORY METALS IN EURC»E, by R. I. Jaffee.
[Rept. on Contract AF 33(616)77471. 1 Feb 61, 6p.
[DMIC mamo. 83.
Order from OT^ $0. 50 PB 161 233
Europe is experiencing a surge of activity in refrac-
tory metals. A^ an example, there may be cited the
recent conference on columbium, tantalum, molybde-
num, and tungstfen held by the University of Sheffield
on September l»-20, 1960. Only a month later, mate-
rials specialist^ from NATO countries met in Athens,
Greece, and Ist4nbul, Turkey, to take action on plans
to initiate a cooperative NATO program on refraaory
metals.
J
Douglas Aircr^ Co. , Inc. , Lx>ng Beach, Calif.
INFLUENCE OP ENVIROI^MENT ON CERAMIC
PROPERTIES, by George R. Pulliam and Bruce G.
Leonard. Rept. for May 59-May 60 on Solid State
Research and Properties of Matter, Contract AF
33(616)5875. Oct 60, 30p. 8 refs. WADD Technical
rept. 60-338.
Order from 0T$ $0. 75 PB 171 398
I
This study was (joncemed with environmental andnon-
stoichiometric effects on three different materials.
The materials u$ed were Zr02. AgCl and MgO single
crystals. Definite evidences of low temperature
plastic strain w^re found for O-deficient Zr02. These
evidences were (on- linear stress -deflection curves at
room temperature, appearance of slip lines on large
grains after stress, and creep of Zr02 at 350°C The
creep of polycryistaliine AgCI was tound to be highly
sensitive to electromagnetic radiation. When an AgCl
specimen in cretp was illuminated with 440mu light
the creep rate wfts reduced and light of 700mu caused
the previously reduced creep rate to be increased.
MgO single crys^ls colored brown by u. v. irradi-
ation were found|to have an absorption peak at 4. 3eV
associated with ^ocygen. Ultra-violet irradiation in-
creased the height of this peak so that it tailed off in
the visible region. It is this tailing off that imparted
the brown color to the crystals. Vacuum treatment of
such specimens to 13(X)'^ removed the peak and pre-
vented further coloration by ultra-violet illumination.
(Author)
Little, Arthur I)., Inc., Cambridge, Mass.
STABILITY OF CERAMIC MATERIALS AT TEM-
PERATURES TOi2000PC. by Joan Berkowitz. Rept
for Ju59-Jan 60{on Ceramic and Cermet Materials
Deralofnient, Contract AF 33(616)6154. Sep 60. 68p.
65 refs. WAC© Technical rept. 60-377.
Order from OTS II. 75 PB 171 406
A study was made of the oxidation resistance of a
number of commercial samples of MoSi2 and WSi2 io
the temperature range i600-17(X)oc. A thermal con-
ductivity technique was developed to measure oxygen
pick-up by the samples continuously. Prom the
thermal conductivity measurement and the net weight
change of the samples, an estimate was made of the
rates of formation of volatile and non -volatile oxides.
On the basis of X-ray analysis, oxidation products
are believed to be volatile XO3 (vapor) and non -vola-
tile glass of the form Si^ nXOm where X«Wo or W;
n and m are not known. Tests were conducted at a
total pressure of one^tmosphere in a helium stream
containing about 10 n^m of oxygen and flowing at 119
cc/min. The oxidatii^n of WSi2 was also studied in a
helium stream containing 5 mm of water vapor. The
principal solid product in this case was metallic tung-
sten. (Author)
Manufacturing Labs. , Inc. , Cambridge, Mass.
INVESTIGATION OF DIFFUSION BARRIERS FOR
REFRACTORY METALS, by E. M. Passmore,
J. E. Boyd and others. Rept. for May 59-May 60 00
Finishes and Materials Preservation. Contract
AF 33(616)6354. Aug 60. 59p. 14 refs. WADD Tech-
nical rept. 60-343; AD- 246 559.
Order from OTS $1. 50 PB 171 400
Twenty-three base -barrier metal combinations were
screened by annealing diffusion couples at 1700^15^
Measurements indicating the extent of interdlffusion
between barrier and base metals were made by metal-
lographic examination, microhardness tests, and elec-
tron microbeam analysis. From these measurements,
it is concluded that Hf and Ir are the most pn»nising
barriers for W at 1700OC. with V as a third choice.
Ir appears to be the best choice for Ta and Mo. No
recommendations could be nwde for Cb base metal,
primarily because of melting at the screening temper-
ature. A comparison of interdlffusion behavior with
base -barrier phase relations indicates no correlation
with either solid solubility or presence of intermedtatt
phases. The melting points of both barrier and base
appear to be the most imponant factors affecting the
extent of interdlffusion. (Author)
Metals Research Lab. , Brown U . , Providence, R. I.
RADIATION EFFECTS INVOLVING THE (n,dL)
REACTION IN GLASS CONTAINING BORON, by
Rohn Truell and Constantine Mylonas . Rept on
Contract AF 49(638)450. 1 Oct 60, 35p. 2 refs .
AFOSR-TR-60-160.
Order from LC mi$3. 00, ph$6. 30 PB 153 439
The damage effects produced in 7070 kIsss by means
of the slow neutron reactions with 85"^ have been ex-
amined by means of the measurement of physical di-
mensions, by photoelastic measurements, and by
means of ultrasonic methods . The measurement of
sample lengths as a function of irradiation time or
flux shows that although there are large changes in di-
mensions as the result of annealing, the irradiation
changes are ai>parently independent of the annealing
changes . The curve of length contraction as a functioa
of irradiation flux is not linear. Photoelastic determi-
nation of optical-stress characteristics has been
carried out with higtier precision ttian previously.
446
intrasonic anenuation and velocity measurements are
valuable in annealing experiments but they are not at
present useful for "in reactor" study of damage with
this material . (Author)
National Carbon Co. , Inc. , Parma, Ohio.
RESEARCH STUDY TO DETERMINE THE PHASE
EQUILIBRIUM RELATIONS OF SELECTED METAL
CARBIDES AT HIGH TEMPERATURES, by
R, T. Dolloff. Rept. for Jan 59-Mar 60 on Ceramic
and Cermet Materials, Contract AF 33(616)6286.
July 60, 28p. 13 refs. WADD Technical rept. 60-143;
AD-244 270.
Order from OTS $0. 75 PB 171 365
The work reported is the result of an investigation of
phase equilibria in the ternary system, silicon- boron -
carbon. Techniques for extending the high tempera-
ture range of measurements have been developed.
Accurate phase diagrams for the silicon -carbon and
the boron -carbon binaries have been obtained and de-
tails of the ternary system have been determined in
the high carbon content region. The data were ob-
tained by high temperature differential thermal analy-
sis and by photoelectric thermal analysis, both sup-
plemented by metallographic, X-ray and chemical
techniques. Results for the boron-carbon binary sys-
tem indicate that boron melts at 2130* 10^ and that
B4C has a congruent melting point of 2470* 20PC.
Boron and B4C form a eutectic at 2080^ 20^0, where -
u carbon and B4C form a eutectic at 2390 A 20^.
Results for the silicon -carbon binary indicate a eutec-
tic between silicon and SIC at 1402^ 5°C. SIC melts
incongniently at 25404 4(PC. The peritectic point is
located at 27 per cent carbon. Results for the ternary
system indicate a eutectic between B4C, SiC and car-
bon at 2250* 2CPC. No compound formation has been
oteerved in the high carbon region of the ternary
system. (Author)
Nuclear Metals , Inc., Concord, Mass. ~
REFRACTORY METAL CONS'HTUTION DIAGRAMS,
by A. R. Kaufmann, J. Wulff (Mass . Inst, of Tech.),
A. Taylor (Westinghouse Research Labs .) and others.
Rept. for July 58-30 June 60 on Contract AF 33(616)602.'
Oct 60, 197p. 57 refs. WADD Technical rept. 60-132.
Order from OTS $3.00 PB 171 391
Nine binary constitution diagrams and one ternary con-
stitution diagram of some of the refractory metals are
presented. The binary diagrams include Hf-Mo, Hf-Re,
Gf-W, Nb-Re, Os-Ta, Os-W, Re-Ta, Ru-Ta, Ru-W
«nd the ternary is Re-Ta-W. Care was taken to obtain
reliable diagrams . In particular the purity of the con-
stituents (99.9 percent plus) was protected at all times ,
•nd the temperatures were measured to an accuracy
within 1 20OC . (Author)
Fuels, Lubricants, and Hydraulic Fluids
Army Engineer Research and Developtnera Labs. ,
Fon Belvoir, Va.
DEVELOPMENT OF OPERATICM^AL DISPATCHING
PAQLITY FOR MILITARY MULTI- PRODUCT PIPE-
LINE SYSTEM, by T. H. Jefferson. 29 Apr 60, 69p.
Technical rept. 1626-TR; AD- 239 399.
Order from LC mi$3. 90, ph$ia 80 PB 153 078
Studies were made of methods of dispatching fuel in
multi-product pipeline systems and the design and
fabrication of two prototype op>erational facilities.
Methods studied included graphic method, tabular
method, and stream tape method. Results indicated
that the stream tape method is the most accurate,
most flexible, and easiest to operate, especially for
large numbers of batches of various products and that
it is, therefore, the most desirable for military use.
(Author)
Brussels U. (Belgium).
INFLUENCE OF EROSIVE BURNING ON INTERNAL
BALLISTICS, by J. A. Vandenkerckhove. Technical
note no. 1 on Contract AF 61(052)354. Oct 60, 52p.
15 refs. AFOSR-TN-60-1403.
Order from LC mi$3. 60, ph$9. 30 PB 153 299
Empirical laws do not describe accurately the influ-
ence of erosive burning and the factors influencing the
burning rate without erosion apparently do not retain
their influence in the presence of a hi^ velocity flow.
It is preferable to base internal ballistics computa-
tions on actual experimental data and a method is
proposed for calculating the front pressure as a func-
tion of ccMnbustion to throat, and throat to port area
ratios. The method is rigorous for a constant port
area and it is also shown that a small port area taper
along the grain length does not introduce a significant
error. Finally the problems of constant mass velocity
and constant burning rate designs are briefly
discussed. (Author)
Jet Propulsion Lab. , Calif. Inst, of Tech. , Pasadena.
THE EFFECT OF STRUCTURE ON COMBUSTION
STABILITY OF LIQUID-PROPELLANT ROCKETS
DURING FLIGHT AND DURING STATIC -TEST-
STAND FIRINGS, by Robert S. Wick. Rept. on Con-
tract DA 04-495-ORD-18. 29 July 55. 40p. 4 refs.
Progress rept. no. 20-274.
Order from LC mi$3. 00, ph$6. 30 PB 154 411
This report released for sale to the public 15 Feb 61.
The influence of vehicle structure on combustion sta-
bility in liquid -propellant rockets during flight, when
the mass dlstritxition throughout the vehicle and the
hei^t of propellants in the feed tanks change, is ana-
lyzed. The results of the analysis are discussed with
regard to the possibility of obtaining, during early
stages of the development of a propulsion system,
assurances that the final vehicle into which it will be
incorporated will operate stably in flight. The effect
of test-stand structure on stability is also discussed.
(Author)
Jet Propulsion Lab. , Calif. Inst, of Tech. , Pasadena.
THE EFFECT OF VEHICLE STRUCTURE ON COM-
BUSTION STABILITY IN LIQUID-PROPELLANT ROCK-'
ETS, by Robert S. Wick. Rept. on Contract DA 04-
495-ORD-18. 1 Dec 54, 52p. 15 refs. Progress rept.
20-248.
Order frxjm LC mi$3. 60, ph$9. 00 PB 154 410
This repon released for sale to the public 15 Feb 61.
\
The effect o* vehifcle structure on combustion stability
of liquid -proprtla^ rocket motors h«a not been con-
sidered in preritm analyses. The basic premise of
these analyses hais been that the propellant feed system
is coupled to the tombustion chamber only through the
action of the chamber pressure on the exit of the pro-
pillant feed system. In the present analysis, the fact
dMt the combustion chamber is actually coupled to the
propellant feed system through the structural connec-
tion between the l|eed system and the combustion cham-
ber ia taken into ^count. Thus the rocket n»tor. when
mounted in a vehicle, has several feedback loops in-
■tssd at the single one considered in the conventional
ai^yses. A gene|ral analysis is developed and then
applied to a simplified monopropellant rocket -propelled
vehicle. The effact of the additional loops on cOTibus-
tlon stability in the rocket thrust chamber is shown in
some instances 19 be more important than that of the
parameters whicH in a single -loop analysis are usually
considered to be (he governing quantities. (Author)
Jet Propulsion Ltb , Calif. Inst, of Tech., Pasadena.
SIMPLIFIED METHOD FOR TESTING THE ACCEPT-
ABILITY OF FUMING NITRIC ACID FOR STORAGE
AND USE AS AN OXIDIZER FOR ROCKET FUELS.
by David M. Mas^ and Stephen P. Vango. Rept. on
Contraa DA 04-4p5-ORD-18. 29 Jan 54, I8p. 12 refs.
Progress rept. n<i. 20-229; AD-49 219.
Order from LC nii$2.40, ph$3.30 PB 153 948
This report releaised for sale to the pubUc 1 Feb 61 .
A method employing the measurement of the tempera-
ture and electric41 conductance of fuming nitric acid is
recommended fori testing the accepcability of this ma-
terial for further; storage and use as an oxidizer for
rocket fuels. Th4 method is both simple and rapid,
and although it dt^s not give precisely the absolute
composition of the sample, ti does indicate whether or
not the compositipn of the sample is within an accept-
able range. A set of curves of conductance vs tem-
perature from 0 %o 5(fiC is provided for fuming nitric
acid in the compdsition range of 12 to 16 weight per
cent nitrogen dlo^de and 2.0 to 3.5 per cent water.
Fuming nitric acjd containing this amount of nitrogen
dioxide and watei} possesses high thermal stability and
therefore develops low storage pressures. Fuifing
nitric acid in thi$ composition range is assumed to be
usable with a givf n rocket fuel. A minimum of 0. 3
weight per cent hydrofluoric acid in fuming nitric acid
is recommended to inhibit liquid and gas-phase corro-
sion of conventioiial 55-gallon aluminum or stainless-
steel storage drums during prolonged storage periods.
Fuming nitric acid containing at least this amount of
hydrofluoric acid is storable with respea to corrosion.
A colorimetric t^st employing the bleaching effea d
fluoride ion on a purple solution of ferric salicylate Is
described for checking semi-quantitatively the hydro-
fluoric acid present. (Author)
Jet Propulsion ijab. , Calif. Inst, of Tech.
STORABILITY OF FUMING NITRIC ACID.
M. Mason, Lois L. Taylor, and Howard F.
Rept. on Contract DA 04-495-ORD-18.
declassified 12 Apr 54. 108p. 38 refs.
no. 20-72.
Order fromLCru$5.70. ph$l6.80 PB 153 949
Pasadena.
by David
Keller.
28 Dec 53.
Rept.
Some of the general problems of storing fuming nitric
acid (the system HNO3-NO2-H2O) in closed metal coa-
tainers far periods at the order of 1 month at 130 and
160*^ were investigated. Two chemical processes
which cause problems in the storage of this widely
used oxidant were specifically studied: (1) the corro-
sion of aluminum (types 61 S-T6. 2S-0, and52S-0)
alloys and steel (types 303. 347. 410, 19-9DL. and
4130) aUoys with change in composition and contami-
nation of the acid with metallic salts and (2) the
thermal decomposition of acid lean in NO2 and H2O
with accompanying high pressures and changes In
composition of the oxidant. The rate of corrosion of
metal containers (mainly Al 61S-T6), the maximum
pressures developed during storage, and the change
of composition of the FNA were measured, and the
resulting data are presented in tabular and graphical
form. Liquid-phase corrosion of the aluminum alloyi
tested and of stainless- steel alloys 303, 347, and
19-9DL is found to be markedly inhibited by the pres-
ence of suitable amounts of HF or NaF in the FNA.
Corrosion of the other steel alloys tested was accel-
erated by HF in FNA.
Pennsylvania State U. , University Park.
THE RATE OF DECOMPOSITION OF NITROSYL
CHLORIDE IN SHOCK WAVES, by Bernhard Deklau
and Howard B. Palmer. Rept. on Contract Nonr-
1858(25). Feb 60, 32p. 27 refs. Proj. Squid Technical
rept. PSU-5-P; AD-235 848.
Order from LC mi$3. 00. ph$6. 30 PB 153 173
Measurements were made of the rate of decompoaltka
of nitrosyl chloride, ONCl. over the temperature raii|e
from 88C^ to 1350OK. Data were obtained in pure ONQ
and in a series of Ar-ONCl mixtures ranging up to 1:20
ONCl-Ar. The room temperature extinction coeffi-
cients, t. which were obtained were in good agree-
ment with the literature. The variation of e with tem-
perature showed considerable scatter, but its behavior
at wavelengths of 3850, 4360, and 5460 A was in gen-
eral accord with expectations on the basis of room
temperature results.
This report relensed for sale to thejxiblic 2 Feb 61
Leather and Textiles
Office of Technical Services, Dept. of Commerce,
Washington, D. C
QUARTERMASTER CORPS TEXTILE SERIES RE-
PORTS (1942-1960). Nov 60, 6p. 104 refs. GTS
Selective Bibliography SB-440.
Order from OTS $0. 10 OTS SB-440
A bibliography of reports listed in the two OTSmoothllf
abstract Journals: U. S. Government Research ReporO
and Technical Translations.
Southern Research Inst. , Birmingham. Ala.
DETERIORATION OF TEXTILE MATERIALS BY UL-
TRAVIOLET LIGHT, by William S. Wilcox, Charles
V. Stephenson and others. Rept. for 1 May 59-31
July 60 on Air Force Textile Materials , Contract
AF 33(616)6565. Oct 60, I60p. 49 refs. Wadd Techni-
cal rept. 60-510.
Order from OTS $3.00 PB 171 417
448
The effects of ultraviolet radiation on polyethylene,
Teflon, nylon. Mylar, and Acrilan were determined.
These materials have been Irradiated in a vacuum and
in an inert atmosphere of nitrogen. Deterioration of
these materials is faster for Irradiation with short
wavelength ultraviolet than it is for long wavelength
(tdiatlon. Deterioration of polyethylene, nylon. Mylar,
and Acrilan is faster in a nitrogen atmosphere than it
il la a vacuum. However, Teflon deteriorates faster
In a vacuum . Experimental evidence as to the proc-
esses of deterioration are discussed and mechanisms
are proposed by which deterioration could take place .
(Author)
MATHEMATICS
Aarhus U. (Denmark).
THE DETERMINANTS OF THE TOEPLTTZ MATRI-
CES OF AN ARBITRARY LAURENT POLYNOMIAL,
by Mie Schmidt. Technical adentific note no. 4 on
Ccotraa AF 61(052)42. 20 Aug 60, 23p. 3 refs.
AFOSR-TN-60-1383; AD- 246 963.
(Ms from LC ml$2. 70, ph»4. 80 PB 153 306
Determinanta jT(n,p)|. iul,2 p-0,t.I,t2, . . .,
of ToepUtz matrices of the type T(n, p)s ] »pf-\-\ \ .
l,]vl,2, . . .,n, ao^l. a^Ofor <0, are stuoled. A
reladon Is found reducing the case p>l to the case p -1.
By means of this the determinanta of the Toeplitz ma-
trices of a given Laurent polynomial f(z) are expressed
explicitly in terms of the zeros of f(z). This is apphed
to determine the asymptotic behavl(ur of such
determinanta. (Author)
Aeronautical Research Labs. , Air Force Research
Dlv., Wright -Patterson AFB, Ohio.
SOME APPLICATIONS OF THE POISSON DISTRIBU-
TK3N, by Z. N. Lch. Rept. on Research on Particle
Dynamics. Aug 60, 30p. 15 refs. A RL Technical
note 60-119; AD-246 3^4.
Ordsr from LC ml$2. 70, phK 80 PB 153 385
This report gives a brief summary of the formula and
use of the Poisson Distribution. TTie introductory re-
marks are concenned with the meaning of the stochas -
tk processes as a model of statistical processes and
the special aspects cf these devices. The poisson dis-
tribution P(n) - e"^^" is known as an approximate ex-
ponential function which eitpresses the probability of
random rare events. It also can be derived as the
limiting case of the binomial distribution. In the
tables, ntmierical values were calculated for small
vihies of n and t, and graphs were drawn by connect-
iag the points corresponding to the small values of t
for specific values of n. The smooth curves show the
■pprooiimations. The use of the Poisson Distribution
tiBctlon is illustrated in special examples, namely.
U^t emission or absorption, and in connection with
liw theory at cosmic ray showers. (Author)
Applied Mathematics and Statistics Labs. , Stanford
U. . CaUf .
APPUCATIC»4S AND EXTENSIONS OF THE
METHOD OF WIENER AND HOPF FOR THE SOLU-
TICW OF SINGULAR AND NON- SINGULAR INTE-
GRAL AND INTEGRO- DIFFERENTIAL EQUATIONS,
by D. W. Swann. Technical rept. no. 87 on Contraa
Nonr-225(ll). 20 Apr 60. 158p. 22 refs. AD- 236 205.
Order from LCml$7. SO, pb$24. 30 PB 147 121
Columbia U. , New York.
A MULTIDIMENSIONAL GENERAUSATION OF THE ,
INVERSE SINE FUNCTIOJ, by Harold Ruben. Rept.
on Contract Nonr-266(59). [i960] 12p. 10 refa.
CU-l5-60-Nanr-266(59) MS; AD- 233 862.
Order from LC ml$2. 40, ph$3. 30 PB 153 754
A class of functions, defined as integrals over unit
hypercubea, which constitute natural generalisations
of the inverse sine function is discussed. In the case
where the unit cube is a square, the corresponding
integral serves to define the latter function. The
measure of a regular simplex in hyper spherical space
may be expreaaed aa a linear combination ctf such
integrals. The simplicity of the integrals gives some
grounds for progress In the difficult problem of
evaluating the measures of regular hyper spherical
aimplices. (Author)
Hebrew U. (Israel).
LOCAL PARTIAL DIFFERENTIAL ALCXBRA, by
S. HalfinandA. Robinson. Technical (sclemlflc) note
no. 12 on Contract AF 61(052)187. Oct 60, 21p.
3 refa. AFOSR-TN-60-1407; AD-246 977.
Order from LC mi$2.70, ph$4.80 FB 153 306
An algebraic theory for the solution of initial value
problems for systems of algebraic differential equa-
tions has been given previously. The present paper
extends the theory to systems of partial differential
equations. (Author)
Hebrew U. (Israel).
RESEARCH IN THE AREA OF MATHEMATICAL
ANALYSIS, by S. Agmon, A. Dvoretzky, and
A. Robinson. Technical (final) rept. for 1 Nov 58-
30 Sep 60 on Contraa AF 61(052)187. Oct 60, 35p.
3 refs. AFOSR-TR-60-169; AD-246 976.
Order from LCmi$3. 00, ph$6. 30 PB 153 306
Contents:
Elliptic partial differential equations and related
boundary value problema
Rearrangement of series; comparison of densities of
sequences
Initial value problems and differential algebra
Univalent functions
Tauberlan theorems and summablllty
The Bergman kernel
(See also PB 146 099)
449
Minnesoca U. , Minneapolis.
AN IMBEDDING OF CLOSED RIEMANN SURFACES
IN EUCLIDEAN! SPACE, by Adriano M Garsia. Rept.
on Contract AF 49(638)857. [1960] 31p. 15 ref«.
AFOSR-TN-60-1266.
Onler from LC *ii$3. 00, ph$6. 30 PB 153 433
I
The following th^rem is proved: Every compact
Riemarai surfac^ has a conformally equivalent C
snxxxh model ii^ 3-dimensicinal Euclidean space.
(Author)
Carnegie Inst. |of Tech. Graduate School at Industrial
Administrationi Pittsburgh, Pa.
OPTIMAL PRC«>ERTIES OF EXPONENTIALLY
WEIGHTED FORECASTS OF TIME SERIES WITH
PERMANENT AND TRANSITORY COMPONENTS, by
John F. Muth. OfJR Research memo. no. 64 on Plan-
ning and Control of Industrial Operations, Contract
(Nonr -760(01)1. May 59, 16p. 9 refs.
Order from LC ^2. 4a ph$3. 30 PB 150 714
I
I
The object of thiis paper is to show that the exponen-
tially weighted forecast is optimal if the time series to
be predicted is composed of two kinds of random com-
poneitts: one lasting a single time period, and the other
lastii^ throu^ 411 subsequent periods. These are
called, respectifely, the transitory and permanent
components of tl^ time series.
inJu.
North Caroling U. (Chapel Hill]
GENERALIZATION OF SOME RESULTS FOR IN-
VERSION OF PARTITIONED MATRICES, by
B. G. Greenberg and A. E. Sarhan. Technical rept.
no. 7 on Estimation erf Parameters by Order Statistics,
Contract DA 36-034-ORD-2184. 12 Mar 59. 18p.
2 refs. OOR reflt. no. 1597 ICW; AD-212 194.
Order from LC hfii$2. 40. ph$3. 30 PB 150 711
The present pap^r extends some of the findings about
panitioning preriousiy reported and now all c4 the ob-
servations reported (Biometrika, v. 43, June 56,
p. 227-231) can be generalized.
themat
Parke Mathemitical Labe., Inc., Carlisle, Mass.
FOUNDATIONS FOR A GENERAL THEORY OF
BOOLEAN FORMULAS, by John A. Riley. Scientific
rept. no. 3 on dontraa AF 19(604)3471. July 60,
106p. 40 refs. AfCRL-TN-6O-970; AD-247 315.
Order from LC mi$5.70, ph$l6.80 PB 153 458
The techniques ^ universal algebra are used to define
and study the algebra of Boolean formulas. The main
topics treated ate: substitution operators, theory at
essential letter^, simplification operators, and the
Quine-Samson theory of prime implicants. (Author)
RIAS, Baltimoije, Md.
EXISTENCE OF A BOUNCCD SOLUTION AND EX-
ISTENCE OF A, PERIODIC SOLUTION OF THE
DIFFERENTIAL EQUATION OF THE SECOND
ORDER, by T. Yoshlzawa. Rept. on Contract
AF 49(638)382. (i960] 17p. 2 refs. Technical rept.
60-18; AFOSR-'|N-60-1064; AD-247 233.
Order from LC >ii$2. 40. ph$3. 30 PB 153 4l4
This paper constderi a differential equation of the
second order x" = F(t,x, x), where F(t,x, x) is
periodic at t. Massera has proved that if all the k>-
lutions exist in the future and if one of them Is
bounded in the future, then a periodic solution exists.
In this paper the existence of a bounded solution is
discussed and applied to the existence of a periodic
solution.
RIAS, Baltimore, Md.
LOCAL LINEAR DEPENDENCE AND THE VANISH-
ING OF THE WRONSKIAN, by Gary H. Melsters.
Rept. on COTtract AF 49(638)382. Nov 60, 26p.l6refi.
Technical rept. 60-22; AFOSR-TN-60- 1213.
Order from LC ml»2. 70, phH 80 PB 153 711
RIAS [Baltimore, Md. ] -
REVERSIBLE TRANSFORMATIONS, by Daniel C.
Lewis, Jr. Rept. on Contract AF 49(638)382. [1960]
13p, 6 refs. Technical rept. 60-16; AFOSR TN-
60-1035; AD-247 231.
Order from LC mi$2. 40, ph$3. 30 PB 153 412
Syracuse U. , N. Y.
PROBABILISTIC METHODS IN MARKOV CHAINS, bjr
K. L. Chui«. Research rept. no. 27 on Contract
AF 49(638)265. Oct 60, 35p. 9 refs. AFOSR-
TN-60- 1243; AD-247 241.
Order from LC ml$3. 00, ph$6. 30 PB 153 358
It Is the main purpose of this paper to show, by vari-
ous Illustrations from recent work, that the structure
ot the transition matrix on the one hand, and the be-
havior of the sample functions on the other, are so
Intimately connected that one can hardly strike a chord
In the one without bringing out an echo from the other.
The two sides of the theory of Markov chains induce,
sustain, and complement each other. (Author)
Syracuse U. , N. Y.
SOME REMARKS ON TABOO PROBABILITIES* by
K. L. Chung, Research rept. no, 30 on Contract
AF 49(638)265. Oct 60, 9p, 3 refs. AFOSR-TN-
60- 1244; AD-247 242,
Order from LC mi$l. 80, ph$l. 80 PB 153 359
Washington U. , Seattle.
INTERSECTK)N IN CARTESIAN PRODUCTS, by
Earnest Michael. Technical rept. no. 7 on Contract
Nonr-477(21). Mar 60, 6p. 2 refs. AD- 235 .581.
Order from LC ml$l. 80, ph$l. 80 PB 153 685
The following theorem is proved: Let X be the product
of Xi, I c A, where each X. is a topological space coa-
Mlnli^ a dense subset of cardinality ^ U. Let V be •
collection of cubes in X such that, for all J V, every
J, Is open, and I A -J. j •5, P, P£ J. If every point of X ii
in^W sets Jt V, then |V| < (UW)P. U, P, and W
denote cardinality. ""
r
4S0
Washington U. , Seattle.
WEAK SEPARABILirV OF PRODUCT SPACES, by
B. Michael. Technical rept. no. 6 on Contract
hJonr-477(21). Mar 60, 8p. 3 refs. AD- 234 938.
Order from LC mi$l. 80, ph$l. 80 PB 153 684
The following results are proved: (1) Any cartesian
product off -spaces Is a f-space, and (2) Any car-
tesian product of separable metric spaces is a
* -space. (Author)
Wayne State U. , Detroit, Mich.
TESTS FOR THE VALIDITY OF THE ASSUMPTIOI
THAT THE UNE«R LYING DISTRIBUTION OF LIFE
IS EXPONENTIAL, by Benjamin Epstein. Technical
rept. no. 5 on Statistical Techniques in Life Testing,
Contract Nonr-2163(00). 2 Apr 59, 83p. 31 refs.
Order from LCmi$4.80, ph$13.80 PB 150 725
This paper gives a variety of procedures for testing,
on the basis of life test data, whether there are
significant departures from an exponential distribution
of life. The particular procedures that one should
adopt depend on the class of alternatives one is testing
against. A number of the tests are based in an
essential way on fundamental properties of Poisson
processes. Questions involving choice of tests are
considered, and a number of examples are worked out
(Author)
Wisconsin U . , Madison .
TOPICS IN MATHEMATICS BASIC FOR PHYSICS
AND ENGINEERING. II: THE LEBESGUE INTEGRAL
(LECTURE NOTES), by J. Korevaar. Rept. on
Contract N7onr- 285(07). Apr 59, 104p. 34 refs.
AD- 225 106.
Order from LCml$5. 70, phJ16. 80 PB 150 061
Computing Devices
Army Signal Research and Development Lab.,
Fort Monmouth, N. J.
PROGRAMMING STUDY OF A DIGITAL COMPUTER
FOR PROCESSING THE UNICOM MESSAGE HEAD-
ING, by Horst E. Ulfers. 1 June 60, 34p. 1 ref.
USASRDL Technical rept. 21 15; AD- 246 076.
Order from LC ml$3. 00, ph$6. 30 PB 153 002
The feasibility of employing a commercial, general
purpose digital computer for processing the message
heeding in UNICOM is studied. The Burrough's
D^TATRC^ 220 is used to execute a test program.
'Die average processing time of a standard message
heading is 10 ms. To serve more than a hundred sub-
scribers within one second, it is necessary to use a
tutor compHJter. A fast, special purpose digital com-
puter would have advantages over the DATATRON 220
due to its limited but more specific instructions.
Furthermore, it should be able to handle binary or
octal digit words. (Author)
Electronic Systems Lab., Mass. Inst, of Tech. ,
Cambridge.
THE PULSED ANALOG SYSTEM FOR EVALUATING
CORRELATION FUNCTIONS FOR RADAR, by
C. Gordon Bell. Scientific rept. no. 1 on Contraa
AF 19(604)6654 and Engineering rept. on Projea
HYVIA, Contraa AF 33(616)6046. 9 Aug 60, 25p.
7 refs. 8494-R-l; 7976-60-5; AFCRL-TN-60-963.
Order from LC ml$2.70, ph$4.80 PB 153 560
Because of the finite width of the antenna pattern,
scanning radars generate a number of pulse echoes
from the same target, and data processing is required
to determine the correct target azimuth for each groixp
of echoes, or "blip. " This processing is complicated
by pulse-to-pulse noise. Cross-correlation with the
antenna gain pattern or other filters appears advan-
tageous for improved azimuth location of the target but
has not been widely used because of the computational
speed required. This report describes an experi-
mental study of a pulsed-analog correlator simulated
by operating the TX-0 computer with associated time-
shared analog computing elements under diglul pro-
gram control. With each analog operation, such as
multiplication, complete in 10 usee (within the 12-psec
TX-0 instruaion time) a 65-point cross-correlation
between 100 data points and a 35-point filter function
was completed in 4.83 milliseconds- -about twice the
time represented by the data points. Suggestions are
given for construction of a pulsed-analog correlator
which would operate on radar data In real time.
(Author)
International Business Machines Corp., Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW-1). VOLUME VII:
THE LEXICAL BUFFER. Final rept. on Contract
AF 30(602)1823. 9 Feb 60, 246p. RADC-TR-59-110G;
AD- 235 064.
Order from LCmi$ll. 10, ph$37. 80 PB 150 086-7
High-speed recording or printing of the translated out-
put from the AN/GSQ-16(XW-1) is achieved by means
of the speed- matching capabilities of the lexical buffer
core memory with its associated components and cir-
cuitry. This unit provides great adaptability for the
translator with respect either to input or output and
frees the translator to operate for the first time at its
full speed capability . The five principal components of
the system are described along with their functional
characteristics, including detailed circuit and logic de-
sign. The report contains a comprehensive mainte-
nance and operating manual for the buffer memory , our
put control unit and power supply, along with the pres-
ent flexpwriter output and the rented IBM Model 11 tape
unit. (Author)
International Business Machines Corp., Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW-1). VOLUME VIII:
LEXICAL BUFFER LOGIC DIAGRAMS, by
M. Kloomok, P. W. Case and H. H. Graff. Final
rept. on Contract AF 30(602)1823. 9 Feb 60, 285p.
RADC-TR-59-110H; AD-235 065.
Order from LC mijl 1.10, ph$44. 10 PB 150 086-8
451
Ck>ntencs:
Preparation and iilterpreatlon of system logic diagram
System logic diagrams
Lexical buffer n|emory logic
Tape control unit logic
Flexowriter control unit logic
Search logic
(See also PB ISO C|B6-7)
Intemational Business Machines Corp. , Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW-1). VOLUME DC:
LEXICAL BUFFER SCHEMATICS Final rept. oo
Contract AF 30(602)1823. 9 Feb 60, 172p. RAIX>
TR-59-110I; AD-t35 066.
Order from LC mjiSS. 10. pb$27. 30 PB150 086-9
(See also PB 150 gIb6-8)
Lincoln Lab. , Mass. Inst, d T^h. , Lexington.
INFORMATION PROCESSING. Quarterly progress
rept. for 15 June-i5 Sep 60 on Contract
AF 19(604)7400. 15 Sep 60, 58p. 11 refs. AFtCDD
TN- 60- 1020.
Order from LC m|$3. 60, ph$9. 30 PB 153 361
Contents:
CXgital computers r
Data processing j
Computer componisnts \
Pattern recognition
Analysis
Psychology
(See also PB 150 6p2)
Melpar, Inc. , Fblls Church, Va.
VOICE DATA PROCESSING SYSTEM, by
L. P. Schoene, Jrl Scientific repc, no. 2 on Contract
AF 19(604)5579. |5 Sep 60, 67p. 1 rrf. AFCRL-TN-
60-1114.
Order from LC m*$3. 90, ph$10. 80 PB 153 455
The results at twc^ feasibility studies in connection
with modifying tha design of the Voice Data Processing
System to provide additional processing functions are
presented. One d these studies is concerned with the
provision d the c$pabUity for comparing spectrum
panem descriptioiis to detect approximate matches
between input and Istored descriptions. The other
study concerns tht provision of a capability for coding ■
patterns in clusters. (Author) (See also PB 144 797)
te^s.
Skiatron Electrofiics and Television Corp.,
New York.
RESEARCH ON HIGH- DENSITY DIGITAL STORAGE
IN PHOS^ORS. final rept. on Contract
AF 19(604)4990. JS ^dy 60, 153p. Rept. no.
201A-205; ERD-TTt-60-170; AD-245 926.
Order from LC m\S7. 50, ph|a4. 30 PB 152 928
This project was oo determine basic limitations of
packing density anp operating speed, and to initiate
effort toward provfiding an optimum dark trace tube
specifically desigiled for high density digital storage.
A digital technique for accurate beam repositioning
was also conceived and is described. A redesigned
triggering and control chassis, and an improved
pulse discriminator circuit for PEC readout, resulted
in a very versatile and efficient test set up for the
evaluation of special dark trace tubes, and the con-
sideration d different operating parameters. Special
tubes included a CRT with: (1) various thicknesses of
KCi (2) no carbon and/or aluminum backing, (3) a
collector ring to faciliute evaluation d secondary
emission readout, and (4) an experimental tube which
represented an initial attempt at depositing another
phosphor over the KQ alkali halide layer. Improved
gun structures, and an effective dual phosphor dark
trace tube, appear to offer best promise for sub-
suntial Improvements in storage capacity and read-
out speed. (Author)
Stanford Research Inst. , Menlo Park, Calif.
RESEARCH ON GENERAL DIGITAL LOGIC SYS-
TEMS UTILIZING MAGNETIC ELEMENTS AND
WIRE Oh^LY. by E. K. Van De Riet, and C. H.
Heckler, Jr. Final rept. on Contract AF 19(604)4509.
Oct 60, 78p. 11 refs. SRI ProJ. 2925; AFCRL-TR-
60-352; AD- 246 315.
Order from LC miM- 50. ph$l2. 30 PB 153 206
A machine was designed to prove the feasibility d all-
magnetic logic systems. All of the circuits except in-
put, output, and pulse power supply were built exclu-
sively of ferrlte magnetic elements and copper con-
ductors. The machine described here is an arithmetic
element which performs addition, subtraction, and
multiplication with three-digit decimal numbers. It
carried out all operations correctly with a simultane-
ous variation of 110 percent on all drive pulse ampli-
tudes. Input is through a keyboard and output is in the
form of indicator lights. A laboratory pulser was used
to supply the clock pulses. Recommendations are
made for increased effon toward developing new ideas
and carrying on a machine building program with suf-
ficient continuity to keep up with the other phases of
development: An evaluation of additional all -magnetic
logic techniques is made. (Author)
MECHANICS
Brown U. Div. of Applied Mathematics, Providence,
R. I.
AXIAL PLASTIC FLOW BETWEEN NON-aRCULAH
CYLINDERS, by V. V. Sokolovsky. Technical rept.
no. 58 on Contract Nonr-562( 10). Arp 60, 15p. Cll-
58; AD-236 728.
Order from LC mi$2. 40, ph$3. 30 PB 147 401
Trans, d paper presented at Symposium on Naval
Structural Mechanics no. 2, Brown U. , 5-7 Apr 61.
The axial flow of a plastic mass in the doubly connected
space between two rough cylindrical surfaces withnoe-
circular cross sections and parallel generators is pre*
sented. A method is developed that reduces the solu-
tion of the problem for a non-linear constitutive equa-
tion to that of the same problem for a linear constitu-
tive equation. The axial flow between cylindrical sur-
faces with confocal elliptical cross sections is treated
as an example. (Author)
452
Brown U. Div. of Engineering, Providence, R. I.
EXTENSION OF THE STABILITY POSTULATE WITH
EMPHASIS ON TEMPERATURE CHANGES, by
D C Drucker. Technical rept. no. 17 on Contract
Noor-562(20). Apr 60, 26p. 9 refs. Nonr- 562(20)1 7;
AD-236 500.
Order from LC mi$2.70, ph$4.80 PB 147 362
A definition of stability of a body d material under
isothermal conditions was phrased in terms of an ex-
ternal agency which can apply any set of forces to the
body. Positive work by each of the sets d forces of
the external agency on the change in displacements
produced insures stability. The proposal is made that
the external agency be thought of as applying other
environmental forces with accompanying changes in
displacement. If temperature change is considered as
a force the corresponding change in displacement is
the change in the flow of entropy into the body. Anen-
cion is devoted to such specialized topics as adiahatic
yield surfaces in plasticity and variation 6f yield
stress with temperature. Consideration is given also
to the reasonableness of the postulate and to its posi-
tion in the laws of thermodynamics. One conclusion is
that it is necessary to use uncoupled thermal and
stress equations in plasticity theory when the yield
stress decreases with temperature. (Author)
Columbia U. , New York.
FREE EXTENSIONAL TORSIONAL VIBRATIONS OF
A PROLATE SPHEROIDAL SHELL, by F. L.
OiMaggio and A. Silbiger. Technical rept. no. 2 on
Coorract Nonr- 266(67). Mar 60, lOp. 4 refs.
CU-1-60-ONR(67)-CE; AD- 235 391.
Order from LC mi$i. 80, ph$l. 80 PB 153 734
Ibrsional vibrations in vacuo of thin shells in the
ihspe of prolate spheroids are investigated to de-
termine the effect of end geometry. The differential
equation for the mode shapes obtained by application of
Hemilton's principle in prolate spheroidal coordinates,
it found to be satisfied by single tabulated prolate
spheroidal angle functions of the first kind and the
transcendental frequency equation is readily solved
with the aid of the tabulated eigenvalues. Numerical
non-dimensional results are presented for the first
eight modes.
Peltman Research Labs. , Picatinny Arsenal, Dover,
N. J.
ANALYSIS OF STRESS DISTRiaJTION ON THE
HYPERBOLIC PARABOLOIDAL SHELL, by JuUan L.
Divis. Dec 60, 22p. 5 refs. Technical rept. FRL-
TR-22.
Order from LC mi$2. 70, ph$4. 80 PB 153 386
A ■Hbematical analysis of the stress distribution on
• hyperbolic paraboloidal shell for certain boundary
conditions is presented starting from first principles.
Tbe geometry of the hyperbolic paraboloidal surface is
deacrlbed. The equilibrium equations are developed
under the conditions of membrane theory, and the
■tress distribution is determined. Special cases are
given. This study stems from the need of the design
engineer for a better understanding of the basic prln-
dpiee underlying the elastic behavior of the hyperbolic
paraboloidal shell in certain military applications.
(Author)
Illinois U. [Urbana].
ANNOTATED BIBLIOGRAPHY AND SEUECTED
REFERENCES ON THE THEORY OF ELASTIC
PLATES, by P. E. Wilson and A. P. Boreal. Tech-
nical rept. no. 5 on Contraa [Nolnr-I834(14). Jan 60,
23p. 19 refs. T.&A.M. rept. no. 158; AD- 234 250.
Order from OTS $0.75 PB 171 374
Particular emphasis has been placed on those theories
which include one or more of the following effects. (1)
Nonlinear effects in the strain-displacement relations;
(2) Transverse shear stress; (3) Transverse normal
stress; (4)Anisotropy; (5)Heating; (6)Nonhomogeneity
(Sandwich plates); (7) Viscoelasticity.
Illinois U. [Urbana]
STRAIN ENERGY EXPRESSION FOR A CIRCULAR
CYLINDRICAL SHELL INCLUDING TRANSVERSE
SHEAR EFFECTS, by R. E. Miller and A. P. Boreal.
Technical rept. no. 6 on Contract [Nonr] -1834(14).
Feb 60, 30p. 6 refs. T. & A. M. rept. no. 159.
Order from LC mi$2. 70, ph$4. 80 PB 153 119
In problems of buckling and of post -buckling behavior
of circular cylindrical shells, restrictive assumptions
which reduce the three-dimensional elasticity problem
to a two-dimensional problem are usually employed.
However, in modem structural prc^lems of moder-
ately thin shells, the effects of transverse shear may
be important. The strain energy expression derived
in this report is based on the exact expressions for the
strain -displacement relations of three-dimensional
elasticity theory.
Lockheed Aircraft Corp. , Sunnyvale, Calif.
STRUCTURAL RELIABILITY METHODS FOR
CYLINDERS AND CONES, by G. W. Reed and E. J.
Pipes. Technical memo, [on Contract Nord- 17017].
May 59, 48p. 10 refs. LMSD-4507.
Order from LC mi$3. 30, iA$7. 80 PB 153 357
This report released for sale to the public 1 F6b 6L
Empirical design curves based on probability theory
are developed in this report for cylinders and cones
under external pressure. The method erf analysis Is
recommended for strength analysis where a level of
structural reliability must be established. (Author)
Purdue U. Div. of Engineering Sciences, Lafayette,
Ind.
PROPAGATIONS OF ELASTIC WAVES GENERATED
BY DYNAMICAL LOADS ON A ORCULAR CAVITY,
by A. Cemal Eringen. Technical rept. no. 16 on Con-
tract Nonr- 1100(02). Jan 60, 18p. 15 refr.
AD- 231 875.
Order from LC mi$2. 40, ph$3. 30
PB 152 904
The Fourier transform technique was employed to solve
the exterior elasto-dynamlc problem concerning the
region outside a circular cavity in a plane elastic body.
The normal and tangential tractions acting at the sur-
face of the circular cavity are prescribed as arbitrary
functions of the polar angle, *, and the time, t. The
case of impact, blast, and moving loads are studied in
detail. (Author)
463
Rensselaer Polyrfechnic Inst., Troy, N. Y.
VBRATICWS OF ROTATING BEAMS WITH TIP
MASS, by WilllamlE. Boyce and George H. Handelman
Repc. on Contraa AF 18(600)1586. 30 Nov 60. 36p.
8 refs. RPI MathRep. no. 39; AFOSR-TN-60-1402.
Order from LCmi$3. 00, ph$6. 30 PB 153 501
The purpose d thi^ Investigation is an anempt to
analyze the effect d a tip mass on frequencies higher
than the first. (Author)
ktKhoi
Aerodynamics and Pneumatics
Aeroelastic and Structures Research Lab. , Mass.
Inst. ctfTech., Canibridge.
TRANSIENT AND NONLINEAR EFFECTS ON HIGH
SPEED, VIBRATORY THE RMCC LASTIC INSTABILITY
PHENOMENA. Pi^T I: THEORETICAL CONSICCRA-
TIONS, byEugeneJJ. Brunelle, Jr. Rept. for 15Jan59-
May 60 on Dynamic Problems in Flight Vehicles, Con-
tract AF 33(616)6185. July 60, I25p. 17 refs. WADD-
TR -60-484, Part j.
Order from OTS S2.75 PB 171 415
This report prese|ics an engineering approach to the
one and two degree of freedom study of both linear dif-
ferential equationf with time -varying coefficients and
autODomous differential equations with constant coeffi-
cients containing iieak. non-linearities. Approximate
solutions dl varying complexiiy and hence accuracy
are presented for these equations and the results are
qualitatively comflared. In order to provide a con-
venient reference lanalysis for assessing aeroelastic
examples of time-tvarying and nonlinear system be-
havior, a portion trf this report is devoted to pre-
senting the generail features of a constant coefficient
aeroelastic proceis in a nonclassical manner.
(Author) ]
i
Arnold Engineer ng Development Center [Tullahoma,
Tenn. ]
COMPRESSIBLE FLOW TABLES FOR GASES WITH
SPECIFIC HEAT RATIOS FROM 1.10 TO 1.28, by
K. E. Tempelmeyir and G- H. Sheraden. Rept. on
ARO, Inc. , Contrfct AF 40(600)700 Sup. 6(58-1).
Mar 58, 172p. 18 refs. AfiDC TN-58-9; AD-152 041.
Order from LC ml$8. 10. ph$27. 30 PB 153 477
This report released for sale to the public 15 Feb 61.
Some of the publicjations containing documentation of
compressible flowt functions are reviewed to indicate
their area of application and range. The more fre-
quently used one-4imen8io.ial isentropic, normal
shock and expansibn flow relationships are presented
for a Mach number range from 0. 02 to 8. 00 and spe-
cific heat ratios f^om 1 . 10 to 1 . 28 in intervals of 0.02
(Author)
Avco fEverett] Rlesearo^ Lab. [Mass. ]
RADIATION FROM HOT AIR, by J. Keck, J. Camm
and others. Rept. on Contraa AF 04(647)278. Feb59,
65p. 35 refs. Reiiearch rept. 42; AD-213 643.
OrtJer from LC i4$3. 9a phWO. 80 PB 149 676
The radiation emitted by 8 hock -heated oxygen, nitro-
gen and air was studied in the wavelength range 2000
to 10, OOOA at temperatures from 4000 to 9000^K and
densities from .01 to 10 times standard atmospheric.
Both spectroscopic and photometric techniques were
employed. The radiation consists of bands from O2,
N2, N2'*' and NO molecules, lines from O and N
atoms and continuum Kramers radiation from O".
Comparison of the experimental results with the theo-
retical expressions giving the wavelength, tempera-
ture and density dependence of the radiation gave
electronic f- numbers for all the bands observed.
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
THE DRAG AND STABILITY OF A CIRCULAR
WEEXJE AIRFOIL IN SUPERSONIC FLIGHT, by
Maynard J. Plddii^ton and Charles H. Murphy. Jan 60,
19p. 3 refs. Memo. rept. no. 1245; AD-234 865.
Order from LC ml $2. 40, ph$3. 30 PB 150069
The drag and sublllty characteristics of circular
wedge airfoils are presented and discussed. Although
linear analysis predicts neutral static stability, these
airfoils were adequately stable for Mach numbers
greater than 1. 8. At lower Mach numbers the drag in-
creased quite rapidly and the models tumbled.
(Author)
Ballistic Research Labs . . Aberdeen Proving Ground.
Md.
MINIATURE HOT WIRE PRESSURE GAGES FOR
WIND TUNNEL WORK, by Herben J. Bomelburg.
Jan 60, 18p. 3 refs. Rept. no. 1095; AD-235 058.
Order from LC mi$2.40, ph$3.30 PB 150 067
A Pirani type hot wire pressure gage is described,
yhich, because of its small size; can be installed with-
in the usual pressure holes of wind tunnel models . Iti
expected temperature drift was compensated and stttic
and pitot pressures were measured. As the response
time of such a small gage Is very short, it can also be
used for indicating unsteady and turbulent flow condi-
tions . Two symmetrical gages of this kind were used
as a sensitive flow angle meter. (Author)
Computer Engineering Associates. Inc. , Pasadena,
Calif.
THE EFFECTS OF TIME VARYING AERODYNAMIC
COEFFICIENTS ON AEROELASTIC RESPONSE, by
Richard H. MacNeal, Jack H. Hill and Bernard
Mazelsky. Rept. for 16 Feb 59-28 Apr 60 on Dynamic
Problems in Flight Vehicles. Contract AF 33(616)6221
Apr 60. 109p. 13 refs. WADD Technical rept. 60-39a
Order from OTS %2. 50 PB 171 407
An investigation was made of the effects of time-
varying aerodynamic coefficients on the flexure-
torsion flutter problem during rapidly accelerated ver-
tical flight. These effects are likely to be significant
in the transonic flight regime of a rocket -boosted ve-
hicle. A mathematical analysis of systems of linear
differential equations with slowly varying coefficients
Is presented. Simplified approximate solutions are de-
rived from this analysis. An analog computer investi-
gation of a lifting surface with pitch and plunge degrees
4M
cf freedom and time-varying aerodynamic coefficients
it described In which the free transient response and
ttie response to continuous excitation were measured
for * variety of parameter configurations. These re-
fults are compared with response envelopes predicted
by a simplified analytical method and the agreement is
found to be satisfactory. (Author)
Cornell U. C^aduate School of Aeronautical
Engineering, Ithaca, N. Y.
THEORY OF LINEARIZED TIME- DEPENDENT
BOUNDARY LAYERS, by S. H. Lam and N. Rott.
Final rept. on Contract AF 49(638)544. July 60, 55p.
9refs. AFOSR-TN-60-1100; AD-246 519.
Order from LC ml$3. 60, ph$9. 30 PB 153 092
A class of laminar, two-dimensional, time-dependent,
incompressible, boundary- layer flows is considered.
"Hie major goal of the preseit investigation is to re-
solve certain mathematical peculiarities of this cate-
gory of unsteady, flat-plate flows, but mosp of the
analysis is not restricted to the flat plate. The ques-
tion of the Joining of the low-frequency and high-
frequency series solutions is given special attention.
Extensive numerical compuutlons, performed to sub-
stantiate the theory, are also presented here.
Institute for System Research, U. of Chicago, ID.
DETERMINING AIR REACTIONS ON MOVING VE-
HICLES. PART IV. METHODS OF AERODYNAMICS:
ELEMENTARY BODIES, by M. Z. Krzywoblocki.
Rept. on Contract AF 33(616)5689. Aug 60, 946p.
1,683 refs. WADC Technical rept. 56-51, Part IV.
Order from OTS $10. 00 PB 171 387
TWs report describes the methods of aerodynamics
wiiich are mainly concerned with the flow of a viscous
gaa and the drag due to viscosity in continuum, as well
uwith the flow of a highly rarefied gas in the high al-
timde domain where the notion of c6ntimttim is no
knfer valid. Accordingly, its contents are divided
into four sections: Section I describes methods based
upon the aerodynamics of continuum applied to the
flowB of viscous fluids. Its particular concern is with
the phenomena In the boundary layer, the resistance of
bodies in viscous fluids, and the heat exchange phe-
nomena between the fluid and the moving body. Section
n describes methods based upon the kinetic theory of
gases applicable to the phenomena in rarefied gases to
determine the friction drag of moving vehicles. Sec-
tion III discusses the methods baaed upon the so-called
Newtonian flow and free molec\ile theories, applied in
particular to the calculation of the drag of a body mov-
ing in a highly rarefied gas domain and to the estima-
tion of the heat transfer phenomena between the gase-
ous medium and the moving body. Section IV presents
methdds referring to magnetoh^rodynamics, particu-
larly to the calculation of the boundary layer in an
electron stream, and to the similarity rules in mag-
netohydrodynamics. (Author) (See also PB 161 141)
Inatitute for System Research, U. of Chicago, 111.
MTERMINING AIR REACTIONS ON MOVING VE-
HKLES. PART V. METHODS OF AERODYNAMICS -
OOlffOSITE BODIES, by M. Z. Krzywoblocki. Rept.
oaCootract AF 33(616)5689 Aug 60, 236p. 901 refs.
WADC Technical rept. 56-51, Part V.
Order from OTS $3. 50 PB 171 388
This report contains the methods used by aerodynam-
icists to determine the quasi -static forces acting on
composite bodies moving in an airstream. Included in
the volume are the methods for arriving at the quasi -
static force picture for complex body shapes whose
elements are subject to interaction. Interference
effects, and deformation (movable control surfaces).
(Author) (See also PB 171 387)
Lincoln Lab., Mass. Inst, of Tech.. Lexington.
UHF RADAR FOR REENTRY PHYSICS PROGRAM,
by B. G. Kuhn. Rept. on Contraa AF 19(604)7400.
19 Sep 60, 77p. 21G-0011; AD- 244 586.
Order from LC mi$4.50, ph$12.30 PB 152 620
Contents:
System Description: Major features; system
functioning
Review of Components: Varian 8128 klystron power
amplifier; duplexer; direaional coupler; waveguide
and antenna system; RF drive system: klystron
modulator; pulse transformer; high voltage power
supply; trigger system and timing; safety interlock
system; receiver
Test System: General; equipment and couplings; per-
formance check sheet; test piaures
Equipment Layout and Cabling
Run-up Procedure
Discussion of Results
Lockheed Aircraft Corp. , Sunnyvale. Calif.
THE EFFECT OF NONLINEAR AERODYNAMIC CO-
EFFICIENTS ON FREE-SPINNING BALLISTIC BE-
HAVIOR AND ITS APPLICATION TO THE EVALUA-
TION OF FLIGHT MEASUREMENTS, byJ.S.Kanno.
Technical rept. on Flight Sciences. June 60, 62p.
LMSD-703013; AD-240 807.
Order from LC mi$3. 90, ph$10. 80 PB 152 844
An analysis is made to predict the effect of nonlinear
aerodynamic characteristics on the free epicyclic mo-
tion of a free -spinning ballistic body aixl to determine
certain nonlinear aerodynamic coefficients from flight -
test motion records. The equations of motion are
briefly developed subject to the restrictions of constant
forward velocity, small iK>rmal and lateral translation
displacements, constant axial spin, small pitch-yaw
angular displacements, and constant dynamic pressure
and Mach number to yield a sixth-order differential
equation describing the motion as observed in body
coordinates. T^ important equation for resolving an
analytic solution is shown to be a second-order non-
linear txxnogeneous differential equation of the de-
pendent variable, the complex -vector representation
of the angle-of -attack. Based on the fundamental oscil-
latory motion of the harmonic ballistic portion of the
equations with a reference "average" aerodynamic
static stiffness coefficient, an approximate quasi -
harmonic solution for the angle -of -attack is derived by
averaging method of Kryloff and Bogolluboff (K -B).
From the K-B solution, it is concluded that the effects
of aerodynamic normal force and damping moment in-
fluence the envelope of the motion independently of the
influence of aerodynamic static moment upon the cyclic
characteristics of the motion. Also, a change in space
motion factor (except for K ■ 0 or tl) reflects non-
linear aerodynamic coefficients. With a monotonically
softening static moment, the period for K = 0 is less
455
than the period foil K- tl. Conversely, with a hard-
ening static momeiit, the period for K = 0 is greater
than the period fo^ K* -^1- Approximations of the K -B
averaging integrals based on quadratic interpolation of
the appropriate aerodynanuc coefficients are devel-
oped for applicatit^ to flight -test motion records.
Mas^chusetts idst. of Tech. , Cambridge.
HYPERSONIC FLOW PAST BLUNT BODIES AT
SMALL ANGLES pF ATTACK, by Gerhard L. Gross
Rept. on Contract AF 49(638)207. Oct 6a 16 refs.
Fluid Dynamic Re$earch Group rept. no. 60-4; OSR
Technical note no.
Order from LC mi $3. 90, ph$ia 80
60-1195.
PB 153 420
An analytical solution is derived for the flow in the
nose region of blufit bodies of revolution with conic
section profiles, ttraveling at hypersonic velocities and
zero or small angles of attack. The approach chosen
is that of lineariz4tion of the inviscid equations of mo-
tion in the ai^le of attack and the ratio of the density
before to that behind the strong bow shock according
to the modified Ne»wtonian approximation. The density
is assumed constant for the flow between shock and
body surface. Th4 possibility is discussed of a numer-
ical extension into the neighborhood of Freeman's
singularity, which does, however, not occur within
finite distance frofn the axis for a paraboloid nose
shape. (Author)
Michigan U. , Am Arbor.
SOME CCTAILS OF THE TRANSITION TO TURBU-
LENT FLOW IN tOISEUILLE FLOW IN A TUBE, by
A. M. KuetheandK. R. Raman. Rept. on Contract
AF 18(603)34. June 59, 36p. 13 refs. UMRI ProJ.
no. 2504; AFOSR |TR-59-84; AD- 232 746.
Order from LC mi$3.00, ph$6.30 PB 150 982
Measurements of velocity fluauations, Reynolds
stresses and sheading stresses at the wall in the
transition region ♦f a tube are presented. The meas-
urements are made in a tube at a Reynolds number d
6000 behind 3 disturbance generators placed in the
fully developed la|ninar flow 620 diameters from the
entrance. The results show the way in which some of
the statistical details at the transition depend on the
nature at the distvlrbance generated. The Reynolds
stresses and the shearing stress at the wall can reach
very high values c)uring the early stages of transition.
Implications are pointed out regarding possible causes
for the hig^ temperature recovery faaor during
transiUon in high speed flow over surfaces. (Author)
Naval Ordnance test Station, China Lake, Calif.
UNSTEADY SUPERSONIC FLOW PAST SLENDER
POINTED BODIES, by John W. ?^les. 1 1 May 53, 73p.
6 refs. NOTS 701;, NAVORD rept. 2031.
Order from LC mi$4. 50. ph$l2. 30 PB 154 403
This repon released for sale to the public 16 Feb 61.
The equations of
fluid are examii
der body, and an
of the fineness rai
number. Followi
tsteady, supersonic flow in an ideal
in the neighborhood of a very slen-
^rder analysis is carried out in terms
io, reduced frequency, and Mach
Ward's analysis for the steady flow
problem, a complex potential is then introduced and
expanded near the body in powers (and a logarithm) of
the complex variable in a plane transverse to the flow.
Momentum balances are used to evaluate the drag,
lift, and moments on the body. The results are used
to determine the drag on an accelerating body of revo-
lution and the logitudinal stability derivatives and
damping in roll for low aspect ratio wings and slender
wing-body combinations. (Author)
Naval Supersonic Lab. , Mass. Inst, of Tech. ,
Cambridge.
A BIMOLECULAR DIATOMIC GAS MODEL APPLIED
TO NONEQUILIBRIUM BLUNT-BODY FLOW, by
William John Towle. Aug 60, 76p. 31 refs. Technical
rept. 462.
Order from LC mi$4.50, ph$12.30 PB 153 106
Derivation of the thermodynamic relations is presented
for a blmolecular diatomic gas nilxture from statisti-
cal thermodynamic considerations including vibrational
and dissociational modes. A review and derivation at
the reaction rate equation for the dissociational proc-
ess is given. An approach for the solution of the flow
field about a blunt body in hypersonic flow for the non-
equilibrium dissociating gas is considered in detail.
(Author)
Naval Supersonic Lab. , Mass. Inst, of Tech. ,
Cambridge.
A MASS TRANSFER FINITE DIFFERENCE FORMU-
LATION EMPLOYING CROCCO VARIABLES, by
James P. Moran and Paul a Scott. Rept. on Contraa
AF 49(638)245. June 60, 81p. 11 refs. Technical rept
443; AFOSR- TN- 60- 846. AD-247 913.
Order from LC miK 80, ph$I3. 80 PB 153 104
Solutions to the laminar boundary- layer equations
have been obtained by Fliigge-Lotz and Baxter using a
finite difference formulation. The same difference
approximations are used here to develop a formulation
for the binary boundary- layer equations for the caseof
helium injection into an air stream. This formulation
is used in obtaining solutions to the problem of a
porous region having an injection function of the form
k/ ^fxc- Corresponding solutions obtained by Moran
using Covert's approximations to the equations are
compared with the finite difference solutions. For low
levels al injection Coven's approximations to the
concentration and shear equations show good agree-
ment with the finite difference solutions. (Author)
Polytechnic Inst . of Brooklyn, NY.
INTEGRAL METHOD COMPRESSIBLE BOUNDARY
LAYER CALCULATIONS FOR STRONG FAVORABLE
STREAMWISE PRESSURE GRADIENTS OVER AN
INSULATED SURFACE, by Martin H. Steiger. Rept.
on Aerodynamic .and Heat Transfer Problems in Hyper-
sonic Flow, Contract AF 33(616)6118. Sep 60, 21p.
5 refs. PIBALrept. no. 621; A RL Technical
note 60-149; AD- 246 441.
Order from LC mi$2. 70, ph$4. 80 PB 153 184
The two-dimensional, laminar, compressible boundwy
layer with strong favorable pressure gradients are in-
vestigated. The main purpose of this note is to preee«
436
a method by which highly non- similar solution may be
obuined regardless of the magnitude of this gradient.
A well-behaved non- similar solution is obtained for the
liypersonic flow about a two-dimensional blunt body
vtth an insulated surface. (Author)
Iblytechnic bist. of Brooklyn. N. Y.
TABULATION OF COORDINATES FOR HYPERSONIC
XXISYMMETRIC fKfZZLES, PART IL COORDI-
NATES FOR TEST SECTION MACH NUMBERS OF
6. 7. 8.5, 9, 10, 14, 16, AND 18, by Robert J.
CrtMd. Rept. on Wind Tlmnel Studies. Contract
AF 33(616)3978. July 60, I34p. PIBAL rept. no. 463;
WADD Technical note 58-300. Part II; AD-240 666.
Order from LC mi$6. 90, ph$21. 30 PB 152 838
Noszle contours are presented for test section Mach
minbers at 6, 7. 8. 5. 9. 10, 14, 16, and 18. These
ooocours were obtained by applying the method at'
characteristics to the region between a spherical
source flow and a uniform, parallel flow. The con-
tours are given for various half-cone angles between
(Ptai2(P (Author)
Rensselaer Polytechnic Inst. , Troy, NY.
EFFECT OF SURFACE MASS-TRANSFER ON THE
IMPULSIVE MOTICW OF AN INFINITE PLATE AT
HYPERSONIC SPEEDS IN A VISCOUS COMPRESSI-
BLE FLUID, by Ting Yl Li. Rept. on Contraa
AF 18(600)1591. Sep 60, 57p. 7 refs. TR AE 6005;
AFOSR -TN- 60-956; AD- 246 621.
Order from LC ml$3. 60, ph$9. 30 PB 153 315
The effects are examined of mass-transfer on an in -
finite flat plate surface when the plate executes an im-
pulsive motion at hypersonic speeds in a viscous com-
pressible fluid. K. Stewartson (Cambridge Phil. Soc. ,
1955) has considered the corresponding pn-oblem for an
impermeable surface. In the present paper, the law of
surface mass-transfer which yields a similar solution
for the viscous boundary layer is derived. The solu-
tion for the viscous region can be obtained by an ex-
tension of Stewanson's result. The matching at the
interface between the viscous and inviscid regions is
accomplished by Stewart son's procedure. Solutions
are obtained in explicit closed forms which give com-
plete information on the effects of surface mass-
transfer on the strong interaction between shock wave
and boundary layer. Numerical examples are
discussed. (Author)
Rennselaer Polytechnic Inst. , Troy, N. Y.
STUDY OF FLUID MIXING AND RELATED AERO-
DYNAMIC PROBLEMS, by K. T. Yen. Final rept. on
Contract AF 49(638)23. Sep 60, 12p. 15 refs. TR AE
6006; AFOSR -TR -60- 136; AD-246 622.
Order from LC mi$2. 40, ph$3. 30 PB 153 261
Contents:
Indeterminateness of the mixing problem
The general mixing problems
Effects of jet mixing on the thrust generation of the
jet flap
Boundary layer flows over a curved surface
Optimal coordinates for viscous flows
Magnetohydrodynamic boundary layer flows and jet
mixing problems
Study of some supersonic rotational flow
Sferi-Coanda, Clichy (France).
STUDY OF A COANDA NOZZLE OPERATING AS A-
SINGLE EJECTOR. STUDY OF THE OPERATION OF
COANDA NOZZLE WORKING IN STAGES. EXTRAP-
OLATION LAWS. Technical (final) rept. on Contract
AF 61(052)158. Aug 59, 250p. AFOSR-TR-60-2;
AD-230 385.
Order from LCmi$l 1.10, ph$37. 80 FB 153 378
Contents:
Study (rf the single coanda nozzle working as an ejector;
and its comparison with a direct ejector
General installation with pendular system
Tests at constant energy intake
Experimental data on direct ejector
Study of the coanda nozzle working as a compressor
Theoretical calculaticMi of the possible backpressure
at coanda nozzle exit
Determmation of the geometrical characteristics c4
the coanda nozzle
Determination of the geometrical characteristics of
the divergent
Theoretical considerations of nozzle set up in stages
The extrapolation laws
Nozzle 70/84; experimental data and results
Study of the extrapolation; experimental data and
results
Conclusions; extrafnlation laws
Hydrodynamics, Hydraulic*, and Hydro*taHcs
Aeronautical Research Associates of Mnceton, Inc. ,
N.J.
EXAMINATION OF THE SOLUTIONS OF THE
NAVIER-STCMCES EQUATIONS FOR A CLASS OF
THREE-DIMENSIONAL VORTICES. PART I: VE-
LOCITY DISTRIBUTIONS FOR STEADY MOTION, by
Coleman duP. Donaldson and Roger D. Sullivan. Rept.
on Contraa AF 49(638)255. Oa 60, I18p. 112 refs.
AFOSR -TN-60- 1227; AD-247 471.
Order from LC mi$6.00, ph$18.30 PB 153 459
A study has been made of the class of solutions of the
Navier-Stokes equations wherein the radial, tangential,
and axial velocities in cylindrical coordinates (r,9 , z)
are of the forms U= u(r), v»v(r), and w»zw(r).
These solutions are found to represent a rather large
class (rf three-dimensional viscous vortex motions.
The class of solutions contains Burger's analytic solu-
tion for an unconstrained one- celled vortex as a spe-
cial limiting case. The solutions obtained show that
vortex motions are possible which have more than one
"cell". That is, the flow may not simpiy spiral in
toward an axis and out along it as in a one-celled
configuration but may have nested regions erf succes-
sively reversed axial flow. The behavior of the solu-
tions in passing from single to multiple -celled con-
figurations is discussed and the solution for the ex-
tremely interesting case of a two-celled analogue to
Burgers' unconstrained vortex, which probably occurs
quite often in nature, is given in closed form. (Author)
457
Brown U Div. jrf Applied Mathematics, Providence,
R. I.
THE OSCILLj\TD0NS
by W. H. Reid
Noar-562(07).
Order from LC
OF A VISCOUS UQUID DROP,
Technical rept. no. 32 on Contraa
60, 7p. 3 refa; AD- 232 752.
1.80, ph$1.80 PB 153 162
F(5b
rii$
Microwave Lab* , Sunford U. . Calif.
THE STATISTICAL BASIS OF HYDRODYNAMICS
AND KINETIC THEORY, by Lawrence William Davis.
Doctoral thesis. Technical note on Contract
AF 49(638)342. itet 60, 90p. 43 refs. M. L. rept. no.
75$; AFOSR-[TNJ 60-1337; AD- 247 590.
Order from LC rii$4. 80, ph$13. 80 PB 153 6"^
A formalism is c^eveloped in which problems d hydro-
dynamics and kii<etic theory are treated as examples
of statistical inference. Recent advances in proba-
bility theory and statistical techniques malcepossiWe
this reformulati* a* these problems, the calculations
now appearing a$ an application of sutistical decision
theory. Thus th^ prediction of some quantity, such as
density, appears as a decision process in which is
incorporated all trf the available macroscopic infor-
mation and which, subject to this constraint, makes
that decision whith minimizes the expected square d
the error. (Authpr)
New York U. Cbll. of Engineering, N. Y,
SOME NON- LINEAR PROPERTIES OF LONG
CRESTED PERIODIC WAVES WITH LENGTHS NEAR
2. 44 CENTIMETtlRS, by Willard J. Plerson, Jr. and
Paul Fife (Stanford U. ). Technical rept. on Contract
Nonr-285(03). Ffeb 60, 33p. 12 refs. AD- 236 215.
Order from LC i^i$3. 00. ph$6. 30 PB 153 159
Formal perturbation procedures are applied to an
analysis ol periodic long crested waves. Qassical
perturbation metjiods yield wave forms for domlnantly
gravity or domin^ntly capillary waves that are in
agreement with itiore exact non-linear theoretical re-
sults. These saifie procedures also yield special so-
lutions at a denu^nerable set of wave numbers where
the general formlilas fall. The PLK (Pbincare Light-
hill Kuo) method jyields. without using the full potential
at the method, airealistic result for the values in
question that redjuces to the special classical solution
at the bifurcatioiTwave number. The results obtained
tvggfnt that the wave form for waves of a length
greater than 2. 44 cm will be like that d classical
gravity waves over an extensive range at lengths and
that only near lei>gths of 2. 44 cm will the profile not
look like the classical picture.
Wigley, C.
CALCULATIC»<
AND MODERATt
on Contract N62358
AD- 236 263.
Order from LC iiil$3.90, ph$10.80
W WAVE RESISTANCE AT LOW
SPEEDS, by C Wigley. Rept. no. 2
-1772. Apr 60, 6^. 6 refs.
PB 147 125
Dealing only witH low and moderate speeds, all com-
parison was restricted to Froude Nurnbers less than
0. 35 for which tl^ trim and sinkage of the model are
negligible, so thit any changed distribution of speed
round the form nruiy be neglected. Calculations were
made for 10 forms. For each form the arbitrary
power n was uken as n= 2, and n 4, so that tl^
fundamental term in a and p was taken as e'^/^^ and
also as e-B/N^. For either power the work was done
for a series of values of the arbitrary constants A or
B embracing that value which gave the beat agreemem.
(Author) (See also PB 146 294) ,
METALLURGY
Battelle Memorial Inst.. Columbus, Ohio.
THERMOS ATIC BIMETALS FOR LOW TEMPERA-
TURES, by H R Nelson, CM. Schwartz and others.
Final rept. on Contract W36-039-sc-32l20.
20 May 49, 2l9p. 27 refs.
Order from LC mi$9. 60, ph$33. 30 PB 153 9»
This report released for sale to the public 15 Feb 61
Contents:
Commercial contaas and experimental materials
Dllatometry
Elastic moduli and proportional limit determinations
of bimetals and components
Load- deflection tests , ;
Temperature -deflection tests
Miscellaneous studies of bimetals
Internal stress measurements of bimetals
Internal stresses in treated bimetals and components
Formation of bimetals by unusual methods
Defense Metals Information Center, Battelle
Memorial Inst.. Columbus, Ohio.
MELTING AND CASTING OF THE REFRACTORY
METALS MOLYBDENUM, COLUMBIUM, TANTALUM,
AND TUNGSTEN, by W. H. Johnson. Rept on Contraa
AF 18(600)1375. 18 Dec 60. 33p. 33refs.DMICrept. 139.
Order from OTS $1.00 PB 151 OM
The technology of melting and casting refractory
metals is considered from the sundpoint of ihgots and
shaped castings. The production of ingots is more ad-
vanced than is the production of shaped castings.
Molybdenum and columbium have been centrifugally
cast with some success. Shaped castings of tantalum
have been produced experimentally. No satisfartory
method for the production of shaped tungsten castings
Is presently available. There is an indicated needfor
shaped castings of the refractory metals, and further
development work appears to be justified. The cold-
crucible Induction furnace, presently under develop-
ment for titanium, might be adapted for the refractory
metals. (Author)
Defense Metals Information Center, Battelle
Memorial Inst., Columbus, Ohio.
PRELIMINARY DESIGN INFORMATION ON RECRYS-
TALUZED Mo-0.5Ti ALLOY FOR AIRCRAFT AM)
MISSILES, by W. P. AchbachandR. J Favor. [Rep-
on Contract AF 33(616)7747]. 16 Jan 61, 12p. 2 refs.
DMIC memo. 79.
Order from OTS $0. 50 PB 161 2»
458
D$U are available on a number erf conditions of
I4o-0-5Ti alloy but few data on any one condition.
Available Information indicates that Mo-0.5Ti shows
wide variation in properties, depending upon lot, con-
dition, and strain rate. The properties of Mo-0.5Ti
in the recrystalllzed condition have been examined,
since it would be expected that this condition would be
indicative of the material condition after exposure to
high temperatures in service. Preliminary data have
shown that differences in recrystallization tempera-
tures of as little as 100 F may significantly affea
strength. The data presented are for material recrys-
Ullired at 2450 F Also mcluded are properties of
recrystalllzed Mo-0.5Ti protected from oxidation by
the W-2 coating.
General Electric Research Lab. , Schenectady, N. Y.
HlOl -PRESSURE RESEARCH IN METALS AND
CERAMICS, by R. E. Hoffman, J. B. Hudson and
othera. Rept. for 1 June 58-31 July 60 on Contract
AF 33(616)5951. Sep 60, 77p. 58 refs. ARL Technical
rept. 60-321.
Order from OTS $2. 00 PB 171 025
The volume self -diffusion in pure lead has been stud-
ied at pressures up to 40 kb and at temperatures from
the melting point at each pressure to about 150^C be-
low this melting point. The influence of pressure on
the melting temperature has been obtained from these
experiments. The diffusion experiments followed es-
tablished radioisotope tracer techniq^ies modified for
use at high pressures. Attempts to measure grain
boundary aelf -diffusion by the modified techniqqes
were successful. The magnetizations of iron and
nickel at room temperature have been studied at pres-
sures up to 3000 atm and fields up to 10, 000 oersteds.
These measurements of saturation magnetization as
a function of hydrostatic pressure were extended to a
aeries of iron-nickel alloys, and the results were
used to Interpret the interactions between the atomic
nraments. From sinular measurements on an iron-
Bilicon alloy single crystal, results were obtained for
the effect of hydrostatic pressure on the magneto-
cryKalline anisocropy of this material. A study was
nMde of the effects of hydrostatic pressure on the
flrat -order magnetic transitions In the materials
MnAs and MnAu2. (Author)
Michigan U. , Ann Arbor.
EFFECT OF STATE OF STRESS ON THE FAILURE
OF METALS AT VARIOUS TEMPERATURES, by
D. R. Jenkins, H. E. Gascoigne and others. Rept. for
June 58 -Mar 60 on Solid State Research and Properties
of Matter, Contract AF 33(616)6041. July 60, 32p.
WADD Technical rept. 60-234; AD-245 245.
Order from OTS $1.00 PB 171 366
The purpose of this research program is to evaluate
the Influence of state of stress and temperature on the
fracture of me tals. To implement the research, a
series of carefully controlled experiments under com-
bined stress conditions is planncid. The work de-
scribed here is concerned primarily with development
of test equipment and the test program. Identification
of a failure criterion in terms of stress is the ultimate
objective. An examination of the technical literature
indicates that the factors involved in purely brittle
fracture have been identified. For brittle fracture,
plausible deformation mechanisms suggest that the
principal normal stress and the ratio of principal
normal stress to maximum shearing stress are im-
portant. Although some of the features of ductile frac
ture have been noted, a connection with the state of
stress has not been proposed. Consec^ently, the de-
velopment of a unified theory may be possible for
brittle fracture. A unified theory of ductile fracture
may be very complex and in panicular may require
consideration of nriore than stress alone to be valid. A
testing machine has been completed which will simul-
taneously apply axial load and torsion, or internal
pressure and axial load to a hollow tubular specimen.
Of the two specimen niaterials selected, AlSl B1113
steel may not be entirely satisfactory but Zamak 3
zinc alloy has given good results in preliminary tests.
It is planned to investigate other low -carbon steels as
a replacement for the AISI B1113. (Author)
Syracuse U. Research Inst. , N. Y.
THE EFFECT OF SEVERAL GEOMETRICAL VARI-
ABLES ON THE NOTCH TENSILE STRENGTH OF
4340 STEEL SHEET HEAT TREATED TO THREE
STRENGTH LEVELS, by Volker Weiss, John Sessler
and others. Rept. for May 59-May 60 on Metallic Ma-
terials. Contract AF 33(616)6523. Sep 6a 42p.
15 refs. WAM) Technical rept. 60-310.
Order from OTS $1. 25 PB 171 396
The effects at stress distribution and tensile strength
level on notch strength weffc investigated for 4340
sheet. Limited data were also acquired f6r a very
brittle titanium alloy. The stress concentration factor
(K) and relative stress gradient (y). which characterizt
the stress pattern at the notch root, were determined
analytically from elastic theory. Edge -notched sheet
specimens were tested for a range of K and \ values.
Test results show that the effect of stress gradient on
notch strength is fundamentally identical with that of
section width. For a brittle material, the stress
gradient is the primary factor that influences notch
strength at a given value of stress concentration.
(Author)
Ferrous Metals
Defense Metals Information Center, Battelle
Memorial Inst., Columbus, Ohio.
TITANIUM -ALLOY FORCINGS, by H. J. Henning and
P. D. Frost. Rept. on Contract AF 18(600)1375.
19 Dec 60. 89p. 2 refs. DMIC rept. 141.
Order from OTS $2. 25 PB 151 100
Current information on the availability, metallurgical
and dimensional quality, and mechanical properties of
titanium die forgings is summarized. Detailed data on
typical forgings are presented, and some forging
techniques are discussed. (Author)
MeMls and Ceramics Lab. , Wright Air Development
Div. , Wright -Patterson AFB, Ohio.
MECHANICAL PROPERTIES OF BERYLLIUM, by
A. E. Riesen and R. T. Ault. Rept. for Mar 58-
Mar 60 on Metallic Materials. Sep 60, 37p. WADD
Technical rept. 60-425.
Order from OTS $1.00 PB 171 411
459
ires
The test prcxredur^s and results of a mechanical prop
ertles determination program which included tensile,
torsion, pin aheai^ creep rupture, and fatigue data on
two lots of beryllium are presented. One lot of mate-
rial was hot pressed with a BeO content of 1. 45%; the
other lot was hot pressed -hot extnxled and contained
1 . 55% BeO. Emphssis was placed on the fatigue and
creep rupture dat4. Fatigue tests were conducted at
room and elevated temperatures with stress ratios of
A» '"and 0. 67. Both lots of material showed surprls
ing strength under fatigue loading conditions whereas
beryllium's inherent brittieness manifested Itself
under static loadiiig conditions by the brittle fractures.
The hot pressed-hDt extruded material was uniformly
stronger and therefore more desirable for design pur-
poses than the material that was only hot pressed.
(Author) i
Office of Technical Services, Depi. of Commerce, '
Washington, D. C
MAGNESIUM No^'60, 23p. 442 refs. OTS Selective
Bibliography SB-4^.
Order from OTS %h. 10 GTS SB-445
A bibliography at teports listed in the two OTS monthly
abstract journals: K]. S. Government Research Reports
and Technical Trafislations. This bibliography in-
cludes reports on ^gnesium metals, alloys, and
compounds added Qo the OTS collection during the
period 1950 to Deaember 1960.
Nonferroui (except light) Metals
Brush Beryllium Co. , Cleveland, Ohio.
DEVELX)PMENT OF WROUGHT BERYLUUM ALLOYS
OF IMPROVED PHOPERTIES, by John G . Klein, Leslie
M. Perleman and Wallace W. Beaver. Repi. for
I July 58-30 June S|9 on Metallic Materials , Delivery
Order 33(616)57-1^ and Contract AT(30-1)541 . Sep 60.
126p. WADC Technical rept. 58-478, Pan II.
Order from OTS $4 . 75 PB 171 389
Mechanical and physical properties are reported for ex-
truded and/or rolled products fabricated from beryl-
lium-rich alloys of silver, tin, cadmium, zinc, nickel,
and copper, as we|I as beryllium fabricated from sub-
sieve-size powderjand powder of higher than normal
beryllium oxide content. (Author) (See also PB 151 711)
Massachusens Inft. of Tech. , Cambridge.
VOID FORMATION AND GRAIN BOUNDARY SLID-
ING IN ALUMINUM! -MAGJ^SIUM SOLID SOLUTION
ALLOYS, by Arthu^ W. MuUendore and Nicholas J.
Grant. Rept. for July 58-Jan 60 on Metallic Materials,
Contract AP 33(616)5926. Sep 60, 37p. 16 refs. WADD
Technical rept. 60*340.
Order from OTS $lj. 00 PB 171 399
Void formation and growth during creep were observed
in aluminum - 1. 93 percent magnesium and aluminum
5. 10 percent magn^ium as a function of temperature,
stress, and time. jThe origin of voids is related to the
development at an irregular (serrated) grain boundary
and to grain boundary sliding. Grain boundary sliding
is shown to result ^rgely from crystal slip crosaing
(Author)
New York U. , N. Y.
PARTITIONING AND MICRODISTRIBUTION OF IN-
TERSTITIAL ALLOYING IN TITANIUM, by Irving B.
Cadoff and Joseph Winter. Rept. for 1 Mar 58-
5 Mar 60 on Metallic Materials, Contract
A F 33(616)5506. Sep 60. 42p. 11 refs. WADD Techni-
cal rept. 60-443.
Order from OTS $1.25 x PB 171 412
The partitioning or segregation of excess interstitial
solutes at the grain boundaries in alpha phase and beta
phase titanium alloys was Investigated. Internal fric-
tion spectra of dilute alloys of titanium with oxygen,
nitrogen and carbon were obtained. From these spectra
the activation energy for grain boundary stress relaxa-
tion, the net interaction energy of a solute atom with t
grain boundary, and the excess solute concentration
were calculated. As in previous investigations of this
type the partitioning of excess solutewas found to obey
a relation of the form Cg > Cq exp *8/kT . The in-
teraction energies were found to lie in the range 0. IS
to 0. 40 eV for binary interstitial alloys. Tensile
measurements Indicated that the increase of excess
solute at grain boundaries and dislocations brought
about by either Increasing the bulk concentration or
decreasing the equilibrium annealing temperature re-
sulted in an increase in yield strength. The effect of
excess solute on yield stress was found to be parallel
to its effect on the internal friction spectra. (Author)
Structural Metallurgy and Corrosion
Armour Research Foundation, Chicago, 111.
A MECHANISM FOR STRESS-CORROSION EM-
BRITTLEMENT, by E. G. Coleman, D. Weinsteln.
and W. Rostoker. Technical rept. on Contract
Nonr- 2602(00). Feb 60, 20p. 7 refs. Rept. no.
ARF 2152-10; AD-234 659.
Order from LC mi$2. 40, ph$3. 30 PB 153 167
It has been demonstrated that stress-corrosion cracks
can be initiated on continuous loading in a suitable
medium. Results are shown for stainless steel Im-
mersed in boiling MgCU solution and for a Mg-6%A1
alloy in aqueous NaCl-KizCrO^ solution at room tem-
perature. This behavior has been used to analyze the
stress-corrosion cracking process in terms of the
dislocation theory of brittle fracture. It is proposed
that the mechanism of cracking originates from a con-
dition of reduced surface energy brought about by ad-
sorption of some ion species from the surrounding
medium. An analysis of the grain size dependence of
Che fracture initiation stress In the stress-corrosion
media leads to estimates of reduced surface energies
of the order of 100-200 ergs/cm2 (Author)
Army Engineer Research and Development Labs. ,
Fort Belvolr. Va.
THE RESPONSE OF MATERIALS TO DYNAMIC
LOADS, by Francis B. Paca. Master's thesis.
20 July 60, 84p. 120 refs Technical rept. 1643-TR;
AD-243 547
Order fromLCml$4. 80. ph$13. 80 PB 153 077
the grain boundary
460
A review Is made of the static and dynamic response
of materials to stress. The action of stress and strain
vtves Involved during impact is discussed in terms of
wave propagation under various bour»dary conditions.
Cottrell's dislocation theory of delayed yielding Is
discussed. The test apparatus used in the application
of dynamic loads are reviewed, and their character-
latics are analyzed. A simplified method is presented
for conducting dynamic loading tests on materials of
various kinds and on materials having a very high
strength. (Author)
Defense Metals Information Center, Battelle
Memorial Inst . . Columbus. Ohio.
JTRESS- CORROSION CRACKING: A NONTECHNICAL
INTRODUCTION TO THE PROBLEM, by Warren E.
Berry. Rept. on Contract AF 33(616)7747. 6 Jan 61,
30p. 119 refs. DMIC rept. 144.
Order from OTS $0.75 PB 151 103
The problem of stress-corrosion cracking is reviewed
from a non-technical viewpoint. The recognition of
this form of corrosion cracking is discussed. The
environments most likely to cause stress-corrosion
cracking are pointed out for each alloy system. The
aalon of material composition, stress, environment,
temperature, and time on stress-corrosion cracking
is discussed and suggestions are made for controlling
these variables. The roles of protective coatings,
inhibitors, and cathodlc protection in reducing crack-
ing susceptibility also are considered. A bibliography
of some of the more recent articles on stress-
corrosion craqklnK is Included. (Author)
General Electric Research Lab., Schenectady, N. Y.
EFFECT OF BASIC PHYSICAL PARAMETERS ON
ENGINEERING PROPERTIES OF INTERMETALLIC
COMPOUNDS, by D. L. Wood and J. H. Westbrook.
Rept. for Dec 58- Dec 59 on Ceramic and Cermet Mate-
rials Development, Contract AF 33(616)6144. Aug 60,
34p. 10 refs. WADD Technical rept. 60-184;
AD- 246 540.
Order from OTS $1. 00 PB 171 393
A method for producing sound, uniform, and reproduc-
ible test specimens has been devised and an investigatio
made at the effects of basic physical parameters on the
mechanical properties. Tensile test specimens d
Bi2Tl and AgMg, produced directly by extrusion, have
provided information applicable to future studies of the
properties of NiAL A proiKxmced yield point is found
in AgMg; high strain rate sensitivity of the yield stress
hat been observed and die effects of grain size, com-
position and test temperature have been documented.
SJjecimens will withstand loading only at very slow
strain rates; after yielding occurs, however, r^id
strain rates may be employed. With total elongations
of more than 50 per cent, the material is ductile under
previously brittle conditions. (Author) »
Metals and Ceramics Lab. , Wright Air Development
Div., Wright-Patterson AFB. Ohio.
EFFECTIVE STRESS CONCENTRATION FACTORS
FOR FUGHT VEHICLE MATERIALS UNDER VARI-
OUS CONDITIONS DURING FATIGUE TE^riNG, by
V. F. Lardenolt. Rept. for Dec 58 -Dec 59 on Metallic
Materials. Oct 60, I61p. 31 refs. WAIX) Technical
rept. 60-419.
Order from OTS $3. 00 PB 171 410
This report presents in the form of tables and curves,
the effective stress concentration factors, Kf, for a
number of aircraft materials subjected to various con-
ditions during fatigue testing. The influence on Kf is
shown for such parameters as temperature, stress
ratio, specimen size, direction at testing, test fre-
quency, fabrication of notches, heat treatment, grain
size, and for titanium and its alloys, interstitial con-
stituents and hydrogen level. Because Kf is sensitive
to so many variables, no attempt is made to relate it
to any of the above listed parameters. (Author)
Metals and Ceramics Lab. , Wright Air Development
Div . . Wright-Patterson AFB, Ohio.
HYDROGEN EMBRITTLEMENT OF TITANIUM
ALLOYS, by A. E. Riesen and D. H. Kah. Rept. for
Jan 57-Mar 60 on Metallic Materials . Oct 60. 49p.
3 refs . WADD Technical rept. 60-275.
Order from OTS $1 .25 PB 171 394
* The effect of various hydrogen interstitial contents be-
tween 60 parts per million and 312 ppm on the notch
sensitivity and low strain rate embrittlement of four
titanium alloys was investigated at room temperature.
The materials investigated included three alpha-beta
alloys: T1-6A1-4V, Ti-2Al-6Mo. and Ti-2.5Al-16V;
and one aU alpha alloy, Ti-5Al-2.5Sn, which were all
heat treated per manufacturers recommended sched-
ules . An optimum embrittling effect was encountered
between 180 to 220 ppm hydrogen content in the alpha-
beta alloys . Over the range of hydrogen content inves-
tigated the alpha alloy was not appreciably embnnled.
(Author)
Physical Sciences Lib. , Ordnance Tai*-Automotive
Command. Center Line, Mich.
METALLURGICAL APPUCATION OF X-RAY PRO-
JECTION MICRORADIOGRAPHY, by John Vettralno
and Fred Seppi. 12 Aug 60, 63p. 14 refs. Rept.
no. RR-28; AD- 246 799. ,
Order from OTS $1.75 PB 171 381
Four aspects of X-ray projection microradiography
were studied to determine the apphcability of this
technique for metallurgical investigation of ordnance
materials. First, methods of preparing the thin
specimens necessary for microradiographic examina-
tion were studied. Secondly, the resolution of the
X-ray projeaion microscope was measured by theo-
retical calculation and by several experimental tech-
niques. Several microradiographs were obtained of
ferrous and aluminum alloys so that the usefulness d
the X-ray microscope could be compared with the
optical metallograph. Finally, conversion of the X-ray
microscope to a more useful metallurgical instrument
capable of recording diffraction data or performing
spectrochemical analyses over microscopic sample
areas is considered.
461
Watervliet Arsenal , N. Y.
PRACTICAL EVAUJATION OF THE STANDARD
STRESS-STRAIN tURVES AND RELATED PROPER-
TIES, by R. H. F^rrington. July 60, 27p. 2 ref s .
Technical rept . \*VTRR-6010; AD-244 642.
Order from OTS |0.75 PB 161 896
The various properties derived from and associated
with the standard stress-strain curve are evaluated and
related to the behavior of alloys under stress . Several
other properties , idirectly related to the stress-strain
curve, are preferkble to the 0. 10% or 0.20% offset
yield strengths for present applications and future de-
velopments . Only major experienced opinion can choose
the property to be^t serve the purpose for this new era.
It is the abiUty of Ian alloy to deform elastically without
measurable plastii; deformation that determines its
most efficient and, safe use in most applications
(Author)
NUCLEAR PHYSICS AND
NUCIEAR CHEMISTRY
imnri
Air Force Camtiridge Research Labs. , Bedford,
Mass. I
TTiE DETECTlOff OF NUCUEAR EXPLOSIONS BY
SEISMIC MEANS,, by Norman A. Haskell. Guenter
Loeser Memorial, Lecture. 1959, 30p. CRD TN-60-632
Order from LC n*$2. 70, ph$4. 80 PB 153 395
I
General Electrid Reaearch Lab. . Schenectady, N. Y.
HIGH -ENERGY NUCLEAR PHYSICS RESEARCH PRO-
GRAM, by W. B. Jones. Final rept. for 1 Dec 46-
1 Dec 59 on Contract N7onr- 332(01). |an 60, 9p.
19 refs. Rept. no.i 60-GC-7; AD-230 162.
Order from LC m<$ 180, ph$ 1.80 PB 152 866
I
A 300- Mev nonfer^xxnagnetic synchrotron was devel-
9ped. A program p( research in high -energy physics
was carried out utilizing the 300-Mev synchrotron and
the 100-Mev betatron. Three large equipments for de-
tecting high-energjy particles or radiation were con-
structed: (1) a 6-l|j. -diam by 4 -in. -deep liquid hydro-
gen bubble chamber, (2) a 2S0-Mev total absorption
Cerenkov counter,; and (3) a 300-Mev magnetic pair
spectrometer. In the experimental program, 3 types
of interactions bet)ween high -energy photons and hydro-
gen were investigated: (1) large angle elastic scatter-
ing of photons by protons, (2) inelastic interactions be -
tween photons and protons giving rise to the production
of neutral and positive pions, and (3) total absorption
of photons in hydr^en to study electromagnetic inter-
actions.
Illinois U. , Urbaha.
PRELIMINARY PROPOSAL FOR OBTAINING
EMULSION IRRAEJIATIONS TO A 30 BEV INTERNAL
PROTON BEAM, b^ R. D. Hill. Technical rept. no.
12 on Contract Nodt- 1834(05). 8 Feb 60, 8p. 5 refs.
AD- 233 132.
Order frtxn LC m^l. 80, ph$l. 80 PB 153 151
Naval Ordnance Test Station, China Lake, Cahf .
SELECTED CHARACTERSITICS OF MARITIME
NUCLEAR POWER SYSTEMS, by Milton Neufeld.
16 Nov 60, lOp. 7 refs. NOHTS TP 2582.
Order from LC mi$l . 80, ph$l . 80 PB 153 407
This memorandum is concerned with determination of
seleaed economic and physical charactersitics of
nuclear power plants that might be used in cargo sub-
marines in the 1970-1980 period. Specifically, char-
acteristics are determined for 10, 25, 50, 85 and 100
thermal megawatt (tmw), maximum output reactors,
corresponding to approxiniately 3, 400 to 34, 000 nor-
mal shaft horsepower (assuming maximum sustained
shaft horsepower at 110]^ normal shaft horsepower and
reactor system ^ermal efficiency of 28. 5%). Esti-
mates are provided for original cost, operating and
nlaimenance costs, weights, and shielding require-
ments. References are provided for operating proce-
dures and power plant volumes. (Author)
Technical Operations, Inc. (Arllngtonl Mass.
A TRANSPORT CALCULATION OF THE NET CUR-
RENT OF PHOTONS IN AN INFINITE ISOTROR-
CALLY SCATTERING NON-ABSORBING ATMOS-
PHERE, by John F. Batter, Jr. Rept. on Contraa
DA 29-044-XZ-587. Mar 58, 18p. 6 refs. Rept.
no. TO! 58-8; AFSWP-1052; AD- 158 775.
Order from LC mi$2.40, ph$3. 30 PB 154 407
This report released for sale to the public 15 Feb 61.
Results are presented of some approximate calcula-
tions to determine the net current of photons impinging
on a specimen perpendicular to a radius from the
source, in a region close to the source. The accuracy
of the method used is dependent only upon the fineness
of the integration increment chosen. The general solu-
tion of the problem is presented and then specialized
for the case of no absorptions. The results are pre-
sented graphically as photon current in an isotropically
scattering atmosphere divided by photon current in a*
vacuum versus non-dimensional distance.
Vienna U. (Austria).
ON THE FERMI -YANG THEORY OF THE PION, by
W. Thirring, K. Baumann, and P. G. O. Freund.
Scientific note no. 4 on Contract AF 61(052)265.
10 June 60, 6p. 6 refs. AFOSR-TN-60-962.
Order from LC mi$ 1.80, ph$ 1.80 PB 153 309
It is proposed to reduce the strong interactions to the
universal weak interaction by considering them as high
energy phenomena of the strongly energy dependent
weak interaction. According to Feirmi and Yang the
pion is assumed to be a nucleon-antinucleon bound
state. A method presented in a previous paper is used
to solve a Bethe-Salpeter equation. The bound state
wave function is normalized, and the pion-nucleon
coupling-constant is calculated. The latter turns out
to be of the order unity although a weak interaction
between the fermions is used. (Author)
4<»2
Instruments and Installations
ComeU U. . Ithaca, N. Y.
THE PERFORMANCE OF A Be-Cu PHOTOMULTI-
PUER IN THE 100A-300A REGION, by D. H. Tom-
boullan. Technical rept. no. 3 on Contract Nonr-
401(37). Feb 6a 34p. 18 refs; AD- 233 222.
(^do- from LC mi$3. 00, ph$6. 30 PB 153 131
■Hie high amplification and the wide frequency re-
sponse of the electron multiplier have led to its use in
the detection of a variety of radiations in spearoscopy
and nuclear physics. It is the purpose of this paper to
describe the performance and reliability erf a particu-
lar photon counter whose behavior was found to be
quite satisfaaory in conjunaion with the determination
of absorption coefficients in the lOOA to 300A spectral
range.
MaterUls Research Lab. , Watertown Arsenal, Mass
A STEP SCANNER FOR EXPERIMENTS ASSOCI-
ATED WITH A NUCLEAR REACTOR, by J. J, Antal
and T. F. Zagaeskl. Feb 60. 26p. 5 refs. MRLrept.
no. 71; AD- 235 654.
Order from LC ml$2. 70, phK 80 PB 150 708
The design and operation is described o< a unit employ-
ti^ a step motor to advance a small mechanical or
electrcfnechanical device in precise increments over
a large angular range with automatic programming erf
this operation with a counting cycle and paper tape
read-out at all pertinent information. The circuitry Is
described in deuU to facilitate operation and mainte-
nance at the unit. The unit is useful In facilitating
procedures such as single- channel analysis, slltscan-
nli« during neutron beam alignment, and angular ro-
utlon of a crystal spectrometer. (Author)
Michigan U. Coll. of Engineering, Ann Arbor.
BEVATRON EXPERIENCE WITH A HOMOGENEOUS
LUMINESCENT CHAMBER, by L. W. Jones, K. Lai
and others . Technical rept. on Contract Nonr-
1224(23). Feb 60, 19p. 2 refs. 03106-2-T:
AD-233 501.
Order from LC mi$2.40, ph$3.30 PB 153 171
The components and uses of the luminescent chamber ,
and its performance in the photography of cosmic ray
tracks, have been discussed in previous papers. The
purpose here is to stress results and observations
based on what is believed to be the first experience
with a luminescent chamber at a muk*-Bev high-
energy accelerator .
Phyaics Lab. , Wright Air Development Div. , Wright -
Patterson AFB, Ohio.
AN INVESTIGATION OF THE RESPONSE OF PHOTO -
MULTIPLIER TUBES, by Gordon H. Griffith. Rept. for
Sep 57 -Aug 58 on Nuclear Instrumentation. Aug 60, 18p
I8p. 5 refs. WADD Technical rept. 60-364.
Order from OTS $0. 50 PB 171 402
The response of a photomultlplier tube Is related to its
average sensitivity and can be Improved by using only
the most sensitive part of the photocathode. This re-
port presents a number of graphs to Illustrate the re-
sponse of a photomultlplier tube as a function of the
point on the photocaihode surface that is Illuminated
and to indicate the improvement in symmetry erf the
isosensitivity lines that may be achieved by varying
the shield voltage. While the obaerved acnsitiviiies
were due primarily to the geometry al the cathode -
dynode configuration, they were also due partUlly to
the non -uniform response of the cathode surface.
(Author)
Western Ontario U. (Canada).
THE SPECTROSCOPY OF IONIC COLLISIONS. L
DESIGN AND CONSTRUCTION OF A SIMPLE 100 KV
PROTON ACCELERATOR, by E. M. Reeves. Scien-
tific rept. no. 4 on Contract AF 19(604)4560; Scientific
rept. no. 1 on Contracts AF 49(638)640 and Nonr-
2895(00). 1 June 60. 38p. 3 refs GRD-TN-60-497;
AFOSR-TN-60-484: AD-247 898.
Order frtwn LC mi$3. 00, ph$6. 30 PB 153 636
In order to study the luminosity arising from collisions
between positive ion beams and atomic qr molecular
gas targets over the energy range from 30 to 100 KV. ,
a pre* on accelerator has been constructed. The accel-
erator employs an Oak Ridge type ion source with an
electrostatic focussing system and magnetic mass
analyser to produce a proton ion beam. This first re-
port deals with the technical details of design, con-
struction, and operatiew of the accelerator, and also
the operating conditions under which preliminary ob-
servations on the spectra resultiiig from the ionic
collisions have been carried out. " Subsequent reports
will deal with the experimental programme carried
out on the accelerator. (Author)
Nuclear Reactions
Ecole Normale Sup^rieure (France).
TECHNICAL REPORT. Rept. for 1 Oct 56-30 Sep 58
on Contract AF 61(514)1060. (1958) 71p. 51 refs.
AFOSR-TN-59-224: AD-211 606. .c^^^o
Order fn)m LC mi$4. 50, ph$l2. 30 PB 150 693
Included in the report are:
Nucleon-antinucleon forces in the intermediate coupling
theory, pub. in II Nuovo Cimento 8:92-134, Apr 58
Exact determination of phenomenological separable in-
teraction, pub. in II Nuovo Cimento 8:699-707,
"June 58
This report summarizes the accomplishments of the
last two years and reviews the present situation of the
theory of nucleon and antinucleon forces.
Harvard U., Cambridge, Mass.
A RIGOROU9-DERIVATICW OF FERMI ACE
THEORY, by Martin A. Lelbowitz. Repc. on Contract
Nonr- 1866(34). Apr 60, I31p. 32 refs. AD- 237 414.
Order from LC mi$6. 90, ph$21 .30 PB 147 900
Fermi Age Theory provides a good representation of
the neutron moderation process in media containing
nuclei of only high atomic weight. The purpose orf this
thesis is to give a rigorous derivation of this theory.
463
TRG. Inc. , Syit*ett, N. Y.
THE SPM (STOCHASTIC PROCESS METHOD) EQUA-
TION FOR CALCULATING THE SPATIAL VARIA-
TION OF NEUTtON SPECTRA, by Carl N. Klahr
and Julius Zell. |ept. for May S9-May 60 on Mace-
rials Analysis and Evaluation Techniques, Contract
AF 33(616)5187 Sep 60, 158p. 47 refs. WADD Tech-
nical rept. 60-312
Order from GTS |3. 00 PB 171 397
Uppsala U. (Sweden).
ANTIFROTON INTERACTION CROSS SECTIONS, by
A. G. Ekspong arid B. E. Ronne. Technical rept. for
1 Sep 57-1 Sep 581 on Contract AF 61(062)13. phase A.
(19581 76p. 67 refs. AFOSR-TN-58-1077: AD-207 456.
Order from LC mi$4. 50, ph$l2. 30 PB 150 694
Included In the report are:
Antiprotons in nuclear emulsions, pub. in II Nuovo
Cimento 8:84-9i. Apr 58
Interactions in flight of negative heavy mesons, pub.
in Arklv fOr Fy^ik, v. 14, no. 18, p. 277-292,
Sep 58 I
Emission of charged £ t- II from K' -proton capture in
nuclear emulsictis, pub. in Artlv (t)r Fysik, v. 14,
no. 20, p. 303-)14, Sep 58
Decay modes and ilifetlme of negative heavy mesons,
pub. in Arkiv fbr Fysik, v. 14. no. 19, p. 293-302,
Sep 58
The research hasi been concentrated on two problems,
the pn^perties and behaviour of (1) antiprotons and
(2) negative K-metsons. The research tool and detect-
ing device has be^n nuclear research plates. (Author)
Radioactivity
Defense Atomic jSopport Agency, Washington, D. C.
HIGH ALTITUDE SAMPLING PROGRAM, by Albert K.
Stebbins, ni. Progress rept. 1 July 59, 33p. 6 refs.
DASA 529; AD- 227 709.
Order from OTS 1 1.00 PB 171 361
The high altitude sampling program was initiated to
determine the spread of weapon produced fission prod-
ucts through the stratosphere. U-2 aircraft was used
to sample stratospheric air at various altitudes along
North- South paths, from 66° N to 57° S at 7(P^. Over
1500 samples were analyzed. Metecn-ological correla-
tion was used to evolve a model of the stratosphere
which accounts fot the non- uniform deposition oi fis-
sion products. The total stratospheric inventory of
Sr90 as of the falljof 1958 was 1 megacurie. The half-
residence time of polar and equatorial injections into
the stratosphere N^as 6 and 12 mo, respectively. The
major portion of tne stratospheric debris moved into
the tropospnere tt^ough the mid- latitude tropopause
break. Prediaion^ of Sr^ levels to be found in equi-
librium bone wer^ made through 1972. (Author)
L
Isotopes, Inc. , We«wood, Hr-J.
HASP. ANNUAL 9RIEFING NO- 3, ed. by Albert K.
Te<4)nical analysis rept. 15 Dec 59,
KD-240 694.
Stebbins, ni.
112p. DASA 531;
Order from OTS $2. 50
PB 171 362
U-2 aircraft, operated by the Strategic Air Command,
have been sampling stratospheric air at various alti-
tudes along North- South paths in the Western Hetni-
sphere from 70° South to 70° North since 1957. Mete-
orological correlation has evolved a model of the
stratosphere which accounts for the non -uniform depo-
sition of fission products. The conclusion is reached
that equatorial Injections in the 1 to 5 megaton range
have a stratospheric half-residence time of around
10 months, while injections In the polar and temperate
regions have a stratospheric half- residence time of
around 5 months. Larger yield tropical injections
probably have residence times on the order of several
years. A definite seasonal effect upon the rate of de-
pftrture of debris from the stratosphere is shown. The
major portion of the stratospheric debris moves into
the troposphere through the mid- latitude tropopause
break. By 1 January I960, 87^ at all material injeaed
into the stratosphere will be on the ground. Predic-
tions of radiation dose from existing nuclear debris of
biological significance are made. (Author)
f^
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
ARCTIC FIELD EVALUATION OF GLOBAL GOG-
GLES, by Robert W. Eisner. [1956] 3p. Technical
note AAL-TN-56-3.
Order from LCml$ 1.80, ph$ 1.80 PB1535W
Testing has been carried out with particular regard to
features of goggle use peculiar to the Arctic. These
features Include function In extreme cold, protection
from snow glare, and protection from wind and blow-
ing snow.
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
CLEANING AND STERILIZATION OF BUNNY BOOTS,
by Lester E. Barlbo. [1956] lip. Technical note
AAL-TN-56-lO.
Order from LC mi$2. 40, ph$3. 30 PB 153 516
Bunny boots can be disinfected by several means to
provide protection of personnel from contaminating
infectious fungi. Formaldehyde gas, dry cleaning, and
washing with bleaching compound and strong laundry
soap at temperatures of 140-160° F. are adequate.
Laundering Is the recommended method fbr cleaning.
However, only bunny boots in top condition and slightly
soiled will be satisfactory for re -use. (Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
DRY COLD EVALUATIC»4 OF THE MD-1 ANTI-
EXPOSURE SUIT ASSEMBLY, by Robert W. Eisner.
[1956J lip. 1 ref. Technical note AAL-TN-56-2.
Order from LC mlS2. 40, ph$3. 30 PB 153 SOS
The MD-I ami -exposure suit assembly has been fleU
tested for an evaluation of Its potential as an arctic
survival garment in dry cold conditions. The assembly
ha« been found unsuitable for prolonged wear under
these conditions because of Inadequate Insulation and
undesirable moisture accumulation within the outer
Impermeable garment. (Author) -i
464
Arctic Aeromedical Lab. , Ladd AFB. Alaska.
RESULTS OF COLD WEATHER TEST ON THE
EVACUATION BAG, by Thomas R. A. Davis and
Franklin T. Elkins. [1956) I2p. 6 refs. .Technical
note AAL-TN-56-4.
Order from LC mi$2. 40, ph$3. 30 PB 153 510
Teats using methods for determining thermal balance
were carried out on the currently used evacuation bag.
The results show that, without further protection, this
piece at equipment, used in the manner described, is
unsuitable for transporting casualties on the HI 3
helicopter in the arctic and subarctic cold. Further
tests and modifications are planned for the future.
(Author)
Quartermaster Research and Engineering Center,
NaUck, Mass.
THE PSYCHOACOUSTIC AND COMFORT PROPER-
TIES OF HELMET COMMUNICATIONS GEAR, by
Alexander Cohen. Jan 60, 26p. 17 refs. Technical
rept. EP-123; AD- 245 090.
Order from LCmi$2. 70, ph$4. 80 PB 152 688
Sound suppression, speech intelligibility, and comfort
properties of the standard communications system
used in the Helmet, Combat Vehicle Crewman's,
T-56-6, were compared with those of an experimental
•ystem (RCA "Quiet Ear" Wt). Threshold- shift pro-
cedures showed that helmets fitted with the RCA gear
gave an average of 1 1 db more suppression for fre-
quencies 1000 to 8000 cps than those fitted with the
tundard system. This difference however, was re-
duced to 5 db In the critical low-frequency range o*
250 to 500 cps, while both helmet assemblies provided
negligible suppression at 400 cps. The RCA system,
despite its increased attenuation, was not believed
capable of reducing the Intense low-frequency compo-
nents of vehicle noise to safe levels. Moreover, both
systems under test greatly reduced the middle- and
high-frequency sounds which are less intense in vehi-
cle noise but are more critical to the perception of
speech sounds in the ambient environment. Speech,
intelligibility with the RCA kit was greater than with
the standard item, as determined in a field test using
M-48 tanks. Subjective appraisals of comfort, how-
ever, showed no preference for either system. The
helmet shell showed the greatest hmitations in
wearabllity and compatibility with operational tasks.
(Author)
PHYSICS
Bureau of Naval Weapons, Washington, D. C.
PRESSURE MEASUREMENTS 0 TO 31.5 IN. Hg.
BuWeps-BuShips Calibration Program. 21 June 60, 2lp.
Secondary Standards Lab. Measurement System Op-
eration Procedure SP-02.
Order from OTS $0. 75 PB 171 237
This procedure describes the operation at a secondary
standards laboratory calibration system which is used
to calibrate absolute pressure instruments and mer-
curial barometers in the range g< 0 to 31. 5 in. Hg.
This procedure normally applies to the calibratioo ct
Teat Instruments with accuracies between 0. 010 in.
Hg and 0. 050 in. Hg.
Brown U. Dlv. of Applied Mathematics, Providence.
R. I.
AN INTRODUCTION TO THE MATHEMATICAL
THEORY OF PERFECTLY PLASTIC SOLIDS, by
P. G. Hodge, Jr. Rept. on Contract N7onr- 358(01).
Feb 50, 401p. 168 refs. A11-S2/396; ATI-148 927.
Order from LC mi$ll. 10, ph$6i. 10 PB 154 291
This report released for sale to the public 10 Feb 61.
Contents:
Basic concepts
Struts and beams
Torsion
Plane strain and plane stress with axial symmetry
Plane strain - general theory
PrxAlems in plane strain
Discontinuous solutions in plane strain
Plane stress. Arbitrary yield conditions
Elastic -plastic problems
Approximate solutions
Extremum principles
Laboratory for Insulation Research. Mass. Inst, d
Tech. , Cambridge.
PROGRESS REPORT NO. 23. Rept. on Contracts
Nonr- 1841(10), AF 30(635)2872, and AT (30-1)1937.
June 58, 61p. 8 refs.
Order from LC mi$3. 90. ph$lO. 80 PB 150 922
Contents:
Dielectric spectroscopy
Electrical range
Optical range
Electrical and optical Investigation of charge-
carrier trapping in iMtile single crystals
Magnetic resonance
High -field -strength research
Ferroelectrics and ferromagnetica
Semiconductors
Single crystals
Ceramics
(See also PB 145 849)
National Bureau of Standards, Washington, D. C
MEASUREMENTS AND STANDARDS IN PLASMA-
PHYSICS AND ASTROPHYSICS AT THE NATIONAL
BUREAU OF STANDARDS, ed. by Lewis N. Brans-
comb. July 60, 33p. 141 refs. Technical note 59.
Order from OTS $1.00 , PB 161 560
Naval Research Lab. , Washington. D. C
A TABLE OF THREE INTEGRALS RELATED TO
THE PLANCK FUNCTION, by A. D. Anderson,
M. P. Shuler, and R. R. Best. Final rept. 6 Oct 60,
19p. 1 ref. NRL rept. 5532; DASA -1190; AD- 245 572.
Order from LC mi$2. 40. ph$3. 30 PB 149 296
A table of three integrals related to the Planck radia-
tion function has been prepared using the Narec.
These integrals give (1) the absorption rate. (2) energy
flux, and (3) number of photona absorbed in a volume
element at a given distance from a point source. The
assumption is made that the predominant emission is
X radiation and that the K edge at the absorbing me-
dium is sufficiently less than the peak of the "Planck
465
function to negledt absorption discontinuities. The
tabular values are given for the following ranges and
intervals of the argument: 0. 001(0. 0001 K) 0099;
0.01(0 001)0.099: 0. 1(0.01)0.99; 1.0(0.1)9.9; 10(1)99;
100(10)990. The table entries are given to four sig-
nificant figures. Aaymptaiic formulas are given which
are useful for calculating the values of integrals (for
energy flux) and (jfor number of absorbed photons)
when the argument is greater than 10. (Author)
Sjpeech Research Lab. , U. d Michigan, Ann Arbor.
STUDffiS ON IMRTLSED RESONATORS. PART L
RECURRENTLY IMPULSED RESONATORS IN
SPEECH AND PSYCHOPHYSICAL STUDIES. PART U.
DETECTION OF COMPLEX SIGNALS AS A FUNC-
TION OF SIGNAL BANDWIDTH AND DURATION, by
Ckn P. Gandhi, C« Otxigias Creelman and others.
Rept. no. 6 on Contract Nonr-1224<22). Feb 60, 42p.
14 refs 03U3-6^P; AD- 235 774.
Order from LC nW$3. 30, ph$7. 80 PB 153 170
The need for data on the perception at sounds pro-
duced by the exciqation d resonance systems is dis-
cussed in relation! to speech and psychioacoustics.
The voltage response d a series d N decoupled low-
pass resonator sections to the sudden application d
various types of iiput pulse trains is reviewed. The
output d such a series d resonators to a recurrent
impulse which is luddenly applied contains a dcterm,
a series of transient terms at the uncoupled resonator
frequencies, and ^ steady- sute term involving the
harmonics d the input pulse train. A circuit for
psychophysical tetts is described which provides a
number oif discretje positions d resonator frequency
and damping. SoitKl spectrographic analyses demon-
strating the transient arxJ steady-state terms for a
single resonator 4re presented. An experimental ex-
amination d the ejfficiency of human observers in de-
tecting a stimulus {waveform which consists of a train
d damped sinusoids is reported. The signal duration
and degree d damping (or spectral bandwidth) were
varied, with the e|iergy of the signal held constant.
Bandwidth is show^ to affect human detection more at
long than at short Idurations. (Author)
Etectricity and Magnetism
Ecole Nationale >uperieure de Chimie de Strasbourg
(France). i
CHEMICAL REACtnVITY NEAR CURIE POINTS, by
H. Forestier. Pinal status rept. for Oct 59-30 Sep 60
on Contract DA 91-591 -EUC- 1296, Continuation of
Contract DA 91-508-EUC-395. (1960) 15p. 3 refs.
Order from LC mtt2. 40, ph$3. 30 PB 153 281
The chemical reacjtivity as a function of temperature is
discontinuous, notonly near the Curie point d analloy,
but also near the ($urle point of the pure ferromagnetic
component. Chlorination was allowed to compare the
importance of the Anomaly of reactivity d several
Nl-Cu alloys near ttie Curie point of Ni. Ttie intensity
d the anomalies d^reases linearly while the percent-
age d non magnetic metal increases. Chlorination and
sulfldization were tallowed to compare the importance
y
of the anomaly in reactivity of several Ni-Cu alloys
near the Curie point of the alloy. The order of magni-
tude of the anomaly seems to be kept up, independently
of the copper content. Corrosion of Ni-Cu alloys
grows near the Curie point. Importance of this in-
crease d corrosion varies from 0 to 50 % with the
reagents used. Besides studying the oxidation of the
• phase of Pe-V alloys, it is proved that a transfomu-
tion takes place near 660^C Experiments for studyii^
the reactivity of a Palladium rich Co-Pd alloy near the
Curie point of cobalt, and the electrochemical behav-
iour of a nickel electrode near the Curie point of
nickel, have not given good results. (Author) (See
also PB 143 451)
Instituto Elettrotecnico Nazionale "Galileo
Ferraris" (Italy).
MAGNETIC VISCOSITY DUE TO INTERSTITIAL
ATOMS ANCHORED IN MSLOCATIONS MAGNETIC
VISCOSITY DUE TO MOTION OF DISLOCATIONS,
by Giuseppe Biorci, Andrea Ferro, and Giorgio
Montalenti. Technical note no. 2a on Contract
AF 61(514)1331. Oct 58, 62p. 37 refs. AFOSRTN-
59-85; AD-210 145.
Order from LC mi$3. 90, ph$10. 80 PB 150 695
Diffusion constants from magnetic measurements
agree with those obtained from internal friction:
Q > 32.000 cal/gr. at., Cq" 10'^*^ sec. in iron sheai
loaded with carbon, cold rolled of 7% and aged at
room temperature. Above 320° C well annealed
Armco specimens show a viscosity field of about
0, 5 A/m. The correspondence with mechanical relax-
ation and the shape of the curve of the magnetic relax-
ation vs. field strength seem to prove that the ob-
served magnetic viscosity is due to motion of
dislocations.
Electronics
Ballistic Research Labs. , Aberdeen Proving Ground,
Md.
A STUDY OF THE SHOCK WAVE GROWTH FROM
A WEAK ELECTRICAL DISCHARGE, by Ona R.
Lyman. Aug 60, 29p. 7 refs. Memo. rept. no. 1300;
AD-246 716.
Order from LC mi$2. 70, ph$4. 80 PB 153 073
The growth of the shock wave around an electrical
spark is studied in an attempt to examine the energy
partition in the spark gap. Several treatments of
shock phenomena are discussed. It is shown that the
treatment d A. Sakurai best describes the stuck wave
associated with the low energy disctiarges discussed.
(Author)
California U. , Los Angeles.
EXTENSIONS IN THE SYNTHESIS OF TIME OPTI-
MAL OR "BANG-BANG" NONLINEAR CONTROL
SYSTEMS. PART IH. SYNTHESIS AND ANALYTIC
STUDIES OF OPTIMUM TYPE II NONI.INEAR CON-
TROL SYSTEMS WITH COMPLEX ROOTS, by
P. Chandaket and C. T. Leondes. Rept. on Contract
AF 49(638)438. June 60, 63p. 44 refs. Dept. of Engi-
neerii^ rept. no. 60-47; APOSR TN-60-960;
AD-246 353.
Order from LC mi$3. 90, ph$10. 80 PB 153 099
It is the purpose of this investigation to present the
(Muired frfiase space solution for the optimum non-
linear controller for second-order systems, and thus,
to fill an important gap in the literature in the control
lystems field. The derivation of the required opti-
mum nonlinear controller is a fairly involved process
u this report demonstrates. The resultant controller
is a fairly complicated device and it presents some
practical problems in its mechanization; as a result
■one compromise optimum nonlinear controllers are
presented. The report concludes with studies of the
(jynamic response capabilities of these systems. A
Ttriety of input forcing functions are applied to sys-
tems with optimum and compromised optimum non-
linear controllers, and their excellent response capa-
bUities observed. (Author)
Electronics Research Lab. , U. of California,
Berkeley.
TRANSIENT BEHAVIOR OF AN ELECTRON STREAM-
AT AND BEYOND LIMITING CURRENT, by W. B.
Bridges and C. K. Birdsall. Interim rept. on Contraa
AF 49(638)102. 2 Aug 60, 29p. 9 refs. lER series
DO 60. issue no. 303; AFOSR TN-60-878; AD- 245 96a
Order from LC mi$2. 70. ph$4. 80 PB 152 931
Contents:
Review of dc theory and solutions, broad stream
Dc experiment, thin stream
Theory and solution for limiting current in thin stream
Estimate of the transient behavior at limiting current
Calculations of trajectories
General Electric Co. , Schenectady, N. Y.
INVESTIGATKDN OF VARIOUS ACTIVATOR -
REFRACTORY SUBSTRATE COMBINATIONS, by
J. H. Affleck. Scientific rept. no. 10 on Contract
AF 19(604)4093. 29 Nov 60. Up. 3 refs. AFCRL-
TN -60-1155.
Order from LC mi$2. 40. ph$3. 30 PB 153 683
Additional data is reported on the thermionic con-
stants and evaporation rates of refractory substrate -
activator combinations. A number of systems exhibit
favorable emission characteristics but have evapora-
tion rates that are higher than most conventional
emitters. Alterations are t»eing made in the twirium
dispensing alloy to lower the evaporation rate of
barium. (Author) (See also PB 152 610)
Molecular Physics and Spectroscopy
Air Force Cambridge Research Labs. , Bedford,
Mass
LINE WIDTHS OF PRESSURE BROADENED SPEC-
TRAL LINES, by C J. Tsao and C. Curnutte (Ohio
State U. Research Foundation). Sep 60. 95p. 19 refs.
Geophysical Research Papers no. 69; AFCRLTR-
60-279.
Order from LC mi$5. 40, ph$15. 30 PB 153 392
This report is mainly of a review and expository
nature and has been prepared for the purpose of out-
lining in considerable detail the method of calculating
the widths of pressure-broadened spectral lines by
using the impact theory of P. W Anderson. The gen-
eral quantum mechanical result is derived, the adia-
baiic approximations are discussed, Anderson's
theory has essentially been repeated with some slight
changes, and several cases of molecular interactions
are treated. The calculations have been extended to
include the effect of the nonresonant terms of the
interaction matrix which are neglected in Anderson's
work. (Author)
Air Force Cambridge Research Labs., Bedford,
PHENOMENOLOGICAL CONSIDERATIONS OF THE
INTERRUPTION THEORY OF LINE BROADENING,
by Robert G. Breene, Jr. Guenter Loeser Memorial
Lecture. 1956, 18p. GRD-TN- 60-630.
Order from LC mi$2. 40, ph$3. 30 PB 153 393
Britis4i Columbia U. (Canada).
THE DETERMINATION OF ICWEZATION AND DIS-
SOCIATION POTENTIALS OF MOLECULES BY
RADIATION WITH ELECTRONS, by a C Frost and
C A. McDowell. Final rept. for 1 Apr 59-30 Sep 60
on Contract AF 19(604)2275. [1960] 36p. 32 refs.
AFCRL-TR-60-423.
Order from LC mi$3. 00, ph$6. 30 PB 153 397
The ionization and dissociatlonof molecules by electron,
impact was studied using the retarding potential
difference method (R. P. a ) to obtain monoenergetic
electrons. Preliminary studies on the photoionization
0^ simple molecules have also been carried out. The
electron Impact studies have led to a considerable
amount of new information about the ionization po-
tentials of molecules and also the electron impact in-
duced dissociation process. Amongst the molecules
studied were C^, the halogens HF, CSo, NUO, COS,
COo. formaldehyde, acetaldehyde, H2O, ¥2^' *"*•
meniyl cyanide. The photoionization studies were
largely restricted to the NO, and NH3 molecules.
(Author)
Mallinckrodt Chemical Lab. , Harvard U. ,
Cambridge, Mass.
STARK EFFECT AND MPOLE MOMENT OP
CH3CHF2. by George H. Kwei and EXidley R.
Herschbach. Rept. rti Contract Nonr- 1866(14). [1960J
7p. 5 refs. AD- 231 493.
Order from LC ml$l. 80, ph$l. 80 PB 153 153
Measurements were made of nonquadratic Stark ef-
fects for the M= 1. J = l-»2, "a-type " transitions,
and quadratic shifts which occur for the corresponding
M ■ 0 lines of the spectrum of the CH3CHF2 molecule
The two types of transitions provided two independeirt
determinations of xhe dipole moment which agreed
within experimental error.
Maryland U. . College Park.
ELECTRON SPIN RESONANCE, by Roy S. Anderson.
Rept. 00 Contraa AF 19(600)1582. Nov 60, 112p.
119 refs. Dept. of Physics Technical rept. no. 200:
AFOSR -TN-60- 1373; AD-246 896.
Order from LC ml$6.00, ph$18. 30 PB 153 291
467
The relatively reqent research technique of electron
■pin resonance is reviewed with particular emp>hasls
on experiniental drtails, such as apparatus and
interpretation. The theoretical section discusses
those aspects erf ttie method required both for the
initiation and intecpreution of experiments. The ex-
perimental section considers those details erf impor-
tance to the design and operation of the apparatus.
The following subjects have been treated: (1) quantum
mechanical descrittion, including energy levels,
selection rules, e^eas al crystalline electrostatic
fields and nuclear magnetic moments, and spin re-
laxation; (2) principles of spectrographs; (3) radio
frequency and microwave components; (4) amplifica-
tloa and deteaion;|(5) magnetic field; (6) sensitivity;
and (7) electron- n^lear double resonance technique.
(Author)
Massachusetts Wst. at Ttech. , Cambridge,
THE AXIAL-FLOW COMPRESSOR IN THE FREE-
MOLECULE RANCE, by Charles H. Kruger. Rept. on
Contract Nonr-lMl (55). Jan 60, 96p. 22 refs. DSR
7-8120: AD- 231 «J5.
Order from LC mi$5. ■«, ph$15. 30 PB 152 874
The performance fci the free-molecule range at an
axial-flow ccmpreisor with flat-plate blades was an-
alyzed. Theoretical calculations are made for single
and multiple blade rows, using the Monte Carlo method.
Results indicate that density ratios per blade row are
significantly greater in the free-molecule range than at
aerodynamic conditions. Density ratio Is found to in-
crease with increaeing blade speed and decreasing
blade angle and to decrease linearly with the upstream
volume flow rate. .Multiple-blade-row calculations
show that single- r0w results may be directly combined
with reasonable accuracy. Experimentally, density
measurements acrtxs a single rotating blade row give
density ratios as high as >6:1 and show a gcjod
agreement with theoretical results. Density ratio is
found to decrease markedly with increasing density
level in the transition from the free-molecule range.
Suggestions are made regarding the design at a
rarefied-gas compressor at this type. A comparison
of such a compresaor with the commonly employed oil
diffusion pumps shews several favorable aspects. The
Monte Carlo method is found to be a useful tool for the
solution of problen- s involving the dynamics of rare-
fied gases. (Authoi)
Michigan U. Coll^ of Engineering, Ann Arbor.
SPIN RESCWANCE PROPERTIES OF SAPPHIRES,
CERTAIN AiiBvi COMPOUNDS. AND CALCITE, by
Chihlro Kikuchl . Final rept . on Contract
AF 49(638)6«. Oct 60, 57p. 67 refs. 2616-17-P;
AFOSR-TR-60-13li
Order from LC inl|3.60, ph$9. 30 PB 152 836
This report summarizes the electron- spin resonance
properties of sapphires with various iron group im-
purities, d ceruln A[]Bvi compounds, and at caldte.
A block diagram of a molecular electronic material,
such as pink ruby, (s given, to indicate possible di-
rections for future Investigations. Extensive refer-
ences are given, (i^uthor)
Ohio State U. Research Foundation. Columbus.
TEMPERATURE EFFECTS ASSOCIATED WITH
PRESSURE MODULATED INFRARED SPECTRA, by
Richard Ronald Patty (Doaoral thesis) and Dudley
Williams. Scientific rept. no. 1 on Contract
AF 19(604)6141. Oct 60, 157p. 24 refs. AFCRL-
TN-60-815.
Order from LC mi|7. 50, ph$24. 30 PB 153 657
The work described in this report represents a con-
tinuation at the earlier work of James C. Gilfert on
pressure modulation at infrared spectra. The con-
struction at a new modulator in which sample volume
is known as a function of time has made it possible to
obtain a more nearly quantitative interpretation at re-
sults obtained in studies at pressure modulated absorp-
tion and has per mined the observation at modulated
emission spectra erf various atmospheric gases.
(Author)
Sarah Mellon Scaife Radiation Lab. , U. of Pittsburgh,
Pa.
A MULTl-MODE CHARGED PARTICLE ANALYZER,
by Lome A. Page. Technical rept. no. 2 on Low Energy
Nuclear and Electron Physics, Contract DA 36-034-ORD-
2765. [1959] 50p. 11 refs. OOR rept. no. 2211. 1-P;
AD- 233 608.
Order from LC mi$3. 30, ph$7. 80 ffl 150 700
A proposed analyzer for ions or electrons having momo
tum per unit charge ranging up to one million volts/c is
based on cyUnch-ical geometry with a homogeneous mi^-
netic field throughout the apparatus parallel to the axis c(
symmetry. It is calculated that point to point focus with
reasonably gtxid aperture can be had by introduaion of
a radial electric field over a certain intermediate reglov
thus having a crew sed- field selection operating in the
common magentic field. A number at possible modes of
operation are discussed, including those applicable to
mcxnentum spectrometry, to specific charge sorting. Mil
to recognition cfkinematically special knock-on electroas.
Washburn Observatory [Madison, Wis.]
COMPARISON SOURCES FOR LOW-DISPERSION RA-
DIAL-VELOCITY MEASUREMENTS IN THE RED
SPECTRAL REGION, by Gerald T. Davidson. Techni-
cal rept. on Contract Nonr- 2824(00). [1960] 5p. 6 refi
AD- 232 041.
Order from LC mil 1.80, ph$ 1.80 PB 153 136
Optics
Bureau of Naval Weapons, Washington, D. C
INFRARED RADIATION BLACK BODY SOURCES
50^0 TO 600PC, 0. 0087 TO 0. 50 INCH DIAMETER
APERTURE, BuWeps-BuShips Calibration Program.
27 Apr 60, 40p. Secondary Standards Lab. Measure-
ment System Operation Procedure NR-01.
Order from OTS $1.00 PB 171 238
This procedure describes the operaticxi of a secondary
standard e:allbratiejn system which is used to calibrate
sources oi. infrared energy by radiometric cxjmparison
46«
against a reference source, the radiation character-
istics of which are acenirately known. This prtKedure
normally applies to the calibration of Test Instruments
with stabilities between 0. 02°C and lO^C.
University Coll. , Dublin (Eire).
OPnCAL ABSORPTION IN INORGANIC SOLIDS, by
W. p. Doyle, G. A. Lonergan, and D. C Conlon.
Annual technical rept. no. 1. 1 Oct 59-30 Sep 60, on
Contract DA 91 -591 -EUC- 1283. 20 Oct 60, lOp. 5 refs.
Order from LC m41. 80, ph$1.80 PB 153 094
The absorption spectra of chin films of germanium
moocKide, germanium dioxide, zirconium dioxide,
vanadium pentoxide, columblum pentoxide and tantalum
pentoxide have been determined from 2000-10. OOOA.
Each material is characterised by strong absorption in
the region studied; the threshold photem energies are
as follows: - germanium monoxide - 2. 7 e. v. ; german-
ium dioxide - 4. 3 e. v. ; zirconium dieixide - 5. 2 e. v. ;
vanadium pentoxide - 2. 4 e. v. ; columblum pentoxide -
3. 8 e. V. ; tat«alum pentoxide - 4. 4 e. v. The absorp-
tion coefficient in the region of high absorption is so
Urge that absorption must be attributed to the bulk
lattice and not to impurities. An A. C. method of
measuring the spectral distribution of photex:onduc -
tivlty In thin films of solids has been developed. Re-
sults are repnrted for the lead and thallium halides.
(Author) >
Solid State Physics
Armour Research Foundation, Chicago, HI.
MECHANISM OF WEAR OF NONMETALLIC MATE-
RIALS, by Edwin J. Latos. Rept. for 1 June 58-
31 May 59 on Research on Interface Phenomena, Con-
tract AF 33(616)5962. Oct 59. 19p. 27 refs. WADC
Technical rept. 59-316; AD-232 467.
Order from OTS $0. 50 PB 171 474
The principal objective of this project is a basic study
to evaluate the mechanism of wear erf nonmetallic ma-
terials at elevated temperatures. Materials selected
for this program included single crystals of sapphire
and quartz. A friction apparatus was designed for use
at high temperatures and has an operating range of 0 to
50 grams load and a speed range of lO'^ to 10"^
cm/sec. The friction specimens are placed into sult-
alde holders and heated with an induction generator.
Initial tests established the reliability eif the design of
the friction apparatus to operate effectively from rcxxn
temperature to VtCfPV. Design of suitable specimen
holders should permit friction studies at temperatures
to 4000^. Sliding of sapphire on sapphire indicated
an increase in the ce^efficient of friction with tempera-
ture to approximately 90C1PF and a decrease with fur-
ther Increases in temperature to 1600PF. The coeffi-
cient of friction also increased with load in the tem-
perature region reported. (Author)
469
Battelle Memorial Inst. , Columbus, Ohio.
INDIUM ANTIMONIDE FOR SEMICCWDUCTOR-
C«VICE FEASIBILITY STUDIES, by F. J. Reld,
T. & Shllliday and others. Rept. on Contraa AF
33(616)6450. Apr 60, 67p. 55 refs. WADD Technical
rept. 60-387.
Order from OTS $1. 75 PB 171 406
The performance of voltage and current regulation
using magnetoresistance effects In InSb has been
demonstrated analytically for both dynamic and steady-
state conditions. Regulation of output voltage to less
than 1 per cent of its steady- state value appears
practicable. Single crystals of InSb having carrier
concentrations in the range 10^^ to 10*^ carriers/cm^
have been characterized by measurements of Hall
coefficient, resistivity and electron mobility as func-
tions of temperature, magnetoresistance and Hall
effect as functions of magnetic field, and minority-
carrier lifetime. Anisotropic distrllxition erf impuri-
ties was observed In InSb crystals grown along the
[111] axis. This effect can be minimized by pulling
crystals on other orientations. Grown p-njunctlons
of InSb have been prepared, and current- voltage
characrteristics of diodes from this material have been
obtained at SO^K and as a function of temperature.
Lifetime values as high as 0. 5 microsecond were
measured at SO^IC Semlconduexlng thin films of InSb
have been prepared by the flash-evaporation method
and were ftxind to be continuous, conducting, and
chemically stable. Their composition, thickness,
size of crystallites, aixl electrical properties were
determined. (Author)
Diamond Ordnance Fuze Labs. . Washington, D. C
NOTES ON THE RELATIONSHIP OF TEMPERATURE
AND RESISTANCE, by Joseph Pearlsteln. 1 Dec 60,
9p. 8 refs. Technical rept. TR-888.
Order from OTS $0. 50 PB 171 187
This report presents some notes on the relationship of
temperature, electrical resistance, and thermal ex-
pansion for metals and semiconductors. (Author)
Illinois Inst, of Tech. , Chicago.
ELECTRON DENSITY DISTRIBUTIONS IN ZnO
CRYSTALS, by Ganesh P. Mohanty and Leonid V.
Azaroff. Rept. on Contract AF 49(638)425. 28 Nov 60,
14p. 12 refs. AFOSR-TN-60-1352.
Order from LC ml$2. 40, ph$3. 30 PB 153 552
Electixxi density distributions have been determined
for two ZnO crystals that had been heated.ln Zn vapor
and for an undoped crystal by very accurate measure -
mentB of their x-ray diffraction intensities. An ex-
amination of the difference between the electron den-
sities of ckjped and undoped crystals shows that the
doped crystals contain 5-20x10^9 atoms/cm^ in the
(x:tahedral Interstices. The incorporation erf this
Urge number of interstitial Zn atoms iocreaaes the
unit cell volume of the crystal by nearly 0. 9%. The
density erf interstitials is approximately 1000 times
greater than that calculated from the elctrical cx)n-
ductlvlty erf these crysuls so that it must be con-
cluded that most of the interstitial Zn atoms are
electricrally neutral. The presence of these intersti-
tials explains why the time required to reach satura-
tion for electrical conductivity is much greater in
virgin crystals than in previously doped ones.
(Author)
niinols U. . Urtiana.
LOW TEMPERATURE PHOTOOONDUCnVITY OF
ADOmVELY COLORED KQ. by Roben L. Wild.
Frederick C. Brclwn. and N. Inchauspe. Technical
note no. S on Contract AF 49(638)579. Aug 60, 36p.
29 refs. AFOSR-tN-60-1117; AD-245 540.
Order from LC ini$3. 00, ph$6. 30 PB 152 604
The main empha
ature yield and t
leased by light
LUty banda at
s in this work is on the low temper -
nsport properties of carriers re-
rbed in the F. K. and so-called
r energy.
Institute c4 Engitieering Research, U. of California,
Berkeley.
EFFECT OF TE1«^RATURE ON THE CREEP OF
POLYCRYSTALLBME ALUMINUM BY THE CROSS-
SUP MECHANISII. by N. Jaffe and J. E. Dorn. Rept.
for 1 Apr 59-31 Mar 60 on Materials Analysis and
Evaluation TechniDues, Contract AF 33<6I 6)3860.
June 60, 2lp. 8 r^fs. [Series 108, issue 4] WADD
Technical rept. 6<)-53; AD- 234 957.
Order from OTS lO. 75 PB 171 360
The apparent actiyaticn energy for creep of polycrys-
talline aluminum was determined over the range of
273° to 350*'K by the effect of small abrupt changes In
temperature qn tli» creep rate. A constant activation
energy of 27, 400 i 1000 cal/mole was obtained over
strains of 0. 003 ti 0. 23, stresses ranging from 2250
to 6000 p. s. i. anq strain rates varying from
0.1145 X 10"5 to ^.5 X 10"5 per minute. Metallo-
graphic studies artd comparison with theory suggested
that creep in this range is controlled by the rate of
cross-slip of disltications. Both X-ray diffraction
analyses and roort temperature tensile stress- strain
data following pre^creep revealed that the substructure
produced In this rjange by creep under a given stress
depended only on the total creep strain being independ-
ent of the actual test temperature. As a result it was
deduced that the tttal strain f, during creep under a
given stress should be a function of temperature com-
pensated time 0 ^ te
■RT'
where t is the duration of
the test, Q the aptnrent activation energy, R the gas
constant and T tM absolute temperature. A number of
creep tests conducted at two different temperatures
verified the validity of this conclusion. (Author)
Institute at Tech , U. at Minnesota, Minneapolia.
THE NATURE Olf THE NUCLEATION OF PRECIPI-
TATES IN THE giLICON-LITHlUM SYSTEM, by
J. W. Ferman and R- A. Swalin. Technical rept. no. 2
on Contract Nonr-f? 10(27). 4 Apr 6a 22p. 13 refa.
AD-236 193.
Order from LC mt)2. 70, ph$4. 80 PB 147 120
The concentration dependence of the kinetics of precipi
tation at lithium ffom silicon has been imreatigated.
The precipitation kinetics follow a simple exponential
decay process for the last 50^ at the precipitation.
From this portion of the process, values of X the
characteristic timie, have been calculated and the fol-
lowing relation apfiears to be valid ijp'^'YIo^^ where C^
is the lithium content at the initiation of precipitation.
A microscopic technique has been devised to delineate
precipitate particles. These appear to have the shape
at disks or oblate spheroids aod are present to the ex-
tent of about 5 X 108/cm3. Values of Tcalculated fixm
the particle shape and number density are in agree-
ment with the experimentally obtained values. Usii^
the relation I/y^Cq^/^ coupled with Pell's obaervatki
that for constant Cq. ^/■y'^Or^^, it la deduced that
the nunnber density of nuclei are proportional to but u
equal to the concentration of dissolved oxygen. Fur-
ther, the number density of nuclei is independent of
Co the initial lithium content. The suggestion is made
that the nucleation catalyst consists erf a complex con-
taining oxygen and some type of lattice defect. (Author)
Laboratory for Insulation Research, Mass. Inst, of
Tech., Cambridge.
COLOR CENTERS IN CESIUM HALIDE SINGLE
CRYSTALS, by Peter Avakian. Rept. on Contraa
Nonr- 1841(50). Apr 60, 44p. 60 refs. Technical
rept. 149.
Order from LC mi$3. 30, ph$7. 80 PB 147 174
Cesium chloride crystals have been grown from solu-
tion with urea activator and from the melt. Cesium
bromide and Csl crystals were grown from the meh
only. Coloration was produced by 130-kv X rays,
3. 0-Mev electrons, and by elearolysis. The absorp-
tion of uhcolored and colored crystals has been meas-
ured from 0. 175 to 3.5 ^at 25°, -78°, and -190OC.
All three crystals show one strong band in the visible
(near infrared for Csl) and several weaker bands at
shorter and longer wavelengths, which shift with tem-
perature change.
Laboratory for Insulation Research, Mass. Inst.
of Tfech. , Cambridge.
PRESSURE DEPENDENCE OF THE NEEL TEMPER-
ATURE IN CoO AND NiO, MEASURED WITH A
NEW DILATOMETER, by Theodore P. Janusz. Rept
on Cbntract Nonr- 1841(10). Apr 60. 32p. 19 refs.
Technical rept. 150. AD- 237 059.
Order from LC ml$3. 00, ph$6. 30 PB 147 759
A high-pressure dilatcmeCer employing a gaseous
pressure medium has been developed to measure, ovct
a range of pressures and temperatures, the change la
sample length that occurs in many solid-state phase
transformations. The device employs a differential
transformer as length detector. The system at pre-
sent covers a temperature range of -40" to 2750Caiid
a pressure range up to 10, 000 atmospheres. With a
low- temperature cryostat the temperature rangemay
be extended downward.
Laboratory for Insulation Research, Mass. Inst, of
Tech., Cambridge.
A REFINEMENT OF THE DICKITE STRUCTURE
AND SOME REMARKS ON POLYMORPHISM IN
KAOLIN MINERALS, by Robert E. Newnham
(Cavendish Lab. , U- of Cambridge). Rept. on Con-
traa Nonr- 1841(10). Apr 60, 32p. 23 refs. Technical
rept. 148; AD-236 323.
Order from LC ml$3.00. ph$6.30 PB 147 173
470
The crystal structure of the clay mineral dickite
(Al2Si2H409) ^^ ^'^^ refined to a greater accuracy
than that reported in an earlier analysis. The refine-
ment was carried out with zero- layer intensity data
collected about [100] and [HO] using MoKa radiation.
Coordinates obtained after ten cycles of (F© - Fq) ^^'
ference syntheses gave an R faaor of 7.5% for 420 ob-
served reflections. Improved lattice parameters,
«-5.150± 0.001, b- 8.940r: 0.001, c -14.424 ±
0.002A, P -96' 441 1'. were determined by graphical
extrapolation from slngle-crysul diffraction spectra
near 9-90 degrees. The dickite structure shows
several significant distortions from the geometry of
the idealized kaolin layer, including deformation and
rotation of the silica tetrahedra. The most striking
features of the octahedral layer are the extren»ely
short shared edges of 2. 37 A. A model consistent with
the infrared absorption spectra is proposed.
Lincoln Lab. . Mass. bist. at Tech. , Lexington.
ANISOTROFY IN PERMALLOY FILMS EVAPORATED
AT GRAZING INCIDENCE, by M. & Cohen. Rept. on
Contract AF 19(604)7400. 23 Nov 60, 8p. 2 refs,
53G-0042. AD-246 887
Order from LC mi$l. 80, ph$l. 80 PB 153 284
The magnetic and optical anisotropies observed in
oblique- incidence Permalloy films show anomalous
behavior for incidence angles greater than 60°
(grazing Incidence). In particular the easy axis and
the direction of greatest optical absorption are paral-
lel to the vapor beam for incidence angles greater than
about 7CP, while they are perpendicular to this di-
rection for smaller angles. The anomalies for grazing-
iocldence films are caused by a shape anlsotropy
differing from that previously found in lower angle ob-
lique-incidence films. This new shape anlsotropy is
attributed to the elongation in the beam direction of
the particles composing the crystallite chains which
•re found in all oblique- incidence films; such shape
anlsotropy has been directly observed by electron
microscopy. (Author)
Materials Research Lab. , U. of California, Berkeley
INVESTIGATION OF FACTORS CONTROLLING
PROPERTIES OF PRESSURE-SINTERED ALKALI
HALIDES, by P. J. FettaandE. R. Parker. Technical
rept. no. 2 on Ductile Ceramics Research. Contract
AF 49(638)601. June 60, 24p. 7 refs. Series no. 150.
issue no. 2; ARPA Order no. 24-59, Task 2; AFOSR
TN-60-707; AD- 243 979.
Order from OTS $0.75 PB 171 371
A method is described for producing fine-grained
polycrystalline alkali halldes by a vacuum pressure
sintering technique CONCLUSIONS: Transparent
disks may be prepared from any of the alkali, sliver,
or ammonium halides. To accomplish this, sufficient
pressure, a sufficiently low vacuum, and fine-grained
powder of high purity and a reasonably low moisture
content must tx used. If powder which has not t>een
freshly prepared is used, surface contamination im-
pana a yellow coloration to the final disk. As the
powder ages, this coloration increases until finally
only translucent or opaque disks are obtained. The
pressure at which a material becomes transparent is
related to its lattice energy. The softest disk is pro-
duced not at the lowest pressure for transparency but
at a higher pressure. This effect seems to be due to
surface contamination. The plates are of almost
theoretical density. (Author)
Massachusetts Inst, of Tech., Cambridge.
NEUTRON AND X-RAY DIFFRACTION STUDIES OF
SOLIDS, by C. G. Shull. Technical rept. no. 5 on
Contract AF 18(603)84. 1 Jan 60, 40p. AFOSR TR-
60-111; AD-245 613.
Order from LC mi$3.00, ph»6.30 PB 152 982
A summary at the projea activities is g^ven in this
final technical report. The design characteristics of
the three neutron diffraction spectrometers (single
crystal analysis, polycrystalline specimen, and
polarized beam units) which have been constructed are
discussed. A description is given of the monochromat-
ing crystal studies and the intensity and resolution
studies on the spectronrieters which have been per-
formed. Research studies which have been carried out
by project personnel are summarized. (Author)
Materials Research Lab. , U. of California, Berkeley.
KINETICS AND MECHANISMS OF SOLID-STATE
REACTION BETWEEN BARIUM METATTTANATE
AND BARIUM CARBONATE TO FORM BARIUM
ORTHOTITANATE, by E. R. McCartney, L, K.
Templeton, and J. A, Pask. Technical rept. no. 7 on
Contracts N7dnr-29524 and Nonr-222(68). 1 Apr 60,
36p. 5 refs. lER series no. 18, issue no. 7; AD- 236 458.
Order from LC mi $3. 00, ph$6. 30 PB 146 924
Reactions between mixtures of BBTIO3 and BaC03
powders of controlled particle size to form BB2Ti04
were followed by the lo«s of weight due to CO2 evo-
lution. A unique feature of this heterogeneous reactiao
is the formation of a ■BBC03-phase " by partial re-
duction of the Ba003 which readily flows unto the
BBTIO3 and resultant BbjTIO, surfaces. The overall
reaction rate is a function of the successive steps of a
chemical reaction mechanism, which is interpreted
as a nucleation process, and a dlffusional mechanism.
The ratio of the total surface to the total volume and
the geometry of the relative particle distribution are
important factors in the overall kinetics. In the
temperature range of 800 to lOSO^C the first order
rate law, wherein the surface was expressed in terms
of the volume or weight, was followed best by
mixtures of fine or precipitated BaC03 and precipi-
tated BBTIO3. The pMrabolic rate law was followed
most closely for mixtures of coarse BaCOs and pre-
cipitated BBTIO3. Zero order kinetics were obtained
for mixtures wherein the BaTlOs was coarse. The
activation energy for the first order process is 56-58
kcal. /mole; for the dlffusional process, 28-31. In
intermediate type mixtures, bothprocesses oftheap-
proprlate activation energies were operative.
(Author)
New York U., N. Y.
THE STUDY OF A CLASS OF INTERMETALLIC
COMPOUNDS, THE CHALCOPYRITES, by S. Zalar
and L Cadoff. Rept. for Feb 57-Aug 60 on Contract
AF 33(616)3959. Oct 60, 63p. 15 refs. ARL Techni-
cal rept. 50-316.
Order from LC mi$3. 90, phJlO. 80 PB 150 323
471
Hiree compositicfeis of the class of polyatomic semi-
conductors d the chalcopyrite structure A'bI^Ic^
were investigated by thermal, microscopic, mechani-
cal and electrcxil^ methods. Only the first two were
found to b» intentietallic semiconductors, the compo-
sition AuInTe? stiowins the metallic character d a two
phase alloy, Au jsin 25^^. 50' Melting points,
Vickers hardnes^, micro and macrostructures of
CuInTe2, and Au^ 25^1 25^* cq were determined. At
room temperatur^ theelectffcal resistivity d
CuInTe2 was at t^ order d 1 x 10'^ ohm-cm, that of
AglnTe2 d the oijder of l2-l0 ohm-cm and that of
A". 25^ 25^* 50 '^ ^*'* order of i x 10"^ ohm-cm.
(Author)'
North Carolina U. , Chapel Hill
ROOM- TEMPERATURE DISLOCATION DECORATION
INSIDE LARGE (pRYSTALS, by Charles a Child*
(National Aerooailtics and Space Administration) and
Lawrence Slifkin., Rept. on Contract AF 49(638)865.
7 Nov 60, 5p. 4 Defs. AFOSR-TN-60-1371.
Order from LC nli$L 80, ph$l. 80 PB 153 564
This note describes a technique which displays with
great contrast thQ distribution d dislocations in the
interior of large jingle crystals d silver chloride.
(Author)
Office of Technipl Services, Dept. of Commerce,
Washington, D.
SEMICONDUCTORS (SUPPLEMENT TO CTR-340).
Sep 60, 20p. 314ref8. OTS Selective Bibliography 435
Order from OTS io. 10 OTS SB-435
A bibliography of (reports listed in the two OTS monthly
aiMtract journals-^ U. S. Government Research Reports
and Technical Translations. This bibliography covers
PB reports, AEC i-eports, and translations on Semi-
conductors added ko the OTS collection during the
period April 1950,to October 1960.
Oregon State Co|l. , Corvallis.
DECREASE OF I^ CENTER PHOTOCXDNDUCTTVITY
UPON BLEACHIN<;, by Fred C. Hardtke. Allen B.
Scott, and Robert E. Woodley. Technical rept. no. 3
00 Magnetic Study of Color Centers in Alkali Halides,
Contraa Nonr- 1246(05). 10 Feb 60, 18p. 10 refs.
AD-232 897.
Order from LC nn|$2. 40, ph$3. 30 PB 153 143
A quantitative study of the rapid decrease in photo-
conductivity accorfipanying the relatively less rapid
bleaching of F ceiters in additively colored KCl is
reported. The exj^rimental observations agree, ex-
cept during very eierly stages of bleaching, with an
equation for the variation of sensitivity with total light
absorbed derived upon the assumption that negative -
ion vacancies are Icreated and traps of smaller cross
section are filled during bleaching. Except during
early stages, where several kinds of traps may be
present in low concentration, only one kind of trap
other than the negative -ion vacancy need be con-
sidered. The effects d added divalent ions, both
positive and negative, upon photoconductivity are re-
ported. (Author)
[Pennsylvania State U. Coll. of Mineral Industries,
University Park].
INFLUENCE OF ASYMMETRICAL FORCE FIELDS
Oti SOME OPnCAL, CHEMICAL, MECHANICAL
AND ELECTRICAL PROPERTIES, by W A. Weyl wA
D. P. Enright. O.NR. Technical rept. nos. 3-7 on
Contract N6onr- 269, TO. 8. June 49, 153p. 77 refs.
ATI- 179 543.
Order from LC mi$7.50, ph$24. 30 PB 154 2W
This report released for sale to the public 17 Feb 61.
Contents:
Influence of surface ions on the rate of inversion of
mercuric iodide, by W. A. Weyl and D. P. Enright
(TR-3)
On the surface structure and surface properties of
crystals and glasses, by W. A. Weyl (TR-4)
Discussion of flow and rupture erf cubic crystals front
an atomic point of view, by W. A. Weyl (TR-5)
Decomposition of complex anions in asymmetrical
force fields (derivation of a theory of detonators) by
W. A. Weyl(TR-6)
Dielectric properties of glass and their structural
interpretation, by W. A. Weyl (TR-7)
Polytechnic Inst, of Brooklyn, N. Y
THE CATALYTIC ACTIVITY OF SODIUM TUNG-
STEN BRONZES, by E. M. Loebl and F. T Jones.
Technical rept. no. 1 on Research on Catalytic Prop-
erties of Semiconductors, Contract htonr- 839(24).
15 Feb 60, 119p. 56 refs. AD-234 112.
Order from LC mi$6. 00, ph$18. 30 PB 153 147
The catalysis by sodium tungsten bronzes with the gen-
eral formula Na^WOs, where x varied from 0. 30 to
0. 98 of the onho-parahydrogen conversion and the
H-deuterium (D) exchange, was investigated from 77®
to 470^ at pressures from 10 to 40 mm Hg.
Uppsala U. (Sweden).
THE CRYSTAL STRUCTURE OF SbCl5 P0(CH)3, by
Carl-Ivar Br^nden and Ingvar Lindqvist. Technical
note no. 12 on Contract AF 61(052)43. 15 Sep 60, 15p.
20 refs. AFOSR-TN-60-930.
Order from LC mi$2. 40, ph$3. 30 PB 153 310
The crystal structure of SbCl5 PO(CH3)3 has been de-
termined and refined from three-dimensional X-ray
dau. The compound is isomorphous with SbCls POClj.
The Sb - O and P - O bond lengths are 1 . 99 1 0. 02 A
and 1. 61 1 0. 02 A respectively. The Sb - O - P bond
angle is 13990 1 294. Ck>mparison8 are made with the
structures of PO(CH3)3 and SbC\^ POCI3. The predic-
tions of the bond length variations in these compounds
based on the theoiy for inductive effects on polar bonds
has been confirmed. The nature of the P - O bond is
briefly discussed. (Author)
Theoretical Physics
Advanced Kinetics, Inc. (Santa Ana, Calif. ]
STUDY OF CONDITIONS IN H1(3H TEMPERATURE
NON -EQUILIBRIUM PLASMA CONFIGURATIONS, by
Ralph W. Wanlek. Scientific rept. no. 1 (Quarterly)
15 June- 15 Sep 60, on Contract AF 19(604)7363. [\9tf^
8p. AFCRL-TN-60-991.
Order from LCnu) 1.80, ph$ 1.80 PB 153 426
472
A study was undertaken to calculate the radiative pa-
rameters of optically thin, high temperature plasmas.
Particular attention is devpted to the Bremsstrahlung
radiation obtainable during encounters of the stripped
electrons with the ions. The energy radiated at vari-
ous temperatures and for given particle densities was
computed for several wavelengths. A study was con-
ducted on the possibility of measuring the energy of a
plasma by stimultaneous determination of the radiant
flux at three different wavelengths. The results of
these calculations have been used to estimate the sig-
1^ detectable in a vacuum ultraviolet spectrograph
vhen aimed at a radiating plasma source. Theoretical
calculations have been conducted on high -field cusp
geometries to be used for plasma containment.
(Author)
Brown U. Div. of Applied Mathematics, Providence,
R. I.
MAGNETOHYDRODYNAMICS OF CONDUCTING
FLUIDS, by G. S. S. Ludford. Scientific rept. no. 2
on Contraa AF 19(604)7236. Oct 60, 31p. 38 refs.
AFCRL-TN-60-800; AD-246 224.
Order from LC mi$3. 00, ph$6. 30 PB 153 074
A critical review is presented of magnetohydrodynamic
flow of conduaing fluids past bodies. Most of the work
Is of very recent origin and some still awaits publica-
tion. The discussion is divided into three parts corre-
sponding to small, large, and general conductivity.
(Author)
Forschungsinstitut fUr Physik der Strahlantrlebe
e. v., Stuttgart (West Germany).
IRREVERSIBLE STOCHASTIC THERMODYNAMICS
AND THE TRANSPORT PHENOMENA IN A REACT-
ING PLASMA , by H . J . Kaeppeler and G . Baumann .
Final rept. on Contract AF 61(514)939. Nov 56, 97p.
123 refs . AFOSR-TR- 57-20; AD- 120 462.
OrderfromLC mi$5.40, ph$15.30 PB 150 688
The investigations presented in this report are a first
venture in attempting a theory of transpon phenomena
in a reacting plasma at elevated and high temperatures
As an essential basis for such studies, the equilibrium
behavior of a plasma is treated. These equilibrium
considerations concern the influence of electrostatic
microfields on plasma properties, termination of the .
electronic partition function, and determination of the
plasma composition. Entering into the problem of en-
ergy transport, the classical diffusion theory of trans-
port is discussed. Then, an attempt is made at estab-
lishing the rudiments of a stochastic description of
plasma physics, the thermodynamics of transport phe-
nomena in particular. It is shown that the theory in-
cludes the purely statistical methods . For the calcula-
tion of intenul energy transport, the formal kinetic
theory due to Wang-Chang and Uhlenbeck is extended
«nd approximate methods for integration of the colli-
sion Integrals are derived. Finally the energy trans-
port in the presence of chemical reactions is treated.
(Author)
Microwave Lab. , Stanford U . , Calif.
INVESTIGATION OF MICROWAVE PROPERTIES OF
PLASMAS, byM. Chodorow. Scienfific rept. no. 9,
1 May-31 July 60, on Contract AF 19(604)5226. Aug 6ft
22p. M. L. rept. no. 747; AFCRL TN-60-998;
AD-246 643.
Order from LC m42.70, ph$4.80 PB 153 098
Contents :
Plasma research: thermal plasmas; noise in plasmas;
harnwnic generation in plasmas; cesium plasma tube
materials and techniques
Other plasma studies: electron beam interaction with
a plasma; plasma parametric amplifier; plasma di-
agnostic techniques; plasma confinement
(See also PB 150 376)
Parke Mathematical Labs. , Inc., Carlisle, Mass
DIFFERENTL\L GEOMETRY AND LAGRANGIAN
METHODS IN QUANTUM MECHANICS, by Nathan
Grier Parke III. Scientific rept. no. 2 on Contraa
AF 19(604)7316. Oa 60, 42p. 47 refs. AFCRL-TN-
60-1131.
Order from LC mi$3.30, ph$7.80 PB 153 728
Contents:
Geometry and quantum mechanics
Finsler space and classical aaion
The Lagrangian and spin
Finsler geometry and the calculus of variations
The notion of a tangent space and a metric
The dual tangent space and the Hamiltonian funaion
The harmonic oscillator as a Finsler space-time
manifold. "^
Physical Research Lab. , Space Tech. Labs. , Inc. ,
Los Angeles, Calif. ->,
PLASMA OSQLLATIONS, by J. D. Jackson. Rept. on
Thermonuclear Propulsion Research, Contraa
AF 04(647)165. 3 Dec 58, 59p. 15 refs. (a4-TR-
0165-00535; AD-ai7 521.
Order from LC ini$3.60, ph$9.30 PB 154 404
This report released for sale to the public 15 Feb 61 .
A coherent account is preseiced of various aspeas of
plasma oscillations. A discussion is offered of disper-
sion equations, conditions necessary for the growth or
decay of oscillations, the physical mechanism of grow-
ing or damping, and the possibility of arbitrary steady
state solutions. The mathematical description is in
terms of solutions of an initial value problem in small
amplitude (linearized) approximations. Some general
results are derived for an arbitrary unperturbed ve-
locity distribution of elearons and ions. From these
expressions the customary results for a stationary
plasma in thermal equiUbrium can readily be obtained.
For simplicity, one dimensional motion of a simple
one component plasma Is assumed; collisions between
particles and nonlinear effeas are not considered.
Appropriate generalizations for two compxinent
plasmas (elearons and ions), however, are indicated
in text. (Author)
^•k;u«:
473
Ttechnlsche Hocischule, Stuttgart (West Germany).
SHOCK WAVES IN PARTLY AND FULLY IONIZED
PLASMAS WITH ^ARTICULAR CONSIDERATION OF
THE DETERMINATION OF MEAN EFFECTIVE
TEMPERATURES DM PLASMAS USING SHOCK WAVE
MEASUREMENTS, by a J. Kaeppeler, a Mayser.
and K. H. Hocket'. Interim rept. (Theoretical part)
for I Jan-31 Dec $9 on Contract AF 61(052)199. Jan
60, 146p. 94 refa. AD- 235 860.
Order from LC rril|7. 20, ph$22. 80 PB 153 466
Theoretical Investigations are presented which consti-
tute a first venture in attempting a general description
of shock wave phenomena in plasmas and their appli-
cations. Fundamental questions such as a statistical
basil for transpo^ equations and conservation laws,
limits for descripltion of plasma behavior by macro-
scopic observablas, and the transport equations and
conservation laws themselves are discussed. The
Rankine-Hugoniot, relations for normal shocks in
plasmas with external magnetic field in the one-fluid
and approximate cwo-fluid formalism are derived.
Shocks in chemic4lly reacting plasmas and in plasmas
with radiative emission only are also treated. The
application is witl^ respect to plasma shock tubes and
the determination of mean effective temperatures in
plasmas using sh0ck wave measurements. (Author)
Th »rmod)rnamics
Air Force Missile Development Center, Holloman
AFB, N. Mex. {
THE EFFECT OF VARIOUS CONSTRUCTIONAL
ERRORS ON THE EFFICIENCY OF A SOLAR
ENERGY COLLECTOR COMPOSED OF SPHERICAL
MIRRORS, by Alfred W. Simon (California State
Polytechnic Coll. )i Nov 60, I4p. AFMDC TN-60-13.
Order from LC mi$2.40. ph$3.30 PB 153 465
It has been propoeed that the condenser of a large
solar energy collector be constructed of a series of
concentric rings of mirrors of approximately square
shape and spherical section, arranged on the surface
at a geometric pa4aboloid. In connection with the con-
strixrtlon of such i collector, the question arises as
to the effect of various constructional errors on the
efficiency of light concentration of the mirrors.
These errors are those of a misalignment of the
mirrors, a mlsfo^using of the ndrrors, and an error
in the radius of a*-vature of the mirrors. The effects
of these errors are investigated. It is found that in
practice the magnitudes al these errors are such that
their effects can tie neglected. (Author)
llrfc
Defense Metals Ifaformation Center, Battelle
Memorial Inst., Columbus, Ohio.
METHODS OF MEASURING EMITTANCE, by W. D.
Wood, H. W. Deem and C. F. Lucks. [Rept. on Con -
traa AF 18(600)1 3175] 27 Dec 60, 22p. 30 refs. DMIC
memo. 78. ,
Order from OTS H 50 PB 161 228
The present memok-andum covers some of the methods
and equipment use^l in emittance measurements. Since
the literature Incltides many types and variations c4
measurement methods and equipment, only a general
survey of some of the better-known methods is in-
cluded. References are listed for those who desire
more detailed information on specific methods or
equipment. (Author) (See also PB 161 222)
[Institute of Engineering Research] U. of California,
Berkeley.
THERMAL RADIATION PROJECT, by J. T. Gier.
Rept. no. 3 for year ending 1 June 48 on Contract
N7[onrl 295(01). 8 June 48, 18p. ATI-210 349.
Order from LC ml$2. 40. ph$3. 30 PB 154 293
Tliis report released for sale to the public 14 Feb 61.
Completed work is summarized on total normal low
temperature emissivities, development of the uni-
directional heat flow sundard, and the effect of am-
bient temperature and pressure on thermopile radiom-
eters. In addition, extensive work is summarized on
ideal radiators, an optical amplifier, a reflectometer,
a total hemispherical radiometer, constants used in
radiation work, and a double-barreled radiometer.
(See also PB 137 126)
Naval Supersonic Lab. , Mass. Inst, of Tech.,
Cambridge .
THE COMPRESSIBLE TURBULENT BOUNDARY
LAYER WITH SURFACE MASS TRANSFER, by
F. E. C. Culick. Rept. on Contract A F 49(638)245.
Aug 60, 67p. 13 refs. Technical rept. 454; AFOSR-
TN-60-1094.
Order from LC mi$3.90, ph$l0.80 PB 153 106
An approximate analysis of the compressible turbulent
bouiKlary layer on a porous flat plate with distributed
surface mass transfer is based on a representation
comprising two regions. A large pcn'tion of the devel-
opment is quite general, but only the cases of helium
and air injection are computed explicitly. The results
are restricted to conditions under which the Prandtl
and Schmidt numbers may be regarded as functions of
concentration alone. Wall concentration of helium and
the reduction in skin friction can be calculated from •
modified integral method; heat transfer and recovery
temperatures are obtained from the differential
energy equation. There seems to be acceptable agree-
ment with measurements, with the exception of
optimistic recovery factors and a failure to show ob-
served dependence of skin friction on Mach number.
An approximate calculation indicates that if the effecu
of thermal diffusion are accounted for, the first error
may be decreased, with but small change in the cal-
culated heat transfer rate. (Author)
Non -Metallic Materials Lab. , Wright Air Develop-
ment Div. , Wright -Patterson AFB, Ohio.
THE EFFECT OF GRAVITY ON FREE CONVECTION
HEAT TRANSFER. PART 1. THE FEASIBILITY OF
USING AN ELECTROMAGNETIC BODY FORCE, by
David A. Kirk. Rept. for Apr 59-Jan 60 on Power
Transmission Technology. Aug 60, 52p. 29 refs.
WADD Technical rept. 60-303, Part 1.
Order from OTS $1. 50 PB 171 395
474
Theories concerning the instability and motion of a
fluid heated from below predicts the effect of various
physical parameters. Experimental investigations
hive succeeded in widely varying all parameters, ex -
cept gravity, in order to determine the validity of the
theories. In extra-terrestrial heat transfer applica-
dooa. such as in free convection, boiling, and conden-
■ation, the effect of gravity should be verified by ex-
periment. This report considers the feasibility of
usii^ an impressed electromagnetic body force acting
parallel to the earth's gravitational field. The result.-
ant of this electromagnetic force is said to be an
"equivalent gravitational" force acting on the fluid
mtM. Based on the analysis made, a series of experi
meats can be performed to ascertain the quantitative
contribution of gravity, over the range from -13. 6 to
15. 6 times ground level gravity, on free convection
heat transfer. An apparatus is presently being fabri-
cated to conduct an experiment for the case when heat
is applied from below. (Author)
Pennsylvania U. , Philadelphia. «
DIELECTRIC BREAKDOWN OF LIQUID HELRJM, by
C Blank and M. H. Edwards (Royal Military Coll. ).
Technical rept. no. 4 on Contract Nonr-551(28). [i960)
16p. 9 refs. AD-232 657.
Order from LC mi$2. 40, ph$3. 30 PB 153 166
The dielectric strength of liquid He* under its satu-
rated vapor pressure has been determined from 1. 2 to
4. 2°K. With 3/8 inch diameter spherical steel elec^
titxies 0. 15 mm apart the average breakdown field, E^,
is approximately 1 MV/cm, nearly independent of tem-
perature. At spacings of 0. 5 and 1 mm. Eb is lower,
and appears to decrease with decreasing temperature
below 2. 5°K. The mechanism of breakdown is not
clear, but field emission of electrons from the cathode
is probably involved, because the average breakdown
voltage 7^, obtained with a point and plane electrode
system when the point is negative, is about half that
obtained when the point is positive, both above and be -
tow the A -point. Pre -breakdown currents were never
detected, and were probably less than lO'^^ imp. im
plying an electrical resistivity for liquid helium of
lff**8 ohm-cm. (Author) /
Stanford U. , Calif.
CONVECTION HEAT TRANSFER COEFFICIENTS
IN DE LAVAL NOZZLES, by R. K. Pefley. Techni-
cal rept. no. HS-3 on Contract N6-onr-251, T. O. 6.
1 Oct 51, 50p. 17 refs. ATI -153 158.
Order from LC mi$3. 30. ph$7. 80 PB 154 294
This report released for sale to the public 10 Feb 61.
The objectives of this program are to determine the
local convection heat transfer coefficients in the con-
vergent ponion and throat sections of de Laval noz-
zles; and to determine the effect on the local heat
transfer coefficients, particularly at the throat, of
varying the contour in the converging section of the
Mczk. Three two-dimensional nozzles with pressure
gradients and resulting cross -sectional areas have
been tested. Heat transfer coefficients have been ob-
tained for both the flat and contoured walls.
Wave PropogaHon
Army Signal Research and Development Lab. , Fort
Monmouth. N. J.
MICROWAVE PROPAGATION CHARACTERISTICS IN
GERMANIUM, by Harold Jacobs. 10 Nov 59, 2Ip.
4 refs. USASRDL Technical rept. 2087; AD- 233 243.
Order from GTS $0.75 PB 171 377
With the increased interest in the use of semiconduc-
tors in microwave devices, the various propagation
characteristics ot germanium may be of assistance to
the design engineer concerned with this area. The
microwave propagatitxi constants in germanium have
been tabulated and are presented as a function of fre-
quency and conductivity. These calculations are based
on classical theory and do not necessarily apply to
quantum mechanical effects such as those that occur in
cyclotron resonance or in "negative mass" experi-
ments. Data are presented as a summary of proper-
ties of microwaves in germanium with resistivities
varying between 2 and 10^ (ohm meters)" ^ . (Author)
Brown U. Div. of Applied Mathematics, Providence,
R. I.
A UNE SOURCE ON AN INTERFACE BETWEEN A
FLUID AND AN ELASTIC SOLID, by V. M. Papado-
poulos. Technical rept. no. 56 on Contracts Nonr-
562(10) and 562(24). Apr 60, 39p. 24 refs. Cll-56;
AD-236 727.
Order from LC mi$3.00, ph$6. 30 PB 147 400
The problem of interaaion between infinitesimal dis-
turbances propagated in a fluid and in an elastic solid
across an infinite plane interface is examined by the
method dynamic similarity. The disturbance is the
result of the setting up, at time t =o, of an infinite
line source of constant strength on the interface; by
the word source it is implied that within the fluid a line
singularity is associated with a flux which is uniform
in all directions aitd with zero circulation. Seen from
the solid the singularity is a line of pressure which is
not, however, uniform in all directions. Within the
limitations of the theory of propagation of weak shocks
the method of dynamic similarity, which is closely
related to the conical flow methcxl of Busemann leads
to exact formulae for the stress and velocity compo-
nents everywhere; these results satisfy the correct
continuity conditions at the interface. The non- uniform
way in which the solilion approaches the COTrespond-
ing elastic half-space solution when the density of the
fluid is small relative to that of the solid is described,
and the non- uniform way in which the surface wave
velocity is affected by the relative density is also
discussed. (Author)
General Electric Research Lab. [Schenectady, N. Y. 1
TROPOSPHERIC SCATTER PROPAGATION STUDY, by
Leonard G. Abraham, Jr. and John A. Bradshaw. Final
rept. on Contract AF 19(604)1723. Oct 59, 137p. 50 refs
AFCRC TR-59-353; AD-232 924.
Order from LC mi $6. 90, ph$2 1.30 ffl 150 718
475
Cent ems:
Long-term slgna) magnitude observations and basic in-
strumentation
Time lapsed picture and midpoint observation
Correlation <rf mieteorological parameters with hourly
median values qi Che received slgiud
Fading spectra '
The distribution of signal amplitude over short records
Airplane doppler patterns
Effective bandwidth experiments
Minor and incomplete programs
Plans for space (vverslty experiments
Appendices:
Correlation stu(lles. orthogonality, and numerical
results '
Derivacion d formulae
Statistical nature ol'^opospheric scattering
Marginal probc^illty distribution for 2 received signal
1
of Pli^
Structurea, Columbia U. ,
Institute
New York.
SURFACE WAVBS IN A VISCOELASTIC HALF-
SPACE, by Jacob Lubliner. Technical rept. no. 9 on
Contract Nonr- 266(34) and Technical rept. no. 24 on
Contract Nonr-2^08). Apr 60. 26p. 15 refs. CU-1-
60-ONR 266(34)OE; aJ-l-60-ONR 266(08)CE:
AD-238 997.
Orxler from LC ii)i$2. 70, ph$4. 80 PB 148 525
The response of k viscoelastic half -space to a suddenly
applied concentrated normal force at its surface is ex-
pressed in terma of double complex integrals. The
a«rface-wave reiponse is then reduced to a single in-
tegral in the coniplex frequency plane, and this inte-
gral is shown to be approximately expressible inclosed
form, provided the major contribution comes from a
high-frequency r^ion. The limits of the domain (in
space-time) in which the high-frequency phase pre-
dominates are found by analyzing saddle points of the
integrand. (Authf>r)
ihbi
Institute of Mat^nnatical Sciences, New York U. ,
N. Y.
AN EQUATION I^OR THE FIELD AMPLITUDE IN
GEOMETRICAL OPTICS, by Irvin Kay. Rept. on
Contraa AP 19(604)3495. Aug 60, 24p. 4 refs. Re-
search rept. no. EM-161; AFCRL-TN-60-967.
Order from LC 4i)2.70, phS4.80 PB 152 781
The geometrical pptics approximation of solutions of
the two dlmensioiial wave equation for an isotropic
inbomogeneous niedium is considered. An ordinary
differential equation for a quantity which is inversely
proportional to the geometrical optics field intensity
(the square of tha field amplitude) is derived. This
new equation aloqg with the standard ray and phase
equations form a system from which a complete wave
solution in the optical limit can be calculated numeri -
cally, e.g., by nieans of an analog computer acting as
a differential analyzer. The examples oif a homogene-
ous medium and a medium whose index of refraction is
a function of cxi« variable are discussed, and the re-
sults of the precefling analysis are verified in these
two special cases. (AiHhor)
Michigan U. Coll. of Engineering, Ann Arbor.
STUDIES IN RADAR CROSS SECTIONS XU. PRES-
SURE PULSE RECEIVED DUE TO AN EXPLOSION
IN THE ATMOSPHERE AT AN ARBITRARY ALTI-
TUDE. PART I, by V. H. Weston. Rept. on Contraa
AF 19(604)5470. Aug 60, 62p. 15 refs. Rept.
no. 2886-1-T; AFCRL-TN-60-649.
Order from LC ml$3.90, ph$10.80 P3 152 83S
This report is mainly concerned with the grbvity wave,
produced by explosions not only on the ground, but m
various heights in the atmosphere. At present the
effect of winds is ignored, but will be considered laiar.
They do have an influence upon the pressure pulse, §]•
thoi.^ the high-frequency acoustical portion is af-
fected the most. It is shown that for certain tempera-
ture models of the atmosphere a good approximation
can be made to the "gravity" wave mode. This ap-
proximation gives good results for Scorer's model of
the atmosphere. The pressure pulse for the directly
received wave (as contrasted to the antipodal wave) It
computed for various ranges, for two models of the
atmosphere. In doing so, a simple source model is .
taken, namely a point source ^n space with a delta
function dependence in time. The intensity of the ex-
plosion is given in terms of volume of gas introduced.
In the calculation of the pressure pulse at various
ranges from the source, emphasis is placed upon the
main body of the gravity wave portion. In calculating
the head of the pulse a new asymptotic technique is
introduced which gives very good results, for Inter-
mediate and long ranges.
RESEARCH METHODS, TECHNIQUES
AND EQUIPMENT
Electrical Engineering Research Lab. , U. of
Illinois, Urbana.
REORGANIZATION BY ADAFHVE AUTOMATION, bji
Murray Lewis Babcock. Thesis. Technical rept. na I
on Contract Nonr- 1834(21). 15 Jan 60, 148p. 40 refs.
AD- 233 187
Order from LC mi$7. 20, ph$22. 80 PB 152 876
Using the present limited knowledge of nervous tissue
of living organisms as a guide, an attempt is made to
construct an adaptive automaton whose internal struc-
ture has a similarity to living nervous tissue. Accept-
ing the general contention that living organisms have
qualities which show adaptation and self-organization
as illustrated by evolution and the individual organ-
ism's ability to self- reproduce, the existence of theee
organisms is taken as a proof that adaptive system!
are possible. Thus, the philosophy and operation oft
general biological computer is described, the internal
components of this computer having functional opera-
tion very similar to that of a biolo;;ical neuron- -a
basic component in nervous tissue. After describing
this general automaton, complete functional specifica-
tions of the individual elementary components are
ideally established. Using these specifications of so-
called artificial neurons, an attempt to reduce the
automaton to practice by the use of electronic tech-
niques Is made. In this reduction the elementary com-
ponents are considered as highly versatile informatioe
processors, the result being an electronic model of ta
476
irformation system having some of the structural and
functional characteristics of nervous tissue. Several
of these electronic elementary components were con-
gffucted. Experimental tests on these components
essentially corroborate the similarity desired between
;bein and the biological neurons. (Author)
Human Sciences Research, Inc., Arlington , Va.
SYNTHESIS AND COMPARISON OF SYSTEM RE-
SEARCH METHODS: REPORT OF PHASE II. by
I E McGrath and P. G. Nordlie. Rept. no. 9 on
Contract Nonr -2525(00). Feb 60, 147p. 477 refs.
HSR-RR-60/l-sm; AD- 234 463.
Order from LC mi$7.20, ph$22.80 PB 153 129
(kntents:
Key problems of system research methodology
Stages of the system research process
The requirement- setting suge
The design guidance stage
The system development stage
The system evaluation stage
A tactical framework for weapon system studies
An approach to a descriptive theory of combat
The combat fundamentals
Mission
System capabilities
Tactics: application of system capabilities
Methodological functions of a descriptive theory of
combat
Methods for systematic projections
Some requirements for a projection methodology
An approach to a method of projection
Translation of requirements mto design guides
Theory of allocation of functions to man and machines
Theory of method for system evaluation
Institute for Applied Experimental Psychology,
Tufts U , Medford, Mass
A SURVEY OF OPERATIONS AND SYSTEMS RE-
SEARCH LITERATURE, by Margaret W. Raben.
Rept. on Contraa Nonr-494(13). 1 Jan 60, 125p.
1,021 refs. AD- 233 505.
Order from LC mi$6. 30, ph$19. 80 PB 152 914
Ckmtents:
Capacities of man and machine: comparison of man
and machine; automation
Methods of experimenul and engineering psychology:
general experimental method; engineering psychology;
cybernetics; methods for studying group processes
Operations and systems research methods in general
Communication and information theory: the human link
in communications systems
Game or decision theory and Unear programming
Computers and simulation
(^ueoeing theory and work measurement techniques
Mui as a system component
Groups as system components: groups structure and
task; interpersonal factors
Communication problems
Transportation problems: weapon systems - aircrafl
tod missiles; ground transportation systems; ocean
transportation systems
Air traffic control
Production, maintenance and su;^ly problems
National Research Labs. , Ottawa (Canada).
NON-AERONAUTICAL APPLICATIONS OF LOW-
SPEED WIND TUNNEL TECHNIQUES, by P. J. Pocock
Sep 60, 131p. 385 refs. Mechanical Engineering
rept. MA-243.
Order from LCmi$6.90, ph$21.30 PB 153 633
Low-speed wind tunnel techniques have been used in
the study of many non-aeronautical problems. This
report describes some of the work that has been done
along these lines. Wherever possible, reports of
experimental work are cited, and among the 385 ref-
erences are several describing the wider implications
of the various problem areas. (Author)
Office of Ordnance Research, Durham, N. C.
PRCXEEDINGS OF THE CONFERENCE [NO. 5] ON
THE ENSIGN OF EXPERIMENTS IN ARMY RE-
SEARCH DEVELOPMENT AND TESTING, SPONSORED
BY THE ARMY MATHEMATICS STEERING COM-
MITTEE CONDUCTED AT THE U.S. ARMY BIO-
LOGICAL WARFARE LABORATORIES, FORT
DETRICK, FREDERICK, MARYLAND, 4-6 NOVEM-
BER 1959. Oct 60, 380p. 160 refs. Rept. no. 60-2.
Order from LCmi$ 11.10, ph$57. 60 PB 152 927
Contents: The method of paired comparisons; Measure
of competing exponential mortality risks with especial
reference to the study of smoking and lung cancer;
Army research and development; Prediction of the re-
liability of complex systems; On the repeated -meas-
urements design in biological experiments; Design of
experiments using germfree animals; The development
of parameters for determining the resistance of se-
lected missile components to microbiological deterio-
ration; Design of environmental experiments for relia-
bility prediction; Multidimensional staircase designs
for reliability studies; A proposed research program
for providing a quantitative basis for preventive
maintenance ];x>licies on ordnance equipment; Statistical
analysis of various parameters erf burning charaaer-
istics of flare systems; A statistical evaluation of the
pyrotechnic electrosutis sensitivity tester; Dispersion
strengthening analjrsis of cermets; Experimental de-
termination of "best" component levels in thermal
power supplies; Medical health statistics; Sampling in
biological populations; The application of fractional
factorials in missile test programs; The design and re-
design of an experiment; Estimating the parameters of
a modified poisson distribution; Detecting and quanti-
fying guess responses in the rating of swtements by a
method of successive intervals; Design for estimation
by covariance techniques; Design c< an experiment to
evaluate a bio-assay with non-parallel slopes; The ORO
aircraft vulnerability experiment; Operational hit prob-
abilities of experimental antitank weapons; Elimination
of bias introduced by transformation of variables;
Mathematical and ststistical principles underlying
chemical corps inspection procedures for product
verification; Measuring a complex field operation; The
conduct of military field research on a shoe-wring;
Sample order statistics of the circular normal distribu-
tion; Determination of systematic errors in tracking
radar. (See also PB 143 833)
477
Ohio State U. Research Foundation, Columbus.
VOWEL DISCRIX|INATIC»J AMONG FOREIGN
NATIONALS, by Henry M. Moser, Herbert J. Oyer and
others. Technlc41 rept. no. 57 on Contract
AF 19(604)4575. ,Sep 60, 26p. 5 refs. [AFCCDDj TN-
60-».
Order trom LC n d$2. 70, ph$4. 80 FB 153 430
This study is concerned with the ability of foreign
nationals to discriminate between English vowels. The
foreign national must not only learn English sounds
which are not in kls language, but also to differentiate
between those English speech sounds which are similar
to sounds in his native language. However, knowledge
of the importanca of discriminative learning, or the
difficulties faced in learning a new language, does not
afford specific information about the discrimination
ability of foreign jnatlooals when learning English. . It
was felt that a study of vowel discrimination would re-
veal information which might facilitate the foreign
nationals' comprehension of Che English language.
(Author)
Syracuse U. , N( Y.
A NOTE ON THE ERGOMC THEOREM OF INFOR-
MATION THEORY, by K. L. Chung. Research rept.
no. 31 on Contract AF 49(638)265. Oct 60, 5p. 4 refs.
AFOSR-TN-60-1^45; AD- 247 243.
Order from LC r#iW. 80, ph$l. 80 PB 153 360
■J.
The purpose o^ tqis note is to extend the result of
Breiman to an infinite alphabet, or equivalently, the
result at Carlesop to convergence with probability one.
(Author)
Phdrographic Equipment
I
Fll^t Accessoifies Lab. , Wright Air Development
Div. , Wright - Fitter son AFB, Ohio.
THE CHANGE IN APPARENT IMAGE SIZE CAUSED
BY MOTION DURING PHOTOGRAPHIC EXPOSURE,
by L. V. Larson. Rept. on Windshield Jet Air Blast
Rain Removal. May 60, 18p. 4 refs. WAOD Technical
note 60-26; AD-2#6 653.
Order from OTS %Q. 50 PB 171 385
r
A photograph of a moving object is always blurred to
some extent. If the size of the object is measured from
the photograph, tjils blurring changes the apparent size
The case treated is an object viewed in silhouette. The'
gradation in light quantity striking the areas panially
shaded by the moving edges of the object is derived for
flash tube and shatter controlled exposure. With the
aid at photographic film characteristics, the resulting
Image is reconstructed and the apparent change in size
determined. Change in size is found to be a function of
film contrast and ratio of object nKJvement during ex-
posure to object Jength in direction of motion. The
effects ot diffraction and imperfect focus are con-
sidered. In the general case an interaction between
the various causes of blurring is found. In the more
practical case of small errors due to focus and dif-
fraction, and small movement during exposure, the
interaction is negligible and the error due to nnove-
ment is directly (proportional to the anKxint of move-
ment. (Author) ^yg
Observatoire de Haute-Paris (France).
THE ELECTRONIC CAMERA, by Andre Lallemaad.
Nov 60, 21p. 14 refs. ARL Technical rept. 60-324.
Order from LC ml$2. 70. ph$4. 80 PB 152 581
It is possible to detect as little as one single photo-
electron with the improved modern electronic camen
which was basically conceived and first demonstratsd
by Professor A. Lallemand in 1936 and further devel-
oped since 1953 by him and his associates at the Lab-
oratoire de Riysique Astronomique of the Paris Ob-
servatory. This electronic camera is of utmost im-
portance for astronomical work especially for ob-
taining spectroscopic recordings, because the ex-
posure time necessary for conventional photography
may be rechiced with this device by a factor of more
Chan 100. With it the speara of distant nebula have
been recorded using an exposure time of two minutes
and resulting in a better quality than can be obtained
with the conventional methods in 10 hours 37 min of
the same object by employing the same telescope.
The electronic camera can be used wich a grain count-
ing device also for nuclear research work and a gain
of 10, 000 with respect to conventional photography is
possible. (Author)
SOCIAL SCIENCES
Alaska U. , College.
PRELIMINARY REPORT ON AIR FORCE - ESKIMO
OWTACTS, by W. a Oswalt. Dec 56, 14p. Techni-
cal note AAL-TN-56-14.
Order from LC mi $2. 40, ph$3. 30 PB 153 520
This report concerns the techniques for establishing
successful working relationships between Armed
Forces personnel and the Eskimos of isolated villages
in western Alaska. The assumption is that the Armed
Forces require satisfactory face-to-face relationships
with Eskimos, and that the Armed Forces desire to
minimize any disorganizing effects that their preseact
may have in a village.
Alaska U. , College.
REPORT ON AIR FORCE - ESKIMO CONTACTS, by
James W. VanStone. Dec 56, 30p. Technical note
AAL-TN-56-15.
Order from LC ml $2. 70, ph$4. 80 PB 153 521
The purpose of this report is to discuss some of the
problems that may arise when groups of military
personnel, or white civilians under contract to the
military, take up residence In or near an Eskimo
village for varying lengths of time. Tlje suggestions
made here will aim toward achieving maximum co-
operation between the two groups and a minimum of
friction due to misunderstandings on the cultural level
(See also PB 153 520)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
OBSERVATIONS ON THE CONTEMPORARY ESKIMO
OF WAINWRIGHT, ALASKA, by Frederick Milan.
Jan 58, 80p. 37 refs. Technical rept. 57-14.
Order froinLCmi$4.50. ph$l2.30 PB 153 367
A group of contemporary Alaskan Eskimos, the
■jjfi^qikamiut. living in the arctic coastal village of
Wainwright was studied during the summer of 1951.
Despite the introduction of a money economy and an
annitti village income of about $65, 000, the cycling
leason still determine the annual rodnd of exploitative
ictivltieB and there is a definite preference for native
type foods. Cooperative hunting and sharing of the
catch continues. The people are bilingual, speaking
Ijoth iNNupiaq, or Eskimo, and English. The religious
beliefs of the uluRunikamiut are based upon somewhat
modified Christian teachings of the Presbyteriarf
Church and a residuum-of aboriginal practices.
(Author)
Harpur Coll. , State U of New York (Endicott, N. Y.]
A COMPARATIVE STUDY OF OFFSHORE CLAIMS
IN NORTHWESTERN EUROPE, by Lewis M. Alexander
Pinal rept. on Contract Nonr- 1349(03). Feb 60, 248p.
193 refs.
Order from LC mijll. 10, ph$37. 80 PB 153 121
Seven of the nine northwestern European countries con-
sidered have territorial belts 3 miles in breadth, while
Norway and Iceland claim 4 miles. Three international
borders in offshore areas are in dispute: (1) the
DoUan-Ems area between the Netherlands and West
Germany; (2) the channel of the West Schelt between
the Netherlands and Belgium; and (3) the seaward ex-
tensions of the border between Ireland and Northern
Ireland. The waters of Iceland, northern Norway, and
the Faroe Islands are important as fishing areas, and
it is here that the problems of local vs. foreign fisher-
men are particularly acute. There is uncertainty over
future attempts at a world conference to achieve a uni-
versal breadth for the territorial sea and rules for the
delimitation of baselines in the case of island groups
and archipelagos. (See also PB 148 580)
hstitute for Quantitative Research in Economics
and Management, Purdue U. , Lafayette, Ind.
THE CAPITAL STRUCTURE OF FIRMS AND THE
RISK OF FAILURE, by James P. Quirk. Rept. on
(iotract Nonr- 1100(16). Feb 60, 27p. 4 refs. Insti-
tate Paper no. 2; AD-233 687.
Order from LC mi$2. 70, phK 80 PB 153 148
An Investigation is presented of the effects of default
risk on the portfolio policies of lenders and the capi-
ul structure of firms under conditions of perfect
competition and constant returns to scale, interpreted
in a stochastic sense. A simplified model of the
process by which firms obtain financing is developed,
employing the assumptions of the complete infor-
mation-measurable utility theory. Within the context
of this model, propositions are established concern-
ing the impact of default risk on choices by lenders
and intrepreneurs. (Author)
Documentation
hstitute for Cooperative Research, U. of
Pennsylvania, Riiladelphia.
INFORMATION RETRIEVAL STUDY,
O'Connor. Annual summary rept. no.
Mtr60, on contract Nonr-551(35). 31
Order from LC mi$l. 80, ph$l. 80
by John
1, 1 Apr 59-31
Mar 60, lOp.
PB 153 770
Contents:
The possibilities of document grouping for reduclog
retrieval storage size and search time
On retrieval in aid of scientific discovery
A note on the possibility of a divided structure file
permitting arbitrary substructure searches
Some suggested mechanized indexing investigations
which require no machines
National Bureau of Standards, Washington, D. C.
A SURVEY OF COMPUTER PROGRAMS FOR CHEMI-
CAL INFORMATION SEARCHING, by Ethel C
Marden and Herbert R. KoUer. Feb 61, 87p. 197 refs.
NBS technical nae 85.
Order from OTS $2. 25 PB 161 586
The authors describe twelve computer systems for
searching chemical literature, ft-eceding discussion trf
the computer systems, a brief description is given of
different chenucal notation systems, indexing and ab-
stracting procedures, punched card systems (which
were the forerunners erf the computer systems), and
special purpose literature searching machines. A
short discussion of the difficulties (linguistic and
other) attendant to literature searcliing terminates the
paper. (Author)
Naval Weapons Lab., Dahlgren, Va.
INFORMATION RETRIEVAL AT THE NAVAL
WEAPONS LABORATORY MISSILE SAFETY INFOR-
MATION CENTER, by R. C. Turner, Jr. 27 Oct 60,
56p. 1 ref. NWL rept. 1724; AD- 245 809.
Order from LC mi$3. 60, ph$9. 30 PB 152 978
A very important part of the Missile Safety Informa-
tion Center at the Naval Weapons Laboratory,
Dahlgren, Virginia, is the Information Retrieval Func-
tion. The use of this retrieval function permits a
rapid and low-cost search of the publications main-
tained in (or referenced by) the Information Center.
The search far discrete information is limited to those
characteristics under which each publication has been
cataloged. Every attempt has been made to keep the
retrieval system comprehensive, flexible and not un-
wieldy. This report defines the categories of informa-
tion used in cataloging the publications and discusses
the following elements of the Information Retrieval
Funaion: (a) Determining the Search Code, (b) Re-
questing a Search, (c) Search Results (format). (Author)
Thermophysical Properties Research Center,
Purdue U. [Lafayette, Ind. )
ANALYTICAL AND EXPERIMENTAL STUDY OF A
METHOD FOR LITERATURE SEARCH IN AB-
STRACTING JOURNALS, by A. O. CezalrUyan,
P. S. Lykoudis, and Y. S. Toulouklan. Dec 60, 79p.
3 refs. TPRC rept. 11.
Order from OTS $2. 00 PB 171 478
A new method for literature search using abstracting
journals developed by Lykoudis, Liley and Toulouklan
is extended. The method consists of searching an ab-
stracting journal for a certain period of time and then
obtaining new Information by going through the bib-
liography section of the papers located by the direct
479
search of the abstracting journal. This procedure can
be repeated in cycles. According to the model of the
new method of literature search, a direct search of
C3iemical Abstracts is made to locate publications on
seven thermophy$ical properties (thermal conduc-
tivity, specific hiat, viscosity, diffusion coefficient,
emisslvity, therjuil diffusivity, and Prandtl number)
tor all maner. "fhis search is done for the period be-
tween January 19S4 and December 1957. The refer-
ences cited by ef^ch publication thus uncovered are
searched to obta$i further new information on the
above mentioned jproperties.
fJiS
CELLANEOUS
Naval Research! Lab. . Washington. D- C
REPORT OF NRt PROGRESS. Mar 61.
Order from OTS 11. 25. $10.00/year PB 171 3H
Contents:
Articles:
Penetration of th^ Ionosphere by Very Low Frequency
Radio Signals -$ome Preliminary Results of the
LOFTl I Experitnent, by R. W Zeek, L. S- Bearce.
J. P. Leiphart, and E. Toch
Regulated Charging Current Supply for Van de Graaf
Accelerators, l^y J. W. Butler
X-Ray Mass Ab8t)rption Coefficients for Mo, Mb. Zr,
and Ti, by W. R. Sweeney, R. T. Seal, and
L. S. Birks ]
Scientific program:
Atmosphere and Astrophysics: Surface characteristics
of the moon as indicated by the March 1960 eclipse
and other obseiVations
Chemistry: Inter )retation of some measurements of
hydrogen over- )otential on palladium. Influence of
temperature on the viscosity and drainage rates c4
mechanically produced fire -fighting foams
Mechanics: Fracture stress of high -strengths speci-
men sheet steels {X-200, M-255, and 300- M) sub-
jected to various environments
Metallurgy and Ceramics: Corrosion of iron alloy
(25%Cr-35^1) by a melt containing oxides of vana-
dium and sodium. High -temperature oxidation of
iron-nickel binary alloys in water vapor. Effects of
sintering time and temperature on the oxide bond
strength of metal (nickel) couples. Relation of total
neutron dosage and irradiation temperature to neu-
tron-induced changes in various pressure -vessel
steels. Effects of alloying elements on niobium-ziic
protective coatings for niobium. Oxidation of
niobium -titanium alloys. Kinetics of the formation
of niobium -zinc compounds on niobium in zinc vapor
Nuclear and Atomic Physics: Electrically exploded
wires: progress report on experiments and theory
Radio: Adaptation of shore radio towers as broadband
communication antennas. Laboratory studies of the
polar absorption mechanism. Digital computer
programmed for mutually interference-free com-
munication channel selection. Use of atmospheric
absorption loss curves for calculating radar range.
Proposed mechanism for electrical breakdown in hi|ti
vacuum electron tubes. Project Trade sVinds IV.
Enhanced reliability of Lyman -« humidiometer used
in radio- meteorological investigations. Atmospheric
refraction of radio frequency electromagnetic wave*
Solid-state inductance circuits. E>arasitic antenna
arrays approaching the gain of a parabolic reflector
Solid State Physics: Cavity ionization chamber for de-
termining exposure dose rates and calibrating kilo-
curie gamma ray sources (Co^
Sound: Capacitor types suitable for use under high
hydrostatic pressure
-0
480
ATOMIC ENERGY COMMISSION REPORTS
Reports may be pnirchased in accordance with instructions on the inside front cover of the U. S.
GOVERNMENT RESEARCH REPORTS. As PB numbers are not indicated, order by series and number.
These reports may also be consulted at any AEG Depository Library. A list of these libraries may be
obtained from the U. S. Department of Commerce, Office of Technical Services, Washington 25, D. C.
Reproduction in whole or part of any report listed herein is encouraged by the U. S. Atomic Energy
Commission, subject to the approval of authors or originating sites. General inquires from the indus-
trial press about AEC-developed information should be directed to the bvlustrial Information Branch,
Atomic Energy Commission, Washington 25. D. C.
General, Miscellaneous, and Progress
Reports
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending June 10. 1951. Oak
Ridge Naticnal Laboratory,
)ak Ridge, Term.
Sep 51. Decl. with deletions November 16, 1959,
Comract W-7405-eng-26. 181p. Order from
LC. Mi $8.70, ph $30.30. ANP-65(Del.)
section B monthly progress report for October,
Chemical technology division. Chemical development
_^ ithlv progress repot
1959, by R. E. Blanco. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Jan 60. 47p.
Order from LC. Mi $3. 30, ph $7.80.
CF-59- 12-20
ams
ment
UnclaBsified research and development progr
executed for the division of reactor aeveiopmer
and the division of research for April 1960, by
L H. McEwen. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. May 60. Contract AT(45-1)- 1350. 60p.
Order from LC. Mi $3.60. ph $9.30.
HW-65078
The sodium graphite reactor: tomorrow's power
plant, by R. J. Beeley and others. Atoniics In-
ternational. Division of North American Aviation,
Inc., Canoga Park, Calif. Apr 60. Contract
AT-ll-l-GEN-8. 39p. OrJer from LC.
Mi$3.00, ph$6.30. NAA-SR-Memo-5114
Summary technical report for the period October I,
1955. to December 31, 1955. Volume II, by J.W.
Simmons! National Lead Company of Ohio, Cin-
cinnati, Ohio. Jan 56. Decl. April 28, I960.
Contract AT(30-1)-1156. 96p. Order from LC.
Mi $5. 40, ph $15. 30. NLCO-601
AHpUcations of ultrasonic energy. Progress report
no. 17 covering period from August 1, 1959 to
r 30, 19591 Aeroprojects, Inc. , West
ijeptembe
<3>ester, Pa
Oct 59. Contract AT(30-1)- 1836.
39p. Order from LC. Mi $3.00, ph $6.30.
NYO-2571
Applications of ultrasonic energy. Task no. I:
Chemical processing. Task no. 2: MetaTand
ceramic powder processing. Process report
epo:
m
no. 18 coverlflg period from October I, l^S^o
November 30,' 1 959. Aeroprojects, Inc., West
Chester, Pa. Dec 59. Contraa ATX30-1)-1836.
38p. Order from LC. Mi $3.00, ph $6. 30.
NYO-2572
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending September J0,T952,
by W.B. Cottrell. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Nov 19, 1955. Decl. with
deletions November 16, 1959. Contract W-7405-
eng-26. 146p. Order from LC. Mi $7.20,
ph $22. 80. ORNL-1375 (Del. )
ress report for period ending Mardi 20
jalprog-
. 1^54, by
Electronuclear research division semiannual
E. T. Howard. Oak Ridge hTational Laboratory,
Oak Ridge, Tenn. May 54. Decl. May 3, 1960.
Contract W-7405-eng-26. 26p. Order from LC.
Mi $2.70, ph$4.80. ORNL-1670
Sandia Corporation pape
}, by L. W. hiewhouse
rs on reliability and related
" Sandia Corporaticn ,
uquerque, N. Mex. June 59. 17p. Order
from OTS. 75 cents. SCR -99 A
topics
Semiannual progress report for the period ending
December 31. 1959. University of California"
School of Medicine, Los Angeles, Calif. 1959.
Contract AT-04-1-GEN-I2. 107p. Order from
LC. Mi $5.70, ph $16.80. UCLA-457
Nonmilitary uses of nuclear explosions, by H.
Brown. University of California. Lawrence
Radiation Laboratory, Livermore, Calif. Jan 60.
Contract W-7405-eng-48. 22p. Order from LC.
Mi $2. 70, ph $4. 80. UCRL-58S2
481
i
Densities and >felocitie9 measured on speciniens
fr
froni instruiient and shot holes, by R. S. Guido
and S. E. \^rner. University of California.
Lawrence Radiation Laboratory, Livermore,
Calif. May 60. Contract W-7405-eng-48. I7p.
Order from
UCRL-5990
Some potential luses of nuclear explosives in the con-
servation arid develcyment of water resources.
University df California. Lawrence Radiation
Laboratory, : Livermore, Calif. May 60. Con-
tract W-740fc-eng- 48. 2^. Order from LC.
Mi $2.70, p^$4.g0. UCRL-600e
Plowshare program; peaceful uses for nuclear ex-
ploeives, by D. B. Lombard. University of
California. Lawrence Radiation Laboratory,
Livermore, Calif. July 60. Contract W-7405-
eng-48. 19i
ph $3. 30.
Order from LC.
Mi $2. 40,
UCRL-608I
B ology and Medicine
Semiannual report to the Atomic Energy Commission
by L. O. Jagobson and M. Doyle. Argon ne
Cancer Research Hospital, Chicago, III. Sep 60.
Contract ATtll-l)-69. Il3p. Order from OTS.
$2.50. r ACRH-14
Protein atructut"e and function. Report of sympoai-
umbeldjund6 - 8, 1960, by D. E. Koshland, Jr.
and others. ' Brookhaven National Laboratory,
Biology Department, Upton, N. Y. I960. 266p.
Order from PTS. $2.50. BNL-608 (C-30)
Effect of radiation on the uptake of S^^ -labeled
sulfonamide i Final report, by P. E. Ray.
University of Florida, Cancer Research Labora-
tory, Gainesville, Fla. May 60. Contract AT
(40-l)-2097.i 9p. Order from LC. Mi $1.80,
ph$1.80. I ORO-258
The effects of ibnizing radiations on the developing
animal with Bpecial reference to the nervous sys-
tem.
"rogr
nic E
of Atomic Eftergy Commission Contract AT(30-1)-
Progr<!8S report and application of renewal
1454, by S. P. Hi'cks. New England Deaconess
Hospital and Harvard University, Medical School,
Boston, Masp. June 60. 68p. Order from LC.
Mi $3. 60. ptt $9. 30
TID-6159
Efect of ioniziilg radiation on the viablliry and antl-
;nicity of pfao-rens of domesticated animals.
inal report for May 1, 1957- April 30. I960, by
Iowa State U<uversity of Science and Technology,
and Iowa State University of Science and Technol-
ogy, Institute for Atomic Research, Ames, Icmt
1960. Contract AT(ll-l)-59. 26p. Order fron
LC. Mi $2.70, ph$4.80. TID-6217
Factors influencing the metabolism of cop
r ani
iron. Period covered: July L 1959 to June 30,
1960, by Johns Hopkins University. Baltimore,
Wa7~July 60. Contract AT(30-1)-18I6. 12p.
Order from LC. Mi $2. 40. ph $3. 30.
TlD-6221
>pe
Quantitative population genetics of mice under irrtdi
ation. Progress report for July 1, 1959 to June "
30. 1960, by E. L. Green. Roscoe B. Jackson
Memorial Laboratory, Bar Harbor, Maine.
July 60. Contract AT(30-1)-1979. lOp. Order
from LC. Mi $2.40. ph $3.30. TlD-6278
Radioactive zinc-65 in marine organiams in Fishers
Island Sound and its estuaries. Progress report
and renewal proposal, by D. M. Skausen. Uni-
versity of Connecticut, Storrs, Conn. [I960].
Contract AT(30-l)-2487. 5p. Order from LC.
Mi $1.80, ph$1.80. TID-6307
Achlohydria in Hiroshima. Relation to age, radia-
tion and ABO blood groups, by J. L. Knittle.
Atomic Bomb Casualty Commission, Hiroshima,
Japan. [1959). 17p. Order from LC. Mi %3M
ph $6.30. TID-6328
Urinalysis for curium by electrodeposition, by
I. Dupzyk and M. W. Biggs. University of Cali-
fornia, Lawrence Radiation Laboratory, Liver-
more, Calif. [>ec 60. Contract W-7405-eng-48.
I8p. Order from OTS. 50 cents. UCRL-61M
Genetic effects of chronic X- irradiation exposure
in mice, by D. R. Charles and others. The
University of Rochester, Atomic Energy Project,
Rochester, N. Y. Nov 60. Contract AT(40-I)-
2136. 354p. Order from OTS. $4.50. UR-565
Chemical Separations Processes for
Plutonium and Uranium
Chemical engineering division sumrnary repwrt for
January, February, and March 19^7 . Argonne
n
482
ational Laboratory, Argonne, III. 1957. Decl.
March 21. 1960. Contract W-31-109-eng-38.
I32p. Order from LC. Mi $6.90. ph $21.30,
AN L- 5730
Solvent extraction studies: pulse generators. Qum"
terly report for May 10, 1'951 "to August 10. 1^51
by A. C. Jealous. Oak Ridge National Laboratwj
Oak Ridge, Tenn. Aug 51. Decl. March 23,
1960. Contract W-7405-eng- 26. 13p. Order fr»
LC. Mi $2. 40, ph $3. 30. CF-51 -8-162
Recent developments in feed preparation and solvent
extraction, by F. E. Blanco and J. C. Bresee. Oak
Ridge hi ational Laboratory, Oak Ridge, Tenn.
May59. 67p. Order from LC. Mi $3. 90,
ph$10.80. • CF-58-11-91 (Rev.)
Hot cell demonstration of the fused salt volatility
process, by C. I. Gathers and others. Oak Ki
g
dge
[ational Laboratory. Oak Ridge. Tenn. June 60.
21p. Order from LC. Mi $2.70, ph $4.80.
CF-60-3-11
Anion exhange separation of trivalent actinides and
lanthanides, by M. H. Lloyd and R. E. Leuze.
Oak Ridge National Laboratory, Oak Ridge, Tenn.
June 60. Contract W-7405-eng-26. 12p. Order
from LC. Mi $1.80. ph $1.80. CF-60-3-23
Reaction of uranyl nitrate hexahydrate with sulfur.
by R. S. Ondrejcin. E. I. du Pont de Nemours &
Company. Savannah River Laboratory, Aiken,
S. C. July 60. Contract AT(07- 2)- 1. 8p. Order
from OTS. 50 cents. DP- 497
Reprocessing of power reactor fuels. Eleventh quar-
terly progress report for April 1, 1960 to luly 1,
1960, by L. H. Meyer and others, p. I. du Pont
de Nemours 8i Company. Savannah River Labora-
tory, Aiken, S. C. Aug 60. Contract AT(07-2)-
l. 17p. Order from OTS. 50 cents. DP-519
Decomposition of the tributyl phos^iate- nitrate
complexes, by G. S. Nichols. E. I. du Pont de
Nemours k Company, Savannah Rieer Laboratory,
Aiken, S. C. Nov 60. Contract AT(07 -2)- 1. 23p.
Order from OTS. 50 cents. DP-526
Reprocessing of power reactor fuels. Twelfth quar-
terly progress report for July 1, 1960 to October
1, 19oQ, by E. S. Occhipinti and others. E. I.
du Pont de Nemours 8i Company, Savannah River
Laboratory. Aiken, S. C. Jan 61. Contract AT
(07-2)-l. 8p. Order from OTS. 50 cents.
DP-546
"Hie hydrolysis products of tributyl phosphate and
their effeci ' "" ' ' '
feet on the tributyl phos
uranium recovery, by R
Works. Richland, Wash,
M
Apr 51
1 phc
phate process for
Wagner. Hanford
Decl. April
21,1960. Contract W-31-109-Eng-52. 39p.
Order from LC. Mi $3. 00, ph $6. 30.
HW- 19959
Liquid- liquid dispersions and the significance of the
Qiaengaging test, by L. L. Burger and others.
Hanford Works, Richland, Wash. July 52. Decl.
March 28, 1960. Contract W-31-109-Eng-52.
12p. Order from LC. Mi $2.40* ph $3.30.
HW -24989
Semiworks studies for the reduction of corrosioo-
product impurities in UR -plant UO^. by L. C.
Amos and others. General Electric Company,
Hanford Atomic Products Operation, Richlaivi.
Wash. July 53. Decl. May 4. i960. lOp.
Order from LC. Mi $1.80, ph $1.80.
HW- 28492
PUREX— a Hanford separation plant, by W. J. Mundt.
General Electric Company, Hanford Atomic Pro-
483
ducts Operation, Richland, Wash. Apr 55.
Decl. May 12, 1960. 5p. Order from LC.
Mi $1.80, ph $1.80. HW-36427
Nuclear safety consideration for continuous ion ex-
change column design, by N. Ketzlach. General
ElecOric Company, Hanford Atomic Products
Operation, Richland, Wash. Mar 56. Decl. April
April 27, 1960. Contract W-31-109-Eng-52.
4p. Order from LC. Mi $1.80. ph $1.80.
HW-41838
Confinement and collection of UO?. tines from a
shearing operation, byG.Rey. Hanford Atomic
Products Gyration, Richland, Wash. Oct 60.
Contract AT(45-1)- 1350. 21p. Order from OTS.
50 cents. HW-63854
The pilot plant operation of a vertical tube, recircula-
ting dissolver for the dissolution of uranium diox-
ide in nitric acid, by P. W. Smith. General Elec-
tric Company, Hanford Atomic Products Opera-
tion, Richland, Wash. May 60. Contract AT(45-
1)-1350. lOp. Order from LC. Mi $1.80,
ph$1.80. HW-64416
Technology of non- production reactor fue^ reproc-
essing budget activity 2790 quarterly report, by
V. R. Cooper. General Electric Company, Hain-
ford Atomic Products Operation, Richland, Wash.
May 60. 18p. Order from LC. Mi $2.40,
ph$3.30. HW- 65267
The sulfex process terrninal development report, by
F. D. Fisher. Hanford Atomic Products Opera -
tion, Richland, Wash. Aug 60. Contract AT
(45-l)-1350. 26p. Order from OTS. 75 cents.
HW- 66439
Modifications for the STR fuel recovery process, by
O. W. Parrett. Phillips Petroleum Company,
Atomic Energy Division, Idaho Falls. Idaho.
Dec 60. Contract AT(10-l)-205. 52p. Order
from OTS. $1.00. IDO-14522
Equilibrium dau for PUREX systems, by J. W.
Codding and others. Knolls Atomic Power Labor-
atory. Schenectady. N. Y. Nov 51. Decl. Febru-
ary 4. 1960. Contract W-31-109-Eng-52. 31p.
Order from LC. Mi $3.00, ph $6. 30. KAPL-602
Idaho chemical ttrocessing plant project completion.
by D. R. Rog^s and B. B. Schroeder, Riillips
Peiroleuin Company, Atomic Energy Division,
Idaho Falls, Idaho. Dec 55. 158p. Order frcwn
LX:. Mi $7.8), ph$25.80. M-6862
E)eterminatlon of plutonium and uranium in scruj
'k
dlsBolver solutions, by R. W. Foster and J.
Cooper. Oalc Ridge Natinnal Laboratory, Oak
Ridge. Tenn. July 55. Decl. June 10, 1960.
Contract W-7405-eng-26. 28p. Order from LC-
Mi $2.70, ph 54. 80. ORNL-1854
Ridge, Tenn. I (nd). Contract W-7405-eng-26.
8p. Order fr^OTS. 50 cents. ORNL-3003
frmi
Power reactor fujel processing pilot plant Brookhaven
ng pilot
McDuffe
fuel prc«ram,| by W. T. NJcbuffee. Oak Ridge
NationalLaboratory, Oak Ridge, Tenn. [nd].
Contract W -7 i05-eng- 26. 64p. Order from
OTS. $1.50. ORNL-30I3
Electron accelerators requiring high p)eak power
pulse modulatprs, by V. L. Smith. University
of California,! Lawrence Radiation Laboratory,
Livermore. Qalif, June 60. Contract W-7405-
eng-48. 4p. Order from LC. Mi $1.80,
ph$1.80. UCRL-60I9-T
Chemistry
Physical properties of the halogen fluorides and
rfieir solution^, by M. T. Rogers. Michigan
Sute University, East Lansing, Mich. [19597]
5p. Order frttn LC. Mi $1.80, ph $1.80.
AECU-4720
Dec 60. Contract W-3l-109-eng-38. 155p.
Order from OfrS. $2.75. ANL-6267
ofrs. $2.
Analysis of UN sblutions forNA, by V
Ridge National
J. Reilly. Oak
Laboratory, Oak Ridge, Tenn.
Sep 52. Decl, with deletions December 1, 1959.
3p. Order from LC. Mi $1.80, ph $1.80.
CF-52-9-170(Del.)
The reaction of airconium with uranium dioxide, by
M. T. kobinsbn. Oak Ridge National Laboratory,
Oak Ridge, T*nn. June 57. Decl. April 20. 1960.
I2p. Order ftom LC. Mi $2.40, ph $3.30.
CF-57-6-42
I
Chemical technology division, chemical developmeat
section C monthly progress report for November
1959, by K. B. Brown and others. Oak Ridge
National Laboratory, Oak Ridge. Tenn. Jan 60.
Contract W-7405-eng-26. 52p. Order from LC.
Mi $3. 60. ph $9. 30. CF-59-11-132
Nitric acid species in Tri-n -butyl phosphate solution
by W. E. Shuler. E. I. du Pont de Nemours & ~
Company, Savannah River Laboratory, Aiken,
S. C. Sep 60. Contract AT(07- 2)- 1. 29p.
Order from OTS. 75 cents. DP- 51 3
Thermodynamic and transport properties of gaseoug
carbon dioxide, by L. H. Chen. General Dynam-
ics Corp»raiion, Electric Boat Division, San
Diego, Calif. Aug 59. Contract AT(04- 3)- 187.
157p. Order from OTS. $2.75. GA-1038
The colorinrtetric determination of chromium in
uranium compounds, by O. A. Vita and L. R.
Mullins, Jr. . Goodyear Atomic Corporation,
Portsmouth, Ohio. Dec 60. Contract AT(33-2)-l.
Up. Order frcm OTS. 50 cents. GAT-T-843
Liquid scintilUtion spectronrtetry for the analysis of
Zr^^ — NL^^ mixtures and coincidence standaria-
tlon of these isotopes, by J. D. Ludwick. Genenl
Electric Company, Hanford Atomic Products Oper-
ation. Richland, Wash. Aug 59. Contract AT
(45-l)-1350. 17p. Order from LC. Mi $2.40.
ph$3.30. HW-61728
The transfer of uranyl nitrate across the water-
tributyl phosphate interface, by L. L. Burger.
General Electric Company. Hanford Atomic
Products Operation, Richland, Wash. Nov 59.
Contract AT(45-1)- 1350. 49p. Order from LC.
Mi $3. 30, ph$7.80. HW- 62087
The preparation of plutonium powder by a hydriding
process- -initial^tudies, by G. L. Stlffler and
M. H. Curtis. General Electric Company, Han-
ford Atomic Products Operation, Richland, Wash.
Mar 60. Contract AT(45-1)- 1350. 17p. Order
from LC. Mi $2.40, ph $3. 30. HW-64289
Ion exchange separation and coulometric titration of
)lutonium in irradiated fuel element solutions, b)
f.
W. Handshuh. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. June 60. Contract AT(45-l)-1350. 21p.
Order from OTS. 50 cents. HW -66441
Hydrolysis of water-saturated chlorofluorocarbona
in the presence of metals and the associated corro-
sion, by A. V. Faloon and R. L. Farrar. Jr.
Union Carbide Nuclear Company, Division of
Union Carbide Corporation, Oak Ridge Gaseous
484
Diffusion Plant, Oak Ridge, Tenn. Feb 61.
Contract W-7405-eng- 26. 20p. Order from
OTS. 50 cents. K-1461
Thermodynamic properties of refractory bordies.
part I. Evaporation behavior and vapor pressure
at zirconium diboride. Part II. Phase studies"
in the tanulum- -boron system between Ta and
TaB, by J. M. Leitmaker. Los Alamos Scientific
Laboratory, Los Alamos, N. Mex. Jan 60.
Contract W-7405-eng-36. 266p. Order from
LC. Mi $11.10, ph $41. 40. LA-2402
Reduction of uranium trioxide to uranium dioxide
with hydrogen- reaction rates at various tempera
W
txures, by C. W. Kuhlman, Jr. Mallinckrodt
Chemical Works, St. Louis, Mo. Oct 48. Decl.
November 23, 1959. 6p. Order from LC.
Mi $1.80, ph$1.80. MCW-142
Report of pilot plant work on UF4 production by
means of stirred fluidization, by E. K. Teier.
Mallinckrodt Chemical Works, St. Louis, Mo.
Nov 49. Decl. January 28, 1960. 6p. Order
from LC. Mi $1.80. ph $1.80. MCW-238
The vaporization behavior and thermodynamic sta-
bility of /Zirconium carbide at high temperature,
by B. D. Pollock. Atomics International . A
CKvision of North American Aviation, Inc. ,
Canoga Park, Calif. Jan 61. Contract AT(11-1)-
CEN-8. 19p. Order from OTS. 50 c6nts.
NAA-SR-5439
The radiochemistry of iCirconium and hafnium, by
E. P. Steinberg. Argonne National Laboratory,
Lemont, III. Jan 60. 52p. Order from OlS.
50 cents. NAS-NS-3011
The radiochemistry of beryllium, by A. W. Fair-
hall. Department of Chemistry, University of
Washington, Seattle, Wash. May 60. 58p.
Order from OTS. 75 cents. NAS-NS-30I3
Semi-annual pre
1960 throut
une
Brunswick
Jan 61. 67p.
ress report for the period January
1960, by C. ]. Rodden. New
jratory, New Brunswick, N. J.
Order from OTS. $1.75.
NBL-165
A process for the recovery of uranium and scandi-
um from uranium refinery raffinates, by G. P.
Lang and others. Mallinckrodt Chemical Works,
St. Louis, Mo. May 54. Decl. March 15, 1960.
Cootraci W-14-109-eng-8. 45p. Order from
LC. Mi $3.30, ph $7.80. NYO-1365
Current practices of reporting spectrochemical
reeults (rf uranium samples, by H. R. Mullla.
Kew Brunswick Laboratory, AEC, New Brunswick,
N.J. Feb 54. Decl. March 7, 1960. -lOSp.
Order from LC. Mi $5. 70, ph $16. 80.
NYO-2046
Quarterly summary report for the period January I,
1960 to March 31, 1960. Radiation Applicationa
Inc. , New York, N. Y. 1960. Contract AT(30-
1)-2318. 3p. Order from LC. Mi $1.80,
ph$1.80. NYO-2525
A report on the "metal E" enriched uranium pro-
gram, by W. A. Oppold. Mallinckrodt Chemical
Works, St. Louis, Mo. Oct 51. Decl. March
15, 1960. 21p. Order from LC. Mi $3. 30,
ph$7.80. NYO-5249
Molecular association inalkali halide vapors.
Thesis, by S. Datz. Oak Ridge National Labora-
tory, Oak Ridge. Tenn. May 60. Contract W-
7405-eng-26. 77p. Order from LC. Mi $4. 50,
^ph$12.30. ORNL-2933
Adsorption of xenon and argon on gra{rfiite, by M. C.
Oak Ridge National Laboiratory7 Oak Ridge,
Tenn. [nd]. Contract W-7405-eng- 26. 21p.
Order from OTS. 75 cents. ORNL-2955
Coulometric determination of uranium in power -
reactor-fuel-dissolver solutions, by B. B. Hobbe.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. [nd]. Contract W-7405-eng-26. I6p.
Order from OTS. 50 cents. ORNL-2987
An investigation at the spectrographic analysis of
high purity rare earth oxides. Thesis, by YTG.
Ishida. University of Kentucky, Lexington, Ky.
1959. Contract AT(40-1)-2124. 79p. Order
from LC. Mi $3.90, ph $10.80. ORO-279
Theory of piC -decay, by H. J. Mang. University
of California, Lawrence Radiation Laboratory,
Berkeley, Calif. Oct 59. Contract W-7405-
«ng-48. 73p. Order frOTi LC. Mi $4.50,
ph$12.30. UCRL-8931
Oxidation potential of the Ce(lII) - Ce(iy) couple
as a function of temperature in perchloric acid
solutions -- thermodynamic properties, by H. L.
Con ley. University of California, Lawrence
Radiation Laboratory, Berkeley, Calif. Aug 60.
Contract W-7405-eng-48. 46p. Order from
OTS. $1.00. UCRL-9332
Separation of uranium from urine by a tri-n-octyl-
phosphine oxide column and an automation of the
procedure, by W. C. Deitrich and others.
4SS
J
Union CarblcU Nuclear Company, Division of Un-
ion Carbide Qorporation, Oak Ridge, Tenn.
Sep 60. Contract W-7405-eng- 26. 37p. Order
fromOTS. $i.(X). Y-1322
Controlled
Thermonucleor Processes
Quarterly status report of the LASL controlled
thermonuclear research program for period
ending Novemjber 20, 1960, university of Cali-
fornia, Los AJIamos Scientific Laboratory. Los
Me
Alamos, N.
lex. Dec 60. Contract W-7405-
ENG-36. 42p. Order from OTS.
$1.00.
LAMS -2488
Discha r ge c lean
Jonea" Jr. an
1 up in tJ
Matterl
sity, Project
60. 55p. Oriler from OTS
the etude stellarator, by M.S.
Smith. Princeton Univer-
atterhorn, Princeton, N. J. Mar
$1.50. MATT-29
Stability of non-linear traveling waves in a cold
plasma, by E, A. Jackson. Princeton University,
Project Matteirhorn, Princeton, N. J. Oct 60.
Contract AT(io-l)- 1238. 8p. Order from OTS.
50 cents. MATT- 53
A li
by
id-helium-jcooled trap for pumping gas
adsorption, b^ G. Gibson and others" University
of California, Lawrence Radiation Laboratory,
Livermore, Calif. Oct 60. Contract W -7405-
eng-48. 22p.| Order from OTS. 50 cents.
UCRL-6113
Some calculatic
Fisher. Uni\
Radiation Lat
Contract W-7j
OTS. 75 cent
on the triax pinch device, by S.
irsity of California, Lawrence
iratory, Berkeley, Calif. Aug 60.
)5-eng-48. 35p. Order from
UCRL-9344
Controlled the r
report foF]
lonuclear research
unje, July
;riity of
tof-y, Ber
Augus
UgUJ
ifor
itch quarterly
t 1966, by R. F.
Post. University of California, Lawrence Radia-
tion Laboratory, Berkeley and Livermore, Calif.
Sep 60. Conttact W-7405-eng-48. 107p. Order
from OTS. $;!.25. UCRL-9393
Experiments on Alfven-wave propagation, by J. M.
Wilcox and otierF! University oif California,
Lawrence Radiation Laboratory, Berkeley, Calif.
Nov 60. Coni-act W-7405-eng-48. 31p. Order
from OTS. 7: » cents. UCRL-9482
Criticality Studies
Thorium uranium physics experiments (TUPE).
Monthly report for Oct<j)er 1959, by R. C.
Anderson and others. Babcock and Wilcox Com-
pany. Atomic Energy Division, Lynchburg, V«.
1959. Contract AT(ll-l)-766. 27p. Order
from LC. Ml $2.73, ph $4.80. BAW-1179
Critical experiments for reactor physics studies.
by R. Gwin and D. W. Magnuson. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Sep 60.
64p. Order from LC. Mi $3.90. ph $10.80.
CF-60-4-12
Design criteria for PRP- -critical facility. Project
CAH-842 by G. L. O'Neill and H. K. Nelson-
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Dec 59.
93p. Order from LC. Mi $6.00, ph $18. 30.
HW-62117
Criticality calculations with regard to the dissolu-
don of 2% enriched slugs, by J. W. Webster.
Phillips Petroleum Company, Atomic Energy
Division, Idaho Falls, Idaho. June 55. Decl.
April 28. 1960. Contract AT(10-l)-205. lOp.
Order from LC. Mi $1.80. ph $1.80.
IDO- 16280
Bare critical assemblies of oralloy at intermediate
concentrations of U-235. by H. C. Paxton and
others. Los Alamos Scientific Laboratory, Los
Alamos, N. Mex. May 54. Decl. January 4,
1960. Contract W-7405-eng- 36. 46p. Order
from LC. Mi $3. 30, ph $7.80. LA-1671
In situ neutron multiplication measurements on a
calcining furnace, by M. G. Arthur and others.
Dow Chemical Company, Rocky Flats Plant.
Denver, N. J. Dec 57. Decl. June 10, 1960.
Contract AT(29-1)-1106. 8p. Order from LC.
Mi $1.80, ph$1.80. RFP-91
Plexiglas reflected assemblies of plutonium, by
C. L. Schuske and others. The I>ow Chemical
Company, Rocky Flats Plant, Denver, Colo.
Jan 61. Contract AT(29-1)- 1106. 7p. Order
from OTS. 50 cents. RFP-213
Angular distribution of neutrons from a graphite
surface, by A. C. Jones, Jr. University of
California, Lawrence Radiation Laboratory,
Livermore, Calif. Nov 60. Contract W-7405-
eng-48. 49p. Order from OTS. $1.25.
UCRL-6223
496
Engineering and Equipment
Heat transfer to a mist flow, by J . D. Parker and
R. J. Grosh. Argonne National Laboratory,
Argonne, 111. Jan 61. Contract W- 31- 109-eng-
38. 234p. Order from 015. $3.00.
AN L- 6291
Development testing and performance evaluation
ol liquid metal and molten salt heat exchangers,
by R. E. MacPherson and M. M. Yarosh. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Mar 60. 43p. Order from LC. Mi $3.90,
ph $10.80. CF-60-3-164
Temperature distribution in a ^llow fuel pellet
and in the surrounding metal wall, by D. R.
Carver. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Aug 60. 14p. Order from LC.
Mi $2.40, ph$3.30. CF-60-8-51
Stresses produced in remote studs by impact and
slowly applied tightening torque, py K. L. Pell
and N. H. Shoup. Haniord Atomic Products
Operation, Richland, Wash. Apr 58. Contract
AT(45-1)-1350. 56p. Order from OTS. $1.25.
HW-67257
Dynamic analysis of the superheater, by J. W.
Crowe. Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. June 59. 14p. Order from LC.
Mi $2. 40, ph$3.30. NAA-SR-Memo-3974
General heat transfer mechanisms suitable for use
in OMR fuel elements. A literature survey and
evaluation study, by J. D. Wilde. Atomics In-
ternational. Division of North American Aviation,
tion, Inc. , Canoga Park. Calif. [195?]. 64p.
Order from LC. Mi $3. 90, ph $10.80.
NAA-SR-Memo-4020
Heat transfer and thermodynamic properties of
mercury, by P. D. Cohn. Atomics International
Division of North American Aviation, Inc. ,
Cinoga Park, Calif. Nov 59. 29p. Order from
LC. Mi $3. 00, ph $6. 30.
NAA-SR-Memo-4666
Effect of fins and heater wires on heat transfer
properties in capsule design, by R. O. Pearson.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park, Calif. Dec 59.
lOp. Order from LC. Mi $2. 40, ph $3. 30 .
NAA-SR-Memo-4743
Centrifugal pump characteristics in the near-boiling
range" by S. Sudar and A. Gallegos. Atomics
International. Division of North American
Aviation, Inc., Canoga Park, Calif. Jan 60.
18p. Order from LC. Mi $2.40, ph $3.30.
NAA-SR-Memo-4906
Design of two electromagnetic pumps for NaK, by
R. S. Baker and W. j7 Eraser. Atomics Inter-
national. Division of North American Aviation,
Inc. , Canoga Park, Calif. Mar 60. lip. Order
from LC. Mi $2.40, ph $3.30.
NAA-SR-Memo-5106
In-pile corrosion test loops for aqueous homogene-
ous reactor solutions, by H. C. Savage ana
others. Oak Ridge National Laboratory, Oak
Ridge, Tenn. [nd. ]. Contract W-7405-eng-26.
66p. Order from OTS. $2.00. ORNL-2977
Design criteria for printed circuit boards, by E. L.
Chavez and others. Sandia Corporation, Albu-
querque, N. Mex. Nov 60. 63p. Order from
OTS. $1.75. ' SCDR-280-60
Electrically operated devices for releasing weights
used in drop tests, by A. R. Phillips. Sandia
Corporation, Albuquerqlr , N. Mex. May 56.
Up, Order from LC. Mi $2, 40, ph $3. 30.
SCD^- 100-56-51
Wind tunnel study of the influence of orifice geome-
try and rates on the measured pressure error
of a static pressure probe at Mach 3, by G. W.
Zumwalt. Sandia Corporation, Albuque rque.
N. Mex. Nov 60. 24p.
Order from OTS. $1.00.
SC'IM-315-60(71)
•-i-'.ji
Insulation-resistance and high-potential testing
guide for the design engineering, by R. E.
iCnutson. Sandia Corporation, Albuquerque,
N. Mex.
50 cents.
Dec 60. lOp.
Order from OTS.
SCTM-376-60(71)
Cyclic pressure tests of large size pressure vessels.
ft-Qgress report no. 17 covering the period from
February 15 to March 16, 1960° by M. M.
Lemcoe. Southwest Research Institute, San
Antonio, Tex. Mar 60. Contract AT( 30-1)-
2140. 22p. Order from LC. Ml $2.70,
ph$4.80. TlD-5699
Heat transfer and critical conditions in nucleate
boiling of subcooled and flowing liquids, by Y. P.
Chang. University of Notre Dame, Notre Dame,
Ind. (I960]. Contract AT(ll-l)-785. 45p.
Order from LC. Mi $3. 30, ph $7.80.
TID-6045
487
Out-of-pile loop for helium purification testing,
by R. H. Stone. General Atomic Division . Gen-
eral Dynamics iCorpo ration, San Diego, Calif.
]an 60. Contract AT(04-3)-3l4. 15p. Order
from LC. Mi t2.70. uh $4.80. TID-6341
lit2.70, ph$4.
icy program. <
Solid State physic^ program. Construction of
equipment for .rneasuring tne de Haas -Van
ng_
lot
Alphen effect, by A. S. Joseph. Case Institute
of Technology, Cleveland, Ohio. June 60. 25p.
Order from LC. Mi $2.70, ph $4.80.
^ TID-6393
The measuremenc of air flow through high efficiency
filters, by C. L. Lindeken and others. Univer-
sity of California, Lawrence Radiation Labora-
tory, Uvermore, Calif. Apr 60. Contract W-
7405-eng-48. 12p. Order from LC. Mi $2. 40,
ph$3.30. UCRL-5978
Geoio }y and Mineralogy
Preliminary studiis of scavenging systems related
,to radioactive jfallout. Summary repon, 6y
ry re
J. Roeinski an* J. Stockham. Illinois nstitute
of Technology,, Armour Research Foundation,
Chicago, III. Apr 60. 56p. Order from LC.
Mi $3. 60, ph 19. 30. ARF-3127-12
Variations in the
ores, by
L
ranium-235 content of fifteen
Smith.
L. a'. Smith. Union Carbide Nuclear
Company, Division of Union Carbide Corporation,
Oak Ridge Y-nh Plant, Oak Ridge, Tenn. Jan
61. Contract W-7405-eng-26. 5p. Order from
ens. SOcenti. K-I462
Variations in lflol|[yic abundances of strontium,
calcium, and 4rgon and related topics. Seventh
annua
EL
eia report for 1959. Massachusetts
Instinite of Technology Cambridge, Mass.
Dec 59. Contract ATO 0-1)- 1381. 247p. Order
fromLC. MiSll. 10, ph $37.80. NYO-3940
Diamond drilling in the Southern Black Hills^ Fall
River County" South Dakota by R. C. Bartley.
Grand Junction Operations 6ttice, AEC, Produc-
tion Evaluatio* Division, Denver, Colo. Oct 55.
29p. Order itom OTS. 75 cents.
RME- 1067 (Rev.)
Nevada test
"Granite" explor ttion hole, area 15
site, Nye Coulity, Nevada --interim re;
B, hydrologic data, by C.
rt, part
, E. Price.
Survey, Washington, D. C. Nov 59.
Order from Up.. Mi $2.70, ph $4.80.
TEM-836-B
gpori
Geological
21p.
Isotopic geochemistry of uranium and lead. A
report for 1959-6(3, byj. L. Kulp and othei
of uranium and lead. Annual
jport for 1959-00, byJ. L. Kulp and others.
Columbia University, Lamont Geological Obser-
vatory, Geochemical Laboratory, Palisades,
N. Y. May 60. Contract AT(30-1)- 1114. 21lp.
Order from LC. Mi $9. 60, ph $33. 30.
TID-5966
Final report on radio-geology, by W. S. Broecker.
Columbia University, Lamont Ge ological Obser-
vatory, Palisades, N. Y. June 60. Contract AT
(30-l)-2364. 39p. Order from LC. Mi $3.00,
ph$6.30. TID-6095
Oceanography in the Atomic Energy Conimission,
I. e7 Wallen. Division of Biology and Medicine,
Atomic Energy Commission. [1959] 17p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-6309
Physical oceanography of the test area, by P. L.
Horrer. Scrippe Institution of Oceanography,
La JoUa, Calif, May 55. Changed from
OFFICIAL USE ONLY September 19, 1959. 35p.
Order from LC. Mi $3. 00, ph $6. 30.
Supersedes ITR-1068. WT-1019
Heolth and Safety
Preliminary studies of scavenging systems related
to radioactive fallout. Summary report, by J.
Rosinski and J, Stockman. Illinois Institute of
Technology, Armour Research Foundation,
Chicago, 111. Apr 59. Contract AT(ll-l)-626.
51p. Order fromLC. Mi $3. 30, ph $7.80.
ARF-3127-6
Preliminary stxxiies of scavenging systems related
to radioactive fallout. Letter report no. 8 cover-
ing period June 1 to August 1, 1959, by J. Stock-
ham and J. Rosinski. Illinois Institute of Tech-
nology, Armour Research Foundation, Chicago,
III. Aug 59. Contract AT(1 1- 1)-626. 7p.
Order fromLC. Mi $1.80, ph $1.80.
ARF-3127-8
Fallout program quarterly sununary report for
September 1, 1960 through December I 19"60,
by E. P. Hardy, Jr. and others. United States
Atomic Energy Commission, New York Opera-
tions Office, New York, N. Y. Jan 61. 182p.
Order from OTS. $2.75. HASL-105
Radiological sciences department quarterly prog-
resB report on research and development activi^-
ties for April through June 1952. by H. M.
Parker. Hanford Works, Richland, Wash.
488
July 52. Decl. March 2, 1960. Contract W-
3l-l09-eng-52. 27p. Order from LC.
Ml $2. 70, ph$4.80. HW-25008
Meteorological factors in the control of short-
period, ground level concentrations of separa-
tions stack effluent, by J. J. Fuquay. Genenal
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Dec 57. Decl.
June 10. 1960. Contract W-31-109-Eng-52. 35p.
Order from LC. Mi $3.00, ph $6.30.
HW- 54286
Off-project exposure from Hanford reactor effluent,
by R. F. Foster. Hanford Atomic Products
Operation, Richland, Wash. Feb 60. Contract
AT(45-1)-1350. 41p. Order from OTS. $1.00.
HW- 63654 REV
PRTR mechanical seal pump operating experience
September, 1958 through August. 1960. by P. A.
Scott. Hanford Atomic Products Operation,
Richland, Wash. Sep 60. Contract AT(45-1)-
1350. 63p. Order from OTS. $1.75.
HW- 65724 REV
iy of mortality from congenital malformation
Benton County, Washington, by R. C.
A study _ ^^
for Benton County, Washington, by R. C. Henle.
General Electric Companyr Hanford Atomic
Products Operation, Richland, Wash. Sep 60.
Contract AT(45-1)-1350. 27p. Order from
OTS. $1.00. HW-66344REV
Quarterly progress report research and develop-
ment activities in the field of radiological
sciences April through J une . 1 960, by the Staff
of Hanford Atomic Procfucts Operation. Richland,
Wash. Aug 60. Contract AT(45-1)- 1350. 40p.
Order from OTS. $1.00. HW-66306
Evaluation of radiological conditions in the vicinity
of Hanford July through September 1960, by RTL.
Junkins and others. Hanford Atomic Products
Operation, Richland, Wash. Nov 60. Contract
AT(45-1)-1350. 46p. Order from OTS. $1.00.
HW-67390
jUdlolofiJcal services standard practice manual,
byJ. T. Mahar and others. Knolls Atomic
Power Laboratory, Schenectady, N. Y. Aug 60.
Contract W-31-109-eng-52. 145p. Order from
LC. Mi $7.20, ph $22.80.
KAPL-A-HP-2 (Rev. 1)
Re-evaluation of CMRE hazards with OM terphenyl
as the moderator-coolant, by E. Clark and
odJers. Atomics International Division of North
American Aviation, Inc. , Canoga Park, Calif.
Sep 57. 29p. Order from LC. Mi $2.40,
Eh $3. 30. NAA-SR -Memo- 2055
489
Utilization of radioactive isotopes in coal process
research, by P. M. Yavorsky and E. Gorin.
Consolidation Coal Company, Research and
E>evelopment Division, Library, Pa. Apr 60.
Contract AT(30-)-2350. 97p. Order from OTS.
$2.25. NYO-2597
Dis
yA
ition of nuclear fallout debris
R. Schulert and others
Annual report,
Columbia Univer-
sity, Lamont Geological Observatory, Palisades.
N. Y. Oct 60. Contract AT(30-1)-1656. 178p.
Order from OTS. $2.75. NYO-9466
Environmental beta-gamma radioactivity in air
at Sandia Laboratory. April through Novembei
1958, by R. E. Wornelsauff and A? Juskiewicz
Sandia Corporation, Albuquerque, N. Mex.
Dec 60. 21p. Order from OTS. 75 cents.
SC-4493 (RR)
Albuquerque winds aloft in relation to fallout, by
C. E. Buell. Sandia Corporation, Albuquerque,
N. Mex. June 56. Contract AT(29-l)-789. 14p.
Order from LC. Mi $2. 40, ph $3. 30.
SCTM-129-56-51
A pilot study of the horizontal transport of fission
products in the troposphere, by R. E. Newell.
Massachusetts Institute of Technology, Cam-
bridge, Mass. May 60. Contract AT( 30-1)-
2241. 24p. Order fromLC. Mi $2.70,
ph$4.80. TID-6132
Project sunshine annual report for- period October 1,
1957 to September 30, 1958. Columbia Univer-
sity, Lamont Geological Observatory, Palisades,
N.Y.Oct 58. Contract AT(30-1)-1956. 226p.
Order from LC. Mi $9. 90, ph $34. 80.
TID-6202
Program of the United States government in atmoe-
pneric radioactivity, by G. T. Anton. U. S.
Atomic Energy Commission, Washington, D. C.
Nov 60. 14p. Order from OTS. 50 cents.
TID-6947
Outline of courses in the department of radiation
biology and Atomic Energy project. University
of Rochester, by J. N. Stannard. University erf
Rochester, Atomic Energy Project, Rochester,
N. Y. July 60. Contract W -7401 -eng- 40. 76p.
Order from LC. Mi $4. 50. ph $12. 30.
UR-600
Missile studies with a biological target, by V. C.
Goldizen and others. Lovelace Foundation for
Medical Education and Research, Albuquerque,
N. Mex. Apr 60. 64p. Order from OTS.
$1.50. WT-1470
Comparison test Of reinforcing steels, by R,
Carlson and ].' ~
Albuquerque,
from OTS. $:
iN.
Murtha. Sandia Corporation,
Mex. Oct 59. 108p. Order
.25.
Instruments
H. of graphite at high temperatures, by W. V.
Goeddel! General Atcwnic Division, General
Dynamics Corporation, San Diego, Calif, jan
WT-1473 " 59. Contract AT(04-3)-314. 6p. Order from
LC. Mi$1.80, ph J1.80. GAMD-1229
Engineering desii ji of microwave electron density
Technical memorandum
measuring syyems.
no. 78, by M. A. Heald. Princeton University,
Project Maitertiorn, Princeton, N. J. July 59
Contract AT(30-1)- 1 238. 22p. Order from LC.
Mi $2. 70. phi4.80. AECU-4498
$2.70. phi4.80.
Magnetic recordejr for nuclear pulse application.
' '■ une 5, 1959 to
r pu
^inaT report covering peri
June 5, 1960, by G. M. Burgwald and C. A
Stone. Illinois Institute of Technology, Armour
Research Foundation, Chicago, 111. June 60.
Contract AT(ll-l)-702. 55p. Order from LC.
Mi $3. 60. phl9.30. ARF-1151-6
Use of the DD2 aikiplifier with the RIDL 200- and
400 -channel ai|alyzers, by H. A. Tood and R. D.
Smiddie. Oak Ridge National Laboratory, Oak
Ridge. Tenn.
26. 5p. Order from LC. Mi $1.
Sep 60. Contract W-7405-eng-
Eddy current detection of Al-Sl penetrations in
ginned slugs, py R. C. Robinson and J. D. Ross.
Du Pont de Neiiiours (E. I. ) 8i Company, Savan-
nah River Laboratory, Aiken. S. C. Dec 57.
1960. Contract AT(07- 2)- 1.
Mi $2.40, ph$3.30.
DP- 243
Decl.
14p.
May 4,
Order fibm LC.
Nonlinear analog! e to di;
. -1 5^^ converter, by L. E.
Goodwin. Du l*ont de^emours (E. I. ) & Com-
pany, Savannah River Laboratory, Aiken, S. C.
Aug 59. DeclJ November 30, 1959. Contract
A'n07-2)-l. 12p. Order from LC, Mi $2,40,
ph $3. 30. I DP-406
Water wheel rivet and stream sampler, by K. J.
u Pont de Nemours (E. I. ) k Com
ia|i
Travers. Du
pany, Savannaii River Laboratory, Aiken, S. C.
Nov 59. Contract AT(a7- 2)- 1. Up. Order
from LC. Mi )J2. 40. ph $3. 30. DP-426
Plutoniion monitor for puncture wounds, by G. H.
r pur
Pori
Gruber. E. I.,' Du Pont de Nemours & Company,
Savannah River Laboratory, Aiken, S. C. Dec
60. Contract AT(a7- 2)- 1. 12p. Order from
OTS. 50 cenu . DP-508
An ajyaratus for
Operating experience with ion pumps on mass
gpectron>eters, by V. E. Schupbach. Goodyear
Atomic Corporation, Portsmouth, Ohio. Aug 60.
Contract AT(33- 2)- 1. 12p. Order from LC.
Mi $2. 40. ph $3. 30. GAT-T-783
Recirculating gas loop rupture monitoring, by D. C.
Pound. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
June 57. Decl. June 10, 1960. Contract W-31-
109-Eng-52. Up. Order from LC. Mi $2.40,
ph$3.30. HW -51032
Eddy current ultrasonic transducer, by H. L. Ubbf.
doieral Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Aug 59.
15p. Order from LC. Mi $2.70. ph $4.80.
HW -61629
A simple telephone telemeter, by C. A. Ratcliffe.
General Electric Company, Hanford Atomic
80, ph$1.80. Products Operation, Richland, Wash. Nov 59.
CF-60-9-ia7 Contract AT(45-1)-1350. 8p. Order from LC.
Mi $1.80, ph $1.80. HW-62419
Glove box integrity study, by R. A. Ciccarelli.
General F'eciric Company, Hanford Atomic
Products Operation, Richland, Wash. Mar 60.
Contract AT(45-1)-1350. 23p. Order from LC.
Mi $2.40, ph $3. 30. ' HW-64258
A wrist badge film dosimeter for hand dose meas-
urement, by P. E. Bramson. General Electric
Company, Hanford Atomic Products Operation,
Richland, Wash. June 60. Contract AT(45-1)-
1350. I6p. Order from LC. Mi $2.40,
ph$3.30. HW -64892
A miniature beta scintillation detector, byR.A.R.
Kent and E. M. Sheen. General Electric Com-
pany, Hanford Atomic Products Operation,
Richland, Wash. May 60. Contract AT(45-1)-
1350. 15p. Order from LC. Mi $2. 40.
ph$3.30. HW -65036
L/R indicator by G. C. Minor. General Electric
Company, Hanford Atomic Products Operation,
. Richland, Wash. May 60. Contract AT(45-1)-
1350. 9p. Order from LC. Mi $1.80, ph$1.80.
HW -65178
measuring the thermal conductivity
490
Scintillation alpha detection probes, by R. A. R.
Kent. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Sep 60. Contract AT(45-1)-1350. 20p. Order
froroOTS. 50 cents. HW-66837
Ganuna radiation detector and warning syster^, by
J. B. Deal and others. The University of Cali-
fornia, Loe Alamos Scientific Laboratory, Los
Alamos, N. Mex. Nov 60. Contract W -7405-
ENG-36. 16p. Order from OTS 50 cents.
LA -2490
Development of temperature protective circuits for
ihe HNPF fuel channel exit, (revised), by D. ^
Brown and C. L. Dunsmore. Atomics Internation-
al. A Division of North American Aviation, Inc. ,
Canoga Park, Calif. Jan 61. Contract AT(11- 1)-
GEN-8. 19p. Order from OTS. 50 cents.
NAA-SR-5313 (REV)
Calculated sensitivity of a circulating uranium hexa-
fluoride continuous neutron flux monitor, byJ.C.
Kin ley. Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. Jan 60. 8p. Order from LC. Mi $1.80.
ph$1.80. NAA-SR-Memo-4617
Mass spectrometry instrumentation. Final report
and research proposal (renewal), by M. K.
Teste rman. University of Arkansas, Graduate
Institute of Technology, Little Rock, Ark. Aug
59. Contract AT(40-1)-2123. 76p. Order from
LC. Mi $4. 50, ph $12. 30. ORO-299
Design and construction of a unit for measuring
metal skin temperatures. Phase II. Laboratory
investigation and construction of developmenf
models" for the period May 1956 through Novem-
ber 1956, by Detroit Controls Corporation, Re-
search Department, Redwood City, Calif. Jan
61. 26p. Order from OTS. $1.00.
SC-4462 (RR)
Instrumentation of aluminum bodies to determine
interior temperature variations and rate of sur-
face recession during exposure to nuclear ex-
plosions. Phase 2: Item 7, Development of
instrumentation. Phase 3: Item 2, LaborTtory
testing of instrumentation. Riase 4: Items 2, 3.
and 4, Instrumentation of 3/4- inch thick alumin-
um melt plates for field testing for tl^ period"
March 1957 through August 1957, by Detroit Con-
trols Division of American -Standard, Research
Departn^ent, Redwood City, Calif. Jan 61. 28p.
Order from OTS. $1.00. SC-4463 (RR)
Interim report on development of design criteria
for relays, for the period 1 June to 31 July I960,
by School of Electrical Engineering, Oklahoma
State University, Stillwater, Oklahoma. Nov 60.
85p. Order from OTS. $2.25. SC-4519 (RR)
Salton Sea meteorological instrumentation test
series Salton Sea, California conducted in Sep-
tember 1959, by L. E. Jones and others. Sandia
Corporation, Albuquerque, N. Mex. Jan 6L
127p. Order from OTS. $2.75.
SC-4521 (RR)
Hi^-speed auto-data system for blast studies, by
R. D. Joies and J. D. Smith. Sandia Corpo ration,
Albuquerque, N. Mex. July 60. Contract AT
(29-l)-789. lOp. Order from LC. Mi $1.80.
ph$1.80. SCR-168
Standard test pattern for printed wiring cards, by
R. P. Noble. Sandia Corporation, Albuquerque,
N. Mex. May 59. 5p. Order from LC.
Mi $1.80, ph$1.80. 5011^-108-55-53
Preliminary investigation of die response of pres-
sure gauges to dust- laden air, by J. R. Banister
and C. D. Broyles. Sandia Corporation, Albu-
querque, N. Mex. Feb 54. 22p. Order from
LC. Mi $2.70. ph $4.80. SCTM-215-53-51
"H" parameter tables, by T. E. Lommasson.
Sandia Corporation, Albuquerque, N. Mex. Dec
55. 9p. Order from LC. Mi $2.70. ph $4.80.
5011^-273-55-53
Experimental evaluation of sources of variance in
spectometer measurements, by W. G. Hart and
L. A. Smith. Oak Ridge Gaseous Diffusion
Plant, Oak Ridge, Tenn. Dec 55. Decl. March
23, 1960. 12p. Order from LC. Mi $2,40,
ph$3.30. TID-5684
In-line radioactivity monitors, by G. Jansen, Jr.
and others. Massachusetts Institute erf Technol-
ogy, Engineering Practice School, Oak Ridge,
Tenn. Jan 57. 15p. Order from LC. Mi $2.40,
ph$3.30. TID-6173
The channeled image Intensifier. Quarterly progres
ress report no. 8, by University of Chicago,
Laboratories for Applied Science, Chicago. 111.
May 60. Contract AT(1 1-1)- 647. 2Qp. Order
from LC. Mi $2.40, ph $3.30. TID-6218
Thermal neutron detection using electromagnetic
waveguides. Final report, by L. T. Ostwald and
P. D. Wickersham. Ramo-Wooldridge. Division
of Thompson Ramo Wooldridge Inc. . Denver.
Colo. May 60. Contract AT(04-3)- 165. 105p.
Order from LC.
Mi $5. 70. ph $16.80.
TID-6296
491
I
Timing and flrtng^of high exploBiveai. Final report,
by R. R. Hamyton. Edgerton, Germeshausen
and Grier, In4. , Lac Vegas, Nev. June 60.
32p. Order fri)m LC. Mi $3. 00, ph $6. 30.
TID-6353
AT(30-l)-2329. 63p.
A aystematic prcx^ure for preparing apectflcations
on electronic iftstrumentation and control sya-
tenis, by H. Olken. University of California,
Lawrence RadliEition Laboratory, Livermore,
Calif. [I960), Contract W-7405-eng-48. 60p.
Order from LC
Mi ^3. 60, ph$9.30.
UCRL-5977-
Transistor counting systems for scintillation detec-
tors, by S. C. Baker and others. University
of California, Lawrence Radiation Laboratory,
Berkeley, Calif. Feb 60. Contract W-7405-eng-
48. 23p. Ord^rfromLC. Mi $2.70, ph $4. 80.
UCRL-9000
Nuclear material
Field testin
T"
control system (NMCS) phase II:
ing c^ the fuel assay scanner, by f.
Arsenault. W^stinghouse Electric Corporation,
Atomic Power Department, Pittsburgh, Pa.
June 60. Cont*act AT(30-l)-2l76. 35p. Order
fromLC. Mi ^3. 00, ph $6. 30. WCAP-6042
Isotopes- -Industriol Technology
Fission product atolications using gaseous beta
sources. Fouyth quarterly progress report for
December 1,
Miller ajid
rogress repo
Sales Compan
1959 to February
J. H. Zufall. Air Reduction
by
inyj,
Murray Hill, N.
2343.
ph$3.
20p.
30.
Central Research Laboratories,
J. 1960. Contract AT(40-1)-
Otder from LC. Mi $2.40,
NYO-2606
Investigation of amplications of Compton backs catter,
— by j: H. Tolan^nd W. T. McIntMh. Lockheed
Nuclear Products, Lockheed Aircraft Corpora-
tion, Georgia Division, Marietta, Ga. July 60.
Contract AT(30- 1)- 2428. 36p. Order- from
OTS. $1.00. i NYO-2779
A. E. C. researdi and development report on effect
of irradiation of solid catalysts, by H. C.
Anderson and others. Engelhard Industries, Inc.
Newark, N.J. Sep 60. Contract AT(30-1)- 2402.
20p. Order fr^m 0T3. 75 cents. NYO-2836
Evaluation of the radioactive tracer technique for
use in tool -wear studies, by N. H. Cook. Ivfas-
sachusens Instiitute of Technology, Department
of Mechanical Engineering, Metals Processing
Division, Cambridge, Mass. June 60. Contract
492
Order from OTS. $2.00.
NYO-9227
Applications of nuclear radiation and radlosotopea
to textile materials and processes. Annual re-
port for the period November 1 , 1 958 to Novem-
Der 1, 1959. North Carolina State College, Tex-
tile Research Center, Raleigh, N. C. 1959.
Contract AT(40- 1)- 2477. 72p. Order from LC.
Ml $4. 50, ph$12.30. ORO-257
The development of short bowl ultracentrlfuges.
Final report, by G. Zippe. University ot Vir-
ginia, Research Laboratories for Engineering
Sciences, Charlottesville, Va. June 60. Con-
tract AT(40-1)- 2400. 107p. Order from LC.
Mi $5.70, ph $16.80. ORO-315
Isotoplc method for age determinations of industrial
products. Quarterly progress report for Janu-
ary to March 1960, by R. C. Gregson and L. B.
Bangs. Goodyear Tire and Rubber Company,
Akron, OHo. 1960. Contract AT(ll-l)-719.
28p. Order fromLC. Mi $2.70, ph $4.80.
TID-6044
Summary of a survey of applications for an x-ray
Raleigh scattering gage. Period covered: April
15 to May 15, 19607 Tracerlab, Inc., Waltham,
Mass. 1960. Contract AT(30-l)-2538. 6p.
Order fromLC. Mi $1.80, ph $1.80.
TID-6104
The applications of isotop)e8 to industrial problems.
Progress report letter no. 15 for the period"
May 16 to June 15, 1960, by F. F. Rieke. Uni-
versity of Chicago, Chicago Midway Laboratoriet,
Chicago, III. June 60. Contract AT(11-1)-712.
lip. Order from LC. Mi $2.40, ph $3.30.
TID-6151
Isotoplc method for age determinations of industrial
products. Quarterly progress report for April
K) June I960, by T. c' Gregson and L. B. Bangs.
Goodyear Tire and Rubber Co. , Akron, Ohio.
1960. Contract AT(11-1)-719. I3p. Order
fromLC. Mi $2. 40, ph $3. 30. TID-6553
Radloi80to{)e3 and nuclear techniques in the
pharmaceutical and allied industries, by J. E.
Christian and W. F. Bousquet. Purdue Univer-
sity, Lafayette, Ind. June 60. Contract AT
(ll-l)-737. 119p. Order from OTS. $2.50.
TID-11215
Marketing feasibility study of radiation processed
fishery products, by U. S. Department of the
Interior, Fish and Wildlife Service, Bureau at
Commercial Fisheries, Washington, D. C.
Dec 60. 33p. Order from OTS. 75 cents.
WASH- 1030
Isotope Separation
The evaporative centrifuge method, by F. C. Armi-
stead and others . University of Virginia, Char-
lottesville, Va. 1942. Decl. September 23, 1960.
Contract OEMsr- 140. 1(^. Order from LC.
Ml $1.80, ph$1.80. A-119
Brief report of type II centrifuge operation, by J. W.
Beams. University of Virginia, Charlottesville,
Va. Feb 44. Decl. September 23, I960. 13p.
Order fromLC. Ml $2.40, ph $3. 30. A-1778
Ammonia process for deuterium concentration, by
W. I. Thompson. Ferguson (H. K. ) Company,
Atomic Energy Division, New York, N. Y. Sep
51. Decl February 20, 1957. Contract AT(30-1)-
1075. 68p. Order from LC. Ml $3.90,
ph $10.80. HKF-113
Ammonia distillation for deuterium separation, by
G. T. Petersen and M. Benedict. Massachusetts
Institute of Technology, Cambridge, Mass. May
60. Contract AT(30-1)- 2249. 212p. Order from
LC. Mi $9. 60, ph$33.30. NYO-2347
Developments in the centrifuge separation project,
by ]. W. Beams and others. Atomic Energy
Commission, Washington, D. C. 1951. Decl.
October 29, 1959. 269p. Order from OTS.
$3.50. TID-5230
Thermodynamics of the hydrogen sulfide- -water sys
tern relevant to the dual temperature process for
the production of heavy water. Technical report
^B, by H. A. Pohl. Princeton University, Plastics
Laboratory, Princeton, N. J. and Du Pont de
Nemours (jE. I.) k Company, Explosives Depart-
ment, Wilmington, Del. July 60. Contract AT
(07-2)-l. 28p. Order from LC. Mi $2.70,
ph$4.80. > TID-6696
Mathematics and Computers
Adjoint flux computation and other additions and im-
Srovements to the equipoise program; the three-
imensional prototype j?rogram, whirlaway. by"
M. Tobias and T. B. Fowler. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Aug 60. 6p.
Order fromLC. Mi $1.80. ph $1.80.
CF-60-8-10
An investigation of the mineralogy, petrography
and paleobotany of uranium-bearing lipiltesT by
Pennsylvania State University, College of Mineral
Industries, University Park, Pa. May 60. Con-
tract AT(30- 1 )-2000. I4p. Order from LC.
., Ml $2.40, ph$3.30. NYO-7950
The dared code; modification of the deadtlme cor-
rection and automatic repetition of counting times,
by J. Jedrudi. Westinghouse Electric Corporation,
Atomic Power Power Department, Pittsburgh, Pa.
Aug 60. Contract AT(30-3)-222. ^. Order
fromLC. Mi $1.80, ph $1.80.
YAEC-104(Suppl.)
Metals, Ceramics, and Materials
Structure and surface chemistry of thorium oxide,
by A. L. Draper and W. O. Mllllgan. Rice In-
stitute, Houston, Tex. Sep 59, Contract W-7405-
eng-26, 90p. Order from LC. Mi $5.40,
ph$15.30. AECU-4395
Physical and mechanical properties of some alumin-
um- lithium alloys. Final report, byH. H. Chis-
wik, and others. Argonne National Laboratory,
Argonne, III, Nov 52. Decl. March 15, 1960.
Contract W-31-109-eng-38. 42p. Order from LC.
Mi $3. 30, ph$7.80. ANL-4992
Metallurgy division quarterly report for October,
Novemoer, and Deceniber 19*6. Aigonne National
Laboratory, Argonne, III. 13ec 56. Decl. Febru-
ary 4, 1960. Contract W -31- 109-eng- 38. 64p.
Order from LC. Ml $3. 90, ph $10. 80.
AN L- 5709
The drip casting of zirconium metal, by R. J
rtn and R. E. Macherey
Dun-
worth and R. K. Macherey. Argonne National
Laboratory, Argonne, III. Oct 60. Contract W-
31-109-eng-38. 18p. Order from OTS. 50 cents.
ANL-6141
Specifications and fabrication procedures for SM-IA
core II neutron absorber sectlcms! AIco Products
Inc., Schenectady, N. Y. May 60. Contract AT
(30-3)-326. 56p. Order from LC. Mi $3.30,
ph$7.80. APAE-Memo-259
Progress relating to civilian apl^licatlons during July
1959. by R. W. Dayton and C. R. Tipton, Jr.
Battelle Memorial Institute, Columbus. Ohio.
Aug 59, Decl. February 4, 1960. Contract W-
7405-eng-92. lOOp. Order from LC, Ml $5.70,
ph $16.80. BMl-1366
493
Pri
ess relating jo civilian applications during Octo-
r, 1960, by It. W. Dayton and C. R. Tipton, Jr.
Battelle Memorial Institute, Columbus, Ohio.
Nov 60. 72p. Order from OTS. $2.00.
1 BMl-1473
Effects of irradiation on the mechanical properties
of tanulum, by C. K. Franklin and ^
telle Memorial! Institute, Columbus,
60. Contract W-7405-eng-92. 19p.
OTS. SO cents
others. Bat-
Ohio. Nov
Order from
BMI-1476
and metal-coa
g^ compatibi
rticlea with graphite and
Hlgh-temperanire^ compatibility of Al^O.^-, BeO-,
Si.
' - By. Bat-
telle Memorial Institute, Columbus, Ohio. Nov
60. Contract W-7405-eng-92, 29p. Order from
OTS. 75cent8l BMI-1479
The effect of radii tion on selected properties of
"X speherical grajhiite fuel elennents
V Smalley and ot^r
11=
y A. IC
rs. Bane lie Memorial Institute,
Columbus, Ohib. Dec 60. Contract W-7405-eng-
92. 21p. OrdAr from OTS. 50 cents.
BMI-1483
m
ay oi
A study of the radatton stability of UO2 dispersions
by D. (Jj. Freas and others. Battelle
Memorial Institute, Columbus, Ohio. Dec 60.
Contract W-74<l5-eng-26. 27p. Order from OTS.
75 cents. BMI-1484
Pre
iperation and properties of UO^ cermet fuels, by
S. J. Paprocki iind others. Battelle Memorial
Institute, Coluxibus, Ohio. Dec 60. Contract
W-7405-eng-9:^. 64p. Order from OTS. $1.75.
BMI-1487
Progress on the development of uranium carbide -
type fuels. P^Jse II report on the AEC fuel-cycle
cnropram, by F; A. Rough and others. Battelle
Memorial Institute, Columbus, Ohio. Dec 60.
Contract W-7405-eng-92. 62p. Order from OTS.
$1.50. BMI-1488
Low volume change concrete studies, by J. H.
Lancaster^ Brookhaven National Laboratory,
Upton, N. Y. Jan 58. 5p. Order from LC.
Mi $1.80, ph$1.80. BNL-4648
Process development quarterly report for April-
June 1957! Bridgeport Brass Company, Bridgeport,
Conn. Nov 57. Decl. February 4, 1960. Con-
tract AT(30-1)-1405. 80p. Order from LC.
Mi $4.80, |^$13.80. BRB-39
Metallurgical investigation of the stress c
failure in the stainless steel clad of the
corrosion
y SIC re-
actor vessel, by G. Zuromsky. Combustion Engi-
neering, Inc. , Nuclear Division, Windsor, Conn,
[ndj. 21p. Order from LC. Mi $2.40. ph $3. 30.
CEND-78
A program to study the feasibility of and develop an
apparatus for the ultrasonic roll bonding of fuel
plates. Summary report for the period June 14,
f
ry repor
959 to August 15, 1960. Combustion lingineering
Inc. , Nuclear Division, Windsor, Conn. , and
Aeroprojects, Inc. , West Chester, Pa. Dec 60.
Contract AT(30-l)-2379. 129p. Order from OTS.
$2. 50. CEND-93
The removal of corrosion scale from heat exchanger
by cheniical treatments, by O. Menis. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Apr 59.
5p. Order from LC. Mi $1.80, ph $1,80.
CF-59-4-107
Operation of HRP in pile corrosion test loop 0'1'25,
by V. A. DeCarlo and R. A. Lorenz. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Aug 60.
36p. Order from LC. Mi $3. 00, ph $6. 30.
CF-60-8-120
Fabrication of beryllium: A bibliography, by E. A.
Cernak. Pratt and Whitney Aircraft Division,
United Aircraft Corporation, Middletown, Conn.
Apr 60. 28p. Order from LC. Mi $2.70,
ph$4.80. CNLM-1802-14
Uranium dioxide- -^stainless steel specimens for Ir- Use of Monel wire tubes in the cleanup reactor filter
radiation in 3o4ium--experiment PW-5-1, by G. D.
Calkins and othiers. Battelle Memorial Institute,
Columbus, Ohio. Apr 55. Decl. January 12,
I960. 19p. OfderfromLC. Mi $2.40, ph $3. 30.
BM1-X-I27
Structural materiils for thermal nuclear reactors
by M. L. Geneva and others. Goodyear Atomic
Corporation, Portsmouth, Ohio. Aug 60. Con-
tract AT(33- 2)- 1. 7p. Order from LC, Mi$1.8a
ph$1.80. GAT-P-22
operating at about 1950 F with air as a coolant,
by W. Cnubb arid others Battelle Memorial In-
stitute, ColumJhus, Ohio. July 60. 76p. Order
from LC. Mi 1 4.80, ph $13.80. BMI-X-159
Metallurgical stability of several boride dispersion
systems Technical report, by K. C. Antony and
W. V. Cummings, General Electric Company,
Atomic Power Equipment Department, Pleasantoa,
Calif. Sep 60. Contract AT(04-3)- 189. 25p.
Order from OTS. 75 cents. GEAP-3530
494
Failure of stressed cylinders, by A. T. Taylor and
M. Pedersen. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Mar 55. Decl. March 31. 1960. 2lp.
Order frc«n LC. Mi $2.70, ph $4.80.
HW-35717
Grain size study on irradiated jpowder metal uranium,
" byj. R. Morgan. General Electric Company,
Hanford Atomic Products Operation, Rlchlaivd,
Wash. May 55. Decl. June 10, 1960. Contract
W-31-109-eng-52. 8p. Order from LC. Mi
Mi $1.80, ph$1.80. HW- 36453
Uranium dioxide- -plutonium dioxide ceramics, by
A. S. Wilson. General Electric Company, Han-
ford Atomic Products Operation, Richland, Wash.
Mar 58. lOp. Order from LC. Mi $1.80,
ph$1.80. HW-55319
Hydrogen absorption in Zircaloy-2 due to aqueous
corrosion at 680"F, by D. L. Gray. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. June 58. Contract
AT(45-1)*1350. 8p. Order from LC. Mi $1.80,
ph$1.80. HW-56515
ETR-MTR experiments on restraint of uranium
Bwelling by zirconium cladding, by J. W. Weber.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Apr 59.
Contract AT(45-1)-1350. I6p. Order from LC.
Ml $2. 40, ph$3.30. HW-59941
Photographic observations of thermal effects in un-
irradiated uranium dioxide fuel cores, by H. W. ,^
NewklrkandJ. L. Bates. General Electric Co. ,
Hanford Atomic Products Operation, Richland,
Wash. June 59. Contract AT(45-1)-1350. 12p.
Order from LC. Ml $2.40, ph $3.30.
HW-60828
Effects of reactor environment on candidate PRTR
8 loop materials, by A. L. Bement and others.
neral Electric Company,^ Hanford Atomic
Products Operation, Richland, Wash. Sep 59.
Contract AT^45-l)-1350. I3p. Order from LC.
Mi $2. 40. ph$3.30. HW-62543
Magnetic force resistance butt welding of Zircaloy-2
fuel element closures, by L. E. Mills. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Nov 59. Contract
AT(45-1)-1350. 12p. Order from LC. Ml $2.40,
ph$3.30. HW- 62482
lite blast cleaning process as an aid to visual weld
inspection, by cf. R. Hanson. General Electric
Company, Hanford Atomic Products Operation.
Richland, Wash. Mar 60. Contraa ATX45-1)-
1350. 12p. Order from LC. Ml $2. 40,
ph$3.30. HW-64196
In-reactor creep measurements on Zircaloy-2, by
L. J. Chockie. General Electric Con^jany, Han-
ford Atomic Products Operation, Richland, Wash.
Apr 60. 7p. Order from LC. Mi $1.80,
ph$1.80. HW-64814
Twin argon welding of alsi-bonded aluminum clad
uranium metal fuel elentents, by T. B. Correy.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. May 60.
Contract AT(45-1)-1350. 15p. Order from LC.
Mi $2.40. ph$3.30. HW-65059
Aluminum alloy work at Hanford. Interim report,
by H. C. Bcwen. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. May 60. Contract AT(45-1)- 1350. 17p.
Order from LC. Mi $2.40, ph $3. 30.
HW- 65077
Examination of an irradiated, Zlrcaloy-2, hot water
loop tube, by A. L. Bement. Hanford Atomic
Products Operation, Richland, Wash. July 60.
Contract AT(45-1)-1350. 17p. Order from OTS.
50 cents. HW- 65999
Zlrcaloy welding techniques developed for plutonium
recycle program UO2 fuel element fabrication, by
L. E. MillsT Hanford Atomic Products Operation,
Richland, Wash. Oct 60. Contract AT(45-1)-
• 1350. 35p. Order from OTS. $1.00.
HW-66178
Non-metallic materials evaluation for April-June
1960, by J. H. Kleinpeter. General Electric Coro-
pany, Hanford Atomic Products Operation, Rlch-
Und, Wash. Aug 60. Contract AT(45-1)-1350.
4p. Order from LC. Mi $1.80, ph $1.80.
HW-66408
Fabrication of aluminum clad plutonium -aluminum
alloy pin elements, by L. C. Lemon and W. "t.
Roes. Hanford AtonUc Products Operation, Rich-
land, Wash. Sep 60. Contract AT(45-1)- 1350.
13p. Order from OTS. 50 cents. HW-66757
Out-of- reactor evaluation of components and assem-
blies - Mark I swaged UO2 PRTR fuel element, by
M. K. MillhoUen. Hanford Atomic Products
Operation, Richland, Wash. Sep 60. Contract
AT(45-1)-1350. 23p. Order from OTS. 50 cents.
HW- 66910
495
AquecwjB corrosioti of alumlnmn-plutonlum alloyg,
by C. H. Blodiister and Y. B. Katayama. Man-
ford Atomic Pnoduccs Operation, Richland, Wash.
Oct 60. Cootriict AT(45-1)-1350. 18p. Order
fromOTS. SOi cents. HW- 67098
Melting points in the system t>u02'U02. by S. W.
Pijanowski and' L. S. DeLAica. General Electric
Ccxnpany, Knolls Atomic Power Laboratory,
Schenectady, li. Y. Apr 60. Ck>ntract W-31-
109-Eng-52. ^p. Order from OTS. 50 cents.
KAPL-1957
Availability of niAium (Columbium), by C. T. Sims.
c Power Laboratory, Schenectady,
iry
lAt
Knolls Atomic
N. Y. Mar 60
Order from LC '
Ckjntract W-31-109-Eng-52. 8p.
Mi $1.80. ph$1.80.
KAPL-M-CTS-1
A study of die handneas of several USMC Inconel tube
welda, by W. A. Owczarski. Knolls Atomic
Power Laboratbry, Schenectady, N. Y. Jan 60.
14p. Order fri«n LC. Mi $2. 40, ph $3i 30.
KAPL-M-WAO-4
Oxidation of metals subjected to a linear temperature
increase: Cubic and logarithmic laws, by J. T.
Waber. Loe Alamos Scientific LaboFatory, Los
Alamoe, N. Mix. July 55. Contract W-7405-
eng-36, 12p. Order from LC. Mi $2.40,
ph$3.30. 1 LA-1929
Caustic stress
rroeion of type 347 stainless steel,
by G. C. Wheetler andE. Howells. Knolls
Atomic Power laboratory, Schenectady, N. Y.
and Babcodc an|d Wilcos Ccnnpany, Research
Center, Alliance, Ohio. [195?]. 14p. Order
from LC. Mi $2.40, ph $3. 30. M-6911
SNAP 1-
$2.40, ph$3.:
id mercury loop tests of selected
loop
materiaTF. PeHod covered: January 1957--June
1959, by J. Mcdrew. Martin Company, Nuclear
Division, Balti|nore, Md. Mar 60. Contract AT
(30-3)-217. 4dp. Order from LC. Mi $3. 30,
ph$7.80. 1 MND-P-2128
4dp.
SNAP- 1 A fuel cor» materials development summary,
riod covered!: July 1959 through June 1960.
irtin Company, Nuclear Division, Baltimore,
Md. 1960. Contract AT(30-3)-217. 87p. Order
from LC. Mi $5.40, ph $15.30. MND-P-2349
An experimental study of intermetallic diffusion In
large temperaoire gradients, by C. J. Meechan.
Atomics Intemiatlonal. A Division erf North Ameri-
can Aviation, Inc., Canoga Park, Calif. Dec 60.
Contract AT(11(
OTS. 50 cents
-l)-GEN-8. 17p.
Order from
NAA-SR-5357
Kinetics of hot pressing, by J. D. McClelland.
Atomics International. A Division of North
American Aviation, Inc. , Canoga Park, Calif.
Jan 61. Contract AT(ll-l)-GEN-8. 21p. Or(fcr
from OTS. 75 centa. NAA-SR-5591
Survey of mechanical properties data of ceramic
materials, by R. dhang. Atomics International
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Mar 57. I6p. Order from
LC. Mi $2.40, ph$3.30.
NAA-SR -Memo- 1887
Thermal cycling tests on U-IO w/o Mo for the ORNL
fast burst reactor, by B. Minushkin. Nuclear
Development Corporation of Anfierlca, White
Plains, N. Y. July 60. 26p. Order from LC.
Ml $2.70, ph $4.80. NDA -Memo- 2 136- 2
Automatic de-canner--SRE fuel elernents, by H.
Schlein. Atomics International. Division of North
American Aviation, Inc., Canoga Park, Calif.
Oct 58. 5p. Order from LC. Ml $1.80, ph$1.80.
NAA-SR-Memo-3132
•4--
Evaluarion of AI^ M-486 welded sheet, by B. N.
Brlggs. Atomics International. Division of North
American Aviation, Inc. , Canoga Park, Calif.
Dec 59. 5p. Order from LC. Mi $1.80,
ph$1.80. NAA-SR-Memo-4836
Zirconium corrosion in polyphenyls: A literature
survey, by F. L. Cochran. Atomics Internatlootl
Divisicn of North American Aviation, Inc. ,
Canoga Park, Calif. Jan 60. 27p. Order from
LC. Mi $2.70. ph$4.80.
NAA-SR-MenK)-4847
Fabrication of OMR cylindrical prototype fuel ele-
ment to be Irradiated in the OMRE, by E. Garren.
Atomics International. Division of North Ameri-
can Aviatlnn, Inc. , Canoga Park, Calif. Jan 60.
22p. Order from LC.
Mi $2.70, ph$4.80.
NAA-SR-Memo-5007
The effect (rf open-air heating (1050^) on the pro-
perties of z'ircaloy-2, by R. K. Wagner. Atoroia
International. Division of North American Avia-
tion, bic. , Canoga Park, Calif. Mar 60. Up.
Order from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-5043
U3Si2^1 evaluation. Parti. Oxidation character-
istics, by N. R. Koenig. Atomics International
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Apr 60. 9p. Order from
LC. Ml $1.80, ph$1.80. NAA-SR-Memo-5199
496
Stability of the high temperature beta phase in beryl-
"llum and beryllium alloys, by S. H. Gelles and
j; J. Pickett. Nuclear Metals, Inc. , Concord,
Mass. Oct 60. Contract AT(30-1)-1565. 44p.
Order from OTS. $1.00. NMI-1218
liotopic Interchange In dispersion fuels, by D. S.
— Kneppel. Nuclear Metals, Inc., Concord, Mass.
Oct 60. Contract AT(30-1)- 1565. 47p. Order
from OTS. $1.00. NMI-1232
Development of plutonium bearing fuel materials.
Progress report for January l"through March~31,
1950 Nuclear Materials and Equipment Corpora-
HonTApollo, Pa. 1960. Contract AT(30-l)-2389.
36p. Order from LC. Ml $3. 00. ph $ 6 30.
NUMEC-P-20
Fuel cycle development program quarterly progress
report for October 1 to December 31, 1^59."
Clin Mathieson Chemical Corporation, Metal lurgi -
cal Laboratories, New Haven, Conn. Jan 60.
Contract AT(30-l)-2374. 44p. Order from LC.
Ml^$3.30, ph$7.80. NYO-2685
X-ray n^easurement of grain size, by B. E.Warren.
Massachusetts Institute of Technology, Cambridge,
Mass. June 60. Contract AT(30-l)-858. 7p.
Order from LC. Mi $1 . 80, ph $1 . 80.
NYO-4836
ImperfSctions in ntetals. The early stages of plastic
deformation in ccypier. Technical report no. 247
by D. A. Thomas and B. L. Averbach. Massa-
chusetts Institute of Technolog*/, Cambridge,
Mass. May 58. 29p. Order from LC. Mi $2. 70,
ph$4.80. NYO-70ei
Fuel element developnr>ent program for the pebble
bed reactor. Quarterly progress report for Nov-
ember 1, 1959 to January 3l7 I960. Sanderson
and Porter, New York, N. Y. Jan 60. Contract
AT(30- 0-2378. 26p.
ph$4.80.
Order from LC. Mi $2. 70,
NYO-9057
Fuel element development program for the pebble
bed reactor. A topical report on subsurface"
coatings for fueled graphite spheres, by Sander-
son and Porter, New York, N. Y. June 60. Con-
tract AT(30-l)-237d. Up. Order from OTS.
50 cents. NYO-9060
rt for
etallurgy division quarterly progress report foi
period ending October 31, 1952. by W. H.
Bridges. Oak Ridge National Laboratory, Oak
Ridge, Tenn. 1952. Decl. with deletions Octo-
ber 29, 1959. Contract W-7405-eng-26. 48p.
Order from LC. Mi $3. 30, ph $7. 80.
ORNL-1437(Del.)
July 54. Decl. with deletions November 12,
1959. Contract W-7405-eng- 26. 114p. Order
from LC. Mi $6.00, ph $18. 30.
ORNL-1729(DeI.)
widi deletions November 13, 1959. Contract W-
7405-eng-26. 209p. Order from LC. Mi $9.30
ph $35.70. ORNL-2080(Del.)
Corrosion resistance oi various ceramics and cer-
mets to liquid metals, by W. H. Cook. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
June 60. Contract W-7405-eng-26. 27p. Order
from LC. Mi $2.70, ph $4.80. ORNL-2391
Papers presented at ANP materials rraeeting Novem-
ber 16-18, 1954, Wri^t Air DevelojMnent Center.
Dayton, Ohio. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Mar 59. Decl. May 9, 1960.
Contract W-7405-eng- 26. I68p. Order from LC.
Ml $7.80, ph$25.80. ORNL-2685
Fuel cycle development program. Quarterly prog'
ress report for May 1, 1^59 to August 1, 1959^
National Carbon Company, Fostoria, Ohio.
Sep 59. Contract AT(40-l)-2560. 15p. Order
from LC. Mi $2.40, ph $3.30. ORO-244
Fuel-bearing fiberglas in aluminum base fuel ele-
ments Third quarterly report for November 1.
1959 to January 31, 1960, by R. H. Baskey.
Clevite Corporation, Mechanical Research Divi-
sion, Cleveland. Ohio. Feb 60. Contract AT
(40-1)- 2557. 20p. Order from LC. Mi $2.40,
ph$3.30. ORO-273
Fuel bearing fiberglas in aluminum base fuel ele-
ments. Monthly progress letter no. 10 for March
1 1960 to March 31, 1960, by R. H. Baskey.
Clevite Corporation, Mechanical Research Envi-
sion, Cleveland, Ohio. Apr 60. Contract AT
(40-l)-2557. 4p. Order from LC. Mi $1.80,
ph$lf80.
ORO-274
Synthesis and fabrication of refractory uranium com-
pounds. Monthly progress report "no. 6 for Janu-
ary through January 31, 1960, by K. M. Taylor
and others. Carborundum Ccunpany, Niagara
Falls, N. Y. Feb 60. Contract AT(40-l)-2558.
7p. Order from LC. Ml $1.80. ph $1.80.
ORO-275
497
Fuel bearing fiberglas in aluminum base fuel ele-
meats. Monthly progress letter no. 13 for the
period June 1, 'l9y to June 30, 1960. by R. H.
■Mkey. Clevike Corporation, Mechanical Re-
search Division, Cleveland, Ohio. July 60.
Contract AT(44)-l)-2557. 5p. Order from LC.
Mi $1.80, ph 11.80. ORO-304
spet
iJra
1
Diapersion type materials for fuel elements. Part II.
Jranium carbide and uranium sulfide dispersion
materials, by I. Sheinhartz. Sylvania-Corning
Nuclear Corpofration, Bayside, N. Y. Mar 59.
Decl. May 13. 1 1960. Contract AT-30-(ll-GEN-
366. 16p. Orjler from LC. Mi $2.40, ph $3. 30.
SCNC-273
Ortier
Isoetatic pressing of UOo in high temijerature metals
: pressing of UOo
Sneinhartz and f.
ipei
5^
by I. ^einhart Andf. Fugardi. Sylvania-Corning
Nuclear Corporation, Bayside, N. Y. Sep 60.
Contract AT-30-1-GEN-366, 17p. Order from
GTS. SOcentfe. SCNC-312
Properties of refifactory nuclear materials, by M.
Comstock. Brpokhaven National Laboratory,
Upton, N. Y. [Feb 60. 18p. Order from LC.
Mi $2. 40, phis. 30. TID-3906
The corroaion of HyMu 80 fluorinators, byF.W.
Fink. Battelle Memorial Institute, Col umbus ,
28p. Order from LC. Ml $3.00,
TID-5935
Ohio. May 60,
ph$6.30.
Measurement of ejlectric field gradients in dilute
silver alloys by angpjlar correlation techniques.
Thesis, by C. A. Giffels. Carnegie Institute of
Technology, Pktsburgh, Pa. May 60. Contract
AT(30-1)-1830
ph$lS.30
91p. Order from LC. Mi $5.40.
TID-6069
Informal letter prjogress report for May 1960.
Sylvania-Cornilng Nuclear Corporation, Bays ide ,
N. Y. 1960. lOp. Order from LC. Mi $1.80.
ph$1.80. 1 TID-6084
A compilation of data on the effect of high -pressure
hyckogen on the ntechanical pr(»erties of metals,
by H, StrombeJ-g. University of California,
Lawrence Radijation Laboratory, Uvermore,
Calif. Sep 58. Contract W-7405-eng-48. I6p.
Or^rfromLd. Mi $2.40, ph $3.30.
Crystallography (
beryllides, by
UCRL-5350
phy ojf some of the transition element
;ryllides, bylA. Zaikinaand D. E. Sands. Diii-
versityoT California, Lawrence Radiation Labora-
tory, Livermo e, Calif. May 60. 6p. Order
from LC. Mi H.80, ph $1.80. UCRL-5988-T
Some properties of vanadium group beryllides, by
^rS
O. H. ICriborian. University of California.
Lawrence Radiation Laboratory, Uvermore,
Calif. May 60. 9p. Order from LC. Mi $1.80,
ph$1.80. UCRL-5989-T
Phase diagrams of zirconium-beryllium and related
systetns, by R. G. Bedford. University of Cali-
fornia, Lawrence Radiation Laboratory, Liver-
move, Calif. May 60. 7p. Order from LC.
Mi $1.80, ph $1.80. UCRL-5991-T
Fission fragment damage to crystal structures, by
R. M. Berman and others. Westinghouse Elec-
trlc Corporation, Bettis Atomic Power Labora-
tory, Pittsburgh, Pa. Feb 60. Contract AT-ll-
l-GEN-14. 32p. Order from LC. Mi $3.00,
ph$6.30. WAPD-T-1125
Zirconium highlights. Westinghouse Electric Corpor-
atlon, Bettis Atomic Power Laboratory, Pittsburgb,
Pa. Mar 60. Contract AT-11-l-GEN- 14. 26p.
Order from LC. Mi $2. 70, ph $4. 80.
WAPD-ZH-23
Uranium alloy newsletter, number 2. by D. W.
Li Hie. Division of Research. AEC. Oak Ridge,
Tenn. Apr 53. Decl. with deletions December
1, 1959. 47p. Order from LC. Mi $3. 30,
ph $7 . 80. WASH- 1 23 (Del. )
Uranium alloy newsletter no. 3. byP.W. Lillie.
Division of Research. AEC. Oak Ridge, Tenn.
May 53. Decl. October 7. 1959. 44p. Order
from LC. Mi $3. 30, ph $7 . 80. WASH-124
Uranium alloys newsletter no. 6, by D. W. Lillie.
Division of Research. AEC. Oak Ridge, Tenn.
Feb 54. Decl. November 30, 1959. 61p. Order
from LC. Mi $3.90. ph $10.80. WASH- 153
Thermoelectric nuclear fuel element progress re-
port no. 23, by G. R. Kilp and others" Westing-
house Electric Corporation, Atomic Power Depart-
ment, Pittsburgh, Pa. June 60. Contract AT
(30-3)-500. 27p. Order from LC. Mi $2.70,
ph$4.80. WCAP-1580
The effect of casting variables and heat treatment
on the tensile properties of lead-0.02 to 0. 10
weight per cent calcium alloy, by A. B. Townsend.
Union Carbide Nuclear Company. Division of
Union Carbide Corporation. Y-12 Plant. Oak
Ridge, Tenn. Dec 60. Contract W-7405-eng-
26. 25p. Order from OTS. 50 cents.
Y-1307
j.\ J'-'
jn;M-
496
Meteorology
Tte U. S. Weather Bureau - Sandia Corporation
"correlations of wind), by M. K. Weston. Sandia
Corporation, Albuquerque, N. Mex. Nov 60.
58p. Order from OTS. $1.75.
SCIM-211-60-51
Nucleor Explosions — ^Peaceful
Applications
Supplementary^report on geologic investigations in
support of Phase II, project Chariot in the vicinity
of Cape Thompson, Northwestern Alaska, by R.
Kachadoorian and others. Geological Survey,
Washington, D. C. June 60. 33p. Order from
LC. Mi$3.00,^ph $6.30.
TEI-764
Application of nuclear explosions as seismic sources,
by C. W. Johnson. University of California.
Lawrence Radiation Laboratory, Uvermore,
Calif. July 60. 5lp. Order from OTS. $1.50.
UCRL-6030-T
Project Cowboy: Fracturing of rock salt by a con-
Mined high explosive, byN.M. Short. University
(A California, Lawrence Radiation Laboratory,
Uvermore, Calif. Nov 60. Contract W-7405-
eng-48. 60p. Order from OTS. $1.50.
UCRL-6054
The system H2O-NCCI at elevated temperatures and
pressures, by S. Sourirajan and G. C. Kennedy.
University of California, Lawrence Radiation
Laboratory. Livermore, Calif. Nov 60. Con-
tract W-7405-eng-48. 45p. Order from OTS.
$1.00. UCRL-6175
Distribution of radioactivity from a nuclear excava
tion. by R. E. Batzel. University of California,
Lawrence Radiation Laboratory. Livermore,
Calif. Oct 60. Contract W-7405-eng-48. 18p.
Order from OTS. 50 cents. UCRL-6249-T
Particle Accelerators and High-Voltage
Machines
Coemotron magnet power supply, by G. K. Green. |n
brookhaven National Laboratory, Upton, N. Y.
July 54. 32p. Order from LC. Mi $3.00,
ph $6. 30. BNL-4632
Orbit conalderations in the linear accelerator, by
L. Smith. Brookhaven National Laboratory,
Upton, N. Y. May 56. 31p. Order from LC.
Mi $3.00, ph$6.30. BNL-4635
Long-term vertical pile load tests, by J. H. Lan-
caster. Broc*haven National Laboratrry, Upton,
N. Y. May 56. 5p. Order from LC. Mi $2.40,
ph$3.30. BNL-4636
Long-term vertical pile-load tests, by J. H. Lan-
caster. Brookhaven National Caboratory, Upton,
N. Y. July 56. 5p. Order from LC. Mi $1.80,
ph$1.80. BNL-4639
Beat factors and stopband widths, by E. D. Courant.
Brookhaven National Laboratory, Upton, N. Y.
Jan 57. 13p. Order from LC. Mi $2.40,
ph $3. 30. BNL-4641
Transient response of AGS magnet, by H. S. Snyder.
Brookhaven National Laboratory, Upton, N. Y.
Jan 57. 5p. Order from LC. Mi $1.80,
ph$1.80. BNL-4642
Beam observation electrodes for the AGS, by E. C.
Raka. Brookhaven National Laboratory, Upton,
N. Y. Mar 57. 9p. Order from LC. Mi $1.80,
ph$1.80. BNL-4643
Linac tuning system, by J. D. Klesling. Brookhaven
National Laboratory, Upton, N. Y. July 57. 17p.
Order from LC. Mi $2. 40, ph $3. 30.
BNL-4645
Injection optical system, by H. N. Brown. Brook -
haven National Laboratory, Upton. N. Y. Aug 57.
I8p. Order from LC. Mi $2. 40, ph $3. 30.
BNL-4646
Magnet support system, by V. J. Buchanan. Brook-
haven National Laboratory, Upton, N. Y. Jan 58.
4p. Order from LC.
Mi $1.80, ph$1.80.
BNL-4647
Long-term vertical pile load tests, by J. H. Lancas-
ter. Broc^chaven National Laboratory, Upton,
N. Y. Jan 58. 3p. Order from LC. Mi $1.80,
ph$1.80. BNL-4649
Ripple filtering for amain AGS magnet generator, by
J. G. Cottingham. Brookhaven Nati '
tory, Upton, N. Y. June 58.
LC. Mi $2.40, ph$3.30.
Jational Labora-
4p. Order from
BNL-4650
499
Modes in long canities , byj. D. Klesllng. Brook-
haven National Laboratory, Upton, N. Y. Apr
59. 6p. Ord^r from LC. MI $1.80. ph $1.80
HNL-4652
Tentative plana rtremerimental equipment at the
AGS, by R. L, Cool and E. D. Courant. Brook -
haven National Laboratory, Upton, N. Y. Apr
59. lip. Order from LC. Mi $2.40, ph $3. 30.
BNL-4653
The focal properyea of certain quadrupole lensea.
by J. P. Blewett. Brookhaven. National Labora-
tory. Upton, N. Y. May 59. 32p. Order from
LC. Mi $3.00, ph$6.30. BNL-4654
Allmment of AGfl linear accelerator tank, by J. W.
Hart. Brookhiven National Laboratory, Upton.
N. Y. May 59. 6p. Order from LC. Mi $1.80.
ph$1.80. 1 BNL-4655
59. 6p.
The dynamic K- meter, by J. P. Palmer. Brookhaven
National Laboratory, Upton, N. Y. June 59.
23p. Order fitom L^- Ml $2.70. ph $4.80.
BNL-4657
Application erf the linear accelerator for production
of intense prooon beams at 10 BEV. II. Neutrino
beams, by J. j, Blewett. Brookhaven National I
Laboratory. Ubton. N. Y. Nov 59. 5p. Order
from LC. Mi 51.80. ph $1.80. BNL-4660
Interim data on tHe stability of AGS foundations, by
O. S. Reading j Brookhaven National Labora tory .
Upton, N. Y. JJan 60. 9p. Order from LC.
Ml $1.80, ph$1.80. BNL-466I
Performance estimates for injector cyclotrons, by
H. G. Blosser and M. M. Gordon. Michigan
State University, East Lansing, Mich. Sep 60.
Contracts AT(il-l)-384 and AT(ll-l)-872. 37p.
Order from OTS. $1.50. MURA-593
.T(ll-l)-3
OTS. $1.
Convergence ratejof the nine-point extrapolated
Liebmann algot-ithm, by H. H Denman. Kfid-
western Universities Research Association.
Madison, Wis. Sep 60. Contract AT(1 1-1)- 384.
12p. Order from OTS. 50 cents. MURA-594
ulsed
Hlg^ current pulsfed electron accelerator, by N.
Chri8tolflo(B. University of California, Lawrence
Radiation Laboratory, Livermore, Calif. June
60. Contract W-7405-eng-48, 5p. Order from
LC. Mi$l.80^ ph$1.80. UCRL-5951-T
Bevatron ope ra tioti and deve lopment . XXVI May,
June, July 196( , by W. D. Hartsougir University
of California, Lawrence Radiation Laboratory,
Berkeley, Calif. Sep 60. Contract W-7405-eng-
48. 1^. Order from OTS. 50 cents.
UCRL-9418
Physics
Physics division summary report. Argonne National
Laboratory, Argonne, 111. June 60. Contract W-
31-109-eng-38. 77p. Order from LC. Mi $4. 50,
ph$12.30. ANL-6169
Table of energy levels of asymmetric even nuclei
with beta- vibration- rotation interaction, by P. P.
Day and others. Argonne National Laboratory,
Argonne. 111. Nov 60. Contract W- 31- 109-eng-
38. 22p. Order from OTS. 50 cents.
ANL-6220
A study of the variation of steam velocity in vertical
boiling channels, by General Nuclear Engineering
Corporation, Dunedin, Fla. Argonne National
Laboratory, Argonne, 111. Nov 60. Contract
W-31-109-eng-38. 65p. Order from OTS.
$1.75. ANL-6251
A pulsed neutron source technique, by R. Siems and
M. Melissaropoulos. Argonne National Labora-
tory, Argonne, 111. Nov. 60. Contract W-31-
109-eng-38. 32p. Order from OTS. 75 cents.
AN L- 6254
ITie effect erf the liquid viscosity in two-phase, two-
component flow, by M. J. Fohrman. Argonne
National Laboratory, Argonne, 111. Nov 60.
Contract W- 31- 109-eng- 38. 96p. Order from
OTS. $2.25. ANL-6256
7405-eng-92. 29p.
levelg. associated w i th
and ^Er^^yby
Argonne Natioo-
al Laboratory, Argonne. 111. Jan 61. Contract
W-31 -109-eng- 38. 135p. Order from OTS.
$2.50. AN L- 6270
Study of the nuclear energy levt
the decay of f^fPy]^. jsqJ"^
R. G. Helmer and S. B. Burson
Dynamic analysis of a pneumatic amplifier, by B.
Kaplan and J. A. Delaney. General Electric
Company, Aircraft Nuclear Propulsion Depart-
ment, Cincinnati, Ohio. July 60. Contracts
AT(11 -1)- 171 and AF33(600)- 38062. 47p. Order
from OTS. $1.25. APEX-576
A simple experimental method for determining ef-
fective threshold energies and cross sections, by
R. G. Jung and others" Battelle Memorial Insti-
tute, Columbus, Ohio. Dec 60. Contract W-
500
Order from OTS. 75 cents.
BMI-1486
Nuclear characteristics of cylindrical breeder re-
actors containing thorium in pellet form, by D. R.
Vondy. Oak Ridge National Laboratory, Oak
Ridge, Tenn. May 60. Contract W-7405-eng-
26 17p. .Order from LC. Mi $2.40. ph$3.30.
CF-60-5-11
Design procedure for a minimum weight space
— radiator, by R. J. Hefner. Oak Ridge National
laEoratory, Oak Ridge. Tenn. Aug 60. 26p.
Order from LC. Mi $2.70, ph $4.80.
CF-60-8-21
Plasma density in IX:X as a function of ARC density,
by E. D. Shipley and T. K. Fowler. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Aug 60.
fo. Order from LC. Mi $1.80. ph $1.80.
CF-60-8-22
Fuel meltdown experiments, by J. R. Seaboch and
J. W. Wade. Du Pont de Nemours (E. I.) i Com-
pany. Savannah River Laboratory. Aiken. S. C.
Oct 58. Decl. May 12. 1960. Contract AT(a7-
2)-l. 42p. Order from LC. Mi $3. 30. ph $7. 80.
DP-314
Neutron thermalization in water, by M. Nelkin.
General Atomic Division. General Dynamics,
Corporation. San Diego, Calif. Jan 60. Contract
AT(04-3)-167. Up. Order from LC. Mi $2.40,
ph$3.30. GA-1180
B-specirum code or thermali/ation, by H. D. Brown,
Jr. and M.S. Nelkin. General Atomic Division.
General Dynamics Corporation, San Diego, Calif.
(19571. Contract AT(04-3)-l67. Up. Order
from LC. Mi $2.40, ph $3. 30. GAMD-1176
Z plant radiation study interim report no. 5. Part II.
Data on gamma shielding of special plutonium
samples by H. A. Moulthrop. General Electric
Company, Hanford Atomic Products Operation,
Richland. Wash. Oct59. Contract W-31-109-
eng-52. 103p. Order from LC. Mi $5.70.
ph$l6.80. HW-61755(Pt. 2)
lers.
Nuclear physics research quarterly report April,
May June 1960, by J. L. Carter, Jr. and oth<
Hanford Atomic Products Operation. Richland.
Wash. July 60. Contract AT(45-1)- 1350. 3^.
Order from OTS. $1.00. . HW-66215
An
integral mediod for identifying net
spectra, by R. G. Nisle. Phillips
Company, Idaho Falls. Idaho. De
neutron flux
Petroleum
Dec 60. Contract
' AT(lO-l)-205. 86p. Order from OTS. $2.00.
IDO-16612
Tensile properties of yttrium -titanium and yttrium -
zirconium alloys, by D. W. Bare and others.
Iowa State University of Science and Technology,
Ames Laboratory, Ames, Iowa. Dec 60. Con-
tract W-7405-eng-82. 20p. Order from OTS.
50 cents. IS-240
Summary of equations for effect of ship attitude and
ship motion on primary coolant system^ flow rates,
by H. E. Stevens, Jr. Knolls Atomic Power
Laboratory, Schenecudy. N. Y. Feb 60. Con-
tract W-31-109-Eng-52, bp. Order from LC.
Mi $1.80, ph $1.80. KAPL-M-HS-U
Hexf it. a data reduction code for cyclically counted
samples, by S. Weinstein and others. Knolls
Atomic Power Laboratory. Schenectady, N. Y.
May 60. Contract W-31-l09-Eng-52. 7p.
Order from LC. Ml $1 . 80, ph $1 . 80.
KAPL-M-SW-1
The spherical-harmonic method and its application
to one velocity neutron problems, by R. J.
Glauber. Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. Nov 44. Decl. April 27,
1960. Contract W-7405-eng-36. 42p. Order
from LC. Mi $3.30, ph $7.80. LA-174
Further investigation of sponuneous fission in
plutonium. by G. W. Farwell and others. Los
Alamos Scientific Laboratory. Los Alamos.
N. Mex. Apr 46. Decl. December 18, 1959.
59p. Order from LC. Mi $3. 60, ph $9. 30.
LA-490
.Emission probabilities of prompt neutrons from
** spontaneous and neutron -inckiced fission, by R.B.
L^chman. Los Alamos Scientific Laboratory,
Los Alamos, N. Mex. Dec 54. Decl. May 5.
1960. Contract W-7405-Eng-36. 41p. Order
fromLC. Mi $3.30, ph $7.80. LA-1863
The production of ions at meuUic surfaces bOTnbard-
ed by energetic ions, by W. T. Leland and R.
Olscn. Vjm Alamos Scientific Laboratory, Los
Alamos, N. Mex. Dec 59. Contract W-7405-
eng-36. 81p. Order frcKn LC. Ml $4.80,
ph$13.80. LA-2344
Dynamics of compressible fluids. byF.H. Harlow.
University of California. Los Alamos Scientific
Laboratory, Los Alamos, N. Mex. Apr 60.
Contract W'7405-ENG-36. 200p. Order from
OTS. $3. Op. LA-2412
501
\
Solution of the initial value problem for the lineariz-
ed multi-veloqity transport equation with a slab
feometry, by b, H. Pimbley. Los Alamos
clentific Laboratory, Los Alamos, N. Mex.
Jan 57. Contract W-7405-eng- 36. I28p. Order
from LC. Mi $6. 30. ph $19.80. LAMS-2116
Period covered: February I, 1957 to June
Hypersonic plag]
University of
Laboratory,
Contract W-7'
OTS. 50 ceatl
thermocouple, by T. Cotter,
ilifornia, Los Alamos Scientific
Alamos, N. Mex. Nov 60.
)5-ENG-36. 12p. Order from
LAMS-2481
Cumulative listing of project Matterhorn reports and
publications. Princeton University, Project Mat-
terhorn, Piindeton, N. J. July 60. Contract AT
(30-l)-1238. .9p. Order from LC. Ml $2. 40.
ph $3. 30. MATT- 1 (2nd Ed. )
Snap I mercury boiler developnrtent, January 1957 to
Snap 1 power conversion system turbine developmeK.
_ __ " _ _ _~ ^^""y ^' ^^^Z to lune~5o;
1959, by D. C, Reemsnyder and E. M. Szanca.
Thompson Ramo Wooldridge Inc. , New Devices
Laboratories, Cleveland, Ohio. June 60. Con-
tract AT(30-3)-217. 54p. Order frcm LC.
Ml $3. 60. ph$9.30. MND-P-2376
Snap I power conversicn system alternator develop-
ment. Period covered: February 1, 1957"to
June 30, 1959. by H. J. Morgan. Thompson
Ramo Wooldridge Inc., New Devices Labora-
tories. Cleveland, Ohio. June 60. Contract
AT(30-3)-217. 43p. Order from LC. Mi $3.30,
ph$7.80. MND-P-2377
ap 1 I
T959:
%
Sna
^ ^ Jicha and J. J. Keenan. Martin
Company, Nudlear DivisionyBaltimore. Md.
June 60. Contract AT(30-3f-217. I02p. Order
from OTS. $2.25. MND-P-2309
I
Interim report ori safety procedures for the task 2
thermoelectric generator, by L. T. Klein.
Martin Compa|iy, Nuclear Division. Baltimore.
Md. Mar 60. ; Contract AT(30-3)-217. 57p.
Order from op. $1.50. MND-P-2335
ID I power conversion system putpp development.
Period covered: February l._i957 to June 30i
1959, by E. S. Kovalcik and D. C. Reemsnyder,
June 60. Contract AT(30-3)-217. 59p. Order
from LC. Ml $3. 60, ph $9. 30. MND-P-2378
Snap 1 power conversion system bearings deyelop-
ment. Period covered: February 1, 1957 to
June 30, 1959, by R. Meredith and others.
ThcMTipson Ramo Wooldridge Inc. , New Devices
Laboratories. Cleveland. Ohio. June 60. Con-
tract AT(30-3)-217. 68p. Order from LC,
Ml $3.90, ph$10.80. MND-P-2379
100-watt curium
tor - - concepts il deal;
f
Sna:
242 fueled thermoelectric genera-
SNAP subtask 5.7 final
^
report, by^. f. WeddellandJ. Bloom. Martin
Company, Nuclear Division, Baltimore, Md.
May 60. Contract AT(30-3)-217. 80p. Order
from OTS. $2.00. MND-P-2342
ID 1 power conversion system control development.
Period covered: February 1, 1957 to June 30i
1959, by W. E. I>auterman and others. Thomp-
son Ramo Wooldridge 'nc . , New Devices Labor-
atories, Cleveland, Ohio. June 60. Contract
AT(30-3)-217. 50p. Order from LC. Mi $3.30,
ph$7.80. MND-P-2380
Snap I power conversion system condenser -radiator
anap 1 power conversion system conoenser-raaiator
Snap 1 radloisoto^-fxieled turboelectric power con- development. Period covered: February 1, 1957
version system summary, January 1957 to June to April 15, 1959, by R. J. Kiraly and D. C.
?yi . ..- r ^
1959, by P. J. 'Pick. Martin Company, Nuclear
Division. Baltimore. Md. June 60. Contract
55p. Order from OTS. $1.50.
MND-P-2350
AT(30-3)-217.
Preliminary safety analysis low power cerium- 144
enerator, by Martin Company, Nuclear Division,
altlmore. M4. June 60. Contract AT(30-3)-
217. 33p. Oikler from LC. Mi $3. 00. pb $6. 30.
MND-P-2363
Snac
OAlei
ipl- power conversion system development.
Period covered: February 1, 1957 to June 30,
1959, by R. C^ Biering and others. ThtHnpson
Ramo Wooldri^e Inc.. New Devices Laboratory
Cleveland, Ohto. June 60. Contract AT(30-3)-
217. 68p. Oader from LC. Ml $3. 90.
ph $10.80. MND-P-2375
Aprl
Reenrisnyder. Thompson Ramo Wooldridge Inc..
New Devices Laboratories, Cleveland, Ohio.
June 60. Contract AT(30-3)-217. 47p. Order
from LC. Mi $3.30, ph $7.80. MND-P-2381
Snap I power conversion system materials develop-
ment. E'eriod covered: February 1, 1957 to
June 30, 1959. by V. F. Hambor and J. J. Owen».
Thompson Ramo Wooldridge Inc. , New Devices
Laboratories, Cleveland, Ohio. June 60. Con-
tract AT(30-3)-217. 38p. Order from LC.
Mi $3.00, ph$6.30. MND-P-2382
Snap III Final performance test sumrnary. by J. D.
Long. Maitin Company, Nuclear Division,
Baltimore, Md. Aug 60. Contract AT(30-3)-2l7.
57p. Order frran LC. Mi $3. 60. ph $9. 30.
MND-P-2398
502
An evaluation of flux flattening in SCR cores, by
— J{^ A. Axford. Atomics International. A Divi-
sion of North American Aviation, Ire. . Canoga
Park. Calif. Dec 60. Contract AT(11-1)-GEN-
8 67p. Order from OTS. $1.75.
NAA-SR-4531
Preliminary graphite sample analysis utilizing the
— L-77 V.O reactor, by R. P. Johnson. Atomics
International. RTvision of North American Avia-
tion, Inc.. Canoga Park, Calif. May 59. Up.
Order from LC. Ml $2.40, ph $3. 30.
NAA-SR- Memo- 3425
A propoeed Monte Carlo method for computing the
" basic lattice parameters and the space dei«ndent
neutron spectra, by G. D. Joanou. Atomics In-
ternational . Division of North American Avia-
tion, Inc. , Canoga Park, Calif. Dec 59. 28p.
Order from LC. Mi $2.70. ph $4.80.
NAA-SR-Memo-4705
The technology and applications of large fission
product beta sources. Quarterly report for
period ending June 30, 1960. Radiation Applica-
tions Inc. . New York, N. V. 20p. Contract AT
(30-l)-2186. 20p. Order from LC. Ml $2.40,
ph$3.30. NYO-2501
Measurement of the spin of arsenic^" by the atomic
beam method, by R. L. Chrlstensen. Princeton
University, Palmer Physical Laboratory, New
York, N. Y. Aug 57. Contract AT(30-l)-937.
206p. Order from LC. Mi $9. 30, ph $31.80.
NYO-8016
The spectrum of a neutron transport operator, by
R. N. van Norton. New York University, Atomic
Energy Commission Computing and Applied
Mathematics Center, New York, N. Y. June 60.
Contract AT(30-1)- 1480. 37p. Order from LC.
Mi $3. 00, ph $6. 30. NYO-9085
Kii«matics of nuclear reactions calculated with the
IBM-704 computer, by B. D. Williams. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
(ndj. Contract W-7405-eng-26. 8p. Order
from 015. 50 cents. ORNL-2963
Dissociation of H2"*" by hydrogen, by H. Postma and
D. P. Hamblen. Oak Rid^ National Laboratory,
Oak Ridge, Tenn. Nov 60. Contract W -7405-
eng-26. 8p. Order from OTS. 50 cents.
ORNL-2966
Low-temperature thermoluminescence of the mmma-
irradiated amino acids and proteins, by J. G.
Carter. Oak Ridge National Laboratory, Oak
Ridge, Tenn. [ndJ. Contract W-7405-eng-26.
60p. Order from OTS. $1.75. ORNL-2970
The depolarization of negative MU mesons, byR.A.
Mann. Oak Ridge National Laboratory, Oak
. Ridge, Tenn. [nd]. Contract W-7405-eng-26.
I43p. Order from OTS. $2,75. ORNL-2990
Neutron
irt for
utron physics division annual progress repo:
feriod ending September 1, 19607 by E. P.
lizard and others. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. 1960. Contract W-
7405-eng-26. 325p. Order from OTS. $4.00.
ORNL-3016
Solid state division annual progress report for period
ending August 31 . 1960, by D. S. Billlngton and
J. H. Crawford, Jr. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. [nd]. Contract W-7405-
eng-26. 130p. Order from OTS. $2.50.
ORNL-3017
Maximum missile ranaps from cased explosive
' charges, by R. H. Bishop. Sandla Corporation.
Albuquerque. N. Mex. July 58. 56p. Order
from LC. Mi $3. 60. ph $9. 30.
SC-4205(TR)
Leakage from pressurized containers dur
term storage, by A. N. Blackwell. San(
%.
.ge. ,
poration. Albuquerque. N. Mex. Jan 61. Con-
tract AT(29-l)-789. 23p. Order from OTS.
50 cents. SCTM-29-60-81
The use of pressure bars and plates for the Investl-
gatlon of shock waves from electrically explo<i(e3
wires, by W. J. Halpln and R. E. Hendricks^
Sandla Corporation. Albuquerque. N. Mex.
Feb 60. 31p. Order from LC. Mi $3.00,
ph $6. 30. SCTM-39-60-5I
Sampled data systems --a tutorial, by R. E. Stephen-
toa. Sandla Corporation. Albuquerque. N. Mex.
Nov 60. 23p. Order from OTS. 75 cents.
SCTM- 334-60-24
Gray body radiation exchan
J. A. Wiebelt. Sandla
N. Mex.
50 cents
Nov 60. 8p.
in an enclosure, by
irporation, Albuquerque,
Order from OTS.
SCTT^- 358 -60-71
Tunnel diode applications to logic and pulse circuita,
by I. W. Jaimey. Sandla Corporation. Albuquer-
que, N. Mex. Dec 60. 36p. Order from OTS.
$1.00. SCTM-375-60-72
The determination of aerodynamic stability coeffi-
■ — izizzzzizzr'"^
Sandla (Corporation. A Ibuque rque,
cients from rocket fli^t test dau. by A. C.
Bustamante.
N. Mex. Jan 61.
75 cents.
Cori
19p. Order from OTS.
SCTM-384-60-71
503
Hl^- altitude wlnda over the southwestern United
Sutes for Japuary, February, and March, by
R. F. Gentzter. Sandla Corporation, Albuquer-
que, N. Mexi Nov 60. 12p. Order from OTS.
50 cents. i SCTM- 389 -60-72
Impulsive loadipg of a circular disk, byW. B.
Murfln. Sanoia Corporation, Albuquerque,
N. Mex. Jan 61.
SO cents.
15p. Order from OTS.
SC'IW-432-60-71
Coulomb disintagration of beam particles, by M. L.
Good and W.'D. Walker. University of Wiscon-
sin, Madison. Wis. [1960]. Contract AT(l 1-1)-
64. lOp. Order frcxn LC. Mi $1.80, ph $1.80.
TID-5930
DtHractlon disintegration of beam particles, by
M. L. Good and W, D, Walker. University ol
Wisconsin, Madison, Wis. [i960]. Contract
AT(ll-l)-64i 1^. Order from LC. Mi $2.40.
ph$3.30, TID-5929
Fbocodissociaticki of the Mu meson
andW
by M. E. Ebel
D. Walker. University of Wisconsin.
Madison, Wi^. [195?]. Contracts AT(1 1-1)- 30
and AT(1 1-11-64. 6p.
Mi $1.80, ph$1.80.
1
Order from LC.
TID-5931
Progress reportj and renewal proposal for a research
program in ecq)erimental and theoretical high-
energy physics, by D. Feldman and A. M.
Shapiro. Br()wn University, Providence, R. I.
June 60. Coatract AT(30-l)-2262. 18p. Order
from LC. Mi $2.40. ph $3.30. TID-6040
Energy and angular distribution of seconda^ elec-
trona produced by protons in gases, by C. E.
Kuyatt. Unitersity of Nebraslca, Lincoln, Nebr.
[19587]. Contract AT(11-1)- 35. 38p. Order
frocn LC. M|l $3. 00. ph $6. 30. TID-6103
Diamagnetic shMglding of nuclei in metals, by R.
Bersohn. Columbia University, New York, N.Y.
June 60. Coiitract AT(30-l)-2498. 6p. Order
fromLC. Mk $1.80. ph $1.80. TID-6111
i
Basic research l^ith high energy electrons and
x-rays produced by a 300 Mev synchrotron. An-
nual progres^ report. Purdue Research Founda-
tion. Lauyette, IndT June 60. Contract AT
(ll-l)-123. )44p. Order fromLC. Mi $3. 30,
ph$7.80. 1 TID-6154
The use of atomic beams as a probe for studying low
en 1,
density plasmas. Quarterly report for Marc
Fia"
1960 to July t 1960, by L. H. Fisher. New
York Univer^ty, New York, N. Y. 1960.
Contract AT(30-1)- 2397. 5p. Order from LC,
Mi $1.80, ph$1.80. TID-6158
1. Flow diagrams. 2. The estimation of signifi-
cance, by R. D. Richtnyer. New York Univer-
sity, Atomic Energy/ Commission Computing and
Applied Mathematics Center, New York, N. Y.
Apr 60. Contract AT(30-1)- 1480. 29p. Order
fromLC. Mi $2.70, ph $4.80. TID-6199
report no. 4, by B. W.
e generation. Technical
Hakki. University Ol
Studies on millimeter wave generation
?port n
Illinois. Electrical Engineering Research Labor-
-atory, Urbana, 111. Aug 60. Contract AT(1 1-1)-
392. 116p. Order fromLC. Mi $6.00,
ph$18.30. TID-6200
Research and Investigation leading to methods of
enerating and detecting radiation in the lOOTo
OOP micron range of the spectrum. Quarterly
progress reix)rtfio. 17 for March 1, 1960 lo
repo
7mn
T5ui
m
une 1, 1960, by P. D. Coleman and others.
Jniverslty of Illinois, Electrical Engineering
Research Laboratory, Urbana, 111. July 60.
Contract AT(ll-l)-392. 55p. Order from LC.
Mi $3. 60, ph$9.30. TID-6201
Nuclear forces and polarization phenomena, by G.
Breit. Yale University, New Haven, Conn. July
27p. Order from
TID-6208
60. Contract AT(30-1)- 1807.
LC. Mi $2.70, ph$4.80.
The MOssbauer effect, by H. Lustig. University of
Illinois, Urbana, 111. [1960]. 66p. Order from
LC. Mi $3. 90, ph $10. 80. TID-6216
Infrared absorption wavelengths for solid LlH and
LID, by W. B. Zimmernian and D. J. Montgom-
ery. Michigan Sute University, East Lansing,
Mich. [I960?]. Contract AT(ll-l)-400. 4p.
. Order from LC. MI $1 . 80, ph $1 . 80.
TID-6262
Changes in macroscopic shape, lattice parameter,
and density in crystals due to point effects"
Technical report no. 22, by r! W. Balluffi and
R. O. Simmons. University at Illinois, Urbana,
111. May 60. Contract AT(11-1)-182. 22p^
Order from LC. Mi $2.70, ph $4.80.
TID-6271
Nuclear chemistry research at Carnegie Institute of
1959-1960. ProgresBjreport.
Technol
Carnegle^Cnstitute of Technology,
July 60. Contract AT(30-l)-844.
fromLC. Mi $5.40, ph $15.30.
.;?
Pittsburgh, Ft.
96p. Order
TID-6322
Solid BiAte physics program. Calculations on the
group theory ana band structure of cadmium sul-
fide. Technical report no. 9. by D. A. Cohen.
Case Institute of Technology, Cleveland, Ohio.
June 60. Contract AT(ll-l)-623. 94p. Order
fromLC. Mi $5.40, ph $15.30. TID-6392
Direct pair production by high energy muons, by
■~ J. F. Gaebler and others" University of Michlgai\
Ann Arbor, Mich. Aug 60. Contract Nonr-1224
(07). 20p. Order from LC. Mi $2.40, ph $3. 30.
TID-6524
Minutes of the Mura general conference, Madison,
Wisconsin, May 16-17, 1960. Miswestern Uni-
versities Research Association, Madison, Wis.
I960. 24p. Order from LC. Mi $2.70,
ph$4.80. TID-6540
ftp. Order from LC.
Progress
C. Parkinson. University of
504
The University of Michigan cyclotron,
report, by W. C. Parkl ""
Michigan, College of Literature, Science and the
Arts, Ann Arbor, Mich. July 60. Contract AT
(ll-l)-275. 23p. Order fromLC. Mi $2.70,
ph$4.80. TID-6575
• V
Diffusion of radioactive gases through power reac-
tor graphite, by H. L. Weissberg and A. S.
Berman. Cak Ridge Gaseous Diffusion Plant.
Oak Ridge, Tenn. Apr 59. Contract W -7405-
eng-26. 19p. Order from LC. Mi $2.40,
ph $3. 30. TID-6678
Basic experimental studies on boiling fluid flow and
heat transfer at elevated pressures for montH
of September 1960. Monthly progress report,
ogr
■m
byj. E. Casterline. Columbia University, En-
glneering Research Laboratories, New York,
N.Y. Sep 60. Contract AT(30- 3)- 187. 3^.
Order from OTS. 75 cents. TID-6689
Sympoaium on particle-fluid Interactions held at the
New York (^rations Office AEC, May 195^7^
by L. Topper and others. New York Operations
Office, Atomic Energy Commission, Research
axid Development Division, New York, N. Y.
Nov 60. 94p. Order from OTS. $1.00.
TID-7592
Variation with electron temperature of the Intensity
ratio of a pair of helium ^pectral lines, by ].C.
Howard. University of California, Lawrence
Radiation Laboratory, Livermore, Calif. June "
58. Contract W-7405-eng-48. I6p. Order
fromLC. Mi $2.40, ph$3.30. UCRL-5265
Ion cyclotron waves in mirror geometry, by H. P.
Furth. University of California, Lawrence
Radiation Laboratory, Livermore, Calif. Feb 59.
Mi $1.80, ph$1.80.
UCRL-5423-T
Stixiy of electric propulsion systems for s
travel. Final report, by R. H ~ '
Oce
nlversity
of California, Lawrence Radiation Laboratory,
U ermore, Calif. Nov 59. Contract W-7405-
eng-48. 175p. Order from LC. Mi $8. 10,
ph$27.30. UCRL-5781
Tables of solutions of lemndre's equation for indices
of nonintegral order, by D. J. BenDaniel and
W. E. Carr. University of California, Lawrence
Radiation Laboratory, Livermore, Calif. Sep
60. Contract W-7405-eng-48. 68p. Order
from OTS. $1.75. UCRL-5859
Tables of conversion of scattering angles for proton-
proton scattering, by B. M. jdnnston and M. J.
Moravcsik. University of California, Lawrence
Radiation Laboratory, Livermore, Calif. Feb 60.
Contract W-7405-eng-48. 203p. Order from
LC. Mi $9. 30, ph $31.80. UCRL-5886
Table of proton-proton scattering phase shift as
calculated from the one-pion exdiange contribu-
tion, by B.M. Johnston and M. J. Moravcsik.
University of California, Lawrence Radiation
Laboratory, Livermore, Ca4if. Apr 60. Con-
tract W-7405-eng-48. 18p. Order fromLC.
Mi $2.40, ph$3.30. UCRL-5955
Analysis of six-bar linka^ using digital computer,
by A. C. Dunk and C. L. Hanson. Purdue Uni-
versity, Lafayette, Ind. , and University of
California, Lawrence Radiation Laboratory,
Livermore, Calif. May 60. Contract W -7405-
eng-48. 13p. Order from LC. Mi $2.40,
ph $3. 30. UCRL-6001
Practical utilization of the nearest singularity in
dispersion relations, by M. J. Moravcsik" Uni-
versity of Ca llfornla, Lawrence Radiation Labor-
atory, Livermore, Calif. Sep 60. Contract
W-7405-eng-48. 59p. Order from 015. $1.50.
UCRL-6I24
Electronic and nuclear properties of some radlo-
active rare-earth elements, by A. Y. Cabezas.
University of California, Lawrence Radiation
Laboratory, Berkeley, Calif. Aug 60. Contract
W-7405-eng-48. 161p. Order from OTS. $2.75.
UCRL-9346
Differential elastic pion - proton scattering at 600,
650, and 750 Mev. by J. I. Shonle. University
of California, Lawrence Radiation Laboratory,
Berkeley, Calif. Aug 60. Contract W -7405-
eng-48. 70p. Order from OTS. $1.75.
UCRL-9362
505
SLOP-l-A thermal multigroup program for the
ffiM-704, by H. Bohl and others" Westin^ouse
Electric Corporation, Betiis Atomic Power Plant.
Pittsburgh. Pii. Oct 60. Contract AT-11-1 -GEN -
14. 151p. Order from OTS. 13.00.
WAPD-TM-ISS
round neutron source in
Calculation of the backa
new, uranium -fueleo reactors, by D. R. Harris .
Westinghousa Electric Corporation. Bettis Atom
ic Power Laboratory. Pittsburgh, Pa. Mar 60.
Contract AT-^1- 1 -GEN- 14. 32p. Order frcrni
WAPD- 1^1-220
OTS. $1.00,
and Maxwe
the Philco
laghan. WesUnghouse Electric Corpora t' an,
Bettis Atomic Power Laboratory, Pittsburgh, Pa.
Oct 60. Connract AT-ll-l'GEN-14. 57p.
Order from 0TS. $1.75. WAPD-TM-232
Nuclear analysia of thermal reflected cylindrical
homogeneous' critical assemblies, by G. P.
Rutleage and !p
A. Kantorczyk. Westinghouse
ElectrTc Cor|oration, Bettis Atomic Power Lab-
oratory, Pitt burgh, Pa. Nov 60. Contract AT-
ll-l-GEN-l4. 18p. Order from OTS. 50 cents.
WAPD-TM-244
Radiation Effects on Materials
Thermal annealing of neutron induced discomposl-
tion in artificial graphite. III. Heating-during
irradiation eiperlments, by T. J. Neubert.
Argonne Nadfnal Laboratory, Argonne, 111.
Apr 53. Deci. February 24, I960. Contract
W-31-109-enk-38. 26p. Order from LC.
Mi $2.70. ph
Induced activity
Burnett
$4. 80.
ANL-5025
in cooling water-are, by T.H.J.
Oali Ridge National Laboratory, Oak
Ridge, Tenn. Mar 52. Contract W-7405-eng-
26. 2p. OrierfromLC. Mi $1.80, ph $1.80.
CF-52-3-172
Thorium oxide s lu
Ridge Nation) rr
Apr
LC.
55. De^l
Mi$l
£0,
, by R. M. Carroll. Oak
boratory. Oak Ridge , Tenn.
July 2, 1957. 9p. Order from
ph$1.80. CF-55-4-162
Metallographic (ixamination of irradiated ceramic
fuel elements and cermet shielding niaterials,
by A. E. Richt and E, J. Manthos" Oak Ridge
National Laboratory, Oak Ridge, Tenn. Oct 56.
Dec!. June KJ. I960. I4p. Order from LC.
Mi $2.40. p^i$3.30. Ct'-56-10-59
Summary report on thorium metal quality for
production reactor use, by E. E. Hayes. Du
Pont de Nemours (E.I.) & Company, Savannah
River Laboratory, Aiken, S. C. July 58. Decl.
June 10, I960. Contract AT (07 -2)- 1. 27p.
Order from LC. Mi $2.70, ph $4.80.
DP- 298
Nuclear metallurgy lectures. Chapter II, by G. A.
Last. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
May 55. Decl. June 10, I960. Contract W-31-
109-Eng-52. 4p. Order from LC. Mi $1.80,
ph$1.80. HW-34868C11
Examination of an internally and externally cooled
water fuel element GEH-4-14 (RM-155), by
W. S. Kelly. General Electric Company, Han-
. ford Atomic Products Operation, Richland, Wash.
Mar 58. Decl. June 10, I960. 7p. Order from
LC. Mi $1.80, ph $1.80. HW-55520
Fretting corrosion irradiation tests, by M. K.
US.
ITHi
MillnoUen. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Sep 58. 9p. Order from LC. Mi $1.80,
ph$1.80. HW -61821
Irradiation effects on boron-containing ceramics
and cermets, by J. G. Morgan and others. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
July 58. Decl. May 5, 1960. Contract W-7405-
eng-26. 20p. Order from LC. Mi $2.40,
ph$3.30. ORNL-2522
Lrradiaaon testing of UO2. A literature search, by
W. E. Boat. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Nov 60. 2lp. Order from
OTS. 50 cents. TID-3559
Effect of radiation on dynamic properties of high
polymers. Progress report for July I, 1959 to
;port tor July
Sauer and A.
une 30, 1960, by J. A. Sauer and A. E. Wood-
ward. Pennsylvania State University, University
Park. Pa. July 60. Contract AT(30-I)-I858.
27p. Order from LC. Mi $2.70, ph $4.80.
TID-6197
General atomic control rod irradiation proposal, by
W. W. Godsin. General Atomic Division, Gen-
eral Dynamics Corpxjration, San Diego, Calif.
Nov 59. Contract AT(04-3)-314. Gp. Order
- from LC. Mi $2.40, ph $3.30. TID-6340
506
Reactor Technology
Rlk River reactor quarterly project report for Sep-
— amber, October, November, 1959. Allis-
Chalmers Manufacturing Company, Atomic
Energy Division, Washington, D. C. 1959. Con-
tract AT(Il-l)-654. 15p. Order from LC.
Mi $2. 40. ph $3. 30. ACNP-ERR-6
fcriodic radiation survey of reactor plant conuiner
— "and components after shutdown "B"' survey.
Section ft. Second performance. Duquesne Light
Company, Shippingport, Pa. May 59. 18p.
Order from LC. Mi $2.40, ph $3.30.
AECU-4215
Radiation levels in the vicinity of the purification
— 'demineralizers. Section l' First performance.
Duquesne Light Company, Shippingport, Pa.
May 59. 9p. Order from LC. Mi $1.80,
ph$1.80. AECU-4217
Helium leak detector test for Hanford and Savannah
River fuel slugs, by A. H. Barnes and others.
Argonne National Laboratory, Argonne, III.
Dec 52. Decl. March 3, I960. Contract W- 31-
I09-eng-38. 12p. Order fi-om LC. Mi $1.80,
ph$1.80. AN L- 4965
EBWR test report, by V. M. Kolba. Argonne
National Laboratory, Argonne, III. Nov 60.
Contract W- 31- 109-eng- 38. 444p. Order from
OTS. $5.00. ANL-6229
Intermediate heat exhanger preliminary dcstg"- ^
Alco Products, Inc. , Schenectady, N. Y. Feb
59. Contract AT(ll-l)-666.
LC. Mi $11. 10, ph$39.60.
235p. Order from
APAE-41 (Vol. 1)
Steam generator preliminary design.
Inc.T Schenectady, N. Y. Feb 59.
Alco Products
Contract
AT(lI-l)-666. 286p. Order from LC. Mi$
Mi $11. 10, ph $48. 60. APAE-41 (Vol. II)
SM-1 reactor core Inspection at 2/3 core life.
Period covered March 7. 1959 to Mayl7ri959,
by B. J. Byrne and others. Alco Products, Inc. ,
Schenectady, N. Y. Jan 60. Contract AT(30-3)-
326. 171p. Order from LC. Mi $6.90,
ph$21.30. APAE-55
Task XV--zero power experiments for the SM-1
core II, by K. A. Robinson and others. Alco
Products, Inc. , Schenectady, N. Y. Mar 60.
Contract AT(30-3)-326. 51p. Order frcwn LC.
Mi $3.90, ph $10.80. APAE-58
A survey of the effects of neutron irradiation on the
impact and other mechanical properties of
pressure vessel steels for the SM-I reactor, by
i.
W. Kelleman. Alco Products, Inc. , Schenec-
tady, N. Y. Apr 60. Contract AT(30- 3)- 326.
77p. Order from LC. Mi $3.90. ph $10.80.
APAE-61
Control and dynamics performance of a sodium
cooled reactor power systetn! Alco Products,
Inc., Schenectady, N. V. 11960). Contract AT
(ll-l)-666. 29p. Order from LC. Mi $2.70,
ph$4.80. APAE-62
SM-2 --Fuel element welding development. Task 5.0,
by R. L. Harris. Alco Products, Inc. , Schenec-
tady, N. Y. Aug 60. Contract AT(30-3)-326.
59p. Order from LC. Mi $3.90. ph $10.80.
APAE-70
Core chaf acteristica of four Army package power
reactors, by J. fc. Gallaher and others. Alco
Products, Inc., Schenectady, N. Y. [1959]. 19p.
Order from LC. Mi $2. 40. ph $3. 30.
APAE-Memo-213
SM-1 --Research and development quarterly report
— for July 1, 1»5» to Sepcernber 30, 1959, by J. O.
Brondel and others. Alco Products. Inc. ,
Schenecudy, N. Y. Jan 60. Contract AT(30-3)-
326. 118p. Order from LC. Mi $5.40,
ph $15. 30. APAE-Memo-237
Tliermal stress testing of SM-2 fuel elements. In-
btermediate heat exchanger and steam generator terim technical reix>rt for January I, i^5^
concept study, by Alco Products. Inc. . Schenec- January 1. 1960. by J. A. Christenson. Alco
ttdy. U V. Feb 59. Contract AT(ll-l)-666. Products. Inc., Schenectady, N. Y. I960. Con
206p. Order from LC.
Mi $9. 30, ph $31.80.
APAE-41 (Vol. Ill)
roducts. Inc., Schenectady, N. Y. I960. Coo-
tract AT(30-3)-326. 94p. Order from LC.
Mi $4. 50, ph $12. 30. APAE-Memo-239
^-2 critical experiments --CE-1. by J. W. Noaks
and others. Alco Products, Inc. , Schenecudy,
N. Y. Nov 59. Contract AT(30- 3)- 326. I80p.
SM - 2 - - Reactor core and vessel monthly report for
December 15, 1959 to February 5 1»60. Alco
Products, Inc., Schenectady, N. Y. Deb 60.
Order from LC.
MI $8.40, ph $28.80.
APAE-54
Contract AT(30- 3) -326. 58p.
Mi $3.60, ph$9.30.
Order from LC.
APAE-Memo-243
507
SM-2 clutch testing, by G. C. Hauenstein. Alco
Products, Iiic, , Schenecudy, N. Y. May 60.
Contract At(30-3)-326. 49p. Order from LC.
Mi $3. 00. pb $6. 30. APAE -Memo- 249
Specifications ind fabrication procedures for PM-2A
core II sutionary fuel elenynts. Alco Products,
Schenectady, N. Y. May 60. Contract
ICOp. Order from LC. Mi $5.40,
APAE -Memo- 261
Tnc
AT(30-3)326».
ph$15.30
Specifications tnd fabrication procedures for nvl-2A
core II neutilon absorber se_ctions . Alco Products,
Schenectady. N. Y. May 60. Contract
59p. Order from LC. Mi $3. 60.
Inc
AT(30-3)-326
ph %9. 30
Liquid nuetal fuel reactor eimeriinent. Quarterly
technical report May 1957 to September 19577 by
J. P. Holliday and tothers. The Babcock and
Wilcox and Company, Lynchburg, Va, 1957.
Contract AT(30-1)- 1950. 75p. Order from OR
95 cents. aAW-1033
Nuclear merchant ship reactor project quanerly
technical report for April- June 1958. Babcodc
and Wilcox Company. Atomic Energy Dtvisioo,
Lynchburg, Va. 1958. Changed from OFFICIAL
• USE ONLY May 1959. Contract AT(30-3)-274
168p. Order from LC. Mi $7.80, ph $25.80.
BAW-1118
Variable modemtor reactor development program.
CXarterly prjogress report no. 1 for August ^
1959. Advaiiced Technology Laboratories. Divi-
sion of American -Standard, Mountain View,
Calif. 1959.! Contract AT(04- 3)250. 36p.
Order from tC. Mi $3. 60, ph $9. 30.
ATL-A-100
APAE -Memo- 262 Nuclear merchant ship reactor project quarterly
technical report for July- -September 1958T~^
Babcock and Wilcox Company, Atomic Energy
Division, Lynchburg, Va. 1958. Changed from
OFFICIAL USE ONLY August 15, 1959. Coo-
tract AT(30-0)-274. 136p. Order from LC.
Mi $6.90. ph $21. 30. BAW-1124
Variable moderftcor reactor development program.
Quarterly progress report no 2. Advanced
rechnology Laiwratories, Division of American
Standard. Mountain View, Calif. Nov 59. Con-
tract AT(04-8)-250. 24p. Order from LC.
Mi $3. 00. pH $6. 30. ATL-A-103
Variable moderttor reactor development program.
Quarterly progress report no.~f. Includes
attachments: J. Kinetics model for boiling water
reactors, by F. E. Romie. II Boch --A pro-
gram for coraputing the hydrodynainlc perform-
ance cf boiling water reactors, by J. O. Bradfute
and others. (ll. Puree'- -A method and code for
the calculation of physics properties of H^O
moderated poMfer reactors, by J. W. Webster a
and others. Advanced Technology Laboratories
Division of Ainerican-Standard, Mountain View,
Calif. Feb dp. Contract AT(04-3)-250. 147p.
Order from V/C. MI $7. 20. ph $22. 80.
ATL-A-107
Variable moderator reactor development program.
Quarterly prajgress report no. 4. Advanced
Technology LIboratories, Division of American-
Standard, Mountain View. Calif. May 60.
Contract AT(Q4-3)-250. 8^. Order from LC.
$19.80. ATL-A-108
Mi $6. 30. ph
Transient flow performance in a multi-loop nuclear
reactor aystete by F. M. Boyd. Jr. and others.
Babcock and Wilcox Company. Atonuc Energy
Division. Lynthburg. Va. Dec 59. 33p. Order
from LC. Mi $3. 00, ph $6. 30. aAW-106-1
Critical experiments for the N. S. Savannah core.
by R. M. Ball and others. Babcock and Wilcox
Camf>any. Critical Experiment Laboratory.
Lynchburg, Va. (1959). I8p. Order from LC.
Mi $2. 40. ph $3. 30. BAW-1131
Nuclear merchant ship reactor shield design sum-
mary report, by W. R. Smith and M.' aT Turner.
Babcock and Wilcox Company. Atomic Energy
Division, Lynchburg, Va. Aug 59. Contraa
AT(30-3)-274. Decl. May 1, 1960. 126p.
Order from OTS. $2.50. BAW-1144-1
Reactor physics of the N. S. Savannah core, by
W. A. Wittkopf and T. M. Schuler. Babcock and
Wilcox Company, Atomic Energy Division.
Lynchburg. Va. Dec 58. Contract AT(30-3)-
274. 21p. Order from LC. Mi $2.40, ph $3. 30.
BAW-1151
Nuclear merchant ship reactor control rod driveline
tests, by D. E. Thoren and D. K. Gestson.
Babcock and Wilcox Company, Atomic Energy
Division, Lynchburg, Va. Nov 59. Contract
AT(30-3)-274. 118p. Order from LC. Mi$6.0a
Ph$18.30. BAW-1176
Preliminary evaluation of materials for use with s
as -suspension coolant, by G. E. Uhland.
abcock and Wilcox Company, Atomic Energy
Division, Lynchburg, Va. July 60. Contract
AT(30-1)-2316. 35p. Order from LC. Mi $3. 00,
Ph$6.30. BAW-1200
Nuclear merchant ship reactor: general guide to
shiDDing reouirements for activated internals
Smith. Babcock and
.icar inercnant smp reacto
shipping requirements for
ana cotnponents. by W. R.
Wilcox Company. Atomic Energy Division,
Lynchburg, Va. Aug 60. Contract AT(30-3)-274.
40p. Order from LC. Mi $3.00. ph $6.30.
BAW-1204
hteavy water reactors and the properties, analysis,
■ — t^ndling, and effects erf heavy water, by D. M.
Duke, i^e babcock and Wilcox Company. Atomic
Energy Division. Lynchburg. Va. Dec 60. Con-
tract AT(30-1)- 2602. 50p. Order from OTS.
$1.50. BAW-1209
Septemoer
der. The fiabcock & Wilcox Company, Atomic
Energy Division, Lynchburg. Va 1960. Con-
tract AT(30- 1)2602. 52p. Order from OTS.
$1.50. BAW-1213
A tracer study of the transport of chromium in
fluoride fuel systems, by R. B. Price and others.
Battelle Memorial Institute, Columbus. Ohio.
June 57. Decl. May 13. 1960. Contract W-
7405-eng-92. 44p. Order from LC. Mi $3.30. .
ph$7.80. BMl-1194
Evaluation of reactor core materials for a gfS'
cooled reactor experiment, by D. L. Keller.
Battelle Memorial Institute. Columbus, Ohio.
July 57. Decl. December 3, 1959. Contract
W-7405-eng-92. 94p. Order from LC. Mi $5. 40.
ph$15.30. BMI-1208
Neutron-flux measurements in a flat plate fuel
element, by W. R. Morgan and others. Battelle
Memorial institute, Columbus, Ohio. Oct 57.
Decl. December 3, 1959. Contract W-7405-eng-
92. 50p. Order from LC. Mi $3.30, ph $7.8 0.
BMl-1231
Further studies with the GCRE critical assembly,
by D. A. Dingee and others. Battelle Memorial
Institute, Columbus, Ohio. Dec 58. Decl. Dec-
ember 3, 1959. Contract W-7405-eng-92. 33p.
Order from LC. Mi $3.00, ph $6.30.
BMl-1306
Canning graphite for gas -cooled reactors, by S. J.
Paprocki and others, Battelle Memorial Institute,
Columbus, Ohio. Jan 59. Decl. December 3,
1959. Contract W-7405-eng-92. 16p. Order
from LC. Mi $2. 40, ph $3. 30. BMI-1311
The effect of fabricatioo variabtes on the structure
and properties of U09--Bttinles8 steel disperaidii
fuel plates, by S. J7 Paprocki and others. Bat-
telle Memorial Institute. Columbus. Ohio.
Feb 59. Decl. December 3, 1959. Contract
W-7405-eng-92. 76p. Order from LC.
Mi $4. 50, ph $12. 30. BMI-1322
Operation and maintenance of an in -pile gas -cooled
loop at the BRR. by S. J. Basham and W. G.
Rieder. Battelle Memorial Institute. Columbus.
Ohio. Dec 60. Contract W-7405-eng-92. 25p.
Order from OTS. 75 cents. BMI-1485
1959. 74p. Order from OTS. $2.25.
BNL-583 (S-53)
Single rod fast effects and related measurements,
by G. A. Price and others. Brookhaven National
Laboratory. Upton. N. Y. May 60. 9p. Order
from OTS. 50 cents. BNL-616 (T-185)
Progress report nuclear engineering department, by
C. Williams and others. Brookhaven National
Laboratory. Upton, N. Y. 1959. 78p. Order
from OTS. $2.00. BNL-595 (S-54)
Status of direct conversion programs in the United
States with special emphasis' on civilian nuclear"
power. Edited version, by W. A. Robba. Brook-
naven National Laboratory, Upton, N. Y. May
60. Up. Order from OTS. 50 cents.
BNL-628 (T-193)
LMFR bimonthly progress report. Mardi "April
1959. Brookhaven National Laboratory. Upton,
KTT: July 59. 96p. Order from LC. Mi $5. 40,
ph $15.30. BNL-4459
Photoelastic analysis of the PWR reactor head at
Brown University, by C. W. Lawton. ComEustion
Engineering, Inc., Nuclear Components Depart-
n»ent, Chattanooga, Tenn. May 58. 42p. Order
fromLC. Mi $3. 00, ph $6. 30. CENC-1030
le developrnent and testing of the uu^ fuel element
system. Summary report for peri«l May 14^
1959- -May 31, I960. CcHnbustion Engineering
Inc. , Nuclear Division, Windson, Conn. June 60.
Contract AT(30-l)-2379. 96p. Order from OTS.
$2,25. CEND-88
Neutron-flux measurements in a concentric-cylinder
fuel element, by J. N. Anno and others. Battelle
Memorial Institute, Columbus, Ohio. Jan 59.
Decl. December 3, 1959. Contract W-7405-eng-
92. 22p. Order fromLC. Mi $2.70. ph $4.80.
BMI-1314
509
ARE design data, by W. B. Cottrell. Oak Ridge
National LaEoratory, Oak Ridge, Tenn. Oct 59.
Contract W-7405-eng-26. 34p. Order fromLC.
Mi $3.00, ph $6.30. CF-53-12-9
An analyBifl of viortex tubes for combined gas -phase
fission -heatijig and separation of the fissionable
materials, by J. L. Kerrebrock and R. V. Meg-
hreblian. 0$k Ridge National Laboratory, Oak
Ridge, Tennj Apr 58. Decl. December 21,
1959. Contract W-7405-eng-26. I07p. Order
from LX:. Mi $5.70, ph $16.80.
CF-57-11-3 (Rev. 1)
ORR
Review of the ORR shield for 30-Mw operation, by
W. Zobel an<) others. Oak Ridge National Labor -
atory. Oak Radge, Tenn. June 58. Contract
W-7405-eng-h6. 21p. Order from LC. Ml $2. 70,
ph$4.80. I CF-58-6-13
Comments on OCR fuel element design, by W. T.
Furgerson. bak Ric^ National Laboratory,
Oak Ridge. Tenn. July 58. lOp. Order from
LC. Mi$l.aO, ph$1.80. CF-58-7-47
ORNL 20 MTR i^ pile lo<y Instrumenution, by
R. G. Affel. Oak Ridge National Laboratory,
Oak Ridge, TJain. Oct 58. Contract W -7405-
eng-26. 53p, Order from LC. Mi $3.60,
ph$9.30. CF-58-10-55
Survey of low et rlchment molten -salt reactors, by
H. G. MacRierson. Oak Ridge National Labora-
tory. Oak Ri^ge, Tenn. Oct 58. 8p. Order
from LC. Ml $1.80, ph $1.80. CF-58-10-60
'■^
Inspection and niaintenance exi)erience with HRE-2,
J. S. Culver and others. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Dec 58. 23p.
Order from LC. Mi $2.70, ph $4.80.
CF-58-12-154
Fuel cycle co8t8| in a graphite moderated slightly
enriched fuaejd salt reactor, by C. E. Gumrie.
Oak Ridge Nafaonal Laboratory, Oak Ridge, Tenn.
Feb 59. 7p. Order from LC. Mi $1.80.
ph$1.80. i CF-59-l-13(Rev. )
Prediction of thermal -neutron fluxes in the bulk
shielding facility from lid tank shieldin
ity
lal
shielding facility from lid tank shielding faclli
data, by A. ri. MacKellar. Oak Ridge Nationa
Laboratory, Qak Ridge, Tenn. Jan 59. 35p.
Mi $3. 00, ph$6.30.
CF-59-1-24
Order from Up.
Calculation at
rJfhM
1 neutron-flux distribution in
nCCk lattioe cell, by T. K. DeBoer. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Aug 59.
8p. Order frfm LC. Mi $1.80, ph $1.80.
CF-59-8-140
Feas ibi H ty s tudy'"
UOo pellets fd
r
-use of small diameter wires in
'2 pellets fqr in pile temperature nKHiitoring,
by R. E. Meadows and W. C. Tliurber. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Oct 59. Contract W-7405-eng-26. 55p. Order
from LC. Mi $3. 60, ph $9. 30. CF-59-10-7
Pressure and temperature in the EGCR exijerimenttl
loop cell in case of accidental release of main '
reactor coolant, by M. H. Fontana. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Oct 59
24p. Order from LC. Mi $2.70, ph $4.80.
- , . ■ CF -59- 10-76
Graphite combustion hazard in the EGCR, by J. W.
nradoe. Oak Ridge National Laboratory, Oak
Ridge. Tenn. Nov 59. Contract W-7405-eng-26.
20p. Order from LC. Mi $2. 40, ph $3. 30.
CF-59-11-134
Proposed modifications to HRE-2 core, by C. G.
Lawson. Oak Ridge National Laboratory, Oak
Ridge. Tenn. Jan 60. 14p. Order from LC.
Mi $2. 40, ph $3. 30. CF-60-1-20
Evaluation of activated charcoal fission gas ad-
sorbers designed for the GC -ORR loop experi
jy R. E. Adams and W. E. Bro
ment no. "17 oy k. c. Aoams ana w. t. Browning.
Oak Ridge National Laboratory, Oak Ridge, Tenn.
Jan 60. 20p. Order from LC. Mi $2.70,
ph$4.80. CF-60-1-24
Nuclear characteristics of BeO-moderated cores
vs graphite moderated cores, by R. S. Carlsmith
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Jan 60. lOp. Order from LC. Mi $2. 40,
ph$3.30. CF-60-1-43
Thorium breeder reactor study: Optimization of a
blanket processing cycle to obtain minimum total
inventory in a chemical reprocessing cycle, by"
Cai
^
W. L. darter. Oak RidgeNational Laboratory,
Oak Ridge, Tenn. Jan 60. Contract W-7405-
eng-26. 28p. Order from LC. Mi $2.70,
ph$4.80. CF -60- 1-63
2G-2R spherical reactor oxie for the lBM-704, by
T. B. Fowler. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Jan 60. 19p. Order from
LC. Mi $2.40, ph $3.30. CF-6O-1-100
Statistical analysis of small power oscillations in
the HRT, by J. Hirota. Oak Ridge National Lab-
oratory. Oak Ridge, Tenn. Jan 60. 31p. Order
from LC. Ml $3.00, ph $6.30. CF-60-1-1D7
Protactinium losses in a BeO moderated reactor, by
R. S. Carlsmith. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Jan 60. 8p. Order from LC.
Mi $1.80, ph $1.80. CF-60-1-108
Xenon control in fluid fueled reactors, by W. D.
— B^ch and others. Oak Ridge National Labors -
Oak Ridge, Tenn. July 60. 33p. Order
CF-60-2-2
tory
from LC. Mi $3. 30, ph $6. 30.
Hazards of nuclear power units In space appllca-
— tions, by P. G. Lafyatis. Oak Ridge National
■CiBbratory, Oak Ridge, Tenn. Feb 60. Con-
tract W-7405-eng-26. 7p. Order from LC.
Mi $1.80, ph$1.80. CF-60-2-18
Observed heat transfer in HRT fuel and blanket
heat exchangers by P. N. Haubenreich and
others. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Feb 60. 15p. Order from LC.
Mi $2.40, ph$3.30. CF-60-2-30
A study of the fuel value of Plutonium, by S. Jaye
and others. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Feb 60. 90p. Order from
LC. Mi $4. 80, ph $13.80. CF-60-2-34
Natural circulation burn out heat flux for the ORR,
by J. F.Wett, Jr. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. Feb 60. 23p. Order
from LC. Mi $2.70, ph $4.80. CF-60-2-61
Numerical three dimensional temperature analysis
at the ECCR fuel rod, by L. G. Epel. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Mar 60.
Contract W-7405-eng-26. 16p. Order from LC.
Mi $2. 40, ph$3.30. ^ CF-60-3-1
ocedure for testing reactor controls pulse anwli-
fiers and preaHiplifier, by J. L. Anderson. Oak
Procedure for testing reactor controls pulse ampli-
Ridge National Laboratory, Oak Ridge, Tenn.
Mar 60. Up.
ph $3. 30.
Order from LC.
Mi $2.40,
CF-60-3-3
510
Effeas of fast neutron reactions in the beryllium
reflector of the HFIR, by H. C. Claiborne.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. May 60, 16p. Order from LC. Mi $2. 40,
ph$3.30. CF-60-3-10
Preliminary hot spot analysis of the HFIR, byN.
Hilveiy. Uak Ridge National Laboratory, Oak
42p
Ridge, Tenn. Mar 60.
Mi $3. 30, ph$7.80.
Order from LC.
CF-60-3-12
Summary of HRT run 16, by J. R. Engel and others.
Oak Hidge National Laboratory, Oak Ridge, Tenn.
Apr 60. Contract W-7405-eng-26. 68p. Order
from LC. Mi $3.90, ph $10.80. CF-60-4-4
Calculated reactivity changes produced by the oscil-
jatloo of an epithermal neutron absorber in the
bulk shielding reactor, by P. Perez-Belles. Oak
Ridge National Laboratory, Oak Ric^e. Tenn.
Apr 60. 14p. Order frcHH LC. Mi $2.40,
ph$3.30. ^. CF-60-4-35
A study of the fuel valve at U^^^, by S. Jaye and
others. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Apr 60. 103p. Order from LC.
Mi $5.70, ph $16.80. CF-60-4-79
Sundard operating procedure for TSR-II, by J. S.
Lewin. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Apr 60. 19p. Order from LC.
Mi $2.40, ph$3.30. CF-60-4-89
Gamma and beta teat generation rates in the HFIR
core, by N. Hilvety. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. Apr 60. 15p. Order
from LC. Mi $2.40. ph $3.30. CF-60-4-110
Events preceding the large power excursion on
November 2, 1959, by P. N. Haubenreich. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
May 60. Contract W-7405-eng-26. 7p. Order
from LC. Mi $1.80, ph $1.80. CF-60-5-18
Activity due to N^^ and N^^ In the FfflR primary
coolant, by H. A. McLain. Oak Ridge Nationial
Laboratory, Oak Ridge, Tenn. May 60. Con-
tract W-7405-eng-26. 32p. Order from LC.
Ml $3.00, ph$6.30. CF-60-5-19
Analog computer study of the MSR-ORR in pile
pressurized water loop no. 1, by S. J. Ball.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. May 60. 12p. Order from LC. Ml $2. 40,
ph$3.30. CF-60-5-50
Evaluation of external holdiq) of circulating fuel
thermal breeders as related to cost ana feasibi -
lity, by I. Spiewak and L. F. Paraly. Qak Ridge
National Laboratory, Oak Ridge, Tenn. May 60.
52p. Order from LC. Mi $3. 60, ph $9. 30.
CF-60-5-93
An investigation of the structuia 1 integrity of select-
ed components of the Oak Ridge Research re-
actor, py J. M. Conim and omers. Qak Ridge
National Laboratory, Oak Ridge, Tenn. July 60.
Contract W-7405-eng-'26. 48p. Order from LC.
Ml $3. 30, ph $7. 80. CF-60-5-109
Activity in the HFIR primary coolant syatem after
a meltdown of the fuel in reactor, by H. A.
McLain. Oak Ridge NationalLLaboratory, Oak
Ridge, Tenn. June 60. Contract W-7405-eng-
26. 17p. Order from LC. Mi $2.40, ph $3. 30.
CF -60-6-52
511
!^
by H. A. MdLain. Oak Ridge National Labora-
lory, Oak Ridge, Term. June 60.
from LC. Nil $1.80, ph $1.80.
8p. Order
CF-60-6-75
Autocorrelaood functions and operational safety
analysis, by P. R. Kasten. Oak Ridge National
Laboratory, Oak Ridge, Tenn. June 60. Con-
tract W-740$- eng-26. 16p. Order from LC.
Mi $2.40. p*$3.30. CF-60-6-102
P>$3.:
Shielding erf pipps In the HFIR primary coolant sys-
gmToy H. X. McUin and L A. Haack. Oak
"R^ge National Laboratory, Oak Ridge, Tenn.
June 60. Contract W-7405-eng-26. 31p. Order
from LC. >ii $3.00, ph $6. 30, CF-60-6-123
>li$3.00, ph$6.30.
jq analysis, by R. S.
APPR-1 Startupl analysis, by R. S. Stone. Oak
Ridge Natio^l Laboratory, Oak Ridge, Tenn.
July 60. Contract W-7405-eng-26. 5p. Order
from LC. Mi $1.80, ph $1.80. CF-60-7-50
Shielding of deihineralizers and filters in the HFIR
primary coojlant system, by H. A. McLain and
L A. Haadi. Oak Ridge National Laboratory,
Oak Ridge. Tenn. July 60. Contract W -7405-
eng-26. 12|>
ph$3.30
Order frcm LC.
Mi $2.40,
CF-60-7-53
Pressure rise ti die reversed flow HRT following
a cold fluid iiccident during startup, by L. L.
Bennett andS. Jaye. Oak Ridge Nlational Labora-
tory, Oak Ridge, Tenn. July 60. Contract W-
7405-eng-26i. Up. Order from LC. Mi $2.40,
ph$3.30. CF-60-7-61
Radiative heat ransfer in multisurfaced nonblack
encloeures with application to the EGCR fueT
buDdle, by li. G. Epel. Oak Ridge National
Laboratory,' Oak Ridge, Tenn. July 60. Up.
Order from LC. Ml $2. 40, ph $3. 30.
CF-60-7-71
RcBcarch and dfcvelopnent program quarter!
lopne
t for t
rogresa report tor the period July i. ^^9 to
?iuarterly
y I, 19S9
eptember 30, 195^ Westinghouse Electric
Corporation^ Atomic Power Department, Pitts-
burgh. Pa. INov 59. Contract AT(30-l)-2289.
126p. Ordelr from LC. Mi $6.90, ph $21. 30.
CVNA-36
1
Analysis of reactivity accidents and of change in
load transients for the CVTR reactor, by D. E.
Radibone anil H. H. Norman. Westinghouse
Electric Corporation, Atomic Power Department,
Pittsburgh, f^. Feb 60. 68p. Order from LC.
Ml $3. 90, pii$10.80. CVNA-47
Radioactive waste disposal system. Core ). Seed L
Section 8. Duquesne Light Company, Shipping-
port, Pa. Apr 60. 7p. Order from LC.
Mi $1.80. ph $1.80. DLCS-1350801
Determinatinn of primary system pressure drop.
Duquesne Li^t Company, Shippingport, Pa.
July 59. 19p. Order from LC. Mi $2.40.
ph$3.30. DLCS- 1470103
River soundings. Duquesne Light Company, Ship-
pingport, Pa. June 60. 6p. Order from LC.
Mi $1.80, ph$1.80. DLCS-3000102
River soundinm. Core I, Seed 2. Duquesne Ug^t
Company, Shippingport, Pa. July 60. 6p. Order
from LC. Mi $1.80. ph $1.80. DLCS-3OOO103
Station perforniance during an unscheduled power
transient. Core I, Seed 2, Duquesne Light Com-
pany, Shippingport, Pa. July 60. lOp. Order
from LC. Mi $1.80, ph $1.80. DLCS-3450101
Heavy water nrKxlerated power reactors. Progress
report for June I960, by D. F. Babcock and
others. E. L du Pont de Nemours k Company,
Explosives Department, Wilmington, Del. Oct
60. Contract AT(07 -2)- 1. 53p. Order from
OTS. $1.25. DP-515
^ ^ er reactors. Progresa
report for August 19^0, by D. F. Babcock and
Heavy water moderated pow
report for August 1960,
others. E. L du Pont de Nemours k Company,
Explosives Department, Wilmington, Del. Nor
60. Contract AT(07- 2)- 1, 41p. Order from
OTS. $1.00. DP -535
Heavy water moderated power reactors. Progres»
report for September 1960, by D. F. Babcock
ana others. E. I. du Pont de Nemours k Com-
pany. Explosives Department, Wilmington, Del.
Dec 60. Contract AT(07- 2)- 1. 18p. Order
frwnOTS. 50 cents. DP-545
Heavy water nioderated
irer reactors
ProgreM
cock and
Babcock
I ted power r
report for October 1960, by"
others. E. I. du Pont de Nemours k Company,
Explosives Depjartment, Wilmington, Del. Dec
60. Contract AT(07 -2)- 1. 30p. Order from
OTS. 75 cents. DP-555
?ram.
Quara
: uecer
rterljr
Maritime gas -cooled reactor progr
progress report for the period ending ueceniSer
31, 1959, by H. Hopkins and others. General
Dynamics Corporation, General Atomic and
Electric Boat Divisions, San Diego, Calif.
1959. Contract AT(04- 3)- 187. 152p. Order
from OTS. $3.00. GA-1195
512
^QCR heat -exchanger test program interim report:
■ [gothermal air and helium testa, by F. B. Ander-
son and others. General Dynamics Corporation,
Electric Boat Division, San Diego, Calif. Oct
59. Contract AT(04-3)- 187. 52p. Order from
OTS. $1.75. GA-1441
for July to September 1959, by"
and others. General Electric (
Nuclear superheat project. First quarterly report
' R. T. Pennington
and others. General Electric Company, Atomic
Power Equipment Department, San Jose, Calif.
Dec 59. Contract AT(04-3)-l89. 122p. Order
from OTS. $2.50. GEAP-3290
Superheat process tube heat transfer testa nuclear
superheat project, by E. Janssen. General Elec-
tric Company, Atonuc Power Equipment Depart-
ment, San Jose, Calif. Jan 60. Contract AT
(04-3)-189. 27p. Order from OTS. 75 cents.
GEAP-3319
A method for the comparative evaluation of reactor
control materials, by T. J. Pashos and others.
General Electric Company, Atomic Power Equip-
ment Department, San Jose, Calif. Apr 60.
Contract AT(04-3)-189. 13p. Order from OTS.
50 cents. GEAP-3344
VARI- -solution of simultaneous, first-order, ordin-
ary, differential equatioris, by B. A. Kerr. Gen-
eral Electric Company, Vallecitos Atomic Labor-
atory, Pleasanton, Calif. May 60. Contract AT
(04-3)-189. 23p. Order from LC. Mi $2.70,
ph$4.80. GEAP-3356
Nuclear superheat project third quarterly progress
report January to Klarch 1960, by R. T. Penning-
Toa. General Electric Company, Atomic Power
Equipment Department, San Jose, Calif. July 60.
Contract AT(04-3)- 189. I91p. Order from OTS.
$3.00. GEAP-3468
Summary design report. The flux trap core for •
marine boiling water reactor in the T7 tanker, by
J. R. Birle and others. General Electric Com-
pany, Atomic Power Equipment Department, San
jo»e, Calif. July 60. Contract AT(04-3)-189.
I19p. Order from OTS. $2.50. GEAP-3476
Neutron and parallel flow channel coupling effects
on the T-7 flux trap reactor, by J. M. Case.
Ceneral Electric Company, Atomic Power Equip-
ment Department, San Jose, Calif. Aug 60.
Contract AT(04-3)-189. 41p. Order from 075.
$1.00. GEAP-3508
Nuclear superheat development program. First
QMarterjy progress report for July-SeptembeF
1^59. Combt^tion Engineering, inc. , Windsor,
Conn, and General Nuclear Engineering Corpora-
tion, Dunedin, Fla. 1959. Contract AT(1 1-1)-
795. 70p. Order from LC. Mi $3.60, ph $9. 30.
GNEC-118
quarter
Second
progress report for October -December
Nuclear superheat development program
ir\y progress report for Octobel
1959. dombustion Engineering, Inc. , Windsor,
Conn, and General Nuclear Engineering Corpora-
tion, Dunedin, Fla. 1959. Contract AT (11-1)-
795. 99p. Order from LC. Mi $5.40, ph $15. 3a
GNEC-125
Nuclear superheat development prc^am. Ppuf tfa
Quarterly progress report, April"- June 1960, by
Combustim Engineering, Inc. , Windson, Conn. ,
and General Nuclear Engineering Corporation,
Dunedin, Fla. Nov 60. Contract AT(ll-l)-795.
155p. Order from OTS. $2.75. GNEC-138
Quarterly report for October 1 to December 31,
1951, by W. I. Thompson. The H. K. Ferguson
Company, New York, N. Y. 1951. Decl. Aug
August 26, 1960. Contract AT(30-1)-1075. 55p.
Order from OTS. 50 cents. HKF-ll6(Rev.)
Reactivity effects resulting from melting hollow
fuel elements -- experiment II, by D7 D. Lanning
and W. P. Stinson. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Nov 54. Decl. February 24. 1960. 9p.
Order from LC. Mi $1.80, ph $1.80.
HW-33654 .
Specifications for WAPD loop, by J. A. Berberet.
General Electric Company. Hanford Atomic
Products Operation, Richland, Wash. Feb 55.
Decl. June 10, 1960. 22p. Order from LC.
Mi $2.70. ph $4.80. HW- 35481 (Del.)
A discussion of techniques for optimizing flux and
pjwer distribution, by G. C. Fullmer and others.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Mar 55.
Decl. April 15, 1955. 3p. Order from LC.
Mi $1.80, ph $1.80. HW-35674
Radiometallurglcal hardness and weight results on
irradiated zirconium and Zircaloy-2 samplesTs
requested by the pile development unit, by W. S.
Kelly. Hanford Atomic Products Operation,
Richland, Wash. Apr 55. Decl. June 18, 1960.
Contract W-31-109-Eng-52. 6p. Order fmm
OTS. 25 cents. HW- 36291
Reactor effluent monitoring, by R. B. Hall. General
Electric Company, Haniord Atomic Products,
Operation, Richland, Wash. May 57. Decl.
May 4. 1960. Contract W-31-109-Eng-52. lOp.
Order from LC. Mi $1.80, ph $1.80. HW -50137
SU
M
.1
w
Presaurized water systema- -selected problems, by
W. J. ^lariiin. General Electric Comv&ny,
Hanford Atomic Products Operation, Pichland,
Wash. Ap* 58. Contract AT(45- 1)- 1350. 6p.
Order fro4 LC. Mi $1.80, ph $1.80.
HW- 55785
model 9tud^ results, by W. j. Morris. General
iuSKTr
lopmer
Sutus of the v»ater-wall development program with
Morris" Genei
Electric C^pany, "Hanford Atomic Products
Operation, I Richland, Wash. Aug 58. Contract
W-31-109-tng-52. lOp. Order from LC.
Mi $1.80, bh $1,80. HW-56881
Rod and shiela cooling water ^"PPly ^y
N design criteria- -project CAI 816,
systems. 105-
by G. E.
General Electric Comp)any, Hanford
Wade.
Atomic Prdducta Operation, Richland, Wash.
Mar 61. lip. Order from IX. Mi $2. 40,
ph$3.30. 1 HW-57016 (Rev. 1)
NPR water quality design bases --revision 2 (mixed
primary system), by W. D. Bainard. General
Electric Olwnpany, Hanford Atcwnic Products,
Operation, Richland, Wash. June 59. Contract
AT(45-1)-1(350. lOp. Order from LC. Mi $1.80,
HW-57252(Rev. 2)
ph$1.80.
Dynamic control characteristics of the plutonium
recycle teat reactor, by H. K. Nelson. General
Electric Ci»npany,~Hanford Atomic Products
Operation, I Richland, Wash. Jan 59. Contract
AT(45-l)-^350. 71p. Order from LC. Mi $4. 50,
ph $12. 30.1 HW-58706
Oxygen scavejiger studies with hydrazine in high
pH 9y8tern»r Interim reixjrt, by L« D. Perrigo,
Jr. and T. F. Demitt. General Electric Com-
pany, HanHord Atomic ProdiKts Operation, Rich-
land, Wasll. Jan 59. 7p. Order from LC.
Mi $1.80. ph $1.80. HW-58932
r
1706 KE wate*- treatment for out -of- reactor test
%
facilities, by T. F. Demmitt. General Electric
Company, Hanford Atomic Products Operation,
Richland, Wash. Mar 59. Contract AT(45-l)-
1350. 8p. Order from LC. Mi $1.80,
ph$1.80. 1 HW-59752
PRTR fuel eletnent nuclear safety, by N. Ketzlach.
General Electric Company, Hanford Atomic
Products
Contract
Ml $1.80,
;ration, Richland,
(45-l)-1350. 5p.
$1.80.
Wash. Mar 59.
Order from LC.
HW-59786
of pjtl
Shielding of PRTR gas locy and filter, by J. J.
Regimbal. ' General Electric Company, Hanford
Atomic Pr<iductfl Operation, Richland, Wash.
Apr 59. 1 >p. Order from LC. Mi $2.40,
ph$3.30. I HW -60101
Improvements in water treatment for once-throu^
reactor cooling, by R. B. Richman. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. May 59. Contrta
AT(45-1)-1350. Up. Order from LC.
Mi $2. 40, ph$3.30. HW -60311
709 program for reduction of exponential pile daa.
by d" D. Mataumoto. General Electric Com-"
pany, Hanford Atomic Products Operation,
Richland, Wash. May 59. Contract AT(45-l)-
1350. 14p. Order from LC. Mi $2.40.
ph$3.30. HW-6G388
PRTR hazard analysis for various mechanical
failures, byj. Muraoka. General Electric
Company, Hanford Atomic Products Opjeraiioo
Richland, Wash. July 59. Contract AT(45-l)-
1350. 14p. Order from LC. Mi $2.40,
ph$3.30. HW- 60963 (Rev.)
Suggested major equipment for NPR water quality
control labs, by W. D. Bainard. General Elec-
trie Company, Hanford Atomic Products Operitic
tion, Richland, Wash. July 59. Contract AT
(45-1)- 1350. 4p. Order from LC. Mi $1.80,
ph$1.80. HW-61391
Design test PR-20 calandria characteristics: final
rq)ort, by R. L. Gruver. General Electric
Qxnpany, Hanford Atomic Products Operation
Richland, Wash. Oct 59. Contract AT(45-1)-
1350. 9p. Order from LC. Mi $1.80, ph $1.8a
HW- 62551
Hydraulic system flow decay relations during losi
of external power, by W. J. Love. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Feb 60. 54p.
Order from LC. Mi $3.60. ph $9.30.
HW- 62846
Ion exchange resins and water conditioning methodi
employed at 1706-Ker for the in-reactor loopg.
nplc
"m:
byM.L. Mutch. General Electric Company,
Hanford Atomic E^roducts Operation, Richland,
Wash. Dec 59. Contract AT(45-1)-1350. 9p.
Order from LC. Mi $1.80, ph $1.80.
HW -62911
Steady-state recirculating reactor stability and
operational characteristics --water and mettl
temperature coefficients, by C. Wesley Allen.
General Electric Company, Hanford Atomic
Products Operation. Richland, Wash. Dec 59.
Contract AT(45-1)-1350. 26p. Order from IX:.
Mi $2.70. ph$4.80. HW-63183
514
j^pj^ gingle pass decontamination, by G. E. Neibaur.
— ^neral Electric Company, Hanford Atomic Com-
pany Hanford Atomic Products Operation, Rich-
land,'Wash. Jan 60. Contract AT(45-1)- 1350.
So Order from LC. Mi $1.80. ph $1.80.
. "** HW-63533
PTTR measurements of the EGCR lattice parame-
— lers, by P. F. Nichols and others. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Mar 60. Contract
AT(45-1)-1350. I6p. Order frcwn LC.
Mi $2.40, ph$3.30. HW-63768
Study report. High speed data acquisition system
" for PRTR. by R. G. Clark. General Electric
Company, Hanford Atomic Ehroducts Operation,
Richland, Wash. Jan 60. Contract AT(45-1)-
1350. 7p. Order from LC. Mi $1.80, ph$1.80.
HW- 63789
Preliminary evaluation of chlorine for "sc a^ a
cooled reactor safeguard, by R. E. Dahl. Gen-
eral Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Mar 60. Contract
AT(45-1)-1350. 19p. Order from LC. Mi $2. 40,
ph$3.30. HW-63902(Rev.)
Reamed rear face parker fitting, by P. B. McCarthy
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Mar 60.
Contract AT(45-1)-1350. 12p. Order from LC.
Mi $2. 40, ph$3.30. HW-64310
Problems of a small leeik between the flow monitor
and heated section of a Pft^fR process tube, by
C. M. Hesson. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Mar 60. Contract AT(45-1)-1350. 6p.
Order from LC. Mi $1.80, ph $1.80.
HW-64340
PRTR fuel element rupture test facility; Application
to power reactor fuels, by W. E. Roake. Gener-
al Electric Company, Hanford Atomic Products
Operation, Richland, Wash. Mar 60. Contract
AT(45-l)-1350. 4p. Order from LC. Mi $1.80,
ph$1.80. HW-64456
Development of pressure tubing for the plutonium
recycle test reactor, by J. W. Riches. General
filectric Company, Hanford Atomic Products
Operation, Richland. Wash. Apr 60. Contract
AT(45-l)-1350. lOp. Order from LC. Mi $2. 40,
I*$3.30. HW- 64965
Coagulant aids as filter aids by W. R. Conley and
R. W. Pitman. General Electric Company, Han-
ford Atomic Products Operation, Richland, Wash.
July 60. Contract AT(45-1)- 1350. 7p. Order
from LC. Mi $1.80, ph $1.80. HW-65333
Computation of materials testing reactor core bum-
up for accountability records^ by F. P. Vance
and F. H. Tingey. Phillips Petroleum Company,
Atomic Energy Division, Idaho Falls, Idaho.
June 54. Contract AT(lQ-l)-205. 9p. Order
from LC. Mi $1.80, ph $1.80. IDO- 16170
Calibration of RMF control elements, by E. Fast
and D. A. Millsap. Phillips Petroleum Company,
Atomic Energy Division, Idaho Falls, Idaho.
Apr 57. Contract AT(10-l)-205. 29p. Order
from LC. Mi $2.70, ph $4.80.
IDO- 1 6610 (Pt. I)
Calibration of RMF control elements: II. Recalibra-
tion of the regulating rod, by D. A. Millsap and
E. Fast, niillips Petroleum Company, Atomic
Energy Division, Idaho Falls, Idaho. Jan 59.
Contract AT(10- 1 )-205. 17p. Order from LC.
Mi $2. 40, ph $3. 30. IDO- 16610 (Pt. II)
Calibration of R^IF control elements: III. Recall-
bration af regulating rod, by E. Fast and others.
Phillips Petroleum Company, Atomic Energy
Division, Idaho Falls, Idaho. Aug 59. Contract
AT(10-l)-2O5. 18p. Order from LC. Mi $2.40,
ph$3.30. IDO- 16610 (Pt. Ill)
Calibration of RMF control eleinents: IV. Recali-
bration of^regulating rod, by D. W. Knight and
others. Phillipe Petroleum Company, Atomic
Energy Division, Idaho Falls, Idaho. Aug 60.
Contract AT(10-l)-205. I6p. Order from LC.
Mi $2. 40. ph $3. 30. IDO- 16610 (Pt. IV)
Proposed 6(»4W operation of MTR, by J. H. Rain-
water. PWllips Petroelum Company, Atomic
Energy Division, Idaho Falls, Idaho. Feb 59.
Contract AT(10-l)-205. 64p. Order from LC.
Mi $3. 90, ph $10. 80. IDO- 16567
Metal- water reactions: rates of reaction of alumi-,
numandaluminum-uranium alloys with water
vapor at elevated temperatures, by W. F.
Zelezny, Phillips Petroleum Company, Atomic
Energy Division, Idaho Falls, Idaho. Nov 60.
Contract AT(10-l)-205. 59p. Order from OTS.
$1.00. IDO-16629
The advanced test reactor "ATR final conceptual
design, by D. R. deBoisblanc et al. Phillips
Petroleum Company, Idaho Falls, Idaho. Nov
60. Contract AT(10-1)- 205. 229p. Order from
OTS. $3.00. IDO-16667
515
ABWR core
i
kameter atudy. Combustion Engi-
neering rn<f . , Nuclear I^vision, Windsor, Conn.
Dec 59. dontract AT(10-l)-967. 198p. Order
from LC. Mi $8.70. ph $30. 30. IDO-19006
Health physic* and radlochemistry manual for
Army nuclear power plants
ry n:
Basic
criteria, biy R. L. Hoover andothers. Combus-
tion Engineering, Inc., Nuclear Division, Wind-
sor. ConnJ [1960]. Changed from OFFICIAL
USE ONLYjune 6, 1960. Contract AT(I0-l)-967.
125p, Or(^Br from LC. Mi $6. 30, ph $19. 80.
IDO- 19014 (Vol. I)
Army gas-coqled reactor systems program monthly
ress rjeport for July 1959. Aerojet -General
jucleonics^ San Rarnon, Calif. Aug 59. Con-
tract AT(10-1)-880, 53p. Order from LC.
Ml $3. 60. ph $9. 30. IDO- 28543
r
Army gas-codled reactor systems program monthly
progress
Gei "
codled
s repo
^n
?rt for September t95^, by Aerojet
:neral Niicleonics, San Ramon, Calif. Oct 59.
Contract Atr(10-l)-880. 66p. Order from LC.
Mi $3. 90. ph $10. 80. IDO-28545
progress rfepo:
Ger>eral Noclet
Army gas-coqled reactor systems program monthly
Aerpject-
Nov 59.
progress report for October 1959
'' ^neral Nucleonics, San Ramon. Calif
Contract Atr(10-l)-880.
Mi $3.90. bh$10.80.
r
6lp. Order from LC.
IDO- 28546
Army gaa-codled reactor systems program monthly
•cocll<
1^
I progra
60. Ae
progress report for January I960. Aerojet -
General Niicleonics, San Ramon, Calif. Feb 60.
Contract Alr(10-l)-880.
Mi $3. 30, |)h$7.80.
52p. Order from LC.
IDO- 28551
Army gas-codled reactor systems program monthly
progress report for February I960. Aerojet-
General Niicleonics, San Rarnon, Calif. May 60.
Contract Alr(10-l)-880. 74p. Order from LC.
Mi $3. 90, t>h$10.80. IDO-28553
Army- gas -cooled reactor systems program monthly
progress report for May 19Rr Aerojet-General
Nucleonics,' San Ramoni Calif. June 60. Con-
tract AT(l()-l)-880. 99p. Order from LC.
Mi $5. 40. i>h $15. 30. IDO-28557
Test requirer
nuclear propulsion
aETR, 6yO.]
nts for Naval reactors and aircraft
^E) applicability of the
nc.
Company
AT(ll-l)-6^8
ph$7.80
applic
Elgert and others. Internuc lea r
Clayton, Mo. Dec 59. Contract
5lp. Order from LC. Mi$3.30,
INTERNUC-51
Reactor technology report no. 14 chemistry, by
B. H, Caldwell and others. General Electric
Company, Knolls Atomic Power Laboratory,
Schenectady, N. Y. Sep 60. Contract W-31-
l09-Eng-52. Ulp. Order from OTS. $2.50.
' * KAPL-2000-U
Chalk River heat generation and fuel burnup daa,
by C. E. Weber. kCnoUs Atomic Power Laboft-
tory, N. Mex. Mar 52. Decl. March 12, 19ia
Contract W-31-109-Eng-52. 12p. Order from
LC. Mi $1.80, ph $1.80. KAPL-M-CEW-U
The total energy release per fission of U^^^ and in
time depenoence, by D. C. Sherman. Knolls
Atomic Power Laboratory, Schenectady, N. Y.
June 60. Contract W-31-109'-Eng- 52. 22p.
Order from LC. Mi $2.70, ph$4.80.
KAPL-M-DCS-4
Determination of the intrinsic neutron source
strength in the FPR critical assembly, by E. C,
Hansen and H. F. Schulz. Knolls Atomic Power
Laboratory, Schenectady, N. Y. May 60.
Contract W-31-109-Eng-52. 25p. Order from
LC. Mi $2.70, ph $4.80. KAPL-M-ECH-5
Method of calculating effective cutoff energies for
filters used with _l/v" detectors, by 0° D.
Hickman and W. B. Leng. Knolls Atomic Power
Laboratory, Schenectady, N. Y. May 60.
Contract W-31-109-Eng-52, 25p. Order from
LC. Mi $2.70. ph$4.80. KAPL-M-GDH-3
Oxygen activity i
Clancy and N.
516
gen activity in water cooled reactors, by E. P.
lancyandN. C. Francis. Knolls Atomic Power
Laboratory, Schenectady, N. Y. Dec 57. Decl.
March 28, 1960. Contract W-31-109-Eng-52.
37p. Order from LC. Mi $3. 00. ph $6. 30.
KAPL-M-NCF-2
Factors used in the calculation of gamma sourcei
in the core and primary shield of the NCR, by
M. J. Leibeon. Knolls Atomic Power Laboratory.
Schenectady, N. Y. Dec 59. 38p. Order from
LC. $3.00, ph$6.30. KAPL-M-NPA-2
Interference tests of large A. C. cables on therroo-
couple signals, by R. A. Kaufman. Knolls
Atomic Power Laboratory, Schenectady, N. Y.
May 60. Contract W-31-109-Eng-52. 20p.
Order from LC. Mi $2.40. ph $ 3.30.
KAPL-M-RAK-1
System design description and operating instructioii
for the Sfc coolant activity test facility, by J. Wi
Sapp. Knolls Atomic Power Laboratory, Schenec-
- tady, N. Y. Aug 59. Contract W-31-109-Eng-
52. 27p. Order from LC. Ml $2.70, ph $4. 80.
KAPL-M-SSD-54(Rev.a)
Trio report: U. S. -U. K. fast reactor meeting,
-^t-April 50 to May 5, 1»S6. by W. M.
Cishin and J. K. Davidson. Knolls Atomic
Power Laboratory, Schenectady, N. Y. [1956]
Decl. May 5, 1960. Contract W-31-109-Eng-
52 I5p. Order from LC. Mi $2.40. ph $3. 30.
KAPL-M-WMC-3
A design for a rotary reactivity c
— reactor, by V. Josephson. d
control for a test
Laboratory, Los Alamos. N
Decl. May 13. 1960. I2p.
>4i$2.40. ph$3.30.
>s Alamos St^ntific
, Mex. Sep 50.
Order from LC.
LA-ll72(Del.)
Quarterly
Derlod
sutus report on LAMPRE program for
ending November 20, 1960, by The Uni-
versity of California, Los Alamos Scientific
Laboratory, Los Alamos, N. Mex. Dec 60.
Contract W-7405-ENG-36. 29p. Order from
OTS. 75 cents. LAMS-2487
Qiarterly status report on turret reactor experi-
ment for period ending November 20 19o0. by
The University of California, Los Alamos
Scientific Laboratory. Los Alamos, N. Mex.
Nov 60. Contract W-7405-ENG- 36. 38p. Order
from OTS. 75 cents. LAMS-2495
Three-dimensional flux and power distribution
measurements in a power reactor, by E. B.
Fehr and others. Knolls Atomic Power Labora-
tory, Schenectady, N. Y. [1959] 19p. Order
from LC. Mi $2.40, ph $3. 30. M-7297
ANPP code development program pressurized-water
task quarterly progress report no. 3 for Febru-
ary I 1960 to April 30, 1960. by T. M. Qlson
andothers. Martin Company, Nuclear Division
Baltimore, Md. May 60. Contract AT(30-1)-
2431. 142p. Order from LC. Mi $7.20,
ph $22.80. MND-C-2202
Liquid fluidi^ed bed reactor study. Quarterly prog-
resa report no. 1 for October 15, 1959 to January
31. 1960. Martin Company, Nuclear Division,
Baltimore, Md. Feb 60. Contracr AT(30-1)-
2460. 84p. Order from LC. Mi $4.80,
|jh$13.80. MND-LFBR-2303
.-ompany,
Md. May 60. Contract AT(30-l)-2460. 50p.
Order from LC. Mi $3. 30. ph $7. 80.
MND-LFBR-2304
PM-1 nuclear power plant: hazards summary evalua-
tloir Martin Company, Nuclear Division,
BaTtimore. Md, Oct 59. 109p. Order from LC.
Mi $6.00, ph$18.30. MND-M-1853
PM-1 nuclear power plant program controls and
instrumentation report, by F. Hittman. Martin
Company, Nuclear Power Plant, Nuclear Division.
Baltimore. Md. Feb 60. Contract AT(30-1)-
2345. I83p. Order from OTS. $2.75.
MND-M-1914
Initial report on nuclear power plant economics.
California Research and Development Company,
Livermore Research Laboratory, Livermore.
Calif. May 53. Decl. with deletions September
23. 1959. Contract AT(ll-l)-74. 51p. Order
from LC. Ml $3. 60. ph $9. 30.
MTA-34(Del.)
Analysis of cylindrical stainless steel canned moder-
ator elements or a dosium graphite reactor, by
W. P. Corcoran and others" Atomics Intemation -
al. A Division of North American Aviation. Inc. .
.. Canoga Park, Calif. Dec 57. Decl. November
9, 1959. Contract AT- 11-1 -GEN-8. llOp.
Order from LC. Ml $5.70, ph $16.80.
NAA-SR-1990
The developmental organic reactor, by J. Jacc*)8on.
Atomics International. A Division of North
American Aviation, Inc. . Canoga Park. Calif.
Sep 58. Coniaact AT- 11-1 -GEN-8- 88p. Order
from LC. Ml $4.80, ph $13.80. NAA-SR-2780
Preliminary design description for the Plqua organ-
ic moderated reactor plant Pi qua, Ohio (Revised)
AtCMnlcs Iniematiooal. A Division of North
American Aviation, Inc. , Canoga Park. Calif.
[1959]. Contract AT-ll-l-GEN-8. 71p. Order
from LC. Ml $4.50, ph $12.30. NAA-SR-3635
Power flattening In CMR cores, by G. K. Gardiner.
Atomics International. TTDivision of North
American Aviation. Inc. . Canoga Park, Calif.
Dec 60. Contract AT(11-1)-GEN -8. 39p. Order
from OTS. $1.00. NAA-SR-5251
Thermal cycling and leadage tests of 2- in. valves
for sodium service, by C. J. Baroczy. Atomics
International. A Division of North American
Aviation. Inc. . Canoga Park, Calif. Dec 60.
Contract AT(ll-l)-GEN-8. 28p. Order from
OTS. 75 cents. NAA-SR-5275
Study of air permeability of concrete paints and
sealants tor reactor housing installations (pre-
liminary report), by L. Baurmash and others.
Atomics International. A Division of North
American Aviation, Inc. . Canoga Park, Calif.
Sep 60. Contract AT(11-1)-GEN -8. 24p.
Order from OTS. 50 cents. NAA-SR-5411
517
Kinetic experlntents on water boilers - "A" core re
port- fart Il|--pile oscillator reaults, by R. N.
Cordy. Atoiiics International. A Division of
North American Aviation, Inc., Canoga Park,
Calif. DecfO. Contract AT(ll-l)-GEN-8. 54p.
Order from JDTS. $1.25. NAA-SR-5417
•Containrnent aspects of hydrogen
\. Greenfield. Atom-
Kinetic emeriraents on water boilers - "A" core re-
Port--Part lV--(
oxygen explosions, by M. A. tfn
ics international. A Division of North American
Aviation, In<?., Canoga Park, Calif. Dec 60.
Contract ATtli-l^GEN-S. 34p. Order from
OTS. 75 cerjw. NAA-SR-5418
The selection, pes ignnxxlifi cation, and analysis of
sodium valvas for Hallam nuclear power facility,
by B. Brooks and others. Atomics International
A Division of North American Aviation, Inc. ,
Canoga Park, Calif. Dec 60. Contract AT(11-1)-
GEN-8. 40pj. Order from OTS. 75 cents.
NAA-SR-5463
Heterogeneous, liquid fuel, beryllium moderated
reactor, by fl. Vleustadt. North American Avia-
tion, TiTc. , Cbwney, Calif. July 51. Decl.
March 2, 1960. 31p. Order from LC. Mi $3. 00,
ph$6.30. I NAA-SR-Memo-45
Intra-cell neutrOn densities--I*art II. 3/4 inch, 1
inch, 1 1/4 ijich, 11/2 inch and 2 inch diameter
natural uranmm rods, by D. Woods and others.
North American Aviation, Inc., Downey, Calif.
Mar 52. Dedl. June 13, 1960. 106p. Order
from LC. N^ $5.70. ph $16.80.
NAA-SR- Memo-244
Test erf the ball
North Ameri
Feb 55. Decjl
Order from
afety device mockup, by E. Phillipa
n Aviation, Inc. , Downey, Calif.
November 13, 1958. 21p.
:. Mi $2.40. ph$3.30.
NAA-SR-Memo-1282
Heterogeneous s ystems and minimum critical mass,
by A. V. Cariipise. Atomics International. Divi-
sion of NorthjAmerican Aviation, Inc., Canoga
Park.Calif . pec 56. 27p. Order from LC.
Mi $2.70, ph
$4.80.
NAA-SR-Memo-1807
sodium freeze seal cooling
Reactor coolant jpumps :
loads, by R. w. Atz. Atomics International.
A Division ofi North American Aviation, Inc. .
Canoga Park, Calif. Jan 57. 12p. Order from
LC. Mi$2.<^, ph$3.30.
NAA-SR-Memo-1843
(^RE low flux (ixperiments and approach to full
xpe
er, byR.!l^. Varnes. Atcxnics International
Division of North American Aviation, Inc. ,
I.'
Canoga Park, Calif. Oct 57. 36p. Order from
LC. Mi $3.00, ph$6.30.
NAA-SR-Memo-I978
Lattice calculations using the IBM-704 Wanda-2-
diffusion code, by W. O. Allen and others.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park, Calif. Aug 57
8p. Order fcmLC. Mi $1.80, ph $1.80.
NAA-SR-Memo-2033
Summary report on OMR maritime R and D shieldiM
studies from March 11 1957 to June 30, 1957,
by D. S. Duncan and H. O. Whittum. Atomica
International. Division of North American Avia-
tion, Inc. , Canoga Park. Calif. 46p. Order
from LC. Mi $3.30. ph $7.80.
NAA-SR-Memo-2044
CMR nuclear parameter survey , by W. W. Davis
and W. D. Leggett. Atomics International. A
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Aug 57. 27p. Order from
LC. Mi $2.70, ph$4.80.
NAA-SR -Memo-2073
Strain gage installation on main secondary sodium
system of SRE, by L. P. Inglis. Atomics Inter-
national. Division of North American Aviation,
Inc., Canoga Park, Calif. Aug 57. 20p. Order
from LC. Mi $2.70. ph $4.80.
NAA-SR -Memo- 2077
Reflector control of OMR, by W. W. Davis. Atom-
ics International. AlJivision of North AmericM
Aviation. Inc., Canoga Park, Calif. Oct 57.
5p. Order from LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-2177
Maintenance procedure for SRE main primary sodi-
um pump, by H. Strahl and H. Chapman. Atom-
ics International. Division of Ncrth American
Aviation, Inc. , Canoga Park. Calif. Oct 57.
lip. Order from LC. Mi $2.40, ph$3.30.
NAA-SR-Memo-2201
An electronic circuit design for providing an indica-
tion when the Mark 11 safety rods are released
from the holding magnet, by R. J. Hall. Atomics
International. Division of North American Avia-
tion, Inc., Canoga Park, Calif. Oct 57. 5p.
Order from LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-2207
Thermal stresses from radial exponential heat gen-
erator in the thermal shields, vessel wall and
biological shield, by C. O. Peinado. Atomics
Internatinnal. A Division of North American
Aviation, Inc. , Canoga Park, Calif. Oct 57.
518
Up. Onkr t^txn LC. Mi $2.40. ph $3.30.
NAA-SR -Memo -22 13
Organic energy absorption in OMRE and in metal
— and UO2 ^led OMR. by V. Keshishian. Atomics
International. Division of North American Avia-
tioo, Inc.. Canoga Park, Calif. May 58. 16p.
Order from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-2484
Preliminary estimates of radioactivity in process
wastes from SENN 150 BMW organic reactor, by
A. R. Piccot. Atomics International. Division
of North American Aviation, Inc. . Canoga Park.
Calif. Mar 58, lOp. Order from LC. Mi $2. 40,
ph$3.30. NAA-SR-Memo-2526
SRE experimental Scrain data November 20, 1957,
by K. W. Foster. Atomics International. A
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Mar 58. 17p. Order from
LC. Ml $2.40, ph$3.30.
NAA-SR-Memo-2578
Tltennal neutron source distribution in an OMR unit
cell, by W. D. Leggett. Atomics International.
A Division of North American Aviation, Inc. ,
Canoga Park, Calif. Apr 58. 6p. Order from
LC. Mi $1.80. ph$l.80.
NAA-SR-Memo-2648
A blackness nDeasurement of an S.R.E. fuel cluster,
by J. W. Zink and W. A. Horning. Atomics
International. A Division of North American
Aviation. Inc.. Canoga Park, Calif. May 58.
9p. Order from LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-2711
HNPF plant heat balances for a design gross load of
WeMW, by T. L. Gershun. Atomics Interna-
tional. A Division of North American Aviation,
Inc., Canoga Park. Calif. June 58 20p. Order
from LC. Mi $2.70, ph $4.80.
NAA-SR-Memo-2763
Design of an eddy-current brake for a sodium-cooled
nuclear power reactor, by R. S. Baker. Atomics
International. A Division of North American
Aviation, Inc.. Canoga Park, Calif. July 58.
I7p. Order from LC. Mi $2. 40. ph $3.30.
NAA-SR-Memo-2881
Ciric indexing using closed circuit television, by
M. L. PeelgrenT Atomics International. Divi-
•ion of North American Aviation, Inc. , Canoga
Park, Calif. Aug 58. 5p. Order from LC.
Mi $1.80, ph$1.80. NAA-SR-Memo-2930
Reactor burnup of poisons in commercial graphites,
by S. C. Carniglia. Atomics International. A
Division of North American Aviation. Inc.,
Canoga Park. Calif. Sep 58. 20p. Order from
LC. Ml $2. 40, ph $3. 30.
NAA-SR-Memo-3092
SRE nitrogen gallery seal, by R. P. Neblker.
Atomics International. Division of North Ameri-
can Aviation, Inc. . Canoga Park. Calif. Aug 58.
7p. Order from LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-3105
Converting data from the water test loop to sodium,
by R. D. Welsh. Atomics International. A Divi-
sion of North American Aviation, Inc. , Canoga
Park, Calif. Oct 58. 9p. Order from LC.
Mi $1.80, ph$1.80. NAA-SR-Memo-3128
Neutron and gamma flux survey of the SRE instru-
ment thinibles, by H. P. Donohue. Atomics
International. A Division of North American
Aviation, Inc. , Canoga Park, Calif. Oct 58.
14p. Order from LC. Mi $2. 40. ph $3. 30.
NAA-SR-Memo-3131
Design and fabrication erf SRE core heater protective
tubes, by R. L. Shelby. Atomics International.
A Division of North American Aviation, Inc. ,
Canoga Park, Calif. Oct 58. 6p. Order from
LC. Mi $1.80. ph$1.80.
NAA-SR-Memo-3134
Reactivity of MC-2-2 in the SRE, by R. W. Wood-
ruff. Atomics International. A Division of North
American Aviation, Inc. , Canoga Park, Calif.
Oct 58. 5p. OrcferfromLC. Mi $1.80,
ph $1 . 80. NAA-SR-Memo-3142
PIQUA-OMR neutron detector shielding, by D. S.
Duncan. Atomics International. >CDivision of
North American Aviation, Inc. , Canoga Park,
Calif. Nov 58. 13p. Order rrom LC. Mi$2.40.
ph$3.30. NAA-SR-Memo-3343
Fuel bum-up study of the U-Moly. Fueled Hallam
reference core, by K. J. Doyas. Atomics Inter-
national. A Division <rf North American Aviation,
Inc. Canoga Park, Calif. Jan 59. 6p. Order
from LC. Mi $1.80, ph $1.80.
NAA-SR -Memo- 3520
Emended scale temperature recorder, by R. W.
Madsen. Atomics International. Division at
North American Avaition, Inc. , Canoga Park,
Calif. Jan 59. 4p. Order from LC. Mi $1.80,
ph$1.80. NAA-SR-Memo-3522
519
Reactivity of a Zircaloy II thimble in the SRE,
R. W. Woodruff. Atomics International. Divi-
Bioo of Nortti American Aviation, Inc. , Canoga
Park. Calif. Jan 59. 9p. Order from LC.
Ml $1.80, phi$1.80. NAA-SR-Memo-3523
Multigroup analysis of neutron flux and current
changes in a reactor due to a 'slab" controTrod,
by r7 L. Motire. Atomics Intemadonal. Divl-
sloo of North American Ayladoa, Inc. , Canoga
Park. Calif. Feb 59. i2p. Order from LC.
Ml $2.40, ph,$3.30. NAA-SR-Memo-3535<Rev.)
kdlologlcal ha2^]
W. F Kunkel
oi North American Aviation. Inc. , Canoga Park,
Calif. Mar S^. I2p. Order from LC.
Mi $2.40, ph|$3.30. NAA-SR-Memo-3654
Piqua OMR-apadlng of cavity liner cooling pipes, by
S. Yee. Atomics International. A Division of
North Ameri(}an Aviation, Inc. , Canoga Park,
Radiological haards of calaodria core renaoval, by
Kunkei Atomics International. Division
Calif.
ph$3.
Apr 5f
30
lOp. Order from LC. Mi $2. 40,
NAA-SR. Memo- 3735
SRE -Edison plaijt control systeni, by R, J. Hall.
Atomics Inteilnadoaal. Diviaion of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. Apr 59.
28p. Order f^xnLC. Ml $2.70, ph $4.80.
NAA-SR-Memo-3760
Television monilor- -SRE fuel coffin, by D. K. Dar-
ley and ]. D. Smith. Atomics International.
Division of North American Aviation, Inc. , Cano-
ga Park, Calil. May 69. 7p. Order from LC.
Mi $1.80, ph $1.80. NAA-SR-Memo-3844
Plux distribution measurements in C^R cores, by
V. A. Swansqn. Atotnics International. Divi-
sion of North jAne rlcan Aviation, Inc. , Canoga
Park, Calif. May 59. 1^. Order from LC.
Mi$2.40, phi$3.30. NAA-SR-Memo-3872
"
Cooceptual desiai study erf OMRE modifications, by
W. B. Wolfe. Atomics International. A Division
at North American Aviation, Inc. , Canoga Park.
Calif. Iuly5^. 5^. Order from LC. Mi $3. 60.
ph$9.30. ! NAA-SR -Memo- 3881
d inspf
Fabrlcatioo and inspection techniques for die SRE
alternate calydria core, by C. L. Pecklnpaugh.
Atomics Interlnational. thvision of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. May 59.
18p. Order f|-om LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-3920
Radial statistica
weight for the SRE,
Woodruff Adamlcs International.
by R. W.
Division ot
North American Aviation, Inc. , Canoga Park,
Calif. May 59. 4p. Order from LC. Mi $1.80,
ph$1.80. NAA-SR-Memo-3934
Analysis of OMRE waste gas, by H. M. Gilroy.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park. Calif. Jan 60.
2^. Order from LC. Ml $2.70, ph $4.80.
NAA-SR-Memo-4130-
Actlvation analysis erf cloaed circuit shield cooling
water, by W. A. Rhoades. Atomics International.
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Oct 59. 14p. Order from
LC. Mi $2.40, ph$3.30.
NAA-SR-Memo-4214
Cloaed circuit cooling water purification system, bjr
H. O. Charnock. Atomics International. Divi-
sion of North American Aviation, Inc. . Canofi
Park, Calif. Aug 59. 9p. Order from LC.
Ml $1.80, ph $1.80. NAA-SR-Menno-4235
Sununary of creep tests on the Piqua OMR flat-platt
fuel element, by C. R. Davidson and S. Bain.
Atomics International. Division of North Amri-
can Aviation, Inc. , Canoga Park, Calif. Aug S9.
23p. Order from LC. Mi $2.70, ph$4.80.
NAA-SR-Memo-4259
Cooling of Piqua OMR source element, by D. J.
McGoff. Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. Aug 59. 12p. Order from LC. Mi $2. 40,
ph$3.30. NAA-SR-Memo-4296
Power flow comparator. 2nd interim report, by H.
Schlein. Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. Aug 59. 6p. Order from LC. Ml $1.80,
ph$1.80. NAA-SR-Memo-4302
Calculation of the temperature distribution in the
HNPF moderator can, by W. H. East. Atomic*
International. Division of North American Avia-
tion, Inc., Canoga Park. Calif. Oct 59. 6p.
Order from LC. Ml $1.80, ph $1.80.
NAA-SR-Memo-4310
Development test of the HNPF hangerrod disconnea-
latcnes and disconnect actuator" by M. L. Pel-
gren. Atomics International. Division of North
American Aviation, Inc. , Canoga Park, Calif.
Dec 59. 17p. Order from LC. Mi $2.40,
ph $3. 30. NAA-SR-Memo-4335
520
Piqua OMR pU>»t steady-state control program, by
"" w. Kushan. Atomics International, ui vis ion of
North American Aviation, Inc. , Canoga Park,
Calif. Oct 59. 14p. *Order from LC. Mi $2.40,
ph$3.30. NAA-SR-Memo-4341
Load-deflection tests of HNPF reactor vessel bel-
lows, by G. M. Merritt. Atomics International.
IHvTsion of North American Aviation, Inc. ,
Canoga Park, Calif. Sep 59. 9p. Order from 1
LC. Mi $1.80. ph$l.80.
NAA-SR-Memo-4346
Temnerature distribution in region of fuel slug end,
by D. J. McGoff. Atomics International. Divi-
sion at North American Aviation, Inc. , Canoga
Park. Calif. Sep 59. 6p. Order from LC.
Mi $1.80. ph$1.80. NAA-SR -Memo-4347
Flaah distillation of synthettic OMKE coolant, by
J. W. Florence. Atomics International. Di vis ion
of North American Aviation. Inc. . Canoga Park,
Calif. Oct 59. 9p. Order from LC. Mi $1.80.
ph$1.80. NAA-SR -Memo- 4420
Preliminary fuel burnup study of the 255 MWE ASGR,
by A. L. Aronson. Atomics Interna tion. Divi-
iion of North American Aviation, Inc. , Canoga
Park. Calif. Oct 59. 14p. Order from LC.
Mi $2. 40, ph$3.30. NAA-SR -Memo- 4455
Further nuclear calculations on the 255 MWE
advanced SGR, by A. L. Aronson. Atomics
International. Division of North American Avia-
tion, Inc. . .Caioga Park, Calif. Oct 59. 26p.
Order from LC. Mi $2. 70, ph $4. 80.
NAA-SR -Memo-4461
Evaluation of HNPF mark B drive, by P. F. Shaw.
Atomics International. Division of North Ameri-
can Aviation. Inc. , Canoga Park. Calif. Oct 59.
15p. Order from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-4514
OMR Piqua waste gas treatment system, prototype
aysMtn description and experimental programT
1
by H. M. CilroyandJ. H. Wilson. Atomics
International. Division erf North American Avia-
tion, Inc. , Canoga Park. Calif. Nov 59. 9p.
Order from LC. Mi $1.80. ph $1.80.
NAA-SR-Memo-4593
Thermal-hydraulic analysis of ttie Piqua core, by T
1. D. Wilde. Atomics International. Division
of North American Aviatiem, Inc. , Caioga Park,
Calif. Nov 59. 25p. Order from LC. Mi $2.70,
ph$4.80. NAA-SR -Memo- 4626
GeCTnetrlc budding of a bare truncated sphere, by
D. P. Gamble. Atomics International. DTvialan
of North American Av lation. Inc., Canoga Park,
Calif. Nov 59. 9p. Order from LC. Mi $1.80,
ph $1 . 80. NAA-SR -Memo- 4665
Performance requirements and dynamic response
of Piqua OMR reactor outlet temperature coiigbl
subsystem, by R. L. Detterman. Atomics
International. A Division of North American
Aviation, Inc., Canoga Park. Calif. Nov 59.
65p. Order from LC. Mi $3. 90, ph $10. 80.
NAA-SR -Memo-4671
Vibrational characteristics of an HNPF 19 -rod 5. 0
square inch fuel element mockiy, by J. A. Hagel.
Atomics Intemariooal. North American Aviation,
Inc. , Canoga Park, Calif. Dec 59. 17p. Order
from LC. Ml $2. 40, ph $3. 30.
NAA-SR -Memo-4698
Steam cycles for advanced orgtnic reactor plants,
by G. R. Terpe. Atomics International. Divi-
alon of North American Aviation, Inc. , Canoga
Park. Calif. Dec 59. lOp. Order from LC.
Mi $2. 40. ph$3.30.
NAA-SR-Memo-4736 (Rev. A)
Preliminary evaluation of the mechanism of fuel
element fouling, by P. Shroff and C. Goetz.
Atomics International EMvlsion of North American
Aviation, Inc. , Canoga Park, Calif. Dec 59.
19p. Order from LC. Mi $2.40, ph $3. 30.
NAA-SR-Memo-4750
Piqua OMR high boiler disposal prototype: s^tem
description and operating experienoe, by R. R.
Stiens. Atomics International. Division of
ntemational
North American Aviation. Inc. , Cane>ga Park,
Calif. Feb 60. 19p. Order from LC. Mi $2. 40.
ph $3. 30. NAA-SR-Memo-4790
Thermal and hydraulic preliminary design method
for the OMrE U-alloy (4th) core loading, by
D. B. Sedgley. Atornics International. Division
of North American Aviation, Inc. , Canoga Park,
Calif. Dec 59. 1^. Order from LC. Mi $2. 40,
ph $3. 30. NAA-SR-Menu>-4810 (Rev. A)
Evaluation erf the use of delayed neutron and gaseoua
fission product monitoring for detection ot fuel
cladding failures in advanced OMR's, by C. C.
Weeks. Atomics International. Diviaion of
North American Aviation, Inc. . Canoga Park.
Calif. Jan 60. 16p. Order from LC. Mi $2.40,
ph$3.30. NAA-SR -Memo -4866
521
Some effects of ifuel element geometry upon the
nuclear, thermal and hydraulic performance of
an OMRE core, by R. W. Hardy and otherB.
Atomics Intepraational. Division of North Ameri-
caa Aviatioai Inc. , Canoga Park, Calif. Jan 60.
19p. Order {from LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo-4907
Radial temperature profile of sodium pool boiling
by H. H, Cai^f. Atomics
heater assembly,
Internationa 1). uTvision erf North American Avia-
tion. Inc. , danoga Park, Calif. Feb 60. 8p.
Order from tx:. Mi $1.80, ph $1.80.
1 NAA-SR-MenK»-49i4
Study of fuel terpperature and flow effects of plug-
ging in SRE lK*el. by R. C. Noyes. Atomics
Inter natiooaC Division of North American Avia-
tion, Inc. , (^noga Park, Calif. Mar 60. 33p.
Order from \JC. Mi $3. 00, ph $6. 30.
1 NAA-SR-Memo-4952
A preliminary 'lucjear analysis of a sodium cooled
fast reactor ISCFR) wity UC fuel elements in a
skewed hexa " " ' " ' ' ~
atonal array, by H. Jackel.
International, Division of North Amer
tion. Inc. Qanoga Park
Order from LC.
Bibli
Atcxnics
rican Avia-
Feb 60. 18p.
Calif
Ml $2.40, ph$3.30.
NAA-SR-Memo
50II
ibliomraphy of treports on fast reactor technology,
byB. R. Hajjward and M. Bloomfield. Atomics
Internationali Division of North American
Aviation, In({. , Canoga Park, Calif. Mar 60.
lip. Order jfrom LC. Mi $2. 40. ph $3. 30.
NAA-SR-Memo-5054
Relatiooahip of t'adlation units to radiation dair.age
for SNAP -2 teactor systems, by F. D. Anderson.
Atomics International. Division of North Ameri-
can Aviation,
13p. Order rom LC.
Inc., Canoga Park, Calif. Mar 60.
Mi $2. 40, ph $3. 30.
NAA-SR-Memo-5059
ement o( radiation about die graphite critical
facility, by (j. H. Skeen. Atomics International.
Division of North American Aviation, Inc.,
Canoga Park,! Calif. Mar 60. lip. Order front
LC. Mi $2.^0, ph$3.30.
NAA-SR-Memo-5064
ition of graphite critical assembly, by
>ni AtCMmics International. Division
Power calibrati<
— C. H. Skeer
of North American Aviation, Inc. , Canoga Park,
Calif. Mar ^. 5p. Order from LC. Mi $1.80,
ph$1.80. NAA-SR-Memo- 5065
Reactor power calibration by the source insertion
technique, b;
E. L. ZimmermalT Atomics
International. Division of North American Avia-
tion. Inc. , Canoga Park, Calif. Mar 60. 9p.
Order from LC. Ml $1.80, ph $1.80.
NAA-SR-Memo-5082
Control rod test furnace control system, by J . W.
Crowe. Atomics International. Division of
North American Aviation, Inc., Canoga Park,
Calif. Mar 60. 19p. Order from LC. Mi $2. 40,
ph$3.30. NAA-SR-Memo-5085
Hydraulic teats of the 5- rod and dummy SRE fuel
elements, by R. ]. Begley. Atomics International
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Apr 60. I4p. Order from
LC. Mi $2.40, ph$3.30.
NAA-SR-Memo- 5124
Flux measurements In the Piqua GMK critical as-
sembly, by R. J. Tuttle. Atomics International,
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Apr 60. 18p. Order from
LC. Mi $2.40. ph$3.30.
t; NAA-SR-Memo- 5145
Analog computer study of the 255 Mw ASGR core
kinetics, by H. H. Cappel. Atomics InternatiooaL
Division of North American Aviation, Inc. ,
Canoga Park, Calif. Mar 60. 38p. Order frcn
LC. Mi $3. 00, ph$6.30.
NAA-SR-Memo-5146
Analysis of OMRE waste gas, by H. M. Gilroy.
Atomics International. Division of North Ameri-
can Aviation, Inc. . Canoga Park, Calif. May 60.
34p. Order from LC. Mi $2.70, ph $4.80.
NAA-SR-Memo-5158
SNAP-II reactor core materials, by J. V. Facha.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park, Calif. Apr 60.
Contract AT-il-l-GEN-8. 12p. Order from
LC. Mi $2.40, ph$3.30.
NAA-SR-Memo-5166
A simplified two group method for calculating re-
actor lifetime Dehavior, by R. Sevy. Atomic*
International. Division of North American
Aviation, Inc. , Canoga Park, Calif. June 60.
12p. Order from LC. Mi $2.40, ph $3.30.
NAA-SR-Memo- 51 68 (Rev. A)
Test results on the power/flow comparator and
flow /flow ratio computer for the HNPF plant
protective system, py E. J. Westerweller.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park, Calif. Apr 60i
I2p. Order from LC. Mi $2. 40. ph $3.30.
NAA-SR-Memo- 5218
522
Design tests, fuel channel exit temperature and
— rate change of temperature circuits, by D. E.
Brown ana E. J. Westerweller. Xtbmics Inter-
national. Division of Ncrth American Aviation,
Inc., Canoga Park, Calif. Apg 60. Up. Order
LC. Mi $2. 40, ph $3. 30.
NAA-SR-Memo- 5222
5MWt sodium deuteriiun reactor experiment- -de-
gign report, by S. Davis. Nuclear Development
Corporation of America, White Plains, N. Y.
June 59. Contract AT(30-l)-2303. 42p. Order
from LC. Mi $3.30, ph $7.80. NDA-84-22
A »tudy of wet steam as a reactor coolant. Quarter-
[y technical progress report for the period Janu-
ary 1 1960 through March 31 1960. Nuclear
Development Corporatinn, of America, White
PUins, N. Y. Apr 60. Contract AT(30-l)-2303.
27p. Order from LC. Mi $2.70, ph $4.80.
NDA-2132-3
Further examination of seawolf (S2G) components.
Nuclear Development Corporation, of America,
White Plains, N. Y. Jan 60. Contract AT(ll-l)-
732. 40p. Order from LC. Mi $3. 30, ph $7. 80.
NDA-2114-2
Power reactor program. Progress report to E. I.
Ai Pont de hfemours and Company for the P^jJoS
November 1, 1958 through Novernber 30. 1958,
with high conversion ration. Qaarterly progress
report for May 1 , to July 31, 1^59. Cornbustion
Engineering, Inc. , Nuclear Division, Windsor,
Conn. 1959. Contract AT(30-l)-2379. 36p.
Order from LC. Mi $3. 00, ph $6. 30.
NYO-2701
Concerning several methods for the removal of
fission products from a gas cooled reactor, by
K. H. Quasebarth and omers. University of
Virginia, Research Laboratories for Engineering
Sciences, Charlottesville, Va. Feb 60. Con-
tract AT(30-l)-2207. 32p. Order from LC.
Mi $3. 00, ph $6. 30. NYO-2708
Study of remote military power applications. Re-
port no. 4 Thule Air Base, Greenland! Kaiser
Engineers, Division of Henry J. Kaiser Company,
Oakland, Calif. Jan 60. Revised July. 1960).
Contract AT(30-1)-2441. I22p. Order from
y OTS. $2.75. NYO-2940
ications. Re-
can Air Defense
itner
by F. S. Gardner and otners. Nlclear Metals,
Inc., Concord, Mass. Feb 59. Contract AT
(30-l)-1565. 20p. Order from LC. Ml $2.70.
pfr$4.80. NMI-4383
Study of remote military power appl
pon no. 5 Nor ad Norm American
Command Operation Center! Kaiser Engineers,
Division of Henry J. Kaiser Company, Oakland.
Calif. Jan 60. (Revised July, 1960). Contract
AT(30-1)-2441. 73p. Order from OTS $2.25.
NYO-2941
Study of remote military power applications. Re-
" " e, Rocky' Mountains Area,
vision of Henry J. Kaiser
Jan 60. (Revised
July, 1960). Contract AT(30-1)- 2441. 79p. Order
from OTS. $2.25. NYO-2943
jrt no. 7. Super Sa
po]
Kaiser Engineers,
Company, Oakland, Calif
Power reactor
• program
Ner
uly 1, 1959 through.
uclear Metals. Inc."
Contract AT(30-l)-1565
Mi $2.70, ph$4.80.
Progress report to E. I. Study of reniote military power arolica
i Comoanv for tte oeriod port no. 6. Fourth U.S. ASA field
lications. Re-
du Pont de Nemours and Company for the period
' ■ - - 31, 1959 byS. Wrow
cord, Mass. Oct 59.
23p. Order from LC.
NMI-4396
i
station.
Kaiser Engineers, Division
Prcyess report on MIT fuel cycle study project.
Period covered September 15, 1957 to March 15,
1958, by T. T. Shanatrom and others. Massa-
diusetts Institute of Technology, Cambridge,
Mass. Apr 58. Contract AT(30-1)- 2073. 57p.
Order from LC. Mi $3. 60. ph $9. 30.
NYO-2128
Heterogeneous reactor calculation rnethoda. Quar-
If ^y progress report no. 3 for October 1 to
Uecember 31. 1959. by C.N. Klahr and others.
Trg. Inc. . Syosset, N. Y. 1959. Contract AT
(30-l)-2375. 68p. Order from LC. Ml $3. 60,
ph$9.30. NYO-2675
Study of slightly-enriched uranium- -water lattices
Asmara, Eritrea,
of Henry J. Kaiser Company, Oakland, Calif.
Jan 60. (Revised July, 1960). Contract AT(30-1)-
2441. 71p. Order from OTS. $2.25.
NYO-2942
Study of remote military power a^ylications. Re-
port no. a, Nike-Zeus far site. Kaiser Engi-
neers, Division of Henry J. Kaiser Company,
Oakland. Calif. Jan 60. (Revised July, I960).
Contract AT(30-l)-2441. 76p. Order from OTS.
$2.25. NYO-2944
Study of reinote military power a
>rt no. 9, Inchon, Korea ^
r
llcation. Re-
rt no. 9, Inchon, j^orea. Kaiser Engineers,
ivision of Henry J. Kaiser Company, Oakland,
Calif. Jan 60. (Revised July, I960). lOOp.
Order from 015. $2.75. NYO-2945
Study of remote military^ power applications .
Re-
port no. 10. Atlantic Barge! Raiser Engineers,
523
DlviBlon of Henry J
-CaUf. Jan 60.
AT(30-1)-24H I
Study (A remote
Kaiser Company, Oakland,
(Revlaed July, 1960). Contract
lOOp. Order from OTS. $2.75.
NYO-2946
military power applicationa. Re-
port no. 11, 'U. S. Naval AirlPacllity McMurdo
Sound, Antarctica. Kaiaer Engineers, Division
of Henry J. iCaiser Company, Oakland, Calif.
Feb 60. (Reilsed July, 1960). Contract AT
(30-l)-2441.
82p. Order from OTS. $2. 25.
NYO-2947
Study of remote military power applications. R<
on no. 12, ^valuation and selection of appli
Re-
le reactor concepts. Kaiser Engineers, Division
of Henry J. KUiser Company, Oakland, Calif.
Jan 60. (Revised July, 1960). Contract AT(30-1)-
2441. top. Order from 015. $1.50.
NYO-2948
StxKly of ronxjte military power applications Hypo-
tfaeticai site. Kaiser fengineers. Division of
Henry J. Kaiser Company, Oakland, Cfelif. Feb
60. (Revised July, 1960). Contract AT(30-1)-
50.
NYO-2978
2441. 93p. Order from OTS. $2.
The pebble bed reactor progri
report for July 1, 1959 through Septi
1959. Sainderson and Porter, New York
res 8 rei
307
•am. Quarterly prog-
59 through September
Oct 59. Contract AT(30-l)-22a7. 21p. Order
fromLC. Mi $2. 70. ph $4. SO. NYO-9066
1
The pebble bed teactor program. Quarterly pr^
id reac
ogram. Quarterly prog-
r 1, 1960 mrough March
res 3 report ffcr January I, 1960 through Marc
31, 1960, Sanderson and Porter, New York.
N.Y. I960. Changed from OFFICIAL USE ONLY
August 16. 1960. Contract AT(3O-l)-2207. 48p.
Order from UC. Mi $3. 60, ph $9. 30.
NYO-9067
An evaluation of time-dependent, materials informa
tion for purposes of pressure ves8el design and
tlysisT r ital ^^P°^ ' J^>**g j. *"d Task II.
by L. U. Rastrelli. Southwest Research Institute
San Antonio, Tex. July 60. Contract AT(30-1)-
2146. 233p. j Order from OTS.
$3.00.
NYO-9376
Tte aircraft nuclear propulalon project quarterly
progreaa report for period et>din£ August 31, '
1955. by C. 8. Ellis and W. E. Thompson. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Dec 60. Decj. widi deletions October 1959. Con-
tract W-7405*eng-26. 64p. Order from LC.
Mi $3.90. ph$10.80. ORNL-858
Aircraft nuclear
propulsion project quarterly prog-
ress report for period ending December 10, 195Q
by C. B. Ellis and W. B. C«treli. Oak HidgeT"
National Laboratory, Oak Ridge, Tenn. Feb 51.
Decl. with deletions November 10. 1959. Cob-
tract W-7405-eng-26. 160p. Order from LC.
Mi $8. 10. ph$27.30. ORNL-919 (Del.)
The sut>ercritical water reactor. A report fo Oak
Ridge. National Laboratory Nuclear Develop-"
ment Associated, Inc. . milte Plains. N. Y.
Feb 52. Decl. with deletions September 21,
1959. Contract AT(30-1)- 1065. 129p. Order
fromLC. Mi $6.90, ph$21.30.
ORNL-1177(Db1.)
Aircraft nuclear propulsion project quarterly pri
' period end" " "~
by W. i. Cottrell. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. 1952. Decl. with dele-
tions November 16, 1959. Contract W-7405-
eng-26. 156p. Order from LC. Mi $7.80.
ph $25. 80. ORNL- 1439 (Del.)
reaa report for period eiKling December lOJ 1952
Aircraft nuclear propulsion project quarterly proy-
ress report for period ending June 10. 1953.
Oak Rioge National Laboratory, Oak Ridge, Teon.
July S3. Decl. with deletions October 28, 1959.
Contract W-7405-eng-26. 106p. Order from
LC. Mi $6.00, ph$18.30. ORNL- 1556 (Del.)
Aircraft nuclear propulsion project quarterly
ress report for ths period ending Septembc
1953. by W. B. Cottrell. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Nov 53. Dele,
with deletions November 12, 1959. Contract
W-7405-eng-26. 124p. Order from LC.
Mi $6.30. ph$19.80. ORNL- 1609 (Del.
An evaluation of die corroaion and oxidation regi>-
tance of high -temperature brazing alloys. Period
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending September \0,
1955, by A. W. Savolainen. Oak Ridge Nationil
Laboratory. Oak Ridge, Tenn. Nov 55. Decl.
with deletions on October 22. 1959. Contract
W-7405-eng-26. 175p. Order from LC.
Mi $8.40. ph $28.80. ORNL- 1947 (DbL)
tory. Oak Ridge, Tenn. Mar 56. Decl. widi
deletions October 22. 1959. Contract W-7405-
eng-26. 206p. Order from LC. Mi $9. 30.
ph $31.80. ORNL-2012 (Pt. I. II, IIlXDel-)
524
covered Jufy 1954 to September 1955. by E. E.
Hcrffman and others. Oak Ridge N«ional Labora-
tory, Oak Ridge. Tenn. Nov 56. Decl. October
9. 1959. Contract W-7405-eng-26. 40p. Order
fromLC. Mi $3.00, ph $6.30. ORNL-1934
Aircraft nuclear propulsion project quarterly prog-
— fess report for period ending September 10,
1956. Oak Ridge National Laboratory, Oak Ridge,
^^. Dec 56. Decl. with deletions October 28,
1959, Contract W-7405-eng-26. 265p. Order
fromLC. Mi $11. 10. ph $47.90.
'ORNL-2157(Pt«. l-5)(Del.)
Aircraft nuclear propulsion project Quarterly prog
reae report for the peri oa ending December 3l"
1957. Oak Ridge National Laboratory, Oak Ridge
T^nn. Apr 58. Decl. with deletions November
4. 1959. Contract W-7405-eng-26. 222p.
Order from LC. Mi $9. 90. ph $34. 80.
ORNL-2440(Del.)
Molten-salt reactor program quarterly progress
report Jot {period ending July 31, I960, by H. G.
Macnierson. Oak Ridge National Laboratory,
Oak Ridge. Tenn. IndJ. Contract W-7405-eng-
26. 89p. Order from OTS. $2.25.
ORNL- 301 4
Monthly technical report for period November 1959.
Power Reactor Development Company, Detroit,
Mich. 1959. Contract AT(ll-l)-476. jZSp.
Order from LC. Mi $2.70. ph $4.80.
PRDC-TR-29
Mondily technical report for December 1959. Power
Reactor Development Company, Detroit, Mich.
1959. Contract AT(ll-l)-476. 38p. Order
from LC. Mi $3. 00, ph $6. 30.
PRDC-TR-30
ICinetic stixlies of heterogeneous water reactors.
Annual summary report - 1959, by R. F. Kemp
and others. Thompson Ramo Wooldridge Inc. .
Ramo-Wooldridge Division, Research Laboratory.
San Francisco. Calif. Feb 60. Contract AT
(04-3)-l65. 208p. Order from OTS. $2.50.
RWD-RL-167
Hot-area concept for radiation test facilities, by
J. L. Colp. Sandia Corporation. Albuquerque,
N. Mex. Dec 60. 20p. Order from OTS.
75 cents. SCR-235
Ab approximate study of the perforrnance of a re-
actor-heat exchange system, by B. Wilcox.
Saodia Corporadon, Albuquerque, N. Mex.
Aug 59. 147p. Order from LC. Mi $7.20.
ph $22.80. SCTM-276-59-12
An eq)erimental study of the coolant flow distribu-
doo widiln the turret reactor core, by B. Wilcox.
Saodia Corporation, Albuquerque. N. Mex. Dec
59. 37p. Order fromLC. Mi $3.00. ph $6.30.
SCTM-383-59-12
A study of spontaneous ignition of metals. Final
report for April 1, 1959 to July 31, 1960, by~
F. E. Littman and F. M. Oiurch. Stanford Re-
search Institute, Menlo Park. Calif. Aug 60.
Contract AT(04-3)-115. 56p. Order from OTS.
$1.75. SRIA-29
Containment of fragments from a runaway reactor,
by G. B. Huber and others. Sunford Research
Institute. Menlo Prrk. Calif. April 60. Con-
tract AT(04-3)-115. 98p. Order from OTS.
$2.50. SRIA-25
Heavy water power reactor pr
ress report for July 1960.
Office, AEC. A
am.
tions
Order from LC.
Monthly prog-
svannah River Opera-
22p.
Aiken, S. C. 1960.
Mi $2.70, ph$4.80.
SRO-35
Heavy water power reactor program monthly prog-
ress report for August i960. Savannah River
Operations Office. AEC. , Aiken, S. C. 1960.
18p. Order from LC. Mi $2.40, ph $3. 30.
SRO-36
Heat transfer analysis of 3. 5 foot square cylinder
reactor, by W. C. Cooley. Oak Ridge National
Laboratory. Y-12 Area, Oak Ridge, Tenn. July
50. Decl. October 9, 1959. 5p. Order from
LC. Ml $1.80, ph$1.80. TAB-57
The applicability of hig^ production methods to
nuclear power reactor fuel element fabrication,
by C. W. Phillips and others. Ford Motor Com-
pany, Dearborn. Mich. July 56. Decl. Novem-
, ber 10, 1959. 49p. Order from LC. Mi $3. 30,
ph$7.80. TID-5431
Control rod drive mechanism periodic test.
I . Twe Ifth pe rf ornM nee . Core I, Seed I
Section
Duquesne lig^t Company, Shippingport, Pa.
Feb 60. Up. Order fromLC. Mi $2.40.
ph$3.30. TID-5613
Station radiation level survey. Section III. First
performance. Core 1, seed 1. Duqueane Li^t
Company, Shippingport, Pa. Feb 60. lip.
Order from LC. Mi $2. 40. ph $3. 30.
TID-5614
Main unit heat rate tests. Section I. Third per-
formance. Core I, seed I, Duquesne Lipit Com-
pany, Shippingport, Pa. Xug 59. 20p. Order
fromLC. Mi $2.40. ph $3.30. TID-S615
Periodic radiation survey of reactor plant container
and components after'ahutdown''C;' survey.
Section III, 5735. 8 EEPH. Fifdi performance.
S2S
Core I, see< _I. Duquesne Light Company, Ship-
plngport, Pal Feb 60. 6p. Onier from LC.
N4i$l.gO. p^$1.80. TID-5616
Pji^l.
Capped valve ayd D/P cell vent test. Section IL '
^
irst perfortnanceT
t perton
U^t Company, Shippingport,
Order from
LC. Mi $1.80, ph$1.80.
Core I, 8eed 1
Duquense
Feb 60. 6p.
TDD- 5617
Refueling seal to reactor vessel head. Section I.
Core 1. seecj I. Duquesne Light Company, Ship-
pingport, Pa',. Feb 60. 4p. Order from LC.
Mi $1.80, pb $1.80. Tir)-5618
Control air conpitions at the reactor chamber.
Section II. lluquense. Li^t Company. Shipping-
port, Pa. Feb 60. Up. Order from LC.
Mi $2.40. ph$3.30. TID-5619
$2.40. ph$3.;
itio|i
icHJj
A generalization of the theory of flux aynthesia, by
ry of flux aynth
>ll8 Atomic Pow
L. Wachi press. Knolls Atomic
atory, Scheiiectady, N. Y. Feb 60.
from LC. Mi $2. 40. ph $3. 30.
erLabor-
llp. Order
TID-5646
I
Reactor kinetice with the group diffusion model, by
E. L. Wachlpress. Knolls Atomic Power Labor -
atory, Schenecttdy, N. Y. Feb 60. 21p. Order
fromLC. Mi $2.70, ph $4.80. TID-5647
J,
Examinaticn of_components for cnxl and corroeton.
Section I. I^irst "performance. Core I, seed I.
Duquesne Light Company, Shippingport, Pa.
Jan 60. 16p4 Order from LC. Mi $2.40,
ph$3.30. TID-5649
Radioactive wa»te disposal system periodic radiation
monitoring jurvey. Section 11. Corel, seeJT
Duquesne Light dompany, Shippingport, Pa.
Dec 59. 17p
ph $3. 30.
Order from LC.
Ml $2. 40,
TID-5650
k
Main unit heat fate tests. Section I. Second
a per-
formance. Core I, seed I" EXiquesne Light Com-
pany, Shippiiigport, Pa. Jan 60. 23p. Order
from LC.
Mi $2.70,
ph$4.80.
TID-5651
survey of reactor plant container
ta after shutdown "B survey. Sec-
th performance. Core I, seed I .
Periodic radiatij
and cor
tion II.
Duquesne Li^t fcompany, Shippingport, Pa.
E)ec 59. 18pu Order from LC. Mi $2.40,
ph$3.30. , TID-5653
Radiation survey of reactor plant containers and
components after shutdown "D" survey. Section
urve^ of 1
;nts after" ^
III. First performance. Core I, seed I.
1
Duquesne Lig^t Company, Shippingport, Pa.
Dec 59. 7p. Order from LC. Mi $1.80,
ph$1.80. TID-S6S4
ECNG-FWCNG gaa -cooled reactor project progren
review meeting, December 15, 1^59, by R. B. "
Finn, Jr. and L. F. Smith. Xmerlcan Electric
Power Service Corporation, New York, N. Y.
1959. 21p. Order from LC. Mi $2. 40,
ph $3. 30. TID-5663
Fuel handling crane and extraction tool. Section I.
Core I, seed I. Duquesne Light Company, ~
Shi[^ingport, Pa. Jan 60. 5p. Order from LC.
Mi $1.80, ph $1.80. TID-5664
Monthly operating report. December 1959. Du-
quesne Light Company, Shippingport, Pa. 1959.
Contract AT(1 1-1)- 292. 42p. Order from LC.
Mi $3. 30, ph $7. 80. TID-5713
Monthly operating report for January 1960. Du-
quenne Light Company, Shippingport, Pa. 1960.
Contract AT(ll-l)-292. 35p.
Mi $3. 00, ph $6. 30.
Order from LC.
TID-57U
Leveling of extraction tool crane rails. Third per-
formance. Core I, Seed T Duquesne Light Com-
pany, Shippingport, Pa. Feb 60. 7p. Order
fromLC. Mi $1.80, ph $1.80. TID-5715
Plcm coastdown test. Section 1. Second perform-
ance. Core I, seed I. Duquesne Light Company,
Shippingport, Pa. Mar 60. 28p. Order from
LC. Mi $2.70, ph $4.80. TID-5716
Charging pump cavitation test. Section I. First
rrformance. Core I, seed 1. Duquesne Light
ompany, Shippingport, Pa. Feb 60. 6p. Order
fromLC. Mi $1.80, ph $1.80. TID-5723
Pl-2 design summary- -1000 KWfe) portable boiling
water nuclear power plant? Cotnbustion Engi-
neering Inc. , Nuclear Division, Windsor, Coon.
1960. 19p. Order fromLC. Mi $2.40.
ph $3. 30. TID-5742
ECNG-FWCNG gas -cooled reactor project; miniaeg
of progress review meeting, January 14, 1960,
by R. B. Finn, Jr. American Electric Power
Service Corporation, New York, N. Y. Feb 60.
16p. Order fr<Mn LC. Mi $2.40, ph $3.30.
TID-5743
Monthly operating report.
Light Company, Shippir
March 1960
. Duquesne
l96U. Coo-
ippmgport
tract AT(ll-l)-292. 30p. Order from LC.
Mi $3.00, ph$6.30. TID-5944
526
fj^frigg and discharging of demineralizer resins.
— Section VI. First performance. Core I, seed I.
IXjquesne Li^t Company, Shii^ingport, Pa.
Mar 60. 5p. Order from LC. Mi $1.80,
pb$1.80. TID-5757
Control and dynamics per^rmance erf a sodium
cooled reactor power system, by R. D. Hansen
and J. H. Eaton. Microtech Research Company,
Cambridge, Mass. Dec 59. Contract AT(1 1-1)-
666. 185p. Order from LC. Mi $8.70,
ph$30.30. TID-5788
Specificatjona for the phase II construction and in-
stallation of the organic moderated reactor ex-
??riment, national reactor station, Idaho.
comics International. Division of North Ameri ■
can Aviation, Inc., Canoga Park, Calif. June 56.
220p. Order from LC. Mi $9.90, ph $34.80
•nD-5763
Core I control rod drive mechanisms periodic tests.
Section I. Eleventh performance. Duquesne
Light Company, Shippingport, Pa. Mar 60. 14p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-5852
Gore instrumenution calibration. Section V.
Sixth performance. EKiquesne Light Company,
Shippingport, Pa. Mar 60. 17p. Order from
LC. Mi $2. 40, ph$3.30. TID-5853
Periodic radiation survey of reactor plant container
and components after shutdown. Section IjT.
"D" survey, first performance. Core 1, Seed I,
;y, Ii
Duquesne Lig^t Company, Shippingport, Pa.
Mar 60. 7p. Order from LC. Mi $1.80,
ph$1.80. TID-5854
Radiation survey of reactor plant containers and
components after shutdown "D" survey. Section
PL Second perotrmance. Core I, aeed I
Duquesne Light Company, Shippingport, Pa.
Mar 60. 8 p. Order from LC. Mi $1.80,
ph$1.80. TID-5855
Periodic radiation survey of reactor plant contaln-
er and components after shutdown "G" survey
Action V. EEW--4235.5. Core I, seed 1, Du-
quesne Light Company, Shippingport, Pa. Mar
60. 13p. Order from LC. Mi $2.40. ph $3. 30.
TlD-5856
Compa
cBti
rison of fedal monitor readings with radio-
mical sample data? Section l..
__^ Third pef-
seed I. Duquesne Li(^t Com-
formance. Core I
pany, Shippingport, Pa. Mar 60. I9p. Order
fromLC. Mi $2.40. ph $3. 30. TID-5857
Periodic radiation survey. Section 11. 5187.7
EFffi. Third performance. Core I, Seesd I.
Duquesne Lig^t Company, Shippingport, Pa.
Apr 60. I6p.
ph$3.30.
Order from LC.
Mi $2.40,
TID-5858
Calibration of core thermocouples . for 0 -300 F
service. Section I. Core 1, Seed I. Duquesne
Light Company, Shippingport, Pa. Mar 60. lip.
Order from LC. Mi $2. 40, ph $3. 30.
TID-5859
Nuclear instrumentation- -determining source ^
spikes in nuclear instruments. Section I. Du-
q^sne Light Company, Shippingport, Pa. Apr
60, 4p. Order fromLC. Mi $1 80, ph $1.80.
TID-5860
Loss of load tests, core I, seed 1. Duquesne Light
CcHnpany, Shii^ingport, Pa. May 60. 37p.
Order from LC. Mi $3. 00. ph $6. 30.
TID-5941
Reactor plant conuiner integrity test, core I, seed
2. Duquesne Light Company, Shippingport. Pa.
^y 60. 6p. Order fromLC. Mi $1.80.
.. ph$1.80. TID-5942
'I
Periodic radiation survey of reactorplant container
and components after shutdown "o" survey.
5532. 3 EEW. Core L seed 1. Duquesne Light
Company. Shippingport, Pa. May 60. I5p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-5960
Determination of blow-crff tank vent throttle valve
cyerating diaracteristlcs. Section L Dquesne
Light C^pany, Shippingport, Pa. Oct 59. 5p.
Order from LC. Ml $1.80, ph $1.80.
TID-5961
Periodic radiation survey erf reactorplant container
and components after shutdown 'TT" survey"!
Corel, seed 1. Test results DLCS-184d303
(T- 61 2076). Duquesne Light Company, Shipping -
port, P^. May 60. lOp. Order from LC.
Mi $1.80, ph$1.80. TID-5962
Examination of ccanponents for crud and corrosion
fpressurizer heaters and heater wells) core I,
Seed 1. Duquesne Light Company, Shippingport,
Pa. May 60. dp. Order from LC. Mi $1.80,
ph$1.80. TID-5963
Core I control rod drive mechanistns periodic tests,
addendum I . U)re I, seed 1. Duquesne Light
Cmnpany, Shippingport, Pa. May 60. lOp.
Order from LC. Mi $1.80, ph $1.80.
TID-5964
527
ussn
V5
;tl4e
Reactivity lifetii^ 3813.0 to 4948.0 EE PH. ccwre I,
Duqufesne Light Company, Shii^ngport,
Xpr 60. 205p.
ph $31.80.
Order from LC. Mi $9. 30.
TID-5965
Survey of the raAatioo levels in the conmnment
vesael of tfaeEorico Fermi atomic power pfant.
Part V. Gamjna radiation levela on the operating
floor of the cqntainment building, a. Levels
above the equipment compartment. Technical
memorandum no. 16 . byW. P. Chaltron and
H. E. Hungerfof^r Atomic Power Development
Associates. L ic. , Detroit, Mich. Dec 59. Con-
tract AT(ll-l 1-476. 47p. Order from LC.
Mi $3. 30, ph >7.80.4
TID-6032
Detailed coocept^al design of the graphite primary
shield for the ^Enrico Fermi fast breeder reac-
tor. Technicil memorandum no. 23,byR. J.
Beaudry and others. Atomic Fewer Deve lopment
Associates, Isc. , Detroit, Mich. Dec 59. Con-
tract AT(ll-li-476. 98p. Order from LC.
Ml $5. 40. ph |15. 30. TID-6033
Heavy water poy^r reactor program monthly prog
'"' 1960. Sa
ress
avannah River Oper-
atioos Operations URlce, ABC. Aiken, S. C.
1960. ISp. QrderfromLC. Mi $2.40, ph $3. 30.
TID-6a77
rmort for May 1
s Operations Oni
Monthly operating report for October 1958, by G.
Rifendifer.
port, PA.
from LC. Ml
iquesne Light Company, Shipping -
Contract AT(ll-l)-292. 37p. Order
$3.00, ph$6.30. TID-6092
Monthly operating report for May j 959. Duquesne
Light Company, Snippingport, ~ '"
tract AT(1 1-13
Ml $3.00. ph
Mootfaly operatir
"u Compar
lRi7~1959. Con-
37p. Order from LC.
TID-6097
13^
(11 -I)- 292.
ph $6. 30.
ioort for June 1959.
Snippingport. Pa.
Order from LC.
Duquesne
Contract AT
Mi $3. 00,
TID-6098
Monthly operatl
"it Compa
ratlr
Light
tract AT(l 1 - 1)
report for October 1959. Duquesne
Shippingport, Pa. 1959. Con-
-292.
Ml $3.00, ph|6.30.
33p. Order from LC.
TID-6099
A method for measuring the specific activity of radio-
active coolant; in a pipe, by E. C^apek and others.
General Dynatnics Corporation, Electric Boat
Division, Groton, Conn. Feb 60. 27p. Order
from LC. Mi] $2. 70. ph $4.80. TID-6116
Reflector albectai and dieir use in simple reactivity
lifetime calctaations, by A. J. Goodjohn and others
simpl
Goodi<
and others. General Atomic Division, General
Dynamics Corporation, San Diego. Calif. Feb
60. Contract AT(04- 3)- 197. 31p. Order froa
LC. Mi $2.70, ph$4.80. TlD-6303
Periodic radiation survey of reactor plant container
and conmonents after shutdown. Core I. seed 2.
Section *! Duquesne Light Company, Shippio^-
port. Pa. May 60.
ph$1.80.
Order from LC. Mi $1.80.
TID-6314
Steam generator level control equipment, by W. H,
Ber^nan! Knolls Atomic Power Laboratory,
Schenectady, N. Y. June 58. 49p. Order froa
LC. Mi $3. 30, ph$7.80. TID-6319
Basic heat transfer formulas and correlations used
for the HTGR heat transfer calculations, by M.
Trooet. General Atomic Division. General Dy-
namics Corporation, San Diego, Calif. June 60.
Contract AT(04-3)-314. 6p. Order from LC.
Mi $1.80. ph $1.80. TID-6320
Monthly operating report for May I960. CXiquesM
Llf^t Company, Shippingport. Pa. 1960. Con-
tract AT(1 1-1)- 292. 30p.
Mi $2.70. ph$4.80.
Order from LC.
TID-6377
S2t
Nuclear superheat meeting no. 1 , September 21 to
23, 195$, by R. Pennington and others. Chicago
Operations Office, AEC. San lose, Calif. No*
59. 42p. Order from OTS. $1.25.
TID-7595 •
Nuclear superheat meeting no. 2. April 7 and 8.
1960, by C. B. Grahm and others . Chicago
Orations Office, AEC. Dunedin, FU. June 6a
48p. Order from OTS. $1.25 TlD-7596
Fast breeder reactor program, by Staff of Divlsloo
of Reactor Developmnet. USAEC Argonne Nation-
al Laboratory, Argonne, 111. and Atomic Power
Development Associates. Jan 60. 12p. Order
from OTS. 50 cents. TID-8523
Heavy water-zirconium-thorium type power confer-
sion reactor, by J. B. Anderson and others.
Argonne Rational Laboratory. Lemont, 111.
Feb 51. Decl. October 7, 1959. Contract W-31-
109-eng-38. 57p. Order from LC. Mi $3.60.
ph$9.30. TID- 10095
The nuclear ramjet propulsion system, by T. C
Merkle. University of California. Law rence
Radiation Laboratory, Livermore, Calif. June
59. Contract W-7405-eng-48. 13p. Order fn»
LC. Ml $2. 40, ph$3.30. UCRL-5d25
Txy U- A instrumenution system. Brief descrlp-
— 5)0, by C S. Barnett and odiers. University
T^lifornia, Lawrence Radiation Laboratory,
Uvermore, Calif. Mar 60. Contract W-7405-
aiiff-48. 24p. Order from LC. Mi $2.70,
ph$4.80. UCRL-5906
Research program at the Livermore pool- type re-
— ictor, oy k. ]. Kirschbaum and W. John. Uni-
veriity of California. Lawrence Radiation Labor-
atory. Livermore, Calif. Nov 60. Contract W-
7405-eng-48. 16p. Order from OTS. 50 cents.
UCRL-6117 (Rev.)
Economic potential of the seed-blanket reactor, by
— p. Schwoerer. Westing^iouse Electric Corpora-
tion, Bettis Atomic Power Laboratory, Pittsburgh
P». Dec 60. Contract AT-ll-l-GEN-14. 92p.
Order ft-om OTS. $2.00. WAPD-237
Bettis technical review. Reactor technology, by W.
Yeniscavich and others. Westinghouse E lectric
Corporation, Bettis Atomic Power Laboratory,
Pittsburgh. Pa. Sep 60. Contract AT-11-1-
GBN-14. 128p. Order from OTS. $2.50.
WAPD-BT-20
Pressurized water reactor (PWR) project. Techni-
cal progress report for the period June 24, 1960
toAt«|Jt23, ly), by P. N. Roes. Westing-
house Electric Corporation, Bettis, Atomic Power
Laboratory, Pittsburgh. Pa. 1960. Contract
AT-ll-l-GEN-14. 115p. Order from OTS,
$2. 50. WAPD-MRP-87
Pressurized water reactor (PWR) project. Techni-
cal progress report for die period August 24 to
October 23, 19&, by P. N. Ross. Westinghouse
Electric Company, Bettis Atomic Power Labora-
tory, Pittsburgh, Pa. 1960. Contraa AT-ll-l-
CBN-14. 97p. Order from OTS. $2.25.
WAPD-MRP-88
Pressurized water reactor (PWR) project. Techni-
cal progress ^PP^} ^9^ the period October 24 to
Decemter 23. 1960, by P. N. Ross. Westing-
bouse Electric Corporation, Bettis Atomic Power
Laboratory, Pittsburgh, Pa. 1960. Contract
AT-ll-l-GEN-14. 122p. Order from OTS.
$2.50. WAPD-MRP-89
Paat absorption erf hafnium and cadmium -si Iyer
control rods, by R. J Neuhold. Westinghouse
Electric Corporation, Bettis Plant, Pittsburg,
P». Oct 58. Contract AT-ll-l-OTN-14. 1^.
Order from LC. Mi $2. 40, ph $3. 30.
WAPD-T-753
Multi-region reactor lattice studies of fuel cycle
development program for the period July 1 to
Decen^r 31, 1960, by I. H. Coen. Westing-
house Electric Corporation, Atomic Power
Department, Pittsburgh. Pa. Apr 60. Contract
AT(30-1)-2176. 47p. Order from liC. Mi $3. 30,
ph$7.80. WCAP-1413
196a
Corpora -
tion. Atomic Power Department, Pittsburgh, Pa.
Oct 60. Contract AT(30-1)-2176. 48p. Order
from OTS. $1.00. WCAP-1423
Nuclear and thermal calculations for WCAP-4 in-
ile loop e?q)eriment, by A. Bournia and others,
^estin^iouse Electric Corporation, Atomic
Power Department. Pittsburgh. Pa. [I960?].
Contract AT(30-3)-222. 41p. Order from LC.
Mi $3. 00. ph$6.30. WCAP-3270
Carolinas Virginia nuclear power associates, Inc
CYVk prolect. Monthly process report for
bly
January 1^. Westinjpiouse Electric Corpora-
tion. AtoinIc~Power Department. Pittsburg^. Pa.
1960. 27p. Order from LC. Mi $2.70,
ph$4.80. WCAP-4009
by S. Preiser. Nuclear Development
Associates, Inc., White Plains, N. Y. Jan 51.
Decl. January 28, 1960. Contracts W-7405-eng-
26 and AT(40-1)-1065. 20p. Order from LC.
Ml $2. 40. ph$3.30. Y-715
Yankee critical eroeriments: hazards summary
report, by D. F. Hanlen and others. Westing-
house Electric Corporation, Atomic Power De-
partment, Pittsburgh, Pa. May 58. Contract
AT(30-3)-222. 44p. Order from LC. Mi $3. 30,
ph $7 . 80. YAEC-31 (SupfH. )
Pressure drop, flow distributioo and mixing studies
for a model heterogeneous reactor vessel, by
R. T. Berringer and A. A. Bishop. Westinghouse
Electric Corporation, Atomic Power Department,
Pittsburgh, Pa. Dec 59. Contract AT(30-3)-222.
61p. Order from LC. Mi $3.90, ph $10.80.
YAEC-74
Bulk biological shielding aspects of the ya">«g core,
byH. W. Graves, Jr., and others. Westinghouse
Electric Corporation, Atomic Power Department,
Pittsburgh. Pa. Oct 57. Contract AT(30- 3)- 222.
37p. Order from LC. Mi $3.00, ph $6.30.
YAEC-88
529
WCAP-4 tn-pite Jtest loop <te»^gP manual, by C.
Dishman. Westinghouse Electric Corporation,
Atomic Power Department, Pittsburgh, Pa. Jan
60. Contract AT(30- 3)- 222. I33p. Order from
LC. Mi $7.50, ph$24.30. YAEC-130
WCAP-4 In -pile test loop hazards analysis manual,
by C. D. Di ahman and others. Westing^use
Electric Corporation, Atomic Power Department,
June 59. Contract AT(30-3)-
Pitts burgh,
222. I19p.
ph$18.30.
Fi.
Order from LC.
Mi $6.00,
YAEC-133
CAT- -an IBM 7(|4 program for coolant actuated
transients in an open- lattice core, by L. S. Tong,
and others. Westin^ouse Electric Corporation,
Atomic Power Department, Pittsburgh. Pa.
Feb 60. Contract AT(30-3)-222. 80p. Order
fromLC. I4 $4.50, ph $12.30. YAEC-145
.1
Yankee control rod programming stixiy, by M.
Robkin. WestinpKJuse Electric Company, Atomic
Power Department, Pittsburgh, Pa. Aug 59.
Contract A'rt30-3)-222. lOOp. Order from LC.
Mi«$5.70, pH $16.80. YAEC-164
Monthly progress report for the period November
1 to 30, 195^, byU E. Walchli. Westin^ouse
Electric Corporation, Atomic Power Department,
Pittsburgh, m. Dec 59, Contract AT(30-3)-222.
I4p. Order ^rom LC. Mi $2. 40, ph $3. 30.
YAEC-173
Monthly progress report for the period December 1
ro 31. 1959, by H. E. WalchU. Westinghouse
Electric Corporation, Atomic Power Department,
Pittsburgh. Ba. Jan 60. Contract AT(30-3)-222.
12p. Order (rom LC. Mi $2. 40, ph $3. 30.
YAEC-I75
Quarterly progijess report for the period October 1
toDei^tnber 31. iffl. by H. ErWalchli. West-
inghouse Electric Corporation. Atomic Power
Department, Pittsburgh, Pa. Feb 60. Contract
AT(30-3)-22l. 36p. Order from LC. Mi $3. 00,
ph$6.30. YAEC-176
Technology — Feed Materials
Refining of Mg>
a is . Quarte ly proyess report, by R. A
Ewins and ot lers. Battelle Memorial Inst
Ewing and
Columbus,
Contract AT
LC. Mi $3
and other uranium-bearing materi-
emorial Institute,
Ohio. JaoeSl. Decl. March 7,1960.
30-1-CXN-228. 51p. Order from
fC. ph$9.30. BMI-254
A semi -empirical method for attaining predeter-
mined uranium saturation levels in tne^lurrex
process, "5y R. W. West. National Lead Con-
pany of Ohio, Technical Division, Cincinnati,
Ohio. April 53. Decl, May 3. 1960. Contract
AT(30-1)-1156. 18p. Order from OTS.
30 cenu. FMPC-216
Laboratory and pilot plant evaluation of Portugueae
uranium concentrate and black oxide blends, by
B. G. Ryle. and others. National Lead Company
of Ohio, Cincinnati, Ohio. Mar 54. Decl. July
13, 1960. Contract AT(30-1)- 1156. 19p. Order
from 015. 30 cents. FMPC-391
An automatic polarograph for the determination of
uranium in process waste streams, by K. Ko-
yama and others. Hanford Atomic Products
Operation, Richland, Wash. Dec 53. Contraa
W-31-109-Eng-52. 26p. Order from OTS.
35 cents. HW-3014S
Uranium nitrate conversion, by E. F. Curren.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. May 56.
Decl. May 10, 1956. Contract W-31-109-Eng-
52. I6p. Order from LC. Mi $2.40, ph $3.30.
HW- 42995
Low temperature conversion of uranium dioxide to
uranium tetrafluoride using aqueous hydrogea
fluoride, by J. S. Fox and S. D. Schiffman.
Carbide and Carbon Chemical Company, Union
Carbide an d Carbon Corporation, K-25 Plant,
Oak Ridge, Tenn. Oct 52. Decl. July 12, 60.
Contract W-7405-Eng-26. 14 p. Order from
OTS. 25 cents. K-965
Hydration of uranium trioxide for improving feed
materials processing, by J. S. Fox. Carbide
and Carbon Chemicsls Comoany, Union Carbide
and Carbon Corporation, K725 Plant, Oak Rid|B,
Tenn. Aug 53. Decl. July 12, 1960. Contraa
W-7405-Eng-26. 16p. Order from OTS.
30 cents. K-104S
Thermodynamic properties of gaseous uranium
hexafluoride by B. H. Parks and D. W. Burton.
Union Carbide Nuclear Company, Division of
• Union Carbide Corporation, Oak Ridge Gaseous
Diffusion Plant, Oak Ridge, Tenn. Sep 60.
Contract W-7405-eng-26. 43p. Order from OTS.
$1.00. K-14SI
Uranium refinery proposal, by A. L. Baker. The
Vitro Corporation of America, New York, N. Y.
May 49. Decl. August 24, I960. 39p. Order
from OTS. 40 cents. KLX-013
530
A<Midonal studies on recovery of uranium hexafluor-
— la^ from vent gases, by W. R. GoUiher and
StBers. Union Carbide Nuclear Company, A Divi-
sion al Union Carbide Corporation, Paducah Plant,
Paducah, Ky. Oct 57. Decl. May 17, 1960.
Contract W-7405-eng-26. I6p. Order from
OTS. 45 cents. KY-230
Specific surface and bulk density of U-^Oq and UO^
as factors in UF4 production on the 250 grauri
uranium scale, by R. J. Bard and othersT Uni-
"versity of California, Los Alamos Scientific
Laboratory, Los Alamos, N. Mex. Dec 54.
Decl. June 18, I960. Contract W-7405-Eng-36.
26p. Order from OTS. 35 cents. LA-1854
Progress report of pilot plant work on UF4 produc-
^ by continuous mediods. Period covered
August 15, 1946 to October 21 1948, "By^ K.
Teter. Mallinckrodt Chemical Works. St. Louis,
Mo. Oct 48. Decl. October 7, 1959. I2p.
Order fromLC. Mi $1.80, ph $1.80.
MCW-152
Process development quarterly report. Part I, by
J. Livasy and others. Mallinckrodt Chemical
Works, St. Louis, Mo. Jan 55. Decl. July 12,
I960. Contract W-14-108-Eng-8. 75f. Order
from 015. 55 cents. MCW-1371
Process development quarterly report .
"■ M. Leaders. Mallinckrodt Chemical Works,
Part II, by
WI _
St. Louis, Mo. Feb 55. Decl. March 31, 1960.
Contract W- 14- l08-Eng-8. 170p. Order from
LC. Mi $7.80, ph$25.80. MCW-1372
Process development quarterly report. Part 11.
Mallinckrodt Chemical Works, St. Louis. Mo.
Nov 55. Decl. April 28, 1960. Contract W- 14-
108-eng-8. 207p. Order from LC. Mi $9. 30,
ph $31.80. MCW-1381
Process developnr>ent quarterly report. Part I.
Mallinckrodt Chemical Works, St. Louis, Mo.
Apr 56. Decl. March 31, 1960. Contract W-
14-l08-eng-8. Il5p. Order from LC. Mi $6. 00,
ph$18.30. MCW-1385
Process devel
irterly report part II- Pilot
" '^■^ — Mallinc-
_-. - May 57.
Decl. August 5, 1960. Contract W-14-108-eng-
8. 176p. Order from OTS. $2.75.
MCW-1402
xaess development twiarterly report part II- Pi!
plant work, by N. Kuhlman ana others . Malli
krodt Chemical Works, St. Louis, Mo. May 1
Prpcesi development quarterly report. Part II.
hlot plant work, by B. Elliott. Mallinckrodt
CbenUcal Wbrks, St. Louis, Mo. Aug 57. Decl.
April 28, 1960. Contract W-14-108-eng-8. 160p.
Order from LC. Ml $7. 50, ph $24. 30.
MCW-1404
Pilot plant production of ionium concentrate, by
R. H. FarlssandG. B. Wills. Mallinckrodt
Chemical Works, St. Louis, Mo. Nov 57. Decl.
Februarys, 1960. Contract W- 14- 108 -eng-8.
21p. Order from LC. Mi $2.70. ph $4.80.
MCW-1408
Process development quarterly report. Part II.
Pilot plant work, by J. Nelson. Mallinckrodt
Chemical Works, St. Louis. Mo. Aug 58. Decl.
March 30, 1960. Contract W-14-108-eng-8.
94p. Order from LC. Mi $5.40. ph $15.30.
MCW-1416
Laboratory work.
report. Part I.
isoni^ Mallinckrodt
Process development quarterly
ry work, by J. Nels
Chemical Works, St. Louis, Mo. Oct 58. Decl.
May 11, 1960. Contract W-14-108-eng-8. 224p.
Order from LC. Mi $9. 60. ph $33. 30.
MCW-1419
Solubility and distribution study of antimony, tantal-
um, niobium, ruthenium, tungsten, and titaniign7
by S. D. Nelson and G. P. Lang. Mallinckrodt
Chemical Works. Uranium Division, Weldon
Spring, Mo. July 60. Contract W-14-108-Eng-8.
lOp. Order from OTS. 50 cents. MCW-1453
Process development quarterly progress report, by
J. H. Yeager and others. Mallindkrodt Chemical
Works, Uranium Division, Weldon Spring, Mo.
Nov 60. Contract W-14-l08-Eng-8. 91p.
Order from OTS. $2.00. - MCW-1459
Evaluation of Australian rum Jungle uranium concen-
trate for use as NLO refine ry"feed, by T. J.
Collopy and others. National Lead Company of
Ohio, Feed Materials Production Center, Cincin-
nati. Ohio. Jan 56. Decl. June 1. I960. Con-
tract AT(30-1)-1156. 20p. Order from OTS.
30 cents. NLCO-613
The recovery of uranium from composite U^ reduc-
tion bomb scrap by a two- stage phoeptMte preci-
Sitation process, by E. R. Johnson and others,
lational Lead Company of Ohio, Technical Divi-
sion, Cincinnati, Ohio. Mar 56. Decl. May 27,
1960. Contract AT(30-1)- 1 156. 28p. Order
from OTS. 35 cents. NLCO-627
\ ^horatory at^d pilot plant evaluation of Anaconda
Bluewater uranium concentrate, by B. G. Ryle
and others. National Lead Company of Ohio,
Feed Materials Production Center, Cincinnati,
Otto. Jan 57. Decl. June 2, 1960. Contract
AT(30-1)-1156. 21p. Order from OTS. 35cent8.
NLCO-664
531
Stripping ageiya fcr re-extraction o< uranium in a
uranyl nitrate hexahydrate-tributyl phoeprfiate
nitric acid sydtern, by P. S. Gentile and T. J.
Collopy. National Lead Company of Ohio, Cin-
cinnati. Ohio. Dec 56. Decl. March 31, 1960.
Contract AT(30-1)- 1156. 48p. Order from IX.
Mi $3,00. ph 16.30. NLCO-666
Acetate proceas tor the production of thorium fluor-
ide. by P. S. (gentile and M. D. Snyder. Nation-
iTLead Company of Ohio, Feed Materials Pro-
ductlon Center, Cincinnati, Ohio. Feb 57. Decl.
July 19. I960.: Contract AT(30-1)- 1156. 19p.
Order from OTS. 30 cents. NLCO-683
OTS.
Refining of tfaoriiim-containing uranium concentrates
' extraction yitfa tributyl phosphate, by C. W.
[untington. h^ational Lead Company, of Ohio.
Cincinmti, Ohio. Aug 57. Decl. April 28. 1960.
J.
Contract AT(3b-l)-1156.
Mi $2. 70. Dh$4.80.
X ph$4.
31p. Order from LC.
NLCO-692
Studies of the behavior (rf the TBP-keroaene solvent
in uranium re
^ning:
recover
ft
of discarded
refinery solvent, by R. H. Eflerhorst. National
Lead Company of Ohio, Cincinnati. Ohio. Jan
58. Dec. April 28, 1960. Contract AT(30-1)-
1156. 25p. Order from LC. Mi $2.70,
ph$4.80. NLCO-714
Labor atory evaluation of Ramapo uranium gravity
concentrate, liyj. H. Krekeler and others.
National Lead {Company of Ohio, Cincinnati.
Ohio. Apr 584 Decl. March 28, I960. Con-
tract AT(30- 11- 11 56. Up. Order from LC.
Mi $2. 40. ph $3. 30. N LCO-741
Studies of the TBP*- kerosene solvent in uranium re -
fiaing: Quality evaluation and treatment tecir~
niquwi for useri solvent, by R. K. Klopfenstein
aodocfaers. National Lead Company of Ohio,
Peed Materia Ip Production Center, Cincinnati,
Ohio. July 60. Contract AT(30-1)- 1 156. 35p.
Order from OlTS. 75 cents. NLCO-815
Summary technical report for the period July 1,
1960 to Septeijber 30, 1960, by F. U Cuthbert.
National liad Company of Ohio. Cincinnati.
Ohio. Oct60^ Contract AT(30-1)- 1156. 88p.
Order from OtrS. $2.00. NLCO-820
OTS.
Process development quarterly report, part I. by
W. M. Leaifs and E. 1. Miller. Mallinckrodt
Chemical WoAts, St. Louis, Mo. Apr 53. Decl.
March 7. 1964. Contract W- 14- 108 -eng-8. 158p
Order from LP. Mi $7.50. ph $24.30.
NYO-1353
nt quarterlj^ report, part 11, by
W. M. Leaders and E. I. Miller. Mallinckrodt
Chemical Works, St. Louis, Mo. Oct 53. Decl.
March 15, 1960. Contract W-14-108-eng-8.
Process devel
Leai
nop. Order from LC. Ml $5.70.
ph $16.80.
NYO-1358
Process development Quarterly report, P^rt II, by
W. M. Leackrs and others' Mallinckrodt Chen-
ical Works, St. Louis, Mo. Jan 54. Decl.
March 24. 1960. Contract W-14-108-eng-8.
146p. Order from LC. Ml $7.20. ph $22.80.
NYO-1360
Process development quarterly report. Part II.
Mallinckrodt Chemical Works, St. Louis, Mo.
May 54. Decl.
14-108-Eng-8.
ph $30. 30.
March 7, 1960. Contract W-
197p. Order from LC. Mi $8.70,
NYO-1363
Inhibition of a»r oxidation of UO2 ^}^^ treatmet.
by J. W. Stevenson. Mallinckrodt Chemical
Works. St. Louis. Mo. Mar 52. Decl. March
7. 1960. 12p. Order from LC. Ml $2.40,
ph$3.30. NYO-5251
Waste Disposal and Processing
V-
Anion replacement reactions for the removal of
strontium from aqueous solutions, by L. L.
Ames, Jr. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
July 60. Contract AT(45-1)-1350. 30p. Order
from OTS. 75 cents. HW-66383
Quarterly progress report research and develop-
ment activities fixation of radioactive residuei,
for April to June. 1960, by D. W. Pearce. Gen-
eral Electric Company, Hanford Atomic Produca
Operation, RichUnd, Wash. July 60. Contract
AT(45-1)-1350. 30p. Order from OTS.
75 cents. HW- 66571
Review of soil chemistry research at Hanford, by
D. W. Bensen. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash- Aug 60. Contract AT(45-1)- 1350. 38p.
Order from OTS. $1.00. HW-67201
S
Chemistry of the intercycle eva
November 26, I»5^. byW~^
rator incident of
vis and others.
Oak Ridge National Laboratory, Oak Ridge, Tenn.
Nov 60. Contract W-7405-eng-26. 17p. Order
from OTS. 50 cents. ORNL-2979
Utmr' GcMral'i Onice,
j^Mcad KlneUca. inc.
I AM. CalU.
Agro Ceo Aacro Corp.,
AltaaadrU, Vi.
^roalMdc wd Structurn Re-
ievch Lab., Maaa. Inat. of
Tach.. Cambridge
l^ttm-Gtmn*! Corp.,
Calif.
Aaionaialril Reaearch Aaac
KrfPrlnceion, Inc., N.J.
Ailiiaialril Reaearch Latia..
Air Force Reaearch D»v„
WrHN-P«teraar AFB, OWo
P»M PB Number
449 tS3 30S
393 1S3 440
472 153 426
420 IS3 712
4.S4 171 415
442 153 441
457 153 459
435 152 320
152 321
449 153 385
Aaiwfflr-I Turbine Lab.,
Naval Air Turbine Teat Sta-
UOB, Trenton, N.J
Aaroauutnlc, Newport Beach.
caif.
tartapace Msdlcal CNv.. Wrlgta
Air Developmeni DIv., Wri^-
Paierton AFB, Ohio
Mr Crew Equipment Lab.,
Naval Air Material Center,
rUladelpMa, Pa.
Air Force Cambrldoe Reaearch
Lite., Bedford, Kteaa.
Air Force Maalle Develcoment
Caater, Holloman AFB, N. Mex.
Abtome Inatrumenu Lab..
DaarPark. N.Y.
U.. CoUege
Allied Reaearch Aaaociatea,
lac., Boaton, Maaa.
Alaricw Electronic Laba.,
he, PhUadelphla, Pa.
tmukm laat. for Reaearch,
PlKiburg^ Pa.
imtrltm Power Jet Co.,
U^prfMd. N.J.
I La>., Calif, inat. of
TadL, Paaadena
AaUad Mathematlca and Siatta-
teUtac, Stanford U., Calif.
AhIM P»cbaloclcal
WiMi, Pa.
Scrvtcea,
AfCdc Aeroniedical Lab..
La«dAFB, Alaalta
532
416 153 289
435 153 744
397 171 392
406 153 354
411 153 394
462 153 395
467 153 392
153 393
393 1S2 686
435 153 408
442 150 719
474 153 465
416 171 370
411
441
478
153 371
153 540
153 520
153 S21
436 153 161
420 153 227
392 153 165
420 150 703
392 153 547
421 153 224
449 147 121
393 153 779
393
394
397
398
iOi
403
411
412
420
153 329
153 323
153 321
153 322
153 369
153 373
153 545
153 372
153 544
153 522
153 507
153 513
153 515
153 518
159 543
153 514
153 324
153 517
SOURCE INDEX
Source
Arctic Aeromedlcal Lab.,
Ladd AFB. Alaaka (coo. )
Armed Forcea-NRC Committee
on Hearing and Bio- Acouatlca,
Waahlngton. D.C. 398
Armour Reaearch Foundation,
Chicago, ai.
460
469
Army Chemical Corpa,
Port Detrlck. Md.
Army Chemical Reaearch and
Developmeat i^aba., Army
Chemical Center, Md.
Army Engineer Reaearch and
Development Laba.. Fprt
Belvoir, Va. 447
460
Army Ordnaace Human Engi-
neering Lab., Aberdeen
Proving Ground, Md. 392
398
Army Signal Mlaalle Support
Agency. White Sanda MiaaUe
Range, N. Mex. 436
Army Sipial Reaearch and
Development l^ab., Fort
Monmouth, N.J.
411
421
451
475
Armv Tranaponation Reaearch
and Engineering Command.
Fort Euaita, Va.
Arnold Enfineerlng Development
Center. TuUahoma, Tenn. 454
ARO, Inc., TuUahoma, Teon. 454
AvcoCorp., WUmincian, Maaa. 445
Avco Everett Reaearch
Lab., Maaa.
Batielle Memorial Inat.
Columbua. Ohio
Behavioral Sciencea Lab.,
Wright Air Development Dtv.,
W right -Paneraor AFB. Ohio
Bell and HoweU Reaearch
Center. Paaadena. Calif.
Bell Aircraft Corp.,
Buffalo. N.Y.
Bell Helicopter Corp.,
Fort Worth, Tex.
Biomadtcal Lab., Wrl|ht Air
Developmem I3lv„ Wright -
Paneraon AFB, Ohio
PB Nuirticr
440
153 519
153 546
441
153 512
153 523
464
153 506
153 509
153 516
465
153 510
478
153 367
BalliaUc Reaearch Laba..
Aberdeen Proving Ground, Md. 422
436
440
442
454
466
Boeing Aitplane Co.,
Seattle. Waah.
391
458
469
436
405
445
416
398
422
l-l
153 778
153 168
171 474
477 152 927
396 153 174
153 078
153 077
153 470
153 469
153 t«2
150 706
150 704
152 998
153 000
153 001
153 004
150 706
153 002
171 377
419 150 075
153 477
153 477
171 413
454 149 676
150 066
153 494
150 068
150 070
ISO 724
.153 42S
154 406
153 493
150067
ISOOM
153 073
154 409
153 929
171406
171 419
171 409
171 390
154 406
171 367
171 416
Soiree
Bolt, Beranek and Newman.
Inc.. Cannbridte. Maaa.
Bonn U., Weat Gerinany
Britiah Cotunnbta U.. Canada
Brooke Army Medical Ce«er,
Fort Sam Houaton, Tex.
Brom U. DIv. of Applied Math-
ematlca, Providence, R. I.
Brown U. Div. of Engineering.
Providence, R.I.
Bruah Beryllium Co.,
Cleveland. Ohio
Bniaaela U., Belgium
Bryn Mawr Coll., Pa.
Bureau o( Naval Weapona,
Waahington. D.C.
Page PB Number
422
406
467
403
404
4.'>2
458
465
473
475
460
447
394
406
422
423
424
Bureau of Shipa.
Waahln|ron,D.C.
468
406
422
423
424
465
468
California State Polytechnic
Coll., San Lula Cblapo
Califonria U., lerlteley
California U.. Loa Anfelea
Calvin Coll., Grand Raplda.
Mich.
CameAe Inat. of Tech., Grad-
uate bchool of Induatrla]
Adrntniatratlon, Plttaburgh. Pa.
Caae Inat. of Tech.,
Qeveland, Olio
Caater for International Studlea.
Masa. Inat. of Tech., Cambridge
399
425
393
411
425
466
407
153 175
150 690
153 397
153 192
153 193
153 194
147 401
153 162
154 291
153 074
147 400
453 147 362
CMcafoU., Ul.
450
42S
394
412
171 389
153 299
153 424
171 236
171 239
171 241
171 243
171 245
171 224
171 225
171 226
171 227
171 228
171 231
171 240
171 229
171 230
171 232
171 233
171 234
171 235
171 242
171 244
171 246
171 238
171 236
171 239
171 241
171 243
171 245
171 224
171 225
171 226
171 227
171 228
171 231
171 240
171 229
171 230
171 232
171 233
171 234
171 235
171 242
171 246
171 237
171 238
474 153 465
153 409
171 414
152 686
153 204
153 438
153 099
152 871
150 713
150 714
153 417
1.53 287
153 232
Source
C««lag and CheiMcal
ou Id. Md.
CctoradoU., BouMer
CotumbM U.. New Yorl
Computer Engineering fUao-
cime». Inc., PaMdenA, Caltf.
CorMllU..
(J.. Denin
khaca. N.
CoTMll U. Cradueie Sciod al
Aeronautical Engiaaci In
N.Y.
ConcU U. Medical Cd I
New York
Cornell U. Schod at El ectrical
Engineering, hhaca. |l.y.
Courtney aad Co.,
PMladdpWa. Pa.
Cryo|Bnlc Lab., Oio ^aie U.
Reaearch Foundation.
Colun*ua
Daniah Meteorological
Carlonenluad
Danmouth Coll., HaaoAei;N.H.
□avkl SamoM Reaearcl
Princeton, N.J.
David Taylor Model Bai in.
- ■ D.C.
Oayatiom Inatrumem,
Arctbald. Pa.
Defenae Atomic Supporf Agaacx
WaaMaroB. D.C.
Defenae Metala Inform^tioa
Center Batielle ^4r^I«rtal
faiat., Cotuir^Ma, Ohii
407
407
449
4S3
4.S4
3«7
463
4S5
412
3«
414
PB Number
171 I2S
171 376
IS3 754
153 734
171 407
133 468
153 131
153 092
153 324
152 >72
150 071
417 150 920
407 154 066
412 153 093
411
413
demer.
DWrote Teetlag Lab., I Ich.
Olamoad Ordnance Fuz ;
Waahittpon. D.C.
I Aircrrt Co.,
Loacleacli. Caltf.
Oynamlc Analyata aad ^oatral
Lib., Maaa. Inat. of Tech.,
Cambridge I 443
Eagle-Picher Co.. )apik. Mo. 426
Ecole Nationale Superl( ure de
CMmto de Siraabourg France 466
Ecoie Ncrmale Superle ire.
France
429
440
425
464
437
444
446
458
459
461
474'
461
391
425
437
469
463
394
Educameial Taatlag Sci Tica,
Prtacatoa. N.J.
Elecrtrical Enctneerlng Reaearch
Lab., U. al Olinou. l|rbana. 476
Electronic Syatema Lab., Maaa.
Inat. of Tech., Cannbr^d«e 451
ElactroBlca Reaearch dab.,
Hutthaaaliia U.. BoatK Maaa. 426
Elactroaica Reaearch 1^., U.
ofCalllania, Berkeldy
426
467
153 480
153 481
171 3*6
152 6*9
153 953
150 698
171 361
151 101
161 230
161 233
151 098
161 229
151 im
151 lOB
161 228
171 394
153 505
153 579
152 654
152 917
153 478
171 187
171 398
152 525
153 231
153 281
150 693
148 018
152 r6
153 560
153 722
153 400
152 931
Source Pai
ring Dl»., Air Materiel
Command, Wright'Pattrraoti
AFB, Ohio 417
FeliRian Reaearch Laba.,
Picatinny Araenal.
Dover. N.J.
Fll^ Acceaaoriea Lab.,
Wright Air Drvelopment Div.,
Wright -Paners<«i AFB. OMo
Forachunoainatitut fOr Phyaik
der Sirahlantriebe e. v. .
Stungart (Weal Germany)
Frankfurt U. (Wcac Germany)
Franklin Inai. Laba. for Reaearch
and Development. Philadelphia.
Pa. 442
F rick Chemical Lab.,
Princeton U., N.J. 408
Galea and Crellin Laba. ol
Chemistry. Calif. Inat. of
Tech.. Paaadena 405
General Electric Co.,
Oeenaboro. Ky. " 426
Po WUfTPCf
I&4 293
4.17
438
4.S3
150 097
152 316
153 111
171 326
1.S3 386
438
4?8
171 363
171 385
473
150 688
442
150 719
General Electric Co.,
Schenectady, N.Y.
General Electric Reaearch Lab.,
Schenectady, N.Y.
niinota State Water Survey,
Urbane
Dlinota U., Urbane
1-2
395
453
153 128
148 081
I50«3
153 156
154 484-1
154 484-2
467 153 683
459
171 085
461
171 393
462
152 866
475
150 718
153 241
408 171 373
General Electronic Laba., Inc.,
Cambridge, Maaa. 426
General Telephone and Elec-
tronics Laba., Inc.,
Bayaide, NY.
George Waahlnaon U.,
WaaMnyon. Oic. 442 153 145
CeorgU U. . Athena 414 150 721
Guataf Werner Inat. (or Nuclear
Chemiatry (Sweden) 404 153 304
Haloid XerOK. faK.,
Rocheater. N.Y. 427 171 380
Harpur Coll.. State V. al Ne«
Yjrk, Endicott, NY. 479 153 121
Harvard Graduate School of
Bualness Administratlcn,
Canrrin-idge. Maaa 394 153 287
Harvard U.. Carr<>Tidge. Mass. 463 147 900
Haverford Coll. , Pa. 427 153 101
Hebrew U., larael 449 153 306
153 308
Heiuy Ford Hoapttal,
Detroit. Mich. 400 153 164
HUler Aircraft Corp.,
Palo Alto, Calif . 417 153 083
IWhea Reaearch Laba.,
Milibu, Calif. 427 153 396
Human Factors Research, Inc.,
Los Anaelea. Calif. 395 153 126
153 141
Human Sclencea Reaearch, Inc.,
Arllnyan, Va. 477 153 129
Ulaoia Inat. of Tech. . Chicago 469 153 552
412 153 239
153 168
153 119
Source
IlinoiaU., Urbana(can.)
Pa«f PB
453
462
470
171 J7»
153 ISI
lUM
Indiana U. School of Medicine,
Indianapolis
Insiilut Pasteur^ ParU (France) 408
400 / 153 SB
/ 153 J
1521
Inaiituie (or Applied Experi-
mental Psychology, Tufia U.,
Medford, ktaaa.
Institute for Cooperative
Research. U. of Pennsylvania,
Philadelphia
Institute (or Fluid Dynamics and
Applied Mathematics, U. of
Iwliryland. College Park
Institute (or Quantitative
Reaearch In Economlca and
Management. Purthie U..
Laiayette, Ind.
Inaiitute (or System Reaearch,
U. of Chicago, Dl.
Inatiiute (or the Study of Metals,
U. of Chicago, 01.
Inatltute of Anatomy, U. at
Uppaala (Sweden)
395
477
479
455
408
404
Inatltute of En0neerlng Reaearch,
U. of California, Berkeley 470
474
Institute of PligK Structurea,
CdunMa U.. New York
Institute of Mathematical Science^
New York U, N.Y.
Inatltute of Tech., U. of
Minnesota, Minneapolis
Institute of Trsnaportatlon and
Traffic Engineering. U. of
California, Berkeley
Intermountain Weather, Inc..
Salt Lake City. Utah
427
476
417
412
International Buaineaa Machinea
Corp.. Yorkiown Heights. N.Y. 4.SI
452
loMaphere Reaearch Lab.,
Poinaylvanla State U.,
University Park
laotopea. Inc., Weatwood, N.J.
latltuto dl Fiaica Unlveraita
di Padova (Italy)
latituto Elect roiecnico Nazionale
■ Galileo FerrarU" (haly)
Jet Propulsion Lab., CalK. Inat.
of Tech., Paaadena
415
464
409
427
438
447
Kentucky U.. Lexington
Laboratory for lAaulation Re-
search, Mssa. Inat. of Tech.
Cambridge
Lincoln Lab., Maaa. Inat. of
Tech., Loxington
428
465
470
391
415
428
429
147 sa
152 «4
153 7)1
408 1497a
479 153 1«
171 sr
171 M
153 7H
153 381
171 M
154]*)
476 148 SB
152 7n
152 7«
470 147 l»
171 3W
153 U«
IJO(
1S0(
1S0(
ISJIff
171 3«
IS2(
466 ISOM
153 W
153W
153 «
154 411
154 411
153 M
153M
409 1534SI
I50 70*
isew
147 17J
147 17i
147 75»
152 87
153 4*
152 »7«
153 217
153 IS
153 4n
153 1*;
153M
UKOls Lab.. Mass Inst of
Tsck., LexinpCTi (con.)
[»),. Arthur D.. Inc..
CanArldge. Maaa.
1^001 laduatrlaa. Salt Lake
Cty, Uah
toOlisad Alrcrrfi Corp.,
Siai^ala, Calif.
f*m
PB Number
4,18
153 220
439
153 21*
153 219
452
153 361
455
152 620
471
153 2*4
446 171 406
429 153 245
lihcOoaaid Physics Lab.,
y^QOi U. (Cfanada)
H^OUl U. (Canada)
iMUnckrodt Chemical Lab.,
Harvard U.. Can*rldge.Maaa.
LUtey, P. R.. and Co.. Inc..
lia, tod.
412
153 437
417
153 435
171 372
429
152 693
152 719
153 645
439
153 055
444
171 379
4 S3
153 357
455
152 844
415
153 061
413
150 723
467
153 153
429
150 689
. .nuring Laba., Inc., .
Cmtn lilffT Maaa.
Vkrylaad U.. College Park
Itasachueetu Inat. of Tech.,
Cia*rirlr
446 171 400
392
467
447
456
460
468
471
150 722
153 291
171 391
153 420
171 399
152 874
152 9U
v.. Amherat 405 150 656
HBwHf Reaearch Lab., U.
ofCaUanila, Berkeley
Masrlals Reaearch Lab.,
VMcrtoen Arsenal, Masa.
he Falla Clmirch, Va.
Vbl^ aad Ceramica Lab.
Wrllti Air Development Div.,
Wrl^-Psnerson AFB. Ohio
M«^ Reaearch Lab., Brown
U.. Prorideace. R.l.
Ifcliael Reese Hospital.
CUcagD, m.
Naval Ord-
I Teat Station, China
Like, Calif.
McMgn State U., Eaat Lanaing
I U., Am Arbor
471
463
452
459
441
446
399
443
397
456
459
McMgan U Coll. cf
Eagtaeering, Ann Arbor
I U. Coll. of Literature.
Sdeacs, and the Arta,
<■ Arbor
I U. Reaearch Inat..
taa Arbor
McToeave Aasociatea, Inc..
larttiWOB. Maaa.
Mcroeavc Lab., Stanford
U., Calif.
McriMave Reaearch Inat.,
nlMactaic Inat. cf Brooklyn,
463
468
476
309
418
429
430
458
473
146 924
171 371
150 708
153 455
171 411
171 394
171 510
153 439
153 365
153 286
153 524
150 982
171 366
153 171
152 836
152 835
1 52 61 1
171 404
153 229
153 504
153 650
153 098
4.30 153 454
Source
Mine Safety Appllancea Co.,
Gallery, Pa.
Mlnneaota U.. MInneapolts
Minnesota U. School of Physics.
MInneapoiis
Mississippi Southern Coll.,
Hattieaburg
Moore School ef Electrical
Engineering, U. of Penn-
sylvsnia, ndladelphia
Motorola. Inc., CMcaga, 111.
National Aeronautics and Space
Adminiatration, Waahln^on,
D.C.
National Aviation Facilltiea
Experimental Center,
Atlantic City, N.J.
National Bureau o( Standards,
Boulder, Colo.
406
430
392
396
431
430
National Bureau of Standards.
Waahington. D.C.
National Carbon Co., tac..
Parma, Ohio
National Library of Medicine.
Waahington. D.C.
National Reaearch Laba.,
Ottawa, Canada
Naval Civil Engineering Lab.
Port Hueneme. Calif.
Naval Orchiance Lab.,
Corona, Calif.
Naval Ordnance Test Ststion.
China Lake, Calif.
PB Number
154 408
153 433
148 496
171 403
153 954
150 692
472 153 564
430 171 368
415
430
408
465
479
447
40t
441
477
418
420
Naval Reaearch Lab.,
Waahington, D.C.
Naval Superaooic Lab., Maaa.
Inat. of Tech., Cambridge
Naval Supply Research and
Development Facility,
Bayonne. N.J.
Naval Weapona Lab..
Dahlgren. Va.
New Hairpahire U.. IXrham
New YorkU., N.Y.
New YorkU. Coll. of
Engineering, N.Y.
Nobel Inat. of Physics.
Stockholm, Sweden
Non- Metallic Materials Lab..
Wright Air Development Div.,
Wrighi-Panerson AFB. Ohio
North Carolina State Coll..
Raleigh
North Carolina U., Chapel Hill
1-3
418
430
431
439
443
456
462
409
431
441
465
480
456
474
161 583
150 064
150 923
161 560
161 586
171 365
150 062
153 632
153 633
153 178
171 375
430 150 707
479
406
460
471
413
458
450
472
153 404
153 0*4
153 221
153 0*6
152 790
153 IB
153 290
154 409
153 407
161 990
143 302
150 319
149 520
149 296
171 316
153 104
153 106
153 106
441 153 198
152 978
153 215
153 216
171 412
150 323
150 060
153 159
431 150 720
474 171 395
439 150 702
150 711
153 564
Source Lie P3 Number
North Dakota U.. Grand Forks 399 153 542
Noyes Chemical Lab.. U. of
Ulinoia, Urbaaa
Nuclear Metala, Inc.,
Concord. Maaa.
Obaervatoire de Haute- ParU
(France)
Office of Ordnance Reaeaich.
Durham, N.C.
Office of Scientific Research
and Development. Div. 19
Office of Technical Services,
Dept. of Coiiunerce,
Waahlnyon. D.C.
Ohio State U. Research
Foundation, Columbus
«09
447
478
477
431
391
448
460
472
415
418
467
468
478
147 776
150 9(21
171 391
152 5*8
152 927
153 954
OrS S8-437
GTS S8-438
0TSS8-440
OTSS8-445
OTSSB-435
150 697
153 283
171 408
153 392
153 657
152 588
153 430
Oregon Stste Coll.. Corvallis 472 1.53 143
Page Communications Engineer^
Inc.. Waahington, D.C
Parke Mathematical Laba.
Inc., Carliale,
432 153 609
450
473
Fennaylvania State U.,
University Park
Peimaylvania State U. Coll. of
Mineral Induatriea,
University Park
Pennsylvania State U. Mineral
Industries Experiment Station,
University Park
Pemaylvsnia U., Philadelphia
Fennaylvania U. School of
Medicine, Philadelphia
Personnel Lab., Wrlgh« Air
Development Div., Lackland
AFB. Tex. ^
410
448
410
472
411
475
153 458
153 728
153 157
153 173
154 296
154 297
153 422
153 166
416 153 334
Ph
hyaical Reaearch Lab.. Space
Tech. Laba.. Inc.. Los
Angeles. Calif.
Physical Sclencea Lab., Ord-
nance Tank -Automotive Com-
mand, Center Line, Mich.
Physics Lab.. Wright Air
Development Div., Wright -
Panerson AFB, Ohio
Pinsburgh U., Pa.
Plesset, E. H., Associates,
Inc., Los Angeles, Calif.
Polytechnic Inat. ct Brooklyn,
N.Y.
Poulter Laba.. Stanford Re-
aearch Inat., Menlo Park.
Calif.
Princeton U., N.J.
393
439
443
473
153 852
153 853
152 829
152 830
154 404
461 171 381
406
463
400
432
439
456
457
472
171 401
171 402
153 127
153 49*
153 3*8
153 1*4
152 83*
153 147
440 153 316
410
418
419
Psychological Lab., U. of South-
ern California, Loa Angeles 396
149 648
152 873
150 075
147 534
148 006
148 007
Source
PuUtc Health Service,
Waahinffon, O. C.
Purdue U., Lafayene.
U. Div. al
Lafayette,
Enfli
Reaeai ch
Ind. " 453
and
465
kj. of
Quaner maaier
Engineering Cemer
Naiick, Maaa.
RKliabialogtcal Lab.,
Texas, AuaUa
Raytheoa Ca, Walttia n. MMa
Reflectone Electronicf. Inc.
Scafliord, Conn.
B— lilatr Polytechnl: InM.,
Troy. N.Y.
Reeearch Late, for i
neerlng Sciences, U
Vlrgmia, Charlonei
RIAS. ■aitimorc, Md.
Rocheaier U. , N.Y.
Rocketdyne. Canoga I ark. Calif. 419
I Cewer,
432
Rome Air Develcsii
GrtffUa AFB. N.Y.
Royal MUltary Coll. (t Caiftda.^ 47S
( adiailan
Sarah MeUon ScaUe
Lib., U. of PtttaburAi,
Sclnoi d AvladoD
Brooka AFB. Tex.
Me Heine.
Science Reaearch
Inc., Cblcago, 01.
Aai ociaiea.
394
Sferl-Coanda. Cllchyj(F ranee) 457
Skiacron Electronlca
Tdevialca Corp.. t
Southern Reaearch
Birmingham, Ala,
Space Sciences Lab,
Electric Co. ~ "
Speech Research Lab
Michigan. Abb ' ^
ArtK r
^e'iSsrry
Co,
Paae
404
Ind. 406
ring
! Engl-
Ule
404
432
436
410
457
4M
410
450
396
399
Pa.
468
3*)
uid
biic
York 452
448
General
PhUaiklpMa. Pa. 440
. U. 0*
466
419
PB_Nun*er.
161 371-10
153 265
152 904
152 688
1.S3 301
150 699
153 240
171 419
147 045
153 261
153 315
153 501
153 356
153 412
IS3 414
153 ■'11
152 881
147 778
152 319
153 205
171 420
153 166
150 700
147 778
153 302
148 771
153 378
152 928
171 417
153 492
153 170
154 298
Source
Sprln^leld Armory, Mass.
Stanford Electronlca Late.,
Siaaford U.. Calif.
Stanford Research Inst.,
NtenloPark. Calif.
Stanford U., Calif.
Stoddan Aircraft Radio Ca,
Inc., Hollywood. Calif.
SyracuaeU., N.Y.
Page
F*Nun4>er
SasSA
445
153 223
Unlveralty of Southern
CalHomla School of Medicine.
432
433
153 169
147 243
147 244
Loa Angeles
Upper Air Lab.. U. of Colorado
Boulder
150 715
150 716
Uppsala U. (Sweden)
411
452
153 314
153 206
Van Canv l.ate.. Terminal
laland. Calif.
475 154 294
433
450
Technical Operationa. Inc.
Arlington, Maaa.
Technische Hochschule.
Stuttgart, West Germany
Tessa A. and M. Coll.,
College Station
Thermophyslcsl Prooenles
Research Center, Purdue U.
Lafayeae, Ind.
ThonBsoa. John 1.. and Co.,
WMhli^on. D.C.
Thonvson Ramo Wooldrldge,
Inc., Ingle wood, Calif.
TRC. toe., Syosett, N.Y.
Ti«s U. School of Medicine.
474
413
479
441
434
464
400
401
4oe
University at Southern
California Engineering
Center, Loa Angeles
434
1-4
150 712
153 358
153 359
153 360
Syracuae U. Reaearch Inai., N.Y. 459 171396
462
154 407
153 466
150 691
171 478
171 418
I
153 235
171 397
153 526
1S3 S27
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 538
153 539
153 363
153 364
153 525
153 541
153 548
UniversUy Coll., Dublin (Eire) 469 153 094
153 446
Pas
399
464
472
Vehicle Research Corp.,
Paaadena. Calif.
Vienna U. , Austria
Vought Aatrcnautlca Div , Chance
Vou^ Aircraft, Inc.,
Dallaa. Texaa
Waahtem Observatory,
Madison, WU.
Washln^on U., Seattle
419
462
WaaMnpon U.. Seattle. Coll.
of En^neerlng
Waahinglon U., Seattle,
lahing
chooT
of Medicine
Waienown Arsenal Late., Maaa. 445
Watervllet Arsenal, N.Y. 462
Wayne State U., Detroit, Mich. 451
Western Ontario U. Csnsda 436
Westlnghouse Electric Corp.,
Baltimore, Md.
Westlnghouse Research Late.,
Pinatergh, Pa.
Willow Run Late., U. of
Michigan, Ann Arbor
Wlaccmain U.. Msdlson
Woodb Hole Ocesnographic
Inatltutlon, Maaa.
Wyman-(jordon Co., North
Grafton, Maaa.
434
434
447
399
413
435
4.S1
413
414
tut '^i 'x*
« f »
lUJtt
434 153 «c
IS3SM
3« IMSII
1M1«
I53»
419 1S2 7W
468 153 131
402
153 »
450
ISSW
451
ISSM
434 I53SSS
399 153 a
ISSW
171 Ik
161 M
1S07B
153tt
IS0 71»
ISOTIfr:
171 3h
171 M
413 ISIM
153)17
153HI
153 M
ISO Ml
l«7»
mill
445 171 PI
s«*e£.«
MM wiitclss
U^mlf costings
AkMTVtto
-llMorT
Aeeiltradon
■ -Ikyslotagical effects
j^ceslaratian tolerance
..fhipslolagical effects
MsriKoneieri
-Errors
419
422
399
437
■MKsbolIsm
400
r
■ ■OmbIcsI resctiuna
A(kti««iDeni tens
-Dwelopment
Acrylfc resina
-AfpUcaliona
■r I
401
«Xl
410
394
443
427
472
436
MfMlpMsry
--Tralalag devices
Aartal pbotograpte
-Alaska 441
Asrtal fbMograiAy
-HMoretlcal correction* 478
Atrial reconnaisssnce
/-Alatka
-Equiimeni
Mn^rsamic coefficients
nic heating
ermeaaures
454
454
441
re Numter
1«2 716
171 416
153 657
171 367
147 778
152 917
153 526
153 sr
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 538
153 539
153 363
153 364
153 525
153 157
148 771
153 286
153 950
153 310
171 419
153 S40
171 385
auremeni
-Ikyslcal effecu
Itn^samics
"Tliiory
Aaiuslaatic response
Atrospacs life support
Air
"Raduaon
"Radloactirity
Mri
411
153 371
427
153 396
454
171 407
454
149 676
438
171 363
474
153 105
439
152 829
454
171 407
454
404
455
Mr traffic control sysiema
-OaBiMnicaiion ayatemit 430
-Hsnan engineering 417
AircrafI
— Aatodynamic cteracter-
Itdca
-Mtlaisnance
•Maatrlals
455
392
458
459
418
-Simulation
Atrcrtfl maienala
"Fatigue 461
Altplaec landlnga
-Statutlcal analysis 416
Alrpitae panela
••tiadslch conatruciion 418
Mip*tf cootrol towers
417
449
-Iknry
450
Atall netal carbonatea
--Ikns Btudtea 410
AkaH asul telide crystsls
--flMBGoaductivlty 472
--Progtrtles 471
"SiMrtag 471
AkaUatuls
171 415
171 407
171 418
149 676
161 371-10
171 387
171 388
171 368
150 920
171 387
171 388
153 547
153 929
161 229
171 411
171 404
171 410
171 570
171 408
150 920
153 306
153 308
153 436
147 045
153 143
171 371
171 371
4M 1S3136
SUBJECT INDEX
Sub|ecf
Alksllne earth telldes
--Bonding
Alloys
7 -Corrosion
- -Deformation
- -Streaaea
pro-
- -Ttennodynamic
pert lea
Aluminum
-Applicattona
--Temperature factors
Aluminum alloys
--Fracture
Aluminum crysuls
- - -Creep
A lumi num - msgneslum
alloys
-Deformsiion
Aluminum oxide films
•Prepsrstion
Aluminum oxidet
--C3iemical reacuons
Aminea
Chemical reactlona
Amino compounds
-AppI lest ions
AN ASC-15-T1
^m^k
XW I)
AN,MRC-71
AN/PRM-10
AN/TJRM-26
AN URM 268
Anslyitc functions
-Theory
Animsis
- -Alssks
--Psrssltea
Annihtlstlon resctions
--Analysis
--Theory
Anoxia
--Fhysiologicsl effects
Antenns radiation pattema
—Madieinaucal aoalysis
--Polsri^stion
Antennss
- -Blbllogrsphy
- -Design
--Toniue
AntlMollcs
- - Effectiveness
Antimony
-Bibllagrs|ihy
Antimony chlorides
- -Crystal structure
Anti protons
--Nulcaar reactioas
PSE
411
461
462
461
462
458
441
470
460
470
460
434
408
409
407
436
424
421
424
424
424
449
403
441
408
464
463
397
399
421
429
429
«»
429
434
43S
431
403
391
472
463
Antltrifoaofneinc functions 449
Applied mathematics
-Theory 465
Approximate computation
--Appllcationa
Aptitude teats
- -Appllcationa
Arctic regions
- -Meteorology
Argtn
--lani,^tion
-niyslcal factors
Armoied vehlclea
--Human engineering
ArtlflcUl kidney
--Appllcationa
Aatronautics
-TheoiTr
Aairoaomical canieraa
Aatroflqwlcs
- -Blbllogrsphy
Asymmetrical force flelda
i-S
496
396
413
410
408
403
439
478
465
472
PB Numter
1S3 314
151 103
161 896
151 103
161 896
153 929
171 418
171 360
153 167
171 360
171 242
171 246
171 246
153 306
153 518
153 540
153 518
1S0M4
150 693
171 392
153 409
153 224
153 696
152 719
153 712
152 719
153 235
153 242
ISO 319
153 192
OTS-SB-438
153 310
150 693
150 694
153 754
154 291
153 104
148 006
ISO 723
153 356
149 731
153 469
153 193
153 055
152 388
161 560
154 297
StJiiect P«ae
Atmosptere
-Arcdc regions 413
--Blbllogrsphy 412
--Chemical reactiooa 406
--Electromagnetic pro-
perties 475
- Motion 413
--Radiation 412
--Radioactivity 464
--Sampling 464
--Spectrograpbic analysis 415
-Wsve trsnsmission 476
Atmospterlc refrsction
- -Opiicsl effects 413
Atomic bomb explosions
-DetecUcn 462
--Riyslcsl effects 432
Atomic spectra
- Ans ly* 18 467
Attention
- - Physiologicsl factors 395
Attitudes
- -Messurement 396
--Test methods 394
Audiences 394
Audiofrequency sttenustors
--Calibration 423
--Test results 423
Audloroeiers
--Test methods 398
Auditory perception
- -Psychologicsl factors 396
Auditory signsls
--Detection 466
Automstion 476
Avlstioo personnel 393
• - Performance 393
- Selection 393
Avoidance betevior 397
Axial flow compreasors
--Performance 468
Axially aymmetrlc fkw
---rU>les 457
Bsckwsrd-wsve smpllfiers
-Development 426
Bs lances
--Cslibrstlon 406
Bsllisuc cameras
--Applications 436
Balllatlc data
- - Photographic analysis 436
Bsllooos
- -Appllcstlons 434
Bsnd-psss filters
-Design 430
Bsng-teng system 42S
466
Bsrium carbonate
--(SKinical reactiooa
Barium tiunates
- -Oiemicsl resctiOBS
- -Risse studies
Barometers
■ -Calibration
Bats
-Ultrssonlc properties
Beaches
- -Erosion
- -Maaaachuaetu
Beam-aplilter
Beama
--Vlbrsticn
Ben^-ene derlvativea
- -Spectra
Ben..oic acids
--Tempersture fsciors
Ben'^yne
Beryllium
-Mectanicsl properties
Beryllium slloys
--Development
--Mectanical properties
Bibliography
- -Adjutant General aOrfice 393
471
471
471
465
428
413
413
484
409
408
409
459
460
460
n Numter
150 723
153 437
150 690
150718
150 723
1S3 634
171 361
171 362
171 361
171 362
150 697
152 835
152 682
153 395
153 205
153 153
153 126
153 141
152 881
153 287
153 287
171 2V
171 228
171 227
171 228
153 778
171 403
153 170
152 876
153 853
153 852
153 852
153 458
152 874
152 838
153 400
171 236
150 070
150 070
153 235
150 692
153 438
153 099
146 924
146 924-
146 924
171 337
153 ««7
147 311
147 311
153 303
153 SOI
152 611
153 76S
152 6II
171 4tl
1713t9
171 389
153 440
Sub)cci P«ae
Biblio(ra|*y (con. )
- - Aerodynamic dau 455
--AaKoaas 429
--Aatro(!iiy*ics 465
-- Atmosphere 412
- -Ceatrifu0e* ^i
- -Chemical e lemanci 391
--Chemtcal informal ion
■earching 479
--CMmag tc»l8
--Documenutioa 479
- -Exploaive forratni
--Germanium 391
--Heat sinks 417
- -Hlgti impsci meta
forming
--Humsa cnginsenni ; 392
-Uljnid-soUd cycle le 391
--Ma«Kslum 460
--MaterUI* 417
-Meul cutting
--Metal plates 453
--Missiles 479
--National Bureau at
Standsrds Wash! igton
D. C. 465
--Operations reaear di 477
--OM»e 412
-Plasma (Fiiysics) 465
--Quamrtnaster Ccf-ps
textile reports
--Rockets
--Scientific repo-ts
- -Semiconductors
-Silicon
--Splroctetoeis
--SysKins engineer
--Textiles
--Transducers
Bioenvi ronments
Bismuth
--Blbllo^aphy
Blackbody radiation
--Absorption
--Energy
--Sources
Blast etfccts
- Couwemwasures
Blindness
- -SatEty devices
Blood
-- Effects of radlatl<^
Blood chemistry
- -Genetic (actors
Blood circulati'41
--Measurement
Blood pressure
--Measurement
Blunt bodies
Bodies of revolmoa
--Aerodynamic
iSUCS
chars :ter
436
393
472
391
404.
I« 477
448
391
411
sry Isyer
-Hypersonic
Body lampersture
- -Climatic (actors 397
Bombing
- Training devices 439
Boolean formulas 450
Boron
- - Bombardment 446
Boron carbides
-niase studies 447
Boron compounds (Or [anic)
-Chemical reactions 406
Boron hydrides
--Toxic effects 396
Boron nitrides
-Symhesis 434
Boron phosphide
-Syndiesis 434
Boundsry Isyer
--Turbulence 456
Brain
--Effects of radtsbVi 4tM
■remssirahlung
Blty 472
391
465
465
466
432
440
427
404
400
399
399
3*9
4S6
4SS
456
456
PB Number
171 387
171 388
152 719
161 560
lt3 437
154 409
OTSSB-438
161 566
MBTAL
161 SM
171 379
OTSSB-437
171 372
171 379
153 547
154 409
01^88-445
171 372
METAL
171 374
152 978
161 560
152 914
153 437
161 560
OTSS8-440
153 182
153 440
OTSSB-435
OTS SB-437
ISO 062
152 914
153 129
OTSSB-440
153 505
153 371
aresa-438
149 296
149 296
171 238
153 30S
154 406
153 101
153 301
153 303
153 347
153 365
' 153 365
153 106
153 420
152 844
154 403
153 106
153 420
153 373
153 0B6
153 458
153 439
171 365
153 215
. 153 216
153 174
171 364
171 364
150 982
153 304
153 426
Subie
Broadbsnd antennas
--Anslysis
Broue
- -Caulytic properties
Bud^t control
Bunny boou
Burns
-Padiotonr
Callbranon
- - Instrumentation
Capacitors
--Development
Capiul structure
CSrbinols
- -Chemical reactKxis
--Isomerism
Carbohydrates
--Metabolism
Page
429
434
472
444
464
403
404
424
428
479
406
40S
401
402
Carbon
--Determinstlon
--Temperature (actors
Carbon dioxide
--Analysis
Cardiac muscle
-Physiology
Cargo
-Transportatian
Cascode amplifier
Csstings
-Production
Csibode ray tube screens
-Visibility
Cathodes (Electron tubes)
--Materials
Cestrifu^rs
-Bibliography
Ceramic materiala
--Development
--Mechanical prtiperties
-Stability
-Temperature (actors
■-Thermal properties
Cerebral cortex
--Riysiolofy
Cerenkov radiation
Cesium cloud
Cesium halides
-Color
Chalcopyrites
Chemical reacuons
--Analysis
405
407
399
396
442
421
458
431
467
391
465
446
446
446
447
422
397
462
414
470
471
407
408
479
Chemistry
Chlorine Isotopes
- - Resonance 409
-Spectrs 409
Chlorophylls
--Phcxochemical reactions 400
Chromatographic analysis
--Applications 405
Chromium plating
-Ultrasonic (actors 445
Circulatory system
--Climatic (actors 397
■niysica I (actors 398
-niyslolofy 396
Clays
--Crysul structure 470
Cleaning fluids
--Development 407
Climate
-Alaaka 411
412
-Greenland 412
Clouds
--Rsdlation 415
--Tlemperamre 415
Cosnda effect 417
Cosnds ooc^le 457
Cohalt compounds
--Spectra 410
Cobalt oxides
-ntase studies 470
Colimycla 403
ColloidB
- -Ap^cations 442
1-6
PS Number
153 696
153 555
153 147
150713
153 516
153 192
153 194
171 233
171 234
171 235
150 709
153 148
153 265
153 156
153 537
153 538
153 541
153 548
171 409
154 096
153 335
153 174
153 145
150 704
151 098
143 302
153 6S3
154 409
ISO 922
171 398
171 406
171 406
171366
171 416
' 153468
152 866
150 721
147 174
150 323
171 376
171 373
161 586
150 921
150 921
153 127
171 409
' 153 223
153 369
171 367
153 174
147 173
171 128
153 514
153 324
153 093
153 061
153 061
154 292
133 378
149 648
147 759
153 192
153 441
Subject
Color centers
Combst skills
Combustion
--Mathematical analysis
--Stability
Cocnmuntt^atton systems
- - Performance
Complex (»mponem develop-
ment
Complex ions
--Decomposition
- -Spectrs
Compressible (low
-Tables
Concrete
--Test results
Conferences
Confinement
Conlcsl bodies
- -Structural analysis
Containers
-Materials
Control systems
--AppUcstiins
--Dtslp
- -Hunan engineering
- -Synthesis
Cools ou
- -Cheiwcal analysis
Copper -'hicke I slloys
--Magnetic properties
Copper plating
- -Ultrasonic (actors
Correlstioo (unctions
- -Applicsiions
Corrosion
--Hiyslcsl (sctors
Cosmic radiation
- -Measurement
--niotogrsphic analysis
-Tsbles
Cosnuc radiation ahowers
- -Sutlstlcsl analysis
Co«4>liiig Circuits
-Design 'a
Crocco vsrisbles
Cross slip mechaniam
Crysul detectors
- -E(|uipment
Crysul holders
--Development
Crysul structure
--Aaslysls
Crysuls
--Exciution
--Resonance
- -Surfscc properties
Curb detectors
Curie points
Curpistor diode timers
Cutting tools
- -BlMlogrsphy
Cybernetics
Cyclic canptxmds
--Solvent properties
Cylinders
--Structural analysis
Cylindrical shelU
- -Stresses
Dsu
--Processing
Dsu storage systems
--Circuits
--Developfnent
--Equipment
--Theory
Data transiiuaaion systems
--Msthemaiical analysis
Day
- -Msssurement
Dshydrogensses
--Biochemistry
Ds-icing systems
--Test results
Delay elements
--Development
Pas
470
447
447
465
427
472
409
410
454
418
477
398
453
441
445
434
392
425
466
405
466
445
451
460
392
463
392
449
421
456
470
420
420
472
465
409
472
427
466
437
392
476
405
453
453
452
479
463
440
451
452
479
426
412
400
416
437
147 174 ,
1»«H
lUM
154 410
154 4U
1S2M
171 «
154]«
147 771
149 Ml
15347)
151 171
152 «0
IS3W
153 S
.171411
171 SI
153 4«
153116
isia
153 DM
154 «
15} ai
153 2S
153 Ml
153 IC
141 M
153171
141 «N
153 3H
152 W
ISSM
mm
153217
153 2r
154 217
l»«
1S01B
1541V
153 W
153 ai
153 «l
metAi.
153 Itf
152 IM
153191
153 3SI
153111
153 HI
153 49S
153711
1907a
152 W
ISOOM-'
190 OIH
190 an
153 7J»
15378
159011
153141
15391
192 «M
[Way Unaa
•-Afphcatlons
..Development
Dslu moduUtors
Orrclopmeni
Its
gflsctiveaeas
"A«sly«'»
"Tteory
Ql^aM concrete pavement
Ockits
Oslectrics
-Electrical properties
..Syalbesis
DM
-Forging
■ -Msdiining
DM
-Alaaka
OMfcrcstial equaiiins
-AsBlysis
■•Ttaory
[Mbsioa
-Aaalysis
Di^silse system
-Hqwiotagy
aisaneiers
-■Dnign
Diodes
--Afplications
Otpoie sniennas
-RadUtlon
DMdaifs tubes
- -Applicalions
-AlaaU
Psje
432
432
421
427
407
450
449
450
418
470
425
434
445
445
441
476
454
449
450
450
446
399
470
433
421
429
403
DIstrliMied amplifiers
-Qrcults 431
-■DMSlopment 421
auon 479
479
391
479
422
436
-kbliagrsphy
-Thsory
sr tracking systems
--Applications
--i^r(onnsnce
Drops
--Coabusiion
"OKlllstion
Dim* door
Bar
--Aoousuc (actors
■-Ihysical factors
Earth
--Radlauoo
Esrthfuskes
- ttlMilsnnn
lie conditions
--Scsttstical analysis
E|acnon sesu
-Ibsi results
BMC pisses
■ksdclty
--Msthtmaticsl analysis
"Thsory
BtKtric discharges
-Baargy
■iKtrlc insulators
-MaKriaU
BiKirlcal networks
su
euc fields
--Optical propertisa
tlwtiniisgiiiuc thsory
BnnaMiPWtlc waves
"MiteMatlcal analysis
"Ptopagatlon
UKtron beams
-Applications
-Essror
436
422
442
458
393
397
399
392
412
411
403
411
479
418
453
453
453
466
434
422
476
474
414
475
476
433
467
PB Number
171 420
171 420
153 004
153 101
171 12*
IS0711
153 305
153 711
153 178
147 173
153 417
171 364
171 378
171 378
153 523
148 525
171 415
147 121
153 414
153711
171 400
1S3S11
147 759
147 244
153 224
153 245
153 407
153 513
150 720
150 704
152 978
171 478
161 586
153 SOS
153 770
153 494
150 724
150 724
150 066
153 441
153 162
153 323
171 392
147 778
ISO 772
153 634
153 422
153 507
153 371
153 148
153 404
171 374
152 904
171 374
153 073
171 364
153 175
152 781
171 395
150 071
ISO 718
152 781
ISO 716
152 931
Sub)e«
Page
Electron beams (con.)
--Interference 426
--Mathematical analysis 433
--Production 430
Electron bombardment
--Applications 400
Electrtn guns
-Design 430
Electron tubes
-Development 432
-Reliability 42*
-Theory
Electromc camera
Electrtmic circuits
--Development
--Mathemaucal analysis
Electronic cdmmuutors
- -Development
Electroiic equipment
- -Applicationa
- -Blaat effects
- -Design
--Testing equipment
Electronic switches
--Theory
Electrons
--Density
--Magneuc moments
--Resonsnce
Electrophilic displscemeni
Equivalent networks
Ergodic theorem
Eskimos
-Alasks
--Ciilture
--Nutritioii
--Physiology
Ethyl fluorides *—
o-Dlpole momenn
--Microwave spectra
Ethyl nitrates
--Propellant properties
Ethylene oxide
- -Optical properues
Euclidean space
Euler's sngles
--Applicationa
Evacusdoo bag
Exit uxiways
Experimental dsM
Analysis
Explosions
--Pressure
--Thet>ry
Explosive cfasrgM
--Applicationa
Explosive forming
Explosives
--Blast
--Sensitivity
--Test methods
Exposure
--Biochemical effects
467
478
431
433
422
430
427
432
427
420
425
4U
432
467
467
406
422
478
47S
47S
4«l
399
403
467
467
438
405
450
418
465
417
477
476
43B
43B
43B
438
400
401
-Countermeasures
-niysiological effecu
1-7
402
465
397
399
PBNionber
153 400
150 715
153 504
153 397
153 504
153 240
154 484-1
154 484-2
152 931
152 588
150 720
147 244
150 066
150 707
153 101
153 205
171 380
150 703
153 S79
153 484
153 498
153 291
153 291
153 215
153 216
153 175
153 360
153 367
153 520
153 521
153 523
153 347
153 SIS
153 153
153 153
152 316
150 656
153 433
171404
153 510
171 369
153 633
152 835
153 HI
171 379
171 379
171 326
153111
171 326
171 326
153 526
153 527
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 538
153 539
153 363
153 366
153 525
153 541
153 548
153 510
153 373
153 545
153 372
153 511
S<*ltt
Exposure suiu
- -Test results
Exterior bsllUtics
--Detenmnation
Extraierritorisl waters
Eye
- -Blood circulation
-Modoa
F-centers
F3H-2N
Fatigue (Mechanics)
- -Teat methods
Fatty acids
- -Blochemicsl etiecu
- -Mataboliam
Paie
464
4SS
479
400
399
470
472
416
461
402
400
401
- -Oxidation
Fermi age theory
Fermi -Yang dieory
Ferrliea
--Machining
Ferrocenea
--C3iemical reacttona
Ferromagnetic films
- -Optical properties
Ferromagnetic iiuterials
--Aaalysis
--Magnetic properties
Ferry service
Fire control
--E(|uipment
Fire control computers
--Design
Fixed capacitors
--Calibration
--Test results
Flame propagauon
Flight attitude indicators
- - Equipment
Flight padis
--Detenninstion
Flight vehicle msterisls
Fluid flow
- -Mathematical analysis
Fluid mechamca
Fluids
- -Conductivity
- -Wave tranamlaaion
Flutter
-Mathematical analysis
Flying platfortns
-Test results
Food
- -Conuiners
Free )et impingement
Free radicals
- - Producuon
Freqitency meters
- -Calibration
-Ttst results
Fre<|uency modulaOon
receivers
--Test methods
Fricoon
--Tempersture factors
402
402
463
462
406
471
466
459
466
435
439
436
422
422
437
418
461
443
473
457
473
475
454
419
441
417
408
423
423
424
41*
469
PSNimiber
153 308
171 387
171 388
153 121
153 303
147 778
152 604
153 143
153 289
171 410
153 363
153 364
153 526
153 527
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 539
153 525
153 541
153 548
147 900
153^309
150706
153 2*5
153 2»4
150 922
171 025
153 281
152 320
152 321
153 0B6
171 419
171 239
171 239
152 654
171404
152 320
152 321
171 410
152 525
153 074
153 261
153 074
147 400
171407
150 075
171 418
153 083
152 685
171 231
171 240
171 229
171 230
171232
171 231
171240
171 229
171230
171232
153 241
171474
rmt»
--towic efiecta
--TruMportatioB
tmctuma
--Aastjrsta
Fundus camera
CalltMn
- -BlMk)grapbt
Oas aaaly^rt
-•Design
Caa baariafs
--SuMllnr
Gaa cycle cooiinf
Gaa dlsdarfea
--Appilcatkna
Qm flo*
•- Measure ment
- Tables
Gaa kaUation
—AffbcmujM
Gaa MrMnes
- - fcrtormsnce
Gases
--Abaorpiive property
--Specihc besi
--Spectra
GeaeUcs
--Alaaka
Oaonaerlcal ofxlca
Germanium
- -MbHofrspiiy
- -CooducUvity
Class
- -Dtelectrlc propernis
--Baacta Qf radtaiion
Ciycslysla
--Tenperaiure factoi
Gaggles
--Arctic )
Gotter
Graloa (Meulhnty)
--Stresses
Grapkite
■-Thermal properaet
Gravity
-Physical eflect*
Grinders
--Develapinent
Ofoand efleci phesome^
Cyronoopes
- -OvsskiproefM
Oyrotron
Halofsn compounda
(Organic)
--Chsnucal reactioni
Halofeaa
--laudation potential
Haap
Haariog
--nysiology
HMrt
--AysiOlagy
Hsai at stAlimation
--OBterminsiion
Haat reals UBi alloys
- -Caatlng
--Europe
■-Patutue
--fhaae studies
Hsatalaks
Helicopters
--fcrtormance
HeUtan
--Tbarmodynamic p^-
pertiea
Hellm (Liquid)
• -Dtelactric properties
Haliun lona
--AooMBtic propertKf
-EquipmeM
Helminth parssiiea
Htpaaiis
- Alaaka
W^ altitude
--Bkptoradon
- - laatmincaiauoa
39i
447
4S0
44«
400
3»l
399
442
438
439
4M
4S4
419
443
41 S
4M
399
476
391
475
472
446
3*7
464
403
470
445
474
444
419
419
419
407
469
464
997
397
407
45*
446
461
447
417
439
474
416
474
475
409
409
4*5
4tS
402
403
416
426
153 174
153 07«
153 711
153 754
153 303
crTsa-43«
153 335
153 12t
171 363
153 245
152 ^74
153 477
152 319
152 525
153 283
153 477
153 136
153 6S7
153 347
152 781
crrss»-437
171 sn
154 397
153 439
153 545
153 909
153 515
171 360
171 390
171 395
ISO 706
130 075
154 298
154 298
171 376
153 397
171 3*1
171 362
171 392
153 369
154 096
151 098
161 233
171 410
171 391
171 372
152 829
171 395
154 406
153 106
153 166
153 608
152 608
152 688
192 688
153 522
153 583
153 334
153 231
SM>>ect rge
High pressure research 459
High temperature resesrch 472
Honrsi John 437
Hoaevcomb structures 418
Human engineering
--Arctic regions
- -Bibllogrsptiy
Hydatid diaeaae
Hydrates
--Spectra
Hydrodynamica
--Theory
Hydrogen
--Oiefnlcaf reacttons
--Determination
--Oxidation
Hydrogen bonding
HydrofM embrlttlement
--Analysis
llydrofsn Ions
--Determination
Hydroxyl radicala
--Excitation
Hydroxyl radical*
--Spectra
Hypersonic flow
- - Mathematica 1 ana lysis 456
392
392
403
409
438
408
406
406
408
410
408
4C8
Hyperaonic noczlea
--Dealgn
Hyperaoiuc wind tunnela
--Calibration
--E>^pment
Hypervekxiiy projectllea
--Penetrauoo
Hypanmlocity vehicles
--Cooling
--Flutter
--Maieruu
--Str
Hypothermia
--Appllcationa
--^yslologlcal eflecu
HYVU
Ice
--Greenland
iMcryaula
--niyaical properties
Icoaoacopes
--Devclopfnent
Igaliers
--A-1-A
--Developtneni
Image laocon tube
Image sl.u
Impact ahodi
--niysical effects
Impedsnce
- -Mesaurement
Indium
- -Blbllagraptiy
hidlum ant imon ides
--Electrical properties
Indoatrlal production
--Coaia
Induatrlal paychology
Informaticn theory
457
457
417
457
440
438
454
417
445
437
398
397
398
399
4SI
411
411
408
425
437
437
425
478
440
422
429
391
469
Infrared dececiors
--Calibralion
Infrared equiptnenl
- -Callbrstion
--Deaign
Infrared spectre
- -Analyaia
Infrarad apectroacopy
--Appllcationa
--Theory
Infrared vavea
--Abaorption
- -Meaaurement
426
452
478
479
4«8
468
399
412
415
466
468
8«7
415
468
415
n Number
171 025
153 426
ISO 097
171 408
153 547
153 547
153 507
147 77*
153 650
190 923
171 409
150 690
148 021
171 394
133 356
ISO 923
150 923
153 106
153 184
153 420
153 315
152 838
153 435
152 838
153 316
171 363
171 407
171 372
171 390
151 101
153 544
153 369
153 544
153 542
153 560
153 480
153 480
148 021
171 386
152*54
IU6S4
171 386
171 385
153 316
171 245
152 693
ore SB-438
171 406
ISO 713
150713
153 722
153 361
153 360
153 770
171 238
171 238
153 335
153*34
190 697
153 657
153 136
153 392
153 393
153 283
153 657
153 061
Subject
Inatrumenu
--Calibration
Pag
423
«»
Inaulaiing cam|
- -Development
Integral equaiiona
--Analysu
Intelligence tests
-Effectiveness
- -Sutistlcal analyals
Interior balliatics
-Madieinatical analysis
Intermeullic compourida
--Electrical properties
International Geophyaical
Year
Interplanetary manauvera
Ion beama
--Production
-Thermal effecta
Ionic colliaions
lonoaphere
--Analysis
- -Electromagnetic pro-
--InnlMrtnn
--Reflective effecu
loooaptteric diaiurbancea
--Analysis
Iron-nlcfcel slloys
--CrystsI structure
Iron-vadhdiura alloya
--Magnetic properties
Pi
]et engines
--Exhauat gaaes
Jei mlxiag flow
--Analyaia
]et atreama (Meteorology)
- -Turbulence
Job analysia
- -Psychologies! factor*
Journal bearings
--Lubrlcaiioa
Kidneys
--Psthology
•-Physiology
Lsminsr boundsry Isyer
--Hast transfer
--Madsmailcal analyals
Landiiw fields
- -Greenland
-Codiag
Laval nozzles
--Hesi trsnafer
Lebesgue iniegrsi
ught
--Intensity
--Meforological factors
LUnoolagy
-Alasfcs
Line broadening
Llqyld iiKtala
- -SolvetK proiKrtica
466
434
47*
4U
4*5
396
394
447
471
461
392
439
U*
419
436
41S
414
415
415
432
432
471
466
416
418
457
413
393
442
409
399
456
455
456
411
491
452
475
451
413
413
413
467
409
171 2SI
171 »
171 M
171 M
171 M
171 at
17128
171 211
171 2»
1712a
171211
171 Ml
171 2»
171 la
171211
17128
171 at
171 235
171 Ui
171 M«
171 M
171 29
17121
171 M
148 SB
158011
14* M
147121
148 01
141 (U
ISS2W
ISO 321
171 MS
141 4N
I5S«
IS21H
lS23if
153 UI
153 4M
19001
ISSlff
161311
153 1«
1SS4II
ISSIM
153 ai
151 at
issm
i5sai
I30MI
15SIS
151 la
15} la
19SM1
151 KM
153 OH
155 W
1514a
liotaM
isoiaH
154 at
isoai
192 Ml
151 Mi
mm
153M
15SM
IMW
im^ meuls (con. )
-Ttennodynsmlc pro-
Bsrtlea
imit racket propellanta
Omtim-'—
U^-soUd cyclone
stion
-HMt trsnsfer
■Vlaoaatty
-Preclptutlon
Ltm
.-gtacheiiusiry
1-8
Psge
409
447
391
442
474
458
470
400
4IN
-nifsiotogy
-llactncal properties
traaaladona
402
3*7
401
402
Logiadi*
--Mariieinsilca I analysis 44i
Lae tenperature research 408
Lmlaeacence
-AMiysi* 440
lU **>
397
451
452
445
392
460
460
430
409
410
-Aaalyais 443
-MaiMfnailcal analysis 473
ifMoatriaion
•Ihaory 466
432
■ArcHc regions 392
ilaMaaaoe peraonnel
-1M«^ 393
■agmaiK engineering
-Iteory 479
Bic aapecta 444
trs
■■DMpt
Hlikovdiaina
Mnaaaargy relaiiona
MH8 ipactrofneiera
"Ooatrol systems
■ -Huaaaei^neering
Mifilien
-Bibliography
Ma^aaluin alloy*
-•Fracture
Msgaetlc modulstors
-Drvclopfnent
Mspnlc resonance
- -Meaaurement
hydrodynamic
•Dawkvmeni
418
450
442
457
417
428
469
417
460
-Hlnrwanic analysis 445
IMiaMlcal computer dsia
--Ggdli« 428
--Fracaaslng 391
438
IMHatkal rmnpimrrs
-Afpticatioa* 413
MMa trsnafer
IkMnals
--Bibliography
■-Dtvelopment
"Frlaion
--Hni transfer
FB Number
161 990
154 410
154 411
154 409
153 441
171 395
153 162
147 130
153 526
153 527
153 528
153 529
153 530
153 531
153 532
153 533
153 534
153 535
153 536
153 537
153 538
153 363
153 364
153 525
153 541
153 545
153 539
153 548
153 145
153 765
153 316
153 492
171 392
150 086-7
150 086-8
ISO 086-9
171 378
153 169
OTSSB-445
153 167
153 454
147 776
149 648
152 830
153 074
150 695
150 699
153 547
153 779
153 148
147 534
152 873
153 358
140719
ISO 700
153 315
171 372
150 709
171 474
171 372
153 077
171 186
152 974
152 827
153 220
153 560
150 060
Subject
Page
Msthematicai computers (con.)
- -Aspllcstions (con . ) 414
440
451
- -Circuits
--Design >
-•Development ■
--Schaduling
MadieiMtlcal predication
-Applications
•-Theory
Matrix algebra^ .
--Appllcationa
MD-1
~Medical cameraa
--Equipment
Memory
-Teat methoda
Merchant vessela
-StAeduling
Meao-meteorological
network
Meaona
--Decay
--Nuclear reactiona
--Theory
Metaboliam
- -Climatic factors
Meul pistes
--Bibliography
Metalorpnic compounds
- -SynthesU
Metala
--Adaorptive properties
--Dlffuaion
--Fracture
-•Machining
- -Microairucture
--Proceasing
--Radiographic analysis
--Stresses
- -Tempersture fsctors
Meteorologies I bal loons
--Appllcationa
- -Tracking
Meteorological dan
Meteorological radar
--Applicaiions
--Development
--Effectiveness
Michigan
M Ic roradiography
--Appllcationa
Microwave amplifiers
-Design
--Development
Microwave equipment
--Design
- -Developtnent
Microwaves
- -Atwnustion
452
479
452
476
452
443
4H
440
4S0
450
464
400
394
442
412
464
464
462
402
453
406
408
446
459
459
444
461
444
461
437
459
460
462
458
392
411
412
432
411
412
413
461
433
432
433
434
435
421
423
--Prtipagation
Millury persomwl
--Alaaka
--Arctic regiona
--AttltiKiea
--Performance
Military resesrch
Military training
- -Effective neaa
Milk
-•Radioactivity
Millatone Hill
Minerals
- -Polymorphiaro
Miniature electronic equip-
ment
--Clrculta
1-9
475
393
393
397
393
477
393
404
438
470
427
n Number
153 134
152 689
ISO 086-7
150 086-8
150 086-9
161 586
153 206
152 876
153 361
153 181
153 002
153 492
150714
190 711
153 508
153 303
153 287
153 145
193 232
150 694
150 694
153 309
153 366
171 374
153 265
152 685
171 400
171 025
171 366
METAL
171 381
171 379
171 381
151 101
171 366
153 077
161 896
153 929
148 496
ISO 70S
153 232
153 498
153 394
153 239
152 682
171 381
147 243
153 240
147 244
150716
153 446
153 242
153 001
171 224
171 225
171 226
171 227
171 228
171 377
153 440
153 323
193 339
153 373
153 323
153 329
153 469
152 927
153 779
161 371-10
153 220
147 173
Subie
f>E
171 380
Missile Isunchers
- - ly rf ormsnce
Missiles
--Aerodynamic character-
is tica
--Bibliography
--Hydrodynamic character -
latics
- -Matsrisla
--Tracking
Modulators
-Clrcuiu
-Development
Molecular associatlan
Energy
Molecular crystala
Molecular apectroacopy
Molecular weight
-Determination
Molecules
- • Adsorption
-Ionization potential
Molten carbonatea
Molybdenum
-CaaUng
Molybdenum allt>ya
-Thermal properties
Molybdenum-titanium alloys
- -Physical properties
Motion pictures
--Psychological effecu
Motor reactions
- -Tempersture factora
Multipadi transmission
-Mathematicsl snalyau
NA 39
Naval equipment
- -Shock resisunce
Nsvsl personnel
-Training
Naval reaearch
Naval atructural mechanics
Navler-Stokeg equations
Neel temperature
Neutron bombardment
-Riysical effecu
Neutron diffrscuon analyaia
--Appllcationa
Neutron spectrometers
--Design
Neutrons
- -Molitxi
--Padiologlcal eflecu
-Spectra
Nickel oxides
--niaae studies
Niobium
-CaatiBg
Nitric acid
--Analyaia
- -Storage
Nitrogen lona
--Determination
Nitrogen oxychlorldes
- -Decomposition
Noise (Rsdio)
- -Meaaurement
--Souroea
Non-deatructlve (eating
- -Appllcationa
Noulaa
--Oeaifn
Nuclear phyalcs
Nuclesr propulsion
-Analyals
- -Economic sapecta.
-Theory
Nuclear apectroacopy
Nuclei (Biology)
- -Stimulation
Obaucles
- -Detection
Ocean waves
--Mathematical analyaia
Ooeanographical data
-Atlantic Ocean
--Pitxxaslng
Cmoer personnel
--Selection
OfWiore claima
Operatlona reaearch
436
436
479
436
458
436
421
421
456
409
436
406
408
467
410
458
445
458
396
394
428
418
441
393
480
452
457
470
446
471
471
4*3
4(M
464
470
4se
410
426
432
418
445
417
462
442
462
443
463
397
427
413
414
413 ^
414
994
479
450
n Number
153 161
153 425
152 978
153 1*1
161 229
150 070
153 004
153 001
153 106
150 921
153 636
171 4IU
152 685
153 397
147 045
151 098
171 390
161 229
152 881
153 321
153 225
153 404
149 520
153 779
171 316
147 401
153 459
147 759
153 439
152 982
152 982
147 900
193 301
171 397
147 759
ISIO**
153 948
153 948
153 949
153 366
153 173
153 400
153 169
171 408
171 18*
154 292
152 8t5
150 719
153 407
152 830
171 402
153 4*8
153 101
190 0*0
153 7*2
150 0*0
193 134
148 771
193 Ul
190 714
SMBt«CI
Operation* reaearch (c^.
- -ftbUocraptoy
Organic compounda
-Aaalyaia
--Ctemtcal ana^raia
OxldBCtan - reduciKxi re -
acTiona
OxidBa
--Spectra
--Surface propeniea
Oxyfen
- -Dewrmiaadaa
•Toxic effecu
Oxyfen (Liquid)
--Cooulnera
Oayfn e<|ulptnenc
--Devcloptneni
-UMlJCrapdy
--Oetnlcal reacHoai
Packaging
-MaierUla
ParaboUc bnttra
--Streaaea
Paramapienc cryaula
--Spectra
Parametric ampliflera
Paraaiiotogy
-Alaaka
Partial difleremlalc<|u itlo
--Applicaiiona 4*4
-Theory *4<>
Particle trajeccoriea
--nwfographic aaal^la 463
Article*
--Aaalyaia
--Oeoatty
--DrMctSon
-OtfluBloa
--Meaauremeni
-Moaon
ParUclea (Airborne)
-lUdiaactiTlty
ftiiiiiiican
Krceptlon
--ftycbological tect^ra
Permalloy filma
Peraooahty ceau
--Aoalyata
ftrturbation theory
--AppUcatioM
Aaae detector*
--Qrcuiia
niaae ahifter*
--Analyaia
ntoaptune oxidea
--Cryaul atructure
Plioaphor*
- - AppUcai lona
--Eflectiveneaa
niocochemical reactlc^
-Analyai*
nncocktauairy
FboMcoaductlvlty
nxuJehoronat ion '
niotograptuc emulaln^
--Appllcationa
--■ooibardntent
Phoiograpiuc Aim
--Proce*»ing
Fluumultipllcr*
- Development
-Senaitlvlty
nioioBa
-AppUcaUooa
--EMtgjr
nmoayiMheala
--Aaalyaia
Plkm
-Tratoing
Ptonck radiation funcf on
-Radw analyats
HjE
«77
40S
405
410
414
4«9
410
400
999
406
406
4U
40t
441
453
467
46«
42i
434
402
403
463
463
462
462
Wl
464
441
39i
471
394
4^8
442
4*4
4i^
42*
472
492
431
409
406
40f
469
406
464
462
«n
463
463
442
462
439
465
9»l
397
PB Number
152 914
171 409
1S4 408
154 2V5
ISO 721
153 094
154 295
153 303
153 409
153 354
153 354
153 437
150 923
153 19*
153 3S6
153 291
152 836
153 494
153 446
153 522
153 507
153 518
171 397
153 306
153 308
153 171
150 700
1^407
153 171
154 407
154 407
150722
171 361
171 362
153 5U
153 470
153 284
153 322
153 421
153 128
153 501
150 066
153 421
153 310
1S2WS
143 308
152 611
190 690
171 376
153 094
153 215
153 216
150 694
153 151
171 389
153 131
171 402
150 719
154 407
153 127
153 086
149 296
152 827
153 524
8Mbi«ct
Plant* (con . )
-Alaaka (coa.)
--Nutritive value
Plaama (Fhyaica)
--Mbliograpliy
--Propertle*
--Temperature factora
--Thoory
Plaanu oaclllatlon*
-Mathematical Jnalyala
Plaatic film*
--Application*
Plaaticlty
- -Temperature (actor*
-Theory
Page
441
397
434
443
472
465
473
474
473
474
473
441
453
452
453
465
432
434
456
Platinolron
Pointing control
ftnaeiulle flow
PoUrtacopea
-Clrculia 392
Political icienoe 479
Polymera
--Cry*ul atructure 405
--Molecular weigh! 406
--Optical properiic* 405
Polynomial*
-Analyai* 449
Poaitlon indlcaiora
--^rformance
PDtaaalum chloride cryatala
--<:>>lor
- -Photoconductivity
Power aeriea
-Theory
famtT aupplie*
--Developfneni
Preamplidera
--rtrformance
Precipitation
■ -Radar analyai*
Preaaure
--Maaauremem
--Fhyaical edect*
Pre**ure gage*
- -Calibration
--Teat reaulu
Pnmate*
--Etiecu at radiation
Printed circulta
--Maierlala
Privation
--Biochemical effect*
--Hiyaiological effect*
Probability (Sutiatics)
--Appllcationa
--Theory
Projectile*
•Velocity
Propellant graina
--Comt>uatian
Propellanta
--Handling
Propeller* (Aerial)
-Wake
Propyl niiratea
- -Propellant properties
Protective clothing
--Arctic region*
Proiactive shelter*
--Arctic region*
Proton acceleraiora
--Development
Proton beaina
--Attenuation
Procona
--Nuclear reactiona
-- Pathological effecia
--Heaonance
-Scattering
Paeudomonaa
- Senaitlvlty
Pseudomonaa infections
--Pittiology
--Therapy
Piychoacoustic*
1-10
430
470
470
472
449
429
422
412
465
459
465
454'
404
427
402
398
432
490
478
437
447
438
418
438
464
465
420
436
462
463
404
409
462
403
404
403
396
466
n Number
153 540
153 524
153 446
152 830
153 426
161 560
153 098
153 466
150 688
193 466
154 404
153 198
147 362
147 401
147 362
154 291
153 240
153 442
190 982
152 872
153 131
150 656
171 401
150 656
153 305
171 368
192 604
152 604
153 143
193 306
190 889
193 494
193 239
171 237
171 025
171 237
190 067
153 301
171 380
153 363
153 469
153 205
153 358
153 359
153 360
152 917
153 299
192 316
192 873
152 316
153 508
153 510
153 517
153 636
153 151
ISO 693
153 304
147 776
153 151
153 192
153 194
153 192
171 403
153 170
s»*i«ct ^ fiK
Piycbomotor tests
-Analyai* 398
Paychothertpy
••P*ychological tactort; 395
PuMic health
--Praaervation 404
Pulae cocnmunication *y*-
lem*
--Mathematical aaalyai* 421
Pulae generator*
•-Analysis 430
--Devekipmeni 430
Pulae undulation
coding 430
Pulae ayatem theory 421
Pulae tranamitters
--Design 430
Pyritea
--Electrical properties 471
QK-324 432
QIC-702 413
QRC-29 4H
Quantimi mcchanica
--Theory
Quantum nature
Quaru cryauls
--Aglnj
--Friction
--Temperature factors
Quaru resonators
--Fretjuency ahlfi
Radar display systems
--Visibility
Radar display systems
(Airborne)
--Performance
Radar duplexers
--Development
R^dar echo areas
--Matlienatical analyau
--Theory
Radar equipment
--Development
Radar mapping
-■Applications
Radar receivers
-Design
Radar acanning
--Equipment
Radar signals
--Detection
--Processing
Radar tracking ayatema
-Applications
Radial ihruai
Radiation belt
Radio aatronomy
--Inatrumenution
Radio interference
- •Measurement
Radio navigation aystems
(Airborne)
--Equipment
Radio relay system*
--Etjulpment
Radio tr*n*mia*ion
--Meteorological factor*
Radio tranamitter*
(Shipborne)
-Development
Radio wavea
--Propagation
--Scattering
Radiofrequency amplifier*
-Teat results
Radiofrequency attenuatora
--Calibration
4C3
473
425
430
469
430
430
431
430
429
476
414
455
427
428
430
491
428
428
438
439
392
428
429
392
433
430
421
475
434
414
415
432
434
423
-T\eai reoults
423
Radiofrequency filters
--Design 435
RadioTrequency oacillators
-CUIibration 424
-Test results 424
Radlofrequency pulses
--Detecuoa 428
153 4S4
I50 7fl»
ISO TV
153 084
153 008
153 OM
ISO 321
ISOtM
ISOM
ISOtN
147 988
153 Ta
171 M
ISOOIt
171474
l»Oti
1S0 8M
143 sn
171 318
153 2J»
1S3M
152 835
130 071
152 810
1SS3M
153 tn
153 TU
191918
153 217
153 2B
153 218
153 on
1»722
153 22S
152 714
152 871
190712
171 3M
152 «W
1»7M
1S07I8-I
ISOTIW
ISO on
161 983
153 W
ISO TIM
171 2M
171 as
171 ai
17104
171 22S
171111
153 Ml
171142
171 Ml
152 W
Ml«« r!E
fgntm^cti contamination
.(Jowianneasure* 404
426
422
413
410
41U
441
427
Biaipnent
(Alrboroe)
dutribution
gdeaatth compounds
..QHaiical reactiona
-SMMIity
gailaaa (Military)
■ Arctic regions
MF-3
laacnirs
-Equipment
Mcnutlog
-Piydiotogical factors
Ifdury serodytumics
lUfrsctory materials
-Appllcationa
■CaaOag
■Europe
-Ifeaae atudles
--ihyalcal properties
--Tbennal properties
-Vapor pressure
laUaMUty
— Dnermination
■-Sialiatical analysis
Baoflraaan
■ -Temperature factors
IkDdlun compounda
(Organic)
• ■Spectra
iKiiiaaa surfaces
locket motora
-■ftrtormance
-Teat methoda
Rockei oxxli.«rs
■-Teat methoda
locket propellanta
--Coabuaiion
—Development
-ttibillty
laOkai propelled sleds
•■Acrtxlynamic character
Mica
"Afpbca.ona
■•Ptrfcrmance
locfeM impulsion
--Ihaory
463
453
451
397
409
4SU
447
443
448
442
443
442
443
418
443
442
trajectoriea
Mathamatical analysis 439
aphy
-hraaliea
-Daaign
-Location
-MaMrula
SsUstry glanda
■■lhy*lok>gy
Sahaooalla
J (Siaiiatlcs)
Sadalck panels
--Itat inethoda
Stl^lres
"Prtalon
SaieUlie ferry
436
436
402
416
417
417
418
399
403
479
418
469
435
Satellite vehicle research 435
SaMUle vehicle trajeciunea
--Aaalysm 439
"OotenBination 436
438
440
--Itatlatlcal analysis 439
"Iheoretical corrections 435
(■iUits vehicles 439
"••Uograptoy 436
-CooUag 438
n Number
161 371-10
153 231
171 416
190 060
153 157
153 157
193 912
193 950
153 951
150 708
393
153 329
417
171 372
455
152 620
446
171 400
467
153 683
498
151098
446
161 233
447
171 391
445
171 413
445
171 390
445
171 413
153 357
150 729
153 545
147 776
153 433
154 410
154 411
153 286
193 948
153 949
153 441
153 493
153 181
193 493
192 790
193 404
153 290
150 719
153 441
153 388
153 182
153 182
153 522
171 370
171 369
171 369
193 1T8
153 302
153 513
171 478
171 408
171 474
152 320
152 321
153 408
150 702
190 070
130 724
153 220
153 492
153 218
153 219
153 774
153 055
153 182
171 363
Satellite vehicles (con. )
- -Detection
--Plight pattia
--Heat iranaier
--Motion
-Ternperature
--Tracking
Scieaufic peraoonel
--Attitudea
•Psychological factors
- -Selection
Scientific reporu
--Bibliography
--Coding
--Processing
Scientific research
Scintillation counters
- -Applications
Seadac
Seakeeping
Sedimentation
--Physical properties
Saiamic waves
--Analysis
■ -Sources
Seiamograplia
- -Applicaiiooa
Selenium
- -Bibliography
Semiconductor*
--Bibliography
--Caulytic properties
--Crysul structure
--Electrical properties
Pa|e
422
435
438
436
439
438
438
393
393
393
393
479
479
477
480
463
463
440
440
413
411
411
462
391
472
472
469
421
469
475
470
432
469
--bnpurmea
--Mathematical analysis
-Tempersture (sciors
Servomechanisms
--Applicstljoa
SC-21 V generator
Shaped charge liners
--Performance
Sheets
- -Heat treatmeni
--Hypersonic character-
.„iic8 497
-Laminar boundary Layer 495
Ship hulls
-Design 441
--Structursl analysis 440
Ships
•Blast effects 441
•Design 440
--fcrformance 440
Shock tubes
--Applications 439
Shock waves
- Chemical effects 446
Shock waves
•Measurement 474
--Hiysical effects 408
--Propagation 476
-Properties 466
--Thermal effecu 454
Shoes
--Clesnlng 464
Signal generators
-Calibration 422
-Teat reaulu
Signal generators (RF)
- Calibration
--Test results
Silica gels
-Surface properties
Silicon
- -Bibliography
- Impurities
Silicon carbidea
--nuse studies
Silver chloride crystals
-Deformation
Silver electrtKies
- -Electrical properties
I-ll
424
422
424
424
424
410
391
470
447
472
407
n Number
193 494
192 320
152 321
153 952
153 182
150 702
153 952
153 220
152 686
152 686
152 686
153 440
152 978
171 478
153 633
171 316
150 708
153 171
192 '«9
192 689
147 311
193 422
153 422
193 395
OTS SB-438
OTSSB-435
153 147
153 552
153 001
171 406
171 377
147 120
193 169
171 187
Subject
f!E
193 315
153 092
153 632
153 953
149 520
153 953
152 689
152 829
153 173
153 466
149 731
148 525
153 073
149 676
153 516
171 241
171 243
171 244
171 241
171 243
171 244
171 246
171 246
154 295
OTS SB- 437
147 120
171 365
-153 564
152 871
Silver oxides
- -Electrochemlotry
Single crystala
- -Ojlor
--Creep
Sky
--Radiation
--Temperattire
Sleeping baga
--Teat reaulu
Sao«
--Traffieability
Soov drags
Snoar roada
--Development
Snow ahelter*
Social commuaicadon
- - F^ychological factors
--Test methoda
Sodium cloud
Solar batteriea
--Development
--Sundards
Solar flares
--Electromagnetic effecu 415
Solar furnacea
--Design
Solar noise dau
--Analysis
Solids
--Elaaticity
--Mattiematlcal aaalyaia
--Wave tranamlaaion
407
470
446
416
416
465
420
420
420
420
395
394
414
429
429
474
392
--X-ray analyaia
Sonar personnel
--i^rformaacc
465
465
453
475
476
471
395
Sonar algnals
•Detection 395
Sound
--Profiagation 475
- - Psychologica I eflecu 396
Sounding rockeu
- -Equipment 434
Space charges
-Electromagnetic effecu 430
Space flight
- -Simulation
Space perception
--Analysis
-■Test methoda
Spaceships
- -Enuiptnent
--Materials
Spectrophotometers
- -Appllcationa
Spectroscopy
--Appllcationa
Speech
--Intelligibility
Speech transmiaalon
--Intelligibility
Spheres
-■Preparation
Splrocheto^s
- -Bibliography
Sponing chargea
- -Materiala
Squid
Suioless steel
--Fracture
■Welding
Sunding wave ratioe
--Measurement
439
435
394
392
441
437
409
465
478
492
404
437
4i0
445
424
Sutisiical analyai*
- -Application* 449
-Theory 430
Steel
-Hfcat treatment 459
--Tewile propertle* 459
Step, scanner 463
Storage tubes
--Development 452
Strategic ituterUla 444
Stress analysis 460
--Applications 453
-Theory 452
Stress concentration factora461
Streas strain curves 462
Strip mapping 427
192171
147 174
171 398
193 334
153 334
153 510
171 375
171 375
171 375
153 517
153 168
153 387
150 721
153 645
153 645
153 197
153 465
152 872
154 291
154 291
152 904
147 400
148 52«
152 982
153 126
153 141
153 141
147 400
171 403
153 442
153 504
153 055
153 408
153 424
193 470
171 418
151 101
153 491
150 922
193 430
153 495
ISO 706
150 062
150 097
153 173
153 167
153 263
171233
171 234
171 235
153 389
150 711
171 996
171 396
150 708
152 928
147 534
153 077
153 386
147 401
171 410
161 896
153 396
S«i>|cct
Pie
ra Number
StractHral ate 11a
"SusMaa
463
153 734
STU-l.
«31
153 221
•-«— laaacu
441
149 520
-Proputaioa
462
153 «77
Sutftir compounda (Orga
lie)
--Oeoucal reactuna
409
153 451
St^raooic alrfnla
•-Drag
454
150 069
-SlabiUty
454
150 069
Supvraoaic flow
-Mathemaucal analyi
la 4S«
154 403
"TaMea
454
153-477
Siynaanic no<:zlea
--Aoalyaia
4S7
153 378
Surfacea <Maitematic4
--Thaory
4S0
153 433
Smtv***!
--Arctic regiona
»7
153 524
441
153 540
— DlMary lactora
397
153 524
••tlcJ»a(BF)
--Teat reaulu
425
150 698
SartlcUac circuin
- -Applicariona
451
153 002
--Throry
425
153 579
Syachroirona
--Dealfn
462
152 866
-UWlograptoy
477
152 914
477
153 129
TamaMn
-OMlaf
458
151 098
TvgM ncofBiuoa
— ViMMl (acton
395
147 533
Taryeu
--DetaciKMi
428
153 225
43t
143 302
TiktroaU ItOA generati
r 422
171 241
Talenia*r aystema
--E^uipnieni
4J0
150 707
434
153 235
Talemetaring recaiwri
- - E ^uipment
427
153 990
- -Oparation
427
153 951
Telluridea
"Blactncal profcrtk
a 471
ISO 323
Telhirtuin
- -Bibllogriphy
391
OTSSa-438
TEMdioctr
425
153 579
Terreacnai magaeuam
--Aaalyaia
392
130 722
TarritorUl waicrs
479
153 121
Taataeta
--Daatfn
433
150712
--Devcloimieat
420
150 703
Teat vehicles
-Teat (aciUtiea
419
152 716
Twia
--Deal«i
477
152 927
Taxdtaa
- -Ubllofraphy
448
OTSS8-440
- -DnarioraOaa
448
171 417
TheodoUtea
--Appiicationa
411
1S0 7<»
Thermal radiauon
474
154 293
- -DMarminaiian
412
153 324
-->«— aynmrni
474
161 228
Tharaal atreases
-Aaalyaia
422
171 416
Tbemuoiuc enuaaioa
lli^fiiinl anal]
■la 467
153 603
--Theory
TWanima
--Optical propertlea
Thyroid glanda
--nquotoor
--Cllwatlr (acton
Time mark generator
Time aeries
--ApphcaiioM
TUian
Sut^ect
Tlmiag circulia
- -OavclapniMN
ftN«anber
SuHect
Page
407
473
469
403
422
430
437
171 376
150 688
153 094
153 515
153 372
171 241
190714
153 478
--Operation
Titanium
-Ptatiag
Tliaouun alloya
- - Porgmg
--Mechanical properties
-'Meullurgical analysis
TtKpliu matncea
Topology
--Tl»ory
Torque
- -Maihematical analysis
--Measurement
Tracers (Ordnance)
--Applicaiioi.a
Track chamber
Tncking
--Paychologlcal (actors
Tracka (Aerodynamics)
--Design
Tnlning devices
--Human engineering
- -Simulaiion
Tnoaducers
- -Bibliography
Trana(ormaiians
(Mathemallca)
--Theory
Tranalaiors
- - Applicauooa
Tranamission lines
--Mathematical analyaia
Tranaparem rocket motor
Traaoporacion
-Scheduling
Traumatic shock
- -Couniermeaaures
Traveling wave tuiiea
--Developmeat
Tuogaien
--Caating
--Oienucal raactlcna
Tunpten broiu«a
Tungaien oxidaa
-Caulytic properties
Turbine blades
-Drag
Turbojet engines
-De- icing gyaiema
Turbulent boundary layer
--Heal tranaler
--Shear sireaaea
U-2
Ultra high fre<|uency com-
municatioa systems
--fcrlormance
UUraaonics
--Applicatiooa
- - liMtrumeniaiion
Ultraviolet radiation
--Oiemical e((ecta
Underground aiructures
- -Blaat effecta
Undenvater communication
aya terns
--Development
Underwater axploaions
-BUai
Universal slgebrs
Upper atmoaphere
- - Inatrumentation
- -Spectrographic analyais 414
Ureikane polymers
-■Appltcattona
Vacuum syatems
-Testing equipment
Vsnable reaiators
--Calibration
Vehiclea
--Aerodynamic character -
latica 455
437
153 478
Vehicles (con.)
430
153 084
- -Aarodynamica ciMr«CMr-
431
153 221
ladca
455
171 «
431
153 221
Veatilatl jo ducta
Dealgn
440
154 4H
445
153 223
Vertical take-o« pUnes
■ ■ Landing
417
153 ON
499
151 100
-Ufl
418
152 nj
461
171 394
--Performance
4W
130 741
460
171 412
Very high frequency com-
449
153 305
municatton lyatema
- Teat facllliiea
432
153 W
450
153 685
/ibratloo
451
153 684
--Mathematical analyais
453
484
1537)1
153 M
453
153 734
Vigilance performance
395
153111
431
150 319
Vlaual perception
-Meteorological faaon
413
151 M
436
150 068
-Teat methoda
392
153 411
435
153 408
Voice communication systema
--Coding
452
153 4«
395
147 533
-•Ei|ulpment
Voice dhta proceaaing
431
153 W
435
153 408
syaiems
Vortlcn
452
151416
436
171 419
--Madiemaiical analyais
457
153 4W
418
171 404
-Moiloa
457
153 4W
Voarel dlacriminaiion
478
153 4SI
391
153 505
Water
--Purification
440
153 Mf
153 3(1
450
153 412
Water activated batteries
-Development
426
153 91
433
190 712
Water aupplies
-' Radioactivity
404
161 VXVk
433
147 243
Water vapor
443
153 286
-■nkxolyaia
Water waves
406
ISO MO
447
153 078
■ -Mathematical analyaia
458
153 l»
--n^rsical edecta
413
147 311
153 193
-•Reaisunce
458
147 IS
--Velocity
458
147 IS
425
171 414
Waveguide slots
--Impedance
429
152 m
458
151 098
Waveguldea
408
171 373
--Electromagnetic
472
153 147
properties
427
152 717
--Exciution
429
152 M3
472
153 147
- -Mathematical analysis
434
153 S5J
- -Wave transmission
425
153 417
443
152 525
Wear mechanics
Weather forecasting
469
171474
416
153 289
--Errors
411
153 IM
-•Siatiaiical analysis
413
IS3W
474
153 105
Weather autiona
456
150 982
- - Location
412
153 232
464
171 361
171 362
Wedyea
- -Superaonlc character-
latlca
454
ISOflM
Welded Joints
455
152 620
- -Test resulu
445
153 M
West Ford
439
153 ai
445
171 186
153 214
428
153 697
Wiener Hop< method
Wind
449
147 111
448
. 171 417
--Determination
413
153 407
--Measurement
411
I5O70J
440
154 406
Wind tunnels
1
•-Applicationa
477
153 4U
--Equipment
454
ISO Of?
431
153 954
WlBga
--Lm
41S
152173
441
149 520
Wire
450
153 438
--Tenaile propertiea
444
161130
WronakUo
450
153 711
434
153 442
Wullenweber antenna
425
ISO**
s 414
150 721
Zinc oiudes
-X-ray analyais
469
153 381
443
153 286
419
152 319
,i '
»'i-
422
171 245
».
171 387
NUMBER INDEX
1-12
AAL 7-7951
»M. 7-7951, R-1
^lH)t0l-000iR-l
23:12-1301-0003.
t-l, MrX* 2
UiL-TH-Vy-i
AAL-TN-56-4
AAL-TN-S6-5
AAL-TN-56-6
AiU,-TN-i6-7
aAL-TN-56-8
AAL-TT(-56-l0
AAL-T>I-S6-11
AAL-TN-56-12
AAL-TT4-»-l3
AAL-TN-S6-I4
AAt-TN-ifc-lS
/kAL-TN-SO-lft
/UU,-TN-S6-I7
AAL-TN-S6-H
AAL-TN-i6-l9
AAL-TN-S6-20
AAL-TN-56-21
/UU.-TN-i6-22
AAL-TN-S6-23
AAL-TN-S6-24
AAL-TN-56-25
AAL-TN-i6-26
AAL'™-S6-27
AAL-TN-36-28
a*L-TX-S6-29
AAL-TN-J6-30
AAL-TN-56-31
AAL-TN-S6-32
AAi,-TN-S6-33
AAL-TN-S6-34
AAL-TN-56-36
A4L-TN-J6-37
AA1.-TN-S6-38
iUL-TN-56-39
AiU.-TN-$7-4
AAL-TN-57-5
AiU.-TN-57-l2
AAL-TN-S7-36
AAL-'Ill-S7-5
AAL-T«-57-6
AAL-TH-57-7
AAL-Tll-57-8
AAL-TR-57-12
AAL-Tll-57-14
AAL-TR-57-27
AAL-Tll-57-32
AAL-TR-57-36
AM.-TII-57-37
AD-49 219
AO-I10M)8
AD- 120 462
Al>-iat06
40-151041
A0-1S1546
40- ISO 775
Al>-»S34S
AO-107 45()
AD-»t328
A0-110ll«
40-110 143
40-ll>496
AO-IU 406
40-111 1*4
40-113 643
A0-li7 143
40-217 321
40-217 543
40-117 980
40-111013
40-111 970
4D-li9 3l4
40-219 f46L
40-120 282
40-12D34S
40-223 106
40-223 462
40-126 373
40-127179
40-127 709
«0-a402
40-129 180
40-nO 162 •
40-230 383
40-131347
40-131388
40-131464
40-131 465
40-131493
40-231 175
40-131895
40-131041
40-231064
«0-»419
40-S467
416
399
394
393
403
4«1
«S
411
403
464
430
403
440
478
478
402
441
J97
402
400
400
400
400
400
401
401
401
401
401
401
401
401
401
441
402
399
403
ym
397
440
392
402
40B
402
399
402
478
397
411
398
397
448
41*
473
41S
4*2
392
4*4
442
42S
4M
413
4*3
490
454
434
473
«1
433
410
411
431
433
431
4*2
437
413
4M
4*7
433
414
4*3
431
'*wri»er
AD- 232 646
AD-232 6S6
AD-232 657
AD- 232 663
AD-232 746
AD-232 752
AD-232 897
AD-232 924
AD-233 061
AD- 233 132
AD- 233 187
AD- 233 212
AD- 233 222
AD-233 243
AD- 233 406
AD-233 434
AD-233 501
AD-233 505
AD-233 608
AD-233 687
AO-233 722
AD-233 862
AD-233 898
AD- 234 086
AD- 234 087
AD-234 112
AD-234 179
AD-234 191
AD-234 250
AD-234 380
AD-234 463
AD-234 481
AD-234 659
AO-234 691
AD-234 693
AD-234 795
AD-234 865
AD-234 866
AD-234 894
AD-234 938
AD-234 957
AD-235 010
AD-2S5 058
AD-235 064
AD- 235 065
AD- 235 066
AD- 235 210
AD- 235 391
AD- 235 447
AD-235 581
AD- 235 651
AD-235 654
AD-235 774
AD-235 848
AD- 235 860
AD- 236 193
AD- 236 205
AD- 236 206
AD- 236 215
AD- 236 263
AD-236 323
AD- 236 458
AD-236 500
AD-236 727
AD-236 728
AD-236 811
AD- 237 062
AD-237 069
AD-2S7 414
AD-2S7 445
AD-237 728
AD-237 754
AD-237 755
AD-237 968
AD-238 769
AD-238 997
AD-239 399
AD- 240 047
AD-240 310
AD-240 666
AD- 240 694
AD- 240 807
AD- 240 814
AD- 241 227
AD-241 588
AD-241 862
AD-241 909
AD-241 995
AD- 242 555
AD-242 802
AD-243 269
AD-243 375
AD-243 454
AD-243 497
AD-243 547
AD-243 621
AD-243 ri
AD-243 898
AD-243 967
AD-243 979
AD- 244 262
AD- 244 270
AO-244 324
Paae
392
442
475
400
456
458
472
475
436
462
476
410
463
475
405
414
463
477
468
479
418
449
407
395
395
472
433
433
453
442
477
413
460
393
398
408
454
436
436
451
470
422
454
451
451
452
419
453
392
450
432
463
466
448
474
470
449
410
458
458
470
471
453
475
452
413
409
470
463
395
444
3<*
396
394
392
476
447
429
429
457
464
455
396
439
412
399
417
444
426
412
429
429
406
441
460
427
435
403
436
471
417
447
412
Mumlier
AD- 244 443
AD- 244 482
AD- 244 494, superseded
AD^244 549
AD- 244 586
AD- 244 607
AD-244 642
AD- 244 736
AD-244 841
AD-244 957
AD-245 090
AD-245 118
AD- 245 156
AD-245 202
AD-245 245
AD-245 325
AD-245 335
AD-245 398
AD-245 443
AD-245 484
AD-245 540
AD-245 549
AD-245 572
AD-245 613
AD-245 663
AD-245 803
AD-245 809
AD-245 853
AD-245 909
AD-245 926
AD-245 968
AD-246 003
AD- 246 048 ,
AD- 246 075
AD-245 076
AD-246 081
AD-246 129
AD-246 224
AD-246 254
AD-246 256
AD-246 306
AD-246 308
AD-246 315
AD-246 334 .
AD-246 353 " -.
AD-246 377
AD-246 410
AD-246 441
AD-246 449
AD-246 496
AD-246 505
AD-246 507
AD-246 510
AD-246 513 r
AD-246 519
AD-246 540
AD-246 559
AD-246 589
AD-246 591
AD-246 621
AD-246 622
AD-246 631
AD-246 643
AD-246 651
AD-246 653
AD-246 716
AD-246 741
AD-246 777
AD-246 778
AD-246 779
AD-246 781
AD-246 782
AD-246 797
AD-246 799
AD-246 801
AD-246 835
AD-246 887
AD-246 896
AD-246 963
AD-246 976
AD-246 977
AD-246 989
AD-247 034
AD-24Z 075
AD-247 121
AD-247 170
AD-247 226
AD-247 227
AD-247 231
AD-247 233
AD-247 241
AD-247 242
AD-247 243
AD-247 244
AD-247 271
AD-247 285
AD-247 290
AD-247 315
AD-247 353
AD-247 381
AD-247 424
AD-247 425
AD-247 471
P— e Numlfer fj/^
406 AD-247 550 422
443 AD-247 577 440
439 AD-247 590 4SS
431 AD-247 5«3 430
459^ AD-247 898 436
432 AD-247 913 «96
413 AEDC-TN-58-9 454
4» AERDL-1626 TR 447
40» AEJUX-1643-TR 460
414 AF-TSEAC4-4461-5-1 417
«•» AFBNC-7-40S9 434
«W AFCCOD-TN-60-34 435
¥S AFCCDO-TN-60-39 478
Sji AFCCD-TN-60-lOBO 452
^ AFCRC-TN-58-4i6 413
«| AFCRC-TR-S8-233 415
<C AFCRC-TR-59-222 413
«H AFCRCTR-59-353 475
«» AFCRC-TR-59-405 414
451 AFCRL-TN-60-261 413
fl? APCRL-TN-60-467 413
*W AFCRL-TN-60-497 463
4*» AFCRL-TN-6O-630 467 j,
471 AFCRL-TN-60-631 411
4E AFCRL-TN-60-632 462
ttj AFCRL-TN-60-649 476
47» AFCRL-TN-60-670 415
4M AFCRL-TN-60-674 415
477 AFCRL-TN-60-685 434
4B AFCRL-TN-60-691 415
4i7 AFCRL-TN-6O-800 473
430 AFCRL-TN-60-815 468
415 AFCRL-TN-60-963 451
421 AFCRL-TN-60-967 476
431 AFCRL-TN-60-970 450
441 AFCRL-TN-60-991 472
401 AFCRL-TN-60-llOB 426
473 AFCRL-TN-60-1114 452
4W AFCRL TN-60-1115 422
430 AFCRL-TN-60-1117 434
417 AFCRL-TN-60-1120 430
4IS AFCRL-TN-60-1121 427
~ AFCRL-TN-60-1127 425
AFCRL-TN-60-1131 473
AFCRL-TN-60-1132 440
AFCRL-TN-60-1134 432
AFCRL-TN-60-1155 467
AFCRL-TR-60-168 408
AFCRL-TR-60-170 452
AFCRL -TF -60-205 411
AFCRL-TR -60-278 467
AFCRL-TR-60-352 452
AFCRL TR -60- 353 427
AFCRL-TR-60-364 420
AFCRL-TR-60-406 412
AFCRL-TR-60-415 440
AFCRL TR-60-423 467
AFMX;-T>J-60-13 474
AFVOC-TN-60-14 435
AFMDC-TR-59-4 442
AFfcCC-TR-60-21 399
AFhDC-TR-60-23 419
AFOBR-TN-58-9S2 392
AFOSR-TN-58-1077 464
AFaSR-TN-59-85 46*
AFOSR-TN-59-224 463
AFCBR-TN-59-746 408
AFOSR-TN-60-164 431
AFOSR-TN-60-334 408
AF(3SR-TN-60-484 436
AF06R-TN-60-707 471
AF(»R-TN-60-846 456
AF06R-TN-6O-854 409
AF06R-TN-60-878 467
AFOKR-TN-60-930 472
AF(36R-TN-60-956 457
AFCBR-TN-60-960 466
AFOSR-TN-60-960. pl.2 425
AFOSF-TN-60-962 462
AFOSR-TN-60-991 409
AFO6R-TN-6O-1035 450
AF06R-TN-60-I064 450
AFOSR-TN-60-1094 474
AFOSR-TN-60-1100 455
AF08R-TN-60-1103 427
AF08R-TN-60-1117 470
AF(»R-TN-60-1169 421
AF06R-TN-6O-1171 426
AFaSR-TN-60-1195 456
AF(BR-TN-60-12l3 490
AFOBR-TN-60-1227 4S7
AFaSR-TN-60-l241 410
AFO»-TN-60-1243 4S0
AF(Wl-TN-60-1244 4»
AF06R-TN-60-I245 473
AF(BR-TN-60-l26l 43*
AF06R-TN-60-I266 490
AFC6R-TN-6O-1270 406
AFOSR-TN-60-1337 4-58
AFOSR-TN-60-1342 499
AFOSIl-TN-60-1346 4»
AFOSR-TN-60-13S2 «*9
AF(38R-TN-60'1355 394
1-13
NuBta
AF06R-TN-60-1362 411
AF06ll-TN-6O-13fc5 406
AF08R-TN-60-1371 472
AFC)SR-TN-60-I373 467
AFaBR-TN-60-13»3 449
AF06R-TN-6O-1402 484
AFCBR-TN-60-1403 447
AFCBR-TN-60-1406 404
AF08R-TN-60-1407 449
AFORR-TR-57-20 473
APC8R-TR-59-»4 456
AF06R-TR 60-2 457
AF06R-TR 60-99 443
AFaBR-TR-60-111 471
AFCBR-TR-60-126 407
AFQSR-TR-60-129 394
AFOSR-TR 60-131 46«
AFC8R-TR-60-136 ! 457
AFOSR-TR -60- 160 ' 446
AP06R-TR-60-169 449
AFSAM-60-20 i 399
AFSAM-60-60 404
APSAM-60-85 399
AFSAM-60-r 400
AU,-7601-H-1 416
Am-244-58-FR-irT 420
Am-290-60-FR-225 392
aMC-TR-60-7-667* 445
AkaiO-PM-U 413
aOHEL-TM- 17-60 398
aGHEL-TM- 18-60 392
ARA-720 i 436
ARCRL-TR-60-412 411
ARF-21S2-10 460
ARL-TN-60-II9 I 449
ARL-TN-60-149 456
ARL-TR-60-i90 j 419
ARL-TR-60-313 435
ARL-TR-60-316 471
ARL-TR-60-319 435
ARL-TR-60-321 459
ARL-TR-60-324 478
ARfA-SFS-7 436
ARPA-SI>S-8 422
ARfA-SFS-19 422
ASROL-2041 421
ASIUX-2043 421
ASROL-2047 411
ASRDL-2049 444
ASRDL-20r7 475
ASRDL-2099 421
ASROL-2114 421
ASRIX-2nS 451
ASROL-2U1 421
ATl-114 680 407
AT1-14S 927 465
ATI- 152 755 417
ATl-153 158 475
ATl-159 367 410
ATI- 179 543 473
ATl-210 349 474
A«co RR-42 4M
■■4-780 422
BN-197 401
BR-NYU-34 417
BRL-1093 422
BRL-1095 454
BRL-U14 436
BRL-1116 442
BRL-Ml-1237 436
BRL-M(-1242 436
BRI.-lkK-1245 454
BRL-MR-1300 466
BRL-TN-869 440
BRL-TN-1304 436
BRL-TN-1354 422
Bul«T* TB-60-3 394
CX;L-9« 407
C<«irt-27 417
CKOLR-SOtS 396
CU-1-60 453
CU-15-60 449
CU-l-6O-C»4R-266(0« 476
CU-1-60-CINR -266(34)! 476
CVA AiTEOR- 13081 , 419
DaCL-124 443
OASA-S29 4«4
DAaA-531 4*4
DASA-730 440
OAaA-1052 462
DASA-1190 465
L»4IC-139 458
OMIC-141 459
DIMiC-142 I 437
0MK:-144 461
OMC-M-78 474
dmic-m-79 «sa
omc-u-m
DUIC-M-»3
OOFL-TR-&57 437
DOFL-TR-874 425
OOI'L-TR-875 437
OOFL-TR-SiS 469
L)OPL-TR-»95 437
COPL-TR-898 391
001-7-8120 468
CrrMI-1353 440
Nuntier
rw
DTKB-C-555
EE-433
E£-461
EM-161
EP-123
ERF-RM-14
ESL UIT-7976-60-5
ESLM1T-8494-R-1
F-TR-2264-1A-1
FAAT«»k D-2-5213
FDRC-60-4
Fl 1-A3049-11
FRL-TR-17
FRL-TR-18
FRL-TR-21
FRL-TR-22
FRL-TR-25
CM-TVl-162
CRD CRP-69
CTEL TR-eO-204.6
cwu-T-u3/eo
HH-60-15
HSR-RR-60/l-»m
1CP-12S2. Mipeneded
lER-18-7
lER-60-29e
lER-eO-303
lER- 108-4
IER-150-2
lRL-142
I PL M-4-29
PL M-4-43
PLPR-20-229
PL PR-20-248
PL PR -20- 274
PL PR-20-294
PL R-20-72
LIR TR-136
LIRTR-148
LIR TR- 149
LIR TR- 150
LL-3C-0OO2
LL-21C-0011
LL-21G-0O19. auperaeded
LL-21C-0027
LL-21C-0028
LL-22G-0O39
LL-34C-0005
LL-46C-0008
LL-47G-00O6
LL-47C-0007
LL-47C-0010
LL-53C-0O42
LL-84C-0013
LL-TR-234
LMSD-4307
LMSO-288 184
LMSO-288 264
LMSD-703 013
LMSD-703 036
LMSD-703 045
LMSO-703 047
LockSB-M>-2S
LockSB-60-29
LockSRB-«0-3
MEDeW-RS-4-59
MEDe*-RS-5-59
MEDE*-RS-6-60
ME WO- 1033
ML-732
ML- 747
ML- 755
MRUORO)-71
MOOP-1851, lupCTMded
MUPTR-200
NAMC-ACEL-439
NATTS-ATL-47
NAVORO-2031
NAVWEPS-5974
NAVWEPS-7043
NAVWc.PS-7563
NAV*EPS-75<>4
NAVWEPS- 7566
NAVWEPS SSL -AC -05
NAVWEPS SSL-AF-21
NAVWcPS SSL-AG-47
NAVWEPS SSL-AC-48
NAVWEPS SSL-AG-51
NAVWEPS SSL-AZ-09
NAVWEPS SSL-GC-06
NAVWEPS SSL-HA-01
NAVWEPS SSL-HA-03
NAVWEPS SSL-HA-05
NAVWtiPS SSL- HA -06
NAVWEPS SSL-HA-07
NAVWEPS SSL-HF-04
NAVWEPS SSL- HF -05
NAVWEPS SSL-HF-06
NAVWEPS SSL -HF -07
NAVWEPS SSL-HV -02
NAVWEPS SSL HV -04
NAVWEPS SSL-HV -06
NAVWEPS SSL- NM -02
NAVWEPS SSL-NP-02
NAVVriPS iSL-NR-01
>ffiS-6062
NBS-TN-59
440
«S-TN-82
414
NBS-TN-85
392
NC8L-R-089
476
NCEL-R-109
465
NOU:-478
444
NOTS-701
451
NOTS-TA-7
451
NOTS-TP-2343
407
NOTS-TP-2434
430
NCrrS-TP-2458
456
NCrrS-TP-2519
442
NarS-TP-2531
437
NOTSTP-2532
438
NOTS TP-2533
438
NOTSTP-2536
433
NOTS TP- 2582
43S
NRCC MA -243
434
NRCC MB- 225
467
NRL-5413
408
NRL-5532
442
NRL-5545
417
NRL-5549
477
NRL-5555
422
NSF Y/9. 5/80
471
NSL-443
436
NSL-454
467
NSL-462
470
NSRDF ER-2.308
471
NWL-1724
41S
OORR60-2
427
OORR 1597: lOM
477
CORR-2125.6-M
448
OORR-2211.1-P
447
OSURF- 778-1
447
arAC-RR-28
438
OTSCTR-340, •
448
OTS SB-435
431
GTS SB- 437
470
OTSSB-438
470
OTSS8-440
470
OTS SB-445
415
PATR-1401. rev
455
PB 143 302
439
PB 146 924
439
PB 147 045
439
PB 147 120
431
PB 147 121
3*1
PB147 125
429
PB 147 173
43>
PB 147 174
438
PB 147 243
431
PB 147 244
471
PB 147 3U
431
PB 147 362
431
PB 147 400
4S3
PB 147 401
439
PB 147 533
439
PB 147 534
495
PB 147 759
439
PB 147 776
444
PB 147 778
«I7
PB 147 900
««4
PB 148 0O6
«I7
PB 148 0O7
ni
PB 148 018
403
PB 148 021
403
PB 148 496
4M
PB 148 525
436
PB 148 771
430
PB 149 296
473
PB 149 520
458
PB 149 648
463
PB 149 676
423
PB 149 731
467
PB 150 060
406
PB ISO 061
416
PB 150 062
4S6
PB 130 064
430
PB 150 066
443
PB 150 067
' 443
PB 150 068
443
PB 150 069
418
PB 150 070
422
PB 150 071
423
PB 150 075
422
PB 150 086-7
424
PB ISO 086-8
422
PB 130 086-9
422
PB ISO 097
424
PB ISO 319
423
PB 130 323
423
PB 150 656
423
PB ISO 688
423
PB ISO 689
423
PB ISO 690
424
PB 150 691
424
PB 150 692
423
PB ISO 693
424
PB1S0 694
424
PB ISO 695
424
PB ISO 697
424
PB 130 698
405
PB ISO 699
465
PB ISO 700
468
PB ISO 702
430
PB ISO 703
465
PB ISO 704
•uppl
4U
409
4M
430
430
4S6.
443
499
443
443
43D
^
4U
418
4M
477
441
&
441
431
409
414
436
474
456
441
479
477
4S0
439
468
415
461
472
472
391
391
448
460
438
431
471
410
470
449
458
470
470
433
433
413
453
475
452
395
444
470
409
399
463
396
396
394
408
392
476
394
465
441
410
454
408
413
451
404
4»
422
454
436
454
436
414
419
451
451
452
437
431
471
405
473
429
406
413
430
463
464
466
415
425
432
468
439
420
421
tluniber
PB 130 705
PB 150 706
PB 150 707
PB 130 708
PB 150 709
PB 150 710-1
PB 150 710-2
PB 150 711
PB 150 712
PB 150 713
PB 150 714
PB 150 715
PB 150 716
PB 150 718
PB 150 Tl*
PB 150 720
PB 150 721
PB 150 722
PB 150 723
PB 150 724
PB 150 725
PB ISO 742
PB 150 920
PB 150 921
PB 150<»22
PB 150 923
PB ISO 982
PB 151 098
PB ISI 100
PB 151 101
PB 151 103
PB 152 316
PB 152 319
PB 152 320
PB 152 321
PB 152 525
PB 152 588
PB 152 604
PB 152 608
PB 152 611
PB 152 620
PB 152 654
PB 152 682
PB 152 685
PB 152 686
PB 152 688
PB 152 689
PB 152 693
PB 152 716
PB 152 719
PB 152 727
PB 152 781
PB 152 790
PB 152 827
PB 152 829
PB 152 8X
PB 152 835
PB 152 836
PB 152 838
PB 152 844
PB 152 866
PB 152 871
PB 152 872
PB 152 873
PB 152 874
PB 152 876
PB 152 881
PB 152 904
PB 152 914
PB 152 917
PB 152 927
PB 152 928
PB 152 931
PB 152 974
PB 152 978
PB 152 982
PB 152 998
PB 153 001)
PB 153 001
PB 153 002
PB 153 004
PB 153 055
PB 153 061
PB 153 073
PB 153 074
PB 153 077
PB 153 078
PB 153 083
PB 153 084
PB 153 086
PB 153 092
PB 153093
PB 153094
PB 153 098
PB 153 099
PB 153 101
PB 153 104
PB 153 105
PB 153 106
PB 153 111
PB 153 119
PB 153 121
PB 153 126
PB 153 127
PB 153 128
PB 153 129
PB 153 131
411
4M
4S
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4a
434
434
4S
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444
43)
431
433
47S
442
431
414
m
413
43k
451
41*
417
4m
MA
401
434
431
451
437
461
431
414
433
433
443
471
4X1
4m
4m
433
4r
413
401
3W
446
440
42*
414
42«
427
47b
443
3N
431
441
47t
4U
437
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4tt
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411
4U
47t
3W
433
477
49
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432
467
4a
47»
471
431
421
421
431
431
431
413
444
473
440
447
417
4S
43»
433
41}
4M
473 •
444
427
434
474
434
411
433
419
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400
441
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4tl
1-14
B 153 136
B153 141
» 153 143
» 133145
« 153 147
B 153 148
« 153 151
mS3l53
ni33l56
n 153 157
» 153 159
n 153 161
n 133 162
n 133164
PI 153 165
n 153 166
n 153 167
nissi68
B 153 169
fl 133 170
n 133 171
P8lJ3i73
n 153174
n 153 175
Bi53l7l
n 133181
PI 133 182
PI 153 184
m53l»2
Pri53l93
PI 133 194
PI 153 197
PI 153 198
PI153 3D4
PI 153 205
Fl 133 206
n 133 215
n 153 216
PI 133 217
PI 133 218
PI 153 219
n 153 220
PI 153 221
PI 153 223
PI.I53 224
PI 153 225
n 153 227
PI 153 229
PI 153 231
PI 153 232
PI 153 235
PI 153 239
PI 133 240
PI |53 241
PI 153 242
PI 153 245
PI |53 261
PI i53 263
PI 153 265
(1153 281
PI 153 283
n 153 284
ni53 286
Fl 153 287
Fl 153 289
PI 153 290
PI 153 291
PI 153 299
PI 153 301
PI 153 302
PI 153 303
PI 153 304
Fl 133 305
Fl 133 306
Fl 153 308
PI 133 309
PI 133 310
PI 153 314
PI 133 315
PI 153 316
1153 321
Fl 153 322
Fl 153 323
Fl 153 324
Fl 153 329
PI 133 334
Fl 153 335
Fl 133 347
Fl 133 334
Fl 133 356
1153 357
Fl 153 358
ni33 3S9
n 133 340
Fl 133 361
Fl 133 363
Fl 133 364
ni33 36S
1133 366
R1SS367
113} J»9
niun
1 153 372
1133 373
1133 378
llSSJIS
P««e
414
468
395
472
442
472
479
462
467
405
410
458
436
458
400
392
475
460
395
432
466
463
4a
396
422
418
443
436
456
403
403
404
415
441
411
432
492
406
406
423
439
438
438
431
445
421
43i;
430
429
426
413
434
412
432
426
435
439
497
449
406
466
415
471
443
394
41«r
443
467
447
408
399
400
449
449
4ir
457
440
394
394
393
412
393
416
399
399
406
410
493
4S0
450
478
452
402
402
399
402
478
397
411
398
397
497
449
Number
PB 153 386
PB 153 388
PB 153 392
PB 153 393
PB 153 394
PB 153 395
PB 153 396
PB 153 397
PB 153 400
PB 153 404
PB 153 407
PB 153 408
PB 153 404
PB 153412
PB 153 414
PB 153417
PB 153 420
PB 153 421
PB 1 53 422
PB 153 424
PB 153 425
PB 153 426
PB 153 430
PB 1 53 433
PB 153 435
PB 153 437
PB 153 438
PB 153 439
PB 153 440
PB 153 441
PB 153 442
PB 1 53 446
PB 153 451
PB 153 454
PB 1 53 455
PB 153 458
PB 153 459
PB 153 465
PB 153 466
PB 153 468
PB 153 469
PB 153 470
PB 153 477
PB 153 478
PB 153 480
PB 153 481
PB 153 484
PB 153 492
PB 153 493
PB 153 494
PB 153 498
PB 153 SOI
PB 153 504
PB 1 53 305
PB 153 507
PB 153 508
PB 153 509
PB 153 510
PB 153 511
PB 153 512
PB 153 513
PB 153 514
PB 153 515
PB 153 516
PB 153 517
PB 153 518
PB 153 519
PB 153 520
PB 153 521
PB 1 53 522
PB 1 53 523
PB 153 524
PB 153 525
PB 153 526
PB 153 527
PB 153 528
PB 153 529
PB 153 530
PB 153 531
PB 153 532
PB 153 533
PB 1 53 534
PB 153 535
PB 1 53 536
PB 153 537
PB 153 538
PB 153 539
PB 153 540
PB 153 541
PB 153 542
PB 153 543
PB 1 53 544
PB 153 545
PB 153 546
PB 153 547
PB 153 548
PB 153 552
PB 153 555
PB 153 560
PB 153 564
PB 153 579
PB ;53 607
PB 153 609
PB 1 53 632
Ptf 153 633
PBil53 634
P^; 1 53 636
Number
493
439
467
467
411
4t3
427
467
431
4I3
4"^
399
450
4S0
425
456
428
411
394
43b
472
478
450
417
412
429
446
393
442
434
434
409
430
452
450
457
474
474
397
398
392
494
437
411
413
415
440
442
422
432
454
430
391
403
464
464
465
399
441
403
411
403
464
420
403
440
478
478
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PB 171 407 454
PB 171 408 418
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PB 171 410 461
PB 171 411 459
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PB 171 414 425
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PB 171 416 422
PB 171 417 448
PB 171 418 441
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PB 171 420 432
PB 171 474 469
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PCE-R-7697A 432
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PtBAL-463 457
PlBAL-621 456
PlBAL-625 439
PlBWRl-797-59 430
PLES-C25-60(U)4O 432
PLES-TR-103 432
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RADC-TR-60-146 432
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RADC-TR-60-228 430
RADC-TR-llOl 452
RIAS-TR-60-16 450
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RLES EP-44I9-105-60U 4lO
Rocket R-2241 419
RPI M«hRep-39 484
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SA-TR16-1116 445
SELTR- 157-1 433
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STL/GM-TR-0165-00535 473
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RADIOLOGICAL HEALTH
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pnpwd by U.S. Public H9alfh Service
puhlish€d by 075
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A revision of the Radiological Health Handbook, compiled and edited by
the Division of Radiological Health, Public Health Service, U. S. Depart-
ment of Health. Education, and Welfare, has been released for sale to
the public through the Office of Technical Services, U. S. Department
of Commerce.
The new edition, which is current to September 1960, supersedes the
former edition published in 1957. The Handbook provides much of the
basic radiological information required in health protection practice.
It was originated in conjunction with the radiological health training
courses presented by the Public Health Service where it has served as
a major reference text in these courses for the past 10 years. During
this time, the Handbook has been widely used by educational institu-
tions, industry and Government.
The revision is similar in scope to earlier editions. Sections are in-
cluded on physical, chemical, and mathematical data; radioisotope, de-
cay, and radioassay data, and radiation protection data. Much of the
material previously included has been up dated, especially the Table of
Isotopes. The glossary has been expanded and modified in consistency
with the definitions in the American Standards Association's "Glossary
of Terms in Nuclear Science and Technology. " Also revised is the
Handbook's Chart of the Nuclides. uscomi— oc
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EPORTS
T
May 16, 1961
Vol. 35, No. 5
A monthly listing of
Government research reports
available to indxistry
this issue:
New Type of Lightweight Cellular
Material. (PB 161 770) p. 613
idbook of Fibrous Materials.
(PB 171 494) p. S89
jh Pressure Physics.
(PB 171 049) p. 630
i-Strength-Steel Forgings.
(PB 151 102) p. 612
irdrofoils. An Annotated Bibliography.
(PB 171 502) p. 609
il Fiber Reinforced Ceramics.
(PB 171 550) p. 591
^sical and Mechanical Properties of
Tungsten and Tungsten-Base Alloys.
|(PB151 084) p. 614
itic Fabric (Vinyl Nylon) Vehicle Tar-
iptulins. (PB 171 525) p. 588
riew of Developments in Iron-Alumi-
llum-Base Alloys. (PB 161 232) p. 610
jparent Packaging.
*B 171 532) p. 593
Complete list of printed reports
begins on page iii
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CONTENTS
^-
MBUOGRAPHY
ASTRONOMY
Astrophysics
BEHAVIORAL SCIENCES
Human Engineering
Personnel and Training
Psychology
KOLOGICAL SCIENCES
Anatomy and Physiology
Biochemistry
Medical Specialties and Equipment.
Pathology
CHEMISTRY.
Inorganic Chemistry
Organic Chemistry .„
Physical Chemistry
EARTH SCIENCES
Climatology and Meteorology
Geodesy >
Oceanography
Physics of the Atmosphere
ENGINEERING
Aeronautical Engineering
Chemical Engineering
Civil Engineering^
Electrical and Electronic Engineering
Sanitation and Safety Engineering
Ship Building
MACHINERY, FABRICATICN, AND ACCESSORY EQUIPMENT.
Engines and Propulsion Systems
Machine Parts and Mechanisms
Manufacturing Equipment and Processes
Transport, Traction and Hoist Facilities
MATERIALS • •
Adhesives andSealants
Ceramics and Refractories
Fuels, Lubricants, and Hydraulic Fluids
Leather and Textiles
Plastics
MATHEMATICS
Computing Devices
MECHANICS
Aerodynamics and Pneumatics
Hydrodynamics, Hydraulics, and Hydrosutlcs
METALLURGY
Ferrous Metals
Light Metals
Nonferrous (except light) Metals
Structural Metallurgy and Corrosion
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY
Elementary Particles • . .
Instruments and Installations
Nuclear Reactions
Radioactivity
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT
PHYSICS i
Acoustics
Electricity and Magnetism
Electronics .* •
Molecular Physics and Spectroscopy
Page
"533
533
534
535
535
536
538
541
542
543
544
544
546
546
547
548
554
555
557
557
558
560
560
564
565
565
585
585
586
586
587
587
588
588
589
590
592
592
593
593
601
602
604
608
610
611
612
613
614
615
616
617
618
619
619
620
620
621
621
623
PHYSICS (coo.)
Opcics
r
Page
. 620
. 624
Solid State Ph^lcs • 625
Theoretical Pbysica ^
Thermodynamics. • ^
Wave Propagation ^
RESEARCH METHODS, , TECHNIQUES AND EQUIPMENT 636
Cotnmunication Theory 637
Photographic Equipment 637
SOCIAL SCIENCES 631
Documenutioti • • 638
MISCELLANEOUS • 639
lOY
ATOMIC ENEROY COMMISSION REPORTS
GENERAU MISCELLANEOUS, AND PROGRESS REPORTS
BIOLOGY AND MEDICINE
CHEMICAL SEPARATIONS PROCESSES FOR PLUTONIUM AND URANIUM.
CHEMISTRY •
CONTROLLED liffiRMONUuiAR PROCESSES
CRITICALTTY STUDIES
ENGINEERING AND EQUIPMENT
GEOLOGY AKD MINERALOGY
HEA LTH AND SAFETY
INSTRUMENTS.
ISOTOPES — INDUSTRIAL TECHNOLOGY •
ISOTOPE SEPARATION
MATHEMATICS AND COMPUTERS
METALS, CERAMICS, AND MATERIALS
METEOROLOGY
PARTICLE ACCELERATORS AND HIGH- VOLTAGE MACHINES
PHYSICS . . . r
RADIATION EFFECTS ON MATERIALS
REACTOR TECHNOLOGY
TECHNOLOGY — RAW MATERIALS
WASTE DISPXpSAL AND PROCESSING
641
641
641
644
646
653
653
654
656
657
658
659
659
660
661
668
668
669
674
674
660
680
SOURCE INDEX! !"1
SUBJECT INDEM
NUMBER INDEX
1-6
1-14
PRINTED REPORTS AVAILABLE FROM OTS
ANNOUNCED IN THIS ISSUE
BEHAVIORAL SCIENCES ^
Some social factors affecting the choice of an "imitative" response
in a probability learning situation. Aug 60. 52p. (PB 171 545) $1.50,
BIBUOGRAPHY
539
U
Cooling and coolants for electrical and electronic equipment, turbines
and reactors. Jan 61. 17p, (OTS SB-449) 10 cents 533
Maintenance and maintainability. An ASTIA report bibliography.
Dec 60. 77p. (PB 171 518) $2.00 533
BIOLOGICAL SCIENCES
Nonlinear passive mechanical properties of skeleul muscle. Aug 60.
lip. (PB 171 495) 50 cents > 542
Ptrachutist's spin problem. Dec 60. 8p. (PB 171 048) 50 cents 542
Pbouxnetry at low levels of intensity. Jan 61. 64p. (PB 161 834) $1.75 542
CHEMISTRY
Aluminum hydride: A literature review. Aug 60. 21p. (PB 171 534)
75 cents 552
Attempted synthesis of beryllium hydride. Oct 60. 35p.
(PB 171 489) $1 . 00 553
Ionic nature of molten slats. Dec 60. 17p. (PB 171 535) 50 cents 553
New approach to the conibustion calorimetry of organosilicon com-
pounds. The heats of combustion and formation of hexsmethyldi-
siloxane. Nov 60. 14p. (PB 171 528) 50 cents 549
Properties of solutions in the neighborhood of the critical temperature
of the solvent. Apr 60. 25p. (PB 171 530) 75 cents 554
Radiation chemistry of chloroform systems. Sep 60. 25p.
(PB 171 497) 75 cents 551
Research on high temperature polymers. 1959. 123p. *
(PB 171 522) $2. 75 551
Surface recombination of hydrogen atoms in the presence of water
vapor. 1960. 19p. (PB 171 512) 50 cents 550
ENGINEERING
Analysis of the relationship between the collision-avoidance trajectory
of an aircraft and its performance capability. Jan 61. 13p.
(PB 171 052) 50 cents 562
Behavior of riveted and welded crack arresters. Aug 60. 134p.
(FB 171 576) $2.75 585
Ceramic tubes development for external heat sources. June 60. 43p.
(FB 171 492) $1 . 25 571
Construction of beacon video defruiting equipment type 2. 3NS10.
Apr i9. 40p. (PB 171 508) $1.00 566
Determination of a standard extinguishing agent for airborne fixed sys-
tems. Oct 60. 62p. (PB 171 552) $1.75 562
Development of ANDB type 2. 3NS9 beacon video storage-tube defruit-
ing equipment. Mar 59. 85p. (PB 171 504) $2. 25 566
Development of a head-mounted camera for recording pilots' eye
movements. Mar 60. 31p. (PB 171 506) $1.00 561
Evaluation of surface -mounted lights for runway guidance. June 60.
18p. (PB 171 507) 50 cents 562
Enrusion die development: Titanium and steel. July 60. 145p.
(PB 171 529) $2.75 562
Liquid oxygen converter. Oct 60. 66p. (PB 171 554) $1.75 561
iii
I
t
ENGINEBRING <coo. ) ''
Magnetic phase jcorrection circuits. Mar 60. I36p. (PB 171 542)$2.75,
Methods for thelcootrol of satellites and space vehicles. Volume I:
Sensing and actuating methods. July 60. 443p. (PB 171 496) $6. GO . ,
Methods for the control of satellites and space vehicles. Volume II:
Control systdm mechanization and analysis. July 60. 300p.
(PB 171 553) $4. 00
New concepts fqr radio frequency transmission lines. Aug 60. 69p.
q« 171 557) :$1 . 75
NRL model E-575S leak detector. Jan 61. 9p. (PB 171 358) 50 cents.
Ordnance engineering design handbook: Servomechanisms. Section I:
Theory, consisting of Chapters 1-10. Aug 59. 232p.
(PB 171 480) $3.50.
Ordnance engineering design handbook: Servomechanisms. Section 2:
Measurement and signal converters, consisting of Chapters 11 and
12. Aug59. 129p. (PB 171 481) $2.75
Ordnance engin^ring design handbook: Servomechanisms. Section 3:
Amplificatio*. consisting of Chapter 13. Aug 59. 224p.
(PB 171 482) $3.50.
Ordnance engineering design handbook: Servomechanisms. Section 4:
Power elements and system design. Aug 59. 206p.
(PB 171 483) $3.00,
Radio dealer detectors for airport ground traffic control. June 60.
72p. (PB17U509) $2.00
Rotor bUde protective covers. Qcx. 60. 32p. (PB 171 514) $1.00
Six year storage program tests -- Packaged items. Aug 60. 84p.
(PB 171 111) $2.25
Staff devielopment in systems research techniques. Aug 59. 149p.
(PB 171 510) $3. 00
Strategic pattern recognition program for the game GO. July 60.
97p. (PB 17| 549) $2. 25
Study of tern poirer transmission. Sep 60. 97p. (PB 171 498) $2. 25 . .
Super-fast recorder for day and night observations of space vehicles
using a light i amplifier capable of suppressing the background and
discriminating moving objects. Nov 60. 21p. (PB 171 108)75 cents
Systems analysis view of longitudinal flying qualities. Jan 60. Il6p.
(PB 171 551) ; $2. 50
Transport aircraft cockpit voice recording. Dec 60. 20p.
50 cents
Page
570
584
, 553
, 575
. 576
(PB 171 505)
of lilt
MACHINERY, fABRICTlON. AND ACCESSORY EQUIPMENT
Oct 60. 115p.
15p.
Application of Ultrasonics to solid rocket systems.
(PB 171 499) $2. 50
Plastic fabric (iinyl nylon) vehicle tarpaulins. Jan 60.
(PB 171 525)] 50 cents
MATERIALS
I
Oct 60. 80p.
Design and evaluation of heat stabilised tapes and webs.
(PB 171 486) $2. 00
Handbook of fibrous materials. Oct 60. 495p. (PB 171 494) $6. 00 . . .
Infrared spectrkl emittance properties of solid materials. Oct 60.
84p. (PB 17i 515) $2. 25
Investigation of longitudinal shear distribution and damping in a
viscoelastic adhesive lap joint. Nov 60. 40p. (PB 171 556) $1.00..
Isocyanate prirter-sealer for masonry. Jan 61. 18p. (PB 171 107)
50 cents. , . -I
Mechanism of growth and physical properties of refractory oxide
fibers. Apr 60. 57p. (PB 171 520) $1.50
Metal fiber reiliforced ceramics. Nov 60. 89p. (PB 171 550) $2.25 .
Physical properties of high temperature materials. Part V. Thermal
diffusivity of magnesia -stabilized zirconium oxide at high tempera-
tures. Oct^. 19p. (PB 171 541) 50 cents
565
561
584
561
575
568
580
563
561
586
588
592
589
S90
589
590
589
591
590
iv
Page
MATERIALS (con.) >:>•
Protection of refractory metals for high temperature service. Prog-
gress report 1, July 1, 1960: The zinc-base coating for niobium.
Nov 60. 37p. (PB 161 932) $1.00 591
Protection of refractory metals for hig^ temperature service. Prog-
ress report 2, October 1, 1960: Durability of the zinc-base coating
for niobium. Jan 61. 27p. (PB 171 159). 75 cents 591
Research on non-oxide glasses. July 59. 55p. (PB 171 526) $1.50 590
Transparent packaging. May 60. 78p. (PB 171 532) $2.00 593
MATHEMATICS
General switching theory. Sep 60. 67p. (PB 171 555) $1.75 601
Symbolic logic and automata. July 60. 36p. (PB 171 548) $1. 00 601
MECHANICS
Hydrofoils. An annotated bibliography. Sep 60. 39p. (PB 171 502) $1.00 609
Stress field ai a slipped crystal and the early plastic behavior of
polycrystalline materials. Apr 60. 35p. (PB 171 531) $1.00 603
METALLURGY
Applicability of present creep prediction techniques for extrapolating
very long time creep behavior. Oct 60. 21p. (PB 171 487) 75 cents 614
CkwTOsion survey of steel sheet piling. Dec 60. 66p. (PB 171 501)$1.75 615
Design properties as affected by cryogenic temperatures (Ti-6Al-4v,
AISl 4340. and 7a79-T6 alloys). Jan 61. 19p. (PB 161 231)50 cents 610
Effect of single trace alloy additions on the properties of pure iron.
Dec 60. 72p. (PB 171 045) $2. 00 612
Evolution of nickel-base precipitation-hardening superalloys. Feb 60.
Up. (PB 161 234) 50 cents 610
High-strength- steel forgings. Jan 61. 64p. (PB 151 102) $1.75 612
Improvement of mechanical properties of steel castings by press
forging. Sep 60. 116p. (PB 171 524) $2. 50 611
Investigation to develop optimum properties In forged Ti-7AI-^Mo.
Oct 60. 145p. (PB 171 546) $2.75 610
New type of lightweight cellular material. Apr 60. 66p.
(PB 161 770) $1.75 613
Fhysical and mechanical properties of commerical molybdenum-base
alloys. Nov 60. 182p. (PB 151 099) $3. 00 613
Fhysical and mechanical properties of tungsten and tungsten-base
alloys. Mar 60. 67p. (PB 151 084) $1.75 614
Pickling and descaling of high-strength hig^- temperature meuls and
alloys. Feb61. 17p. (PB 161 235) 50 cents 610
Review of developments in iron -aluminum -base alloys. Jan 61. 6lp.
(PB 161 232) 50 cents 610
Study of rate controlled process for compressive deformation of high
purity aluminum. Sep 60. 27p. (PB 171 488) 75 cents 614
Vacuum melting of beryllium by electron bombardment. Dec 59. 41p.
(PB 171 521) $1 . 25 613
MISCELLANEOUS
Report of NRL Progress. Apr 61. (PB 171 317) $1.25, $10.00/year 639
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY
Dosimetry by luminescence degradation in organics. Oct 60. 66p.
♦(PB 171 491) $1.75 617
Electron induced radiation damage in pure meuls. Dec 60. 43p.
(PB 171 523) $1 . 25 619
Solid state Bragg-Gray cavity chamber. Oct 60. 24p. (PB 171 490)
75 cents 617
I (■
PERSONhJELSUtTLlES AND PERSONAL EQUIPMENT
Improved earcu#hions tor flying helmet. Oct 60. 31p. (FB 171 493)$1.00.
Underwater swi^nming. May 57-Mar 60. 230p. (FB 171 577) $3.00.
PHYSICS
Page
Baalc transport Iphenomena In germanium and indium antimonide.
Oct 60. 12p( (PB 171 511) 50 cents
Bibliography of tropospheric radio wave scattering. Nov 60. 82p.
(PB 161 581) J2. 25 • •• • •
Charts of corrc^tloos to radar observations for refraction by terrestrial
atmospheres. Feb 60. 148p. (PB 171 544) $2.7&
Ejqwrimental 8?udie8 on the interaction of strong sound fields with free
convection boundary Uyers. Oct 60. 79p. (PB 171 485) $2.00
High pressure jihysics. Dec 60. 47p. (PB 171 049) $1. 25
Influence of vertical vibrations on the rate of heat transfer from a
horizontal cjflinder in air. Oct 60. 65p. (PB 171 484) $1.75
NBS meteor -buijsr pr(^>agatioo project. A progress report. Mar 60.
46p. (FB 161 587) $1.25 r;
Self-consistent field dieory of quantum electrodynamics. May 60.
51p. (PB 17^ 533) $1 . 50
Single domain criteria and their Implications. Oct 59. 25p.
(PB 171 543) 75 cents
Study of sputtering of materials. Oct 60. 75p. (PB 171 513) $2. 00
Study of the alloys of transition elements. Dec 60. I7p.
(PB 171 113) 50 cents
Theoretical study of sporadic-E structure in the light of radio meas-
urements. |an6l. 42p. (PB 161 588) $1. 25
VHF radio prc^gation dau for the Cedar Rapid-Sterling, Anchorage-
Barrow, and Fargo-Churchill test paths April 1951 through June
1958. Sep 60. 262p. (PB 161 580) $4. 00
X-ray mass attenuation coefficients in the 1.49 to 11.9 kev range.
Jan60. 62pl (FB 171 527) $1.75
SOCIAL SCIENtES
vese
An operations Research study of the dissemination and use of recorded
scientific inlormation in rfiree parts: I. Journal reading by physicisw
andchemist$. II. The cost of Journal publications. III. The effect
of condensa^on on comprehension of journal articles. Dec 60. 74p.
(PB171 503) $2.00.
For your convetilencc GTS order blanks (Form TS-37) are
available on request from the OFFICE OF TECHNICAL SERVICES.
619
620
626
635
635
633
630
635
635
632
627
622
628
635
636
620
638
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
Office Of TECHNICAl SERVICES
Pages 533 - 680
May 16, 1961
m
BIBLIOGRAPHY
Armed Services Technical Information Agency,
Arlington, Va.
MAINTENANCE AND MAINTAINABILITY. AN A^HA
REPORT BIBLIOGRAPHY . Attachment to Office of
Defense Research and Engineering MENEX: Mainte-
ntnce Engineering Exchange Bulletin, Dec 60, 77p.
411 refa. AD- 247 300.
Order from OTS$ 2. 00 PB 171 518
The reference in this bibliography represent those
reports in ASTlA's AD collection (1953 to the present)
pertaining to the following phases of maintenance
engineering and maintainability: (1) the general con-
cepts, principles, and related aspects, and (2) studies
on maintenance and maintainability of equipment of all
types. References are arranged in 2 parts, according
to these broad categories, with further breakdown by
specific type of equipment. Entries appear only once,
under the subjea area primarily indicated by the con-
tents of the report . Within each category, reports
published by Department of Defense contractors are
listed alphabetically by source, contract, and date;
military reports are alphabetically arranged, within
each category, by source and title. This arrange-
ment permits the reader to follow the continuity of
research completed by a given activity and provides
an approach for reviewing future reports through use
of the source index in ASTIA's Cumulative Index.
Office of Technical Services, Depi. of Commerce,
Washington, D. C
COOLING AND COOLANTS FOR ELECTRICAL AND
ELECTRONIC EQUIPMENT, TURBINES AND REAC-
TORS. Jan 61, 17p. 263 refs. OTS Selective Bibliog-
raphy SB -449.
Order from OTS $0. 10 OTS SB-449
Lists PB reports, AEC reports and translations added
to the OTS colleaion during 1950 to Jan 61 . Contains
information on the various methods of coohng (evapo-
rative, transpiration, air-cooling, etc. ); cooling of
(Uesel engines, aircraft engines, turbine blades,
clutches, and rocket motors. (AEC reports cover re-
actor cooling and coolants) Also includes reports on
spot cooling of subminiature electronic equipment,
vacuum tubes, transformers, digital computers,
semiconductors, and elearonic equipment in general.
(Author)
ASTRONOMY
Aeronautical Research Lab. , Air Force Research
Div. , Wright -Patterson AFB, Ohio.
A COMPARISON OF THE PHOTOGRAPHIC DE-
TECTIVITIES ATTAINABLE WTTH AhTO WTTHOUT
ELECTRONIC LIGHT INTENSIFICATION, by
Radames K. H. Gebel and Lee Devol. Technical note
on Research on the Quantum Nature of Light. Oct 60,
28p. 17 refs. ARL Technical rept. 60-315.
Order from LC mi$2. 70, ph$4. 80 PB 150 322
A comparative mathematical analysis is made re-
garding the limits of performance of the closed cir-
cuit television type optical amplifying system, and of
conventional methods, for obtaining and observing
photographs of faint celestial bodies, having a mag-
nitude comparable to that of the sky background.
Primary attention is given to the cases in which de-
tectitn is accomplished by visual observation of a
photograph, but also the potentialities of electronic
counting of the developed grains in a photographic
emulsion, is considered. When using either con-
ventional photography or photography aided by an
image converter, the contrast between the celestial
body and background, necessary for visual discrimi-
nation, is determined by the photographic emulsion
or the limitations of the human eye. and an optimum
exposure time exists. With the closed circuit tele-
vision system the instrumental and sky backgrounds
can be suppressed elect ronically. Then the brightness
of the image of the celestial body increases as the
exposure time, but the brightness of the remaining
background fluctuations, being statistical in nature,
increases only as the square root of the time. TTius,
as long as the device is capable of effective storage
and integration of the electronic charge image, the
contrast increases as the square root of the expo-
sure time, and the ability to detect increases also.
(Author)
533
Astrophysics
Chicago U., Ul.
BENDDC LUMICO^
Pinal rept. on
5p. AD-247 365.
Order from LC
RESEARCH, by W. A. Hiltner.
tract AF 19(604)4540. 19 Nov 60.
80. ph$1.80
PB 153 452
Two stars. oLeo and "Lyr were compared to a stand-
ard lamp at 16 wavelength band 50A wide from 3200
to 6400 Angstroms. A relative net -work of 25 stars
were set up at different right ascensions. fTioto-
metric observations were made of 45 Northern
Cepheids and 80 ff int blud surs at the North Galactic
pole. (Author)
Harvard Coll. Cbservatory, Cambridge, Mass.
RESEARCH DIRECTED TO THE STUDY OF PLANE-
TARY ATMOSPHERES, by Donald H. Menzel and
G. de Vaucouleurt . Final repc. on Contract
AF 19(604)3074. 10 Oct 60, 15p. 9 ref s . AFCRL TR-
60-414; AD- 246 546.
Order from LC mi$2. 40, ph$3. 30 PB 153 285
Several planewryi investigations were carried out dur-
ing the 2 1/2 yea^ . Regional and integrated photome-
try of Mars has been done. The occultation of Regulus
by Venus on July 7. 1959, was observed and informa-
tion obtained on tjie scale height and its variation in
the planet's atnwiphere, and corrections to the ephem
eris position of the planet were derived. Two heat de-
tectors were studied with regard to obtaining pictures
of the temperaturie distribution over the lunar surface;
special instrumems were constructed for observing
the occultation of j Regulus; and improved techniques of
composite printii^ of planetary photographs were de-
veloped. Studies of the possibilities of conducting high
resolution photography from a balloon-borne telescope
were made. An e^aensive program for obcaining accu-
rate coordinatfes ^ surface features on Mars was un-
dertaken, based ijn pan on composites made from the
best available negatives taken at Mt. Wilson and
Johannesburg. (Aluihor)
Minnesota U. Sihool of Physics. Minneapolis.
OBSERVATION OF THE SOLAR BREMSSTRAHLUNG
BURST AT 1926 UT. 11 AUGUST I960, by
JR. Winckler, T. C. May, and A. J. Masley. Rept.
on Contract NAs4r-56. Oct 6a Up. Technical rept.
no. CR-32; AD- 3*7 161.
Order fiDm LC rt»i$2. 40. ph$3. 30 PB 153 444
An observation wLs made with balloon detectors of a
radiation increase which can be identified with cer-
tainty as a burst of bremsstrahlung originating on the
sun during a cla^s 2+ flare. The observation was
made simultaneously with identical detectors on a
balloon at MinneSpolls, Minnesota, at 45° geographic
latitude and at Ppn Churchill. Manitoba. Canada, at
58. 5° geographic} latitude and essentially at the same
longitude of 950^^. The instruments consisted d an
aluminum -walle< ionization chamber filled with argon
gas operating on the pulsing electrometer system, an
aluminum Geiger counter, and a copper Geiger
counter. The twto counters were also electronically
connected to form a vertical coincidence train. The
readings ol these Instruments are shown for boch
geographic locations. The event Is observed about
equally on both ion chambers and both aluminum
counters and with negligible response on the copper
counters and the telescopes. The event cannot be due
to primary charged particles as there is no geomag-
netic effect observed between Minneapolis and
Churchill. The ion/count ratio of about six times
minimum corresponds to protons which would pene-
trate the copper counters and be observed as a coin-
cidence count. There is no obvious local electron
source which would account for these observations.
The response of the aluminum instruments and not
the copper ones shows this event to consist of low
energy x-rays with a mean energy of approximately
aOkev. (Author)
New Hampshire U. [Durham].
THE 27-DAY RECURRENT VARIATIONS IN THE
COSMIC- RAY INTENSITY, by M. A. Shea and J. A,
Lockwood. [1960] 47p. 22 ref s. AFCRL- TN-60-699.
Order from LC ml $3. 30, ph$7. 80 PB 153 878
An analysis has been made of the 27-day recurrent
variations in cosmic-ray intensity from 1954 to 1959
using data obtained from nucleonlc detectors at Mount
Washington and Dnrham, New Hampshire. The re-
latloship between the planetary magnetic index, Kp,
and the nucleonic intensity variations was also studied.
Periodicities ranging from 24 to 31 days found during
this interval Indicate that the Intensity variations are
not necessarily associated with the central meridian
passage at active solar regions. No consistent change
was found In the length at the period with respect to the
solar activity cycle. (Author)
Radio Observatory, C-alif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RADIO OBSERVATORY. 1959.
1 A SOLAR OCCULTATION OF THE CRAB NEBULA
AT A WAVELENGTH OF 12 METERS, by
J. G. Bolton, G. J. Stanley, and B. G. Clark. Rept.
on [Contract Nonr -220(19)). 1959, 5p. 2 refs.
Order from LC mi$ 1 . 80, ph$ 1 . 80 PB 147 323
Radio Observatory, Calif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RADIO OBSERVATORY. 1959.
2. RADIO EMISSION FROM JUPITER AT A WAVE-
LENGTH OF 31 CM. by J. A. Roberts and
G. J. Stanley. Rept. on Contract Nonr -220(1 9). 1959,
14p. 20 refs. AD-236 749.
Order from LC mi$2. 40, ph$3. 30 PB 147 324
Radio emission from Jupiter was measured at a wave-
length of 31 cm. The mean equivalent disk tempera-
ture is 5. 5 X 103 deg K. Two possible sources of the
radiation are discussed: free-free transitions in a
Jovian corona, and synchrotron emission from a
Jovian van Allen belt. (Author)
534
[Udlo Observatory, Calif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RADIO OBSERVATORY, 1959.
J. POSITIONS AND SUGGESTED IDENTIFICATIONS
FOR THE RADIO STARS HYDRA -A AND HEROJ-
LES-A. by J. A. Robe/ts, J. G. Bolton, and
D. E. Harris. Rept. on [Contract Nonr-220(19)1.
(1959) 7p. 2 refs. AD-236 751.
Order from LC mi$l. 80, ph$l. 80 PB 147 325
Pbsltion measurements were made of 2 radio stars.
The measurements confirm the identification of
Hjdra-A with a close pair of galaxies and suggest
tfast Hercules -A may be a very distant elliptical.
Radio Observatory, Calif. Inst, of Tech. , Owens
Valley.
08SERVATIC»^S OF THE CALIFORNIA INSTITUTE
OP TECHNOLOGY RADIO OBSERVATORY. 1959.
4. A STUDY OF CENTAURUS-A/NGC 5128 AT 31
CM. by J. G. Bolton and B. G. Clark. Rept. on [Con -
tiact Norr-220(19)]. [1959] 8p. 9 refs. AD-236 754.
Order from LC mi$l. 80, ph$l. 80 PB 147 328
A «udy of Centauru8-A/NGC 5128 at 960 Mc/s shows
that the radio extensions are visible in the decimeter
vavelength range as well as at meter wavelengths. A
comparison of the results at 960 Mc/s and 85 Mc/s
ihows that the brightness distributions are very sim-
ilar, thus the spectrum at the radio emission is in-
dependent of the region at emission. The brightness
distribution can be clearly separated into at least
three components, a central source and two extended
aources. The two extended sources resemble the
two source distribution of Cygnus-A determined from
iaerferometry. (Author)
Radio Observatory, Calif. Inst, of Tech. , Owens
VaUey.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RACHO OBSERVATORY, 1960.
1. RADIO SOURCE MEASUREMENTS AT 960 MC/S,
byD. C. Harris and J. A. Roberts. Rept. on Con-
tract Nonr -220(1 9). (1960) 25p. 14 refs. AD-236 747.
Order from LC mi$2. 70, ph$4. 80 PB 147 322
A atudy was made of 106 radio sources, using one of
the equatorially mounted 90-ft paraboloids of the
Owens Valley Radio Observatory. This investigation
was made at a frequency of 960 Mc. The primary re
■ult of the study is a reliable catalog of sources
which will be used as a 'finding list' for precise po-
sition measurements which are currently being
undenaken with the two antennas operating as an in-
terferometer. In addition, the results provided valu-
•Ne information on the spectra of the sources, and
were also used in a search for optical counterparts
to the sources. (Author)
Radio Observatory. Calif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OP TECHNOLOGY RADIO OBSERVATORY, 1960.
2. A SURVEY OF GALACTIC RADIATION AT
%OMC/S, by R. W. Wilson and J. G. Bolton. Rept.
00 Contract Nonr-220(19). [1960] 24p. 10 refs.
AD-236 750.
Order from LC mi$2. 70, ph$4 80 PB 147 326
Observations were made at galactic radiation at a
frequency erf 960 Mc/s with an antenna of 0. 8 beam-
width over a range of 300° in galactic longitude. The
beamwldth used Is comparable to that used by Hill,
Slee and MiUs (Aust. J. Phys. 11:530. 1958) at
85 Mc/s, and by Westerhout (B. A. N. 14:215. 1958)
at 1390 Mc/s. The present survey has considerably
greater coverage than either of these and sufficient
overlap to permit a reasonable study of the variation
in bri^tness dlstributim with frequency. The ob-
servations are presented as a series of contour maps
on equal area charts. Data is given on the 110 dis-
crete sources observed, including their position,
flux density, angular size and, where possible, spec-
trum and Identification. (Author) ^
Radio Observatory, Olif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RADIO OBSERVATORY, 1960.
3. SELF -ABSORPTION IN THE 21 -CM RAIMATION
FROM GALACTIC NEUTRAL HYDROGEN, by
V. Radhakrishnan. Rept. on Contract Nonr-220(19).
[1960] 8p. 7 refs. AD-236 752.
Order from LC ml$l. 80, ph$l. 80 PB 147 327.
Self -absorption of 21 -cm radiation by a 'cool' cloud
was detected near IC 443. An upper limit tothe tem-
perature of the cool dense cloud is put at 60rK.
(Author)
Radio Observatory, Calif. Inst, of Tech. , Owens
Valley.
OBSERVATIONS OF THE CALIFORNIA INSTITUTE
OF TECHNOLOGY RADIO OBSERVATORY, 1960.
4. POLARIZATION AND ANGULAR EXTENT OF
THE 960 MC/S RADIATION FROM JUPITER, by
V. Radhakrishnan and J. A. Roberts. Rept. on Con-
tract Nonr-220(19). [1960] 4p. 6 refs. AD-236 753.
Order from LC mi$l. 80, phjl. 80 PB 147 329
BEHAVIORAL SCIENCES
Human Engineering
Armed Forces -NRG Vision Committee, Washington,
D. C.
INFORMATION REQUIREMENTS FOR THE CON-
TROL OF COMBAT FORCES. SUMMARY OF TTIE
PROCEEDINGS OF A CONFERENCE SPONSORED
BY WORKING GROUP VL VISUAL DISPLAYS HELD
AT THE NATIONAL ACADEMY OF SCIENCES,
WASHINGTON, D. C. JUNE 24-26, 1959, ed. by
J. W. Gebhard and R. M. Hanes. Rept. on Contract
Nonr- 2300(05). Mar 60, 33p. l ref. AD- 234 060.
Order from LC ml^.OO, ph$6.30 PB 153 755
Dynamic Analysis Control Lab., Mass. Inst, of
Tech . , Cambridge .
MEASUREMENT OF HUMAN OPERATOR ALERT-
NESS IN CONTINUOUS CONTROL SYSTEMS, by
Peter Briggs . Rept. on Contract AF 19(604)4548.
Apr 60, 35p. Rept. no. 8055-2; ERD-TN-60-794;
AD- 246 429.
Order from LC mi$ 3.00, pb$6. 30 PB 153 202
535
The human operator is often assigned continuous vis-
ual tracking tasHs which demand a high degree of pre-
cision during a prolonged period of time. It is com-
mon experiencelthat over the course of such a task the
human is prone |o boredom, fatigue, drowsiness ,
etc. , and as a result his performance is degraded. It
is the objective bf the present report to evaluate one
method for measuring the alenness of a human with
the expectation <hat such a technique might be applied
to the monitoring of critical human control tasks so as
to anticipate serious performaifce decrements . The
proposed technique is this: while the hun«n operator
is tracking a colitinuously varying reference input, a
relatively high frequency, low amplitude disturbance
is intermittently introduced at a point between the
operator and the process he is controlling; it is thus
necessary for tie operator to cancel the disturbance
by appropriate tianlpulatlon of the control elemeits .
His amplitude-ptiase response to the disturbance in-
put is taken as 4n alertness measure. The results of
laboratory testa on subjects performing a simulated
vehicular control task indicate that over the course of
a one hour run Jtatisiically significant decrements in
the alertness m»y be discerned by this technique.
However, additional data are required to fully evalu-
ate the feasibility of the method for application in an
alertness monitjring device. (Author)
Pi rtonnel and Training
Air Crew Equ pment Lab. , Naval Air Material
Center, Riilacjelphia. Pa.
COMPILATION OF ANTHROPOMETRIC MEASURES
ON U. S NAVtY PILOTS, by Edmund C Gtfford.
2 refs. NAMC-ACEL-437; TED
Part I.
mi$2. 70, phK 80 PB 153 489
28 July 60, 24p
NAM AE-I404.
Order from LC
One thousand o0e hundred ninety Navy pilots were
measured with »^espect to 25 different morphological
features. Of these pilocs, approximately 450 were
from fighter squadrons, 450 from atuck squadrons,
and 290 were from other types d squadrons. Per-
centiles and frequency distribution are presented as
well as cross correlation coefficients among the 25
variables (Author)
BureauofNaviil Personnel, Washington, D. C
. - _....« *« A up-v^.*^^. nrwtn T?'VnD C7CCX:
PERSONALITY
r^.vo^.— ».. TEST FAKING: THE EXPRESSED
WILLINGNESS OF COLLEGE MEN TO FAKE ON A
PERSONALITV TEST, by Bernard Rimland. Aug 60,
lip 2 refs. Technical Bulletin 60-13; AD- 248 141.
Order from LC|ml$2. 40. phS3. 30 PB 153 604
Due to the Importance of personality as a critical de-
terminant of effective performance by naval personnel,
new tests and tfchniques are being devised in an at-
tempt to provid*j accurate measures o* personality
traits. One pr(*)lem faced by research workers hi
this field and bf operating personnel who must use the
results of personality tests, is the control and de-
tection of pers<»is who deliberately give false answers
This report is a by-product of a larger
to produce a fake- resistant personality
on such tests
study designed
test. It is based on the answers given by a group of
students when asked directly whether or not they
would have faked on the test If It had been given oper-
ationally. Only a small percentage of the students ad-
mitted that they would have engaged in extensive
falsification, though many said they would havt biased
their answers to some extent. This finding was the
same whether the students signed their papers or re-
sponded anonymously. Secondary findings indicated
that the students' answers had been influenced, pre-
sumably without their awareness or Intent, by the in-
structions they had been given during the earlier ex-
perimental administration of the test. (Author)
Bureau of Naval Personnel, Washington, D, C
THE TRAINING AND UTILIZATION OF SONARMEN
ASSIGNED TO CRUISER- C«STROYER FORCE
UNITED STATES PACIFIC FLEET, by Edward J.
Pickering and Adolph V. Anderson. SeiJ 60, 50p.
3 refs. Technical Bulletin 60-11; AD-248 140.
Order frtwn LC ml$3. 30, ph$7. 80 PB 153 561
During the period from March through July 1959, one
hundred and thirty-four sonarmen on twenty-six
randomly selected Pacific Fleet destroyers were
interviewed In order to obtain Information about their
training and utilization. In general. It was found that
the destroyer sonarman is adequately trained by the
sonar school to perform the duties to which he is as-
signed; however, It was noted that the school graduate
is not as well prepared to maintain sonar equipment
as he Is to operate that equipment. Suggestions are
made for using the survey results when planning modi-
fications to sonar school training; for taking steps to
insure school graduates are thoroughly familiar with
electronic test equipment; for providing guide lines
for shipboard maintenance training programs; andfor
orienting sonar school training around the specific
equipments the sonarman will operate in the Fleet.
(Author)
Clifton Corp . , Washington , D . C .
STAFRNG REQUIREMENTS FOR CVA-59 CLASS
SHIPS, by C. Thomas Clifton. Rept. on Contract
Nonr- 2476(00). May 60, 137p. 10 refs . AD-238 995.
Order from LC mi$6. 90. ph$21. 30 PB 148 555
In studying the utilization of naval personnel and in de-
termining personnel requirements two independent
studies --one employing a management analysis ap-
proach, the other a work measurement diary- -were
undertaken aboard three ships of the CVA-59 Class.
Each of the approaches employed in this study provide
valuable staffing data and establishes a data-gatherln|
method which can be utilized by naval, personnel with
only a minimum of additional training. The Staffing
Guides , derived as a product of management analj^l*.
will be useful to manpower planners in developing com
plem^nts and allowances , to Type and Ship Commands
in distributing and allocating personnel , and to re-
searchers in further study of personnel staffing prob-
lems . This conclusion is supported by the difference*
found between actual work requirements figures gen-
erated by the contractor and the average of authorized
allowances for the CVA-59 Class of ships , as well M
between requirements totals and on-board counts for
two of the ships studied. The management analysis
536
gppioach is a practical and feasible method for obtain-
SgreUable and valid data , as a basis for determining
personnel requirements . The diary method is useful
in developing personnel requirements; it provides re-
liable and stable workload data, and such data can be
obuined in a relatively short period of time. Study of
the relationship between the management analysis and
diary approaches gives support to Staffing Guide rec-
ommendations , and provides assurance that the guide-
lines may be used with confidence. (Author)
Human Resources Research Office, George
Washington U. , Washington, D. C.
SOME PROBLEMS IN PREDICTING TRAINING
REQUIREMENTS FOR FUTURE WEAPON SYSTEMS,
by Robert A. Goldbeck and Emanuel Kay (American
tost, for Research). Rept. on Contract DA 49-106-
qm-l. Nov bO, 32p. 36 refs. Research rept. no. 6.
Order from Lt mi$3.00, ph$6.30 PB 153 288
•IWs study includes ^ (1) A review and summary of
several earlier AIR studies concerned with prediction
(< job and training requirements, delineating problem
areas for which solutions must be found If a complete
and systematic procedure for predicting the training
requirements of future weapon systems is to be
developed; (2) an anempt to develop training require-
raeots information for a specific missile system
(Hawk) just prior to development of a complete proto-
type, listing sources of information available at this
stage and assessing their relevance in predicting
future training needs. Administrative arrangements
needed with system-development agencies to facilitate
effective predictions of human factor requirements
are discussed. (Author)
Personnel Research Board. Ohio State U. Research
Foundation, Columbus.
PATTERNS OF LEADER BEHAVIOR: A FACTORIAL
STUDY OF NAVY OFFICER PERFORMANCE, by
Ralph M. Stogdill, Robert J. Wherry, ai»d William E.
Jaynes. Rept. on Studies in Naval Leadership, Con-
tract N6ori- 17, T.O. 3. 1953, 90p. 14 refs.
AD-13 911.
Order from LC mi$4.80, ph$13.80 ' PB 154 836
This report released for sale to the public 17 Mar 61.
Empirical tests were used to study the following hy-
potheses: (I) Leadership behavior is multidimensional;
lu dimensions are finite in number. (II) The pattern
of behavior along the different dimensions is affected
by the position to which the leader is assigned. (Ill)
The paaem of behavior along different dimensions is
•ffeaed by the type erf organization. Test measure-
ments and sociomecric data were obtained for each of
120 STO's (S{>ecialty by Type of Organization) by com-
bining the scores for all officers of the same specialty
in the same type of organization. The 120 STO's rep-
resent 47 organizations of 12 types (plus a combined
group), 45 billets, and 470 officers. A factor analysis
of the correlations among the 120 STO's yielded 8 in-
dependent dimensions among the officer activities:
puWlc relations representatives, professional con-
sultants, personnel administrators, technical super-
visa's, schedule-procedure makers, maintenance ad-
ministrators, decision makers, and coordinators. A
marked tendency was noted for similar specialties to
appear with high loadings on the same factor. Simi-
larities were revealed among different specialties in
the same type of organization, and in other cases
among different specialties in the same echelon of
organization. The scores of those specialties with the
highest loadings on a particular factor iiKiicate that
each factor isolates a distinctive pattern of perform-
ance. Many of the specialties show hij^ loadings on
more than one factor.
Peraonnel Research Board, Ohio State Research
Foundation, Columbus.
THE PRECMCTION OF NAVY OFFICER PERFORM-
ANCE, by Ralph M. Stogdill, Ellis L. Scoa and
others. Rept. on Studies in Naval Leadership, Con-
tract N6ori-17, T.O. 3. 1953, 80p. 1 ref.
AD-18 814.
Order from LC mi$4.50, pti%^2. 30 PB 154 837
This report released for sale to the public 16 Mar 61.
This research was designed to predia the behavior of
Navy officers who were transferred to new positions.
The objectives were to determine which aspects of ad-
ministrative jjerformance can be predicted most suc-
cessfully, which types of transfers can be prediaed
most successfully, which predictive methods are most
successful, and what factors are Involved in success-
ful prediction. Data were accumulated on predicting
individual items of behavior and the behavior erf dif-
ferent subjects. The predictors used the clinical and
sutlstical methods in making their predictions.
Personnel Research Board, Ohio State U. Research
Foundation, Columbus.
A STUDY OF LEADERSHIP AMONG SUBMARINE
OFFICERS, by Donald T. Campbell. Rept. on Studies
in Naval Leadership, Contract N6ori-17, T.O. 3.
1953, 2l7p. 56 refs. AD-13 890.
Order from LC mi$9. 60. ph$33. 30 PB 154 838
This report released for sale to the jniblic 16 Mar 61.
Data were coUeaedfrom 68 officers and 600 enlisted
men comprising the crew of 10 submarines in one
squadron. The following factors were considered in
the study of leadership: the definition and criterion of
leadership, setting of the research, naval records of
ship efficiency, ship morale, leadership correlations,
naval records evaluating individual officers, repixa-
tlonal measures and secondary criteria of officer
leadership, administrative performance variables,
leader behavior description, soclometrlc variables,
and estimates of group opinion.
Purdue Research Foundation, Lafayette, Ind.
A COMPARISON OF THREE TYPES OF WORK
ACTIVFTY STATEMENTS IN TERMS OF THE CON-
SISTENCY OF JOB INFORMATION REPORTED BY
INCUMBENTS, by E. J. McCormick and Keith B.
Tombrink. R^. on Contraa AF 41(657)240. Aug 60,
79p. 5 refs. WADD-TR-60-80; AD-248 386.
Order from LC mi$4.50, phJ12.30 PB 153 855
537
ff »
iork
Three types of tlrork aaivity statements (tasks, ele-
ments, and wori aaioos) were compared for consia-
ency at Job information collected through their use in
check lists. Check lists d activities of two main-
tenance pxwition types were administered to incum-
bents and supertisors. These provided for reporting
Job information on seven scales: (I) frequency of
performance of activities; (2) time required for
performance; (3) mental difficulty; (4) physical dif-
ficulty; (5) type of training received; fe) type of train-
ing desired; an^(7) type of assistance obtained.
Three indexes of rater consistency were used:
(a) test-raest Reliability of scale responses: (b) test-
retest reliability of reports about the occurrence of
activities; and (fc) inter-rater consistency of scale
responses. Fof the quantitative scales, (1-4) tasks
and elements ylielded more consistent information
than work actions. With the qualitative scales (5-7),
work actions w^re more consistent than tasks, with
elements fallintf between and not differing signifi-
cantly from either of them. (Author)
Research
USE
Purdue
reVELOPMEN' '
LISTS FOR
by E. J.
on Contraa AF
WADD-TR-60
Order from LC
Foundation, Lafayette, Ind.
OP WORKER ACTIVITY CHECK
IN OCCUPATIONAL ANALYSIS,
McCoijmick and H. L. Ammerman. Repc.
41(657)237. July 60. 92p. 6 refs.
■7; AD- 248 385.
mi$5. 40, ph$15. 30 PB 153 854
To determine tlie consistency with which Job incum-
bents respond ta a list of task activities, several
forms of check lists were completed by Job incum-
bents in three Air Force position types. An identical
form was readiiinistered one week later. Consistency
was measuredby test-retest correlation erf scale re-
sponses and by the proportion of tasks marked con-
sistently on bo* administrations. Consistency in re-
porting frequency of task performance and length of
task time was fcirly satisfactory with mean relia-
bilities around]. 70. Those for relative proportion of
total time per cask and for general task difficulty
were considerably lower (. 53 and . 52). From analy-
ses of variancei it was determined that: (a) consist -
jency in reportitog task occurrence is not generally
related to consistency in reporting other types of
task informaticr: (b) a recall period of six months
elicits more refliable task occurrence information
than a one-mor^h period, but the one-m^h recall
yields greater consistency of time and difficulty
Judgments thanlthe six -month period; and (c) inter-
actions among experimental factors (scales, recall
periods, positipn and equipment types, methods of
response) wer^ generally negligible. The degree of
reliability sho^n and the absence of imponant inter-
actions are evidence that the check list may prove a
useful procedure for gathering information over a
large variety of conditions and Jobs. (Author)
PsycholoQ)^
American Inst, for Research, Pinsburgh, Pa.
PROMPTED PUJS UNPROMPTED TRIALS VERSUS
PROMPTED TRIALS ALONE IN PAIRED- ASSOCIATE
LEARNING, by David Angell and Arthur A. Lumsdaine.
Rept. onContraaAF 49(638)681. Oa 60, 22p. 12 refa
Research rept. AIR-314-60-IR-129; AFOSR-TN-60-80a
Order from LC mi$2.70, ph$4.80 PB 153 497
An experiment is reported which was concerned with
the use of a partial degree of prompting as compared
with complete prompting. The basic comparison was
between two groups, one of which received promptin|
on all trials in learning a set of paired associates, aad
one of which practiced responding without prompting «
every fourth trial. The paired-associate learning
materials and the intra-trial stimulus -response time
intervals were substantially the same as those em-
ployed by Cook (1958). The results showed that, con-
trary to the interpretation of previous data by other in-
vestigators, learning was significantly more efflcien
under the experimental condition of incomplete profun-
ing (prompting on three-fourths of the trials) than
under conditions of complete prompting (prompting a
every trial). (Author)
Amherst Coll. , Mass.
MEASURING ELEMENTS OF NEED ACHIEVEMEhTr,
bv Robert C. Blmey, Harvey Bur dick, and Richard
C. Teevan (Smith Coll.) Annual rept. for Sep 58-Sep»
on Contraa Nonr- 2309(02). [Feb 60] 13p. 2 refs.
Order from LC ml$2.4a ph$3.30 PB 153 ISO
A thematic scoring system indicative of a fear of fail-
ure is being developed. Data were gathered under 4
conditions: (1) a group testing session during a regular
laboratory period; (2) individual performance on the
dart task (3) filling out the Habar-Alpert test anxiety
questionnaire outside die laboratory; and (4) answerinf
the level of aspiration items immediately before the
final examination in the course. The following panemi
were derived: (I) negative- average expected D below
the midpoint of score and norm; (2) low positive
cautious -- average expected DJust above score -norm
midpoint, pleased D below or equal to the expected R
(3) low positive optimistic -- same as 2 but pleased D
is above expected D; (4) high positive cautious -- ayer-
age expected D is well above score- norm point but
pleased D lies between score and expected D; and (S)
high positive optimistic -- same as 4 but pleased D
lies above expected D. Results showed the relation of
need achievement to the groupings created by use of
the pfleased D score to designate pessimism -optimism.
The t value for the difference between the pessimistic
and optimistic groups is 1.65, PC 10, 36 df. Data
further showed that need affiliation is most character-
istic of the negative group on expected D score, die
difference from the low positive group yielding a t of
1.40, PC 20. Comparison of the pessimlstic-optlmU-
tlc groups yields a t value of 2.66, PC.Ol. The nega-
tive group departs from the optimistics at the P<.001
leveL
Applied Mathematics and Statistics Labs. , Stanford
U., Calif.
THE USE OF MODELS IN EXPERIMENTAL
PSYCHOLOGY, by Richard C. Atkinson. Technical
rept. no. 28 on Contract Nonr-225(17). 24 May 60,
17p. 9 refs. AD- 237 829.
Order from LC mi$2. 40, ph$3. 30 PB 148 IW
A formal analysis of the function of models in psychol-
ogy is considered. A simple model of behavior is de-
scribed, and the method of application to a complex
problem in decision making is Illustrated. By exami-
nation of this particular case, the role of mathemati-
cal models will be indicated in determining program*
of psychological research and specifying the types of
empirical observations to be made. (Author)
538
Qikewood Corp. , Albuquerque, N. Mex.
INFORMATION CONTENT OF LEARNED MES-
SAGES by L. Wayne Davis and Bennett L. Basore.
a«nt on Contract AF 30(602)1890. 28 May 59, 58p.
27i«f8. QR-3-1004; RADC-TN-59-209; AD-217 682.
Older from LC mi$3. 60, ph$9. 30 PB 150 904
The primary purpose of this study was to investigate
the application of communication -theory techniques to
the theory of learning. A search of the existing liter-
ature revealed a dearth of material in the field; there
(ore, it was necessary to initiate a new effon. En-
couraging' results were obtained in |he direction of
neMuring the information content of learned mes-
Mges and were applied to the learning of "binary
moMics" or simple message patterns. (Author)
Duke U. Medical Center, Durham, N. C.
PSYCHOPHYSIOLOGICAL MECHANISMS OF
STRESS RESPONSIVITY, by Stanford 1. Ohen.
Albert J. Silverman, and B. M. Simavonian. Semi-
amual rept. for Ajff-Oct 60 on Contract
AF 49(638)354. [1960] 2 8p. AFOSR-TN-60-1178.
OrdB- from LC mi$2.70, phV-80 PB 152 837
The responses of "field" and "body" orientated sub-
jects toward sensory deprivation were recorded. In-
dividuals were designated "field" or T)ody" orien-
tated by the Draw a Person Test or the Rod and
Frame Test. Subjects were tested for toudi thres-
hold and pain tolerance before and after sensory de-
privation. The subjects were left in a dark sound-
proofed room for 2 hr without Instruction, during
which time, EEG, skin resistance, peripheral
pletfaysmographic, respiratory and cardiac rate
records were obuined. Individuals who relied more
on field (external) cues, revealed less ability to dis -
criminate sensory cues, remained more aroused,
moved around nwre, appeared more uncomfortable,
struggled more with feelings and fantasies or denied
diem, were more suspicious, projected Internal per-
cepts more, and showed a greater degree of dis-
organization. Individual differences reflected in
body/field i>erceptual dimensions may reflect neuro-
humoral (nonadrenaline) and physiologic differences
or differences in the central nervous system between
die two groups, as well as in the response to the en-
Tironment. Preliminary studies were made of the
relationship of sex to die body /field perceptual di-
meosions.
Pels Group Dynamics Center, U. of Delaware,
Newark.
SOME SOCIAL FACTORS AFFECTING THE CHOICE
OF AN "IMITATIVE' RESPONSE IN A PROBABILITY
LEARNING SITUATION, by John T. Lanzena and Vera
T iCanareff. Rept. on Psychological Research on
Human Performance, Contract AF 33(616)5845. Aug6Q
52p. 26 refs WA DO Technical rept . no. 60-196;
AD- 249 042.
Order from OTS $1.50 PB 171 545
Seven studies are reported concerning the frequency of
occurrence of an imitative response in a two-choice
probability learning situation as a function of the char-
•aerlKlcB of the task and the choices ostensibly made
by a partner. On each trial the subject had the optioo
of either agreeing or disagreeing with a "partner's"
response (which was actually controlled by the experi-
menter). Over trials one of these modes of behavior
would maximize the probability of success. In addition
several methods were used to induce attitudlnal sets
concerning the legitimacy of the imitative behavior.
Results of the studies tend to support predictions
deduced from a modified decision theory framework.
The extent of utilization of an imitative response is a
positive function of its instrumental value and the
amount of reward obtained. The effects of the atti-
tudlnal sets, however, appear to depend on the experi-
mental procedures employed. Possible reasons for the
Inconsistent results and the relevancy <rf the experi-
ments to the problem of social learning are discussed.
(Author)
Langley Porter Neuropsychiatric Inst. , San
Francisco, Calif.
RELATIONSHIP BETWEEN ALPHA PHASES AND
REACTION TIME, by Enoch Callaway III, Charles
L. Yeager, and Pat Compton. Annual technical rept.
on Contract Nonr-2931(00). 18 May 60, lOp. 11 refs.
AD-237 757.
Order from LC mi$ 1.80, ph$ 1.80 PB 147 561
A method was presented for studying the relationship
between brain potentials and behavior that allows a
statistically reliable demonstration of a slight in-
crease in simple reaction time when the stimulus is
presented at a particular alpha phase. It would ap-
pear from this study that during an alpha cycle of . 01
second, there is a period of approximately 10 milli-
seconds during which reaction times are slowed by
approximately 10 milliseconds. (Author)
Louisiana State U. [Baton Rouge]
CONFORMITY, DEVIATION, AND A GENERAL
THEORY OF INTERPERSONAL BEHAVIOR, by
Bernard M. Bass. Technical rept. no. 20 on Behavicnr
in Groups, Contraa N7onr- 35609. Mar 60, 59p.
133 refs. AD- 233 293.
Order from LC ml$3. 60, ph$9. 30 PB 153 760
Conformity has been conceived as the reflealon of
successful Influence. This conception makes it possi-
ble to apply a general theory of interpersonal be-
havior in order to derive a series of theorems ac-
counting for much of what is known about conformity
and deviation as well as providing hypotheses about
conforming behavior for which no experimental evi-
dence yet exists. (Author)
Michigan U. [Ann Arbor].
FACTORS IN RESISTANCE TO ATTTTUC*: CHANGE.
L PERSONALITY FACTORS, by Helen Peak.
H. William Morrison and others. Technical rept. no.
1 [on Contract Nonr- 1224(10)]. 15 Aug 56, 54p.
AD- 123 629.
Order from LC mi$3. 60, phJ9. 30 PB 154 866
This report released for sale to the public 17 Mar 61.
Hypotheses and results are presented regarding the
following variables: (1) The influence of attitude c€ ex-
539
perlmentally induced pressure to diange In different
directions (2) The relation at personality measures and
Initial attitude (3) The relation oT personality factors
and susceptibility to attitude change.
New York U., H. Y.
THE VARIABLE^ AND CCM)m(»lS OF SMALL
GROUP INTERACTION, by Edgar F. Bcwgatta (Cor-
nell U.). Final nept. for 1 Sep 57-8 Oct 60 on Con-
traa AF 49(638)195. [1960) l6p. 17 refs. AFOSR-
TR-60-165; AD-i48 453.
Order from LC i^$2. 40, ph$3. 30 PB 153 080
This project expfcores the scope and inclusiveness of
variables relevant to the understanding of individual
%nd group behavlpr in small group interaction. Brief
summaries are given on studies bearing on the de-
scription of individual behavior, the exploration erf
additional aspect^ of personality, the inducibilily of
changes In persotiality, and the structure variables in
small groups.
Personnel Research Board, Ohio State U. Research
FouiKlation, Couumbus.
MOTIVATIONAL FACTORS IN INDIVIDUAL AND
GROUP PRODUOTIVITY. IV. THE EFFECTS OF
PERSONAL AND SITUATIONAL MOTIVATION UPON
INDIVIDUAL PEHFORMANCE IN A a4ALL- GROUP
SETTING, by WHllam R Pavllk. Rept. on Contract
N6orl-17, T. 0.,3. 1956. 76p. 50 refs. AD- 115 143.
Order from LC ^IH 50. ph$12. 30 PB 154 835
This report released for sale to the public 16 Mar 61.
The focus 0* attention is upon the interactive effects o€
personal and sitiiational motivation upon the per-
formance of individuals in a group situation. Situ-
ational motivation is varied through the use d a mone-
tary Incentive aifd the frequency of interpolated time
signals; personal motivation or "individual drive level"
Is inferred frora scores on the Taylor Scale of Mani-
fest Anxiety; and individual performance is defined by
scores on anassjcmbly task oerformed in a small-group
sening. (Authoi)
Small Groups T esearch Center, Washington U. ,
St. Louis, Mo
STATUS VARIABLES AND MATCHING BEHAVIOR, by
Richard deChariJis and Milton E. Rosenbaum. Tech-
nical rept. no. ion Contraa Nonr-8l6(ll). May 60,
18p. 14 refs. A >237 641.
Order from LC ni$2. 40, ph$3. 30 PB 147 767
Seven-two subjeirts (Ss) participated in a conformity
experiment whe|e matching behavior was the dependent
}h evidence indicated the efficacy of
le independent variables of status and
atus, they were not found to be di-
matching behavior. The S's self-
to be related to matching in two in-
dependent samples. There was tentative evidence that
revocability of liig^ status may augment matching be-
havior in comparison with other conditions, and that
telling a high seflf-esteem person that he has low
status may decrease his matching behavior. (Author)
measure. Alth
manipulation of
revocability of
rectly related t
esteem was fou
Small Groups Research Center, Washington U. ,
St. Louis, Mo
VARIATIONS IN INTERACTION PROFILES AND
GROUP SIZE, by Robert L. Hamblin and Keith Miller.
Technical rept. no. 3 on Contraa Nonr-8l6<ll).
May 60, 19p. 13 refs. AD- 237 642.
Order from LC mi$2.40, ph$3. 30 PB 147 76S
An attempt was made to determine how and to what ex-
tent interaction profiles are influenced by the size of
the interaaing group. The data consisted of 27 inter-
aaion profiles, each of which was a summary or the
average of the amount of Interaction of the individuals
in several groups of a given size. A matrix of corre-
lation coefficients for the 12 Interaction categories
and group size was calculated and then factor analyzed
using the principal axis method and an oblimax rota-
tion. Two faaors were Importantly related to group
size. Factor II, interpreted as an Asch effect, was
correlated with group size .63. Giving agreement was
positively loaded on the faaor, whereas giving orien-
tations, and showing tension were negatively loaded.
Group size was more highly correlated with a third
faaor- -.74. Three of the interaaion variables were
significantly loaded on this factor, indicating that
giving and asking for evaluations decrease as group
size increases, and giving orientations increases.
The suggestion is that as group size increases, the
tendency for the group to become centralized into
faaiona increases. When this happens, the faaiona
tend to develop their own representatives who, in the
process of representing the faaios, abandon attempts
to communicate insightful opinions and evaluations as
well as other idiosyncratic content, and tend to utilize
orientations which are based on more objeaive data.
Thus, the tendency is for interaction to become more
objeaive and less subjeaive as group size increases.
(Author)
Washington State U . , Pullman.
STUDIES OF SHORT TERM RETENTION: 1 RE-
CALL OF UNRELATED ITEMS IN A SEQUENTIAL
TASK, by Kenneth E. Uoyd. Rept. on Contract
AF 49(638)805. June 60, I5p. 6 refs. Research rept.
WSU-1; AFOSR-TN-60-1057; AD- 247 385.
Order from LC mi$2. 40, ph$3. 30 PB 153 403
Short term retention was studied in a situation requir-
ing subjects to remember familiar letter-word pairs
until their recall was requested. During the time the
subjects were required to remember these items they
were presented other items or asked to recall previ-
ously presented itertSs . A measure of the average
number of items being remembered at the time of a
requested recall was investigated as an independent
variable. Subjects listened to tape recorded sequences
of the letter- word pairs . When they heard a lener
alone they were instructed to recall all words previ-
ously paired with that letter. The average number of
letter-word pairs that the subjects were required to
remember varied from 2.5 to 12.5. Recall errors
were found to increase systematically with an increaK
in the average number of items the subjects were
remembering. These results show high agreement
with previous studies of short term retention in this
sequential task. This independent variable, termed
average storage load, has now been shown to be re-
lated to recall errors over a wide range of its values,
for related and unrelated items , and under conditions
irliere subjects recall one or several items at each re-
call point . Average storage load may provide a n>eans
of scoring, or ordering, operational tasks that re-
ailre storage of information (or short periods of time.
(Author)
Washington U. , Seattle. Dlv. of Counseling and
Testing Services.
COMPARABILITY OF FACTOR STRUCTURE OF
PERSONALITY ITEMS UNDER VARIED INSTRUC-
TIONS, by Max L. Hillmer, Jr. Rept. on Contract
NoBr-477(08) and Public Health Research Grant
||-743(C5). May 60, 90p. 13 refs.
Order fromLCmiW 80, ph$l3.80 PB 148 610
A method of demonstrating the common faaor struc-
ture of three or more data matrices developed by
Horst was applied to a set of personality items ad-
ministered with three different sets of instruaions.
The principal axis factors underlying each of the three
forms of the questionnaire were determined and the re-
sulting faaor loading matrices were rotated by an
tnalytic method so that the corresponding faaors from
each-Wbtest were maximally correlated and the non-
corresponding factor correlations were minimized. Six
common factors were established. Applications of this
method to situations where several measurement tech-
niques are used on a single group or a single technique
is used on several groups were indicated. (Author)
540
BIOLOGICAL SCIENCES
[Defense Atomic Support Agency] Washington, D. C
THE RESIDUAL RADIOLOGICAL HAZARD FROM
THE AIR DETONATION OF AN ATOMIC WEAPON
IN THE RAIN, by L. D. Gates, T. A. Gibson, Jr.
•nd others. May 53. declassified 15 Sep 59, 46p.
AFSWP-501(Del).
Order from LC mi$3. 30. ph$7. 80 PB 154 402
This report released for sale to the public 2 Mar 61.
The residual radiological hazard which might result
from the use of an atomic weapon air burst during a
continuous rain situation was investigated. T^s re-
quired a consideration of atomic cloud heights and
dimensions in rainy weather, of radioactive decay, of
the scrubbing aaion by rain and other precipitation
which brings radioaaive debris to the ground, of the
altitudes of preclpiution levels, erf the times re-
quired for the radioaaive material to reach the earth,
tad of the reduaion in the residual radiation due to
■hiel^ng by surface features. A mathematical
method taking these factors into account was devised
to calculate dosage and doee rate. Calculations were
made for yields from 1 to 14 KT. It is concluded that
this estimation of the hazard is sufficiently reliable
(or operational planning and that a full-scale atomic
test in rain is not necessary to verify the magnitude
and extent of the hazard. (Author)
SkKrllng Labs. , Arlington, Va.
DfHOPARGYL ETHER: 1.6 HEPTADIYNE. Sum-
mary rept. on Contract Nonr-2727(00). [1960] 45p.
AD- 230 814.
Order from LC mi$3. 30, ph$7. 80 PB 152 902
Dipropargyl ether produced liver danuige after both .- -
oral administration and after exposure to vapors. T^ "
possibility of such damage resulting from repeated ex-
posures to low levels should be considered. Dipropar-
gyl ether produced gastrointestinal damage following
inhalation of vapor a. Similar damage was produced by
1,6 heptadiyne after oral administration to doga; 1,6
heptadiyne produced severe hypotension after both oral
administration and after inhalation of vapors. This
was seen Ih the presence of chicken- fat clots in the
heart and in the difficulty of obtaining per^eral blood
after exposure. Dipropargyl ether also caused some
instances of this. Both compounds produced lung con-
gestion and hyperemia after t)oth oral administration
and exposure to vapors. Both compounds are potent
central depressants at all concentrations studied. Both
compounds induce profound anorexia after both oral
administration and Inhalation of vapors. Both com-
pounds induce headaches and nausea in humans breath-
ing low concentrations even though they are not aware
of the nature of the compound. This was noted when
the odor from opened bottles were detected at a dis-
tance of a few hundred feet. Both compounds change
with time. This change reduces the toxicity. This is
especially true of 1, 6 heptadiyne. (Author)
Syracuse U. , N. Y.
CONTROL OF WOOD- ROTTING FUNGI, by
M. W. Jennison, Francis Milazzo, and Alexander
Perrln. Rept. no. 10 (Final) 1 Oa 57-31 Dec 59 on
Contract Nonr-669(06). Feb 60, 22p. 8 refs.
AD- 232 662.
Order from LC ml$2,70, ph$4,80 PB 153 122
Seven species al terrestrial wcxxl-rotting Basiditxny-
cetes utilized, in a synthetic medium, only the L-
(natural) form erf two common amino acids --alanine
and aspartic acid. The D- (unnatural) form was not
utilized in any instance. Eleven species of terrestial
wood-rotting Basidiomycetes grew in a synthetic
medium with thiamine as the only vitamin; with a mix-
ture of the thiamine moieties, thiazole and pyrlmidine;
and with thiazole alone. None at the organisms grew
in one chemical type of pyrimidine, yrfiile 3 species
did grow in aiKXher type. One organism grew well in
neopyrithiamine, a thiamine antimetabolite. All but 2
of the species tested were able to use the thiazole
moiety of penicillin. BioCin could not be substituted
for thiamine in any case. A simple synthetic medium
was developed for the growth at 7 species at non-
basldiomycecous marine fungi. Nine polysaccharides
were isolated from a simple synthetic medium in
which 4 species of terrestrial wood-rotting Basidiomy-
cetes were cultured in 3 separate carbon sources.
The polysaccharides were purified, and qualitatively
characterized by a variety of procedures. The poly-
saccharides were found to be qualitatively identical;
all were 1-4-llnked, unbranched glucans. Two con-
tained beta configurations, the others contained alpha
configuations. (Author)
541
knofo
my and Physiology
Aeronautical Research Lab. , Air Force Research
DIv. . Wright -Patterson AFB, Ohio.
PARACHUTIST'S SPIN PROBLEM, by Otto Walchner
and Prank Sawyer. Kept, for Mar-Sep 58 on Aerody-
namics at High Dtag Bodies. Dec 60, 8p. ARL Tech-
nical note 60-150.
Order from OTS la 50 PB 171 048
TTje purpose of this research was to estimate the apin-
rates possible when a man falls free from high alti-
tudes in a supine position. The spinning moments act-
li^ on a small model in a uniform airflow were deter-
mined for some configuration which were slightly un-
symmetrlcal with respect to the spinaxis. The spin-
rates were then calculated assuming that the body does
not pitch and roll during the fall. Per a vertical fall
from an altitude of 83, 000 feet, splnrates were deter-
nUned which far exceed the value which may be fatal
to man. (Author)
California Inst . at Tech. , Pasadena.
THE MECHAMSM OF THE HYPERACTIVITY AND
PROLONGED ANOXIC SURVIVAL OF SPINAL RE-
FLEXES IN CORDS WHICH HAVE RECOVERED
FROM ASPHYXIATION, bv A. van Harrcveld. Annual
progress rept . for June 59- Apr 60 on Contract Nonr-
220(34). 25 Apr 6C, 5p. I ref. AD- 235 755.
Order from LC m|$ 1.80, ph|l. 80 PB 154 099
Following recovery from asphyxiation of the spinal
cord for periods of 30-35 min the remaining reflex
activity consists mainly of an exaggerated extensor
tone. This reflex activity will survive renewed as-
phyxiation for unusually long periods (up to about 15
nnin.). An attempt is being made to elucidate the
mechanisms underlying these changes in the reflex be
haviour of the coitl . (Author)
Ub.,
Naval Research |^b. , Washington, D. C
PHOTOMETRY At LOW LEVELS OF INTENSITY,
by L. R Diwton and E. F. I>»Pre'. Interim rept.
12 Jan 61, 64p. 2$ refs. NRL rept. 5530.
Order from OTS |1. 75 PB 161 834
In an attempt to clarify the problems involved In the
field at physical and visual photometry, and to give
some helpful suggestions concerning their solutions, it
is desirable to retiew and summarize the principles ol
photometry, colo?imetry, and the physiology of the eye.
Several instruments and methods were developed to
help In solving the problems in this field. Step-by-
step descriptions for the calibration of instruments,
and the measurement of luminances at low- level
sources are given in order to point out appropriate
precautionary steps. The spectral sensitivity curveof
the eye shifts towtrd the region at shorter wavelengths
for sources at low-intensity light levels and the eye
then becomes many times more sensitive. Thus,
measurements of the intensity and color at a source,
using visual photctnetrlc techniques, are strongly In-
fluenced by these characteristics at the eye. Also,
the angular subtense of the source at the retina at the
eye determines thfe eye's ability to distinguish small
differences in source brightness. This results from
the physiological nuikeup at the cone and rod structure
at the retina. Special procedures must then be de-
veloped and instruments designed to take these effects
into account. Physical photometry is related to visual
comparison of a physically measured quantity with
the characteristics at a standard source at radiation
as seen in a calibrated photometer. This comparison
depends strongly upon whether it is made in the pho-
topic, mesoplc, or scotopic region of vision.
Ohio Sate U . , Columbus , Ohio.
NONUNEAR PASSIVE MECHANICAL PROPERTIES
OF SKELETAL MUSCLE, by N. A. Coulter, Jr. and
J. C. West. Rept. on Research on Physics and
Chemistry of Neurosensory Processes , Contract AF
33(616)5780. Aug 60, Up. 3 ref s . WADD Technical
rept. 60-636.
Order from OTS $0.50 PB 171 495
The nonlinear, passive mechanical properties of skel-
etal muscle were investigated. The response of frog
gastrocnemius muscle to sinusoidal displacements
over a frequency band of 0.5 to 25 cps was determlDed
From the experimen»l data a nonlinear differential
equation characterizing the passive mechanical be-
havior of muscle was constructed. (Author)
School of Aviation Medicine [Brooks AFB] Tex.
EFFECTS OF OXYGEN AND DECOMPRESSION ON
SALIVA, by David F. Mitchell. 11 June 45, 8p. 1 ref.
Proj. no. 392. rept. 1; AD- 139 670.
Order from LCmi$ 1.80, ph$ 1.80 PB 154 426
This report released for sale to the public 7 Mar 61.
There were no demonstrable differences between the
test and control groups in the 4 factors under con-
sideration, namely, pH, volume, Lactobacillus
acidophilua counts and apparent gingival condition.
School of AvUtion Medicine, Brooks AFB, Tex.
THE PHYSIOLOGICAL EFFECTS OF HYPO-
DYNAMICS INDUCED BY WATER IMMERSKW, by
Duane E. Graveline and Bruno Balke. Sep 60, I2p.
6 refs. Rept. 60-88; AD-247 163.
Order from LC mi$2. 40, ph$3. 30 PB 153 402
Body immersion in water was used to produce an ex-
perimental situation in which the normal weight sen-
sation was altered and in which slow movements were
effortless. The hypodynamlc effects of such immer-
sion on orthostatic tolerance, on cardiorespiratory
adaptability to physical stress, and on other biologic
and psychophysiologic parameters were studied on
one human subject in experiments of 2 and 7 days'
duration, respectively. Pronounced functional deterio-
ration resulted from the hypodynamlc situation in both
experiments; cardiovascular reflexes were severely
disturbed and muscular tone was diminished. The ex-
tensive biochemical studies on blood and urine showed
marked deviations from the normal. Psychomotor
effectiveness, tested on a complex systems task, was
impaired noticeably. The need for sleep appeared to
be markedly reduced during the periods of water
immersion. (Author)
542
School of Aviation Medicine [Brooks AFB] Tex
REFERENCE CURVES FOR ALVEOLAR COMPOSI-
TICW AND ARTERIAL OXYGEN SATURATION AT
VARIOUS ALTITUDES, by John S. Gray. 15 July 44,
l6p. 14 refs. Project rept. no. 290, rept. no. 1;
AD- 106 522.
Order from LC mi$2.40, ph$3. 30 PB 154 819
Ttda report released for sale to the public 17 Mar 61 .
On the basis of 1 156 alveolar samples reported in the
literature, a reference curve has been constructed
shofwiog the average composition of alveolar air at
varioua altitudes from sea level to 22, 000 feet. On
the basis of more than 500 determinations of arterial
oiygen saturation, reported in the literature, a refer-
ence curve has been constructed showing the average
arterial oxygen saturation at various altitudes from
•ea level to 22, 000 feet. (Author)
School of Aviation Medicine, Brooks AFB, Tex.
A SIMPLE AND RAPID POLAROGRAPHIC METHOD
FOR BLOOD OXYGEN DETERMINATION, by James
R. Neville. Sq>59, lip. 11 refs. Rept. 60-3;
AD- 231 545.
Order from LC mi$2.40, ph$3.30 PB 153 ^
A simple, rapid polarographic method for determining
oocygeo cottent cf blood is discussed in detalL The
me^od is shown to give results comparable to those
obuined by the Van Slyke manometric analysis. The
technic can be quickly learned and requires only a
Bominal degree of skill. The catalasellke effects of
mcthemoglobin and other blood derivatives is shown
to have a quantitative influence on the oxygen current
obtained with the dropping mercury electrode at the
plateau of the oxygen wave. The oxygen current at
(he plateau cf the hydrogen perootlde wave is found to
be Independent of the concentration of such substances.
lUa effect, which is to be distinguished from that
produced by whole blood, is discussed with reference
to other proposed polarographic methods for deter-
mining blood oxygen content. (Author)
Stanford U. School of Medicine, Calif.
A THERMODYNAMIC ANALYSIS OF THE AD-
SORPTION OF ANTIBODIES TO NORMAL GUINEA
PIG TISSUE, by George A. Feigen. Annual interim
progress rept. for 1959-1960 on A Study of "Im-
mediate" Sensitization by Adsorption of Antigens and
Antibodies, la Vitrp". Contract Nonr-225(46).
1 May 60, 26p. 31 refs> AD-239 177.
Order from LC mi$2. 70, ph$4. 80 PB 148 931
Experiments dealing with the effects of sex and
strain upon the adaptation of rata to an altitude of
12, 5(X) feet were carried out. Fourteen primary
variables were measured on each rat to determine
the changes occasioned by the stress upon the blood
picture, serum protein and electrolytes, and the
elearolyte pattern of the hean. The energetics of
the binding of antibodies to strips of normal guinea
pif ileum were studied by the methods of classical
kinetics and thermodynamics, using the magnitude of
the Schultz-Dale response as a measure of the
•mount of antibody bound to the tissue.
Biochemistry
Brooke Army Medical Center, Pon Sam Houston,
Tex.
MBTABOUSM OF BURNED PATIENTS. II. AN ESTI-
MATION OF POTASSIUM REQUIREMENTS FOR
EC^UBRIUM. by Elinor Pearson, Harry S. Soroff
and others . Final rept . on Radiation and Thermal
Bums. Aug 60, 31p. 7 refs. Research rept. MEDEW-
RS-4-60. AD-247 336
Order from LC nU$3. 00, ph$6. 30 PB 153 405
Potassium balances were measured in eleven burned
patients during four ten -day periods . The periods
represented the acute catabolic phase, the late cata-
bolic phase, the anabolic phase, and the late convales-
cent phase. The intake furnished 3,500 calories per
square meter. Eleven normal controls were (^served
on an intake identical to that of the patients . The pa-
tients stored increasing amounts of potassium during
the successive periods, but the controls showed more
positive balanqes than the patients during Period 4.
Potassium and nitrogen were stored in a ratio larger
than the protoplasmic ratio in 10 of the II patients .
Regression lines of the potassium balances on the in-
take showed that the requirements for equilibrium de-
creased as the postbum course progressed. The re-
quirement of the controls agreed closely with that of
the patients during Period 4. The ratio of the x-inter-
cepts of the poussium and nitrogen regression lines
suggests that during Periods 1,2, and 3 a K:N ratio
of 6:1 in the intake will result in the most efficient
utilization of the elements at equilibrium . A ratio of
4: 1 in the intake was required by the patients during
Period 4 and by the controls . (Author)
Brooks Army Medical Center, Port Sam Houttoa,
Tex.
MBTABOUSM OF BURNED PATIENTS, ffl. AN
ANALYSIS OF ALTERATIONS IN BODY OOMPOS-
TION, by Harry S. Soroff, Elinor Pearson and others .
Final rept. on Radiation and Thermal Bums . Oct 60,
31p. 5 refs. Research rept. MBOEW-RS-5-60.
Order from LC mi|3. 00, ph)6. 30 FB 153 406
Eleven male burned patients were studied for four ten-
day periods representing the acute catabolic phase,
the late catabolic phase , the anabolic phase , and the
late convalescent phase. Among the information
accumulated were nitrogen, potassium, and sodium
balances and daily weights . Theoretical weight curves
calculated from the three balances were compared
with the observed weight curves . The patients of Plan
I stored fat and protein during Periods 2 and 4 and
were catabolizing fat in the presence of lean tissue
gain during Period 3. Presumable the caloric intake
was inadequate during this period of active protein
synthesis , and additional calories were obuined from
the endogenous fat stores . The order of the adminis-
tration of the high nitrogen intake had an apparent in-
fluence on the changes in fat storage of the patients in
Plan II . When the low nitrogen intake was given first,
it was accompanied by a higher carbohydrate intake,
and fat was stored throughout the period. But, when
the low nitrogen intake was given last , fat was lost
during the entire period. This phenomeiKxi was most
striking for Pair I . It is suggested that during certain
543
periods of the po4tbum course, anabolism o( protein
has priority and stored f«t may be utilized to further
procein synthesis and storage. (Author)
Naval MissUe a^ Astronautics Center, Point Mugu,
Calif. I
STUDY OF ULTlLA VIOLET ABSORFHON SPECTRA
OF DEOXYNUCLEOSU3BS AND POLYNUCLEOTir«S
IN RELATION Tp THE GENERAL PHENOMENON
ENTITLED "THE HYPOCHROMIC EFFECT" , by W . C .
Glllchriest. 15 J*jv 60, 8p. 7 ref s . Technical memo,
no. NMC-TM-60-56.
Order from LC nii$ 1.80, ph) 1.80 PB 153 355
Ejqwrlmental evl^oKe was gathered in a study of the
"hypochromic effect" at the monooucleoside, nucleo-
tide, and oligonucleotide levels of molecular orgaid-
zatloa. The ultraviolet -absorption spectrum of a mix-
ture at nucleotide* equivalent in nunniber to the nucleo-
tides in an organieed polynucleotide did not demon-
strate the "hypockromic effect." Therefore, at least
two conclusions raay be drawn: (1) That the "hypochro-
mic effect" is thei result ot sequence of the nucleotides
in a given cluster (oligonucleotide) in the polynucleo-
tide, and (2) that the "hypochromic effect" is the result
of the magnitude of or the number of nucleotides in the
cluster . The experimental evidence demonstrated an
absence of the "hypochromic effect" and consequently
an apparent abseQce of change in molecular orbital
organization. It ilB clear that the molecular orbital
organization is not due to what is contemporarily
called "hydrogen bonding." Funher studies with a
specifically designed calorlnteter should produce dau
that can be coupl^ with the ultraviolet -absorption
data to clarify th^ mechanics of the "hypochromic"
phenomenon in niicleic acid 'structure. (Author) ,
M«dical Specialties and Equipment
Spec
Indiana U. Scho4>l of Medicine, Indianapolla.
A METHOD OF IHOTOGRAPHING FLUORESCENCE
IN CIRCULATING BLOOD OF THE HUMAN EYE.
by H. R. Novotn/ and D. L. Alvia. Sep 60. Sp.
2 refa. Rept. 60-t82; AD-247 162.
Order from LC n|i$L 80, ph$l. 80 PB 153 401
The development of methods for measuring change in
the caliber of retinal vessels (1) and for estimating
the retinal arteriovenous blood oxygen difference
(2) has made it possible to evaluate, to some degree,
the direction in which retinal blood flow may change
In response to various stimuli, and the PO2 at which
the oxygen requirement of the retina is being satis-
fied. These meaas of estimating changes and ade-
quacy of retinal Uood flow are indirect. A more di-
rect means of observing retinal blood flow would pro-
vide nnore precise information about variations in the
retinal jtrculation under different condiUons. The
purpose of this report is to describe some preliminary
observations on tke use of intravenous fluorescein and
retinal pthotograp^y to study retinal blood flow.
(Author)
Ohio State U- Research Foundation, Columbus.
RESEARCH ON THE PRODUCTION OF CUNICAL
RADIOGRAPHS BY MEANS OF COMPACT, LOW-
ENERGY AND HIGH -INTENSITY RADIOACTIVE
SOURCES, by H. D. Spangenberg and M. L. Pool.
Annual technical rept. no. 2, 1 Jan-31 Dec 59, on
Contraa Ncnr-495(I7). 4 Jan 60. 59p. 35 refs.
AD-233 093.
Order from LC miS3. 60, ph$9. 30 PB 152 865
Roentgenograms with the best diagnostic characteria-
tics are shown to be produced by either a 65 Itv ma-
chine operated at 70 kv or by a 90 kv machine operated
at 90 kv when their beams are filtered by Cu and Al.
Such roentgenograms possess less over -all contrast
and may be psychologically less pleasing, but provide
a greater amount of information. The Victoreen R
Meter indicates that less radiation is required to pro-
duce a diagnostic roentgenogram when a filtered beam
is used. Of the 3 filter configurations 0. 375 nun of Cu
and 0. 5 mm of Al proved the best. The spectral analjr
ais by the scintillation spectrometer indicates that the
reduction in dosage occurs as a result of the elimina-
tion of much d the low -energy part of the white radia-
tions emitted by the dental x-ray machines. If the
x-ray beam is unfiltered by added external filtration
or is filtered by a 0. 5 nun Al added filtration, the
radiation dosage required to produce equivalent
roentgenographic film density is less when the radia-
tions from a 90 kv machine are used in place of the
radiations from a 65 kv machine operated at 70 kv.
Under these filter conditions, it would seem that the
inclusion of a 90 kv machine in the diagnostic arma-
mentariums at the general praaitioner of dentistry i^
fully indicated. (Author)
Research Lab. of Electronics, Mass. Inst, of
Tech. , Cannbridge.
COMPUTER TECHNIQUES FOR THE STUDY OF
PATTERNS IN THE ELECTROENCEPHALOGRAM,
by B. G. Farley, W. A. Clark, Jr. and others. Repi.
on Contraas DA 36 - 039 -sc- 64637 and AF 19(122)458.
6 Nov 57, 21 p. 7 refs. Technical rept. no. 337;
Lincoln Lab. Technical rept. no. 165; AD- 110 027.
Order from LCmUS 2.70, ph$4. 80 PB 150607
A process has been explored, using the Lincoln TX-0
computer, for detecting pjaiterns in the elearo- '
encephalogram and for recognizing the characteris-
tics at the EEG corresponding to individual subjects.
Preliminary results indicate that a number of differ-
ent subjects and states of the same subject can be
distinguished with excellent probability. (Author)
Pathology
Arctic Aeromedical Lab. , Ladd AFB. Alaska.
EFFECT OF HYPOTHERMIA ON THE CELLULAR
RESPIRATION OF VENTRICULAR TISSUE, by John
p. Hannon and Benjamm G. Covino. Mar 58, 13p.
20 refa. Technical rept. 57 -40.
Order from LC mi$2. 40, ph$3. 30 PB 153 374
544
Ite respiration of ventricular slices and homogenates
is tbe presence of various substrates was studied in
control normothermic and experimental hypothermic
rata. The QO2 of the slices prepared from rats
cooled to a rectal temperature of 15^ C. was signifi-
omtly higher than that of control normothermic ani-
mals. No difference in the rate of oxidation of ven-
tricular homogenates was observed between the two
groups except when no substrate was used or when
pyruvate was added as the test substrate. In the ab-
gwce of substrate there was a tendency toward
h^wr rates in the hypothermic group, whereas ad-
didon of pyruvate caused a significant depression in
the oxygen consumption of this group. Addition of *
malate to the pyruvate containing medium produced
a marked increase in respiratory rate. The data ob •
tained indicate that hypothermia does not have any
adverse irreversible effect on the function of the tri-
caiboxylic acid cycle and its associated enzyme sys-
tems. The results do suggest a possible alteration
in membrane permeability, an accumulation of re-
dKed intracellular intermediates, or both, as a re-
sult at the hypothermic episode. (Author)
Arctic Aeromedical Lab. , Ladd AFB, Alaska.
GLYCINE AS AN ANTIFIBRILLARY AGENT IN
HYPOTHERMIA, by William R. Beavers and Benjamin
C C3ovino. Mar 58, lip. II refs. Technical rept.
57-29.
Order from LC ml$2. 40, ph$3. 30 PB 153 370
k both accldenul and surgical hypothermia, the chief
hazard to life is the occurrence d ventricular flbrll-
litkm. Glycine, an amino acid, has been used to in-
hibit cyclopropane -epinephrine Induced arrhythmias,
•ad this compound was evaluated in the prevention at
arrhythmias due to lowered body temperatures.
Mongrel dogs were used; pH, blood pressure, electro-
cardiograms, plasma potassium, and blood sugar were
determined at frequent intervals during cooling. Con-
trol animals, receiving no medication were cooled to
terminus and the incidence of ventricular fibrillation
was 96%. A second group receiving glycine, 1. 5 to
2.0 gm. /kg. , was cooled to terminus, and the inci-
dence of fibrlllatian was reduced to 0%. In animals
cooled to a reduced temperature of 24° C. and sub-
jected to a right thoracotomy, right ventriculotomy,
and 10 minutes' venous occlusion, the incidence at
ventricular fibrillation was 93%; the frequtacy of
flhrillation In glycine treated animals during hypo-
diennic cardiac surgery was 29%. Glycine treated
animals exhibited significantly higher blood sugar and
plasma poussium levels during hypothermia. The
molt likely explanation of the antiarrhythmic effect of
glycine in hypothermia appears to be Its ability to in-
crease plasma potassium concentration. (Author)
kooke Army Medical Center, Port Sam Houston.
TtaL
MEASUREMENT OF THE MOUSE PROTECTIVB
EFFECT OF ANTIBODY FOR PSEUDOMCWAS
AERUGINOSA IN BURNED AND UNBURNED
STENTS' SERA, by Charles D. Graber, Dan Q«n-
rali^s and others. Interim rept. on Radiation and
Tbermal Burns. ProJ. no. 6X59-06-001. Oct 60, 12p.
9 refs. MEDEW-RS-7-60.
Older from LC mi$2. 40, ph$3. 30 PB 153 640
Native hemagglutinin to a pseudomonad polysaccharide
(PC-9) present in the sera of burned and non- burned
patients was shown to have little protective function .
for mice injected with a highly virulent nosocomial
Paeudomonag aeruginosa phage type. Study of se-
quential sera cf a single burned patient surviving long
enough to produce hyperimmune antibody to his pseudo-
monad septicemia suggests that inunune bacterial
agglutinin and immune hemagglutinin are protective.
Hyperimmune sera from an unbumed rafaUt further
substantiated this relationship. (Author)
Brooke Army Medical Center. Pon Sam Houston.
Tex.
METABOLISM OP BURNED PATIENTS. I. AN ES-
TIMATION OF THE NITROGEN REQUIREMENTS
FOR EQUILIBRRJM, by Harry S. Soroff. Elinor
Pearson and Curtis P. Artz. Pinal rept. on Radiation
and Thermal Bums. May 60, 41p. 29 refs. Research,
rept. MEDEW-RS-2-60; AD -246 506
Order from LC mi$3. 30, |*$7. 80 PB 153 191
Nitrogen requirements for equilibrium in burned
patients were estimated by two plans of study in which
the nitrogen intake ranged from 1 . 0 to 28. 8 gm per
square meter and the total calories remained con-
stant at 3. 500. The two experimental designs were
such that the balance data could be sutOected to re-
gression analysis. Eleven male patients between the
ages of 18 and 33 were studied for four ten -day peri-
ods. The periods represented the acute catabolic
phase, the late catabolic phase, the anabolic phase,
aix] the late convalescent phase. The patients studied
had a bum index ranging from 20 to 35. Eleven
normal controls were studied for a ten-day period.
The amounts of nitrogen per square meter per day
estimated to be necessary for equilibrium duriqg the
four phases ranged from 20. 7 to 25. 5 gm, 13. I to
16. 4gm, 3. 3 to 9.3 gm, and 3. 3 to 7. 0 gm. respec-
tively. The nitrogen requirements of the patients
during the late convalescent phase were similar to
the requirements of the controls. (Author)
Brooke Army Medical Center, Port Sam Houston,
Tex.
MODIFIED EXPOSURE: A NEWER TECHNIQUE IN
THE MANAGEMENT OF THE BURNED PATIENT, by
Duane L. Larson, Wilfred T. Tumbusch and others.
Interim rept. on Radiation and Thermal Bums, ProJ.
no. 6X59-06-001. Oct 60, 17p. 6 refs. MEDEW-RS-
8-60. ^
Order from LC ml$2. 40, ph$3. 30 PB 153 641
The exposure method in the management of burn Injury
is more desirable than is the use of massive, occlu-
sive dressings. In order to eliminate the use of occlu-
sive dressings, even in the grafting phase, the tech-
nique which we have called "modified exposure" for
grafting has been developed. This is the application of
one layer of coarse-mesh paraffinized gauze over the
grafted areas; no other dressing is applied. The
modified exposure technique has proved extremely
useful, and is far superior to the conventional bulky
dressing technique. Although it is impossible to say
that this procedure has reduced mortality or serious
infeaion, it has contributed materially to the survival
of a number of extensively burned patients. (Authtn')
545
CorneU U Medical CoU. , New York.
STUDIES ON THERMAL RADIATION, by Jamea D.
Hanty. Pima repl. on Ckjotnurt N6-OR1-91, T. 0. Itt
1 Sep 52. I5p. 26 reft. ATI- 199 919.
Order from LC mi$2. 40. ph$3. 30 PB 154 803
I
Ttaia report releaJBed for sale to the public 17 Mar 61.
I on thermtl' radiation in indoor and outdoor
environments
Studies on pain sensation evoked by thermal radiation
Studies on tempe^ture sensation evoked by thennal
radiation
Measurement of heat loss and heat production in
humans and anlfials at different environmental
temperatures
Studies at Infrarad spectra of biologically important
compounds.
New York Medical CoU. , N. Y.
ANNUAL PROGRESS REPORT. Rept. on Contracts
Noor-2754(00) and (pi). [1959] lOp. AD- 231 817.
Order from LC iiii$1.80, ph$1.80 PB 153 152
The observations made in a pilot experiment are con-
firmed. A large number of animals either recover
completely or th^lr diabedc cotxlitlons improve In the
4 to 8 wk period after being given alloBcan. The degree
al the diabetic st^te does not greatly influence the
gross appearance at a fetal tissue implant, nor do
these factors se«n to influence the persistence d the
transplanted tissue. The persistence o< the graft and
its continued growth after the first week are signifi-
cantly related to the age at the donor. When compared
to the controls, % appears that alloxan causes a
marked redualoii In white bkxxl cells (WBC), whUe a
larger percentage at polys and a smaller percentage
0* lymphs Is maintained. The more severe diabetics
have lower hematocrit and hemoglobin values than do
the controls. In ^e hlsh diabetics, the albumin and
beta globulin risi whUe the controls drop In the period
followii^ alloxan dosage. Both high and moderate
diabetics show a less -marked decline In gamma glob-
ulin than do the doocrols in the same period. After
transplantation, bodi the controls and low diabetics
show increases in WBC while the high and moderate
diabetics do not Ibow this rise. (Author)
Inorga
CHEMISTRY
nic Chemistry
Crystallography Lab. , U. of Pittsburgh. Pa.
THE POLYHEDRAL CLATHRATE "ICE" STRUC-
TURES IN HIGH HYDRATES, by C A. Jeffrey.
D. Fell and R. f^cMullen. Technical note on Contract
AP 49(638)456. Oct 60. 22p. 9 refs. AFOSR-TN-
60-1479; AD- 246(986.
Order .from LC iti42. 70, phM- 80 PB 153 490
Richmond Research Lab. , Suuffer Chemical Co. ,
Calif. ' ,
INORGANIC POLYMERS PROGRAM, by F. O. Greek,
V. Hubbard and others. Semi-annual technical rept.
for 1 Jan 59-1 Jan 60 on Contract Nonr- 2259(00).
25 Feb 60. 82p. 34 r^fs. AD-233 515.
Order from LCmiM.80. ph$l3.80 PB 152 875
laorganic polymers: Trls-trlmethylsilylphosphine (I)
was synthesized. Anaul-141 ether was added to Na
which was dispersed in toluene. PH3 was then passed
with N into the Na dispersion. The NaPH2 produced
was added to trimethyl sllylchloride; the reaaioo was
allowed to proceed until I was completely evolved.
Chemical reactions of I were studied including oxida-
tion with slow diffusion of air, the reactions with B2H^
B5H12-9. C0CI2, diphenyldlchloroeilane, and thermal
decomposition. The reactions of perhalonitriles with
B2H6 indicated that with simple nitriles the nwin prod
uct is the expected borazine. The preparation of
pentachlorophenylsllanes was Investigated. Direa
chlorination of phenyl silanes was successful. C-P-^
polymers, irlazines: Perfluoromalononltrlle was pre-
pued. Kitriles and related compounds were prepared
from duPont lelomer alcohols. The alcohols were con-
verted to the acids, to the esters, amides, and to the
nitriles by distillation at the amides with P2O5. In
preparing amldlnes the nltrile had to be added to the
NH3 since the reverse addition produced Imidines.
The struaure of p6rfluoroglutaronitrile-NH3 addition
product was studied by IR and UV absorption. C-F-M
polymers, triazoles: The preparation of di -perfluoro-
alkyleneaminotriazole polymers was studied by 2
methods: (I) pyrolysis of an o,«i;-dlhydrazide; per-
fluoroglutaro hydrazlde, and (2) pyrolysis of an
o.<J-dihydrazidine; perfluoroglutaro hydrazidine.
Pyrolysis of perfluorobutyro hydrazine yielded 3,5-dl-
perfluorobutyro-N-aminotriazole and the isomeric
3, 6-di-perfluorobutyro-dihydrotetrazine.
Included in this report Is:
Fluorination of hexachlorobenzene with antimony
pentafluoride, pub. in the Jnl. of Organic Chemistry
24:1132-1133, 1959.
(See also PB 148 594)
Technische Hochschule, Vienna (Austria).
INORGANIC CHLORIDES AND OXYCHLORIDES AS
SOLVENTS, by Viktor Gutmann. Annual technical
rept. no. 1. I Oct 59-30 Sep 60, on Contraa DA 91-
591 -EUC- 1252. 87p. 37 refs; AD- 246 544.
Order from LCmi$4.80, ph$l3.80 PB 152 841
Systematic investigationa were carried out on donor-
and acceptor-properties of chlorides in solutions of
phosphorus oxychloride and phenylphosphonic dichlo-
ride. An apparatus was devised for ebullioscopic
measurements in hygroscopic and reactive solutions
with a high degree of accuracy. Potentiometric and
conductometric titrations were examined critically
with respect to conclusions on the occurrence of chk)-
ride ion transfer reactions. A new spectrophotomet-
rlc method was worked out to give direct proof for
chloride -ion transfer reactions. This method uses
the color differences between either FeCls and
(FeCU)- or WCl^ and (WCI7I'. The donor strength*
of chlorides and the first chloro-complexes (recipro-
cal acceptor strength of the chlorides) and the chlo-
ride ion aaivities in the solutions of the pure chto-
rldes in POCI3 were found to decrease The soluWli-
S46
tlea were found to decrease with increasing charge of
the Ions. Some di- and trichlorides may donate all
chloride ions, while this is restriaed to 1 chloride
ton with tetrachlorides. Chlorometal late -ions with an
tvcB co-ordination number are un«olvated, but
tolvated with an uneven co-ordination number. Chlo-
ronium ions are usually solvated. Numerous indica-
tions were obtained for the existence of chemical
asaoclation by chlorine bridges in solutions of non-
polar chlorides and the compounds formed from them.
B)erriim's ion association was found to occur in solu-
tions of alkali chlorides, perchlorates and chloro-
metallates and seems to be of more general
occurrence.
Yale U- . New Haven, Conn.
DETERMINATION OF THE STANDARD FREE
'BNBRGY OF FORMATION OF LEAD SELENIDE.
ky Cabell B. Finch and J. Bruce Wagner. Jr. Tech-
nical rept. no. 1 on Contract Nonr-609(34). [I960)
7p. 6 refs. AD-237 619.
Order from LCmlSl. 80. ph$ 1.80 PB 147 528
The standard free energy of formation of lead sel-
enide between 200^ and SOO^C has been determined
using a galvanic cell involving a solid electrolyte.
The standard free energy of formation may be ex-
pressed by AGO •1-23, 352 4 3. 8(t-250)l cal. (Author)
Organic Chemistiy
Institute of Polymer Research, Polytechnic Inst, of
Brooklyn, N. Y.
TOE ADSORPTION OP POLYDIMETHYL SILOX-
ANES PROM SOLUTION, by Robert Perkel (Doctoral
thesis) and Roben Ullman. Technical rept. on Con-
tract Nonr-839( 19). 10 May 60. 65p. 20 refs.
AD- 239 106.
Order from LC ml$3. 90. ph$10. 80 PB 148 788
Experiments were carried out to analyze the adsorp-
tion of the coiling polymer molecules of dissolved
polydimethyl siloxanes on the surfaces of glass and
Iron powder. Polypentamethyl dlsiloxane methacry-
late was also studied Molecular weights were ob-
tained by viscosity measurements, and infrared
spectra were used to analyze the polymer solutions.
The general experimental procedure consisted of
wMi^lilg a pyrex glass powder into an adsorption
tube; 10 ml of solution of known concentration was
pipetted on top of the powder. Most experiments
were performed with a constant weight of adsorbent
and varying solution concentration. The tubes were
inunersed in dry-ice -acetone mixture, sealed, and
agitated ovemi^t. The supernatant liquid was trans
ferred to a small flask for IR analysis and subse-
(|uent calculation of the specific adsorption. Analy-
■U of isotherms obtained when the amount of adsorb
ent is constant and the initial polymer concentration
of the solution is varied and vice versa revealed the
taMbltory action of small amounts of water on ad-
sorption of the polymers. General results of the
studies are as follows: (1) polymer adsorption at the
liquid -solid interface exceeds that possible in a 2-
dimensional layer; (2) adsorption isotherms indicate
monolayer formation; "(3) polymer adsorption In-
creases with a low power of molecular weight when
monolayer coverage is complete; and (4) adsorption
from a poor solvent is greater than that from a good
one. except where the solvent is strongly adsorbed.
Massachusetts Inst, of Tech., Cambridge.
PREPARATION OF PERFLUOROVTNYL-METAL
COMPOUNDS, byD. Seyferth, K. A. Brttndle. and
G. Raab. Technical rept. no. 3 on Contract Nonr-
1841(43). 29 Jan 60, 3p. 4 refs. AD- 231 951.
Order from LCmlJl. 80. ph$l. 80 PB 152 877
The following perfluorovlnyltln compounds were pre-
pared by the reaction of perfluorovlnyl -magnesium
bromide in tetrahydrofuran with a series of organotin
haUdes: (1) (C2H5) 3S11CF-CF2. (2)
(n-C4H9)3SoCF-CF2. (3) (n-C4H9)2So<CF=CF2)2. *nd
(4) (C6H^3SoCF^F2.
Noyes Chemical Lab . . U . of Illinois , Urbane .
SPIN DENSITIES IN ORGANIC FREE RADICALS, by
Thomas H. Brown, D. H. Anderson, and H. S.
Gutowsky. Technical rept. no. 27 on Contract Nonr-
1834(13). 2 Mar 60, 23p. 38 refs. AD- 234 555.
Order from LC mi$2.70, ph$4.80 PB 153 814
The proton hyperfine consunts obulned from protcm
magnetic resonance spectra of polycryitalline free
radicals and from valence bond calculations of <-orbi-
tal spin densities are compared for the free radicals
• ,a'-diphenyl-p-p*cryl hydrazyl and trls-p-chloro-
phenylaminlum perchlorate. Two lines are observed
in the proton magnetic resonance spectra, one shifted
upfield and one downfield from the normal resonance
frequency. These are assigned to the ortho and para
protons , and the ioeju protons of the free radicals ,
respectively. Though the agreement between theory
and experiment Is not quantitative for the hyperfine
constants , the theoretical and experimental ratios of
hyperfine constants agree within experimenul error.
Thii serves to esublish the existence of positive and
negative spin densities and to verify the signs of some
of the relationships Involved. (Author)
Pennsylvania State U. , Uplverslty Park.
BOND CHSSOaATION ENERGIES IN SMALL HYDRO-
CARBON MOLECULES (A REVIEW) by Bruce E.
Knox and Howard B . Palmer . Rept . on Contract Nonr-
1858(25). Mar 60. 26p. 64 reft. ProJ. Squid Technical
rept. PSU-6-P; AD-235 849.
Order from LCmi$2. 70. ph$4. 80 PB 153 686
A literature review is presented of the theory and
measurement of the dissociation energies of C-H and
C-C bonds in simple hydrocarbons . The compounds
and bonds discussed are : (1) methane (CH3-H, C-H,
CH2-H, and CH-H); (2) ethane (CH3CH2-H, CH2CH2
-H. and CH3-CH3); (3) ethylene (CHtCH-H. CHCH-H.
and CH2 =dH2>". *«* <*> •cetylene (QH-H. C2-H.
CH CHfandC2).
547
Textile Reaeardi In«. , Princeton, N J.
THERMAL EXPANSIOl (XEFFIQENTS AND THE
STRUCTURES O^ POLYMERS, by AUsoa Sutherland,
JwnesH. Wakeliil. and Howard J. White, Jr. Techni-
cal rept. no. 20 qn Contracts Nonr- 09000 and Nonr-
09001. May 60. 56p. 43 refs. AD- 236 670.
Orter from LC mi$3. 60. ph$9. 30 PB 147 170
X-ray diffraction Imeasurementa were made of the
linear thermal extiansion coefficierts of high polymera
The changes In the lattice parameters of crystallized
material and in tl»e interchain separation of disordered
material were noted. Measurements of the angle of
the diffraaed beani were obtained from X-ray dif-
fractometer traces of patterns from polymer fiber
bundles and filma at temperatures from -196°C to
room temperature . Tabulation of thermal expansion
coefficients showed that contraction is first observed
at a temperature dependent on the looseness of inter-
chain bonding. It was thought that contraaion might be
associated with transition to hexagonal packing d the
chains, but can apparently result at lower tempera-
tures, before rotational modes are excited. Studies
were made of the ichange in thermal expansion values
for the three crystal lographic directions with tem-
perature, mechaitical strain, and intracrystalline
swelling.
University of Southern California. Los Angeles.
NEW APPROACHES TO THE PHOSPHINOBORINE
POLYMERS, by Anton B. Burg and Peter J. Slota, Jr.
Technical rept. np. 6 on Contraa Nonr-228(l3) and
rept. on Contraa AP 33(616)2743. 1 Nov 59, I5p.
17 refs. AD- 228 ^50.
Orxler from LC mi$2. 4a ph$3. 30 PB 150 520
The trlmer (Me2PBH2)3 was made in 52% yield by the
reaction d Me2P0Cl with NaBHf in diglyme. The re-
action of E12PCI with NaBH^ in diglyme gave an air-
stable oil appearing to be (Et2PBH2)3; and admixed
EtPC92 ^^ ^^ similar material presumed to contain
P-H bonds. Thei^al decomposition cA such material
yielded H2. the etSiylphosphines. (Ei2PBH2)3 snd
boron-rich residues. The adduct Me2NPMe2- BH3
(m. p. 12°; b. p. e#t. 21 1°) decomposed above ibOP to
give H2, amlnoborines. Me2PH. (Me2PBH2)n (23%,
nnostly trlmer), the rare biphosphine P2(C5^3)4 (20%)
and non -volatile [B3H5(Me2P)2Me2Nlx, having soft-
plastic character. The solid adduct Me2NPMe2(BH3)2
above 200° gave 82- Me2PH, aminoborines
(Me2PBH2)3 (over ,50% yield) and thermoplastic mate-
rial wherein B atcins outnumbered the basic units at
least two to one. The plasticity and high thermal ata
bility of such materials can be explained in terms erf
a boron -hydride network structure which is rendered
opener but less labile by entrapped basic units.
(Author)
Ptiysicat Chemistry
Aerojet -Genera]] Corp. , Azusa, Calif.
RESEARCH (M ELECTROCHEMICAL FUEL CELLS,
by M. J. Cramer, S. B. Kllner, and E. M. Langworthy.
Rept. for 15 Nov |1-10 Aug 56 on Contract N7onr-
46207. 24 May 57, decUssifled. 82p. 13 refs. Rept.
no. 1233 (Final); AD- 133 949.
Order from LC mi$4.80, ph$13.80 PB 155 002
This report released for sale to the public 16 Mar 61.
The general purpose has been to determine the feaai-
bility o< employing primary batteries as the prime
propulsion unit of undersea vehicles. A battery of tht
type developed during the program could be used to
power a submarine for a 1 to 2-week cruise at very
low noiae levels and without the necessity of surfacing
to recharge batteries. The zinc-chlorine electro-
chemical system was selected for intensive develop-
ment after an initial examination of potentially appU-
cable battery systems. The battery at the present
stage of development consists of a continuously fed,
gaseous chlorine cathode, and a zinc anode that is ia-
stalled at time of manufacture. The electrolyte is a
recirculated zinc chloride solution in sea water. Aux-
iliary equipment consists of the tanks, piping, valves,
and controls necessary to control the circulation of
electrolyte and chlorine to the banery proper. During
the exploratory phases of this program, magnesium,
aluminum, zinc, many alloys of these metals, and hy-
drogen were studied as possible anode reactants.
Early battery designs were based on a moving-cell
system, by which a constant interelectrode spacing
was maintained as zinc was consumed by compressioa
of cell stocks. The present program has produced a
zinc-chlorine battery of praaical design. A specific
energy of 1/5 hp-hr/Ib is indicated.
Air Force Canibridge Research [Labs. ] Bedf(n-d,
Mass.
A REVIEW OF CHARGE TRANSFER PROCESSES
IN GASES, by S. N. Ghosh, W. F. Sheridan and othera
July 55, 30p. 48 refs. Geophysical Research Papers
no. 48: AFCRC-TR-56-205.
Order from LC mi$2. 70, ph$4. 80 PB 154 748
This report released for sale to the public 16 Mar 61.
A review is given of the nature and importance of the
charge transfer process (A'*" + B— >A + B"*") particularly
with regard to its role in ceruin chemical and physi-
cal processes. Experimental techniques for deter-
mining the charge transfer cross sections are dis-
cussed, with special reference to the recent method
whereb^ the number of ions due to charge transfer la
directly compared with that of the primary beam.
This technique has been utilized by the authors. The
cross sections obtained from experimental data in the
energy range 50 - 800 eV are discussed in some
detail. The data obtained by other investigators from
thernul energlea to 40 KeV are also presented. It is
shown that the adiabatic theory (Massey) satisfacto-
rily explains the charge transfer reaction for a large
number of simple atomic and molecular cases. How-
ever, certain very simple cases cannot be explained
in terms of this theory even by assuming excited
states or dissociation of the molecules by collision.
(Author)
Arizona State U. , Tempe.
THERMOELECTRIC MATERIALS AND DEVICE RE-
SEARCH, l^ B. R. Gossick and H. B. Whitehurst.
Quarterly progress rept. no. 3, 18 Mar- 17 June 60 oa
Contract DA 36-039- sc- 85249. [1960] Up. 3 refs.
AD- 243 115.
Order from LC mi$2. 40, ph$3. 30 PB 153 233
548
Methods are described which were developed for puri-
fication of the precipitated titanium dioxide used in
these experintients. The methods of preparing high
melting point metala in colloidal form is alao de-
icribed. together with the procedures which were
used to mix these particles into a matrix of titanium
dioxide. Theoretical consideration of the principles
involved in the electrical behavior of two phase sys-
tems is reviewed. The work being done on the sys-
tems for evaluation of the new materials is repcarted
lofetfaer with the experiments which were done to
Mtablish macroscopic metal to rutUe junctions.
(Audior)
Arkansas U. [F^retteville].
HIGH TEMPERATURE ELECTROCHEMISTRY, by
K H. Stem. Final rept. on Contract AF 49(638)653.
[19601 18p. 4 r«fs. AFOSR-TR-60-17LAD-248 496.
Orier from LC ml$2. 4a ph$3. 30 PB 153 827
RMaarch was carried out oa- (a) Kinetics of the re-
action between metallic silver and fused sodium chlo-
ride using both conventional and EMF techniques,
(b) Development of a chlorine reference electrode in
molten boric oxide medium, (c) Mechanism of the
thennal decomposition of potassium perchlorate.
Biophysics Lab. , Stanford U. . Calif.
PRECISION g-VALUE MEASUREMENTS ON FREE
RADICALS OF BIOLOGICAL INTEREST, by M. S.
Rials, H W. Brown, and J. E. Mallng. Rept. on Con-
tract AF 18(600)1511. Ai«60, 22p. 11 refs. B. L.
rept. no. 11;AF0SR TN-60-716.
Order from LC ml>2.70, phM 80 PB 152 961
Id previous work [Adams, et al. J. Chem. Physics
a, 774 (1958)1, it had been noted that g-values of
■emiquinones appeared to be different and to depend
upon features of molecular structure . Because the
loterpretatlon of experimental results when dealing
with biological free radicals would seem to lean
heavily upon correaly explaining the origin of g-value
differences, a systematic study of the g-values of
•emiquinone-free radicals and hydrocarbon Ions was
done.
Bureau of Mines. Bartlesville. Okls.
A NEW APPROACH TO THE COMBUSTION CALO-
RIMETRY OF ORGANOSILIOON COMPOUNDS. THE
HEATS OF COMBUSTION AND FORMATION OF
HEXAMETHYLDISILOXANE, by W. D. Good.
J. L. Lacina and J. P. McCullough. Technical note
on Contract CS0 59-9. Nov 60. 14p. 12 refs. ARPA
Order no. 24-59, Task 3; AFOSR-TN-60-1414.
Order from OTS $0. 50 « 171 528
A routing -bomb method was developed for the pre-
dalon combustion calorimetry of organosilicon com-
pounds. The standard heat of combustion of hexa-
methyldisiloxane was determined, and a tentative
value of the heat of formation was derived. An ex-
perlmenul method was found that may ultimately lead
to Impnrved values of the heat of formation of aqueous
fUioailicic acid solutions. More reliable values of
the heats of combustion and formation of benzotri-
fluorlde were determined. (Author)
Bureau of Mines , Pittsburgh, Pa.
THE PROCESS OF IGNITION BY HOT GASES, by
M. Vanpfe, A. E. Bniszak, and H. G. Wolfhard.
Rept . on Contract Nonr- 1 858(25) . Mar 60, 37p. 9 refi
Proj. Squid Technical rept. BUM- 29-P.
Order from LC mi|3.00, pH»6.30 PB 153 687
A detailed study of the process of ignition of explosive
mixtures by contact with hot gases is presented. The
ignition Is produced by a laminar Jet of hot nitrogen
issuing into a cold explosive mixture of carbon man-
oxlde and air . The ignition may be quenched by a cool
plate placed in the path of the Jet . a few centimeters
upstream of the nonnal point of igiUtion . A complete
exploration of the velocity, temperature and composi-
tion field is made in the Jet , which Is luminous . The
results indicate that: (1) in all the regions considered
the flow lines are vertical , with some divergence at
the edge of the Jet; (2) the temperature and velocity In
the center of the Jet renoain practically constant; and
(3) the luminous region is a region of combustion with
low fuel concentration and with d» point of maximum
reaction lying well within the hot Jet and moving
further toward the center with increasing height. A
method Is proposed for the determination of specific
reaction rates . The method is based on the applica-
tion of the heat equation (in its differential form) in
the central part of the Jet where the temperature of
the Jet remains constant with height. In this region all
the heat produced by chemical reaction is conducted
away in the radial direction and therefore the determi-
nation of reaction rates requires only the measure-
ment of the first and second derivatives of the tem-
perature profile in the vicinity of the center of the Jet.
(Author)
California U., Berkeley.
THE LIGHT-INDUCED cis -trans ISOMERIZATJON
OF NITROUS ACTD FORMED BY PHOTOLYSIS OF
HYDRAZOIC AOD AND OXYGEN IN SOLID NTTRO-
GBN, by John D. Baldeschwlder and George C
Pimentel. Rept. on Contract AF 49(638)1. 31 Aug 60.
30p. 20 refs. AFOSR TN-60-1018; AD- 246 358.
Order from LC ml$2. 70, ph$4. 80 PB 15S 051
Photolysis of hydrazolc acid in solid nitrogen at 20P K
with oatygen present yields both cis- and trans -nitrous
add. The identification is based on infrared detectioo
of features of the isotopicallv substituted species
HONO, DCWO, and HOI8NO18. The nitrous acid prob-
ably reaulta from the reaction of imidogen with oxygea
NH ♦ O2 ■ HCWO. Isomerizatloo of nitrous add oc-
curs in the matrix at 200K under the influence of irra-
diation. Ultraviolet radiation causes the trans- to cis-
rvaction, probably by electronic excitation to give a
random mixture of the two forma. Near infrared rm-
dUtion reverses the reaction but the role of the radia-
tion is not known. Bulk besting of the sample Is not
Involved and a broad range of near infrared frequen-
cies is effective. No Isomerizatlon of DONO could be
detected and HO^^nq^S seemed to isomerize more
slowly than did HONO. (Author)
549
California U. . Bfcrkeley.
THE NITRIC OXIDE -FLUORINE DILUTE DIFFUSION
FLAME, by Donald Rapp aivl Harold S Johnaton.
Pinal rept. on Cofitract Nonr- 222(56). 10 Mar 6a 20p.
19 refa. AD- 233 316.
Order from LC it4$2. 4a ph$3. 30 PB 153 764
The dilute diffusion flame method for meaauring the A
rates of fast gas teactlons were used to study the re-
action: 2NO + F2 •20NF. The reaction proceeded with
the emission of visible light, and photographic meth-
ods were used to pbcaln concentration profiles in space.
With a reasonable assignment of rate constanta for
succeeding steps, it is shown that the experimentally
measured race constant can be interpreted as the rate
constant for the first step in this mechanism. The rate
cooatant was determined at room temperature aixl at
dry-ice tennperanire, and is given by. K "6 x 10^^
exp (-1500/RT) cc/mol-sec. The probable error in
the activation is estimated to be 1000 calories, so that
the activation energy for this reaction is limited to the
rai^e 500 to 2500 calories. Calculation at the theo-
retical pre -exponential factor showed the direct one-
step termolecular reaction to be too slow by many
orders of magnitude to account for the observed rate
constant. It is estimated that significant quantities of
fluorine atoms are produced in this system, and the
radiative lifetime of ONF* is approximately 10 msec
California U [Berkeley).
PROCEEDINCS Op CONTRACTOR'S MEETING ON
AIRBREATHING COMBUSTION [NO. 4 J. Rept. on
Contract AF 49(6^8)166. Oa 60, 18p. AFOSR-TN-
60-1253; AD- 247 033.
Order from LC inl$2.40, ph)3. 30 PB 153 448
T
Contents;
E)evelopment of detonation
Combustion in thei vicinity of a hypervelocity missile
Standing detonation wave
Recent results on standing detonation waves
Supersonic combustion, by W. Koffer
Supersonic combustion, tqr G- Dugger
Pinch induced chemical reactions
Investigation of screeching combustian and preasure-
wave flamefront interaction
Natural convection above open fires
Theoretical research in combustion aerodynamics
Interactions among burning fuel droplets and their
effects on combustion stability and roughness
Properties at iona in flames
Thermal decomposition and related reactloos at
organometallic compounds
Chemical Engineering Lab. . Princeton U. . N. J.
SURFACE RECOMBINATION OF HYDROGEN
ATCMVfS IN THE PRESENCE OF WATER VAPOR, by
E. J. Nowak, S. I^urzlus and others. Rept. on C<»-
iraa AF 49(638)32 [1960] 19p. 10 refs. AFOSR-
TN-60-1302; AD- 247 517.
Order from OTS 10.50 PB 171 512
The probability y Ol reconibinatloQ of hydrogen atoms
on Pyrex glass hat been m— wirrrl between 390 and
*60^. The (^ta tre repr— — ted by the expression
t =2.6 • 10-2 exD-(E/RT) where E = 9 kcal/g-mole.
The measuremenqs were nnade in the presence of
water vapor . These rates of recombination are
slower by more than three orders of magnitude thaa
correspaoding rates on Pyrex in the absence o< water
vapor. There results demonstrate unequivocally for
the first time that water vapor poisons glass walls for
the recomtnnation of hydrogen atoms . (Author)
Florida U. Engineering and Industrial Experiment
Station, Gainesville.
FLUOROCARBON NF COMPOUNDS, by J. A. Young
and R. D. Dresdncr. Quarterly technical rept. no. 5,
1 July-30 Sep 60. on Contract DA 01-009-ORD-772.
[1960] 7p. ARPA Order no. 40-59, Task no. 3.
Order from LC mi) 1.80. pi4 1.80 PB 152 409
At least one represenutlve of a new class of fluoro-
carbon compounds has been synthesized, the reacdoo
between CF3COCI and the mercury derivative of N,N'
-t>i« (trlfluoroacetyl) hydrazine giving a good yield of
(CP2lCO)M2- N-Acetylperfluoroglutarlmlde,
CF2(CF200^2^*^0*^^3' "^^y *^^° *^^* '**" obtained.
Attempted alkylation of an N-bromoamide by use of a
fluoroalkyl mercurial failed, a fluorocarbon bromide
being formed by combination of the positive bromine
with the fluoroalkyl group. Several Quorocarbon
iminosulfur dlfluorides , RpN- SF2, have been made
for fluorinarion studies . First results indicate that
their reaction with AgF2 is surprisingly slow aad thft
no NF compounds were obuined . (Author)
Frlck CSiemlcal Lab. , Princeton U. , N. J.
THE INFRARED SPECTRUM AND FORCE FIELD OP
CRYSTALLINE HYDROGEN PEROXIDE» by
R. L. Miller (Doctoral thesU, Brown U. ) and
D. F. Homig. Technical rept. no. 4 on Contract
Nonr- 1858(27). 15 Apr 6a 26p. 26 refs. AD- 235 769.
Order from LC ml$2.70. ph$4.80 PB 154 1Q9
The Infrared spectrum cf crystalline and vitreous
hydrogen peroxide was studied from 300 cm' to
4000 cm-1. A normal coordinate analysis of the tetra-
gonal crystal with four molecules per unit cell is given.
The hydrogen bonds are only slightly weaker than in
H2O but the 0-H Line widths are only 80 cm'^. From
the coupled motion of the torsion and the high fre-
quency libration. thetorsionalfrequency inthegasis
estimated to be about 230 cm~l. (Author)
Fulmer Research Inst. , Ltd. (Cit. Brit. ).
MEASUREMENTS OF THE HEATS OP FORMATION
OF INORGANIC FLUORIDES ESPEQALLY THE
ELEMENTS OF ATOMIC NUMBER BELOW 2a by
P. Gross, C Hayman and others. Pinal technical reft
for 1 Nov 59-31 Oct 60 on Contract DA 91-591-EUC-
1316. 23 Nov 60, 32p. 12 refs. R. 146/4; AD- 247 281.
Order from LC m43. Oa ph$6. 30 PB 153 445
The heats of formatioo of phosphorus pentafluorlde ud
boron trifluoride were determined calorlmetrically bj
combustion of the elements in fluorine at 25°C. In the
case of boron, preliminary experiments indicated thit
spontaneoua bunting of the fluorine did not take place
at room temperature. A small quantity of sulphur
which Ignites spontaneously in fluorine was therefore
used to initiate the reaction. Extensive studies have
550
also been made towards establishing a suitable experl-
giental method for the combustion of beryllium in fluo-
rine under conditions which can be applied in calori-
metric measurements of the heat of reaction. (Author)
Gates and Crellin Labs, of Chemistry, Calif. Inst.
of Tech., Pasadena.
SMALL- RING COMPOUNDS. XXVUl. ISOTOPE -
jOSrriON REARRANGEMENTS OF ALLYLCAR-
BNYL GRIGNARD REAGENTS, by Marc S. Silver,
pfeul R Shafer and ahers. Technical rept. no. 8 on
Contract Nonr -220(26). Mar 60. 6p. 3 refs.
AD- 235 340.
Order from LC mi$l . 80, ph$l . 80 PB 153 812
Presented in part at the Sixteenth National Organic
Symposium. Seattle. Washington, June 15, 1959.
Gates and Crellin Labs, of Chemistry, Calif. Inst.
of Tech. , Pasadena.
SOME IODINE ATOM RECOMBINATION RATES BY
PLASH PHOTOLYSIS, by Rolf Engleman, Jr. and
Norman R Davidson. Rept. on Contract [Nonr-
220(01)1. [1959] 22p. 16 refs.
Order from LC mi$2.70, ph»4.80 PB 152 102
The rate constants of the homogeneous gas -phase
iodine atom recombination have been measured by
flash photolysis in the presence of several third body
gasA. Hydrogen, helium, benzene, and methyl iodide
have been studied as third body gases at several tem-
peratures between 323 and 548<^. , and their third
order rate constants aj-e 1.41 x 109 (298/T)0-80 ,
4.93X 109(298/T)1 '♦0. 1.00 x 10^^298 /T)^^^, and
1.50 X 10^1 (298/r)3-24 liter82 moles-2 seconds" 1,
respectively. Ethyl iodide, hydrogen iodide, and car-
bon monoxide were used at 323<^. aitd yielded
2.38 X lOll. 2.81 X lOlO, and 5. 42 x 109 liters2
motes -2 seconds' 1, respectively. Limited experi-
ments were made with nitric oxide as a third body gas.
The recombination rate was afiparently too fast to
measure with this apparatus, but an apparent lower
limit of 1.8 X 10^^ liters2 moles"2 seconds'^ was
established. (Author)
Hebrew U. Osrad)-
THE RADIATION CHEMISTRY OF CHLOROFORM
SYSTEMS, by Gabriel Stein, M. Ottolenghi and
I. Eliezer. Rept. for Jan-Dec 59 on The Chemtistry
tnd Physics of Materials , Contract AF 61(052)224.
Sep 60, 25p. 8 refs . WADD Technical rept. 60-668.
Order from OTS $0.75 PB 171 497
A dosimeter based on solutions of blallyl in chloror
form is developed . TTie radiation chemistry of pure
H2O and Oo free chloroform is investigated and all
products i<Kntified. A reaction mechanism is derived.
(Author)
Hughes Aircraft Co. , Culver City, Calif.
RESEARCH ON HIGH TEMPERATURE POLYMERS,
by J. B. Rust. C L. Segal, and H. H. Takimoto.
Technical rept. no. 3. 1 Mar-1 Sep 59, on Contract
Nonr 2540(00). [1959] I23p. 30 refs. AD- 235 020.
Order from OTS $2. 75 PB 171 522
Syntheses and characterizations were conducted on:
(1) poly(triorganometalloxy)metalloxane polymers,
and (2) poly(chelated)metalloxane polymers. A large
batch of a poly(trimethyl8iloxy)titanoxane polymer
was prepared which is soluble in polar solvents di-
methylformamlde and MeOH, and non-polar solvents
benzene, toluene, and CCL4, The molecular weight
was determined from light scattering measurements
of the polymer in CCI4 solution to be 26, 000. Films
of the polymer were prepared by evaporation of sol-
vent or fusion of the solid resin. Synthesis <rf the tri-
phenylsiloxymetalloxane polymer was approached by
the isolation of bi8(triphenyl8iloxy)dialkoxy deriva-
tives of Ti, in which the alkoxy groups were either
pentoxy, heptoaty, benzyloxy, or phenoxy, in addition
to the Isopropoxy derivative. Reaction of bi8(tri-
phenylsiloxy]idiisopropoxytitanium with diphenyldiace-
toxysilane resulted in a fusible, soluble polymer,
from whose melt a fiber could be drawn. Syntheses
of polymers with a quartz- like structure were also
conducted. The chelated metalloxanes, with maxi-
mum coordination number internally satisfied, were
prepared by the alkoxyacyloxy reaction of the corre-
sponding di- or tri -chelated derivatives <rf Ti or by
their controlled hydrolysis.
llllncris U.. Urbana.
SELF-DIFFUSION OF THE CHLORIDE ION IN SO-
DIUM CHLORIDE, by Neal Laurance. Technical rept.
no. 4 on Physics of the Solid State, Contract Nonr-
1834(19). Jan 60. 51p. 43 refs; AD- 231 346.
Order from LC ml$ 3.60, ph$ 9. 30 PB 152 884
The self -diffusion coefficient of the chlorine ion has
been measured in pure sodium chloride crystals and in
sodium chloride crysttls doped with calcium chloride.
The measured diffusion coefficient can be expressed
as D« 56.6 exp (-2.12 ev/kt) between 520^0 and 740OC
for pure sottium chloride . and D = 1280 exp (-2.49
ev/kT) between 5850C and 730^0 for sodium chloride
crystals containing 0.05 mole % calcium. The units of
D are cmVsec . The diffusion coefficient of chlorine
has been measured at constant temperature as a func-
tion of calcium concentration. The results are not
expressible by a simple relation, but they indicate
that the diffusion coefficient is lower in crystals con-
taining calcium than in pure crystals by a factor of
from 5 to 10. and that the diffusion coefficient is insen-
sitive to the magnitude of the calcium concentration.
H is concluded that the nnotion of free negative ion va-
cancies , while adequate to explain the observed diffu-
sion coefficient in the case of pure crystals , fails to
explain the observed dependence of the diffusion coef-
ficient on calciuni coi»centration . The iiKCion of va-
cancy pairs is examined as' a mechanism for diffusion,
and it is concluded that unless the theoretical treat-
ment of the vacancy pair has been grossly inadequate
the observed temperature dependence of the diffusion
coefficient of chlorine in both pure and doped crystals
precludes the motion of vacancy pairs as a possible
mechanism of diffusion. The details of the penetration
of the isotope into the crystal exclude any effects due
to dislocations lines which are long compared to the
penetration disunce . (Author)
551
Illinois U. Engineering Experiment Station, Urbana.
THERMOELECTRIC PROPERTIES OF MAGNESIUM
TITANATES, by Stuart Maurice Myron. Thetis.
Technical note on Contract AF 49(638)212. 10 Nov 60.
69p. 6 reft. AFOSR-TN-60-118& AD-248 554.
Onler fran LC nit$3. 90, pti$10. 80 PB 153 836
Sintered ditc-sha^ tamplet of three magnesium titan -
ate« were partially re<kiced by heat treatment in hydro-
gen. The values at electrical resistivity, thermo-
electric coefficients, and donor concentration were de-
termined in dependence both of degree of reduction and'
of temperature. Linear, logarithmic relations were
established berwe«n these quantities. Moderately large
thermoelectric coefficients were found but the corre-
lated electrical rosistlvltles were too high for technical
applications of thase materials for power generadon or
for refrigeration. (Author)
latltuto dl Pialoi) Superiore. Univeraita dl Ptvia
RECENT RESULTS ON NUCLEAR MAGNETIC
RELAXATION, by G. Bcxiera. L. (3iiodi and others.
FlMil technical rept. for Mar 59- Feb 60 on Contract
DA91-591-EUC-K)S8. Feb 60. 39p. 6 reft,
AO-234 9ia
Order from LC mi$3. 00. ph|6. 30 FB ISO 063
Theoretical work Was conducted on an adlabaticpast-
ages picture In nutlear magnetic resonance with the
routing coordinate method. Experimental work was
concerned with the comparison between the longitudinal
and transversal relaxation time in some pure liquids.
Results recently dbtalned with nuclear relaxation in
colloidal solutions are reported. (Author)
Lockheed Aircmft Corp. , Sunnyvale, Calif.
ALUMINUM HYDRIDE: A LITERATURE REVIEW,
by C J. Hcrffman. Technical note on Chemistry.
A\ig 60. 2lp. 31 refa. LMSD-70315O; AD-244 583.
Order from GTS l|0. 75 PB 171 534
The existing unclatssified literature pertaining to
aluminum hydride has been reviewed. Methods of
preparation, the physical and the chemical properties
are discussed. A number of thermodynamic vaiues
have been estimated for the monomeric form of alu-
minum hydride. (Author)
Michigan U. C>>|1. of Literature, Science, and the
Arts, Ami Arbor.
MOLECULAR FRAGMENTS IN SHOCK WAVES, by
R. Stephen Berry, i Final rept. on Contract
AF 49(638)538. Aug 60. 35p. 24 refa. 02878-1-F;
AFOSR-TR-60-118; AD-244 842.
Order from LC ml$3. 00, pb$6. 30 PB 152 612
The following war|c is described: (1) the design of an
apparatus used fof absorption spectroscopy of mate-
rials behind shock fronts, with proviaion for multiple-
pass optics; (2) preliminary results based on shocks
through alkali halUdes, giving evidence of dissociation
and formation of (diatomic alkali metal van der Waals
molecules; (3) results on the fragmentation of dl-
borane behind shock fronts, showing the formation,
possibly, of an unstable polyatomic intermediate, then
BH and finally polymeric species; and (4) preliminary
results of flash photolysis of benzene, 2-dlazonlum
car boxy late, directed toward the identification of
benzyne, C^H4. (Author)
Massachusetts Inst, of Tech., Cambridge.
HYDROGEN PEROXIDE LABORATORIES. byC. N.
Sanerfleld . Quarterly periodic status rept . on Coo-
tract N<»r-184l(ll). 31 Mar 60. 13p; AD-235 699.
Order from LC miJ2. 40. ph$3. 30 PB 153 769
Hydrogen peroxide decomposition flame: Measuremctt
were made of the burning velocities of H2O2 vapor at
a function of vapor concentration at atnx)SjMieric pres-
sure. Thermocouple measurements of the vapor in a
burner tube confirmed the previous belief that the tem-
perature of the vapor between the bottom and top of the
tube does not differ by nwre than 2% and that the va-
por at the top is normally superheated by 79 to ^PC
according to the heat input to the superheater. Poroui
walled reactor studied: Experiments were conducted lo
a porous suinless steel reactor using various flow
conditions . Trial runs with H2O2 in N were made widi
the main stream introduced near the middle of the re-
actor. Decomposition of H2O7 vapor on catalytic sur-
ace^: "fhe rate of decomposition of H2O2 vapor on a
Ag tube decreased with time, while there was an in-
crease of reaction rate on the surface of a Cu tube.
Other experiments demonstrated the increase with
time of the caulytic effect of Cu . Decomposition of
tJ[2Q2 vapor on relatively inactive surface_^: Expefl-
ments in a 304 stainless steel tubular reactor using N
as the carrier gas showed no dependence of H2O2 de-
composition rate on the flow rate of the gas steam .
This indicated that the decomposition rate was not
mass transport controlled. The H2O2 decomposition
rate was dependent on the concentration of H2O2 but
not that of O or H2O .
Mellon Inst. . Pittsburgh, Pa.
SOLID STATE VIBRATIONAL SPECTRA OF THE
METHYL AND METHYL -d3 HALIDES. by Marilyn
E. jacox and Robert M. Hexter. Rept. on Contract
AF 49(638)542. 1 Nov 60. 27p. 15 refs. (AFOSR)
TN-60-1420: AD-247 745.
Order from LC mi$2. 70, ph$4. 80 PB 153 54*
The vibrational fundamentals of solid CH3CI. CH3Br,
aixl CH3I and of their fully deuterated counterparts
have been examined at 77(1C under high resolution.
CH3C1^ has been synthesized and its W3 spectrum
compared to that of ordinary CH3CI, permitting the
assignment of the CH3CI35 and CH3CI37 contributions
in the V3 multiplei structure. The relative intensi-
ties of absorption in 1: 1 CHsXrCDjX solid solutions
have been nneasured to test the relationship between
splitting, frequency, and absorption intensity pre-
dicted by the dipolar correlation model. The test
proved to be insensitive. A study of theV3 absorp-
tion of each component in CH3C1:CD3C1 solid solu-
tions throughout the concentration range has show^
that multiplet splitting persists at concentrations aa
low as 1%. (Author)
W
fx m:
S52
Metal Hydrides . Inc . . Beverley, Mats .
ATTEMPTED SYNTHESIS OF BERYLUUM HYDRIDE,
by Jbhn C . Powers , Donald W . Vose , and Edward A .
Sullivan. Rept. for June 58-July 59 and May-Aug 60 on
Materials Analysis and Evaluation Techniques ,
CooOKt AF 33(616)5847. Oct 60, 35p. 12 reft.
WADD Technical rept. 60-543.
Order fromOTS$ 1.00 PB 171 489
The direct synthesis of beryllium hydride from the ele
ments was attempted in two sets of equipment designed
to grind beryllium metal while subjected to heat and
hydrogen pressure. Grinding action was supplied by
mechanisms which provided the reaction vessels with
either reciprocating vertical moticm, or motion in
which the reactor's horizonul axis described a circle.
The ability of both mechanisms to grind meuls satis-
factorily was demonstrated in test runs , in which mag-
nesium hydride was synthesized. However, beryllium
hydride was not prepared by this method, even when
catalytic additives were used. There were no indica-
tions even of partial hydriding. Operation with beryl-
lium, which is highly toxic, was carried out safely by
conforming to recognized standards of industrial prac
tlce. (Author)
Naval Ordnance Lab. , White Oak. Md.
THE ENERGY OF INTONATION, by SigmundJ.
Jacobs. 17 Sep 56, 18p. 8 refs. NAVORD rept. 4366.
Order from LCmi$2. 40. ph$3. 30 PB 154 813
This repon released for sale to the public 16 Mar 61 .
The energy of detonation is calculated for a "ganruna
law" gas using two simple models for the hydrody-
namic problem. In the first a Taylor wave expansion
follows the detonation. In the second a piston follows
the detonated gas to maintain a constant pressure in
it. The energy distribution in the Taylor wave is found
for the case gamma equal to 3. It is shown that the
average energy release by the chemical reaction per
gram la given by: Cq - Pi/2(y - l)<<b where pi la the
C-J preasure and /^o Ib the initial loading density to
produce that pressure. The value of gamma, taken as
conaunt, can be evaluated from detonation pressure
data. These approximate results should be of use in
gaining an understanding of the disposition of energy
in a detonating charge of finite dimensions. (Author)
New York U.. N. Y.
BASIC RESEARCH IN X-RAY SPECTROMETRY
(2-12A), by Hartmut Kallmann. Quarterly rept. no.
12 (Pinal) 1 Dec 56-28 Feb 57, on Contract DA 36-
099-8C-56732. May 57, 29p. AD- 138 891.
Order from LC mi$2. 70. ph$4. 80 PB 150 895
Thla report released for sale to the public 7 Mar 61.
Samples which consisted of known amounts of Cu in
an Sn matrix were analyzed quantitatively by means
of X-ray spectrometry. The apparatus consisted of a
cooled photomultiplier tube with associated electronic
cui'rents, an analyzing crystal mounted on a goniom-
eter, alit collimators and X-ray equipment. Concen-
trations of 100% to 2%tu were detected. X-ray in-
tensities as low as 0. 23 quanta/sq cm/sec for Ni K
radiation (1. 65 A) and 1 quantum/sq cm /sec for sul-
ftir K radiation (5. 36 A) were measured. Sensitivity
decreased for softer X-rays because about 4000 e»
must be absorbed by the phosphor in order to release
one electron from the cathode of the photomultiplier
tube. The methods Investigated for the detection of
low intensities of soft X-rays were (1) through the
use of small photoconductlve crystals of CdS, (2) by
means of an ionization chamber, (3) by means of a
proportional counter, and (4) by scintillation. Vari-
ous phosphors were tested by irradiation with ameas
ured Intensity of As K-X-rays (10. 6 kv) and compar-
ing the relative efficiency of each. The effect of the
increase in ligjit emission by the phosphors when
irradiated by a constant intensity of X-rays was
studied. The increase was greater when the irradia-
tion was performed at dry ice temperature.
Pennsylvania State U. Coll. of Chemistry and
Physics, University Park.
THE SOLVATION OF AMMONIUM IONS AND THE
ACIDITY FUNCTIONS Hr AND Hq. by Robert W.
Taft, Jr. Technical rept. no. 25 00 Contract Nonr-
656(05). Mar 60. 8p. 8 refs.
Order from LCmiJ 1. 80, ph$ 1.80 PB 153811
The effects on addlty of (1) solvation of ammonium
ions and hydronium ion by H-bond formation and (2)
acidity functions. Hq and Hr. were wudtted; these 2
topics appear to be closely related. The Hq and Hr
functions differed markedly even in dilute acid solu-
tion. Experimental evidence indicates that the R"*
species solvate normally in much the same manner as
quaternary aBtyl anunonlum ions, R4N''r Abnormal
interactions were appeared to be generally involved
with BH* species. In the region 44 to 64 wt-% H2SO4.
a closely linear relationship exists between (Hr-H©)
and the activity of H20(-lbgaH20) From 60 to 75
wt-56 H2SO4, the slopes of (Hr-Hq) vs log aH20 i«
cinrved. In the acidity region below 40 wt-% H2SO4 the
slopes are curved. The results suggest that with an
abundance of available molecules, additional H-bonding
interactions of weak and variable strengths occur
with BH^ (H20)n. ROH. and B.
Rensselaer Polytechnic Inst. , Troy. N. Y.
IONIC NATURE OF MOLTEN SALTS, by George J.
Janz. Final rept. on Contract AF 49(638)50. Dec 60.
17p. 12 refs. AFOSR-TR-60-176.
Order frtMn OTS $0. 50 FB 171 535
Techniques and apparatus are described for the pre-
cise simultaneous measurement of surface tension
{y), density (d), and viscosity (^) of melts up to
lOOOOC, and for the measurement of electrical con-
ductance (>^KC1. a completely ionized melt, has an
»2 of 1.21. ay of 98. 4. ad of 1.977. andaAof 114.
Li2C03 melts to form a liquid with a d of 1. 812, a y
of 240, and a-Aof 99. a HgBr2 shows a d of 4. 41, an
yj^of 2. 52, and a Aof 10-2; the liquU is essentially
molecular and only inclpently ionized. The-Arfif an
infinitely dilute solution is 1 15. 03 for LiCl. 126. 45
for Naa. and 149. 86 for KCl. TheAof a 0. 1 H
aqueous solution is 95. 86 for LiCl. 106. 74 for NaCL
and 128. 96 for KCl. TheAof the molten salt is 170
for LiCl, 143 for NaCl. The pure molten n>elt corre
sponds to a state in which the solvent to solute ratio
is 1. 0/o». A comparison ofAvalues for a aeries erf
alkali halides and carbonates in the molten state
553
shows that molten carbonates form molten highly
Ionized electrolytes. The carbonate ion CO3 con-
tributes a signlflcsnt pert to the process at charge
tranapon in molttn carbonates. The fraction of cur-
rent transported respectively by cations (t+) and
anions (t*) in aqueous solutions is 0. 4643 and 0.5357
for AgNOj, 0. 3963 and 0. 6037 for NaCl. and 0. 48
and 0. 52 for PbClg. In fuzed salts these values are
0. 75 and 0. 25 for AgNOa. 0. 76 and 0. 24 for NaO.
and 0. 35 and 0. 63 for PbCl2- (Se« «i80 PB 149 436.
PB 151 171, PB 1)1 429)
-I
iSiemii
TheOTetlcal Cheiiistry Lab. , U. at Wisconsin,
Madison.
INTERMOLECULAR POTENTIAL FUNCTIONS FOR
NONPOLAR MOLECULES, by Daniel D. Konowalow
and josepbO. Hlr$chf elder. Rept. on Contract
AF 33(616)7174. Dec 60. 39p. 41 refs. ARL Tech-
nical noce 60-158.
Order from LCml$3. 00. ph$6. 30 PB 153 114
I
The Morse pocentlal function is used to represent the ^
intermolecular potential for several nonpolar sub-
stances The pocantial constants are determined from
a combinatian d qrystal structure and second vlrial
coefficient data for Ne, Ar. Kr, Xe, CH4. and N2.
Over a wide temperature range the t^jeoretlcal second
vlrial coefficients cJetermined from the Morse poten-
tial for these substances agree very well with experi-
mental dau and are qiiite comparable with calcula-
tions using the Buckln^m (exp-6) or the Lennard-
Jones (12-6) potentials. For Kr, it is foiaid that the
agreement with the experimental second vlrial coef-
ficients la greatly Improved by dividing the inter-
molecular potential into two separate Morse functions^
one applicable where the potential Is negttlve and the
other applicable where the potential ia positive.
(Author)
University at Southern California [Los Angeles].
COMPUTER SIMULATION OF AGGREGATE FOR-
MATION, by Marjorie J. Void. Technical rept. no. 5
on Particle Interactions in Colloidal Systems in Non-
Polar Media. Contraa DA 04-495-ORD-1296. Ai^ 60,
20p. 4 refs. OOR; rept. 1923. 5-C; AD-241 824.
Order from LC nii$2. 40. ph$3. 30 PB 153 667
Computer geoeraQed nrnxkel sediments d spherical
particles, formed by addition to the sediment at one
particle at a time appeared in previous work to be
adequate to represent the behavior of physical model
systems composeti of microscopic glass beads. How-
ever, sediment densities of seml-coUoidal silica in
hydrocarbon solvents are too low by a factor of ca. 30
to be represented by such a model. Observation sug-
gests that the model must take floccuiadon and aedi-
mentatloo into account simultaneously. In the work
reported here moCtel floes have been generated and
their shapes, structures and densities explored. Par-
ticle by particle addition to the floe was assumed. A
sediment formed 6n the previous pattern from these
floca rather than from primary particles is still more
dense than experimental sediments but by a smaller
factor (cs. 6). A tnore sophisticated model Is under
study. (Author)
University at Southern California. Los Angeles.
PROPERTIES OF SOLUTIONS IN THE NEIGHBOR-
HOOD OF THE CRITICAL TEMPERATURE OF
THE SOLVENT, by Sidney W. Benson. Charles S.
Copeland and others. Final rept. for 1 Feb 59-
I Nov 59 on Contract N6-onr-2381l. 1 Apr 60, 25p.
II refs. AD- 235 316.
Oixler from OTS $0. 75 PB 171 530
Contents:
Experinnental techniques and difficulties
Dielectric properties of H2O and EtOH
Fliue diagram for H20-NaCl
Conductance of NaCl-H20 systems, hydrolysis
Conducunce of HCI-H2O systems and observations
or Na0H-H2O
Conductance of Nal-EtOH system
Thermodynamic quantities, compressibility, partial
molar volumes, entropies, and enthalpies
Some empirical relationships, rectilinear laws for
2 -phase systems
Partial molar volumes of ions. (See also PB 135 729)
EARTH SCIENCES
CkMStal Studies tost. . Louisiana State U. . Baton
Rouge.
THE ROLE OF ALGAE IN THE FORMATION OF
BEACH ROCK IN CERTAIN ISLANDS OF THE
CARIBBEAN, by Robert W. Krauss and Raymond A.
Galloway (U. at Maryland). Technical rept. no. 11,
part E, on Caribbean Beach Studies, Contracts
N7oiir-35608 and Nonr- 1575(03). 20 Mar 60, 53p. 20
refs. Contribution no. 60-1; AD- 235 466.
Order from LC mlJ3.60, ph$9.30 PB 153 735
Notes on nxire than 80 beaches on Grenada, St. Lucia,
Guadeloupe, and Puerto Rico are accompanied by
comment! on algae and other organisms with particu-
lar emphasis on the role they play In forming and
modifying beach rock. It is concluded that algae are
not directly responsible for cementation of beach rock.
Incipient beach rock occurs in close association with
the water table in the sand at beaches, SpectrograpWc
and quantitative analyses are given for water, sand,
beach rock, and a sample of algal rock, from 7
beaches. OUoride and pH values are listed and cal-
cium content of inshore and offshore waers tabulated
for 17 beaches. The conclusions advanced have
general application in explaining beach rock origin
generally. A detailed transect and tables showing
relative abundance of various algae covering beach
rock are at interest from the standpoint of reel
origin. (Author)
Indiana U . Bloomington.
COMMERaAL GEOGRAPHY OF THE GRENADINES,
by Robert C Kingsbury. Technical rept. no. I on
Contract Nonr -908(1 3) May 60, 43p. 17 refs.
AD- 240 287.
Order from LC mi$3.30. ph$7.80 PB 149 321
"*€^'l^
•tPi.V lu,-: .-/ip
554
Climatology and Meteorology
Air Weather Service, Washington, D. C.
SEVERE WEATHER FORECASTING. 1 May 56, 152p.
Air Weather Service Manual AWSM 105-37, super-
sedes AWSM 105-37. Nov 52.
OttJerfrom LC mi$7.50. ph$24.30 PB 153 659
The purpose of this manual is to outline and illustrate
certain specialized methods and procedures used by
the Air Weather Service Severe Weather Warning
Center (hereafter abbreviated as SWWC). This outline
11 not intended to qualify the reader as an expert in
predicting severe weather, but rather, to provide
AWS forecasters and observers with a basic under-
lunding of how the severe weather warnings which are
transmitted on Air Force teletype networks in the
United Sutes are prepared. The techniques involved
In forecasting tornadoes are extremely deull«d . and
require the preparation of so many adaltlonsl charts
and analysis of so much dau that they are not recom-
meoded for normal weather station operational use.
. However, practicing forecasters nuy find guidaiKe
and help in this presenution, and the portions dealing
with methods of forecasting wind gusts , hail . and tur-
bulence, are sufficiently simplified so that they may be
•(kpted for routine use in most AWS weather stations.
(Author)
Olifomia U. . Los Angeles.
STATIC STABILITY MEASURES IN THE ATMOS-
PHERE, by W. Lawrence Gatea. Scientific rept. no. 3
on Dynamical Weather Prediction Project, Contnct
AF 19(604)4965. 31 Oct 6ft 25p. 23 refs. AFCRL-TN-
60-817.
Older from LC ml$2. 7ft ph$4 80 PB 153 745
Various measures ot static stability In the atmosphere
are reviewed and their uses briefly discussed. The
mean venical distribution of nine stability measures is
given for 100 mb troposfAeric layers, and for selected
stratospheric layers. The average geographical distri-
bution over the United States is also discussed and Illu-
strated for the measure -TSl 90/ dp. The seasonal
dlfferencea In stability distribution are discussed from
the January and July average dau for forty-five United
Sutes radiosonde sutions. (Author)
Imperial Coll. of Science and Tech. , London
(Gt. Brit.)
RAOAR ANALYSIS OF A HAILSTORM, by K. A.
Ipownlng and F. H. Ludlam. Technical (scientific)
note no. 5 on Contract AF 61(052)254. July 60. 107p.
28 refs. AFCRC-TN-60-426. AD -247 287
Order from LC mi$ 5. 70, phi 16. 80 PB 153 390
Observations of a summer hailstorm which travelled
■cross England from the SW were made with five ra-
dars and a dense network of ground observers . It is
ibown that In the Intense phase of the storm, when
2-inch hailstones fell, the radar echoes persistently
thosred some features from which the pattern of the
«lr flow in the storm can be deduced. According to the
analysis the updraught was composed of air which en-
tered the storm at low levels in a NE'ly current and
left it at high levels In a SW'ly curreitt. Strong wind
shear caused the updraught to be tilted at an angle of
about 45° to the horizontal . Precli^tation from the up-
draught Induced a downdraught In the region beneath
It; air entered the rear of the storm in the middle
tr^x>8phere, descended In the downdraught and left the
storm near the ground as a NE'ly current. It Is sug-
gested that In the presence of wind shear the down-
draught Is essential for the maintenance of organized
convection, and often alto for its establishment when
the instability is latent . The tilted Intense updraught
is favourable if not essential for the growth of large
hailstones . for the small stones which are carried for-
ward from the cloud tops descend and re-enter the up-
draught at low levels: in this way some cloud particles
can pass through the updraught twice or more, until
they reach the largest size which it can support.
(Author)
North American Aviation, Inc . , Downey. Calif.
STUDY OF BACKGROUND RADIATION AND HIGH
ALTITUDE WEATHER. Final rept. for 27 July- 22
22 Oct 54 on Contract AF 33(600)24347. Dec 54, 107p.
262 refs . WADC Technical rept. 54-581; AD- 54 347.
Order from LCml$5. 70, ph$16. 80 PB 154 808
This report released for sale to the public 16 Mar 61 .
A background radiation and high-altitude weather pro-
gram was instituted by the AF to annas s a body of
radUtion messuremems on sky background, to investi-
gate the literature in the high-altitude weather field,
and to summarize the state of present knowledge of
pertinent weather topics . Effon to a large extent was
directed toward the development of reliable measuring
equipment with which a mass of data can be gathered.
Information was recorded in the field only to the
extent erf proving the operabillty of the equipment and
of enabling a practical criticism of the methods of
dau reduction . The approach chosen in the spectral
intensity measurements was to build a radiometer,
and to achieve wavelength discrimination through the
insertion of selective filters In the beam . Spatial
variations are disclosed by a gradient meter, a spe-
cially deigned instrument for scanning backgrounds
m various patterns at a fairly rapid rate and with high
angular resolution. After the 2 Instruments were de-
veloped, it proved possible to combine them, creating
a radiometer-gradient meter . This device has 2 re-
ceivers in the focal plane, a set of filters which can
be employed at will, and scanning nK)tlons as desired.
In one mode of operation It measures the spectral In-
tensity of urgets; in the second nuxle, the Intensity
gradients . The literature study conulns information
on high-altitude clouds . water vapor, ozone, OO2,
and dust. (See also AD-44 372)
(^rtermaster Research and Engineering Center.
Natick, Mass.
CANAL ZONE ANALOGS IX. ANALOGS OF CAKAL
ZONE CLIMATE IN THE FAR EAST, by Robert L.
Anstey. Oct 60, 58p. 18 refs. Technical rept. EP-141.
Older from LCmi$3. 60, ph|9. 30 PB 153 427
The climate of the Far East is compared with that of
two locations In the Canal Zone: Balboa Heights , repre
senting the drier, leeward. Pacific side of the Isthmus
555
<rf Panama, aqd Cristobal, representli^ the wetter,
windward, Atlantic side. Areas o( analogy of pertinent
climatic elements and combinations of these elements
«re shown on piaps . The Far East does not contain
areas ot comnlete climatic analogy to either Canal
Zone station. Winter'temperatures are too low in all
parts ci the siudy area to show coincidence with the
three cllnutic elements normally used for comparison.
Nearly all a< <he study area is comparable with the
Canal Zone stations in respect to mean temperature of
the warmest month . Much of the lowland area of Japan,
Formosa , southern China and a small area in extreme
southern Korea have mean annual precipntation analo-
gous to Balboa Heights , but only five areas on the south^
east coast a€ Jkipan have mean annual precipitatioo
amounts which are analogous to Cristobal. Other cli-
matic elements , such as mean daily maximum temper
ature for the warmest nx>nth, and number at wet
nKxiths , show large areas with analogous , or greater
than analogous, conditions . Kftich of Japan and south-
em China are analogous to Canal Zone stations in
mean cloudiness of the wettest month and mean rela-
tive humidity of the driest month. Mean wiodspeeds
in the warmest month, n»an precipitation of the wet-
test month, and mean daily temperature range of the
warmest mortfc in nearly all of the lowland {»rtions of
the study area are analogous to Balboa Heights , but
only small areas are analogous to Cristobal. (Author)
(See also PB l43 281)
Stanford Research Inst. , Menlo Park. Calif
STUDY OF WEATHER STATIONS FOR ARMY USE.
PHASE IIL- DE$IGN GUIE«, by R. C. Goettelman.
F. L. Ludwig »nd others. Summary rept. on Con-
tract DA 36-03P-8C-78154. 30 Nov 59. 231p. 14 re<a.
SRI Project no. SU-2594: AD-234 194.
Order from LO mi$10. 20, ph$36. 30 PB 153 601
A guide was prepared for the design of 2 general
types ot automatic weather stations for Army use:
these are: (1) anuill, ponable (by 1 or 2 men) sta-
tions capable of sensing and telemetering b««ic
weather parameters, and capable of unattended oper-
ation for 1 or 2 weeks; and (2) large, research -type
stations, capafaie of sensing and telemeterii^ many
weather parameters of meteorological interest, and
capable of unattended operation for periods from 3
mo to 1 yr. Components are suggested which should
be capable erf reliable operation under many climatic
environments and which should provide reasonable
accurate and rapresentative data. Selections were
made based on |he following criteria: (1) commercial
availability or straightforward development require-
ments, (2) long-term reliability, and (3) low power
requirement. Over -all station configuration is dis-
cussed and schematic and block diagrams are pre-
sented to illustrate suggested solutions. Power
source recommendations are made. The necessity to
consider both etvlronment and logistics in choosing
power sources lor particular situations is discussed.
Power, weight, and volume estimates are made for
both types of stations. (Author) (Sec also PB 149 711)
Travelers Life Inaurance Co. , Hartford, Conn.
A MOVING- COORDINATE PREDICTION MOMIL
APPLIED TO EAST COAST CYCLC»<ES. by Frederld
P. Ostby and Keith W. Veigas. Scientific rept. no. l
on Contraa AF 19(604)5207, continuation of Contraa
AF 19(604)3877. Nov 60, 81p. 28 refs. AFCRL-TN-
60-675; AD-247 686.
Order from LCmi$4.80, ph$13.80 PB 153 550
A statistical prediction technique to forecast the betav-
lor of east coast cyclones is developed using multipk
linear regression analysis. The predictands are the
24- hr northward and eastward displacements of the
cyclone, the 24-hr change in central pressure, and iki
24-hr change in intensity. The sample consists of 35J
cyclone cases. A major feature of the technique is tte
a moving coordinate system is employed: the obsen^ad
and derived prediaor information is measured relattn
to the cyclone center rather than at fixed geographical
locations. (Author)
Weadier Forecasting Research Center, U. at
Chicago, IIL
A MOraPIED "SIGMA" SYSTEM OF COORDINATE^
by Wayne E. Sangster. Scientific rept. no. 1 on Coo-
trao AF 19(604)7230. Sep 60^ 75p. 12 refs. AFCRL-
TN-60-668. AD-247 338
Order from LC inl$4. 50, ph$12.30 PB 153 443
A coordinate system is presented in which the lowest
cocntlinate surface represents the topography of the
earth's surface. Higher coordinate surfaces reflea
this topography in diminishing degrees and become
Isobarlc at and above the 500-mb level. Some basic
equations of dynamic meteorology are derived In rermi
at this coordinate system. A numerical prediction
scheme using the primitive equations of motion and
this coordinate system is oallned. A method of reprr
sentlng the field of the horizontal pressure force in
the nonisobarlc coordinate surfaces, using geostrofAlc
stream and potential functions, is described. This
method is applied to a variety cf synoptic situatlcqs,
and the results are compared with the conventional
sea-level charts. The charts at the geostrophlc
stream and potential functions appear to give a more
accurate represoitation of the geostrophlc wind field
than do the sea-level charts. It is shown that an
appreciable diurnal variation of the geostrophlc wind
at the ground occurs over the Qreat Plains if the
diurnal temperature variation is large. Evidence it
presented to show that adlabatlc heating due to down-
slope motion may be a contributing factor to cyclo-
genesls in the lee o< the Continental Divide. (Author)
Wisconsin U., Madison.
SOME ATTEMPTS AT THE EXTRAPOLATION OF
STRATOSPHERIC PRESSURE PATTERNS USING
TROPOSPHERIC DATA, by Harold A. Corzine, Reld
A. Bryson and Lyie H. Horn. Scientific rept. no. 4
on Contraa AF 19(604)5191. Aug 60, 69p. 14 refs.
AFCRL-TN -60-642; AD-248 206.
Order from LC mi$3. 90. phJlOiSO PB 153 608
A mean 50 pib chart is obulned by extrapolating the
contour patterns at lower levels to the 50 mb level.
Orthogonal polynomials are used to describe the coa-
stant pressure charts at the standard levels from
556
1000 mb to 100 mb. The coeffidenta of the polynomi-
als are extrapolated to the 50 mb level and a mean
chart reconstructed from the extrapolated coeffl- 1'«
dents. Two methods of extrapolation are discussed.
One method consists of extrapolating the mean values
of the coefficients, while the second involves the ex-
trapolation of dally coefficient values which are then
tveraged to obtain a mean value. The polynomial
descriptions Indicated that the data period could be
itratifled into four types. The mean 50 mb chart of
one cf these types is otxalned using the two extrapo-
lation methods mentioned above. The relative merit
of the two tnethods is tested and discussed. (Author)
Wright Instruments, Inc., Vesul, N. Y.
A SURVEY OF PRESSURE AND DENSITY SENSORS
AND ASSOCIATED PROBLEMS FOR THE N.O.L.
HASP PROGRAM, by William Flnley Wrl^t. Final
rept. on Contraa NOL-N60921 -5608. Apr 59, I86p.
82refs. W. I rept. 4/59; AD- 21 8 681.
Order from LC ml$8. 40, ph$28. 80 PB 154 762
This repon released for sale to the public 15 Mar 61.
Contents:
Pressure, density and gas laws, and upper atmos-
pheric considerations
KAO atmosphere
HASP pressure cr density accuracy requirements
Radar accuracy
Wind determination drop sonde vehicle and fall rates
Aaalog vs digital recording
Laboratory calibrations
Sutic pressure defect
Pressure switches
Capacitance diaphragm transducers
loducunce diaphragm pressure transducers
Bourdon tube gage
Hjrpaometers
Glow discharge gages
Ionization gages
Thermal conduaivlty gages
Beu ray backscattering
Geodesy
Aero Service Corp. , Philadelphia, Pa.
[KVELOPMENT OF CHART REVISION PLOTTER,
by E. M Rhodes. Final technical rept. on Contraa
AF 33(600)33646. 28 Sep 59, 87p. 16 refs. RADC-
TR-59-219; AD-230 794.
Order from LC n\l$4. 80, ph$13. 80 PB 153 886
Tht approach to the solutions for a map revision in-
strument is studied. Results of the testing of a pro-
totype instrument are reported. Efforts were directed
primarily toward the solving of optical, rectification
•ad light transmission problems. (Author)
Institute of Geodesy, Photogrammetry and
Cartography, Ohio Sute U. Research Foundation,
Columbus.
ASSEMBLY OF GRAVITY DATA, by W. A. Heiskanen.
Rept. no. 11 (Pinal) on Contraa AF 19(604)1963.
Dec 59, ?5p. 85 refs. RF ProJ. 716-Final; AFCRC- .
TR-60-238; AD-238 248.
Order from LCmi(5.40. ph$15.30 PB 154 810
This report released for sale to the public 16 Mar 61.
Attention is given to the theoretical studies, the
practical procedure, and remiUs of the gravimetric
method. Maps showing the available gravity material,
the status of the isostatic reduaion, and the mean free
air anomalies of 5^X50 squares are Included. Three
graphs illustrating the development of the free air
gravity anomalies in spherical harmonics (Legen-
drians) to 8th degree for flattening values 1:297. 0 and
1:298. 3 are Included. (Author)
Oceanography
Dartmouth Coll . , Hanover , N . H .
DEVELOPMENT OF SURFACE MORPHOLOGY ON
FLETCHER'S ICE ISLAND, T-3, by David D. Smith.
Scientific rept. #4 on Contract AF 19(604)2159.
15 Feb 60, 77p. 17 refs. AFCRC-TN-60-437.
OrderframLCml$4.S0. ph$l2.30 PB 153 482
Fletcher's Ice Island, a mass of fresh-water ice adrift
in the Arctic Ocean, is composed primarily of Iced
fim which contains numerous elpngate, lensoid bodies
of old lake ice that formed during builflup of the parent
Ellesmere Ice Shelf. The parallelism of these bodies
Imparts a pronounced structural grain to the island.
Superposed on the two bedrock ifce types are large pads
of modem Ifke ice forn>ed after unusually short, cool
summers within the iMt 5 years . Ablation causes a
progressive, though non-cyclic sequential development
of surface forms characterized by repeated inversion
of relief. Ice units having higher albedo values and
more favorable crystal structure weather into promi-
nence. The surftice of the island has a gently undulat-
ing topography made up of numerous broad, parallel
ridges and intervening narrow but shallow vaUeys;
together, these forms comprise the fir<t order relief.
Second order relief features are present on the first
order ridges . lliese consist of 1) long narrow ridges
underlain by bodies of resistant old Uiie Ice, 2) inter-
ridge valleys and lowlands underlain by non-resistant
iced fim, and 3) mesa -like forms which develop on
the modem lake ice pads . A variety of third order or
microrelief forms are also present. First order
ridges develop in areas where resistant second order
ridges are concentrated; first order valleys form in
intervening areas where second order ridges are
more widely spaced . (Author)
Lamont Geological Observatory, Palisades, N. Y.
DREDGED GRAVELS FROM THE CENTRAL
ARCTIC OCEAN, by Walter Schwarzacker and
Kenneth Hunkins. Scientific rept. no. 2 on Contraa
AF 19(604)2030. Oct 60, 29p. 20 refs. AFCRC-
TN-60-258; AD-246 243.
Order from LC ml$2. 70, ph$4. 80 PB 153 076
SS7
A series of nine* bottom trawla was made in die Arctic
Ocean from Drtltlng Station Alpha. The trawls were
taken In the area between S4P and 850N and between
13«o and 1520Wj All the trawls produced high per-
centages at gra^l. Macroscopic and microscopic
analyses showed these gravels to be predominantly
sedimentary roclcs, few igneous or metamorphic speci-
mens were found. One fossiliferous sandstone speci-
men is Permocarboniferous in age. Bottom cores con-
tained simlllar pebbles at depths in the sediment of up
to 115 cm below the bottom. Studies of the striatlon,
roundness and shape of the pebbles reveal them to be
typically glacial i material which has undergone little
or no water transport, it is concluded that these
gravels have be«n rafted by ice from a shore contaln-
iag active glaclors. CooslderUions of Arctic Ocean
circulation. Pleistocene giidatlon and lithology make
it probable that the source area was Axel Heiherg
Island, Ellesmet^ Island or the northern coast at
Greenland. (Autfior)
Lament Geological Observatory, Palisades, N. Y.
SEISMIC STUDIES OF THE ARCTIC OCEAN FLOOR,
by Kenneth Hunkjns . Scientific rept. no. I on Contract o
AF 19(604)2030.; Oct 60. 34p. 9 refs . AFCRC-TN-60-
^7; AD- 246 243.
Order from LCtoi$3. 00, ph$6. 30 PB 153 075
Reflection and rffractlon seismic measurements from
Drifting Station Alpha in the Arctic Ocean have re-
vealed details of a prominent submarine rise, called
the Alpha Rise. This feature trends across the Arctic
Ocean subparaU«l to the Lomonosov Ridge. The mini-
mum depth sounded in its central portion was 1426
meters at S5P 03'N and 171° OO'W. The rise descends
to depths of over 3000 meters to the north and south.
Sub-bo«om reflections reveal a characteristic echo
from a depth of several hundred meters below the
ocean floor in the eastern area of the rise. This re-
flection is not prpoounced in the western area . The
eastern area als(> has a rougher bottom texture than
the western area,. Several short unreversed refraction
profiles were m^de . Dips and strikes of the ocean
floor from reflection records aided interpretation . An
average of three measurements shows the upper "un-
consolidated" layer to be 0.38 kilometers thick. One
profile revealed a 2.80 kilometer thick layer of
4.70 knVsec velocity. Below this lay the "oceanic"
layer with a velocity of 6.44 km/sec and an undeter-
mined thickness ^ (Author)
Pfiysks of fh« Atmotph«r«
t Ionic
Advanced Electronics Center, General Electric Co,
Ithaca, N. Y
A DETAILED DQSIGN STUDY FOR A TOPSIDE
IONOSPHERIC SOUNDER, VOLUME 11, by Leonard
C. Humphrey. Scjientiflc rept. na 1 on Contract
AF 19(604)7221. (5 Oct 60, 40p. 4 refs. APCRL-
TN-60-1125 (II). |AD-247 284.
Order from LC n^$3. Oa ph$6. 30 PB 153 399
This volume summarizes the design of a Topside
Ionospheric Sounder, detailed in Volume I (PB 153050)
and outlines an action plan for implementing the sat-
ellite and the necessary equipment for the ground
support complex. The Topside Sounder is an instru-
mented satellite system designed to make continuous
topside measurements of the entire ionosphere over
the earth. Tliis instrument fulfills the requirement
of an urgently needed basic research experiment and
is a high -potential tactical tool. Reconnaissance of
the upper ionosphere will make possible detection
and observation of remote electromagnetic disturb-
ances that are artificially as well as naturally in-
duced. (Author)
Avco-Everett Research Lab., Mass.
ABSOLUTE INTENSTTY OF NON- EQUILIBRIUM RA-
DIATION IN AIR AND STAGNATION HEATING AT
Hiai ALTITUDES; by J. C. Camm, B. Klvel and
others. Rept. on Contracts AF 04(647)278 and DA 1^
020-ORD-4862. Dec 59, 37p. 17 refs. Research reix.
93; AFBMD TR-60-184.
Order from LC ml$3.00, ph$6.30 PB 153 569
An attempt to obtain the magnitude erf the non-equilib-
rium radiation behind a normal shock in air is re-
ported. It is noted that the high non- equilibrium tem-
peratures force one to extend studies further into the
uv and ir than required for equilibrium predictions of
significant sources at radiation. For example, to
ascertain that the total non- equilibrium radiation is
less than I w/cm2 requires measurements from sev-
eral hundred angstroms to more than 10 microns.
Measurements covering much d this region using:
(1) monochromator and photocells, (2) bolometers, (3)
photoelectric detectors, (4) spectrographs and, (5) ir
photocells, are reported. At 23, 000 ft/sec the radia-
tion integral normal to the shock is about 0.4 watt /km'
steradian and most of the radiation originates within
5 cm of the shock front. We also report on calcula-
tions which show that the effect of ambient atomic ox-
ygen at high altitudes does not introduce any pro-
nounced changes. Application of the results to the
problems of satellite heating is made. (Author)
California U. , Los Angeles.
SOLUTION OF RADIATIVE TRANSFER IN AN INFI-
NITE SCATTERING MEDIUM ILLUMINATED BY A
POINT SOURCE, by Jacqueline I^enoble. Scientific
rept. no. 6 on Light in the Atmosphere, Contract
AF 19(604)2429. Oct 60, 14p. 1 refs. AFCRL-
TN-60-816. AD-248 028.
Order from LC mi$2. 40, ph$3. 30 PB 153 S66
The method of expansion in series of spherical har-
monics Is applied to the problem of radiative transfer
In a scattering medium homogeneous and Infinite, il-
luminated by an isotropic point source. Starting with
the solution of the problem of neutron transport with
spherical symmetry and without source, a very simple
formula for the diffuse luminance is given. (Author)
558
Electrical Engineering Research Lab., U. of Texas,
Austin.
gOLAR EMISSION AND ATMOSPHERIC ATTENUA-
TION BETWEEN FREQUENCIES OF 100 AND 114
ICMCS* by C. W* Tolbert, L. C Krause, and
W. W. Bahn. Rept. on Contraa AF 19(604)2249,
20 Oct 60, 29p. 13 refs. Rept. no.6-39; AFCRL-TN-
tfhiliy; AD- 246 059.
Order from LC ml$2.70, ph$4-K) FB 153 081
llMSurements were made of the atmospheric attenua-
tiaa aDd equivalent solar blackbody temperature at die
frequencies of 100.0, 109.8 and 114.0 kmcs from an
devatlon of 0.25 km at a site near Austin, Texas.
Observations were also made in frequency ranges of
calculated molecular ozone and carbon monoxide lines.
lite solar equivalent blackbody temperature was found
to have a value of 5870 ^950' K at 100.0 kmcs and a
nlue of 5500 * 715* K at 109.8 kmcs. The atmos-
piierlc attenuation measured between 12 July and 13
Sqxamber 1S60, had values between 1.2 decibels and
5. 4 decibels . When correlated with the total atmos-
pheric precipltable water, the attenuation was fcund to
have t value of 0.32 decibel gram"^ centimeter"^ at
]ff).0 kmcs, 0.57 decibel gram"^ centimeter"2 at
109.8 kmcs and 1.00 decibel gram'^ centimeter'^ at
114.0 kmcs. No emission or absorption anomalies
«ere observed in die vicinity of the calculated frequen-
cies of the ozone and ca{hon monoxide lines. (Author)
Intermountain
ATMOSPHERIC
MICRON TO 8.
Hales , Thomas
Scientific rept.
15 Aug 60, 22p.
Order from LC
Weather, Inc. . Salt Lake City, Utah.
RADIATIVE FLUX IN THE 6.3
2 MICRON INTERVAL, by J. Vem
A. Studer, and Donald Henderson.
•2 on Contract AF 19(604)2418.
12refs. AFCRL-TN-60-638.
mi$2 . 70, ph$4 .80 PB 1 53 635
Using the radiative transfer equations in the form
given by Elsasser, R(u,T) tables needed to determine
the atmospheric radiative flux in the 6.3 to 8.2 micron
interval were computed. Values of constants , etc . ,
used by Elsasser (1960) were used. Flux computations
were made by a numerical integration of R(u,T) using
the moisture and temperature distribution given by the
radiosonde sounding of 29 April 1959 at HoUoman Air
Force Base, New Mexico. Comparisons were nriade
with balloon measurements made by Strong at the «
lame time and in the same spectrum interval . The
computed net flux was found to agree with the meas-
ured flux within reasonable limits . (Author)
ionosphere Research Lab. , Pennsylvania State U. ,
IMiversity fcrk. ifT
INSTRUMENTATION FOR ROCKET MEASURE-
MENTS OF ELECTRON DENSITY IN THE IONO-
SPHERE, by E. A. Mechtly, R. W. Himaker and
others. Scientific rept. no. 127 on Ionospheric Re-
•eerch. Contract DA 36-061 -ORD- 577. I Jan 60. 98p.
Illfs. AD- 236 787.
Ondar from LC mi$5. 40, ph$15. 30 PB 147 532
The development and testing of Instrumentation for the
measurement of electron density in the ionosphere by
Bsans of rockets is reported. Circuit diagrams, per-
fanaance characteristics, and test procedures are
given. Several observations made by this instrumen-
t«ioo and telemetered from rockets in flight are
•hown. (Author)
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
OONVBCTION AND IXFFUSION OF IONIZATION IN
THE E-LAYER, by H. Peshbach and P. Villara. Rept.
on Contract AF 19(604)7400. 1 Dec 6a 50p. 17 lefa.
33G-0014; AD-248 362.
Order from LC mi$3. 30, ph$7. 80 PB 153 698
It has been suggested that auroral backacatterlng of
radio waves in the frequency range from 100-800
mc/sec is due to the joint action ot turbulence and
eanh's magnetic field, which was assumed to produce
small scale elongated Irr^ularities of ionization lined
up with the earth's field. The present work investlgatea
solutions of the equation for diffusion and transport of
ionization in a weakly ionized turbulent plasma in the
presence of a magnetic field. Due to space charge ef-
fects, thp problem is non linear In the ionlzatioD den-
sity n (x. t). In the linearized approximation the effect
of the magnetic field on turbulence does not lead to
irregularities of a scale sufficiently small to explain
the observed data. Non linear effects may pday a role
and are presently being investigated. (Author)
Little, Arthur D. , Inc. , Cambridge, Mass.
MEASUREMENT OF THE UPPER-ATMOSPHERE
DENSITY. Rept. on Contract AF 19(604)4127. 2 Feb 59,
92p. 14 refs. C-61489; AFCRC-TR-59-217;
AD 230 944.
Order from LC mi$5. 40, ph$15. 30 PB 153 586
A study was conducted to determine whether estimates
of the upper -atmosphere density can be obulned from
measurements of die drag on a fast-moving body In the
altitude range of 150 to 400 mi, and If esthnates are
feasible to devise methods and apparatus for making
and reporting the required measurements. Corre-
lations are available which will permit accurate density
measurements up to altitudes of 250 mi and reason-
ably good estimates up to400mi. Information on satel-
lite electrical potential or atmospheric electron flux is
needed to secure improved accuracy at the upper altl-
fude extremes. Drag forces on bodies moving at near
satellite velocity can be measured if they have
area-to-weight ratios greaternhan about 0. 23 ft^/lb.
For standard satellites, such ratios can be obtained by
having the satellite tow a large, lightweight balloon.
Balloons ejected overboard from ICEM's also would
have adequate velocities and area -to- weight ratios.
Measurement of the drag force Is possible either as a
tension force in the tow line of a satellite trailing a
lightweight drag device or as an acceleration of the
satellite. Instrumentation and mechanisms for making
the measurements are partially specified. (Author)
National Research Labs. . Ottawa (Canada).
ATMOSPHERIC TURBULENCE ENCOUNTERED BY
A FAIRCHILD C-119 AIRCRAFT OVER THE
CANADIAN ARCTIC, by R. T. SeweU. Nov 6a 22p.
2 refs. Aeronautical rept. LR-290.
Order from LC miJ2. 70. ph$4. 80 PB 154 058
V-G-H records were obtained from a Fairchild C-119
aircraft ope rat it^ between Thule. Greenland and
Alert, Ellesmere Island, covering a period of appro*- ■
imately 50 flying hours between 31 July and 11 August
1960. From the limited number of records obtained,
it would appear that the frequency of occurrence erf
559
▼ertical gusts exceeding 10 feet per second equivalent
velocity is considerably lower than that suggested by
the Royal Aeronautical Society as representing a
world-wide average. However, it is considered that
the analysis does not represent a true statistical
average, and the results naay be coosiderably modi-
fied if records wtre to be obtained over a longer
period. (Author)
New York U. Cbll. d Engineering, N. Y.
THE PROBING GF THE TROPOPAUSE BY BAL-
LOONS THAT FOLLOW IT: A SIXXJESTION, by
Wan -Cheng Chiu. Scientific repc no. 1 on Contract
AF 19(604)6146. Oct 60. 16p. 8 refs. AFCRL-
TN-60-808; AI>i4& 280.
Order from LC iil$2. 40. ph$3. 30 PB 153 643
The major mytteory of the trofwpauie it considered to
be the sharpness o< the change at the temperature
gradient that Is often associated with it. It is proposed
that constant lev^l balloons be employed to follow the
tropopause and to probe Its deuiled temperature
structure. The i*ay that this may be done is briefly
outlined. (Auchot)
Nichols Oiemiatry Lab. , New York U. . N. Y
THE REACTION OF NITROGBN ATOMS WITH
OZONE, by H. Austin Taylor and Mei Chlo Chen.
Final rept. on Contract AF 19(604)2076. 15 Oct 6a
I9p. 11 refa. AFCRL-TR-60-420; AD- 248 192
Order from LC ^2. 4a ph$3. 30 PB 153 567
The reaction of (jgonlzfld oxygen and active nitrogen at
room tenr\perature has been shown to produce, almost
exclusively, nitrous oxide. Rate measurements in a
flow system hav< been analyzed as Involving a primary
reaction N +03->NO ♦ 02- Accepting present values
for the specific fates at subsequent reactions a< nitric
oxide, the rate at the primary reaction is found to be
lOlO ml/mole sac. This is several orders faster than
the reaction of nitrogen atoms and oxygen nnolecules
and many order a faster than the three -body recombina-
tion of atomic aitrogen and atomic oxygen, substantiat-
li% the Barth- Kaplan suggestion of the probable source
ol nitric oxide in the upper atmosphere. (Author)
Ohio Slate U. Research Foundation, Columbus, Ohio.
SURVEY OF TtC LITF.RATURE ON RADIATION IN
THE ATMOSPHERE, by J. H. Shaw. Technical rep.
no. I on Contraqt DA 36-039-sc-78153. Sep 58, 179p.
406 refs. RF prt)J. 854; AD-210 805.
Order from LC ^8- 10. ph»27. 30 PB 150 896
This report released for sale to the public 8 Mar 61
A survey at the literature pertaining to radiation In the
atmosphere frota the sun, the earth, the sky and the
clouds that influences the measurement of atmospheric
temperature from sea level up to 150, 000 ft has been
made. Literature from which evaluations can be made
at the errors due to radiation on the measurement ol
temperature, and at methods and techniques for cor-
recting for the8« radiation errors, is also Included in
this survey The results are presented in the form of
an annotated bibliography.
ENGINEERING
Burns and Roe, Inc. . New York.
A LOGISTIC STUDY OF NUCLEAR AND CONVEN-
TIONAL POWER PLANTS FOR THULE, GREEN-
LAND. Rept. on Contraa AF 30(602)2095. June 60,
132p. 14 refs. RADC-TR-60-85; AD-238 286.
. Order from LC mi$6. 90. ph$21 .30 PB 153 931
This report released for sale to the public 16 Mar 61.
This report covers a study made to determine the
comparative coats of logistic support for conventiooal
vs. nuclear facilities as sources d power and stean
heat for the Air Force Base and Ballistic Missile
Early Warning System (BMEWS) at Thule. Greentand.
The existing conventional facilities consist of a float-
ing power ahip with three oil fired bo*lera and three
steam turbines, backed by 27 land-based diesel gea-
erators and 43 package-type heating boilers. The cob
ceptual nuclear plant is designed to furnish all elec-
tric power and heating steam normally produced by
the conventional facilities. The results of the logistic
cost comparison indicate that an annual saving of
roughly $528. 600 to $854. 000 may be reaUzed by
utilizing nuclear power and steam generating fadli-
tlea in place of the existing conventional facllitlea.
These savings are brought about by drastically re-
ducing the dleael fuel requirements, the transporta-
tion costs of which constitute 85 percent of the con-
ventional plant logistic costs. Although not included
In the Scope of Work, development of the study also
revealed that an annual saving of approximately
$1,000,000 in fuel costs could be realized by utilizing
nuclear power. The reaulta of the study indicate thtt
the advantages of lower fuel and logistic supply cbmM
inherent in the nuclear plant should be given serious
consideration when the relative merits of conventional
and nuclear facilities are compared. (Author)
A«ronautical Ertgineering
Aerojet -General Corp., Azusa, Calif.
HYPERVELOCITY DATA RECORDING STUDY, by
G. J. Woffinden. Final rept. on Contract
AF 08(603)4558. Feb 59, 155p. 128 refs. Rept. no.
1541 (Final); APGC-TR-59-33 (X). AD-216 295.
Order from LC ml$7.5a ph$24.30 PB 154 758
This report released for sale to the public 15 Mar 6L
Recommendations are provided for the InstrumentatlM
at a hyperveloclty facility designed for the study of
the target Impaa effect of small projectiles. The
data Include the velocity, size, and flight character-
istics of the projectiles, details of Impact, and result-
ing cAects on various types of targets. Recommenda-
tions include (1) the use of flash X-ray units and high-
speed framing camera for measurements of size and
flight characteristics; (2) flash X-ray units, a framlil
camera and Kerr cells for the observation of impaa
details and target effects; (3) time- Interval meters
(counters) and flash X-ray units for velocity determ*-
560
ladons; (4) synchronization techniques allowing maxi-
nyim precision, reliability, and versatility of the
dtfs-recordlng system; and (5) gas discharge tubes,
arfon bombs, and exploding wires, illumination
lources for photographic -lighting techniques. Optical,
X-ray, electrical, and mechanical methods of data
recording were surveyed. (Author)
Aeronautical Research Lab. , Air Force Research
Dlv., Wright -Patters on AFB, Ohio.
STABILITY STUDIES FOR THE TWIN WHEEL
LANDING GEAR, by Artie M. Vahldlek. Dec 60,
46p. 8 refs . ARL Technical rept. 60-282.
Older from LC ml$ 3.30. ph$ 7. 80 PB 152 583
The nuthematlcal equations for the system of twin
corouiing nosegear contain nineteen parameters.
This report is an attempt to supply the results of
ttudiec that were performed by varying various theo-
retical values of these parameters and conuins three
tipilficant features which it Is believed appear In
pclat for the first time: a. Proof that the stability of
the fear is not a friction phenomenon but is an elastic
•ffsct; b. A new approach to stability margin; and c.
A twin wheel parameter study. Included, also, are
mrtjf showing these parameter variations using the
dbBSnalons of a proposed commercial jet aircraft.
(Author)
Air Force Flight Test Center, Edwards AFB. Calif.
F-104C WORLDS ALTTTUDE RECORD, by Johnny G
Armstrong and Joe B. Josdan. Apr 60. 36p. AFFTC-
TN-60-10; AD- 236 865.
Order from LC ml$3.00. ph$6. 30 PB 153 591
This report released for sale to the public 15 Mar 61.
Od 14 December 1959. a new world's altitude record
of 103. 395. 5 feet was set by a modified F-104C air-
craft A new time to climb record waa also set during
dw same flight of 15 ndnutes 4.92 seconds to reach 30
kikmetera. In order to obtain this record altitude the
aircraft was required to fly faater and slower than
ever before. The zoom was started from 2. 35 Macfa
Bumber at 39. 600 feet with a clinU> ai^(le of almost
SO degrees which resulted in a minimum Indicated air-
S|Md of 54 knots at the peak altitude. The test air-
craft was modified by Lockheed Aircraft Corporation
at Palmdale, California. An F-104B ull assembly was
tnauUed In order to Improve the directional stability.
The inlet cone was modified in order to Improve the
airflow to the engine at the higher supersonic speeds.
Engine thrust was Increased by Increaalng maximum
WHliwi speed and afterburner fuel flow. The record
t^ waa witnessed by officials of the National
AerODiutic Association. Askania records of the fUght
been sent to the Federation Aeronautlque Inter -
il In Paris, France for tbelr official ruling.
(Autiior)
Armour Research Foundation. Chicago, 111.
UfjUlD OXYGEN CONVERTER, by John Bitten.
Uft. for 16 Sep 59- 15 Aug 60 on Equipment for Life
ftippon In Astronautlcal Operations . Contract AF
33(616)6756. Oct 60, 66p. 76 refs. Rept. no.
ARF 3164-12; ARF Proj. C 164; WADD Technical rept.
tt-669.
Order fromOTSJ 1.75 PB 171 554
A 5-liter zero gravity liquid oxygen converter based
on the paramagnetic and surface tension propenles of
liquid oxygen was designed, axxl a prototype unit was
constructed. The design study showed that the magni-
tude of the magnetic or surface tension forces is
sufficient to operate the unit under zero gravity condi-
tions. lirvestlgacions showed that possible operatioaal
and construction problems due to tbernoal stresses in
the magnet, the magnetic field on the gaging system,
the physical properties of the liquid oxygen, and the
wettability of the metal tubes by the liquid oxygen will
not adversely affect the construction or operation of
the converter . Theoretical calculations determined
the magnitude of the magnetic forces on various sizes
of liquid oxygen droplets and correlated the data ob-
tain^ from measuring the flow rate of liquids in hori-
zontal capillaries . (Author)
It
Army Transportation Research Command, Fort
Bustia. Va.
ROTOR BLADE PROTECTIVE COVERS, by Robert '
M. Bemardin. Final rept. on Project 9R38 -01 -017-51.
Oct 60, 32p. 7 refa. TREC Technical rept. 60-19;
AD-248 2ia
Order from OTS $1. 00 PB 171 514
The report covera the investigation of and develop-
n^ent of design criteria for Improved equipment for
environmental protection of Army helicopter rotor
blades. Included Is the construction and laboratory
testing of an experimental model cover. (Author)
Courtney and Co. , Philadelphia, Pa.
STAFF DEVELOPMENT IN SYSTEMS RESEARCH
TECHNIQUES, by J. S. Kldd and K. M. Michels.
Rept. on Contract FAA/BRD-8S. 15 Aug 59, 149p.
16 refa. Rept. no. 29.
Order from OTS $3. 00 PB 171 510
Contenta:
Pt. 1. Research methods in the analysis, design, and
evaluation of man -machine aystems
Pt. 2. Statistical techniques
Federal Aviation Agency, Atlantic City, N. J.
DEVELOPMENT OF A HEAD-MOUNTED CAMERA
FOR REOORtXNG PILOTS' EYE MOVEMENTS, by
E. E. Pazera. Mar 60, 31p. 3 refs. Task assignment
no. 59-205.9.
Order from OTS $1. 00 PB 171 506
One phase of a study of cockpit visibility requirements
for Army Ualson- reconnaissance -type aircraft called
for the evaluation of the visual performance ct Army
pllota. A head -mounted cantera was developed to
Implement this Investigation. This report describes
the camera' a development and the general aspects at
its use. (Author)
Federal Aviation Agency, Atlantic City, N. J.
TRANSPORT AIRCRAFT COCKPIT VOICE RE-
CORDING, byF. W. Jefferson. Final rept. on Taak
D/E-1-6089. Dec 60, 20p.
Order from OTS $0. SO PB 171 506
561
TestB were conducted at the National Aviation Facill-
tlea Experlmentai Center utilizing chree aircraft, a
C-131, • DC-3, «nd a Gninunan Gulfstream. to de-
termine the most desirable method for recording
crew conversaticns as an aid to accident Investiga-
tlon. Currently available area and individual pickup-
type microphone* were employed. The application d
electronic noise-fllterlng and nolw-cancelllng tech-
niques was investigated for improving the Inteillgl-
Wllty of the recorded voice. The recording of crew
conversation in transport aircraft utilizing area
[rickup-type micropboDes is feasible. (Author)
1.
Flight Accessones Lab. , Wright Air Development
Div. , Wright- Patterson AFB, Ohio.
DETERMINATION OF A STANDARD EXTINGUISH-
ING AGENT FOR AIRBORNE FIXED SYSTEMS, by
Ralph L. Hough. Oct 60, 62p. 40 refs . WADD Techni-
cal rept. 60-552. J
Order from GTS $1 .75 PB 171 552
This report presents Investigations to determine the
optimum chemioU liquid extinguishing agent for use in
airborne fixed systems at high temperatures . The de-
velopment history, theories of flame inhibition, and
the design of airborne fixed systems are examined.
Agents included bronnochloromethane , dlbromodifluo'
romethane, bromocrlfluoromethane , bromochlorodl-
fluoromethane . and trichlorofluoromethane . Effectlv-
Ity test showed that trichlorofluoromethane is inferior
to the bromine-containing agents . The agent should be
selected by the temperature requirements for the
agent -conuiner System. For temperatures to 250OF,
bronx)chlorometbane is superior, for temperatures to
350PP , dlbromodlfluoromethane is best; and for tem-
peratures to 400^F , bromochlorodifluoromethane it
best . No agent is suitable at temperatures above
400OF. (Author)
Harvey Aluminum, Inc. . Torrance, Calif.
EXTRUSICW DIE DEVELOPMENT: TITANIUM AND
STEEL, by G. A Moudry, R B. Simonaon and A. Toy.
Final Technical Engineering rept. for I Feb 58-
30 Nov 59 on Conlraa AF 33(600)36303. July 60,
145p. 36 refs AMC Technical rept. 60-7-577;
AD- 247 359.
Order from OfTS $2. 75 PB 171 529
Precision hoc exrtusion of titanium and steel struc-
tural sections for aircraft, missiles, and aerospace
vehicles may be accomplished most effectively with
bonded carbide ot M-36 high speed steel dies and a
lubricant at the graphlte-moly-disulphide type. Fric-
tion Studies: cobalt -bonded carbides yielded the con-
sistently best friction test results. A 9 percent Co
content la suggested. A nickel-bonded titanium car-
bide yielded results comparable to the carbides. The
other most promising group, was the flame- sprayed
oxides and siUcates; in particular, zirconium silicate
and magnesium aluminate spinel. The high alloy
steels and nitrldqd and carburlzed alloy steels were
not as resistant to wear and seizing. Carbide yielded
a superior exiruaion, provided the ram speed did not
exce«d 2 to 4 incftes per second. Extrusions from the
high speed steel ilea were also excellent. The high
speed steel is more suiuble for shan runout, where
a larger number of billets are to be extruded. It Is
difficult and time constimlng to fabricate dimension-
ally stable carbide dies Based on these considera-
tions, the general use of steel dies is Indicated.
These may be Improved by carburlzlng or nltriding.
Inatitute of Transportation and Traffic Engineering,
U. of California, Berkeley.
AN EVALUATICW OF SURFACE -MOUNTED LIC3HTS
FOR RUNWAY GUIDANCE, by Dan M. Finch and
Robert Horoi^eff. Final rept. on Cootraa
FAA/BRD-4. June 60, 18p. 3 refs.
Order from OTS $0. 50 PB 171 507
The concept of providing visual guidance by means of
closely spaced, low-wanage Light sources mounted oa
the surface of the runway or taxiway in lineal pattenu
is described In this report as well as in the prior re-
ports related to this contract. The center line lightlni
system at San Prandsco International Airport was
rehabilitated after the 1958-59 teats to perndl further
evaluation during the winter of 1959-60. It turned ou
that the 1959-60 winter season was very mild; there
were, however, some periods of reduced visibility
wherein a limited amount of bad weather evaluation
was obtained. The 1959-60 test data verified the
previous observations In which very favorable pilot
reactions were obtained in clear weather operations.
The few obaervatlons that were made in poor visibil-
ity also indicate that the centerline system is a
desirable adjuna to the existing lighting system. Bu
an evaluation of the system in very poor visibility
conditions is still incomplete. (Author)
Naval Research Lab. , Washington, D. C.
AN ANALYSIS OF THE RELATIONSHIP BETWEEN
THE COLLISION- AVOIDANCE TRAJECTORY OP
AN AIRCRAFT AND ITS PERFORMANCE CAPABIL-
ITY, by P. A. Grafton. Interim rept. 24 Jan 61, 13pi
1 re*. NRL rept. 5578.
Order from OTS |0.50 . PB 171 052
The problem of the avoidance of collision between air-
craft on curvilinear flight trajectories has been the
subject of an earlier investigation and is here further
analyzed in order to obtain a relationship between the
collision -avoidance trajectory required of an aircraft
and its ability to meet the requirement. On this rela-
tionship would rest the verification of an avoidance
path before an aircraft actually enters upon the path.
(Author)
Pitman-Dunn Labs. [Group] Frankford Arsenal,
Philadelphia, Pa.
STUDY OF SENSITIVITY RESPONSE OF BARIUM
TTTANATE ACCELEROMETERS SUBJECTED TO
VARIOUS EXTREMES OF CLIMATIC ENVIRON-
MENTS. ACOUSTIC NOISE AND SHOCK TESTS, by
Aleck Goldberg. 3 Aug ^8. 19p. Technical rept.
S-5584; AD- 159 318.
Order from LC ml$2. 40, ph$3. 30 PB 154 424
This repon released for sale to the public 8 Mar 61.
This repon discusses the effects on the sensitivity flf
barium titanate accelerometers when subjected to tbe
following conditions; (I) extreme temperature enviros-
562
1
Qieats. (2) exposure to salt fog and rainfall, and (3)
applied tranverse shocks. In addition the reaponae to
acoustic noise field was determined. Four (4) to
eleven (11) G of acceleration response resulted from
acouffic exciutlon of 125 to 135 decibels of field in-
lettsity. The results of extreme temperature environ-
meois on accelerometer sensitivity indicate the need
of accelerometer sensitivity evaluation in its particu-
lar temperature environment. Little or no effects
are due to transverse shock and rainfall. Salt fog ex-
posure produced functional failire in two (2) out of
three (3) accelerbmeters tested. (Author)
Princeton U. , N. J.
A STABILITY ANALYSIS OF TDLT-WING AIRCRAFT
(ANALYTICAL) by Charles H. Cromwell, III and
Henry E. Payne, IIL Rept. on Contract Nonr- 1858(14).
May 60. 176p. 10 refs. Rept. no. 477; AD- 239 964.
Order from LC mi$8. 10. ph$27. 30 PB 149 354
A general development of methods for predicting the
•erodynamic stability derivatives of propeller-driven
tilt-wing vertical take-off and landing (VTDL) air-
craft is presented. The concept of slipstream dy-
namic pressure (q") is reviewed along with the basic
atiumptions behind it and their limitations. The use
of q" it then extended to give a semi -empirical method
of predicting lift and drag on a wing, at any tilt angle,
which is fully immersed in slipstream. This analysis
it Justified by experimental data, and other wind tunnel
data which was taken for a general tilt-wing transport
model is presented. The linearized small-pertur-
bttlon equations of motion are reviewed and then
adiped to the tilt-wing aircraft. The aerodynamic
termi in the stability derivatives are evaluated in
geaeral form using either experimental data or the
(kaoretlcal method previously mentioned to account for
the wing's contributions. The other components of the
aircraft considered as contributing to stability are
propeller, fuselage and tall. The methods devlsedfor
predicting the stability derivatives are then used to
make an illustrative series of calculations for the
HUler X- 18 test bed. The stability roots are calculated
and the aircrafts' characteristic response is de-
termined by use of an analog computer. (Author)
Princeton U. , N. j.
A STABO^iry ANALYSIS OF TILT- WING AIRCRAFT
(EXPERIMENTAL) by Henry E. Payne, lU and Charles
H Cromwell. IIL Rept. on Contract Nonr- 1858(1 4).
May 60. 53p. 14 refs. Rept. no. 478; AD- 239 963.
Order from LC ml$3. 60. phJ9. 30 PB 149 355
An experimental investigation of longitudinal forces
and moments acting on a generalized tilt-wing assault
transport was conducted in order to extract the neces-
»ary stability derivatives for use in the equations of
motion. Since this was the first true VTOL aircraft to
be tested in the Subsonic Aerodynamics Laboratory,
new facilities and techniques were developed for ob-
tslnlng complete and accurate VTOL hovering and
transition data. A wind tunnel was modified to give the
oecetsary ground clearmnoe, and strain gauge Instru-
mentation was successfully developed for obtaining
total model forces and moments as well as propeller
contributions. The primary forces acting on an in-
clined propeller, thrust, normal force, aixl pitching
moment, were completely determined over a range of
tilt angles from 0 - 90° for two propeller pitch set-
tings in both the propeller -alone configuration and the
propeller -wing configuration. (Author)
Systems Technology , Inc . , Inglewood , Calif .
A SYSTEMS ANALYSIS VIEW OF LONGITUDINAL
FLYING QUAUTIES, by DuaneT. McRuer, Irving
L. Ashkenas, andC. L. Guerre. Rept. on Cotitract
AP 33(616)5661. |an 60, 116p. 22 refs. Wadd Techni-
cal rept. 60-43.
Order from OTS $2.50 FB 171 551
Pilot describing functions and airframe transfer func-
tions are combined within a servo analysis framework
to develop a partial theory of longitudinal flying quali-
ties . Criteria and procedures are established for es-
timating both pilot dynamic behavior and ojAnion..
Tentative criteria for certain pitch angle , normal
acceleration and air speed to elevator transfer func-
tion quantities are derived and compared with existing
pilot opinion data. New parameters of possible signif-
icance are identified. The report contains a summary
of pilot dynamic capabilities in closed loop tasks and
airframe longitudinal transfer function parameters
and characteristics . (Author)
Texas Instmments, Inc. , Dallas.
THE STUDY AND DEVELOPMENT OF CLOSELY
REGULATED ELECTRIC POWER GENERATING
AND CHARGING SYSTEMS FOR US ARMY AIR-
CRAFT, by Wilson W. Fortner. Final rept. for
15 June 58-31 May 60 on Contract DA 36-039-8C-
78003. 31 May 60, I68p. 30 refs. Rept. no.
8-40600-8; AD- 246 013.
Order from LC miJ7. 80, ph$25. 80 PB 153 933
No usable correlation between the transistor break-
down data and the measureable parameters of the in-
dividual transistors was noted. Good correlation
exists between tbe destructive breakdown data and
the junction type. The junctions are listed in de-
scending order of breakdown levels: grown -diffused
transistors, grown junction transistors, diffused base
meaa transistors, and alloy junction transistors. The
non -destructive transistor breakdown data indicates
the relation between pulse width and pulse amplitude
required to break down the transistor. The pulse
ener:gy required to break down a transistor was
almost constant for tbe range of pulse widths tested.
The transistor will first break down In a non-destruc
tlve manner. If it receives sufficient energy, the pa-
rameters (1. e. , d-c beta) will change or the transis-
tor may be destroyed (normally by shorting). In tbe
broken down condition, a transistor presents a very
low impedance to the transient. This tends to protect
the transistor from transients of high source imped-
ance. Transients of sufficient amplitude to break
down a transistor junction but noraully not destruc-
tive, may be destructive if the pulse rate frequency
la great enough for them to heat up the junction. Re-
liability and long term stability can be improved by
replacing the carbon pile regulator with a static de-
vice. A transistorized regulator does not decrease
the generator transient. This transient is believed to
be a function of the generator magnetic circuit.
Transient suppression devices should be installed on
the electronic bus. Either shunt or series, devices
may be used to protect the electronic bus. (Author)
S6S
United Aircraft Corp. fEast Hartford, Coon. ]
WIND TUNNEL TESTS OF SHROUDED PROPEL-
LERS AT MACH: NUMBERS FROM 0 TO 0.60, by
Ronald M. Groaei Rept. on Contract AF 33(616)5363.
Dec 58. 207p. llrefs. WA DC Technical rept. 58-604
AD- 206 464.
Order from LC im$9. 30. ph$31 .80 PB 154 504
This report releiwd for sale to tbe pubUc 2 Mar 61.
Wind tunnel tests were conduaed by the United Air-
craft Corporation Research Department to determine
the aerodynamic performance d a 2.5-ft diameter
ahrouded propelkr. The model. Installed on a
12, OOO-rpm propeller dynamometer, was teMed at
Mach numbers batween 0 and 0. 60 and at angles d.
attack between 0 and 6 deg. Shroud lift and drag
forces were obulned. and Independent measurements
d propeller thruit and torque were made with and
without the shroud installed. A shroud having two
leading-edge configurations was tested, one with a
small lip radius co provide low drag at high flight
speeds and tbe o^ier with a large lip radius designed
to provide high static thrust. Both shroud configura-
tions had a ratio of chord length to propeller diame-
ter of 0. 50 and the plane of the 4 -blade model propel-
ler was located at the mid-chord of the shroud. In
general, it was cletermlned that the static thrust of a
given propeller ftr a fixed power input can be in-
creased as much as 65 percent by the use of a prop-
erly designed shroud. For Mach numbers below 0. 30
and for high propeller power loadings, a thrust force
was obtained on the shroud configuration designed for
the high-speed condition. At higher Mach numbers,
the performance of the propeller with the high-speed
shroud configuration was inferior to that of the iso-
lated propeller a$ a consequence of shroud drag. The
lift of the high-sfeed shroud was found to be approxi-
mately the same as that of a ring wing, i.e. , twice
that of a simple rectangular wing having a span equal
to tbe diameter qf the shroud and a chord equal to
the length of the shroud.
Vertol Aircraft 'Corp. . Morton, Pa.
THE VBRTODYNE VTOL AIRCRAFT STTUDY SEMl-
SPAN MODEL TESTS IN HOVERING AND FORWARD
FLIGHT , by E . Brogan , G . Casey and ochers . Rept .
on Contract Nonn- 2364(00) . 30 Mar 60, 106p. 13 refs .
R-158' AD- 234 751.
Order'from LC i|ii$5.70, phH6.80 PB 153 740
The Vertodyne f«di-in-wing concept has been studied In
a series of static and forward speed tests . A semi-
span model was Oested Incorporating Instrumemation
for measuring fan thrust, torque and wing surface
pressures . Forces and moments on the model were
measured at the model support. Tests were per-
formed at the University of Detroit using the available
laboratory and wing tunnel facilities . Dau is pre-
sented In dimensionless form which covers the forces
and moments acting on the model and the fan power
required for a range of swtlc and forward flight condi-
tions. Wing surflKe pressured are presented for the
same range of conditions . Significant increases in
wing lift accompanied by high nose-up pitching nx)-
ments were obtained in forward flight. Model static
thrust per horsepofwer was found to decrease in
ground effect. A| discussion of results with conclus-
ions and recommendations f6r further study is in-
dudad in the repon . (Author)
Vertol Aircraft Corp. , Morton, Pa.
WIND TUNNEL TESTS AND FURTHER ANALYSIS
OF THE FLOATING WING FUEL TANKS FOR
HEUCOPTER RANGE EXTENSION. VOLUME I.
HEUCOPTER RANGE EXTENSION WIND TUNNEL
SrUDY, by C. B. Fay and R. B. Johnstone. Rept. oa
Comraa DA 44-177-tc-550. Oct 60, 147p. 11 refs.
R-204: TREC 60-64; AD-248 516.
Order from LC mi$7. 20, ph$22. 80 PB 153 879-1
A wind tunnel test has been conducted on a model
helicopter fitted with floating wing fuel tanks for ferry
range extension. The model consists of a tandem
rotor helicopter with 3. 9 ft. diameter electrically
powered rotors mounted on a HUP (H-25) configured
fuselage. Floating wing fuel tanks of an overall spaa
of 4.7 ft. are attached to the fuselage through a
skewed hinge. QuaUtatlvely, the test proved the
excellent behavior of the hinged wing panels at all
operational speeds and attitudes, in and out of ground
effect. Quantitatively, the results show that: (l)The
effea on induced power on the front and rear rotor
due to the presence of the fuel wing was of the same
magnitude as that predlaed in the theoretical analysis
and in the feasibility study. (2) The stability charac-
teristics of the fuel-wiilg were better than that i*b-
diaed, which, in turn, will improve the stability and
dynamic charaaerlstics of the total system. (3) The
trajectory of the Jettisoned wing panel was below the
helicopter rotors, which Is required if Jettisoning the
wing 18 to be used In the event of an emergency.
(Author)
Vertol Aircraft Corp. , Morton, Pa.
WIND TUNNEL TESTS AND FURTHER ANALYSIS
OF THE FLOATING WING FUEL TANKS FOR
HEUCOPTER RANGE EXTENSION. VOLUME 2.
GROUND AND AIR MECHANICAL INSTABILFTY
ANALYSIS, by V. Capurso, R. Ricks and R. Gabel.
Rept. onContract DA 44-177-tc-550. Oct 60, 225p.
14 refs. R-197; TREC 60-65; AD-248 517.
Order from LC mi$9. 90. ph$34. 80. PB 153 879-2
Mechanical instability of a helicopter range extensicn
system utilizing hinged wing fuel tanks has been In-
vestigated for acceptable charaaerlstics on ground
and In the air. Ground Instability Is studied for the
H-21, H-25, and H-34 helicopters with wing tanks
through a simulated takeoff with full tanks to a landing
with empty tanks. Instability ranges appear due to
antisymmetric blade lag motions coupling with aircraft
roll and lateral motions and wing flap and bending
modes. Critical conditions are in the roll mode in
takeoff with full tanks and In landing with empty unto,
but damping from the heUcopter and wing oleo struts
Is always sufficient to control the instability. (Atchor)
(See also PB 153 879-1)
Ch«mical Engineering
Advanced Metals Research Corp. , Somerville,
A METHOD FOR IDENTIFICATION OF STRATO-
SPHERIC PARTICLES, by R. Lewis, S. Moll and
others. Rept. on Contract A F 19(604)4146. 30 Sep 6a
74p. 1 ref. Research rept. AMR 1006; AFCRL-TR-
60-419; AD-248 133.
Order from LC mi$4. 50, ph$l2. 30 PB 153 653
564
^andard x-ray fluorescent techniques proved appli-
cable for analyzing only microgram quantities of ma-
Itrlsl. An x-ray micro-fluorescent technique was
developed capable of analyzing minute deposits on
(brmvar films. Detecubility limits were of tbe order
(^ 10-9 grams. Electron beam microanalysis proved
to be an applicable method which combined good ac-
curacy and high resolution. Analysis of a number of
Walloon flight and high altitude aircraft collected
Munples Indicate that sulfur, probably present as a
fulfate, may be the most important constituent of
stratospheric aerosols. Smaller but positive amounts
of ailicon. aluminum, and iron were also present in
die collections. The presence of calcium, tnagne-
sim, chlorine, phosphorous, vanadium, titanium and
nickel were detected In Isolated cases but their in-
clusion as constituents of stratospheric aerosols is
debatable.
Naval Engineering Experiment Station, Annapolis.
Md.
DECARBONATION OF SEA WATER FOR EVAPO-
RATOR SCALE CONTROL, by J. R. Bell. (1950] 26p.
2 refs. B.E.S. rept. 1A66024.
Order from LC ml$2.70, ph$4.80 PB 154 746
This report released for sale to tbe public 15 Mar 61 .
A method for prevention of scale in low-pressure dis-
tllllig plants by removal of the carbon -dioxide content
of Ite sea-water feed has been proposed by Armour
Research Foundation. This consists of thermal de-
composition of the carbonate and bicarbonate Ions
present and subsequent stripyping of the carbon dioxide
from the water by aeration. The completeness of the
reaction at moderate temperature Is predicated upon '
the buffering action of magnesium Ions in alkaline sea
water. An investigation at Fort Story, Virginia, using
full-scale equipment, showed that the reaction de-
scribed does not proceed to the predicted extent at
moderate temperature and that the degree of decar-
boastlon possible with feasible equipment is of no
raise in scale reduction. (Author)
Civil Engineering
Army Snow Ice and Permafrost Research Esublish-
ment, Wilmette, 111.
CUT-AND-COVER TRENCHING IN SNOW, by
R W. Waterhouse. July 60, 15p. Technical rept. 76.
Order from LC ml$2. 40, ph$3. 30 PB 153 556
A method developed and tested In Greenland in 1955
tad 1956 for making covered trenches in snow for use
u subsurface shelters and communication-ways in
the lee Cap is described. The machine used for
trench-cutting and roof-forming operations was a
Peter enow miller. The initial installation consisted
of a trench 8 ft wide and 10 ft deep with a 2- ft shoulder
cseach side, over which an arched snow cover was
(ornted on a removable steel form system. During
initial stripping, considerable shock and raultllation
could be sustained by the snow seat and the filled arch
*tlhout apparent damage to the roof system. The
'onn system was easy to handle with a min. of in-
■niaion. A covered trench of 500 ft was constructed
•nd Instrumented to gage the time deformation and
closure rate. Experience has proved that the method
uaed is sound and practical. Undershow facilities of
significant size and durabiliry may be produced
quickly by service personnel. A sequence of photo-
graphs is included showing details of the construaion
techtdques, and dau on arch-form details are
appended. (Author)
Columbia U. , New York.
INEQUALmES FOR FIRST EMPTINESS PROBA-
BILITIES OF A DAM WITH ORDERED INPUT, by
R. Pyke and ]. Gani (Stanford U. \ Rept. on Contract
Nonr-266(59) and NSF Grant 9670. [1960] 23p. 4 refs.
CU-17-60-Nonr-266(59)MS; AD-236 737.
Order from LC mi$2. 7a ph$4. 80 PB 147 546
Probabilities of first emptiness times for a dam fed
by certain ordered inputs ij a_, and subject to a
steady release rule are considered. The unwieldy
equations for these probabilities restrict their use-
fulness, and simple inequalities are derived for them
which prove more tractable in practice. These are
applied to the particular case of the dam with two
ordered Poisson inputs a^, a2, the exact probabilities
of first emptiness and their upper and lower bouixls
being compared for various values of the parameters
involved. Conditions for the probability that the dam
will eventually become empty are presented.
(Author)
Electrical and Electronic Engineering
(Aerial Reconnaissance] Lab. , Wright Air Develop-
ment [Div. ] Wright -Patterson AFB, Ohio.
ALTERNATING-TRACK COUNTER- ROT ATICW RE-
CORDER FOR MAGNETIC RECORDING, by Charles
Colbert and William G. Siryker. Rept. on Automatic
Recorder for Electronic Countermeasures Equipment.
June 52, 48p. 2 refs. WADC Technical rept. 52-2;
ATI -162 940.
Order from LC ml$3. 30, ph$7. 80 PB 154 296
This report released for sale to the public 6 Mar 61 .
In the storage erf Intelligence for later reproduction,
it is Important that (1) the greatest amount of intelli-
gence be stored in the smallest amount of space, (2)
the reproduction be of acceptable quality, and (3)
editing be facilitated. To this end, a magnetic re-
corder (Altracor) utilizing several parallel recording
paths on the magnetic tape was designed, wherein the
recording elements are In motion in a direction oppo-
site to that of the tape. Significant features of the
laboratory model are piresented. A theoretical treat-
ment of this recording scheme is also presented. It is
concluded that application of the Altracor principle
will provide a recorder which, for many applications,
will allow better utilization of the available magnetic-
tape storage volume. (Author)
Airborne Instruments Lab. , Deer Park, N. Y.
RADIO DOPPLER DETECTORS FOR AIRPORT
GROUND TRAFFIC CONTROL, by J. C. O'Connor,
J. B. Leary and D. J. Greber. Rept. on Contract
FAA/BRD-53. June 60. 72p. Rept. na 5934-1.
Order from OTS $2. 00 . PB 171*509
565
This report deKrlbes the Investigation at a radio
doppler detector as a boundary-crossing sensor for
purposes al airfort ground traffic control. It is ca-
pable of detecting surface traffic and airborne traffic
in the approach zone and over the runways of an air-
port. This program developed and delivered 22
doppler detectors for approach -zone, ninway, and
uxiway detection capable of showing detection, loca-
tion, and direction of travel of vehicles and aircraft
on the instrumented areas of NAFEC. (Author)
Airborne Instruments Lab. , Melville, N. Y-
TRANS1STOR125ED NfTl CANCELER. by C J.
Melselbach. Pinal engineering rept. on Contrmct
AP 30(602)1750. 22 Aug 59, 29p. 6 refs. Rept. no.
4520-1; RADC-TR-59-220; AD- 230 992.
Order from UZmiil. 70, pb$4 80 PB 153 888
An ei^ineerlng model of MTI Group AN/CPA-{ )
(Transistorizedl MTI Canceler] will demonstrate the
feasibility of manufacturing transistorized and minia-
turized cancellation equipment with electrical per-
fonnance characteristics comparable with those of
tube equipment. The engineering model is 0. 75 cuMc
foot in volume, is completely transistorized (using
91 transistors) and operates on about 10 watta of
power. A miniaturized 2778-usec folded ultrasonic
delay line mouixed in a temperature-controlled oven
is used to determine the system PRP. This delay line
is approKlmately one -half the diameter at a cooven-
doaal delay lin«. The high-quality performance of
tUa delay line verifies the practicability of the folded
type at conairuction. The Canceler includes auto-
matic pulse amplitude and timing circuits that main-
tain a cancellation ratio in excess of 36 db for ex-
tended periods The Canceler operates satisfactorily
over a temperature range of 40 C (from *5 C to ♦45C).
This performance is achieved using germanium tran-
sistors without elaborate temperature -compensating
devices. A smaller unit, meeting stricter tempera-
ture requirements appeared completely feasible using
the improved transistors and components now
available. (Author)
Airborne Instruments Lab. , Mlneola, N. Y.
CX)NSTRUCTION OF BEACON VICCO DEFRUTTTNG
EQUIPMENT TYPE 2.3NS10, by P- C Holcombe.
Final engineer lug rept. on Contraa FAA/BRD-76.
Apr 59, 40p 1 ref. Rept. no. 4614-1.
Order from 0T$$ 1.00 PB 171 508
In a dense air traffic environment many nonsynchro-
nous beacon replies are generated. These replies or
"fruit" clutter the PPl display and thereby mask true
or synchronous beacon replies. Beacon Video De-
fndting Equipnwnt 2. 3NS10 was designed to elinunate
the fruit or unwanted replies without detericx-ation at
the synchronous replies. This report describes the
defruitlng equipment and the associated design prob-
lems encounterfd. (Author)
Airborne Instruments Lab , Mlneola, N. Y
DEVELOPMENT OF ANDB TYPE 2. 3NS9 BEACON
VIDEO ?rORA<)E-TUBE DEPRUITING EQUIPMENT,
by W. Smith, rtnal engineering rept. on Contract
NOaa 57-405-c Mar 59, 85p. Rept. no. 3689-1.
Order from 0T$ $2. 25 PB 171 504
This equipment Is a part of the ANDB Type III Air
Traffic Control Radar Beacon System (ATCRBS) and
is deslgpwd to eliminate random asynchronous replies
from the beacon display. In system operation, a
beacon interrogator-responder (IR) unit transmits •
series of paired pulses at the radar PRF (or a sub-
multiple frequency) that are received at an airborne
transponder. In the present system, the transponder
replies with a train of from two to eight pulses havli^
a nominal pulse duration of 0. 45 psec. The first and
last pulses (bracket pulses) of the reply train are
spaced 20. 3 paec apart. Coded information pulses
may occupy any assigned intermediate pulse poeitioo,
the spacing between adjacent pulse positions being
2.9 HBCC. Future system operation will include up to
13 information pulses spaced 1 . 45 \xaec apart.
(Author)
Armour Research Foundation. Chicago, 111.
HIGH POWER TRANSDUCERS, by H. B. Karplus
and R. R. Whymark. CMnerly rept. no. i 15 Peb-
15 May 60. on Contract Nonr-2900(00). (1960) 3p.
ARF-1149-4.
Order from LCmi$ 1.80. ph$ 1.80 PB 147 498
7^ detailed study of the relation of magnetic and
motional parameters of nickel strips and stacks has
continued for both the quasi -static and the dynamic
(resonant) conditions.
Army Signal Research and Development Lab. , Pon
Monmouth, N. J.
APPLICATION OF MASER TO NUCLEAR/WEATHBR
SURVEILLANCE RADAR, by Raymond L. Robbiani.
15 Sep 60, I6p. USASRDL Technical rept. 2151;
AD-244 752.
Order from LC mi$2. 40. ph$3. 30 PB 153 250
A bench test, performed to determine the increase In
sensitivity that an X-band helium MASER could afford
a Radar Set AN/CPS-9 receiver, indicated an average
improvement of 20 db in receiver sensitivity. Assum-
ing an input antenna noise of 29CPYi, the receiver sen-
sitivity improvement to be expected from an operatin|
radar equipment was calculated to be approximately
12. 5 db. The MASER was tested in a Radar Set
AN/CPS-9 to determine the effect at the transmitted
energy on the MASER's amplification. The MASER
was completely saturated by the transmitted pulse.
In an effort to reduce the MASER saturation, a fixed,
two -dish venically directed antenna system was
assembled. Even when the two-dish system was
operated with the antennas 300 ft apan, the MASER
was completely saturated. Radar sensitivity improre-
nr>eni opens nrtany prospects for future uses of X-band
radars. These include Improvement in nuclear-
weather surveillance, improved meteorological in-
telligence, satellite operations, etc. The new, mudi
smaller MASER, which uses liquid nitrogen instead
of liquid helium, may lend itself more readily to in-
clusion in tactical -type radar equipments. A calcu-
lated comparison of a parametric amplifier and the
MASER shows the MASER to have a 15 -db advantage
in sensitivity if antenna noise is ignored, and at lea*
a 5. 7-db advantage if a 290^ antenna noise is
assumed. (Author)
566
Army Signal [Research and Development Lab. 1 Port
Monmouth, N. J.
A HIGH VOLTAGE COAXIAL CABLE CC»MNECTOR
POR RADAR SET AN/TPS-ID. by William E. Mayo.
30 Dec 57. 17p. 2 refs. Technical memo. no.
M-1926; AD-160 0S5.
Older from LC mi$2. 40, ph$3. 30 PB 153 248
An Unproved version of connector adaptor assemtdy
(CG-90C)( )/\J was designed which will meet the re-
quirements for use in radar equipment AN/TPS-ID.
•niB newly designed connector, when assembled to a
lenth (rf RG-19/U cable without the use of DC -4 high
voltage grease, was found to have a 60-c corona ex-
dnciion voltage of 10. 500 (RMS). With the applica-
tion of DC -4, the voltage level was increased to
12, 500 V (RMS). The VSWR at 2 connectors attached
to an 8 ft length of RG- 19/U cable waa less than 1.15
over the required frequency band. The VSWR of the
Individual connector is estimated to be below 1 . 08
■ad Che connector should be capable of handling peak
polar power levels In the order of 500 kw without
filhire.
Army Signal [Research and Development Lab.]
Fort Monniouth. N. J.
A NOVEL ANTENNA FOR MOBILE RADIO RELAY
OTCRATION IN THE UHF RANGE, by Frank J.
Trido. Nov 57, 28p. 4 refs. Technical memo. no.
M-1924; AD- 160 061.
Order from LC ml$2. 70. ph$4. 80 PB 153 247
A novel type antenna configuration called the Double-
Rhombic was designed and conatructed for use in the
frequency range from 400 to 600 mc. This configura-
doa la formed by combining 2 rhombic antennas whose
pUnes form an angle with each other and which have a
common diagonal. The input and output terminala of
bodi rhombic s are connected in parallel with each
(Nher. A 60° angle between planes was optimum on
. te baais of full scale radiation pattern measure-
OMnu. The antenna is capable of handling approxi-
mately 100 watts of power. Its gain compared to the
standard Radio Relay Set Band "D" dipole array varies
from -2 to ♦2. 5 db over the frequency band. The SWR
was found to be less than I. 4 to 1. The antenna is so
mechanically designed that it is relatively light in
view of Ita fairly large dimensions, being in the order
of 25 lbs. It Is constructed of thin- walled aluminum
nMng and employs girder- type support in its fabrica-
ttOB. It has a very low wind drag when compared to
other antennas utilized in the same range. The an-
toma Is capable of being assembled and disassembled
in a very short time, and therefore is very attractive
for use in military applications for mobile radio relay
operation in the UHF frequency range.
Army Signal [Reaearch and Development Lab. ]
Port Monmouth, N. J.
A VERNIER TIME INTERVAL MEASURING SYS-
TEM, by Herbert D. Tanzman. 26 Feb 58. 32p.
2 refs. Technical mema no. M- 1948; AD- 160 057.
Order from LC mi$3. 00, ph$6. 30 PB 153 249
Aa t result of the investigation of time measuring
•Vlipmeat. a system has been produced which will
precisely measure time Intervals between two pulses.
The system consists of two pulsed crystal ringing
oscillators, a coincidence detector, several gates,
and flip-flops, and two electronic counters that ac-
curately display the time difference between the start
and stop pulses and the coincidence pulse. The sys-
tem works satisfactorily for time intervals having a
range of 0. 9 to 1(X)0 >wec. All component assemblies
are commercially available with the exception of the
pulsed crysul ring oscillators and the coincidence
detector, which were designed by the Frequency Con-
trol Branch. (Author)
Battelle Memorial Inst. , Columbus, Ohio.
THERMOELECTRIC PRCFERTIES OF Bi2Te3 -
Bi2Se3 ALLOYS, by R. T. Bate. Technical rept.
no. 3 on Contract Nonr-2316(00). 15 Mar 6a IQp-
5 refs. AD-233 62S.
Order from LC mljl. aa ph$1.80 PB 153 753
Thermoelectric properties of W2Te3-Bl2Se alloys
were studied in the lower temperature region. A
technique used by Putley (Proc. Phys. Soc. (London),
68a- 35, 1955) and by Herman, Cohn, and Logan 0-
Appl. Phys. 30:1351, 1959) waa used. In this tech-
nique, the sample is suspended by fine current leads
in an evacuated can. When current passes through
the sample, a temperature gradient develops across
' it because the Peltier heat is absorbed at one end and
liberated at the other. This gradient builds up until
the rate of evolution and absorption of heat by the
Peltier effect is balanced by conduction back through
the sample and out through the leada. and by exchange
of heat by radiation between the can and the sample.
Since die temperature gradieiu produces a Se^>eck
potential, the voltage across the sample increases
until the steady-sute cottdltion is reached. Iso-
thermal resistivity vs temperature data for p-type
Bl2Te3. fi-type Bl2Te3-Bi2Se3. and commercial 3-
type Bi2Te3 alloys were plotted. The temperature
d^ndence of the realstlvlty of the alloys was simi-
lar at high temperatures while that of the p-iype
Bi2Te3 was steeper. Figure of merit (•2/x^j, where
• is the absolute thermoelectric power, >t is the
thermal conductivity, and^i is the Isothermal re-
alstlvlty) vs temperature was ploned; a decrease in
Z with decreasing temperature was shown. A plot of
temperature dependence of thermal conductivity
ahowed that the commercial alloy was independent of
temperature at low temperatures. Bi2Te3-Bi2Se3
alloys went through a broad maximum, and Bl2Te3
increased roughly as 1/T.
Boston Coll. . Qiestnut Hill. Mass.
RESEARCH DIRECTED TOWARD THE DEVELOP-
MENT OF A PULSED AIR- CORE BETATRON, by
William G. Guindon. Scientific rept. on Contract
[AP 19(604)2195]. 19 Sep 60. 47p. 4 refs. AFCRL
TN-60-822. AD- 248 588.
Order from LC mi$3. 30. phf7. 80 PB 153 822
Tbe equations of motion of an electron in a cylindri-
cally symmetric changing magnetic field are analyzed
with a view to displaying the conditions for betatron
acceleration and focussing of a betatron beam. De-
tails are given of a 36-kilo)oule capacitor bankand-
related switching apparatus which were designed
primarily for powering a pulsed air-core betatron. A
series of models of betatron coil configurations is de-
scribed, together with the method and results of
567
measuring theiif magnetic field dlttrlbutloot. Pull-
scale tests Qt a model that appeared likely to satisfy
the conditions for betatron operation proved unsuc-
cessful. In a di4cussionctf the results o< these tests,
suggestions are given for further theoretical analysis
and for experimental refinements of the apparatus.
(Author)
Brown U. CMv. of Applied Mathematics, Prorldence.
R. I.
APPROXIMATE DISTRIBUTIONS GP NOISE POWER
MEASUREMENTS, by Walter Preiberger and Ulf
Crenander Technical rept no. 2 on Contract DA 36-
039-8C-78130. Oct 58. 26p.\i refs. Rept. DA-SC-
78130/2; AD- 208 225.
Order from LC mi W- 7a ph»4. 80 PB 153 599
I
The frequency functions of certain spectral estimates
are studied analytically and numerically. An appraxi-
macion is obtaiaed for the case of a Poisaon weight
function and coqipared to the true distribution. The
eigenvalues of products of ToepUtz matrices play a
crucial role in the sampling theory of quadratic forms;
an approximation to their distribution is discussed and
its accuracy studied numerically. This leads to ap-
proaiimate probability densities which are thought to be
valid for modeiBte or even small sample sizes.
(Author)
California U . . Los Angeles .
ON MINIMUM OF MAXIMUM EXPECTED DEVIA-
T\Oti FROM AN UNSTABLE EQUILIBRIUM POSITION
OF A RANDOMLY PERTURBED CONTROL SYSTEM,
by Masanao Aoli . Rept . on Contract Nonr- 233(52).
May 60, 36p. 15 refs . Dept. of Engineering rept. no.
60-42; AD- 239 942.
Order from LC!ml$3. CO. pl46. 30 PB 149 090
A sequence of optimal control variables (an optimal
policy) is detertnined, and how such an optimal policy
depends on the f:hoice of the performance-criterion
functions is Investigated . The switching boundaries foi
minimizing the maximum expected deviation in N con-
trol stages are Shown to be different from those for
minimizing the mean of final deviation . The effective-
ness of such aDiOptimal policy when only partial infor-
mation is glvenion the random variable disturbing the
system is discussed. The performance of a certain
sub-optimai po^cy is also described. (Author)
pokey IS
Carnegie Inst j of Tech. , Pittsburgh, Pa.
ELECTROMAGKETIC PROPERTIES OF INSULATORS
FROM A MANY-PARTICLE POINT OF VIEW, by
Vinay Ambegao|ar. Doctoral thesis . Technical rept.
no. 12 on CcHitilact Nonr-760(13). Mar 60, 85p.
40 refs. AD- 23k 927.
Order from LC mi$4.80, ph$l3.80 PB 153 776
A discussion is presented, from a many particle point
of view, of the response of insulators to weak long-
wavelength electromagnetic fields . The nwdel consists
of a lattice of nuclei (supposed rigid and of cubic sym-
metry) and electrons which interact with these nuclei
as well as with each other. The Coulomb interactions
between the electrons are allowed for to all orders of
perturbation theory, and Peynman graphs are intro-
duced to describe the terms of the perturbation series
The perfect insulator is treated and results show thit
the response of this many particle system to long
wavelength electric fields of arbitrary polarization Is
exactly contained in a single frequency -dependent
dielectric constant. In the limit of long wavelengths
and low frequencies , the effects of an external mag-
netic field are included on the system. A discussiooof
the system of insulator plus one electron is glvenusiif
methods similar to those applied to the perfect insuk-
tor. The true effective mass , m* , of the extra parti-
cle is defined as the curvature in wave-vector space «(
the energy surface connecting the many particle
ground state and the low-lying excited states . The est
tral result obtained is that 'the response Af the systea
to weak long wavelength, low frequency electric fiekh
is exactly that of a single particle of effective mass
m* moving in a medium characterized by the dielec-
tric constant of the perfect insulator. The effective
mast picture of the response is thus shown to be
exact when one extra electron is added to the insulsiac
and consequently very nearly exact when a few parti*
cles are present. (Author)
Carnegie Inst . of Tech., Plnsburgh, Pa.
A STUDY OF TEM POWER TRANSMISSION, by
Frederick J. Youi«, Keith Soo Hoo. and Juda L.
Shohet . Rept . for Sep 59- Aug 60 on Contract AF
33(616)6760. Sep60, 97p. 43 refs. W ADD Technics!
rept. 60-691.
Order from 0TS)2. 25 PB 171 411
Means of Increasing the power carrying capacity pf
coaxial transmission lines are sought. A multiconduc-
tor system is devised which can handle about twice the
power per cross sectional area of conductor than an
ordinary coaxial conductor. This configuration com*
prising several concentric conductors is most useful
at frequencies where dielectric breakdown limits the
nwximum power handled. In cases where the limltlai
factor is dielectric hot spot temperature a three con-
ductor line is optimized to yield a promising impnwt-
ment over ordinary structures . Both lines devised *n
Inherently low impedance structures and must be
matched by tapered transmission lines . A field theory
solution to the upered transmission line problem is
presented. Expressions relating the upered line g8»>
metry to the Impedance transformation ratios are de-
rived. (Author)
Centre de Physique Blactronlque et Corpusculairs
(France).
WIDE DYNAMIC RANGE BARRIER GRID STORAGE
TUBE T. C. M. 16, byG. Wendt. Quarterly rept.
no. 3 on Contract N62558-2275. 1 Mar 60, 44p.
WR, 505; AD- 234 831.
OrxlerfromLC mi$3.30. ph$7.80 PB 153 809
Contents:
Some general characteristics of the TCM 16 storage
tube
Ion spot
Distortion of the output signal base by the secondar-
ies issued by the neck of the tube
Resolution curves corresponding to two possible
focus ings
Anempts to improve the gun of the TCM
Study of the behavior of the target
568
Decrease of the output signal with an increase of the
backpUte bias
Garland shaped shading
[^isnce of the number of writings on the output signal
XCM 17 tube
1X34 14 tubes with a 40 mesh per millimeter storage
grid
(See^so PB 152 092)
Certre de Physique Electronlque et Corpusculaire
(France).
WIDE DYNAMIC RANGE BARRIER GRID STORAGE
TUBE T. CM. l6[l7]byG. Wendt. Quarterly rept.
BO. 4 on Contract N62558-2275. 31 May 60, I7p.
WR. 535; AD-238 983.
(]rder from LCml$2.40, ph$3.30 PB 148 656
During the last quarter the behaviour of tube TCM 17
and its gun was examined. In this tube the beam was
modulated by the application of the Input signal to an
arrangement of deflection plates. The proportionality
between the beam current and the modulating volugc
was very satisfactory. The correction for field curva-
ture and astigmatism was carried out as in tube TCM
14-J. When the beam current was modified, a sll^t
iUft of the spot was observed on the target. This shift
was measured by means of a special tube. It was of
the order of 0. 1 mm and depended on the ratio of the
modulating voltages applied to plates 11 and 12 of the
modulator system. The Influence of this shift snd of a
certain amount of spot defocusing near the cut-off
voltage on the amplitude of the output signal, as well
*8 on the resolution, was examined with a complete
TCM 17 tube. A lowering of this amphtude below the
?alue required was observed for small values of the
writing current. The behaviour of the target in
TCM 17 was about the same as in TCM 16. Shading in
the X direction was slightly different. It was con-
cluded that the present gun for the TCM 17 was not
yet quite suitable for mounting in a memory tube
which required a linear response. It should be capa-
ble of Improvement after further development.
(Author) (See also PB 152 092)
Clevite Research Center, Cleveland, Ohio.
RESEARCH AND DEVELOPMENT OF ULTRA-
HlOl-TEMPERATURE DIELECTRIC MATERIALS
F(» CAPACITORS, by John Koenig. Quarterly rept.
DO. 2, 1 Aug-31 Oa 58, on Contraa NObs-72404.
17 Nov 58, 22p. 6 refs.
Order from LCml$2. 70, ph$4. 80 PB 154 541
This report released for sale to the public 2 Mar 61.
Ceramic discs of BaZr03, La2'I'i2(^ ^^^ ^<^ without
soma partial cation substitutions, LaAlOs, ZrTl04
aadLaNb04 were prepared. X-ray diffraction pat-
terns indicate that almost every composition was
single-phase. Up to 500°C, dc-reslstivity and dielec-
tric constant, and dielectric quality factor at 1 Mc
were measured. The dielectric constant and quality
faaor were determined at room temperature at 1 Mc
nd 100 Kc as well. BaZr03 modified by La203 and
La2Ti207 modified by Nb205 approach contraa re-
<|ulrenients in the properties evaluated so far. At
SOO^C resistivities are between 10° - 10' /1-m and
qutUty faaors in the neighborhood of 1000. Room
temperature dielectric constants are about 30 and 50
respectively changing not more than 109& up to 500°C.
(Airhor) 569
Columbia U. School of Engineering, New York.
EXPONENTIAL DETECTORS, by Christopher
Kaiteris. Technical rept. T-2/M on Contract Nonr-
266(60). 1 Mar 60, 27p. 6 refs. CU-8-60-Nonr-
266(60)-EE; AD-235 778.
Order from LC mi$2. 70, ph$4. 80 PB 153 736
Semiconductor diodes are used extensively to gener-
ate nonlinear functicms by piecewise linear approxi-
mation. The voltage -current relationship for these
diodes is of an exponential form. If a semiconductor
diode is used in conjunction with other circuit ele-
ments, the characteristics of the circuit will differ
from what would be obtained by using an "ideal" diode
This difference is greatest when the input signals are
small and the diodes are unbiased. It is Important to
determine the effect of the exponential diode relation-
ship on the output signal to noise ratio of circuits
using diodes. A good idea of the effect of the expo-
nential diode characteristic is obtained from a study
of the sisnal to noise ratio of the diode current which
results from a signal plus noise voltage applied to
the diode. A detector formed by following the diode
with a low pass filter is similarly analyzed. The re-
sults are compared to those for a square law device *
and the effect of an exponential transfer function is
discussed. (Author)
Cornell U. , Ithaca, N. Y.
A STUDY OF THE THERMIONIC POINT FILAMENT
ELECTRON GUN, by Malcobn Richard Specht.
Technical rept. no. 18 on Theoretical and Experi-
mental Investigations of the Atomic Phenomena Occur-
ring on and Near the Surfaces of Solids, Contract
AF 18(600)674. I July 60, 92p. 17 refs. AFOSR
TN-60-756.
Order from LC ml$5. 40, ph$15. 30 PB 153 830
Tlje brightness and diameter of the effective electron
source produced by thermionic point filaments of 3>* ,
2 > , and 1 m radii of curvature have been determined
as functions of the bias voltage. The peak brightness
Is found to vary between 48% and 78% of the theoreti-
cal maximum value expressed by Laogmuir's formula.
The most significant result found in this experiment li
that a minimum source diameter of about 8* can be
obtained with a point filament. The results of this In-
vestigation of the point filament electron gun Indicate
that this type of gun might advantageously be employed
in electron microscopes and electron dlffraaioo
cameras when the need for a smaller effective source
is sufficiently great to Justify die additional time and
care required to manufacture and properly align the
point filament.
Cornell U . School of Electrical Engineering,
Ithaca. N. Y.
THE MEASUREMENT OF CATHODE RESISTANCE
USING RETARDING AND ACCELERATING FIELDS,
by Eugene George Todd. Master's thesis . Technical
rept. no. 37 on Contract DA 36 - 039- sc- 64646.
15 Aug 58, 51p. 6 refs. Research rept. EE 401;
AD- 202 672.
Order from LC mi$3. 60, ph$9. 30 FB 154 420
Two methods for measuring cathode resistance under
CW conditions are described. In the first a movable
•node diode is lused to oiXAin the voltage drop «croas
the cathode costing. Measurements are taken by
placing an accelerating field on the plate of the tube.
The second method is used on a conventional parallel
plane-type triode vacuum tube. Cathode resistance
measurements are taken by placing a retarding field
on the plate of the tube. In both methods , the voltage
drgp across tt|e cathode coating is measured. Prom
knowledge at the emission current, the cathode resist-
ance is then calculated. These methods, therefore,
measure the total cathode resistance offered to the
d-c emission (^urrent. (Author)(Ai$o included in
PB 145 472)
David Samcrft Research Center, Princetoo, N. J.
' METEOR FAqSIMILE VIA METEOR TRAIL PROP-
AGATION. Final rept. on Contract AF 19(604)4102.
19Ai«60. nip. 20ref8. AFCRL-TR-60-190.
Order from LC mi$6. 00, ph$18. 30 PB 153 818
A meteor prop|tgatlon research study was initiated to
determine the irelationship of bandwidth, system gain,
duty cycle and i the picture quality for the graphic
transmission of information over ionized meteor
trails. Terminal instrumentation was developed to
L transmit and ipceive fiscaimile by meteor burst prop-
agation over 8:910 mile path on frequencies of 40. 0
and 49. 72 mc4 At the transmitter, printed text and
other test patterns were scanned at the rate at two
complete frames per second. At the receiver, an
electronic facsimile system recorded a picture when
the received signal rose above a pre -set threshold.
Tests were cotKkicted at r-f bandwidths at 27, 55,
110, and 220 hc/s. with maximum keying rates of
41.000. 92.000. 164,000. and 370, 000 binary bits
per second, respectively. The occurrence ct multi-
path delay waa relatively rare, and measured values
were in the mijcrosecond range. IXty cycle rarled
over a wide range, depending on threshold, time ct
day. and tran*nitter power. Average information -
handling capability was 2300 binary bits per second
on 220 kc/s bc«idwidth and 1400 binary bits per sec-
ond on 110 kc/s bandwidth, in the early morning.
The larger raoe with wider bandwidth indicates the
propagation medium is not a limiting factor in
achieving higher transmission rates. The synchro-
nous system, employing synchronous horizontal
■weeps at eacU ferminal provided a tool for measur-
ing relative tmnsit time of individual meteor bursts,
and improved the facsimile quality by maintaining
scanning synclronlsm independent of signal level.
(Author)
David Samoff Research Onter, Princeton. N. J.
RESEARCH A^D DEVELOPMENT ON SEMICON-
DUCTOR PARAMETRIC AMPLIFIERS, by K. K. N.
Chang, H. J ^rager and others. Scientific repc. no. I
1 Jan 59-31 AiJg 60 on Contract AF 19(604)4980.
31 Aug 60, 91i>. 22 refs.
Order from L : ml$5. 40, ph$15. 30 PB 153 268
p-n Junction diodes were designed which are not con-
ventionally m<iunted or wired. Instead, individual
units of p-n jiiictions are attached directly to a non-
dispersive slcrw-wave structure such as a helix. By
carefully moufiting three individual parametric diodes
on the helix turns, net power gains of 26 db have been
obtained. Nol^e factors of 5 to 7 db were nr^easured.
An improved version of an helix type amplifier using
18 distributed parametric diodes has achieved band-
widths of the order of 200 mc. Work on low -fre-
quency pumping was also extended to an investigatun
of the possibility of harmonic generation of milli-
meter waves using nonlinear reactances. The intro-
duction of tunnel diodes prompted an investigation of
a new set of semiconductor microwave amplifiers
and frequency conveners with a D. C pump. A tun-
nel diode amplifier was first investigated. The ex-
pressions for gain, bandwidth and noise factor of this
amplifier are shown to be analogous to those found
for a cavity-type parametric amplifier with one strik-
ing difference, the bandwidth of the tunnel diode am-
plifier is comparatively broad. The noise in the tun-
nel diode was found to be essentially of the shot-
effect type. When the tunnel diode amplifier operate*
at infinite gain, oscillation takes place. A simple
theory for a tunnel diode oscillator was derived. In
addition to amplifiers and oscillators, tunnel diodes
can be used as frequency converters. The unusual
I-V characteristic of tunnel diodes suggested a down
converter which can exhibit both conversion gain and
low noise factor. Parametric and tunnel diodes are
both two-terminal devices. To achieve four -terminal
amplifiers with these devices, a traveling -wave
scheme using a series of distributed diodes has been
suggested.
DigiUl Computer Lab. , U. of Illinois, Urbana.
A THEORY OF ASYNCHRONOUS CIRCUITS III. bjr
W. Scoa Bartky. Rept. on Contraa Nonr- 1834(27).
6 Jan 60, 53p. Rept. no. 96.
Order from LC mi$3. 60. ph$9. 30 PB 152 91$
Contents:
Section 11. C!ycllng in distributive circuits
Section 12, A general synthesis procedure
Dunham Lab. , Yale U. , New Haven, Conn.
MAGNETIC PHASE CORRECTION aRCUITS, by
Richard Clark Barker and Alglrdas J. Gruodis. Rep.
onContractAF 33(616)5018. Mar 60, 136p. 15 refs.
WADC Technical rept. 59-237; AD- 238 049.
Order from OTS %2. 75 PB 171 542
The objective of this work was to do research and
development on techniques for integration and differ-
entiation of the modulation on suppressed- carrier si|-
nals, using solid state and magnetic components. A8
of the techniques developed make use of saturable
magnetic cores, because they lend themselves to bok
long and short range storage of electrical signals. •
function necessary in any system having ocher than i
flat frequency response. Specifically, circuits have
been developed which differentiate and integrate the
modulation on a suppressed-carrler signal by, re-
spectively, taking finite differences and by accumull-
tion. Also, techniques are discussed for altering
^ magnetic amplifier design to produce integration aid
differentiation. In all cases the emphasis has been
placed upon the basic theory of operation rather thss
design for particular specifications. It has been
shown that the different types of integrators and dif-
ferentiators have many basic features in common, ^
recognition of these basic features is essential totto
full exploitation of these circuit techniques. (Author)
S70
Dunlap and Associates, Inc., Stamford, C!onn.
DEVELOPING AND TESTING THE EFFECTIVENESS
OF THE "PREMCTOR INSTRUMENT", by Charles R.
Kelley. Rept. on Contract Nonr -2822(00). 7 Mar 60,
31p. 3 refs. Technical rept. 252-60-1; AD- 234 494.
Order from LC mi$3.00, ph$6.30 PB 153 758
The predictor instrument is a newly invented display
(or use In manual control systems. The purpose of
(be present study was to develop further and to test
[fae predictor instrument as an aid to manual control.
Tlje project is concerned with 4 problems: (1) the
iffect of simplifying the fast-time simulation which
comprises the heart of the predictor display; (2) the
effea of changes in the time span for which a predic-
tion Is made; (3) the effea of changing the program of
the predictor instrument, which is based on assump-
tions made about the future position of the operator's
control; and (4) determination of ways of coding three
dimensions of information into the cathode ray tube
type predictor display. Research so far completed
was principally concentrated on the second and third
of these problems, which have proved to be the easiest
to equip for. Although the predictor instrument has
many other applications, research so far was con-
centrated on vehicular control systems. It was for
the most part, limited to cathode ray tube display
configurations In which one or more tracM are shown
to represent predicted system output from present
dBC continuously to a point in the future. (Author)
Bltel-McCulloug^, Inc . , San Carlos , Calif.
CERAMIC TUBES DEVELOPMENT FOR EXTERNAL
HEAT SOURCES, by John F. Richter. Rept. for
8 June 59-7 June 60 on Receiving Tubes , Contract
AF 33(600)39665. June 60, 43p. 6 refs. WADD
Technical rept. 60-565.
Order from OTS $1 . 25 PB 171 492
The material, design, and processing problems
tssociated with the development of an electron tube
structure capable of sustained operaticm by means of
an external radioisotope heat source are discussed.
The adaptation of an existing ceramic -metal , planar
structure for use with an existing polonium 210 heat
source in a proof-of- principle device is described,
•nd performance of this device during and after its
successful demonstration is reported . The limitations
of the planar structure are discussed and design
experiments utilizing a cylindrical structure with an
electroformed cathode, are described. Affirmative
conclusions are drawn as to the feasibility of the cy-
lindrical structure. On this basis, recommendation is
made to utilize the cylindrical structure as the basis
for development of a practical tube . (Author) .
Electronics Research Lab. , U. of California,
Berkeley.
NdSE IN CROSS- FIELD EUECTRON BEAMS, by
T. Van Duzer. Rept. on Contraa DA 36-039-8C-
IS278. 23 May 60, 207p. 65 refs. Series no. 60,
tsaueno. 280; AD-245 161.
Order from LC mi$9. 30: ph$31 .80 PB 153 937
Microwave amplifiers and oscillators employing elec-
tron streams which move through mutually perpen-
dicular electric and magnetic fields have been found
to have characteristically large outputs of broad-band
noise pxjwer. The present investigation concerns the
causes of the mMse. Particular emphasis is placed on
the behavior of the stream in the elearon-gun region.
A method of measuring the velocity distribution in an
accelerating croesed-fleld beam was devised and ap-
plied to the study of a beam in a simple gun. An anal-
ysis of the high-frequency behavlcM- of the croesed-
fleld potential-minimum was performed to study the
effea of the magnetic field. The propagation of cur-
rent and velocity fluctuations along accelerating
crossed- field streams was studied theoretically.
(Author)
Electronics Research Lab. , U. at California,
Berkeley.
STUDY OF CROSSED-FIELD AMPLIFIERS, by
J. R. Whlnnery, C. K. Birdsall and others. Quarterly
progress rept. no. 2, 1 May- 31 July 60, on Contraa
DA 36-039-SC-85278. [1960] 23p. 12 refs.
AD-245 160.
Order from LC ml$2. 70, ph$4. 80 PB 153 938
Changes were made in the single-anode velocity ana-
lyzer to increase the accuracy of velocity distribution
measurements at the inner edige of the beam and also
to facilitate measurement of noise current In samplea
across the beam. Diocotron gain in the gun region is
discussed; an approximate calculation of noise figure
for • crossed-field amplifier is presented. A noise
figure of 20 db is obuined in a particular case. Elec-
tron trajeaories in a crossed-fteld potential minlmun)
are calculated with and without time-varying perturba-
tion of the static paential. Electrons can be trapped
at the minimum for special conditions on the
perturbation. (Author) (See also PB 152 562)
Engineering Research Associates, Inc. , St. Paul,
Minn.
STATIC READING OF MAGNETICALLY STCMIED
DIGITAL INFORMATION, by S. M. Rubens. Rept. on
Ckjntraa NObsr^2001. 21 Aug 51, 34p. 1 ref.
PX 29501
Order from LC ml$3.00, ph)6.30 PB 154 747
This report released for sale to the pubUc 16 Mar 61.
It has been demonstrated that the harmonically-
variable reluaometer type of static reading device
can be used satisfaaorily to read magnetically-re-
corded binary digital information. With the circuits
developed in this investigation, the device operates
successfully and reliably for reading in contaa rec-
ords of 100 bits per inch or less (recorded in contact)
so long as the equipmetu is in continual readiness for
use (tubes "warmed up").
General Telephone and Electronics Labs. , Inc. ,
Bayside. N. Y.
STUDIES OP ELECTRON TUBE MATERIALS AND
THERMIONIC EMISSION PROCESSES. Scientific
rept. no. 1 for 1 Apr-30 June 60 on Contract
AF 19(604)7286; Continuation of Ultrapure Nickel
Studies. Contract AF 19(604)5213 and Studies of the
Reaction between W and AI2O3, Contract
AF 19(604)4083. 1 Aug 6a 5lp. JO refs. TR 60-704-
104-204-206-208.2; AFCRL-TN -60-993; AD- 247 123.
Order frc»n LC mi$3. 60, ph$9, 30 PB 153 431
571
Wort continued ofa ttm dgftiapuevti d experimental
tubes adapted to Kudy the theimioolc properties of
^yiA» cattiodes applied on an ultrapure nickel base
with a minimum trf uncontrolled chemical ccntribu-
tkns. An important phase of this work is the preps -
radon of ultrapure nickel for cathodes. In connection
with the study of the chemical reaction between tung-
aien and alumina the Installatian in the new spectrom-
eter source of the components previously fabricated
and assembled was started. A thermionic emission
micrtMCope ada{Xed for research on emission phe-
nooicm la described. A review is presented of ex-
latiaf instrumentation. (Author)
Hazeltine Electronics Corp. , Little Neck, N. Y.
DEVELOPMENT OF BEACON, RAMO AN/DPN-
31(XE-1), by Rol»ert Olsen. Ronald A. Orlando, and
R. F. Teseo. Fi^l technical rept. for 30 June 53-
15 Nov 57 CO Coi^ract DA 36-039- $c- 36590. [1957]
lOSp. 7 rcfs. Reft. 9905; AD- 200 945.
Order fromLCnii»5.70, ph$16.80 « 154 418
ati)<
Inatltuce at Mat|iematlcal Sciences, New York U. ,
N. Y.
DYNAMICS OF NONLINEAR STOCHASHC SYSTEMS,
by Robert H. Kraichnan. Rept. on Contraa
AF 49(638)34L July 60, 88p. 39 refs. Research rept.
no. HT-7: AFOgi-TN-60-717; AD- 245 489.
Order from LC iuHW, ph$13.80 PB 152 726
A method for triting nonlinear stochastic systems Is
described which it is hoped will be useful in both the
quantum -mechanical many-body problem and die
theory at turbul^ce. In this method the true problem
is replaced by rrtodels that lead to closed equations for
correlation functions and averaged Green's functions.
The model solutions are exact descriptions of possi-
ble dynamical sylstems, and as a result they display
certain consistency properties. The models involve
a new stochastic element: Random couplings are
Introduced among an infinite collection at similar
systems, the true problem correspcndlng to the limit
where these couplings vanish. The method is first
applied to a linear oscillator with random frequency
parameter. ApfJlcatlons then are made to the
Schrodinger equation cf a particle in a random poteo- .
tial and to Burgers* analog for turbulence dynamics.
For both problems, closed model equations are
obtained which daermine the average Green's func-
tion, the amplitude of the mean field, and die covari-
ance of the fluctuating field.
John Carroll ul , Cleveland. Ohio.
THEORY OF ULTRASONIC ATTENUATION IN
CYLINDRICAL AND RECTANGULAR WAVEGUIDES,
by E. F. Carome and J. M. Witting. Technical rept.
no. 3 on Coniraat Nonr-2577(0l). 31 Mar 6a 7lp.
8 refs. AD-235 081.
Order from LC mi^. 50, ph$l2. 30 PB 153 775
A theoretical siidy is made of attenuation of ultra-
sound in cylindrical and rectangular waveguides. The
systems treated: consist of a piston source radiating
into a bounded, pon-absorting medium and a receiver
of the same siz^ as the source. Expressions for re-
ceiver output are derived, and acoustic loss as a
function of path length is computed for various source
and waveguide configurations. Boundary conditions
corresponding to both perfectly rigid and perfectly
free walls are considered. Oscillations in receiver
output as a function of path length are predicted, and
these oscillations are especially large for the rigid
wall cases. The waveguide approach is extended to
the limiting case of radiation into an unbounded me-
dium, and results are given for both square and cir-
ular systems. In the latter case the curve of loss
versus path length agrees well with that previously
obtained using more conventional diffraction theory.
(Author)
Johns Hopkins U. School of Engineering, Baltimore,
Md.
REPRESENTATION AND ANALYSIS OF SIGNALS.
PART U. AN ORTHOHORMAL FILTER FOR EXPO-
NENTIAL WAVEFORMS, by David C. Lai. Rept. on
Contract AF 19(604)1941. 15 June 58. 52p. AFCRC
TN-58-191. AD- 152 443.
Order from LC ml$3. 60, ph$9. 30 PB 154 483
This report released for sale to the public 13 Mar 61.
A brief description is given of the mathematical notio^
such as orthogonal vector spaces, and the spectral
theory of functions and operators, which have been
widely used in physics, especially in (>jantum mechtn-
ics. Althouj^ all of these techniques have been dis-
cussed, to some extent in the engineering literature la
connection with signal theory and information theory,
they have not yet been reduced to a practical form
which can be manipulated easily. This report describes
a newly designed device which will generate sets of
orthonormalized exponential functions; measure the
coonlinates of a signal vector in the space spanned by
these exponential functions; synthesize the signal from
its vector representation by forming linear combina-
tions of the basis; transform the basis into a new basis
as desired; represent an arbitrary system by its H
matrix; and simulate the system for a given class of
signals. Experimental results are given to demon-
strate some of these important applications. A very
detailed circuit description and step -by- step instruc-
tions on the use of the equipment are given. (Author)
(See also PB 133 065 -R)
Laboratory for Insulation Research, Mass. Inst, d
Tech., Cambridge.
HIGH- DIELECTRIC- CONSTANT MATERIALS AS
CAPACITOR DIELECTRICS. A STUDY IN DIELEC-
TRIC SPECTROSCOPY, by A. von Hippel and
W. B. Westphal. Final rept. on Contract ATP0-l)lW
continued under Contract Nonr- 1841(10). Dec 59,
76p. 36 refs. Technical rept. 145; AD- 232 381.
Order from LC mi$4.50, ph$12.30 PB 152 128
A comparison was made of the electrical propertiei
for materials of normal dielectric constant (AI2O3
and Mgn03) with those of high dielectric constart
(n02. CaTlOs, SrTi03, [BaQ. 65*0. 351^03, «nd
BaTiOs). Single crystals and ceramics were Invesn-
gated from dc to the microwave range as a function d
time, temperature, field strength, and prehistory.
Three types of relaxation spectra were identified; oot
was caused by dipolar scroups in uneaual double wells,
572
•■ifT
and the other 2 were caused by charge carriers
itopped in the volume of the material or in front of
the elearodes, respectively. 0-H groups in rutile,
kjeotified by IR absorption, appeared to cause a
(flpolT spectrum by thernial excitatioa leading to
H-bond formation. The nonlinear response character-
istics of BaTiOa and (Bao^^sSrQ. 35)Ti03 were meas-
ured in the ferro- and paraelectric range and the on-
let of ferroelectricity for SrTi03 at liquid-He temper-
(ture. Some dc breakdown dau are given for ceram-
ics, and impulse and dc strength measurements on
ndla single crystals parallel and perpendicular to
tbeaxis.
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
THE DESIGN OF AN "ERROR-FREE" DATA
TRANSMISSION SYSTEM FOR TELEPHONE QR-
CUrrS, by B. Reiffen, W. G. Schmidt, and H. L.
Yudkin. Rept. on Contract AF 19(604)7400.
22 Dec 6a 30p. 12 refs. 25G-0029; AD- 248 637.
Older fnxn LC mi$2. 7a ph)4. 80 PB 153 803
ieoent experimental results verify that easily im-
plemented codes can detect essentially all errors
occurring in digital data sent over toll grade tele-
phone circuits. A two-way cotiimunications system is
described which uses these codes to detect the occur -
! of errors and requests a retransmission of any
in error. The feedback logic is described in de-
tail and the buffer required to adapt the system to
nrlous data sources is discussed. Extrapolated ex-
perimenul results indicate that the system will de-
lim data in each direction at an average rate of
miliiiliniiii Ij 7/8 the modem bit rate with a mean
tine to error of several hutxlreds of years. The
pidloaophy that guided the design of this system can
be applied to other media where hi^ noise bursts or
km signal levels occur infrequently. (Author)
Lincoln Lab. , Mass. Inst, of Tech.. Lexington
EFFICIENT ITERATIVE METHODS FOR OPTIMIZ-
ING THE PERFORMANCE OF MULTI-PARAMETER
NOISY SYSTEMS, by Harold Kushner. Rept. on Con-
tract AF 19(604)7400. 20 Oct 60. 75p. 5 refs.
22G-0043; AD-245 802.
Order from LCmi$4.50, ph$12.30 PB 152 970
The modified Keifer - Wolfowltz process is extended to
multi -parameter problems. The basic pvocess is an
iterative n^ethod of locating the maximum or minimum
of regression functions under very general conditions.
The modifications form a process that adjusts itself to
the curve being operated on such that the rate of con-
vergence is a maximum.
Little. Anhur D. . Inc. , Cambridge, Mass:
I4ETH0DS FOR PREQSION TEMPERATURE CON-
TROL, by Theodore P. Heuchling. Igor A. Black, and
Aaoe Everest. Quarterly progress rept. no. 1,
15 May- 15 Aug 60 on Contract DA 36-039-8C -85328.
(1960) 68p. AD-244 236.
Older from LC mi$3. 90, ph$ia 80 PB 153 246
Tbe purpose of this project is to study methods and
^Wices by which the temperature of a single quartz
crym*l blank can be maintained at 85°C in amt>ient
temperatures ranging from ±80^ to -55°C Two
ovens - one having an average energy input of 500
milliwatts; the other an average energy Input of 50
milliwatts - are to be investigated. The volume of
each oven must not exceed 3 cubic inches and the 500
milliwatts oven must be designed so that the crysul
within it is accessible. The design problems pre-
sented by the 500 milliwatt and 50 milliwatt ovens
were analyzed. The steady state heat flux through
the insulation aix) electrical. leads was calculated and
the type of insulation for the prototype ovens was
selected. An experimental model of the 500 milliwatt
oven was made and tested in the cold chamber. The
materials necessary to manufacture 50 milliwatt oven
were ordered. Tbe problem of the thermostatic con-
trol within the oven prompted the design of a thermo-
stat. (Author)
Lowell Technological bist. Research Foundation,
Mass.
A PHASE HEIGHT AND AMPLITUDE RECEIVING
AND RECORDING SYSTEM FC» MEASURING IONO-
SPHERIC WINDS, by Kenneth F. Klnnard and Venxm
a TUmer. Final rept. for Jan 59 -June 60 on St»ecUl-
Ized Data Recelvli^ and Recording System, Contract
AF 19(604)5461. June 6a 50p. AFCRL TR-60-4ia
Oitler from LC ml $3. 30. ph^. 80 PB153 821
This report contains a description of equipment de-
signed and built for measuring changes in phase and
amplitude of pulsed radio waves reflected from the
iofiosphere. Riase measurements are made by inte-
grating a d. c. signal over the time period between
zero crossings of the transmitted and received signals.
Amplitude measurements are made by peak detection of
gated echo pulses. Recording is in analog form on
dual -channel magnetic tape. (Author)
Marine Riysical Lab. , Scrlpps Instltutioa of
Oceanography. San Diego, Calif.
THE DETECTION OF WEAK SIGNALS BY CORRE-
LATION METHODS, by PhiUp Rudnick. Rept. on
Marine Physics Researdi, Contract NOb8r-43356.
10 J^y 52. 30p. 7 refs. SIO Reference 52-26.
Order from LC mi$2. 70. ph$4. 80 PB 154 546
This report released for sale to the public 2 Mar 61.
Marine Physical Lab. , Scrlpps Institvffion of
Oceanography. San Diego. Calif.
THE MEASUREMENT AND DETECTION OF
STEADY A.C. AND D.C. SIGNALS IN NOISE, by
CarlEckart. Rept. on Marine Physics Research.
Contract NC*)8r-43356. 4 Oa 51. 71p. 8 refs.
Reference 51*39
Order from LC ml$4.50,' ph$l2. 30 PB 154 545
This report released for sale to the public 2 Mar 61 .
[Melabs[ Inc. , Palo Alto, Caltf.
STUDY OF A PARAMAGNETIC SEARCH RECEIVER,
by Jack L. Melchor and James H. Burgess. Final rept.
for 1 Oct 57-30 Sep 58 on Contract DA 36-039- sc-
74844. [1958] 55p. 10 refs. AD- 207 750.
Order from LC ml$3. 60. ph$9. 30 PB 150 894
573
Ibe feaaibillty at usii^ organic free radical In a 500-
1000 mc paraisagnetlc receiver has been demonstrated.
Uaeful operation applies only to CW signals at present
with frequency resolution at 1 mc Serpentine lines
above a ground plane were used in the resonance teat
section. The pest section was mounted inside a sole-
noid with homogeneous field. Magnetic field at the
solenoid could be swept from a value oorrespoodiog to
resonance at 300 mc to that of 1000 mc in 0. 1 second.
Stnsiiivity erf qhe system manually swept was -SOdhm
wtien used with a narrow band 1000 cp« amplifier -
meter and -77 dhm with an added TWT preamplifier.
Comparisions <rf measured sensitivities aremade^th
theoretical seasitivUies. Although the receiver is not
competitive with the sensitivity of a video receiver In
this frequency range, it provides additional fre-
quency Information which is not available from a video
receiver. Several other uses at paramagnetic reso-
nance are suggested for systems applications.
Microwave Liab. , Stanford U- . Calif.
NUMERICAL SOLUTIONS TO THE SPACE -CHARGE
LTMITED FLpW OBTAINED BY THE SEPARATION
OF VARIABLES METHOD, by P. T. Kirateln,
R. Kantor and J. Szego. Scientlflc rept. no. 23 on
Contraa AF 19(604)1930 Aug 60, 80p. 11 refi.
M.L. rept. no. 714; AFCRL-TN-60-999.
Order from LCmU4. 50. ph$12. 30 PB 153 503
The method or aeparatlon d variables was used many
years ago by Langmuir to find a limited number d
solutions to the equations d space-charge limited
flow, in this paper a whole new class d solutions to
this problem l»y the method d separation d variables
is discussed. These new solutions are characterizad
by the curviliJiear nature of the electron trajeaoriea,
in contrast to Langmuir's, which were rectilinear.
The mathemaifcal method used here permits the re-
duction d the Ijartial differential equations deacrlbing
the flow to a set of ordinary differential equations
which are subsequently solved on a digital computer.
A large numb«r of different solutions were obtained
in this mannet and have been tabulated in this paper.
Because of their unique and varied nature, they
should find numerous applications in the field d
electron beam generation. (Author)
Microwave rtiysics Lab. . SyWanla Electric Products,
Inc . , MounMin View. Calif.
INVESTIGATIW OF MICROWAVE FREQUENCY
HARMONIC C3ENERATION IN PLASMAS, by R. P./
WWtmer. Final rept. for I Mar 57-31 Aug 58 on
Contract DA ab-039-sc-73l87. 21 Aug 58, 47p. 5 ref s .
Technical rep|. MPL-14; AD- 204 225.
Order from LCml$3. 30. ph$7. 80 FB ISO 898
Microwave Hesearch Inst. , Polytechnic Inst, d
Brooklyn, N. Y.
AN ALGEBRAIC METHOD FOR THE DETERMINA-
TION OF THE C»^N-LOOP TRANSFER FUNCTION
PROM THE CLOSED- LOOP SYSTEM FUNCTION, by
Jerry M. Mendel. Thesis. Rept. on Contract DA 30-
0e9-ORD-156q. 25 July 60, 49p. 3 refs. Research
rept. PBMRI $49-60; OOR rept. 1538. 13-E;
AD- 242 701.
Order from L : ml$3. 30, ph$7. 80 PB 153 663
The results d an iovestigation to find a new method <■
the determination d the open- loop transfer function
from the closed-loop system function are presented.
The system is a single- loop feedback control system.
A new method is developed which is algebraic and
exaa, the results of which are presented as general
equations. The method Is rapid and Increases the
circumspection of the designer in that not only is ti»
open- loop transfer function determined but also the
sensitivity of the closed- loop transfer function to dtf-
ferential variations of a parameter K, in the forwani
path, is able to be controlled within limits. These
limits are the same limits that determine the aucce»
ful calculation of the open- loop transfer function by
this new method. (Author)
Microwave Research Inst. , Polytechnic Inst, of
Brooklyn, N. Y.
CHOOSING FUNCTIONS FOR ORTHONORMAL EX-
PANSIONS, by Robert A Reiss. Rept. on Contract
DA 30-069-ORD-2646. 25 July 60. 36p. 4 refs. R«-
search rept. PIBMRI-848-60; COR rept. 2268. 3-B;
AD- 242 667.
Order from LC mi$3. 00. ph$6. 30 PB 153 «77
A method for treating the identification problem in
adaptive control systems is to approximate the im-
pulse response of the system by a series of orthogoai
eiqxjnential functions. The problem is to develop a
method for choosing the particular exponential func-
tions which gives the best approximation with the
fewest number of terms. A procedure is investigued
for the case where the system has one negative real
pole varying between two extremes known to the de-
signer and where an expansion of not over three terai
is desired. The method of optimizing the coefficiem
of a series expansion In the Integral square error
sense is reviewed, and the technique of orthogooallx-
Ing exponential funaions is shown. A one and two
term series expansion are investigated, and the opti-
mum placement of the poles of the approximating hac
tion are found for minimizing the maximum normal-
ized error between the actual and approximate im-
pulse response. Although an exaa solution is not
found In the three term series expansion, an iteratiw
procedure is suggested for calculating the ofXiroum
exponential approximating functions. (Author)
Microwave Research Insi. , Polytechnic Inst, d
Brooklyn. N. Y.
MILLIMETER WAVEGUIDE COMPONENTS, by
J. W. B. Griemsmann. Comprehensive final rept. ■
Contract DA 36-039- sc-73219. 1 May 58, 84p. 26r*
Rept. R-656-58; PIB-584; AD-201 672.
Order frtwi LC mlH 80, ph$13. 80 PB 150 W?
(Contents:
Basic research program
Special model design services
Broadband rugged power meters
Open waveguides components
Multimode studies in circular waveguides
574
lUcrowave Research Inst., Polytecluic Inst, of
Irajdyn, N. Y.
RBAUZATION OF BOOLEAN POLYNOMIALS BASED
OH INCIDENCE MATRICES , by S. Okada, Y.
Moriwaki , and K . P . Young . Rept . on Contract
AF 18(600)1505. 16 Nov 59, 37p. 41 refs. Rept. no.
R-790-59; FlB-718: AFOSR TN-59-1299; AD 230 765.
Order from LC mi$3.00, ph(6.30 FB 1S3 234
An algebraic metixxl for finding minimum switching
2-terminal networks for any given Boolean polynomial
S is established by adopting node-branch incidence ma-
trices as unknown quantities . Generators of invariant
transformaoon group of S are determined. Prime im-
pUcant Si , or any ottier equivalent polynomial & , are
expressed by loops passing the relay branch and by a
let of vectors 0^(1) modulo 2 in a branch-number-di-
nwnsional affine space. Dually open circuit conditions
Rj are expressed by a set of hyperplane covectors
P(i) of cut-sets . B^(i) and Cg(i) give realizable range
of number of nodes , branches , and degree of freedom
for each R^ and Sj . Base vectors Cp(i) of subspace
Cg(i) and all vectors Ck(i) which egress loops passing
the relay branch are determined based on linear depen-
dency. Dually B^i) gives base covectors B^l) and all
covectors B^i) of cut- sets cutting the relay branch.
Sneak paths or barriers in 8^(1) or C|^i) are eliminated
by increase of contacts . Networks of solution are ob-
tained from either B*(i) or Cq(i) by a new graphical or
alfsfcralc ambit-method, generally with addition of
some pseudo-ties Ci](i) which are loops including make
■nd break contact of a relay in series . Dually, pseudo
cuu B"^i) can be added to B*(i) for realization.
(Author)
lAcrowave Research Inst. , Polytechnic Inst, d
Brooklyn, N. Y.
A STUDY OF MULTI-PATH TRANSMISSICW LINE
FILTERS, by Kei Takiyama. Rept. on Contracts
DA 36 -039 -sc -78001 and AF 30(602)1650. 5 Mar 59,
7Sp. 1 ref. Research rept. R-693-58; PIB-621;
AD-220 851.
Order from LC mi$4 50, ph$12. 30 PB 153 598
RcMSrch is concerned with the analysis of multi-path
CTHiMnlssion line sections and their use as filter ele-
BMKS. Design techniques are developed for a filter
otMOinlng two-path line sections. The impedance and
transfer matrices for the multi-path sections and the
image parameters for these sections are derived The
corresponding parameters are obtained for the network
ooulsting of a multi-path section connected between 2
kaglba of ordinary transmission line. The conditions
under which infinite insertion loss is realized are of
particular interest in filter designs. These conditions
aad their physical meaning are examined. When many
filter sections are connected in cascade, the image
parameters are most useful for determining the char-
actarlatics of complete filters. The results of the dis-
caaaton concerning the characteristics of the image
parameters are tabulated and design equations are de-
rived for the two-path low pass filter using these
tables. (Author)
Moore School of Electrical Engineering, U. d
Pennsylvania, Philadelphia.
NEW CONCEPTS FOR RAC»0 FREQUENCY TRANS-
MISSION LINES, by Pietro P. Lombardinl, Richard C.
Schwartz, and Leon W. Zelby. Rept. for Sep 59-
July 60 on Contraa AF 33(616)6769. 31 Aug 60. 69p.
36 refs. WADD Technical rept. 60-701.
Order from OTS $1 . 75 PB 171 557
The work conuined in this report has been aimed to-
wards development of new concepta of poim-to-pcrint
transmiaaion of radio frequency energy, suitable for
general applications in air and space craft. The lines
investigated were: (a) a modified Goubeu line (b) an
elearolytic transmission line, and (c) a magneto-
ionic line. Basically, line (a) implies the use of many
directionally coupled G- lines as a way of improving
die performance of a single G-llne from the vievrpoint
of radiation losses. Experimenul results obtained
were inconclusive and further work is required, but
the study of electromagnetic wave propagation on
coated wires has been extended. Line (b) was found
too lossy for practical use. The study of line (c) was
limited to a cylindrical waveguide filled with plasma
and subjeaed to an axial magnetic field. This line
offers the possibility of simultaneous transmission in
low and high frequency bands. (Author)
Moore School of Electrical Engineering, U. d
Pennsylvania. Rilladelphla.
A STRATEGIC PATTERN RECOGNmON PROGRAM
FOR THE GAME GO, by David Lefkovitz. Technical
iKXe no. 4 on General Switching Ilieary, Contraa
AF 33(616)5886. 1 July 601 97p. I ref. WAIX) Tech-
nical note 60-243.
Order from OTS $2.25 FB 171 549
A set of "primitive" routtnes are defined for charac-
terizadon of patterns on die (X) board. Strategic
patterns are listed in a "Catalogue by primitive
classes" and organized into a tree struaure. (Audior)
Motorola . Inc . , Scottsdale , Ariz .
ELECTRONIC SURVEYING EQUIPMENT, RADAR
SET AN/PPN-13 (XE-2), byD. Zusman. Final rept.
for I June 57-30 June 59 ot Contract DA 36-039-sc-
74833. 15 Dec 59, 115p. 5 refs; AD- 244 779.
Order from LCinl$6.00, Ft4l8. 30 PB 153 595
Radar Set AN/PPN-13(XE-2) Is an electronic surveying
equipment designed to detern\ine terrestrial distances
by measuring the time required for electromagnetic
energy to traverse the distance between two points .
Two radar sets are used as beacons , one at each end
of the unknown range, to alternately transmit and re-
ceive coded pulse pairs of 440- mc energy and thus
establish a repetition period pr(^>ortional to the station
separation . A loi^ internal time delay has been added
to each equipment to place an upper limit on the mu-
tual beacoiung, or meaconing, frequency. This delay
is extracted from the total period by using a second
mode of operation called double traverse . This nK)de
reouires the signal to traverse each receiver twice
before it is retransmitted to the otiier radar set; it
also requires that delays encountered in both instances
be equal. The latter is accomplished by automatic
attenuation control of the signal during its second trav-
erse. A counter unit measures the period in both
S7S
mode* of operatloti tnd presents a direct dtgiul out-"
put in units of propagation rime, or in distance. The
difference between these readings is the one-way air-
path propagation time, or the distance in meters un-
corrected by the ihdex of refraction. Range capability
it 1 to SO nwles , frith accuracy o< 1 I part per 5000
for distances above 10 miles and t 10 feet for dis-
taiKes less than lb miles . (Author)
r^-iAa^/i « r J
.V. -iTT '^*riiiii ii ' Ei» ■
•|
Naval Ordnance Lab. , Corona. Calif.
SOLUTION OF THE GENERAL INTERFEROMETER
ANTENNA -rXFFfijRENTIAL DETECTOR PROBLEM,
by David F. Scherta. 15 Aug 60, I2p. NAVWEPS
rept. 7152; NOLC rept. 528; AD-246 906.
Order from LC m^2. 4a ph$3. 30 PB 153 294
The interferometen- antenna -differential detector is
an electromagnetic -radiation detection device that is
used in certain directional sensing functions for mis-
sile guidance systems and missile fuzing systems.
This report preseiits a derivation erf a general solu-
tion for the output voltage of a device of this type.
(Author)
Ub..
Naval Ordnance )Lab. , White Oak, Md.
FERROMAGNETIC SWITCHING, by O. J. Van Sam.
18 Mar 58, 30p. 3 refs. NAVORD rept. 6076;
AD- 159 800 I
Order from LCn^2. 70, phM- 80 PB 154 771 .
This report relea^ for sale to the public IS Mar 61.
The ferromagnetic switching process is analyzed to
detemiine the mioimum switching time and the mecba
nisms Involved injthe 180° switching processes. A
special ferromagnetic equation at mocion is presented
which is used to aiialyze both the fast ferromagnetic
switching process (irreversible domain rotation) and
the slow ferromagnetic switching procesA (180° Bloch
domain wall mov^nent). The reveraible magnetic
viacoaity coefficient is derived and from measure-
meaca made on the magnetic vlscoalty coefficient of
1/8 nrUl 4-79 Molybdenum Permalloy tape, the swltch-
iag cooscanta for $lcm and fast ferromagnetic switch-
ing are calculated; these calculations agree with
experiment. It is shown how the effective width at the
dynamic domain wall increases with an increase in the
switching magnetic field intensity. This factor and
others are applie4 to analyze the switching curve
(magneclc Intensi^ vs. the reciprocal at the switching
time) and the sliaiea of the votuge traces observed
during the switctang process. (Author)
Naval Research iLab. , Washington. P. C-
THE NRL MODEL B-5753 LCAK DETECTOR, by
C C Mlnter. S F. Andersen, and R. W. Dolk. In-
terim rept. 18 Jan 61, 9p. NRL rept. 5593.
Order from OTS ^50 PB 171 358
I
A 21 -pound portaWe Freon leak detector has been de-
valoped. Air froit the vicinity of a probe is pumpod
thrOMgh cubing so as to first pass two of the four cells
of a thermal conductivity brUfiB and then through a
lei^h of tubing atound to tile other pair of cells. Thus
if the probe is monred past a leak, the bit of Freor-
contalnii^ air unbalances the bridge first in one direc-
tion and then in thfe other. These unbalances cause the
successive dashing of a red Ught and a white Tight hi.,
the Lucite probe head, where the operator's attenUoo
is focused. Since the air flows past one end of each
conductivity cell and not through it, a lag time occurs
before the sample diffuses into the cell and reaches
the filament; this lag time Is predominant in producing
a total lag time of at least 3 to 4 seconds. Bridge
excitation is by a regulated ac power supply, and the
ac output signal when the bridge is out of balance goes
to a five -stage RC-coupled transistorized amplifier.
Printed circuit and plug- in construction facilitates cir-
cuit checking and amplifier replacement. While the
indicator gives a clear response for a Freon concen-
tration of 4 to S ppm, such sensitivity is not needed
under service conditions, where detection of the signal
produced by changing the concentration of Freon by 50
ppm is satisfactory in most cases. (Author)
Paatificia.Universidade Catolica, Rio de Janeiro
(Brazil)
SINGULARITIES OF UNEAR SYSTEM FUNCTIONS,
by Bernhard Gross and Elde Plres Braga. Rept. on
ContraCT AP 49(638)648 Sep 60, 127p. 39 refs.
AFOSR TN-60-I04; AD- 246 691.
Order fromLCmi$6.30. ph$19.80 PB 153 107
A discussion of the general, finite or infinite, homo-
geneous ladder structure with l,umped or continuously
distributed parameters is given. The use of infinite
continued fraaioo expansions for the representation of
highly singular network functions is discussed. Ex-
amples of networks with various singularities are
given. Complex singularities were found to occur
always in conjugate pairs. Branch cuts are shown to be
physically interpreted as line singularities resulting
from distributions of alternating poles and zerps which
have become infinitely dense. A method for the d««-
* mination of the locus and number of poles without
knowledge of the coordinates of the individual poles Is
given. Some problems of equivalence of networks are
discussed. Examples are given for equivalence be-
tween an infinite continuous and an infinite lumped net-
work and for eqolvalence between a finite continuous
and an infinite lumped network. (Author)
Radio Corp. of America. Harrison, N. J.
A STUDY OF ELECTRON TUBE DETERIORATION
UTILIZING KINETIC THEORY, by E. R. Schrader.
Quarterly rept. no. 1, 1 July-1 Oct 59 on Contraa
NOb8r-77637. (1959) 34p. 5 refs; AD- 227 147.
Order from LCml$3. 00, ph$6. 30 PB 154 544
This report released for sale to the public 2 Mar 61.
Research concerns the establishment of basic kinetic
characteristics on 2 tube types and detailed support-
ing work on gas evolution, sublinuition and tube proc-
essing and aging. Initial experiments give the gas
evolution vs. time for some typical receiving tube
plate materials at one representative condition of
temperature. Kinetic data was secured for 3 plate
materials showing general expected trends and clari-
fying the need for more refined testing methods. A
special test for measuring the gas, grid emission,
leakage and retarding potential grid characteristics
of tubes is described. An outline of the principles
employed in setting up a computer solution for the
Child- Langmuir equation is given. (Author)
576
Kadio Corp. of America, Princeton, N. J.
HIGH -TEMPERATURE. IMPROVED EFFICIENCY.
PHOTOVOLTAIC SOLAR ENERGY CONVERTER, by
J. J. Wysocki, J. J. Loferskl and others. Triannual
progress rept. no. 6 for 16 Mar-15 July 60 on Contract
DA 36-039-8C-78184. 31 July 60, 33p. 5 refs.
Older from LC mi$3. 00. ph$6. 30 PB 153 602
OaAs cells made by Zn diffusion using an open furnace
•re equivalent to those made in sealed ampiiles, except
(or a reduced surface concentration. Spectral response
curves on GaAs cells indicate a lifetime in the diffused
ridn of approximately 10-10 sec A spectral study of
ihtUow Si junctions with n- and p-type surface layers
yield a carrier lifetime in the base which is in good
agreement with the lifetime measured by the pulse in-
jection technique. The agreement is poor for deeper
junctions. A Light source calibrated by a standard
solar cell gives accurate measurements of the sunlight
oonversion efficiency for only those cells which have a
spectral response sin liar to that of the standard cell.
Photovoltaic effects have been seen in metal -CdSe junc
dons. The threshold for radiation damage produced by
electrons in phosphorus diffused Si appears to be sig-
nificantly higher than the threshold In boron diffused
Si. (Author)
Ray-O-Vac Co. , Madison. Wis.
LOW TEMPERATURE BA-2270AJ-XLT-1 BATTERIEl^
byj. W. Paulson. Interim rept. no. 1, 15 July 58-
15 Ai« 60. on Contract DA 36-039- 8C-78144. (I960]
21p. 1 ref; AO-244 298.
Order from LC mi $2. 70, phH 80 PB 153 935
The purpose of this work was to construct 500
BA-2270/U batteries of the flat cell type for initial and
delayed service testing. This production was preceded
by the construction of 50 preproduction hatterlei for
0 and 3 month testing. A performance of 6 to 8 hr at
-40 r is obtainable at 3 mo In the flat cell type con-
struction providing the battery can be maintained free
of construction defects causing leakage. Failure of A
sections was caused by the occasional occurrence of
microscopic pinholes in the conductive sheeting which
caused partial loss of a section by corroding off the
sliminum foil backing to the conductive sheeting, and
general leakage due to heat seal failures, causing cor-
rosion of terminal connections. Failures in B sections
waf due largely to intercell leakage plus the effects of
general leakage due to heat seal failures which caused
corroding off of terminal connections and/or cor-
rosioa of Intercell connections. Batteries tested at 0
months did not exhibit the high percentage of failures
that occurred at 3 mo. The factors causing failure,
though present initially, developed to a damaging de-
gree during the 3-mo storage period. Batteries giving
the design performance of 6 to 8 hr generally were
free of construction defects. No advantage was ap-
parent In storing at 35°F as compared to storing at
7(rP after 3 mo. Performances at 70°F were about
60 hr In a battery free of the aforementioned defects.
Where defects occur performances drop to about 30 hr.
elections are performing satisfactorily. (Author)
Raytheon Co. , Burhngton, Mass .
STUDY OF PLATINOTRON DEVICES. Quanerly
rept. no. 5, 1 Nov 59-1 Jan 60, on QKS779. Contract
DA 36-039- sc-78229. [1960] 22p. AD- 240 192.
Order from LC mi$2.70. pWj4.80 PB 153 230
Progress on the QKS779 platinotron tube is discussed.
The dibslpation density evaluation for the anticipated
slow-wave structure Indicates an aiKide dissipation
rating of 1 kw. The necessary cooling system has been
designed, constructed from commercially available
components , tested and found to be adequate. Tests
have been run on the cathode that insure the capability
of the cathode to absorb any back bombardment that
might be encountered In operation of the tube . A
small amount of hot test information has been obtained
that Indicates that the leakage currents are satisfac-
torily low. Five tubes have been constructed. Infor-
mation from the construction of these tubes has deter-
mined the direction of the mechanical design refine-
ment program . Cold testing has produced lnformati<»
about the net-work Insertion loss and phase shift. Hot
tests have been run which Indicate that voltage break-
down should not be a problem. (Autiwr)
(See also PB 150 446)
RCA Service Co. , Camden, N. J.
A PREDICTION OF AN/GRC-27 REUABIUTY, by
H. L. Wuerffel, D. I. Troxel and others. Rept. on
Contract AF 30(602)1623. 26 Aug 57, 81p. 5 refs.
RADC-TN-58-18; AD- 148 554.
Order from LC nu$4. 80, ph$13. 80 PB 154 516
Thia report released for sale to the public 2 Mar 61.
The AN/GRC-27 Radio Set is a ground base communi-
cations equipment that operates between 225.0 and
399.9 mc. The reliability analysis, conduaed on an
individual part basis, indicates a Mean Life of 399
hours for the OHnplete equipment being used imder
the typical 4:1 receive-transniit operating ratio. This
results in a Probability of Survival of 94. 2 percent for
a 24 hour period. Corresponding mean life values for
the individual components are: Receiver, 884 hours;
Transmitter 1097 hours; Modulator 2161 hours. The
electrical stress levels indicate the design to be
moderately conservative. The overall temperature
rise is about 8 to 10 degrees Centigrade but'tbe
packaging is such that localized ha spots nuy exist.
(Author)
RCA Service Co. , Camden, N. J.
A PREDICTION OF ELECTRONIC REUABIUTY
FOR THE AN/FPS-3 SEARCH RADAR EQUIPMENT,
by H. L. Wuerffel, G. J. Galanek and others. Rept. on
Contraa AF 30(602)1623. 1 Oa 57, 94p. 5 refs.
RADC-TN-58-19; AD-148 555.
Order from LC mi$5. 40, phJlS. 30 PB 154 844
This report released for sale to the public 16 Mar 61.
There are three general methods for predial on of re-
liability for complex systems. The methods are: part
count, complete reliability analysis, and sampling. A
random sampling technique was applied in the analysis
of the AN/FPS-3. This technique is an anempt to ad-
vance the art of reliability predial on by reducing time
and cost factors. Through the use of this random
sampling approach the AN/FPS-3 is prediaed to have
the mean life (i.e. mean time betweeti Random Fail-
ures) atid probability of survival values shown below,
assuming an equipment ambient temperature of 20°C
sn
Equipment
|«feanUfe
|(Hour»)
ProbabiUty of Surviv«l(5y
for 24 hours
72
90
81
Overall
AN/FPS-3 74
Tower Groups 221
Building Groups 111
(Author)
Research Lab. d Electronics, Mass. Inat. d Tech. .
Cambridge.
QUARTERLY PtOGRESS REPORT NO. 52, by
J. B. Wiesner, <$. & Harvey, and H. J. Zimmermann
Rept for (30 At«)-30 ^4ov 58 on Contract DA 36-039-
8C-64637. 15 jaq 59, 203p. 88 refa.
Order from LC |n49. 3a ph$31. 80 PB 154 190
This report relebsed for sale to the public 16 Mar 61
Contents: '
Physical electrotilcs
Microwave gaseous discharges
Plasma dynamic^
Solid state physics
Low temperature physics
Thermoelectric processes and materials
Microwave spectroscopy
Nuclear magnetlt resonance and hyperflne structure
Microwave electronics
Atomic beams
Siroboscoplc research
Frequency modulatloo
Statistical communication theory
Process analysis and synthesis
Processing and transmission of information ^
Artificial intelligence
Sutistlcal thermodynamics
Speech communication
Physical acoustics
MechanicAl translation
Communications! biophysics
Neurophysiology
Signal detection py human (4>servers
Network synthesis
Circuit theory '
Noi«e in electron devices
Linguistics J
(See also PB U:! 556)
Sperry Microwave Electronics Co. , Clearwater,
FU.
S- AND L-BAND FERRTTE ATTENUATORS FIXED
CN-O/CT. by B. Duncan, W. Helthaus and ochers.
Interim developdient rept. no. 4, 15 Apr-14 July 58,
on Contract AF 30(602)1724. 15 Aug 58. 25p. 6 refs.
Sperry rept. no^ 200-13019-4; RADC-TN-58-269;
AD- 148 930.
Order from LC inl$2. 70. ph$4. 80 PB 154 805
This report rel^sed for sale to the public 16 Mar 61
S-band 9ui>pres»?r: Improved attenuation charaaerls-
tics were obtained by better control of magnetic bUs;
transitions wera designed, and the fabrication of parts
was initiated for the final model, ^-baod suiwn-esscr:
Broadbandlng methods and heat dissipation problems
were investigated.
Stanford Electronics Labs. , Stanford U. . Calif.
ACTIVE NETWORKS; PAST, PRESENT AND FU-
TURE, by J. G. Linvlll. Rept. on Contract Nonr-
225(24). 10 May tO, lip. Technical rept. no. 1507-1;
AD- 238 165.
Order from LC mi$2. 40, ph$3. 30 PB 148 411
The decade of the forties saw the full-scale develop-
ment of the feedback system and the assessment of the
limitations inherent In the parasitic elements that
always accompany active componems. The problem of
realization of low-drift structures in the presence of
drifting elements was attacked. The first encounter of
the network theorist with elements that refuse to be-
have like a simple model brought new ideas and ap-
proaches. The fifties wss the decade of the transistor.
The transistor, less capable of simple representation
than Its predecessors, offered new capabilities to re-
ward the network designer. The physicist and netwoit
theorist, each being now more dependent on the other,
have been drawn together. Many of the old problems
have been re-solved without the earlier simplifying
assumptions. The pressure to make more complex,
more compact and faster systems bids to make the
sixties the decade of integration of the device with the
circuit. The key problems Inherent in this area are
Just now emerging. Their solution will depend on cer-
tain foundation lines drawn earlier, but with detailed
character that is new. The purpose of this paper is to
trace the development of areas of emphasis in the field
of active networks, to note the evolution a< its char-
acter with the changes occurring in its scope and thea
finally to look briefly at the opportunity it presents In
the future. (Author)
Stanford Research Inst. , Menlo Park, Calif.
INVESTIGATION OF METHODS OF SCANNING THE
BEAMS OF LARGE ANTENNAS, by W. F. Gabriel
and M. G. Andreasen. Scientific rept. 12. 1 Mar-
31 May 60, on Contract AF 19(604)2240. Sep 60,
80p. 25 refs. SRI ProJ. 2184; AFCRL-TN-60-1106;
AD- 246 455.
Orderfrom LCml$4.50, phJ12.30 PB 153 20S
An Investigation is presented of both electrical and
mechanical methods for scanning the beams of large,
ground-based antennas . The compound interferometer
is discussed as a possible radar anteniu. The com-
pound interferometer is a radio astronomy antenna
which has a single-lobed power radiation pattern of the
form sin ^a, with approximately half the beamwldth
of a conventional antenna of the same aperture dimer
sion. In addition, this antenna offers the unique advw
tage (A almost unlimited apenure conservation (reiic-
tion In the number of elements) with savings of 75 to
95 percent readily attainable. When operated in
"pseudomonopulse" fashion, rather than being phase-
switched, it can have a gain commensurate with the
anMXint of active aperture (number of elements) em-
ployed. High sidelobes are a major problem with diii
antenna, although, for radar point target situations,
they can be reduced to the extent of near-eliminatioa
by means of simple video circuit techniques . As an
aid to better undersundlng of antennas of this type, •
brief review section is included on the application d
Fourier Transform Techniques to amenna analytil.
Linear antenna arrays with differently spaced ele-
ments are discussed. A linear array with variable
578
ipadiV may approximate a desired space factor bet-
ter ttMn a similar array with constant spacing. Some
netbods of synthesizing linear arrays with variable
ipaclng are considered. Most methods for finding the
array parameters involve the solution erf telrly com-
plicated systems of equations . (Author) (See also
PB 149 543)
Stanford Research Inst. , Menlo Park, Calif.
THEOREnCAL LIMITATIONS ON THE BROAD-
BANDING POTENTIAL OF ANTENNAS, WITH AP-
PLICATION TO CAVITY BACKED SLOTS AND
OTHER ANTENNAS, by A. VasslUadis and
R. L. Tanner. Technical rept. no. 71 on Contract
AF 19(604)3458. Aug 60, llOp. 12 refs. SRI ProJ.
2494; AFCRL TN-60-997; AD-246 316.
Order from LC ml$5. 7a ph$l6. 80 PB 153 097
A method is presented whereby, for a given anteima.
the maximum bandwidth poasible for a certain VSWR
la eatlmated. The optimum bandwidth is obuined by
applying the lumped element circuit theory, so that a
rational function approximation to the antenna input
impedance must first be obtained. The functions used
ate sufficiently complex so that a good approximation
to the aitenna impedance is obtained up to a frequency
where the wavelength approaches the alze of the an-
tenna. The method is applied to a number of slot an-
tennaa. The effects on optimum bandwidth of such
factors aa end-loading, depth d tlie backing cavity,
width of the slot, and electrical size, are discussed.
An an example of a commonly used practical antenna
the E-fed VOR cavity antenna is treated. Finally,
the method is applied to both simple and folded dipole
antennas, and it is shown that the folded dipole has a
poorer broadbandlng potential than the equivalem
simple dipole. The superiority of the simple antenna
la very slight for antennas with half length greater
dian A/8, but becomes pronounced for antennas
appreciably shorter than this. (Author)
Itehnische Hochschule, Vienna (Austria).
HYI»ODYNAMICAL TREATMENT OF PLANE
ELECTRON FLOW, by H. Potzl, O. Hintringer, and
K. Rlchter. Annual technical rept. no. 1, 1 Nov 58-
31 Oct 59, Contract DA 91-591 -EUC-986. 30Nov59. 64p.
56 refs. AD- 231 358.
Order from LC mi$3. 90, ph$ia 80 PB 153 276
A simplified approach tothe problem of one-dimensional
electron flow is given. The present method Is based on
the transport equations of macroscopic particle density
and momentum (hydrodynamlcal equations) which are
(terlved from the LiouvlIIe equation. Results of differ-
ent approadmatkx) methods are compared with density
function results for the sutlonary case and it is seen
that the assumption of constant kinetic temperature is
promising. The equations of the Isothermal diode
problem are solved for the sutlonary and non stationary
cue neglecting the ac behavior of kinetic temperature.
For the stationary case a solution can be given In .
closed form which is continuous in the potential mlni-
mian plane. CXfferent types of isothermal diode flow
are discussed. An analytical expression was derived
for the ac solution. In the experimental part, noiae
measurements on plane diodes at 2 mc are described.
Ibe results show a less rapid decrease of the sup-
pression factor with increasing plate voltage than all
existing theories predict. The suppression factor it
between 0. 5 and 2 mc Independent of frequency and has
a wavy form originating from elastically reflected
electrons. Noise measurements on plane diodes in a
longitudinal magnetic field show dependent on magnetic
field strength, sharp noise peaks at certain plate
voluges. (Author)
Telephonies Corp. . Huntington. N. Y.
THE DESIGN AND FABRICATION OF FOUR AUDIO,
ACCESSORIES DESIGNED FOR USE WITH BROAD-
BAND FM RADIO EQUIPMENT. AND ONE CESIGNED
FOR USE WITH FOUR WIRE AUTOMATIC FIELD
TELEPHONE SETS, by Harold C Rowehl and William
S. Craig. Final engineering rept. for 27 Nov 57-
30 Apr 60 on Contract DA 36-039-8C-74880. 30 Apr 60.
118p. 21 refs. Rept. no. 235-25; AD- 242 747.
Order from LC ml$6.00. pb$18.30 PB 153 228
This report covers the design and fabrication of five ,
audio accessories. The development of the AN/VRC-12
brought about a need for appropriate audio accesscn-ies
for use with forward area combat radio communicatioo
equipment. This report discusses the difficulties en-
countered in meeting performance requirements with-
out abrogating the weight, shape, or size requirementa
Ulustrarions. tabular dau and text are used to sub-
stantiate conclusions reached and equipment design.
The human engineering and engineering feasibility
portions of this project are reinforced by the "Human
Factora Report", submitted as an Appendix to this
report. Universal application of compooenta is
stressed throughout the report and; consistently. Is
emphasized in the design of these audio acceasoriea.
(Author)
t
Wisconsin U. , Madison.
SURFACE WAVE, ANTENNA AND MICROWAVE
FILTER ENGINEERING RESEARCH STUDY, by
Elmer H. Scheibe. Quarterly progress rept. no. 2,
1 Dec 59-29 Feb 6a on Contraa DA 36-039- sc- 78326.
31 Mar 60. 18p. 10 refa. AD-243 872.
Order from LC ini$2. 4a ph$3.30 PB 153 243
A reasonably complete study of a one stage constant
Input Impedance microwave branching filter was made.
A sinqde sweep frequency generaimr formed by apply-
ing a sawtooth voltage to the repeller of a klystron
was used to tune and adjust the filter. The measured
and predicted characteristics of die filter were In
good agreement. Work on the two stage branching
filter will now proceed. Work on the design and coa-
structloD of an open resonator for making loss
measurements on a waveguide beam line was surted
in this period. It is hoped the resonator will be
completed and ready for test during next period.
(Audxn-) (See also PB 153 242)
Wisconsin U., Madison.
SURFACE WAVE, ANTENNA AND MICROWAVE
FILTER ENONEERING RESEARCH STUDY, by
Elmer H. Scheibe. Quarterly progress rept. no. 3,
1 Mar-31 May 60. on Coocract DA 36-039-8C-78326.
30 June 60, 28p. 10 refs. AD- 242 437.
Order from LC ml$2. 70. phj4. 80 PB 153 244
sn
A brief cHBCtwslon. with llltiatrations by means at
pbotographs, of the various filter configurations used
in the comptete filter study is given in this report.
The study of a vmo stage constant impedance micro-
wave branching filter was completed. Tills study in-
volved t))e design, fabrication, and final testing d the
filter. The nrte4sured char aaeri sties al the filter
were in ezcelleiK agreement with those predlaed from
the equivalent circuit. Work on the construction ct an
open resonator to be used for making loes measure-
meats on a waveguide beam line was continued.
(Author) (See ajso PB 153 243)
Ordnanc*, Missiles, and Satellite Vehicles
[Aero- Space Labs. ] North Anierlcan Aviation Inc. ,
Downey, Calif i
DESIGN, DEVELOPMENT, AND TESTING OF AD-
VANCED PNEUMATIC SOLENOID VALVE (SINGLE-
PASSAGE) PART NO. 4683-59302, by Charles P.
Bacha . Subcontraa to Rocketdyne, Contraa
AF 04(647)160. Nov 59, 126p. 8 refs. Rept.
MD 59-79; AFBMD TR-59-18; AFBMD Doc. no. 60-
862; AD- 232 180-
Order from LC »ni$6. 30, ph$19. 80 FB 153 613
Design, development, operation, and analysis of a
single -passage pneumatic solenoid valve are de-
scribed. Results of performance demonstration, flight
rating, and qualification tests are given and analyzed.
Sundard test equipment used is listed, and descrip-
tions are given of procedures and arrangements for
special tests suth as combined environment and limit
tests. Conclusitns derived from test results are
sttted, along with reconmiendatloas for further
derelopnieat. (^uthar)
Aerojet -Generlil Corp. , Azusa, Calif.
HYPER VELOCITY -DATA RECORDING SYSTEMS (A
CXJMPREHENSIVE BIBUOGRAPHY), by J. L. Squler
end G J Woffinden. Rept. on Contract AF 06(603)4558.
Feb 59, 88p. 538 refs. Aerojet rept. no. 1541 (Supple-
ment); APGC-Tll-59-33 (U); AD- 216 294.
Order from LCtniM 80, ph$13. 80 PB 154 968
This report released for sale to the public 16 Mar 61 .
References are listed by subject in 4 categories; opti-
cal, radiation, tlectrical, and mechanical methods.
Some of tlie references are listed several times, each
under a different heading. Hils is not a complete
bibliography in the field of high speed instrumentation.
(Author)
Aeronautical Research Lab. , Air Force Research
Dlv. , Wright -I^atter son AFB, Ohio.
A SUPER -FAST RECORDER FOR DAY AND NIGHT
OBSERVATIONS OF SPACE VEHICLES USING A
UGHT AMPUFIER CAPABLE OF SUPPRESSING
THE BACKGROUND AND DISCRIMINATING MOVING
OBJECTS, by Radames K. H. Gebel. Rept. on Re-
search on the Quantum Nature of Light. Nov 60, 21p.
18 refs. ARL Technical note 60-109.
Order from OTS $0.75 PB 171 108
The usefulness of the closed circuit television light
amplifier system capable of suppressing the back-
ground and discriminating moving objects is empha-
sized fcr detecting, tracking, and photographing
missiles, etc. , in flight. Special pick-up tubes have
been developed which produce video signals from
moving objects only and the mechanism involved is
explained for two (Afferent solutions. The importance
of these solutions consists in that it is the pick-up
tube itself rather than any auxiliary electronic com-
puter, which dellvera a signal representing the mov-
ing abject only. The improvements which may be
expected by using an image converter tube as light
intensifier between an optical system and the photo-
graphic camera is briefly discussed. (Author)
Air Force Ballistic Missile Div. , Air Research and
Development Command, Inglewood, Calif.
RELIABILITY PROGRAM FOR BALUSTIC MISSILE
AND SPACE SYSTEMS 1 June 59, 23p. AFBM Ex -
hiblt 58-10; Supersedes WDT Exhibit 57-3 d
16 Aug 57 and 23 Dec 57.
Order from LC ml$2.70, ph$4.80 PB 154 811
This report released for sale to the public 17 Mar 6L
The purpose of this exhibit is to provide effective re-
quirements and isrocedures for implementing a relia-
bility program by the contractor to assure the attain-
ment of reliability goals and/or requirements speci-
fied by the procuring agency.
Ai research Mfg. Co., Phoenix, Ariz.
DESIGN, DEVELOPMENT, AND TESTING OT MUL-
TIPLE-PASSAGE PNEUMATIC SOLENOID VALVE
AIRESEARCH PART 319152. VOLUME I, by H. P.
Horacek, J. T. Haley and others . Final rept. on
Contract AF 04(647)163. July 60, i78p. 14 refs .
Rept. AE-7474-R, volume 1; AFBMD TR-60-179;
AFBMD Doc. no. 60-6122, vol. 1; AD-243 350.
Older from LC mi$8.10. ph$27.30 FB 153 616-1
The multiple- pas sage solenoid valve configuration de-
veloped consists of a four-way valve controlled by aa
integrally nrKxmted, internally- vented, solenoid oper-
ated pilot valve. Both the main valve and the solencrfd
valve employ double poppet and seat arrangement. The
solenoid coil developed is capable of operation over a
temperature range erf -320^ to-f 250^ with no appre-
ciable change in current. The valve is designed for
operation with cryogenic fluids in ballistic missile
press urization systems, and is capable of operating
with inlet pressures up to 5000 psig. (Author)
AI research Mfg. Co., Phoenix, Ariz.
DESIGN, DEVELOPMENT, AND TESTING OF MJL-
TIPLE- PASSAGE PNEUMATIC SOLENaO VALVE
AIRESEARCH PART 319152. VOLUME U, byH. P.
Horacek, J. T. Haley and others. (Final rept.] on
Contract AF 04(647)163. July 60. 195p. Rept. AE-
7474- R; enclosed is rept. nos . SC-5175, rev. 2, AI-
6378-MR. rev, 3, AE-7029-MR, rev. 2, AE-7030-
MR, rev. 2. AE-7518-MR; AFBMD TR-60- 179-2;
AFBMD Doc no. 60-6122, vol. 2; AD-243 351.
Order from LC mi$8.70, phJ30.30 PB 153 616-J
580
Qomeots: ......
Drtwlngs
Ptellminary specification for a four-way pneumatic
solenoid valve
Test schedules fc
Design of a combined environmental test annratus.
(^alsoPB 153 616-1)
Army Ordnance Corps, Washington, D. C
OMWANCE ENGINEERING DESIGN HANDBOOK:
SERVOMECHANISMS. SECTION 1: THEORY, C(M-
SISTINC OF CHAPTERS 1-10. Aug 59. 232p.
180 refs. ORDP 20-136.
Onlerfrom.CTS$3.50 PB 171 480
Concents:
Chap. 1. Properties erf feedback control systems
Cfaap. 2. Dynamic response
Chap. 3. Methods for determining dynamic response
of linear systems
Ctep. 4. Stability of feedback control systems
Cfaap. 5. Gain determination
Chap. 6. Compensation techniques
Cfaap. 7. Performance evaluation
Cksp. 8, Optimization methods for transient and
stochastic inputs
Cfaap. 9. Data systems
Chap. 10. Nonlinear systems
Army Ordnance Corps, Washington, D. C.
ORDNANCE ENGINEERING DESIGN HANDBOOK:
SERVOMECHANISMS SECTION 2: MEASUREMENT
AND SIGNAL CONVERTERS, CONSISTING OF
CHAPTERS 11 AND 12. K\j% 59, 129p. 89 refs.
ORCP20-137.
Order from OTS $2. 75 PB 171 481
Contents:
Cfasp. 11. Sensing elements
Oiap. 12. Signal converters.
(See also PB 171 480)
.-U
Army Ordnance Corps, Washington, D. C.
ORDNANCE ENGINEERING I^SKJN HANDBOOK:
SERVOMECHANISMS. SECTION 3: AMPLIFICATION,
OONSESTING OF CHAPTER 13. Aug 59, 224p.
62 refs. ORDP 20- 138.
Older from OTS $3. 50 PB 171 482
Cboients:
Cfasp. 13. Amplifiers used in controllers.
(See also PB 171 481) r'
Army Ordnance Corps. Washington, D. C.
ORDNANCE ENGINEERING DESIGN HANDBOOK:
SERVOMECHANISMS. SECTION 4: POWER ELE-
MENTS AND SYSTEM DESIGN. Aug 59. 206p.
97 refs. ORDP 20-139.
Older from OTS $3. 00 PB 171 483
GooMnts:
Chip. 14. Power elements used in controllers
Chap. 15. Mechanical auxiliaries used in controllers
Chap. 16. Typical procedure
Cbsp. 17. Representative designs
Chap. 18. Auxiliaries associated with servo-
mechanisms
Chap. 19. Constructional techniques
Chap. 20. Supplenr>entary tables, formulas, and
charts
(See also PB 171 482)
Army Ordnance Corps, Washington, D. C.
ORDNANCE MATERIALS HANDBOOK. CORROSION
AND CORROaON PROTECTION OF METALS.
July 57, 88p. 80 refs. Ordnance Corps Pamphlet
ORDP 20-311.
Order from LC mi$4.80. pb$l3.80 PB 154 757
This report released for sale to the public 15 Mar 61.
Army Ordnance Corps, Washington, D. C
OREWANCE MATERIALS HANDBOOC. TITANIUM
AND TITANIUM ALLOYS. Oct 56, 27p. 4 refs.
Ordnance Corps Pamphlet ORDP 20-305.
Order from LC mi$2. 70, ph$4. 80 PB 154 756
This report released for sale to the public 15 Mar 61.
Directorate of Researdi Analysis, Holloman AFB,
N. Mex.
ON THE USE OF A RADIOACTIVE SOURCE IN
THE VELOCITY MEASURING SENSING HEAD ON
A SLED ON THE HlCSl-SPEED TRACK, by Howard
E. Carr (Alabantf Polytechnic Inst. ) and Howard G.
HanscH) (U. of Minnesota). Dec 60. 46p. 16 refs.
AFOSR -TR-60- 150; AD- 248 579.
Order from LC ml$3. 30. ph$7. 80 PB 153 826
Various radiosctiye sources and means of signal de-
tection are considered for use in the velocity meas-
uring sensing head now used in the space -time systenr
at the Holloman track. Numerous advantages and
limitations of such sources and detectors are con-
sidered. The most attractive possibility is the use of
a 1 -curie gamma ray source in the 0. 1 to 0. 3 Mev
range. To obtain a detector which is suitably rugged
yet sensitive, modest development costs will be re-
quired. To date the best choice is a solid state photo-
detector with a luminescent crystal. Other detectors
are too delicate or otherwise insufficiently developed
at tfiis time. A new method of space -time determina-
tion is proposed for use once the radioactive source
technique is practicable. (Author)
Directorate of Research Analysis, Holloman APB,
N. Mex
STUDIES ON THE PROBLEM OF MONITORING THE
PLATFORM ATTITUDE OF A SLED BY OPTICAL
MEANS, by Gordon Hughes and Fred Allison, Alabama
Polytechnic Inst. Dec 60, 25p. 2 refs. AFOSR-TR-
60-149; AD-248 542.
Order from LC ml$2. 70. ph$4. 80 PB 153 825
Examination was made of several schemes, either
proposed or currently under field test, for determin-
ing the orientation of a sled -carried platform in azi-
muth, pitch, and roll. Emphasis was placed on ar-
581
ruigementg permitting • continuous monitoring at the
attitude d the pl«tft>rm by optical means during the
whole at the motior
(Author)
of the platform along the track.
[Douglas Aircraft Co. . Inc. , SanU Monica, Calif.]
3-D TRAJECTORY SIMULATION FOR AERODY-
NAMICALLY CONTROLLED MISSILES, by T. J.
Mueller, J. C. Waicer and others. [Rept. on Cootraa
DA aO-OftP-CWD-l-flSl. 8 Feb 60, I30p. 4 refs.
A260-CETM-A06.d.
Order from LC mli6. 30. ph$l9. 80 PB 154 970
TUB report released for sale to the public 20 Mar 61 .
Presented is the mathematical formulation of the
trajectory simulatltxi program A06.0 along with
ejqplanations of the geometry and mechanics involved.
Where the derivatl^ at equations is not straight-
forward, the derivitiooa are presented.
Peltman Research Lab*.
Dover. N. J.
Plcatiniy Arsenal,
ELECTROSTATIC (sENSITlVITY OF 95/5 HMX /TI-
TANIUM. 95/5 RDK /TITANIUM. 95/5 PETN/TI-
TANIUM. AND COLLOIDAL LEAD AZIDE, by
Anthony F. Taschltr and Seymour M. Kaye. Jan 61,
ll9p. 1 ref. Technical notes FRL -TN-9.
Order from LC mi^2. 40, ph$3. 30 PB 153 627
The electrostatic sensitivity of the following physical
mixtures was determined; 95/5 36 -micron HMX (Lot
DBS-l)/7-mlcron dtanium; 95/5 PETN (Lot 32)/7-
micron titanium; 9$/5 RDX (Lot PAE-ll335)/7-ml-
crco titanium; and colloidal lead azlde (IXipont). The
energy level needed to ignite these four systems was
found to be less than a 001 1 Joule. The colloidal lead
azide was most setisltive, and the RDXAtt*ni»"" '"**"
ture least sensitive. (Author)
1
Pekman Research Labe. , Plcatlnny Arsenal. Dover.
N. j.
INFRARED PHOTOMETRIC METHOD FOR DETER-
MINING ALPHA AND GAMMA POLYMORPHS IN
BETA HMX. by Fnank Pristera, Walter E. Fredericks,
and Michael Halik Nov 60, 9p. Technical
rept. FRL-TR-l9;:AD-248 550.
Order from LCml$ 1.80, ph* 1.80 PB 153 857
I
A method using inft^red spectroacopy baa been
developed whereby the presence of S^ of the alpha or
gamma polymorph! of HMX can be ascertained. The
decectioa of 3% of fihese polymorphs can usually be
•GUeved with som< experience together with the use
of prepared standards. The method uses a 5% mull of
the sample in a 0. 5-mm cell compensated with a 5%
mull of pure beu HMX. The presence of alpha or
gamma HMX produces an absorbance in the 14.0-to
14.3-mlcron regioh. (Author)
nindale
Frebank Co. , Gl4ndale, Caltf-
DESIGN AND DEViEUDPMENT OF NON-MODULA-
TING PRESSURE CONTROL DEVICES, by Erhest A.
Lamoot and Melvil|e D. Ferguson. Repc. on Contract
AF 04(647)429, Ph«ses I and II. Apr 60, 107p. Fre-
bMik rept. no. 160; AFBMD TN-60-18; AFBMD Doc
no. 60-4867; AD- 239 181.
Order from LC ml|5.70, ph$l6.80 PB 153 615
Effort is being made to show the adaptability of the
snap action concept to a family of nonmodulating prea-
sure control components for ballistic missile use. The
•nap action concept is essentially the utilization of the
reverse spring rate achieved with properly designed
belleville spring washers. Consideration was given to
the desirability of the snap action concept for (1) re-
lief valves, (2) pilot actuators, (3) high variation inlet
pressure regulators, and (4) relatively constant inlet
pressure regulators. The medium pressure switch
operated satisfaaorlly at -4230F. Use of a pressure
switch and solenoid valve to control tank pressure was
satisfactorily demonstrated, and the effects of pres-
sure switch deadband and solenoid valve delay were
shown. A snap action pilot for a pressure actuated
valve was proven as a nonmodulating regulator and u
a relief valve. Both the regulator and relief valve con-
trolled an ullage pressure satisfactorily. A nonmodu-
lating helium regulator operating directly from the
snap action device controlled ullage pressures satis-
factorily. A nonmodulating direct acting regulator for
large flows with relatively constant inlet pressures
was tested. A large snap action device for mass flows
higher than 0.25 lb/sec of hydrogen gas is considered
feasible but not practical for airborne service. Use of
the snap aaion concept as a direct acting relief valve
was proven. Ullage pressure was satisfactorily con-
trolled with nearly instantaneous opening and reseadng
within a narrow pressure deadband.
Prebank Co. , Qendale, Calif.
THE DEVELOPMENT OP ADVANCED CRYOGENIC
PRESSURE SWITCHES FOR BALLISTIC MISSILES,
VOLUME I. by Ernest A. Lamont. Rept on Contract
AF 04(647)158. Mar 60. 172p. AFBMD TR-60-85;
AFBMD Doc. no. 60-5488. vol. 1.
Order from LC ml|8 la ph|27. 30 PB 153 614-1
TWs report describes the research and development
program required for the successful development of
advanced cryogenic pressure switches. Two novel
pressure switch concepts were discovered and proven
experintentally. Advanced techniques of omnienviroo-
mental testing were employed. A switch was developed
that la adjustable between 100 and 1000 psia. Another
switch developed Is adjustable for actuatton between
10 and 100 psig Both switches have a unlq^ demSiui
adjustability. (Author)
Prebank Co. , <3endale. Calif.
THE DEVELOPMENT OF ADVANCED CRYOGENIC
PRESSURE SWITCHES FOR BALLISTIC MISSILES.
VOLUME II, by Matthew J. Farrell- Repc. on Contrac^
AF 04(647)158. June 60. 93p. AFBMD TR-60-85;
AD- 243 423.
Order from LC mi$5. 40, ph$15. 30 PB 153 614-2
Development is reported of an advanced cryogenic low-
pressure switch which functions essentially the same
as the nriedlum pressure switch previously developed
(PB 153 614-1). The switch consists of 2 pressure -
sensing diaphragms linked with an actuation shaft
which rests against a stack of preloaded belleville
582
8prli« washers. The Internal diaphragm senses op-
erating fluid pressure, and the external diaphragm
senses atmosphetic pressure. The diaphragms have
tbe same effective area ao that the unit is a gage pres
Hire sensing unit. The belleville spring washers are
preloaded by a load adjustment ring to a given set
pressure. Fluid enters the inlet port and pressurizes
die Internal diaphragm, causing a force to be devel-
aptd on the belleville spring washer mechanism. At a
preset actuation pressure, the mechanism becomes
ratable and a snap-action deflection occurs, actua-
di^a commercial electrical switching element which
is converted to the electrical receptacle. The switch
if at^uatable between 10 and 100 psig and has a unique
il^i^anil adjustment. The switch successfully wlth-
■tood the severe environmental conditions encountered
Id • ballistic missile by passing the (^lificatic»
Plight Rating Tests.
Massachusetts Inst, of Tech., Cambridge.
DEPOT SYSTEM SIMULATOR I. (ORDNANCE
LOaSTIC STUDY), by Herbert P. GalUher and LeRoy
H. Walker. Interim technical rept. no. 16 on Funda-
menul Investigations in Methods of Operations Re-
•earch, Contract DA 19-020-ORD-2684. Sep 60, 6lp.
iref. OOR rept. 968:31 -M; AD- 247 219.
Order from LC ml$3. 90. ph$l0. 80 PB 153 660
A simulation program was constructed for the IBM 704
type computer, which operates a geographic complex
of cooperating depots stocking a given item of supply
tor a captive demand. Stationary random demand pat-
terns of seleaed types are allowed at each of the
individual depots. Under appropriate controlled con-
(Udooa, stocked depots cover customers of depots
with depleted stocks while bulk Interdepot shipments
ire made to preserve balanced distribution. Periodic
or continuous review of stock in the toul complex is
used to generate and allocate constant -lead-time re-
plenishments of total stock. The simulation output in-
cludes a tabulation of average stocks, out-of-stock
frequencies, covering and balancing aalons among
the depots, and average dehvery delays due to stock
ifaoruges. It also includes a tabulation of costs in-
curred in each Individual type of supply action.
(Author)
Minneapolis -Honeywell Regulator Co., Hopkins,
Minn.
PROCESS DEVELOPMENT PROGRAM FOR THE EX-
PLOSIVE FORMING OF T54E1 MISSILE SKINS, by
A. M. House. Final sununary rept. on Coitfract
DA 11-022-501 -ORD- 2662. 21 June 60, 71p. 33 refs.
Technical document 42060; Serial no. 24905;
AD- 240 799.
Order from LC mi$4.50, ph$12.30 PB 154 769
Tills report released for sale to the public 15 Mar 61.
Studies were made of explosive forming techniques
for die production of skin parts for the Little John
missile. The best results were obtained when 6061
Al alloy preforms were solution heat-treated and then
placed In a cold box until ready for forming. This
•ging process resulted in 6061 -T6 tensile and yield
tnechanlcal properties which exceed values specified
for the part. The dies were fabricated from 4140 cast
•taal with the die cavity machined to the nominal di-
mensions of the formed skin. The explosive charge
was 39 in. of 100- grain Petn detonating cord. Water
was used as the medium. Metallurgical examination
showed the skins formed by this process consistently
had better properties than those produced by odier
methods.
Naval Ordnance Test Sutlon. China Lake, Calif.
DEVELOPMENT OF THE SIGNAL. PLASH. MK 49
MOD 0 FOR THE TERRIER BT-3 MISSILE AND
THE SIGNAL, FLASH, MK 56 MOD 0 FOR THE
OORVUS MISSILE, by J. W. Haldeman. Sep 6a 19p.
2 refs. NOTS TP 2452; NAVWEPS rept. 7055;
AD- 247 758.
Order from LC ml$2. 40, ph$3. 30 PB 153 487
The Signal, Flash. Mk 49 Mod 0 (Terrier BT-3) and
Signal. Flash, Mk 56 Mod 0 (Corvua) were developed
to evaluate the fuzea of the respective mlasilea. The
design made eacb signal operable with the missile.
The brilliant flash produced by the signal indicates
fuze functioning in the telemetering head at the time
the missile Intercepts the target. In producing such a
flash, the signals meet requirements of abort function-
ing time, constant performance under all service con-
ditions, and compatibility with their respective mis-
siles. The signala are aafe for handling and for use in
the two missiles. Tests were carried out in more than
20 firings of the Terrier BT-3 missile. (Author)
Naval Weapons Lab. , Dahlgren, Va.
EXPLOSION BULGE TEST EVALUATION OF HY-100
STEEL PLATES WELDED BY AIR REDUCTION
COMPANY, INC. , by W. H. HaU. 18 Nov 60, 32p.
5 refs. NWL rept. no. 1723; AD- 248 067.
Order from LC mi$3.00^ ph|6.30 PB 153 551
HY- 100 steel material obtained from one inch and two
inch thick plates was balllstically tested and subjected
to experimental welding. Tbe technique used in weld-
ing the subjea specimens produced a generally satis-
factory weld on the HY- 100 steel plate material. The
performance of welded HY-100 steel plates compares
very favorably with that of HY- 80 and STS weldments.
Weld beads with smoother surfaces than those shown
by the subject one inch specimens would provide
welded structures with fewer stress -raisers when
subjected to eicplosive loading. (Author)
Physical Sciences Lab. . Ordnance Tank -Automotive
Command, Center Line, Mich.
APPLICATION OF FLUOROSCOPY TO INSPECTION
OF 20 mm FUZES, by Otto Renius and Gregory
Arutunian. Oct 60, 3Cip. Rept. no. RR-29;
AD-247 096.
Order from LC nii$2. 70, ph$4. 80 PB 153 447
>
Several methods of fluoroscopic viewing were investi-T
gated for 20 mm fuze evaluations. These included
(a) Five-inch electronic image intensifier viewing.
(b) Nine-inch electronic image Intensifier viewing.
(c) Closed -link image orthlcon and vldicon viewing.
When X-ray generators operating in the range of 50
kvp to 200 kvp were used to irradiate the specimen
fuzes, an operator was able to detect fuze compo-
nents such as: firing pin, booster, detonator in the
^
^V
583
TCtor, and the po0itioa of the arming spring. Tech-
niques at shielding, specimen rotation, and compari-
son at ftizes, wene varied in an attempt to attain op-
timum sensitivity and ease of inspection. (Author)
Pitman -Dunn L4>s. Group, Pranltford Arsenal,
Philadelphia. Pa
GAS GBNBRATOR STUDIBS FOR HAWK ELECTRI-
CAL POWER UNIT, by L. Stiefel. Technical rept.
Nov 59. 23p. 1 i^f. Mema rept. M60-14-1:
AO-231 142.
Order from LC n|i$2. 70. [>t$4. 80 PB 153 944
A propellant chaz]ge was designed which would extend
the operating time of the gas generators of the HAWK
missile electrical power unit within the original space
limiutions. The design Involved the use of a douhle
base propellant, designated X- 13. Two end -burning
sticks are placed side by side and burned one after
the other. A crossover arrangement to ignite the
•ecoDd stick aftef burnout of the first one was de-
signed and tested. Furthermore, nylon -asbestos phe-
nolic laminate HT 5000 was found to be a satisfactory
Inaulating material to prevent premature Ignition at
the unbumed charge. Several dlfficultiea will, how-
ever, have to be overcome before the system is suit-
able for inacallatlcn in a missile. A completely re-
liable inhibiting technique will have to be established.
The temperature aensitivity of the propellant will re-
quire additional study to And the optimum operating
pressure and, finally, a means of assembling and
sealing the charges, which is compatible with the
cemperatiue cycling requirements of the unit, has not
been developed. iXuthor)
Rock Island Arsenal Lab. , IlL
SEX YEAR STORAGE PROGRAM TESTS -PACK-
AGED ITEMS, by Linden H. Wagner. Final rept.
na 6E cf 6 parts on Open, Ltaderground, 9ied and
Warehouse Packaging Storage Tests. 2 Aug 60, 84p.
Rept. no. 60-2313.
Order from OTS $2.25 re 171 111
The results are glren al the "Sfat Year Storage Pro-
gram Tests - Bi^caged Items": (a) In open storage
after 4 years at Rock Island Arsenal, Rock Islano,
minois; Red Rirer Arsenal, Tezarkana, Texas; San
Jacinto Orckiance Depot, Channelvlew, Texas, and
3 years at the Natal St^iply Depot, Bayonne,
New Jersey, ^) Va underground storage after 3 years
at Natural Cooler (Cave) Storage, Atchison, Kansas;
(c) In shed and wyehouse storage after 8 years at
Rock Island Arsenal, Red River Arsenal, San
Jacinto Ordnance Defxx, and 7 years storage at
Bayonne. In evaluating the effect at the environment
on the packaged items, open storage was the most
severe; shed storage was next; warehouse and cave
storage was the l#ast severe. In comparing the
severity at the exposure locations on the packaged
Irema, Bayonne and San Jacinto (salt water sites)
showed an increased effect. Red River Arsenal and
Rock Island Arsei)al (Inland sites) were less severe,
and AtcfaisoD, Kadsas, (cave site) showed the least
I. (Author)
Rocketdyne [Canoga Park. Calif. ]
DESIGN. DEVELOPMENT. AND TESTING OF AD-
VANCED UQUID OXYGEN TANK VENT AND RE-
LIEF VALVE, PART NO. 551430. by L. E. TomllnsoB
and R. H. Reinicke. Rept. on Contract AF 04(647)160.
Mar 60, 230p. 5 refs. R-2175; AFBMD TR-60-55;
AFBMODoc. no. 60-2288.
Order from LC mi$9. 90, ph)34. 80 PB 153 612
The purpose at this program was to develop a compo-
nent which would advance the state-of-the-art of liquid
oxygen tank relief valves. The engineering analysis
and design of the component are presented. A de-
scription at test facilities, procedures, and the re-
sults of development, performance demonstration,
flight rating, and qualification testing is given and
analyzed. Conclusions derived from test results and
recommendations for future design improvements and
applications are presented. (Author)
Robertshaw- Fulton Controls Co. , Anaheim, Caltf.
ANALYSIS, DESIGN AND DEVELOPMENT OF HKH-
FLOW HELIUM PRESSURE REGULATOR. VOLUME
1, by W. Thompson and F. Nepo. Rept. on Contract
AF 04(647)161. June 60. 473p. 4 refs. AFBMD
TR-60-72(l); AD-244 788.
Order from LC mi$ll. 10. ph$72. 60 PB 153 617-1
The analysis, design, development, and test of a high-
flow helium pressure regulator for ballistic missile
use is presented. Thefollowlng basic subdivisions are
discussed: (1) an account of extensive dynamic control
analyses performed on the developmental regulator
systems using analog computers, (2) the design and
development work, and (3) testing accomplished on
various regulator configurations. (Author)
Robertshaw- Fulton Controls Co., Anaheim, Calif.
ANALYSIS, DESKN AND DEVELOPMENT OF HCH-
FLOW HELIUM PRESSURE REGULATOR. VOLUME
2. Rept. on Contract AF 04(647)161. June 60, 333p.
AFBMD TR-60-72(2); AD-244 789.
Order from LC ml$ll. 10, ph$51. 60 PB 153-617-2
Presented are the results at two analytical studies of
transient pressure response for charging and venting
volumes through nozzles in various combinations.
These studies are printed as a separate volume to
permit them to be used as a handbook or reference
guide when similar studies are being made. One
section presents the study of a single volume connected
through a. nozzle to an infinite reservoir. The study
Covers the Isothermal and adiabatic volume condltioni
for diatomic and monatomic gases, and Includes a
generalized problem solving method. Another sectioi
presents the study of two volumes Interconnected in
series with three nozzles and two infinite reservotri.
The study covers the Isothermal condltJonrfor a moB-
atomlcgas. (Author) (See also PB 153 617-1)
Systenu Corp. of America, Los Angeles, Calif.
METHODS FOR THE CONTROL OF SATELUTES
AND SPACE VEHICLES. VOLUME I: SENSING Ah©
ACTUATING METHODS, by Robert E. Roberson, ed.
Rept . for 30 June 59-31 July 60 on Stability and
Control Investigations , Contract AF 33(616)6674.
31 July 60. 443p. 203 refs . WADD Technical rept.
60-463, Volume I.
Order from OTS $6.00 TO 171 496
584
A survey of sensors and actuators for the attitude con-
trol of space vehicles is presented with emphasis on
[he devices which presently appear to possess the
Mstest potential. Brief descriptions of each device
sie given along with published references where addi-
tloMl information can be obtained. Some of the newer
leasing and actuating techniques , on which published
Information is inadequate, are analyzed in some de-
tail. Recommendations regarding sensors and actua-
tors are made and some development problems are
described. (Author)
Systems Corp. of America, Los Angeles, Calif.
METHODS FOR THE CONTROL OF SATELLITES
AND SPACE VEHICLES. VOLUME II. CONTROL
SYSTEM MECHANIZATION AND ANALYSIS, ed. by
Roben E. Roberson. RepT on Stability and Control
Investigations, Contract AF 33(616)6674. 31 July 60,
300p. 183 refs. WADD Technical rept. 60-643, vol. 2.
enter from OTS $4 00 TO 171 553
Information of importance to the synthesis of space
vehicle attitude control systems is presented. This
Includes: (1) Survey of recent published literature on
complete attitude control systems. (2) Abbreviated
survey of the aspects of control theory which may be
of particular Interest for space vdiicle attitude control
(3) Development of the basic attitude equations of mo-
tion. (4) Investigation of inenial actuator tradeoffs.
(5) Some basic studies in synthesis. (6) System re-
sponse studies with the analog computer. (Author)
(SMalaoFB 171 496)
Sanitation and Sof«t)< Engineering
Naval Civil Engineering Lab. , Port Hueneme, Calif.
FEASIBILITY OF FLOTATION CLARIFICATION FOR
WATER TREATMENT, by J. E. Halton, W. R.
Nefalsen. and J. V. Graham. Final rept. Technical
rept. 103; AD- 248 070.
Order from LC mi$2. 40. ph$3. 30 PB 153 610
The feasibility of expanding the application at the flo-
tatlan process for waste-water clarification to turbid
water was studied. A 5-gpm experimental water-
treaonent flotation clarlfier was constructed and used
to treat naturally and artificially turbid waters.
Experiments also were made to show the effects of
water alkalinity variations on the process. Retention
ttones of about 20 minutes in the clarlfier were satis -
faaory and process control using pH meters was re-
liable. Alum dosages of about 10 gpg and sodium
tiydroxide dosages of 2. 5 gpg were required for the
water tested. When the water to be treated conuined
iifficient natural carbonate alkalinity, it was not
necessary to use sodium hydroxide. Because of high
chemical requirements, the process is not considered
suitable for further development. (Author)
Naval Radiological Defense Lab. . San Francisco,
CaUf.
THE SHELTER OCCUPANCY TEST OF 3-17
DECEMBER 1959. by W. E. Strope. H. S. Etter and
others. Preliminary rept. 4 May 60, 93p. 2 refs.
Research and development technical rept. USNRDL-
TR-418; AD-237 130.
Order frtxn LC mi$5. 40, ph$15. 30 re 154 503
This report released for sale to the public I Mar 6L
The USNRDL experimental shelter at Camp Parks.
California, was occupied continually for a period of
2 wk by 100 male volunteers. During this period, all.
aspects of the shelter environment were monitored
as well as the actions and responses of the shelierees.
Shelter facilities were tested, the effectiveness of a
proposed stielter organization and procedures were
evaluated, and the palatability and preparation pro-
cedures of several food rations were evaluated. Thia
is a preliminary report made in advance of complete
analysis of the data. (Author)
Ship Building
IlUnoiaU.. Urbana.
BEHAVIOR OF RIVETED AND WELDED CRACK
ARRESTORS, by R. J. Mosborg. Final rept. on Con-
traa NObs-65789. 31 Aug 60, I34p. 22 refs. Ship
Structure Committee serial no. SSC-122; AD-242 415.
Order from OTS $2. 75 TO 171 576
Laboratory work was undertaken (1) to investigate the
feasibility of developing a welded crack arrestor and
(2) to observe the behavior of varioua crack arresting
devices. The study was accomplished by propagating
a brittle crack, initiated by driving a wedge into a
notch at the edge of the specimen, into 2-ft and 6-ft
wide steel plates containing either (a) welded inserts
of T-1 steel (b) riveted doubler platea or (c) welded
inserts of ABS Claas C nornulized steel, which were
located at various distances from the edge of the plate.
Most of the testa were conducted at nominal stresses
between 20 and 30 kai and at temperatures between
-25 and 40 F . The progreas of the crack and the ex-
tent of its penetration in the T-l steel insert depended
primarily on the severity of the resulting eccentric
load and the width of the arrestor material. The
average speed of brittle crack propagation waa gen-
erally between 2800 and 3800 fpe and that little change
occurred in the strain across the uncracked portion of
the plate beyond the localized influence of the crack
front. A riveted doubler plate waa shown to be an
excellent form of arrestor if the discontinuity pro-
duced by Che slot in the main plate beneath was pres-
ent. However, the rivet holes did not necessarily
attract propagating cracks. In tests of specimens
with ABS Claas C nornulized steel aa the arrestor
material, a brittle crack which had propagated 12 in.
was either completely accepted or refused by the
strake of killed and normalized steel; this transition
in behavior occurred between 10 and 35 F . (Author)
N«tion«l Research Labs . , Ottawa (Canada).
COMPUTING EFFECTIVE POWERS AND ASSOCIATED
COEFFIQENTS PROM SHIP MODEL RESISTANCE
TESTS, by P. G. Morel. Sep 60, 76p. Mechanical
engineering rept. MB- 226.
Orderfrom LC mJJ4.50. ph»l2.30 PB 154 057
A detailed descrli^ioa Is given at tbe program for ana-
lyzing the resultfjof a resistance test of a ship model,
using the Bendix C|-15D digital computer. The flexibil-
ity of entering the' input data allows output data for any
size of model or sjhip in salt or fresh water at any tem-
perature, and als^ allows for different skin rough-
nesses and for tha introduction of a form factor. Be-
sides absolute values for resistance, power, and speed,
various coefficients are given. The possibility of cal-
culatii^ the tow-rope force correction for a self -pro-
pulsion test is als3 incorporated. (Author)
MACHINWY, FABRICATION, AND
ACCESSORY EQUIPMENT
Engines and Propulsion Systems
Aeronautical Research Lab. , Air Force Research
Div. , Wright -Patterson AFB, Ohio.
THEORETICAL CONSIDERATION OF NONUNI-
PORMLY CHARGED EXPELLANT BEAMS, by
Robert E. Hunter. Rept. for ]une-Aug 60 on Ion Pro-
pulsion Technique! Research. Oct 60, I8p. ARL Tech-
nical note 60-138.
Order from LC nt$2. 40. ph$3. 30 PB 150 320
Non-unlfbrmlty c4 charge -mass ratio in the expellant
beam of electrostStic thrust devices is shown to be
expressible as a power efficiency factor. Non-uni-
formity in ion beams, in the form of neutral atoms
and multiply charged ions, is examined and the con-
clusion is drawn Oiat the existence of multiply
charged ions in the specie percentages which reason-
ably can be expected from non -contact ion sources Is
not a serious prol^lem. Presently available experi-
meoul data indicate that the colloid thrust devices
will produce particles with a wide range of charge-
mass ratio, posaiibly including ions. A generalized
exponential form is assumed for the mass distribu-
tion function in terms of charge-mass ratio. The
beam efficiency iS shown to be critically dependent
upon the range of charge -mass ratio In the beam.
The presence of ions In the colloid beam is shown to
be an additional serious factor. Non -uniformity ot
charge-mass ratio in colloid expellant beams may
be serious enough to require the expellant beam to be^
filtered, for example, by a magnetic deflection, to
recover the mass carried by neutral and slightly-
charged partlclea In addition, the energy carried
by the ions may Imve to be recovered. (Author)
James ForrestaJ Research Center, Princeton, N.J.
PROJECT SQUID. Semi-annual progress rept. for
I Oct 59-31 Mar 40 on Contract Nonr- 1858(25).
I Apr 60, I02p. 4p refs . AD-236 163.
Order from LC nil$5.70, ph$l6.80
PB 154 104
Contents:
Fundamental investigation of nonsteady flow
Investigation at turbulence
Investigations in magnetohydrodynamics
Thermal conductivity and tbe viscosity of ammonia anl
hydrazine
Thermal conductivity at gases and liquids over a nop
of temperatures and pressures
Elementary reactions in combustion
High temperature reactions
Surface-catalyzed atom and free radical reactions
Investigation of reaction kinetics in high-cemperatuie
gases
Inelastic molecular collisions
Solid-propellant flame mechanisms
Ignition by hot gases , and initiation of detonation by
electric spark
Investigation of transport properties at high tempera-
ture and of gaseous combustion
Ionization in detonation waves
Total radiation from burning solid propellant strands
Turbulent flame thermometry
Plasmaflow in nozzles
(See also PB 152 155)
Naval Ordnance Test Station. China Lake, Calif.
A SYSTEM FOR CORRECTING FOR SPURIOUS
NATURAL- FREQUENCY RINGING OF ROCKET
STATIC THRUST STANDS, by John S Ward. Rept.
for 24 July -5 Sep 59. 1 Sep 60. 200. NOTS TP 2541;
NAVWEPS rept. 7569; AD-246 982.
Order from LC mi$2.40, ph$3.3Q PB 153 449
A model was designed to demonstrate the feasibility cf
a data-combinatlcm system for a large rocket -motor
static-test stand. This dau-combination system was
designed to ellnUnate effects of stand vibrations on
the thrust load-cell data- -the effects occurring due
to tbe low natural frequency of the stand. The syston
employs an accelerometer to Indicate tbe nnotico d
the rocket motor due to changes in dirust or stand
vibrations as the motor deflects the thrust load cell.
The accelerometer signal is 180 degrees out at phase
with the thrust -load- cell signal; when the two signals
are added together, the effects of spurious stand
vibrations are eliminated. The functioning of the
data -combination system was demonstrated by the
model within the accuracy of the experimental equip-
ment used. It was also found that accelerometer
phase shift will be a major problem in this system,
depending upon accuracy requirements. To maintain
an accuracy of 0.1% for this model system, an
accelerometer with a natural frequency of 9, 820 cps
or above is required. (Author)
Ultrasonic Testing and Research Lab. [Paramount,
Calif.]
APPUCATION OF ULTRASCWICS TO SOUD
ROCKET SYSTEMS, by R. E. Kleint, R. D. McKow.
and J. B. Ramsey. Rept. for June 59- Aug 60 on
Materials Analysis and Evaluation Techniques,
Contract AF 33(616)6603. Oct 60, I15p. 7 refs.WADO
Technical rept. 60-553; AD-249 103.
Order from OTS $2.50 PB 171 499
This report conulns the results of investigations to
establish the applicability of ultrasonic inspection
586
techniques to solid fuel rocket motors . Special empha-
,if was placed on the detection of unbonded areas at
tbe interfaces of solid fuel rocket motors having a
basic construction of a steel case, rubber liner and
lolid propellant bonded together in that order. The
acoustic properties were obtained for these and other
tmterials used for construction of rocket motors .
Commercially available ultrasonic inspection and re-
coixllng equipment was used to obwin data. Various
puhe-echo and through-transmission techniques were
utilized to determine optimum conditions for detecting
defects and displaying them on both cathode ray image
and C-Scan (plan view) facslnUle paper recordings .
(Author)
Machine Parts and Mechanisms
PraAlln Inst. Labs, for Research and Development,
PhlladelphU, Pa.
REFINEMENTS OF THE THEORY OF THE
INFINITELY- LONG, SELF-ACTING, GAS- LUBRI-
CATED JOURNAL BEARING, by Harold G. Elrod, Jr.
and Albert Burgdorfer. Interim rept. on Contract
ffenr-2342(00). Jan 60, 50p. 11 refs. I-A2049-10;
AO-232 705.
Order from LC ml$3. 30, phfZ. 80 PB 155 001
This report released for sale to the public 16 Mar 61.
The lubrication equations for an arbitrary Newtonian
fluid are derived directly from the general equations
for conservation of mass, momentum, and energy.
From the lubrication equations an inequality is ob-
tained for the internal film temperature rise. The
Isothermal film equations are derived, and for per-
fectly-aligned self-acting Journal bearings, a con-
servation equation is obulned. Application of this
condition to the infinitely -long gas bearing gives more
accurate pressure solutions for this case. The Katto-
Soda form of the differential equation for the in-
flnitely-long bearli^ is solved by a series expansion
in the eccentricity ratio, the first terms of which
give the original, approximate Kattcf-Soda solution,
h addition, solutions obulned numerically by digiul
ooRipuutions are presented in graphical and tabular
form for eccentricity ratios from 0 — > 0. 9 and com-
pressible bearing parameter, X^ from 0~* "
(Author)
General Electric Co. , Schenectady, N. Y.
GAS BEARING STABILITY STUDY; VERTICAL
ROTOR INVESTIGATION, by R. C Elwell, R. J.
Hooker, and R Stemllcht. Technical rept. on Contract
NoBT- 2844(00). 20 May 60. 62p. 5 refs. AD- 237 432.
Order from LC ml$3. 90, ph$10. 80 PB 148 01 1
An analytical and experlmenul study of the subillty of
vertical rotors, supported by self-acting gas bearings,
i« reported. Three main groups of results are pre-
lented: (I) Forced vibration of an unbalanced rotor.
(2) Unstable rotors with nexible drive. (3) Instabilities
of a direct driven (integral electric motor) rotor.
Methods of calculating forced vibration amplitudes due
to unbalance are presented, based on previous analyti-
cal work, and supported by the experiments reported.
The unstable behavior of a variety of rotors is pre-
sented, to Illustrate the commonness cf ha If -frequency
conical whirl, and its persistence. Methods of calcu-
lating the "threshold of half -frequency whirl" are given,
and verified by experimental results obulned on tiiree
different rotors. The technique predicts the mole of
whirl to be encountered, and is a useful design tool.
(Author)
Manufacturing Equipment and Processes
Applied Mathematics and Statistics Labs . , Stanford
U., CaUf.
ON LERNER AND SAMUELSON'S THEOREM IN
NONUNEAR PROGRAMKttNG, by Hlnrfumi Uzawa.
Technical rept. no. 79 on Contract Nonr-225(50).
25 Mar 60, 21p. 12 refs . AD-235 143.
OnJerftomLCmi$2.70, ph$4.80 PB 153 690
Lemer and Samuelson's principle of complete factor
equalization is formulated in terms of activity analy-
sis , and the range of factor endowments is character-
ized for which imputed prices of factors are identical.
In the case of (strictiy) diminishing returns to scale
and diminishing marginal rates of substitution, factor
prices are equalized if and only if factor endowments
are the same. In the case In which constant returns to
scale prevail , the range of factor endowments with the
same factor prices is determined by optimum factor
requirements In various Industries . The criteria for
equalization of factor prices are given without refers
ence to non-specialization of activity levels , as re-
quired in the Samuelscm analysis , The application of
the analysis to the factor price equalization in Inter-
national trade is not so transparent . The domain of
tector endowments for which factor price equalization
takes place is determined relatively to commodity
prices , which in turn reflect the interaction of both
demand and production structure of each country. The
condition under which factor prices are equalized by
free trade in commodities is not characterized.
(Author)
National Research Council, Washington, D. C.
MANUFACTURING IN THE CONCEPaON REGION
OF CHILE. PRESENT POSmON AND PROSPECTS
FOR FUTURE DEVELOPMENT, by Joseph H. Butler.
Doctoral thesis . Rept. no. 7 on Foreign Field Re-
search Program , Nonr- 2300(09). I960, 115p. 82 refs.
Order from LCm46. 00, ph$18. 30 PB 153 763
Contents:
The nuuiufacturing r^on delimited and Its geographi-
cal setting described
Industrial history of the region
The existing manufacturing Industries
Characteristics of production In the region
Local extractive industries as sources of raw mate-
rials and fuel
The availability of electric energy
The influence of physical site factors
The Influence of transporutlon
The region's population growth and general economic
developnient
587
Availability of products , lenrlces , and other re<]uire-
nients for use i^ manufacturing
The influence of markets
The influence of labor
The availability of capital
A synopais of tha outlook for future development of
manufacturing
u.. A. J.
ON CHAN
Princeton
PRODUCTION CHANGE COSTS AND THEIR EF-
FECT UPON INVENTORY AND PRODUCTION
POLICY, by Dan^l Orr. Research memo. no. IS on
Bcooometric Research Program. Contract Nonr-
1858(16). l3Ma3|60. 88p. 30 refs. AD-240 299.
Order from LC rDi$-4. 80. phJlS. 80 PB 149 155
r
Chapter I has foUr main purposes: the first is to de-
scribe the probletns encountered in dealing with the
type of productioti change cost visualized in this
■ludy; the second is to describe two rigorous analytic
methods (the recursive functional equation approach
of dynamic programming, and the sundard method
of obtaining the aUtionary distribution of a Markovian
inventory proces$) which have been successfully used
in conjunction with other Inventory policies and which
have been considered as possible approaches to the
present problem; I the third is to describe certain ap-
praximation te<^h4iques which have served to simplify
the computational problems frequently encountered
in dealing with inventory processes; and the fourth
is to review that portion of earlier work in which
different formulations of production change cost
appear. In Chapter II the new production policy la
described, and in an appendix the attempts to ana-
lyze this policy by rigorous analytic methods are re-
produced. The approximations based upon sequential
analysis are developed and suggested as an alterna-
tive when more rigorous analysis is not successful.
Chapter III is an Investigation of production cost and
production change cost. Support is developed for the
contention that production change costs will depeixl
(a) upon the frequency at production changes, and
(b) upon the nuniber of di^erent production rates
specified by the policy. Chapter IV is concerned with
methods for determining when the new policy is suit-
able for use; several important questions regarding
its form are answered. It is also appraised from the
sundpolnt of application. (Author)
Transport, Traction and Hoist FocilitlM
Dynamic Simulations Lab. , Ordnance Tknk- Auto-
motive Command, Center Line, Mich.
WGITAL COMPUTER PROGRAM. DRAWBAR PULL
PREDICTION WHEELED VEHICLES, by Howard C
Mottln. 15 Nov 60L 28p. 1 ref. Rept. no. RR-30:
AO-248 004. ]
Order from LC mil2, 70, ph$4. 80 PB 153 562
A digital computer program is presented for deter-
mining the drawbar pull or gradeability of a wheeled
vehicle with eitheii a standard or automatic trans-
mission. (Author)
Ordnance Test Aalvlty, Yuma. Ariz.
PLASTIC FABRIC (VINYL NYLON) VEHICLE
TARPAULINS, by LeoC. Graff. Final rept. for
26 May- 20 Nov 59. Jan 60, 15p. 3 refs. Rept.
no. OTA/TBS- 1401/483; TW-601/15: AD- 231 299.
Order from OTS %0. 50 PB 171 525
Plastic fabric (vinyl nylon) tarpaulins were installed
on an M35E7 truck and on an M105 trailer which were
then operated approximately 1 300 ml to evaluate the
auitability of the tarpaulin as a proteaive cover for
cargo vehicles. The test Item was easier to handle
and install than the standard tarpaulin and no abnor-
mal wear or deterioration resulted from exposure to
high ambient temperatures during vehicle operation
on paved and secondary roads. Further tests are
recommended to determine the durability of the vinyl
nylon fabric and the feasibility of using this fabric as
a covering for the cabs of Ordnance vehicles which
presently employ a canvas top. (Author)
Transportation Center, Northwestern U. , Evanston
111.
TRANSPORTATION GEOGRAPHY RESEARCH. Pre-
liminary rept. on Contract DA'44-177-tc-574.
1 July 60, 152p. Proj. 9R99-01-004/HT17. 13.
Order from LC miJ7. 50, ph|24. 30 PB 153 605
This report released for sale to the public 15 Mar 61.
A preliminary report is given of fundamental research
relating to areal distributional aspects of transporta-
tion resources, oriented toward the development of
transportation forecast methodology. The study In-
vestigates (1) the relation between economic develop-
ntient, natural environment, and the physical develop-
ment of transportation stock aggregates; and (2) the
relation between the location of activities, natural
environment, and the spatial distribution of transpor-
tation facilities. Transport systems of many countries
are com{)ared at one point in time and a single country
is examined over time. An "ideal -typical" historical
sequence of transport development is hypothesized
and examined, and individual -country studies are
made relating the growth of population and produCTlon
centers to transport networks. First approximations
of key variables and their relative importance are
stated. Data weaknesses are identified and sugges-
tions are made regarding necessary refinements in
data and techniques for further progress toward
predictive models. (Author)
MATERIALS
Bausch and Lomb Optical Co. , Rochester, N. Y.
INFRARED COATING STUDIES, by A. Francis
Turner. Quarterly technical rept. no. 3A, 23 Apr-
22 July 59, on Contract DA 44-009-eng-323O.
15 Sep 59. 26p. AD- 227 703.
Order from LC mi$2.70, ph$4. 80 PB 153 920
This report released for sale to the public 15 Mar 61.
588
Ptftber investigations were carried out in the employ
0ieat of PbTe as a filming material. This consisted in
tbe fabrication of a series of nine layer lew pass fil-
lers, a series of band pass filters in the ten niicron
rflgioa aa well as absorption fitters utilizing the in-
trinsic absorption of the PbTe. Combined with this
was a study of the effea of the substrate index on the
windows of low pass filters. (Author)
Horizons, Inc., Cleveland, Ohio.
MECHANISM OF GROWTH AND PHYSICAL PROP-
ERTIES OF REFRACTORY OXIDE FIBERS, by
Andrew L. Cunningham. Final rept. on Contract
Nonr- 2619(00). 14 Apr 60, 57p. 4 refs. AD-240 892.
Order from OrS $1.50 PB 171 520
A study was nude cf the growth and properties of
refraaory oxide fibers as formed from the vapor
pteae in the case of AI2O3, and from colloidal sus-
pensions in the case of Zr02, Si02 and related fibers.
The vapor phase method entails the heating of high
purity aluminum melts under carefully controlled
conditions in a hydrogen atmosphere. The presence
of controlled amounts of moisture facilitates the for-
mation of a volatile and relatively stable suboxide oi n
aliinlnum. The second approach is baaed upon rapid
drying of stabilized colloidal suspensions which resuli
In a fibering reaaion. The resultant fibers are heat-
treated and are thus rendered thermally and mechani-
cally stable. Physical testing was limited to maxi-
mum tensile strength determinations. The indicated
tensile strengths of AI2O3 fibers are much in excess
of those In the literature. Mechanical properties and
high thermal stability of both groups of fibers attrib-
ute to them a significant superiority to all other
fibers in this category, (Author)
McGraw-Hill Book Co. [Inc . . New York] .
HANDBOOK OF FIBROUS MATERIALS, by Harry
Mileaf . Rept . for July 58-July 60 on Materials Applica-
tion, Contract AF 33(616)5726. Oct 60, 495p. 19 refs .
WADO Technical rept . 60-584.
Order from OTS $6 .00 PB 171 494
This repon conuins the summarized and consolidated
information extracted from WADD Technical Repwns
covering several phases of fibrous materials research.
The information is arranged to make^the results of
these reports more readily available and useful to de-
celerator designers and others interested in the fi'
brous materials phase of Air Force research. The re-
port is divided into sections covering the pertinent
(aceu of flfirous material infortnetion . Fairly com-
plete Information is supplied on various phases of
basic design data, sewability, friction, abrasion and
weather resistance, porosity and air permeability,
temperature propenies and chemical resistance of
different yams , cords , webbings and fabrics . Some
Information is also supplied on sunlight and weather
res isunce, tear resistaiKe, radiation, aging and elee
troautlc properties, stiffness, flexibility, elongation,
siAstic recovery and energy absorption . (Author)
Naval RadUcdogicsl Defense Lab. . San Francisco,
Calif.
THE MECHANISMS OF' IGNITION OF CELLULOSiC
MATERIALS BY INTENSE THERMAL RADIATION,
by S. Martin. 10 Feb 56, 43p. 78 refs. Research and
development technical rept. USNRDL-TR-102;
AFSWP-799; AD- 108 394.
Order from LCmI$3. 30, ph$7. 80 PB 154 754
This report released for sale to the public 15 Mar 61.
Existing Information about the processes occurring In
a cellulosic solid undergoing pyrolysis is summarized
with attention dlreaed toward possible changes In re-
aaion mechanism with Increased heating rates. The
significance of such mechanism changes in regard to
the ignition event is discussed. The properties and
rate behavior characteristics of gas phase oxidation
reactions are presented along with some examples of
analytical expressions describing the temperature -
concentration profiles in the system. The combinatiaa
of heat and mass transfer widi classical reaction
kinetics is suggested as a powerful tool for uncovering
the fundamental processes involved in the ignition of
cellulose by intense radiant energy. (Author)
Pennsylvania State U., University Park,
SCABBING AND FRACTURE OF MATERIALS BY
STRESS WAVES> by Norman Davids. Final rept. for
1955-1960 on Contract DA 36-061 -ORD-465. 15 Sep6a
lOp. OOR r^. 1253:20; AD- 246 136.
Order from LC mi$1.80. ph$1.80 PB 153 661
This project has been concerned with a theoretical in-
vestigation of "scabbing" in materials. Its scope has
included an analysis of wave propagation effects and
reflection at free surfaces. Due to the broad nature
of this scope the work naturally divided into (A) Elas-
tic problems, (B) Plastic problems. Utader "scabbing
phenomena" or spalling, were Included In this study
various related types of damage embracing cracking
as a result of destructive interference by stress
waves. Under (A) linear behavior was assumed (Justi-
fied by many materials, both metal and noa-metal)
while (B) dealt with more general stress -strain and
failure criteria. (Author)
AdhMives and S«alants
Miimesota U. , Minneapcdis.
AN INVESTIGATION OF LONQTUDINAL SHEAR
DISTRIBUTION AND DAMPING IN A VISOOBLASTIC
ADHESIVE LAP JOINT, by Carlos P. Avery. Rept.
for June 59-July 60 on Metallic Materlala, Contract
AF 33(616)6828. Nov 60, 40p. 5 refa. WADD Techni-
cal rept. 60-687.
Order from OTS %l. 00 PB 171 556
An analysis of the damping in a viscoelastic adhesive
of a simple lap Joint is presented. Expressions are
developed for shear distribution and damping in the
adhesive when the lap is sheared by a low frequency
sinusoidal force. Calculations are made illustratlr^
the variation in damping and shear distribution as a
function of the dimensions and material properties of
the lap components. Experiments were performed
which confirm the theory. Limitations, extensions,
and possible refinements of the theory are presented.
(Author)
589
Naval Research Lab. . Waahington. D. C
AN ISOCYANAT3 PRIMER -SEALER FOR MASONRY,
by J. R. Griffith and G. E. Rohi. 30Jao61. I8p.
4 refa. NRL rept. 5580.
Order from OTS ^50 FB 171 107
I
A new primer- setler haa been developed for uae on a
variety of weathered masonry surfaces. It containa a
commercially available material al the isocyaoate type
which has previously been adapted to use as a bonding
ooat in the appllc«tlaa d. orfudc linings to the interior
•urfkcea al large, concrete, fuel storage tanks. A
program ia in progress in which the isocyanate primer
shows prcxnise for use as a base coating on various
masonry surfaces prior to the application of acrylic
emulsion paixica. (Author)
CMfMnio and RafroctoriM
Chicago Midway Labs. , U of Chicago, lU.
RESEARCH ON MON-OXIC« GLASSES, by W. A.
Fraaer. Final rept on Contraa DA 44-009-Eng-
3702. July 59, 55p. 24 refs. CML-TR-P153-12;
AD- 231 071. I
Order from OTS ^1.50 PB 171 526
Th* work of preparing new glasses involved two types
of operations which progressed somewhat independ-
encly al each other One type of operation waa re-
quired for preparing specific compounds suitable for
combining Into glasses. The second type was the
melting of the micures of the compoiunda to form
glasses. The techniques at producing the sulfides and
selenides were developed so that most Ol the prepara-
tions are now roKine in nature. One or two of the
preparations still present some problems which have
not been completely Investigated. However, the
majority of the compounds can be prepared quite
simply and no new development Is required with
respect to these ifiateriala. This phase of the pro-
gram can be conaldered to have been satisfactorily
completed. The program on the development of new
Don -oxide glasses produced two new glass fields, the
calcium thiogallase glaases and the calcium thlo-
aluminate glasses. A few glasses in s third field d
the calcium selenogallates were prepared. As Is
true In all new glass fields, more research and de-
velopment work it required to produce stable compo-
sitions suitsble fqr Isrge melts and for weather
stability. When the amount of time spent on this
development is considered, it is believed that a
satisfactory start has been made in the development
of new glaaaes with very good tliennal properties. A
few years sgo, it was considered unlikely that non-
oxlds glasses with annealing and softening tempera-
tures above SOO^C could be developed. Glasses In
the two new glass fields have annealing temperatures
over 500OC. (Atthor)
1
Georgia Inst, d Tech. Engineering Experiment
Station. Atlanta.
STUDY AND PRELIMINARY EVALUATION OF
CERAMIC BRAKE FRICTION MATERIALS FOR
AIRCRAFT, by W. F. ZenoniandJ. D. Walton. Rept.
for IS Apr 57-14 Apr 58 on Carriage Systems, Con-
tract AF 33(616)5191. Apr 58, 32p. WADC Technical
rept. 58-118.
Order from LC mi$3. 00, ph$6. 30 PB 154 751
This report released for aale to the public 15 Mar 61.
A laboratory friction material brake tester was de-
signed and fabricated. This tester plsces a dynaniic
test on the ssmple rather than a drag test, therefore
ntore cloaely aimulates a braking process. Samples
utilizing zlrccnls and fused silica as the main ceramic
body were fabricated. An organic realn and commer-
cially available colloidal silica were studied as Im-
pregnants for the silica base samples. Silica base
sample compoaitlans were varied by the addition of
fused slumina, calcined alumina and clay. Silica
samples impregnated with colloidal silica showed
Qonslderably better wear resistance than 8ilica ssm-
ples impregnated with an organic resin. Silica sam-
ples with refractory additiona showed friction proper-
ties and wear resistsnce thst compared very well with
those of organic friction material presently being
used In aircraft brakes. A new type of cermet desig-
nated thermltic cermet was Included In the test pro-
gram. Test dau were insufficient to permit proper
evslustlon of this cermet ss a brake friction material.
(Author)
Little, Anhur D. , Inc. , Cambridge, Mass.
INFRARED SPECTRAL EMITTANCE PROPERTIES
OF SOLID MATERIALS, by Henry H. Blau, Jr. ,
John B. Marsh and others. Final rept. on Contract
AF 19(604)2433. Oct 60. 84p. 7 refs. AFCRL-TR-
60-416; AD-248 276.
Order from OTS $2. 25 PB 171 515
Attempts to utilize s solsr furnace for high -tempera-
ture emittance and reflectance measurements were
almost completely unsuccessful. TTie basic problems
encountered were instabilities ^n specimen tempera-
ture and instabilities in incoming solsr flux. The two
are clearly cloaely related. At least some of these
difficulties could be overcome by substituting a well-
^^Y^M-r^A src furnace for the solar furnace.
National Bureau of Standards, Washington, D. C.
PHYSICAL PROPERTIES OF HlCai TEMPERATURE
MATERULS. PART V. THERMAL DIFFUSIVITY OF
MACa^BSIA-yTABIUZED ZIRCONIUM OXIDE AT
HIGH TEMPERATURES, by Howard W. Flieger, Jr.,
Friedrich P. Knudaen, and Defoe C. Glnnings. Rept.
for 31 Mar 57-21 Dec 59 on Materlala Analysis and
Evaluation Techniques, Contract AF 33(616)56-21.
Oct 60, 19p. WAEX: Technical rept. 57-374, pt. 5.
Order from OTS JO. 50 PB 171 541
^^•ir
590
1^ g part of a program developing standards of ther-
n^ coaductivity and thermal diffuaivlty of refractory
QKtcrlals at high temperatures, thermal diffuaivlty
oessurements have been made on dense polycrystal-
Uae zirconium oxide which had been stabilized with
BCgnesium oxide. The results indicate that the sta-
Mllzation of the zirconium oxide was inadequate, giv-
U^ progreaslvely increasing value* d thermal dif-
l^vlty after cycling to temperaturea d about 1200%.
Thermal expansion and X-ray measurements indicated
l^tbe Increase in thermal diffuaivlty values corre-
fmfff,*»A to a change from cubic to monoclinic crystal-
Ho* form. (See also PB 140 817)
hhval Research Lab. , Washington, D. C
PROTECTION OF REFRACTORY METALS FOR
HIGH TEMPERATURE ffiRVICE. PROGRESS RE-
P(»T1, JULY 1. 1960: THE ZINC-BASE COATING
FOR NIOBIUM, by a F. Brown, R. A. Meussner and
odrrs. 28 Nov 60. 37p. 1 ref. NRL rept. 5550.
Qttkr from OTS $1. 00 PB 161 932
IhB protective action d a zinc -base coating on ni-
rjt^^^n is due to the formation of a tight layer of ZnO.
Any breaks occurring in the oxide barrier are self-
bealed by the formation of additional ZnO resulting
from the reaction d air with zinc vapor arriving from
slac-rlch buermeullic compounds between the oxide
barrier and the niobium. The zinc- niobium phase
diagram has been determined sufficiently well toplace
the temperature llmlution of the coating at 2048*T, at
shicfa temperature the most stable niobium -zinc
compound decomposes. Alloy additions have not
raited this celling while at the same time reuining
the letf-heallng properties. No other metals have
heea found which are as satisfactory as zinc inform-
lAg protective coatings for niobium. Furthermore, it
appears that zinc is as suitable for niobium alloys as
it Is for pure nlobiian, unless these contain highper-
i:w<ig<ii d vanadium. Complex shapes can be vapor
costed, but this process does not permit the ad-
mixture with the zinc d small amounts of aluminum,
rtwahan, and zirconium, which appear desirable for
rsUabUlty, particularly in the range 1800° to 2000P.
(Author)
Nival Research Lab. , Washlr^ton. D. C
PROTECnCW OF REFRACTORY METALS FOR
meal TEMPERATURE SERVICE. PROGRESS RE-
PORT 2, OCTOBER 1, 1960: DURABILITY OF THE
ZINC- BASE COATING FOR NIOBRJM by B. F.
kowa, R. A. Meussner and others. 31 jux 61, 27p.
2r«fs. NRL rept. 5581.
Oixler frxxn OTS |0. 75 PB 171 159
Ibe cffeas d the ooatlng thickness, the method of
spptication and the temperature d application d the
ooatlng. the composition d the compounds, the
temperature o^ the test, and thermal cycling have
been examined in life tests lasting approximately 1000
bours. The beneficial effects of titanium and aluml-
nin in the coating have been indicated and the effects
of Mne transition meul additions are briefly re-
ponad. Some additional data are presented on Che nl-
<MaBi-zinc system. The report also includes some
oiwervations d the redistribution d interstitial im-
pirities in the niobium as a result d the coating and
testing procedures and the results d exploratory
studies on the oxidation d titanium -zinc and nicfcel-
zlnc alloyt. (Author) (See also PB 161 932)
New Jersey Oeramlc Research Scacion, Rutgers
[State] U. , New Brunswick.
THE GROWTH AND INVESTCATKN OF FERRO-
ELECTRIC AND ANTIFERROELBCTRIC CRYSTALS^,
by Etsuro Sswaguchi and Melvln L. Charters. Final
technical rept. for 1 Sep 56-31 Aug 57 on Contract
DA 36-039-SC-70137. Aug 57, 97p. 20 refs.
AD- 149 504.
Order from LC mi$5. 40, ph$15. 30 FB 150 899
Contents:
Peculiar hysteresis behavior of Pb^ jCbq 5TIO3
Effect or small additions of 1^, Cu, and Fb on the di-
electric properties of cadmium niobate
Effect of polarization reversal on the dielectric con-
stant of barium tltanate
Automatic bridge for measuring dielectric constant
Study preparatory to the nuclear magnetic resonance
of cadmium niobate
New York State Coll. of Ceramics, Alfred U.
METAL FIBER REINFORCED CERAMICS, by
J. R. Tlnklepaugh, B. R. Goes and ochera. Rept. for
1 Sep 59-31 Aug 60 on Ceramic and Cermet Materials
Development, Contrsct AF 33(616)5298. Nov 60, 89p.
18 refs. WADC TecSmlcal rept. 58-452, pt. 3.
Order from OTS $2. 25 FB 171 550
The flexural properties of a ceramic -metal fiber sys-
tem were studied and It was found that the meul fiber
does assume a part of the load which is to some de-
gree in proportion to the relative elasticity moduli of
the ceramic and metal. The test dau for the alumina-
molybdenum and alumina -mulllte-molybdenum sya-
tema were extended to 3000°F. Hafnium oxide was
found to have desirable characteristics for use in a
composite system. (Author) (See also PB 161 481)
Stanford Research Inst. [Menlo Park. Calif. ]
MECHANICAL PROPERTY SURVEY OF REFRAC-
TORY NONMETALLIC CRYSTALLINE MATERIALS
AND INTERMETALUC CCftffOUND^ by William a
Snlley, Leon E. Sobon and others. Rept. for
15 June 58-15 June 59 on Solid State Research and
Properties of Matter, Cootract AF 33(616)5907.
Jan 60, 333p. 1201 refs. WADC Technical rept.
59-448; AD- 234 775.
Order from LC ml$11.10, ph$51.60 FB 154 846
This report released for sale to the public 16 Mar 61.
The llterature-on the mechanical properties of nan-
metallic polycrystalline compounds and intermetalllc
compounds with melting points above 1500^ was sur-
veyed. The theoretical concepts of flow and fracture
were reviewed. It was determined that die mechanical
properties of many potential high temperature materi-
als have not been evaluated. It was concluded that the
intermetalllc compounds which are brittle at room
5(91
temperature (nd sUgbtly ductile at high temperature
(wtiere some at them are also stronger) are more
vortfay of future study than the much worked-over
orldes and inter scldal compounds. Another conclusion
d this study vas that conventional parameters, such
as tensile strength, etc. , may not be d value for de-
signing high temperature structural components, and
that data from tests closely simulating actual use
conditions ar^ necessary before the designer can con-
fidently use brittle materials. (Author)
Pu«ls, Lybricants, and Hydraulic Fluids
Phillips Petroleum Co. , Bartlesvllle. Okla.
CHEMICALLY REACTIVB SPECIES: THEIR PRO-
DUCTION. STABILIZATION, CONCENTRATION AND
STORAGE, by Raymond L. Amett. Eugene a Gutb.
and Julius R. Berreth. Pinal rept. on Contract
AF 49<638)45. Oct 59. 41 p. 10 rcfs. Research Div.
rept- no. 2478-59R; AFOSR-TR-59-190. AD- 235 428.
Order from LC ml|3. 30, ph$7. 80 PB ISO 072
The continual search for higher energy propulsive fuels
has fostered research on tbe generation and stabiliza-
tion al free radicals. The radicals are generated ]q.
iiOl, in solids \>y gamma irradiatian. Ite solids are
condensed \ow molecular weight gases. The energy
stored In these systems Is measured by direct calori-
metric observations at the apparent heat capacity d
tbe Irradiated material as compared to that for the un-
irradiated material. The apparatus for making these
measurements is described and a summary discussion
at the results is given. Curves are given showing the
the energy released as the solid Is warmed for each
tystem ezamitted. (Author)
a..
Propulsion Lib. , Wiight Air Development [DIt. ]
Wright -ftner son AFBl Ohio.
IMPROVEMEMT OF THE STORAGE LIFE OF MIL-
L-7808 OILS, by Eldred N. Cart. Rept. on Aviation
Lubricams. J«n 59, 4Ip. WADC Technical rept.
59-379; AD- 225 033.
Order from LC mi$3.30, ph|7.80 FB 154 969
nds report released for sale to tbe public 16 Mar 61.
Different additives were tested in MIL-L-7808 oils to
see if they would increase the storage life d the syn-
thetic oiL Prom this group, aliphatic amines were
found to be efl»ctlve in Increasing the storage life.
2-6, Di-tert-butyl-o-dlmethylamlno-p-cresol was
tested in three different lubricants and Improved the
storage life d these oils. However, it is possible that
this additive wtxild not be effectlTe in oils having dif-
ferent base stocks or additive package and another
compound might have to be used. Complete specifi-
cation tests w«re riai on qualified oils cosKaining 0.1%
d 2-6, di-tert<-butyl-*-dimethylamino-p-cresol, with
the additive having no effect on any d these tests.
Pour engine tests were rin on qualiflfid oils containing
0.1% d the same additive with satisfactory results.
Correlation d an accelerated oven test with tropical
storage condition is given. Prom this correlation, die
estimated Increase in storage life by the use d 2-6^
di-tert-biffyl-a-dlmethyiamino-p-cresol is about 2 is
3 years, depending on the initial storage life cf tha
oiL (Author)
Leather and Textiles
Narrlcot Corp. , Philadelphia, Pa.
THE DESIGN AND EVALUATION OF HEAT STAB-
UZED TAPES AND WEBS, by Jacob Serbin and Her-
man Becker. Rept. for May 59-May 60 on Air Force
Textile Materials, Contract AF 33(600)39447. Oa 60,
80p. WADD Technical rept. 60-252.
Order from GTS $2. 00 PB 171 416
The basic purpoae d thla work was to design and
evaluate a series of 13 representative webbings,
tapes and ribbons, which would maintain minimum
breaking strength and maximum shrinkage when sub-
jected to a temperature of 250^^ for a period of five
hours. Each of the 13 samples were to be made fron
Dupont Type 330 or 700 nylon, Chcmstrand Type RHB
nylon and Dupont Type 51 or 52 Dacron. A heat atairi-
Uizatlon process was found necessary to accomplish
the desired shrinkage. An experimental pilot pro-
gram, involving three types of stabilization proc-
esses, indicated that a "heat stabilized" continuoM
method (HSCM) using a dry air oven was the moK
practical method. Investigation has shown that, with
dxie consideration given to the strength per weight
ratio, a woven end item of nylon or Dacron can be
stabilized with a measurable degree of success.
Additional information was sought to ascertain
strengith and shrinkage of all Items at room tempera-
tures, and also after five hours at 3(Xf*P. Dacroa
items only were tested at 350°F after one hour ex-
posure. All items were checked for seam efficien-
cies In the natural state and after exposure to 250^^
and 300OF for five hours. (Author)
(Quartermaster Field Evaluation Agency, Fort Lsa,
Va.
AN INVESnOATION OF AN OBJECTIVE METHOD
FOR DETERMINING MOISTURE PENETRATION AND
ABSORPTION PROPERTIES OF END ITEMS OF
LEATHER FOOTWEAR UNDER DYNAMIC FIELD
TEST CONDTTIONS. by James C Perkins, Jr NovJO,
37p. 7 refs. Technical rept. R-8; FEA MRS 59-7L;
AD- 247 06S.
Order from LC nii$3.00, pl46. 30 PB 153 HI
This study was conducted to develop a more refined,
objective, and reliable method for determining, on a
continuing basis, the Instant and location of leak aai
the amount of moisture penetration and absorption li
leather footwear under dynamic or field conditions.
The Agency developed and tested an 8-circult mois-
ture detector and a sensing element for use in con-.
Junction with the multi-circuit detecting Instrument.
This elen»ent inctn-porates a detection principle in-
volving electrical resistance and resultant changes is
resistance aaivaied by water penetration. The
detector proved satisfaaory and completely met die
test objectives.
592
hf^cfanlsche Hochschule] Graz (Austria).
^ MICELLAR STRUCTURE OF FIBRES (CBLLU-
U06B AND CERTAIN NYLONTYPE SYNTHETICS),
n MEANS OF X-RAY SCATTERING (1). THE
fflHUCTURE AND PROPERTIES OF SELECTED
MACRCMOLECULES (NATURAL AND SYNTHETIC)
IN SOLUTION, USING LIGHT- SCATTERING AND
OTHER PHYSICAL- CHEMICAL TECHNIQUES (2), by
a Kratky. Final technical rept. for I Oct 59-
» Sep 60 on Contract DA 91-591-EUC-1253. [1960] 49p.
16 refs. AD- 247 569.
Order from LC ml$3. 30, ph$7- 80 PB 153 389
A snMll-«Qgle> X-ray method was developed and Im-
pravcd for use in experiments on the structure of fibers
ifld devices were designed for measuring the absolute
tatenslty. A method is described for ellminatlog the
obilknatkxi errors which occur in small -angle. X-ray
oposures of solutions. The degree of colling of cellu-
lose nitrate was Investigated. The chain molecules
consisted of a large number of persistence lengths
lUch decreased as the degree of coiling Increased.
Ugbt scattering measurements were made on purified
unples of cellulose nitrate In acetone. An experl-
uMBtal source of errors was thought to be microgels,
■IxMit 10 rimes as large as the molecules themselves.
For studies of their super-molecular striKrture, thick
fibers were prepared Isotropic with regard to X-rays
iosn air swelling (P. H. Hermans and P. Platzek,
Z. Physik. Chem. Leipzig, A185:260. 1939) range
from about 1. 03 to 2. 2. Light scanering measure-
ments indicated that the particles separated from each
odwr were of an order d magnitude uniform among
dMBSelves, the micelles. Investigations were also
lOfflKl with low-concentration HoO solutions of the
ooDtent of the spinning gland of the silkworm at differ-
ent sates of biological development.
Plastics
Nsval Supply Research and Development Facility,
Isyonne, N. J.
TRANSPARENT PACKAGING, by S. Stambler.
C Katz, and S. Gordon. 3 May 60, 78p. Engineering
npt no. 2.5082. AD- 246 061.
Older from OTS $2. 00 PB l7l 532
TUs report released for sale to the public 7 Apr 61
w PB 153 198.
This report presents the results of a study to evalu-
■e transparent films for packaging appUcatlotis. It
sas determined that no one film could be used as an
•U purpose military barrier material. Four mil low
density polyethylene and laminations of mylar and ,
polyethylene may be used as additional miliury bar-
rier materials and provide the added property of
ttSBsparency. Perfonnance requirements based on
the needs of the military supply system were de-
vtkiped for transparent films. (Author) v
Osanermaster Research and Engineering Center,
Mmck, Mass.
THB OPTICAL AND MECHANICAL PROPERTIES OF
HIGH POLYMERS, by Joseph D. Loconti, Nathaniel S.
Schneider, and Harold W. Coles, eds. Rept. on a
Series of Lectures by Richard & Stein, University d
Masaachuaetts. Mar 6a 281p. 69 refa. Reaearcfa rept
High Polymer series no. 14.
Order from LC ml$ll. la phM2. 60 FB 153 62B
This report released for sale to tbe public 15 Mar 61.
Contents:
Statistics of chain configurations
Kinetic theory of rubber elasticity
Birefriitgence of rubberlike networks
The flow of annorphous networks in the rubbery state
Molecular theories of relaxation time distribution
The glassy state
The crystalline sute
Measurement of orientation in crystalline polymers
Mechanical properties of crystalline polymers
Ultimate mechanical properties of polymers
MATHEMATICS
Aarhus U. (Denmark).
A COMBINATORIAL LEMMA FOR COMPLEX NUM-
BERS, by Glen Baxter (U. of Minnesou). Technical
scientific note no. 1 on [Grant] no. AF AF06R-6I-4.
1 Nov 60, 7p. 3 refs. AFCISR-TN-60-1419;
AD- 248 006.
Order from LC ml$l. Sa ph$I. 80 PB 153 646
Let S be any permuution of 1 throMgh n. Each fixed
permutation S determines a set of points in the com-
plex plane, which in turn determines a convex hull.
Properties of the set of convex hulls generated aa S
ranges over all permutations are investigated. For
example, the average number of sides in each of the
convex hulls is found to be IndependeA d the com-
plex numbers. The combinatorial results are used to
analyze properties of sums of complex -valued, in-
dependent and identically distributed random varl*
ables. (Author)
Air Force Cambridge Research Labs. , Bedford,
Mass.
AN ALGORITHM FOR FINEHNG RATIONAL AP-
PROXIMATIONS, by H. P. Mattson, Jr. Sep 60, 22p.
6 refs. AFCRL-TR-60-I96. AD-248 573.
Order from LC ml$2. 70.' pbK 80 PB 153 806
Scientific work frequently requires numerical values of
functions. Although much general information Is often
known about these functions, values of them are never-
theless often difficult to compute; although in almost
all cases some method for making this computation,
however lengthy it may be, is known. The purpose of
a rational approximation to a function is to provide a
rapid and convenient way to calculate numerical values
of the function to within a predetermined error. This
paper considers the question of how to find rational ap-
proximations to given functions. There appear defi-
nitions of terms, a precise sutement of what tbe cri-
terion of best fit Is, and statements of some classical
results. Two closely related iterative methods for
finding best rational approximations are defined. A
proof of convergence of these methods is given for a
593
■pedal caae (in which both tnedwds are die s«ine)aiid
these methods axe compared with some others. Some
reauks obtained by one of the methods are presented,
together with a brief description at the computer
pgoHimi used ti) obtain them. (Author)
Applied Matheautlcs and Statistics Labs.,
atanfcrd U. , QallL
APPUCATIONS OF SEMI-MARKOV PROCESSES TO
COUNTER AND RELIABIUTY PROBLEMS; by Rich-
ard Barlow. Technical rept. no. 57 on Contract N6onr
251(40). 29 Apr 60, 96p. 35 rets. AD- 238 360.
Order Crona LC ^^.40, ph$lS.30 FB 148 419
1^ A class at coiBitiBr problems Is solved using the tech-
^^ nique at the embedded semi-Marked process. A new
J feature consists at input processes which are non-
rcnewaL In order to sohre these problems, some Ira-
portant properties of finite semi -Markov processes
are developed. A unified treatment is made at a large
I / class at repairman problems which arise in reliability
' theory. These problems are identified with appropri-
ate stochastic models from qpeuelng and telephone
trunking theory. (Author)
s^at
Applied Mathe^tlcs and Statistics Labs. . Stanford
U., Calif.
BILATERAL BIRTH AND DEATH PROCESSES, by
William E. Pruitt. Technical rept. no. 22 on Contract
Nonr-225(28). IB May 60, 137p. 12 refs. AD- 237 626.
Order from LC|nl$6.90, ph$21.30 PB 148 092
AppUed Matbefiatlca and Sudatlca Laba. , Stanford
U., CaHf. I
EXPONENTIAL POLYNOMULS ON OOMMUTATIVB
SEMIGROUPS, b^r Jeremy J. Stone. Technical rept.
BO. 14 on Contract AP 49(638)294. 2S Nov 60. 74p.
11 refa. AFOSR-TN-60-1097; AD-248 780.
Order fromLCmi^.SO, pb$l2.30 PB 153 860
AppUed Matheitiatlcs and Statistics Labs . . Stanford
U., Calif.
A GBOMErrnc proof of the bieberbach oon
JECrURE FOR THE FOURTH OOEFFIQENT, by
Z. Charzynski atid M. SchlfTer. Technical rept.
no. 86 on Contract Nonr- 225(11). 23 Mar 60, 16p.
7 refs. AD-234 732.
OrderfrmiLC «ii$2.40. ph|3.30 PB 153 689
Let F be the fkn^ly of all analytic functions which are
regular and univtlent In the unit circle |z|<0 and
possess the Taylor development f(z)-z ♦stz^ ■♦•a3Z^ ♦
. . . ♦agZ°^. ... An alternative proof of meberbach's
conjecture Isnlj^n Is presented for the Inequality
la^l ^4. The proof Is modeled after that of
Garabedian-Schiffer for the inequality |a3| ^3 (Annals
of Math. 61:116-136, 1955). Each exiremum problem
with respect to tbe coefficients aj^ leads to exiremum
flinctlans f(z) £ P which map the unit circle into a slit
domain whose boundary curve satisfies a first order
differential equation whose coefficients depend on the
»^. An auxiliary extremum problem in F which can be
solved completelV due to its particular structure is
considered. Theunequality [a4l <4 is then derived
by combining the new inequality wlt^ some known and
elementary es unices for the coefficients a^.
Applied Mathematics and Sutlatlcs Laba. ,
Stanford U. , Calif.
A NEW proof of THE BIEBERBACH CONJEC-
TURE FOR THE FOURTH COEFFICIENT, by
Z. Charzynaki and M. Schiffer. Technical rept.
no. 85onContraaNanr-22S(ll). 15 Feb 60, 16p.
4 refa. AD- 232 835.
Order from LC mi$2. 40, ph(3. 30 FB 153 131
Elementary methods are shown to be sufficient to
establish the proof at the theorem that the fourth co-
efficient In the Taylor aeries at a function f(z), uni-
valent in the unit circle, satisfies the inequaUty
fa4| i 4. The methods are based on the Grunsky
nequallty which can be derived elementarily by the
uae at the Schwarz Inequality and the standard meth-
ods at contour integration. A new proof is given of
the Grunsky inequality based on variational methods.
Applied Mathematics and Statistics Lab. , Stanford
U., Calif.
ON STURM SEQUENCES FOR TRIDL^GONAL
MATRICES, by J. M. Ortega. Technical rept. no. 4
on Contraa Nonr- 225(37). 15 Feb 60, 9p. 3 refa.
AD- 232 679.
Order from LC ml$l . 80, ph$l .80 PB 153 144
Applied Mathematics and Statistics Labs . , Stanford
U., Calif.
THEORY AM) APPUCATIONS OF THE SEQUENTIAL
DESIGN OF EXPERIMENTS, k-ACnONS AND IN-
FINITELY MANY EXPERIMENTS. PART 1. THBORX
by Stuart A.Bessler. Technical rept. no. 55 on
Contract N6onr-25140. 31 Mar 60, 51p. 13 refs.
AD-235 276.
Order from LC ml$3.60, ph$9.30 FB 153 68S
The theory of sequential design of experiments is a
formulation of the experimentation-decision procedure.
A k-actlon problem Is discussed In which the space of
possible experiments is infinite. The assumption it
made that there are 2 actions and that the number of
possible state of nature is finite. Tlie sequential prob-
lem is shown to exhibit s risk which Is ssymptotlcally
equal to -c log c/I(e) as c tends to zero. 1(8) Is a
measure of information . The procedure remains u-
ymptotically optimal In the sense that, for any proce-
dure to do significantly better than the sequential pro-
cedure for some value of the parameter, it must do
worse by an order of magnitude for some other values
of 0 . Sicveral examples are considered: problems
which Involve the Identification of several known but
untagged populations , procedures for checking thft-
reUability of a 2 component system, and problem of
determining which of 3 populations has the greatest
mean . A means of measuring the efficiency of an aili
trary procedure is presented, and, in each example,
the efficiencies of a common alternative procedure is
completed .
Brown U. Dlv. of Applied Mattiematlca, Providence.
R. I.
AN ESriMATE OF THE SPECTRUM CW A STA-
TIONARY TIME ^RIES, by R. H. Jones. Technical
rept. no. 3 on Contraa DA 36-039-8C-78130. Feb 59,
lip. I ref. Rept. DA-SC-78130/3; AD- 211 414.
Order from LC ml$2. 40, ph$3. 30 PB 153 608
SM
iminl analysis of a stationary time series is oon-
lUered for the case of discrete spectrsl windows. A
^Mbod for determining optimal estimates of the
ipectral density la studied by using the concept of
toadwldth. tAuthor)
Chicago U. (m.l
DECOMPOSABILITY OF MODULES, by Irving
JUpitoaky. Technical rept. no. 2 on Investigations in
Algebras and Finite Fields, Contract DA 1 1-022 -ORD-
3492. Oa 60, 8p. 5 refs. OOR rept. 1833:2-M:
AD- 246 299.
Order from LCmi^l. 80, phSl. 80 PB 153 664
The following theorem is proved: For any Noetherian
Integral domain R, the following two statements are
squivalent: (1) R is local, complete, and of KruU
dimension less than or equal to 1, and (2) Any torsion-
free R-module of rank two which is not finitely
■■■rated is a direct sum of modules of rank one.
(Auto)
Columbia U. , New York.
RECURRENT GAMES AND THE PETERSBURG
PARAIX)X, by.Herbert RobWns. Rept. on Contract
Nom-266(59). (1960) 13p. 2 refs. UC-l8-60-Nonr-
]66(S9) MS; AD- 236 738.
Order from LC mi$2.40, ph$3.30 FB 147 547
Columbis U. School of Engineering, New York.
MULTIVARIATE ASYMPTOTIC DISFRIBLmONS OF
EXTREME VALUES, by E. J. Gumbel and Simeon M.
Berroan. Technical rept. T-19A on Contraa DA 30-
OW-ORD-1061. [I960] 26p. 6 refs. CU 14 58 ORD
1061 IE; OOR rept. 1716. I3-E; AD- 240 734.
Order from LC ml$2. 70, pb$4. 80 FB 153 665
Examples of multivariate asymptotic distributions of
largest and smallest values are presented. Explicit
•nalytical expressions for some distributions in the
daas are given. The elements of bivarlate distrlbu-
tlon theory are reviewed, snd a system of bivarlate
distributions with arbitrary margins is constructed.
This construaion is used to form bivarlate dlstribu-
I which are Joint asymptotic distributions of the
and smallest values, respealvely. Some gen-
eralizations follow. The largest and the smallest
fslues of a blvariate logistic distribution are analyzed
ind are shown to behave in entirely differeiu ways,
due to the asymmetry of the distribution. Another bi-
vtrlate asymptotic distribution of extremes is found
(ram the smallest values of the blvariate logistic
distribution. (Author)
David Taylor Model Basin, Washington, D. C.
LBCrURES ON TOHCS IN NONLINEAR DIFFER -
BKITAL EQUATIONS. byG. Temple (Oxford U.)
Mar 60, 49p. 8 refa. Rept. 1415.
Order from LCmi)3. 30. ph$7. 80 PB 154 766
This report released for sale to the public 15 Mar 61.
'Riese leaures describe some recent researches on
irdlmry tKxUinear differential equations. The first
iKturc Is devoted to a search for a "superposition"
principle for these nonlinear equations and it deter-
mines the class of nonlinear equations for which such
a superposition principle exists. The remaining four
leaures provide a rigorous, analytical theory of the
technique Invented by Lighthtll (1949) for solving non-
linear differential equations with an "Irregular" per-
turbation. Such equations involve s small parameter
a and audi that the coefficient of the highest derivative
vanished Identically, or at the "Initial point", when
a ■ 0. The theory is developed from s number of
simple examples and given a rigorous form by means
of the theory of "dominant functions" . (Author)
Digital Computer Lab. , U. of Illinois, Urbans.
ROUNDOFF -ERROR ACCUMULATKW IN ITERA-
TIVE PROCEDURES, by Robert T. Gregory and
A. H. Taub. Rept. on National Science Foundation
Grant G-9503. 31 Oct 60, I2p. Rept. no. 103;
AD- 247 367.
Order from LC mi$2. 40, ph$3. 30 PB 153 415
Educational Testing Service, Princeton, N. J.
AN IBM 650 PROGRAM FOR A COMPLETE PAIRED
COMPARISONS SCHEDULE (PARCOPLBT-2-21) by
Harold Gulliksen. Rept. on Mathematical Techniques
in Psychology, Contraa Nonr- 1858(15) and National
Science Foundation Grant 0-642. May 60, 4p. 2 refa.
AD-237 504.
OrYler from LCmi$ 1.80, ph$ 1.80 PB 147 363
In order to facilitate analysis of paired comparif
data, an IBM 650 program waa prepared that will
handle a complete paired comparison schedule for
any number of objeas up to. and including 21. It is
also possible to append and analyze an absolute Judg-
ment set of data in which the subjea classifies the
stimuli into two categories as positive or n^ative,
like or dislike. A checking program was aim pre-
pared to Insure that the data cards are in proper
form. (Author)
Electronics Research Lab. , U. of California.
Berkeley. _aafn
ON THE SUMMATION OF ^-<\^ AI© ITS ASSO-
CIATED INTEGRALS, byB. I. Jury and M. A. Fai.
Rept. on Contract AF 18(600)1521. 14 Sep 60, 25p.
12 refs. Series no. 60. issue no. 315; AFOSR-TN-60-
1145; AD- 246 763.
Order from LCmi$2. 70. pttM- 80 FB 153 313
A geometrical interpretation of the coiwolution z trans-
form is given and this is aisled to develop z trans-
forms of functions of the type f(t)/t*. k> 0. After
establishing the equivalence between certain forms of
integrals , the authors have used the integrals to sum
certain forms of Infinite series. Possible extensions
of this technique to other forms of series and to sum
finite series is also Indicated. (Author)
Harvard U. [Cambridge, Mass.]
ON THE DEGREE OF CONVERGENCE OF SE-
QUENCES OF EXTREMAL POLYNOMIALS AND
OTHER EXTREMAL FUNCTIONS, by J. L. Walsh and
A. Sinclair. Rept. on Contracts AF 49(638)574.
595
AF 18(600)I46i, and NSorl- 076(34). Mar 60, 48p.
25 refs. AFOSH TN-60-223: AO-244 390.
Order from LO mi$ 3.30, ph$ 7. 80 PB 152 370
L«c a given fuofrtlon F(z) be at cJaas LP, p >1 , oo ao
analytic Jordan, curve y In the plane al the complex
variable z, and let pn (z) be the unique leaience of
polynomials in^ of respective degrees n cif best ap-
prxjximation to P(z) on y in the sense of mlnlmlzir^!
J|F<»)-Pn(»)iP|<b|.
These mlnlml^ng Pn(z) in*y ^so be subjected to cer-
tain auxiliary dondlnons of interpolation Pi](^)*Uvi
k'1,2 m, which are independent of n and are not
necessarily related to F(z). Convergence and degree
of convergence of the sequence Pn(z) to a possible
limit mlnimiziiig function, and various properties of
this limit function are studied. (Author)
UllnoiB Inat. <tf Tech. , Chicago. 111.
A GRAPHICAL METHOD FOR THE DOUBLE-
SPECIF ICATIOH UMTT ACCEPTANCE SAMFUNG
PROCEDURES OF MIL-CTD 414, by George J.
ReanlkcM and Ueroy A. Wickatrom. Technical rept.
no. 1 on Contract Near -1406(05). 19 Feb 60, 44p}
AD- 236 065.
Order from LC!ml$3.3a pfa$7.80 FB 153 146
[IlUnoia U. . lAbtifial.
SOME THEOREMS OH THE GRO\*rrH OF PARTI-
TION FUNCTIONS, by Sufaramonier Parameawaran.
Theala. Technical. rept. on Contract Nonr- 1834(18).
11959) 47p. 14 tefa. AD-232 644.
Order from LC tni$3. 30, ph$7. 80 PB 153 135
An aaymptotic relation ci the form n(u)''^u* L(u) aa
u— »-fMia conaldered for a kO, where L(u) ia a alowiy
oadllatlng function.
Institute for Advanced Study, Princeton, N. J.
RESEARCH IN ANALYSIS AND ALGEBRA, by
Andrew Gleason and S. |[x>]a8iewlcz. Final rept. on
Contract DA 36-034- OR D- 2884 RDt July 60, 3p.
OOR rept. 242Z5-M.
Order from LC |ml|1.80, ph$1.80 PB 153 67&
kief report on function algebras and sheaves at sets
over a manifold
olcL
'^ioatltute at Stadatlca, North Carolina U. ,
Chapel Hill.
BAYES RULES FOR A COMMON MULTIPLE COM-
PARISONS PROBLEM AND RELATED STUDENT-t
PROBLEMS, by David B Duncan Rept. on Contracts
AF 49(638)929, AF 49(638)261 and Nonr-355(06).
Nov 60, 36p. 1ft refs. Mimeograph aeries no. 266;
APOSR-TN-60-|418, Reviaion and extension o(
APOSR-TN-59-492; AD- 248 659
Order from LC tni$3. 00, ph$6. 30 PB 153 840
The paper ia nruiinly concerned with the multiple
comparlaons problem in the analysis of variance
aetting. A principal finding is that the Bayes solution
for the multiple comparisons problem corresponds to
a tolerated error probability " of the first kind" far
each single difference, which is independent of the
number of treatments being compared.
Institute at Statistics, U- of North Carolina, Chapd
Hill.
ON A NEW DERIVATION OF A WELL KNOWN OB-
TRIBUnON, by S. N. Roy. Rept. on Contract
AP 49(638)21 3. Apr 60, Up. 5 refs. Mimeograph
sertea no. 254; AFOSR-TN-60-985.
Order from LC ml$2. 4a pl43. 30 PB 153 832
It ia well known that so far the Joint distribution of tte
latent roots aaaodated with normal multivariate analy-
sla at variance haa been considerably more difficult to
derive If the effective number of varlatea is greater
than the number of components of the linear hypotheili
than if it ia the other way around. Thia report oCfen
both on the null and the non null hypothesis a simple
method of derivation of the diatrlbution for the fonaK
case by throwing it back on the distribution for the
latter case, and in this tie-up a pivotal role is plajtcd
by the distribution of the latent roots connected with
the testing of the hypothesis of independence befWeea
two seta d varlatea. (Author)
Institute of Statlstlca, U- of North Carolina, Chaptl
Hill.
ON CERTAIN ALTERNATIVE HYPOTHESES ON DB-
PERSION MATRICES, by S. N. Roy and R. Gnanaded-
kan (Bell Telephone Labs. ) Rept. on Contract
AP 49(638)213. Aug 6a 19p. 10 refs. Mimeograph
series no. 261; AFOSR-TN-60-984; AD- 248 657.
Order from LC mi$2. 4a ph$3. 30 PB 153 831
For two multivariate nonsingular normal dlstributloBi,
the familiar null hypothesis of equal dispersion matil-
cea ia conaldered agalnat various alternatives stated,
in terms at certain characteristic roots. Based on two
independent random samples from the two distributions,
similar r^on tests are proposed for the null hypad»-
sis agalnat each of the alternative hypotheses. AlsO)
for each case, conaervatlve confidence bounds are ok-
tained on one or more parametric functions which
measure departure from the null hypothesis in the di-
rection of the corresponding alternBiive. Finally, «
physical interpretation is given for the alternative lif
potheses considered. (Author)
Institute of Statistics, U. of North Carolina,
Chapel Hill.
ON SEQUENCES OF SUMS OF INDEPENDENT
RANDOM VECTORS, by Wassily Hoeffding. Rept. <■
Contract AF 49(638)261. May 60. 25p. 7 refs.
Mimeograph series no. 258; AFOSR-TN-60-987. .
Order from LC mi$2. 70, ph$4. 80 PB 153 833
A particle in k-space starts at Sq ■ 0 and after n tlMI
units is at Sn. where Sn is the sum of n independent,
identically distributed random vectors with integer-
valued components, zero mesne, and non- singular
second-moment matrix. A time-dependent absorptios
boundary is present such that the expected time to
absorption is finite. A relation is established befwees
the expected number of times the particle is at the
origin prior to atMorptlan and its expected distance
from the origin at the time of absorption. (Author)
5^w
laatltute of Sutistlcs, U. of North CaroUna,
Oiapel HiU.
ON SOME METHODS OF CONSTRUCTICW OF
PAHTIALLY BALANCED ARRAYS, by I. M. Chakra-
varti. Rept. on Contraa AF 49(638)213. May 60,
lOp. 7 refs. Mimeograph series no. 260; AFOSR-TN-
60-1019.
Ordff fromLCml$1.80. ph$1.80 FB 153 834
IlKhmlT of construction of partially balanced arraya
are conaldered in this report. Two methods of con-
imictlon are given. One of them derives partially
(nlfpr-Ati arrays from ( X- ^- v) configurations and
Che otber is an extension of Bose-Shrikbande method
of construction of orthogonal arrays . (Author)
bitltute of Tech. , U of Minnesota, Minneapolis.
HFURCATION OF AN INVARIANT MANIFOLD
FROM A PERIODIC SOLUTION OF A DIFFEREN-
TIAL SYSTEM, by Fred S. Van Vleck. Technical
rept. for 16 June- 15 Aug 60 on Problems in the Theory
of Ordinary Differential and Difference Equations,
Co*raaDA 11-022-ORD-3369. July 60, 98p. 20 refa.
OOR rept 2560. 2-M; AD- 243 170.
Order from LCini$5. 40, ph^lS. 30 PB 153 6M
CuMllIni the real autonomous system dx/dt > f(x,u),
etaere p is a real parameter and x, f are (n-i-l) -veoora
The assumption is made that f haa second partial
derivatives with respect to x which are continuous in
(x,ul. Assunoe ttiat the system has a periodic solution
I . ^t) for all ^l and that the characteristic exponents
of the autonomous system, based on <^, have zero real
ptru for'^ - 0. No restrictions are placed on the
Imaginary parts. Under certain restrictions, an
D-manifold in the x- space bifurcates (branches off)
from the fixed periodic solution for values of p near
iero. This manifold Is homeomorphic to the product
ofdH (n-l) -sphere and the 1-sphere and contains the
periodic solution in ita interior. (Author)
loaa Sute U. of Science and Tech. , Ames.
SOME ALMOST PERIODIC SOLUTIONS OF THE
VAN DBR POL EQUATION WITH ALMOST PERIODIC
FORCING, by D. D. Jamea and C E. Langenhop.
Technical rept. no. 2, 1 July- 31 Aug 60, on Alnnoat
Periodic Solutions of Differential Equations, Contract
QA11-G22-ORD-2630. (I960] 17p. 4 refs. OOR r«^.
1K7. 4-M; AD- 242 576.
Order from LC mi$2. 4a ph)3. 30 PB 153 668
The differential equation
x + i(x2 - lyk. +(«2 - (>)■ . cP sin at + kbft^t).
where ^ P, l ,w and k are positive parameters and b(t)
is slmoM periodic, is treated. The use of a perturba-
t^ procedure provides results regarding the existence
tnd stability of certain almost periodic solutions of the
^erential equation for f sufficiently snvall and k or
^- sufficiently small. The existence and nature of
almost periodic solutions is determined by re-
l«loos among the three parameters •, P, y. (Author)
Li^eU. (Belgium).
PROBLEMS AND METHODS IN PARTIAL DIFFEREN-
TIAL EQUATIONS. PART U: THE METHOD OF
SINGULARITIES, by P. J. Bureau. Technical (scienti-
fic) note no. 4 on Contract AF 61(052)86. July 60, 89^.
17 refs . AFOSR-TN-60-890. AD- 246 981
OrderframLCml$4.80, pl4l3.80 PB 153 307
The method of singularities is used to solve the
Cauchy problem for simple hyperbolic partial differen-
tial equations , namely , the wave equation and the
damped wave equation . The represeniatlon formula
for the solution of the Cauchy problem is written in
terms of finite parts and logarithmic parts of certain
divergent integrals . A process of analytic continua-
tion is also used to solve the Cauchy problems under
consideration. However, to obtain explicitly the
representation formulas for the solutions , one must
actually perform the analytic continuation. It Is shown
that this is best achieved by making use of finite and
logarithmic parts. Simple examples were purposely
chosen so as to show that cotwideration of finite and
logarithmic parts is naturally unavoidable. (Author)
Lincoln Lab. , Mass. Inst, of Ted). , Lexington.
CODING INSTRUCTIONS FOR FLOATING POINT
TRIGONOMETRIC, INVERSE TRIGONOMETRIC
HYPERBOLIC AND EXPONENTIAL FUNCTIONS, by
B. A. Jensen. Rept. on Coturact AF 19(604)740a
1 Nov 60, 8p. 30G-0009; AD- 246 189.
Order from LC mi^l. 80, ph$l. 80 PB 153 062
The addition of the trigonometric, inverse trigono-
metric, exponential and hyperbolic functions to the
floating point program of the OG 24 computer pro-
vides the programmer with a method of doing many
computations tliat formerly required desk calculators.
The rules for writing the instructions are simple,
programming time Is reduced, numbers are written
in the ordinary decimal form ±23. 9 x 10^, seven sig-
nificant decimal figures are kept during the compu-
tation, and the answers can be printed out at the ma-
chine in decimal form. Any computation involving
addition, subtraction, multiplication, division,
square root, sin. coa. tan, cot, sec, esc, sin'^
cos
1
tan'^ cofl.
aCC
•1
CSC
-1
. e*. e"*, sinh.
coeh, tanh, coth, sech, each and requiring an accu-
racy of seven significant decimal flgurea can thus be
carried out on the OG 24 computer. (Author)
Lincoln Lab., Mass. Inat. of Tech., Lexington.
AN EMPIRICAL INVESTIGATION OF PROCEDURES
FOR LOCATING THE MAXIMUM PEAK OF A
MULTIPLE -PEAK REGRESSICW FUNCTION, by
E. J. Magee. Rept. on Cootraa AF 19(604)7400.
20 Oct 60, 32p. 4 refa. 22G-0046: AD-245 672.
Order from LC mK3. 00, ph$6. 30 PB 152 956
This study ia concerned with the developmeu of aa
efficient prtxedure for locating the (absolute) maxi-
mum of an unknown regression function which may
have a number of local maxima. Procedures com-
bining stochastic approximation and random search
techniques are described and experimental results
are presented. Experimentation with procedures of
597
this type imfioates diat the approach is an effective
one. It Is evl4eat that stochastic approxlmatlaD alone
is not sufflcietn but must be combined with a search
mechanism to avoid cooverging to a local maxlminn.
The most effideitf at three versions tested is one in
which two self-adjusting ICiefer-Wolfowitz stochsstic
approximation processes are in operacioa concur-
rently and time is distributed randomly between the
processes. There appears to be no advantage In
having more than two processes in operation con-
curremly, particularly when it is desired to remem-
ber only the t^axlmum peak. (Author)
Uncohi Lab. , Mass. Inst. dfTech., Lexington.
ON THE BEHAVIOUR OF THE GEOMETRIC GENUS
UNDER GROUND FIELD EXTENSION, by Peter Palh.
Kept, on Contract AF 19(604)7400. 20 Oct 60, lOp.
2 refs. 220-0051; AD- 245 548 .
Order from LC mill 80. ph$ 1.80 PB 1 52 828
The behavior erf the georaetrlc genus, p^/k), al a
fimctlon field, K/k, in two variables unoer constant
field exienslo« Is discussed. If K' is obtained from IC
by the constam field extension k-to k*. then
pl(K/k) ^ Pg(K' A), with e<iuality if k' A i« Purely
transcendenral or separable algebraic. (Author)
MassachuseQs Tnst. afTe<A , Cambridge.
GENERALI2ED HOMOLOGY THEORIES, by George
W. Whitehead. Interim technical rept. no. 3 on Group
Ccmplexes and Cohomology Operations, Contraa
DA 19-020-ORD-4851. tl960l 86p. 43 refs. OOR
rept. 2246:4-M; AD- 246 688.
Order from LC mi$4. 80, ph$l3. 80 PB 153 676
Prtxrf Is presented that the generalized homology
groups satisfy the Eilenberg-Steenrod axioms, except
for the dimension axiom. Homology and bomotopy
properties of the reduced Join are discussed as are
properties at spectra. In addition proof is given for an
Alexander duality theorem. (Author)
Massachusetts Inst, of Tech. , Cambridge.
ON STABLE HOMOTOPY THEORY, by Daniel M Kan.
Interim technical rept. no. 2 on GroiQ) Complexes and
Chomology Operations, Contract DA 19-020-ORD-
4851. [1960] 36p. 21 refs. OOR rept. 2246. 2-M:
AD- 242 660.
Order from LC nil$3. 60, ph$9. 30 PB 153 675
The notion of ipectrs is defined in the semlslmplldal
context. A simple definition which has (unlike the
topological definition) all the maps built in is possible,
and a homotop^ theory of these spectra can be devel-
oped which parallels the usual homotopy theory al
semlslmpllclaj complexes. A discussion is presented
of the homotopy groups and homology groups of spec-
tra (which are also defined in negative degrees) snd a
kind of Hurewicz bamomorphisma connecting tbem. A
spectral sequence is obtained which relates, for any
■emlsimpliciaj complex, the Integral homology with
the stable homotopy groups.
Mlrhli^n State U. ^ast Lanslnj^.
MULTIVARIATE ANALYSIS, by Ingram OUdn. Pi^
technical rept. for 1955-1960 on Ccmtracts DA 11-
022-ORD-1998 and DA 20-018-ORD- 14735. 10 JumM
17p. 19 rsft. OOR rept. 1840.18-M; AD- 243 172.
Order from LC mi$2.40, ph$3.30 PB 153 6i|
Technical reports en the research In multivariate
analysis, as well as the status of publication are
listed. A general survey of the project and the rasafei
achieved is reviewed. (Author) (See also AD- 243 171)
Mchlgan U. Coll. of Literature, Science and the
Arts, Ann Arbor.
ASYMMETRIC PRIME ENDS, by B. F. Colllngwoai
and G. Plranian. Technical note on Contract
AF 49(638)633, Oct 60. lip. 6 refs. 2913-3- T;
AFOSR-TN-60-992; AD- 246 373.
Order from LC mi$2. 40. ph$3. 30 PB1S3»
Bach timply connected doraafai in the plane hat atats
oountably many prime ends whose right and left w^i
do not cotnclde. On the other hand, to each countaMt
set E on the unit circle C there corresponds afiBCtta
which is holomorphic and univalent in the unit disk 0
and which has the property that it carries each potattT
B and no point of C E onto a prime end with unequal
wings. (Author)
Michigan U. Coll. of Literature. Science, and lbs
Arts, Ann Arbor.
A CONVERSE OP A THEOREM OF R. H. BING AN)
ITS GENERAUZATION, byR. L. Wilder Technlcri
note on Contraa AF 49(638)774. Sep 60, 9p. 4 refs.
03597-2-T; AFOSR-TN-60-1071; AD- 246 627.
Order from LCml$ 1.80. ph$ 1.80 PB 153W
RH. Blng(Am. Math. Soc. 838, 1959) announced llK
la 3-8pace every topological 2-sphere S is "almost
free" la that for every positive number e there eiiM
a CaAor set C in S and an e-transformatlon of S iM
a set which meets S only in C; and It seems hlgMjr
probable that the general 2-inanlfold will have ths
aame property. A converse of this is shown sad a
new positional characterization of the manifold Is «b-
talned. An analogoua sufficient condition is also
provided for the general n- dimensional Euclldeao
•paoa. (Author)
Michigan U. Coll. of Literature, Science, and da
Arts. Ann Arbor.
EXTENSION OF LOCAL AND MEDIAL PROPER-
TIES TO OOMPACTIFICATIONS WITH AN APPLI-
CATION TO CECH MANIFOLDS, by R. L. Wilder.
Technical note on Contracta AP 49(638)104 and
AF 49(638)774. Sep 60, 22p. 11 refs. 03000, OSSfl-
1-T; APOSR-TN-60-10t2; AD- 246 626.
Oixler from LC mi$2. 70, ph$4. 80 PB 153 2W
Of central importance in topology and Its applicadosi
iMve been the manifolds of various dimensions, b
1936, in a paper published in the Proceedings of *•
M«rif«al Academy of Sciences, Eduard Cech proposd
for study a type of manifold which embodied a con-
dition theretofore not used, to wit, thst every pc4«
ygft a neighborhood whose one -point compactlficatiot
Is sn orientable closed manifold. In the present
paper, the chief question studied relates to the Im-
(dlcation of this condition if applied to arbitrarily
ntall neighborhoods of a point. This necessitates a
tesrch for conditions under which a locally compact
gpue, which has a given type of local connectedness,
will preserve this under compactlficatlons. Neces-
aary snd sufficient coixlltions are obtained which
apply to both the one -point and to the Freudenthal
cooipsctifications. In ^rticular, it is found that If a
manifold satisfies the Cech condition for arbitrarily
Moall neighborhoods of a point x, then x has arbi-
tiarlly small neighborhoods that are r-acyclic (in
terms of compact homology) in all dimensions r. The
question which then obviously arises, whether all
nianifolds of the type in current use have such neigh-
borhoods, is answered by providing an example of
one which does not. (Author)
lUcnmsve Research Inst. , Polytechnic Inst, of
Irooklyn, N. Y.
ON THE FACTORIZATION OF RATIONAL MA-
TRICES, by D. C. Youla. Rept. on Contract
AP 19(604)4143. 20 Sep 60, 44p. 11 refs. Research
rept. PIBMRl 855-60; AFCRL-TN-60-1112.
0nlerfromLCml$3.30. ph$7.80 FB 153 554
k systematic account is given of some of the more re-
cent developments in the algebra of rational matrix
(unctions of a single complex variable. Several algo-
ridms for the (actorizadon of such matrices are pre-
sented snd illustrated with two non-trivial examples .
The theory is applied to three problenu of engineering
Importance , one of them being the solution of matrix
Wiener- Hopf integral equations. (Author)
Minnesota U. , MlnneapoUs.
THE CIRCUMFERENCE OF A COttVEX POLYGON.
by Frank Spitzer and Harold Widon. Technical rept.
no. 2 on Contract Nonr-710(28) (1960] 7p. 2 refa.
AD- 233 291
Order from LCmifl. 80, pb$l. 80 FB 153 771
A convexity theorem of Caudiy (Cambridge Univ. Press,
1958) is combined with the combinatorial identity of
M. Kac (Duke Math. J.21;501-509. 1954). Cauchy's
dieofem concerns the length L of the circumference of
• compact convex set A in the plane. Kac conaldered a
vector x*-(xi,X2, ■ ..Xq) with real compoDencs. A
vactor !^-(z|,Z2. ■ ■ .,Zq) with complex componenta la
■ow considered.
Minnesots U , Minneapolis.
SOME PROPERTIES OF RECURRENT RANDOM
WALK, by Frank Spitzer. Technical rept. no. 4 oa
Contraa Nonr-710(28). (1959) 28p. 5 refa.
AD- 236 405.
Order from LC mi$2. 70, ph^. 80 PB 147 176
Ckmsider tiie stochastic process SsS]-^^X{, jsO
•ndi*'l,2 n. Sj is an arbitrary integer, and the
Xi are independent, identically distributed, integer
valued random variables. The aasunr^xion is made
that the state space of the process is the act of all
hKegers. and that every point is visited infinitely often
with probability one, for every starting point Sj. S is
an indecompoaable recurrent Markov chain on the set
of all integers. Let x and y be two distinct integers,
|x-y| = k> 0. Considef the embedded Markov ciiain
Induced by the set S* ^x, y} of these two pcAnts. The
Markov chain whose transition matrix is P(S)s (Pij(S));
1, j « 1, 2; is discussed. Fourier analytical estimates,
baaed on ^ technique of Chung and Erdos (Memoirs
Am. Math. See. 6, 1951), are used. The pro<rf re- ;;
qulrea an extension of the investigation to the em-
bedded Markov chain Induced by a set of three instead
of two statea. Tbeae extended results arc
summarized.
Minnesota U . , Minneapolis .
THE TOEFUTZ MATRICES OF AN ARHTRARY
LAURENT POLYNOMIAL, by Palle Schmidt and
Prank Spltzcr. Technical rept. no. 3 on Contract
Nanr-710(28). 24 Feb 60, 37p. 9 refs. AD-233 292.
Order form LC ml$3.00, ph$6.30 FB 153 133
North Oarolins State Coll. , Raleigh.
GENERAL PERTURBATIONAL SOLUTK)NS OP TOE
MATHIEU EQUATION, by Raymond A. Struble and
John E. Fletcher. Tedmlcal memo. no. 5 on Contract
DA 36-034-ORD-2733. Sep 60. 20p. 1 ref. OOR rept.
2125:12-M; AD- 244 087.
Order from LC ml$2. 40, ph$3. 30 PB 153 672
General perturbational solutions of the Mathieu
equation are obulned In die form of asymptotic series.
The principal part of a solution is obtained by a modi-
fied variation of parameter technique which admits
only slow (long period) variations in the amplitude and
phase. All rapid (short period) perturbations are ob-
tained as additive corrections to the principal part.
The explicit solutions are either almost-periodic
functions or diverging or decaying oscillations. The
resonance phenomena associated with critical values
cf the equation parameters are manifest in the vari-
ational equations and the familiar periodic solutions
(Mathieu functions) emerge merely as singular so-
lutions of these variational equations. Also both di-
vergent and decaying oscillations emerge near the
critical parameter values, thus revealing the well-
known stability properties of the Mathieu equation.
(Author)
Northwestern Technological InK., Evanston, Til.
SOME NOTES ON NOfJ- HOMOGENEOUS CONVEX
POLYHEDRAL CONES, by A. Ben- Israel. C»«l Re-
search memo. no. 30 on Temporal Planning and
Management Decision under Risk and Uncertainty,
Contract Nanr-1228(10). May 60, 9p. 6 refs.
AD- 237 864.
Order from LC ml$1.80, ph$1.80 PB 148 200
Nuclear Development Corp. of America. White
Plains, N. Y.
A PROGRAM FOR THE NUMERICAL INTEGRATION
OF THE B0LTa4ANN TRANSPORT EQUATION,
NIOBE, by S. Preiser. G. Rabinowltz, and
B. deDitfour. Rept. on Study for a Code Embodying
the Numerical Integration of the Boltzmann Equation,
Contraa AF 33(616)6184. Dec 60, 67p. 9 refs. ARL
598
999
Technical repl. 60-314.
Order from LC ml)3.90, ph$10.80
X code (NIOBE) for numerically Integrating the time-
Independent neutron or gamma ray Boltzmann trans-
port equation has been written for the IBM -704. The
code will calculate angular distributions, total fluxes
and currents fot neutrons (or photons) as a function at
energy (or wavQ length) in a finite, multilayered,
spherically syn|metric configuration. (Autlior)
respdcS loboA ttieir general operating characterlitia
PB 152 587 and their effect en the point of optimum split. The
stationary distribution at the inventory content varia-
ble Is found under the various replenishment policial;
these probabilities are used to obtain the point at
optimum split. Comparison between the policies,
under assumptions of geometric demand dlstrlbutlOD
(discrete), or negative exponential demand dlstrllM)-
Uon (continuous), is nnade. Tables for making these
comparisons are also presented. (Author)
Polytechnic In«t. at brooklyn. N. Y.
fflGH ORDER CORRECT DIFFERENCE SCHEMES
FOR ANISOTROPIC PARABOLIC EQUATIONS^ toy
Richard Hermaa and J. R. M. Radok. Rept. on
Contract AF 49^638)302, Oct 60. lOp. 2 rrfs. PIBAL
rept. no. 581; AFOSR-TN-60-1304; AD- 246 922.
Order ftom LC nai$1.80. ph$1.80 PB 153 2%
Difference schemes for anisotropic parabolic equations
are deduced for given order of truncation errors and
their relationship to similar schemes for the one
dimensional he^t equation is demonstrated.
RIAS, Baltimore. Md.
ALGORITHMS FOR JORDAN CURVES ON COMPACT
SURFACES, by Bruce L. Reinhart. Rept. on Contract
AF 49(638)382. Nov 60, 28p. 17 refs. Technical
rept. 60-21; AFOSR-TN-60-1123; AD-248 305.
Order from LC pii$2. 70, ph$4. 80 PB 153 710
The purpose is io give an algorithm for determining
which free homotopy classes admit a simple closed
(Jordan) curve in the case of compact surfaces of
negative Euler aumber.
RIAS. Baltinwre, Md.
CLOSED METRIC FOUATIONS, byB. L. Reinhart.
Rept. (Ml Contract AF 49(638)382. Sep 60, Up. 6 refs,
Technical rept 60-17; AFOSR-TN-60- 1039;
AD- 247 232.
Order from LC mi$2. 40, ph$3. 30 PB 153 413
M is a C^^n dimensional manifold with a p dimen-
sional foliation F and a fibre-like Riemannian ds.
This report is ooncemed solely with the case that all
leaves are dos^ subsets of M.
r
Virginia AgrlOiltural Experiment Station, Blacks burg
AN INVENTORY COhTTROL PROBLEM WITH REGU-
LAR AND EMERGENCY DEMANDS, by Roshan L.
f>«<Vi^ Technical rept. na 11 on Development of
Statistical Methods for Experimental Designs in
Quality Control and Surveillance Tesdng. Contract
Nonr- 2352(01). Mar 60, 204p, 33 refs. AD- 236 467.
Order from LC mi$9.30. phJ31.80 PB 153 782
Optimum split df a stock of a single item is discussed
under the assumption that the decision to replenish
the Inventcry Is taken at equally space time intervals.
The lag time between ordering and receiving an order
(or replenishmc^ is assumed to be zera The demand
distribution Is assumed to be independently and iden-
tically distributed in successive time intervals. Four
different replenishment policies are considered with
Washington U. , Seattle.
THE EFFECT OF LIMITING THE NUMBER OF
ITERATIONS ON A PRINCIPAL AXES FACTOR
ANALYSIS SOLUTION, by Harold William Burk. R«|X.
on Ccntract Nanr-477^) and Public Health Research
Grant M-743(D4). Feb 60, 58p. 18 refs; AD- 233 211
Order from LC ml$3.60, ph|9.30
PB 153 132
Using a mathematical rationale developed by Horst
(Servant of the Human Sciences, U. of Wash. . 1953)^
data from several sources, and a program written if
Lunneborg and Wright which allows limiting the
number of Iterations completed, arbitrary factor load-
ing matrices were found for several matrices using
different Iteration limits. Prom the results, it
appears that limiting iterations can be a useful pro-
cedure. It would reduce considerably the cost of fac-
tor analyses, particularly in cases where some of thl
latent roots of a matrix were close together in value
The cycle limits would not affect the determination of
the rank of a matrix. The shortened procedure will
account for about as much of the variance in the
matrix as the unlimited procedure if cycle limits are
not set too low. If precise principal axes data is
desired or primary interest is in interfactor correla-
tions, this shortened procedure has less value. The
values of elements in corresponding residual matrica
will not be identical with those obtained with the un-
limited procedure. Limiting cycles will tend to
increase inter-factor correlations. When factorii^
Is continued until some specified value is reached, the
procedure may result in the isolation of an additional
factor when law limits are used. The removal of a
given number of factors with limited Iterations gener-
ally accounted for more variance than did the unllmlul
calculation with one less faaor. Hence the ultinute
usefulness of the shortened procedure will depend oa
the nature of the original data and the purposes of Ik*
e:]q)erimenter. (Author)
[Wayne State U- , Detroit, Mich. ]
PIBERINGS OF ENVELOPING SPACES, by Sze-
Taen Hu. Technical note no. 10 on Contract
AF 49(638)179. Oct 60, 36p. 7 refs. AFOSR-TN-
60- 1224; AD- 246 491.
Order from LC mi$3. 00. ph$6. 30 PB 153 177
Since the enveloping spaces and the residual spaces
were shown to be very useful in distinguishing spaces
of the same homotopy type, the homology groups and
the homotopy groups of the enveloping spaces of a
manifold are computed. For this purpose, the fact
is established that the natural projection is a fiberlai
The method of fiber spaces can be applied and mo«
of the groups computed. (Author)
600
Yale U. (New Haven, Conn. ]
SELECTED TOHCS IN FUNCTICWAL ANALYSIS, by
Biaar Hllle, Alexandra and Cassius lonescu Tulcea.
Pinal technical rept. for 1 Sep 58-31 Aug 60 on Con-
traas DA 19-059-ORD-2707 and DA 19-020-ORD-
4912. (1960) 17p. 11 refs. OOR rept. 2070: 1-M;
AD-247 239.
Order from LC mi$2. 40. ph$3. 30 PB 153 671
Computing DevicM
"<-'r*
Beodbt Aviation Corp. . IDetroit, Mich.
THRBB DIMENSIONAL FLIGHT TABLE E«V1CE
NO. 24-X-5, bvM. Kanes. Final rept. on Contract
Nonr-321(01). [1955] 9p. Rept. no. 775; AD-82 734.
Onkr from LC ml$l. 8a ph|l. 80 PB 154 806
TUs repon released for sale to the public 17 Mar 61.
The simulator waa developed for use with a master
computer for the purpose of simulating the flight of
tut air-to-air missiles on a 1 -to - 1 time scale. The
■ft consists of a high-performance, servo -controlled
fbnbal system which follows command inputs from an
aaalog computer. Missile sections and components
mounted on these gimbals are subjected to the torques,
angular accelerations, and angular velocities which
would be experienced in the flight being simulated. In-
itnanents on the gimbals system monitor velocity and
poaltion, and compute Euler angle transformations.
Galtfomla U- , Los Angeles.
BIJB0TION1C DATA PROCESSING MACHINE RE-
QUIREMENTS, by Richard G. Canning. Rept. on
Management Sciences Research Proj. [Contraa Nonr-
233(02)) 31 July 53. 31p. 11 refs. Research rept.
no. 16; AD- 143 050.
Order from LC mi$3. 00. ph$6. 30 PB 154 422
TMs report released for sale to the public 8 Mar 61 .
Uaooln Lab. , Mass. Inst, of Tech. , Lexington.
DBTBRMINATION OF Rcutoff FOR ASYMMETRIC
CHANNEL, by B. Reiffen. Rept. on Contraa
AP 19(604)7400. 24 Oct 60, 18p. 25G-0021;
AD-246 372.
Order from LC mi$2. 40, ph$3. 30 PB 153 106
Prerlously the author defined a computation cutoff
™*. Rcutoff' 'or ■ discrete memoryless channel
symmetric at its output with equally likely inputs.
For information rates R < Rcutoff ' sequential decod-
lagmay proceed with an average number of decoding
''"fMtton which does jjgt grow exponentially with
"Mstraint length n. In this report, Rcutoff i" defined
for the general non -degenerate discrete memoryless
clXBel ^th arbitrary input probabilities. (Author)
Lincoln Lab.. Maas. Inst, of Tech., Lexington.
GRAPHICAL MANIPULATI(»I TECHNIQUES USING
THE LINCOLN TX-2 COMPUTER, byHerschelH.
Loomis, Jr. Rept. on Contract AF 19(604)7400.
10 Nov 60, 28p. 3 refs. 51G-0017.
Order from LCmi$2. 70, ph$4. 80 PB 153 48S
The results of an investigation into the use of a com-
puter controlled oscilloscope display for graphical
manipulation. Including symbol ch-awing and position-
ing of symbols to form a drawing, are reported. The
structure and operation of a program to cb'aw sym-
bols and to use these symbols for the construction of
a drawing are discussed. Finally, the type of pro-
gram which would aid the logical designer in his
logical circuit design by preparing and filing the
drawings and analyzing the circuits for such items aa
signal delays and unit loading factors is discussed in
brief. (Aichor)
Moore School of Electrical Engineering. U. of
Penns^vania, Philadelphia.
GENERAL SWITCHING THEORY, by S. Litwln.
R. McNaughton, and R. L. Wexelblat. Rept. for
July 58-Sep 60 on Contract AF 33(616)5886. 15 Sep 6a
67p. 30 refs. WADD Technical rq?t. 60-678.
Order from OTS |1. 75 PB 171 555
After summarizing the entire effort, detailed reviews
of the GO program and the work on languages of sym-
bolic logic are given. The RENJYU program is de-
scribed in detail and a natural- language leartilng model
is described. (Author)
Moore School of Electrical Engineering, U. of
Pennsylvania , Philadelphia .
SYMBOUC LOGIC AND AUTOMATA, by .Robert
McNaughton . Technical note no . 3 on GeneraTSvitch-
ing Theory, Contract AF 33(616)5886. July dO.'ibp.
10 refs . Rept. no. 60-25; WADD Technical note
60-244.
Order from OTS $1.00 PB 171 548
This paper presents certain languages of symbolic
logic for the description of the behavior of finite auto-
mata. It describes precisely the conditions under
which a formula of these languages describes the be-
havior of an automaton, and presents a synthesis al-
gorithm which constructs a state graph for an automa-
ton given a formula that describes the automaton. It
closes by listing some unsolved problems about these
languages . (Author)
Naval Ordnance Lab. , Corona, Calif.
THIN FILM MAGNETIZATION REVERSAL STUD-
IES, by Robert L. Conger. Sep 58. 18p. 5 refs.
NAVORD rept. 5929; NOLC rept. 425; AD-205 586.
Order from LC mi$2. 40, ph$3. 30 PB 150 073
The suitability of very thin evaporated magnetic alloy
films for use in coincident current memory devices
in high-speed digital computers is shown. A method
of preparing such films is outlined, and two methods
of utilizing them in memory devices are presented.
The process of magnetization reversal in thin films
is discussed. (Author)
601
Sonford Bleocronics Labs . . Stanford U . , Calif .
APPUCATION OP THE MAGNETORBaSTANCE EF-
FECT TO ANALOG NfJLTlPUCATION, by J. M.
Hunt . Repc . o» Contract Nonr- 225(24) . 25 May 60.
I32p. 10 ref 8. Technical rq?t. no. 1504-1;
AD- 239 778.
Order from L<tmi$6. 90. ph$21. 30 PB 149 333
Bounds on the performance of a magnetoreslstance are
■tudied. Empltasis was placed upoo the following
areas: (1) analysis of multiplier error In terms d con-
stituent errors . (2) theoretical analysis of the source
of certain errors caused by imperfections In the
paired magnetoresistor unit which is the novel element
at the multiplier, and (3) fabrication and test of suffi-
cient magnetoresistor elements to permit the estab-
lishment of a realistic bound on the error component
contributed by these elements . Attention also was de-
voted to methods for minimizing multiplier errors
without recourse to external corrective circuitry.
(Author)
MECHANICS
Bolt Beranek and h4ewman. Inc. [Cambridge, Maaa. 1
DAKfflNG FLEXURAL VIBRATIONS IN PLATES BY
FREE AND CONSTRAINED VISOO- ELASTIC LAYERS.
Final rept. on phases I-III of Contract NOba-
72452(375). 28 May 59, 118p. 13 refg Rept. no. 632.
Order from LC m46. 00, ph$18. 30 FB 153 794
This report ril^aaed for sale to the public 15 Mar 61.
at<kt
Gcntenta:
Measures of <»mping effectlveneaa
General analyvls of three-layer plate
Homogeneous damping treatment
Constrained -layer damping treatments
Other damping configurationa
Effects of water load and plate curvature
Experimental methoda
Bolt Beranek and Newman, Inc. , Cambridge, Mass.
MOMENT IMPEDANCE OF PLATES, by Ira Dyer.
Rept. on Contract Nonr-2322(00). 30 Mar 6a 31p.
17 refs. Rept.i no. 727; AD-234 724.
Orxler from LC mi$3. 00. ph$6. 30 PB 153 739
The moment impedance of an Infinitely extended plate
is calculated with the use of plate equations that allow
for finite transverse shear and rotatory Inertia. It is
shown that the effects at finite transverse shear may
be Important even for thin plates, a result that la
contrary to classical theory. Classical theory Is
shown to be inadequate for the caloilation at moment
impedance when the distance over which the moment
is applied is amaller than plate thickness. The mo-
ment Impedance for geon^etrles of greatest practical
Interest Is foixl to consist of a reslsunce connected
In series with a stiffness reactance, both roughly in-
versely proportional to frequency, with the reactance
of greater magnitude. Both the realsunce and the re-
actance decrelise with decreasing distance over which
the moment i« applied, because of the increasing im-
portance of transverse shear flexibility. The practi-
cal Implicatlcns erf the results are discussed, and
some tbou^ts are given concerning other problems
where claasical theory for flexural waves In thin
plates may not be applicable. (Author)
Brown U. Dlv. of Applied Mathematics. Providence.
R. I.
AN ELEMENTARY DISCUSSION OF DEFINITIONS
OF STRESS RATE, by William Prager. Technical
rept. no. 53 on Contract Nonr-562(10). Feb 60. Up.
7 refa. Cll-53; AD- 232 491.
Order from LC ml$2. 40, phS3. 30 PB 153 142
A condensed version of this paper was presented at the
First All-Union Congress at Applied Mechanics in
Moscow Oan. 27 - Feb. 3. 1960).
Brown U. Div. of Applied Mathematics. Providence,
R. I.
ON A PROBLEM OP MINIMUM WEIGHT DESIGN,
by Zenon Mr&z. Technical rept. no. 59 on Contraa
Nonr-562(10). May 60, 19p. 14 refs. Cll-59;
AD-236 729.
Order from LC mi$2. 40. ph$3. 30 PB 147 402
A problem of optimal design for perfectly plastic,
Isotropic structures Is analyzed. It is shown that for
such structures as plates or shells, an extremum
of the volume, if it exists, may be either a local
maximum or a minimum. (Author)
Brown U. Dlv. of Applied Mathematics. Providence,
R. I.
PLASTIC DEFORMATIONS IN IMPACT AND 11^
PULSIVE LOADING OF BEAMS, by S. R. BodnlT
and P. S. Symonds. Technical repc. no. 61 on Coo-
tract Nonr -562(10). May 60. 26p. 9 refs. Cll-61;
AD-239 005.
Order from LC mi$2. 70. ph$4. 80 PB 148 812
A summary of recent experimental work to evaluate
the assumptions of dynamic rigid -plastic theory Is
presented. The experiments were performed on caa-
tilever beam specimens of mild steel and of alumi-
num alloy, and tentatively indicate that strain rate
effects are the principle cause of discrepancies be-
tween theory and experiments. The need to consider
the space and time variation of the yield moment lo
interpreting experimental results Is shown, and a
mathematical model that Incorporates these features
is discussed. In a numerical example the predlctiosi
erf this model are found in excellent agreement with
experimental results. (Author)
Brown U. Dlv. of Applied Mathematics, Providence,
R I
PLASTIC DEFORMATIONS OF SQUARE PORTAL
FRAME UNDER HORIZONTAL IMPACT, by
H Tanaka. Technical rept. no. 60 on Contract Nonr-
562(10). May 60, 27p. 5 refs. CI 1 -60; AD -219 OW.
Order from LC mi$2. 70. ph$4. 80 PB 148 811
This paper presents an analysis at the plastic defor-
mations of a square portal frame subjected to a hori-
zontal Impact such that the beam instantaneously
acquires a horizontal velocity. The results show tW
602
the magnitude of mass of the beam greatly affects the
final plastic deformations. Finally, an approxlma -
don for the deformations is proposed. (Author)
Brown U. Div. of Engineering, Providence, R. I.
A NOTE ON THE YIELD STRENGTH OF A DUC-
TILE MATRIX WITH DILUTE CONCENTRATIONS OF
RIGID INCLUSIONS, by B. Paul. Technical rept. no. 5
on Contract Nonr-562(19). May 60. 8p. 2 refs.
Nonr 562(l9)/5: AD-239 645.
Order from LCmi$l. 80. ph$l. 80 PB 148 346
A simple model of particle action Indicates that the
yield strength of a dualle matrix containing a dilute
(Hitrlbutlon at rigid particles varies linearly with the
volume fraction of rigid matter. The slope of the yield
stress versus volume fraction curve is shown to be
directly proportional to the yield stress of the matrix.
(Author)
David Ta^or Model Basin, Washington, D C
THE STRESSES AROUND A RECTANOJLAR OPEN-
ING WITH ROUNDED CORNERS IN A BEAM SUB-
JECTED TO BENDING WTTH SHEAR, by
S. R. Heller, Jr. , J. S. Brock, and R. Bart. Mar 59,
3Qp. 8 refs. Rept. 13II.
Order from LC ml$2. 70, ph$4. 80 PB 154 766
This repon released for sale to the [Xiblic 15 Mar 61.
A ioiutlon for the stresses around a rectangular open-
ing with rounded comers in the web of a beam sub-
jected to bending with shear is presented. The aspect
rttlo (height to width) and the radius at curvature of
the comers are general. The complex -variable
method of MuskhelishvUi is used In conjunction with a
conformal mapping technique to obtain the solution.
Curves showing the tangential stress around the bound-
ary of a typical family of rectangles are presented. In
addition, curves are given which show the maximum
values of the boundary stress as a function of both
twpect ratio and comer radius. The numerical cases
are sufficient to cover most openings found in engl -
neering structures. The effect of small eccentricity is
given. (Author) (See also PB 154 765)
David Taylor Model Basin, Washington, D. C
THE STRESSES AROUND A RECTANGULAR OPEN-
ING WITH ROUNDED CORNERS IN A UNIFORMLY
LOADED PLATE, by S. R. Heller, Jr. , J. S. Brock.
andR. Bart. Jan 59. I3p. 13 refs. Rept. 1290.
Order from LC ml$2. 40, ph$3. 30 PB 154 765
TUa report released for sale to the public 15 Mar 61.
Reprinted from Proceedings of the Third U. S. National
Ccogress of Applied Mechanics held at Brown U. .
Providence, Rhode Island. June 11-14, 1958.
This paper presents a solution for the stresses around
a recungular opening with rounded comers in a uni-
formly loaded plate. The aspect ratio (length to width)
•nd the radius of curvature of the comers are general.
The complex -variable n^thod at Muakhelisfavill is used
to conjunction with a conformal mapping techniq^je to
crfxain a solution. Curves showing the tangential stress
around the boundary of a typical family of rectangles
are presented. In addition, curves are given which
show the maximum values of the boundary stress as a
function of both aspect ratio and comer radius. The
numerical cases are sufficient to cover most openiings
found in en^neering structures. (Author)
Harvard U. Div. of Engineering and Applied
Physics, Cambridge, Mass.
THE STRESS FIELD OF A SLIPPED CRYSTAL
AND THE EARLY PLASTIC BEHAVIOR OF POLY-
CRYSTALLINE MATERIALS, by Bernard Budiansky.
Zvi Hashin, and J. Lyell Sanders, Jr. Technical
rept. no. 7 on Contract Nonr-1866(02). Apr 60, 35p.
13 refs. AD-235 934.
Order from OTS $1. 00 PB 171 531
The initial phases of plastic deformation of polycrys-
tals during which elastic strain predominates was
studied. Consideration is given to the stresses in
single and double slip systems of crystals. Esti-
mates were made for the initial shape of the stress-
strain curve of a polycrysul on the basis of single
crystal properties. Interference effects of nteighbor-
ing slipped grains were neglected. The results ob-
tained for the polycrystal composed of grains indi-
cated that, in the absence of mechanisms of plastic
deformation other than slip, such a hypothetical
material would need stresses far above the elastic
limit for plastic strains to became comparable to
elastic strains. This is qualitatively consistent with
the behavior of zinc polycrystals, 1. e. , having but
one slip plane per crystal with three possible slip
directions per plane, which tend to exhibit very non-
ductile behavior up to fracture. For a face -centered
cubic material, the elastic -plastic material may
have an uniaxial stress-strain curve that is asymp-
totic to the Taylor limit; part of this asymptotic ap-
proach is shown. Errors originate not only from the
neglect of the influence of multiple slip but also from
the neglect of interaction between slipped grains as
the concentration approaches 100%.
Institute of Engineering Research, U. of California.
Berkeley. *
STRESS- STRAIN RELATIONS IN PLASTiaTY AhD
THERMOPLASnaTY, byP. M. Naghdl. Technical
rept. no. 9 on Contract Nonr-222(69). Mar 60, 86p.
80 refs. Series 131, issue 9; AD-236 454.
Orderfrom LCml$4.80, ph$13.80 FB 153 767
Contents:
Isothermal stress-strain relations i'
Fundamental concepts. Stress-strain relations
Subsequent loading surfaces: hardening rules
Singular regimes and their use with total strain
theories
Thermoplasticlty
Non- isothermal plastic deformation
Basic concepts in Irreversible thermodynamics
Irreversible themnodynamics and plastic stress -
strain relations
603
Lockheed Aircraft Corp. . Sunnyvale. Oilif.
ON THE ROLE QF BEhfDlNG IN THE DYNAMIC
RESPONSE OF THIN SHELLS TO MOVING DIS-
CX)NTINLIOUS LOIADS. by Pauline Mann Nachbar.
Technical rept. ofi Mathematics. June 60, 55p.
5 refs. LMSD-70i021; AD-243 181.
OrtJer from LC n^3. 60, ph$9. 30 PB 153 502
vniii
Mellon tost. , Ptttsburgh, Pa.
NORMAL STRESSES IN SECCWD ORDER VISCO-
ELASnCITY, by Bernard D. Coleman and Walter Noll
(Carnegie bi»t. at Tech. ) Rept. cxi Contract
AF 49<638)541 and National Science Foundation Grant
NSF-G 525a Dec 60, lOp. 5 ref«. AFOSR-
TN- 60- 1461; AD-p4« 596.
Order from LC mi$l. 80, ph$l. 80 PB 153 749
Some prediction* are indicated concerning the normal
stresses derived from the second order theory at In-
compressible visf»elastic fluids.
Metals Research Lab. , Carnegie Inst, of Tech. ,
Plnsburgh, Pa.
ENERGY OF CRACK FORMATION AND CRACK
PROPAGATION UT^DER IMPACT LOADING, by Cyril
Wells and W. B. Triplett. Rept. for 1 July 58-31 Dec 59
on Mechanisms oi Ductility and Fracture, Contract
AF 33(616)5830. Aug 60, 71p. 17 refs . ARL Technical
J2.
note 60-124. AD-1248 508
Order from LC nii$4.50, phJ12.30
PB 153 856
A basic study of ^) the relative energies of crack for-
mation aixl crack, propagation and (b) mechanisms of
fracture occurring under impact loading has been
made . The proceidure developed for determining crack
formation, crack propagation, and overall impact
transition curves from impact versus testing tempera-
ture data has beeti shown to be reliable and to have a
wide application.! Crack formation, crack propagation,
and overall impact energies have been determined for
standard V-notch'CharpY specimens from several
steels having body-centered cubic structures and from
an annealed comniercial tiunium having a close-
packed hexagonal structure. For the steels , a deter-
mination has bee4 made of the effect on these energies
of testing temperiture, tensile strength, anlsotropy,
and composition. Composition variations were small
and limited to (a)<changes of impurity content,
(b) changes of cotiposition within the AlSl 4340 limits ,
and (c) boron plui rare earth additions . (Author)
Polytechnic Inst^ d Brooklyn, N. Y.
EXTENSIONAL VIBRATIONS OF ELASTIC SAND-
WICH PLATES, \iy Yi-Yuan Yu- Technical note no. 9
on Contract AF 4^(638)453. Oct 60, 13p. 2 refs.
AFOSR-TN-60-1129; AD- 248 301.
Order from LC nH$2.40, ph$3.30 PB 153 639
Three systems o^ extenslonal equations d motion of
symmetrically arranged three-layered elastic plates
are presented. The first system takes Into account al
thickness -stretcli deformation of both the core and
face layers, and the second only that at the core. In
addition to the ex|ensianal deformation of the layers.
The third system takes no consideration of thickness-
stretch deformation and Is thus of the classical type.
It is shown that, for ordinary sandwich plates that
have relatively thin but heavy and rigid face layers,
all three systems of equations yield practicaUy the
same result for the lowest branch of the frequency
spectrum of extenslonal vibration of an infinite sand-
wich plate covering low frequency ranges. For such
plates and for such low frequency ranges, considera-
tion of thickness -stretch deformation is therefore un-
necessary, in contrast to the case of flexural vibra-
tion of such plates, for which the Inclusion of thick-
ness-shear deformation cf the core is an absolute
necessity even for low frequencies. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
FLEXURAL VIBRATIONS OF RECTANGULAR SAND-
WICH PLATES^ by Yi-Yuan Yu. Technical note no. 8
on Contract AF 49(638)453. Aug 60, 18p. 10 refs.
AFOSR-TN-60-953; AD- 248 073.
Order from LC mi$2.40, ph$3.30 PB 153 638
On the basis of three recently derived systems of
flexural equations cf motion the free vibrations of In-
finite sandwich plates in two dimensions and simply
supported rectangular sandwich plates are investi-
gated. (Author)
Polytechnic I net . of Brooklyn, N. Y.
PLASTIC INTERACTION CURVES FOR CIRCULAR
CYLINDRICAL SHELLS UNDER COMBINED LAT- .
ERAL AND AXIAL PRESSURES, by R. Sankarana-
rayanan. Rept. on Contract Nonr-839(17). May 60,
15p. 3ref8. PIBALrept. no. 563; AD- 237 075.
Order from LC ml$2. 40, ph$3. 30 PB 147 757
A Circular cylindrical shell, made of a rigid perfectly
plastic material, is subjected to a lateral pressure P
and an axial compressive pressure Q. The shell Is
built-in at one end and free at the other. The nruterlal
of the shell is assumed to obey Tresca's yield condi-
tion and the associated flow rule. Plastic interaction
curves based on a linearized yield surface are ob-
tained for all values of P and Q. (Author)
Aerodynamics and Pneumatics
Aero-Space Labs. , North American Aviation. Inc.
EFFECT OF ROUGHNESS ON TRANSITION IN
SUPERSONIC FLOW, by E. R. Van Driest and C R.
Blumer. Rept. on Contract AF 49(638)250. Mar 60,
38p. 4 refs. MD 60-329; AFOSR-TN-60- 1164.
Order from LC ml$3. 00, ph$6. 30 PB 153 743
Further experiments carried out to Investigate the
effect of three-dimensional roughness elements
(spheres) on boundary- layer transition on a I0-degr«s
(apex ar^le) cone without heat transfer are reported.
The local Mach number for these tests was 2. 71. T^
dau show clearly that the minimum (effectlv^ size of
trip required to bring transition to Its lowest
Reynolds number varies as the one-fourth power of
the distance from the apex of the core to the trip.
Use of available data at other Mach numbers indicates
that the Mach number influence for effective tripping
is uken into account. (Author)
604
Avco- Everett Research Lab. , Mass. - -
UNSTEADY ABLATION, by Steven Georgiev. Rept on
(}oatract AF 04(647)278. Sep 59, 25p. 2 refs. Re-
tearch r«pt. 94; AFBMD TR-60-180.
Onler from LC mi$2. 70. ph$4 80 PB 153 568
"pie transient ablation proceas for non- radiating glass>
materials Is discussed and numerical calculations are
presented for quartz along an ICBM trajectory. It is
lliafirn that the transient effects do not appreciably af-
toct the amount of ablated material along the trajec-
tory, but that they affect very significantly the amount
of Inaulating material required after ablation ceases.
The transient ablation analysis la also applied to
quartz under arc wind tunnel heating conditions and it
Is shown that the experimentally obtained ablation his-
tory can be used to deduce the high temperature
thermal diffusivity of the ablating material. (Author)
Bell Aerosystems Co. , Buffalo, N. Y.
A NEW APPROACH TO SAFE FUGHT FLUTTER
TESTING, by Melvin B. Zisfein and Benjamin B.
D'Ewart. Rept. on Contracts AF 49(638)749 and
AF 49(638)380. Sep 60, 45p. Rept. no. 9015-19-002;
AFCSR TN-60-1027.
Order from LC mi$3. 30, ph$7. 80 PB 152 687
The basic research program was concerned with the
lynthesis , analysis , and experimental evaluation of a
new method of flight flutter testing . The method is
based on the well known fact that small changes in
mass distribution can drastically change the vibra-
donal properties of an oscillating aero-dynamic sur-
ftce, and can bring about substantial changes in its
flutter speed . This method employs a Jet device to
ilmulate the force effects of mass and to create
thereby an apparent change in the mass distribution of
sn aerodynamic surface. This apparent mass change
can be easily manipulated to make flutter come or go,
•nd can therefore be used as a safe, fail safe, posi-
tive, flight flutter test device. This report presents a
very brief historical backgroufkl, a discussion of the
bisic principles of "jet mass" and its effect on flutter,
sod a^ description of the design deuils of two Jet mass
prototypes/and a wind tunnel fluner nwdel . Subse-
quent sections of this report describe the laboratory
•nd wind tunnel tests on the prototype jet mass sys-
tems. The repori is completed by a statement of con-
clusloos including recommendations for future Jet
mass system development. (Author)
ktmn U. Dlv. of Applied Mathematics,
Providence, R. I.
TWO INITIAL VALUE PROBLEMS IN ISOTROPIC
TURBULENCE, by W. H. Rdd. Technical rqx. no. 33
on Contract Nonr-562(07). Mar 60, 37p. 3 refs.
AD- 235 030.
Order from LC ml$3.00, ph$6.30 PB 153 737
l^D initial value problems are considered which lllus-
trtte the detailed transfer of energy between different
wave numbers. In the first problem, the initial energy
distribution consists of two line spectra whose subse-
VK interaction Is studied. The resultant distribution
^••Sy transfer consists of three distlna parts: the
tateractlon of two lines with themselves which result
In continuum contributions centered about each of the
and the mutual interaction which results In a
further continuum contribution centered about the
line located at die larger wave number. In the second
problem, the initial energy distribution consists of a
line spectrum and a continuous spectrum of the "final
period" type. The interaction between these spectra
is strongly dependent on the position of the line spec-
trum relative to the continuous spectrum. In both
problems it is found that there Is a local transfer in
both directions about any given wave number but that
the overall transfer is in the direction of large wave
numbers. (Author)
Brown U. Dlv. of Engineering, Providence, R. L
LINEARIZED TRANSCWIC FLOW ABOUT SLENDER
BODIES AT ZERO ANGLE OF ATTACK, by P. F.
Maeder and H. U. Thonunen. Rept. on Contract
AF 49(638)444. Oct 60, 40p. 14 refs. Technical rept.
WT-34; AFOSR-TN-60- 1247; AD- 248 228.
Order frtxn LC mi$3. 00, ph$6. 30 FB 153 644
The simple linearized transonic flow theory as origi-
nally proposed by Oswatitsch and Keune (Proc. erf the
Conference on High-Speed Aeronautics, 1955) and by
the present authors (]. Aeronautical Science 23: no. 2,
1956) is improved by considering and partially cor-
recting its error. In this manner a theory which is
easy to apply and which should be valid for a great
number of smooth bodies is obuined. This Improved
theory predicts shock Waves in the lower transonic
regime. It Is applied to a number of significant body
and airfoil shapes and its predictions are compared
with experiments and results of other theoretical
investigations. (Author)
Cornell Aeronautical Lab. , Inc. . Buffalo, N. Y-
THE TWO-DIMENSIONAL EFFECTS OF SLIP-
STREAM SHEAR ON AIRFOIL CHARACTERISTICS,
by R. J. Vidal, J. H. Hilton, and J. T.Curtis. Rept. on
Contract DA 44-177-TC-439. Sep 60, 93p. 27 refs.
Rept. no. AI-1190-A-5; TREC Technical rept. 60-56;
AD- 246 522.
Order from LC mi$5. 40, pfa$lS. 30 PB l53 463
The available theories for two-dimensional airfoils In
uniform and non- uniform shear flows of infinite extent
are reviewed. An inuige analysis Is presented to make
these reaults applicable to shear flows of finite extent.
Experiments with a two-dimensional symmetrical
Joukowsky airfoil in uniform shear flow and in simu-
lated two-dimensional propeller slipstreams are de-
scribed. Results are compared with the applicable
theory. The airfoil section characteristics can be
predicted with good accuracy at all positions tested in
the slipstream. (Author)
Cornell Aeronautical Lab. , Inc. , Buffalo, N. Y.
WEAK, NONEQUILIBRIUM, DIFFUSIVE WAVES IN
A DISSOCIATED GAS, by F. K. Moore and J. T.
Curtis. Rept. on Contract Nonr- 2653(00). Feb 60,
16p. 8 refs. Rept. no. AF-1285-A-1; AD-234 107.
Order fixxn LC mi$2. 40. ph$3. 30 PB 153 125
A theoretical study is made cf the nonsteady diffusive
wave produced in a semi -Infinite region filled with
dissociated gas, initially at rest, when a weak
temperature disturbance Is imposed at the bounding
plane. The effects of 2 specific typ^s of disturbance
tiOS
•re studied: wall temperature varying exponentially
with time, and trail temperature undergoing a step-
function In tlmei Finite reaction rates and wall cataly-
clty are assumed. The puticular purpose of the
present study is to contribute to a qualitative picture
at nonequlllbriian viscous phenomena, emphasizing
analytical solutkns at a simple character, which have
a bearing, by analogy, on non- linear boundary- layer
problems. Especially simple scHutlons are otxained
by assuming that, during a temperatur* change at
constant pressure, the heat absorbed by internal de-
greet at freedoti Is much less than the heat of chemi-
cal reaction absorbed. This assumption Is particu-
larly appropriate at low preaaures. (Autlior)
Prick OienrUc^l Lab. , Princeton U. , R J.
THE THlCK>fESS OF SHOCK FRONTS IN ARGON,
by K- Hansen aUd D. F. Homlg. Technical repc.
na 1 on Oootratt Nonr- 1858<24). 5 Jan 60. 13p. 9
refs. AD- 231 4$0.
Order from LC mi$2.40, ph$3.30 PB 152 895
The accuracy and sensitivity at the optical reflectivity
mccbod for determining the thickness d shock fronts
were improved. The chicknessea at shock fronts in
Ar were measured up to M - 2.38. Moat o< the effort
was conceiffratad at M ■ 2.38 where the reciprocal
thickness in mean free paths, Iq/L© " 0.234 1. 007.
At M ■ 2.38 the Croot is about 20^ thicker than calcu-
lated from the Navler- Stakes equations but the tliick-
ness agrees very closely with tliat calculated by
Muckenfuss usliig a bimodal dlstrlbutian function.
(Author)
Institute of En^eerlng Reaearch. U. of California,
Berkeley.
SOME PRELIMINARY RESULTS IN SEPARATED
FLOW AERODYNAMICS, by L. L. Lynes and S. A.
Schaaf. Rept. <ii Contract Nonr- 222(45). 10 Feb 60.
12p. 2 refa. R^t. no. HE-150-178; Serlea no. 20.
laaue no. 133; Xo-234 018.
Order from LC mi$2. 40, ph$3. 30 PB 153 118
A preliminary eeq)erlmental investigation is reported
of separation phenomena on a hemiapherlcally capped
cylinder with a conical skirt. It was found that sepa-
ration existed itj the region between the cylindrical
body and the for^»rard face of the conical skirt. The
separation point was on the shoulder of the hemispher-
ical cap and the' reattachment was at or near the heel
of the conical sMirL These two points remained
oearly fixed as the axial length of the cylinder in front
da the conical skirt was increased until a point was
Reached where ifie separation point began to slide
back along the body. Also, no hysteresis was de-
tected as a function of forward or aft nK>vement of
the conical akirt. (Author)
National Research Labs. , Ottawa (Canada)
REFLECTION OF A PLANE ACOUSTIC SHOCK BY
A SURFACE O^ REVOLUTION, by P. Mandl. Aug 60,
104p. I3ref8. Aeronautical rept. LR-289; AD-249 103.
Order from LC JmiSS. 70, ph$l6. 80 PB 153 475
The Influence o^ a structure on the pressure field and
form of a passlag shock wave, and that of the shock
wave on the atructure. are of conaiderable practical
and theoretical interest. This report extends exlstlai
two-dlmenaicnal theory to the case at bodies of revolu-
tion. Although the resulting series solutions for the
general caae are rather unwieldy, they permit certali
conclusions about the transient loading on a struaure
as a function at the principal curvatures of its bounda-
riea. When the solutions are applied to the particular
caae at a spherical reflector, they are considerably
simplified, and permit the transient loading and the
blast impulse at varlou^ positions on the boundary to
be calculated, for various forms at incident front. Tht
solutions converge well near the stagnation point but
are leaa aatisfaaory near the ahadow boundary. The
results compare well with previous two-dimensional
calculations. Certain extensions of the theoretical
approach are suggested. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
BLUNT BODY HEAT TRANSFER AT HYPERSONIC
SPEED AND LOW REYNOLDS NUMBERS, by
Antonio Ferri, Victor Zakkay, and Lu Ting. Rept.
on Contract AF 33(616)6118. June 60. 79p. 19 refa.
PIBAL rept. no. 611; ARL Technical note 60-140;
AD-242 704.
Older from LC mi$4. 50. ph$l2. 30 PB 150 636
An analytical method for the determination of the
effect at shock curvature on heat transfer in the re-
gion of the nose was developed. For practical body
shape the viscoua terms in the Navier -Stokes equa-
tions are not important in the region of the flow far
from the wall and the displacement thckness can be
neglected. Then the flow can be approximately rep-
resented by an inviscid flow solution ha/lng as bound-
ary conditions the body shape, which is not affected
by the Reynolds number and by a boundary layer type
of flow near the wall, having appropriate boundary
conditions. This approach permits us to determine
the heat transfer in the region of the nose even at
very low Reynolds numbers. Bxperin^ntal results
are presented. The experimental results agree with
the values given by the analysis. (Author)
Polytechnic Inst, of Brooklyn. N. Y.
INTEGRAL METHOD BOUNDARY LAYER CALCU-
LATIONS FOR STRQNG FAVORABLE STREAMWBB
PRESSURE GRADIENTS, by Martin H. Stelger. Re|X.
on Aertxlynamlc and Heat Transfer Problems in Hyper-
sonic Flow, Contract AF 33(616X»118. July 60. 17p.
6 refs. PIBAL rept. no. 613; ARL Technical note
60-137; AD-242 171.
Order from LC mi$2. 40. ph». 30 PB 150 327
The two-dimensional, laminar, incompressible
boundary layer with strong favorable pressure gradi-
ents Is bivestlgated. Similar and non -sim liar solutioi
are olxained, covering the range of the shape factor
2< ;!<,"•. ^milar solutions, corresponding to A"
constant, are given In closed form. Well -behaved nor
similar solutions are derived and an approximate so-
lution for non-similar flows in which A>100 is glvet
in closed form. (Author)
606
polytechnic Inst, of Brooklyn, N. Y.
LAIflNAR FLOW IN FINITE POROUS CHANNEL
fTTH VARL^BLE INJECTION OR SUCTION, by
Kooo-Sang Wan. Rept. on Contraa AF 49(638)445.
Sep 60, 56p. 9 refs. PIBAL rept. no. 614; AFOSR-
TM-60-1197; AD- 248 666.
Order from LC ml$3.60. ph$9. 30 PB 153 837
An Investigation was carried out to obtain the incom-
pressible laminar flow characteristics In a channel
with porous walls of finite length In which fluid is
beli« Injeaed or sucked through the channel walls.
An approximate solution Is obtained based on the varl-
ttional principle. This solution is expressed in terms
of the given, but arbitrary, function charaaerlzing
(be variation of the injection velocity at the parous
•alls for any given velocity profile at the entrance to
the porous region It depends on two parameters, the
Reynolds number Rg and the nondimenslonal maximum
iBjealon velocity Vq, both of which are based on a re-
duced maximum velocity at the entrance. A similarity
rule for the present jn-oblem is then established,
numerical examples are given for the case where the
etfraoce velocity profiles are "inlet" or parabolic and
the injection velocity ia a ccnaunt or varies linearly.
The reaults of the flow characterlBtica for these ex-
anqriea for different valuea of v^ are presented in the
fonn of curves . (Author)
Polytechnic Inst, of Brooklyn, N. Y.
PERTURBED BOUNDARY LAYER SOLUTIONS
APPUED TO THE WALL JET AND BLASIUS
PROFILE, by Martin H. Bloom and Martin H. Steiger.
Rept. on Contract AF 49(638)217. Oct 60. 40p.
lOrefi. PIBAL rept. no. 471; AFOSR-TN-60- 1340.
Order from LC ml$3. 00. ph$6. 30 PB 153 838
Two types of first-order perturbation solutions are
investigated. In the first limiting case It is assumed
that the zero-order solution is that of a wall Jet with
»ro outer -velocity, and the first-order cwrection
ODhaiders the effect of a small outer streamwise flow.
The special case of the constant velocity is treated in
detail. In the second limiting caae the consunt pres-
sure Blasius solution is taken as the zero-order solu-
ttoo and the first -order correction is a wall Jet type of
fkw. Thia investigation considers both twa-dimen-
aional and axially symmetric flows. (Authn:) ^. .
V.
Polytechnic Inst, of Brooklyn, N. Y.
RATE CHEMISTRY AND FLOW OF AN AIR-UKE
MIXTURE, by Harold Rosenbaum and Martin H.
Uoom. Technical rept. on Aerodynamic and Heat
Transfer Problems in Hypersonic Flow, Contract
AP 33(616)6118. Aug 60, 38p. 13 refs. PIBAL rept.
no. 533; ARL technical note 60-145; AD-246 440.
0n»erfromLCmi$3.00. ph$6.30 PB 153 183
An investigation of the inviscid non-equilibrium molec
ular dissociation and recombination of a flowing
model gas consisting of oxygen and nitrogen is pre-
sented here. One reaction and one catalyst each Is
•ssumed to describe the rate chemistry of oxygen and
nitrogen. Similarly one reaction is used to describe
the chemistry of the production of ions . These rate
equations . the statistical thermodynamic equations .
•ad the conservation equations are combined to deter-
mine the flow field. Four representative calculations
were performed. The rate of dissociation of oxygen
and nitrogen through normal and oblique shock waves
with constant pressure downstream was investigated.
Another constant pressure calculation through a nor-
mal shock wave was performed to determine the elec-
tron density. A complete calculation around a b}unl
body with prescribed pressure distribution investi-
gates all the flow variables . The final calculation was
performed to Investigate the effect of a normal shock
wave on the wake of a blunt body. Constant pressure
was assumed behind the wave in ttiis case. (Author)
Rensselaer Polytechnic Inst. , Troy, N. Y.
ON THE MAGNETOHYDRODYNAMIC BOUNDARY
LAYER THEORY, byK. T. Yen. Rept. on Contract
AF 49(638)23. Sep 60. 22p. U refs . TR AE 6004;
AFOSR-TN-60- 1162; AD-246 623.
Order from LC ml$2.70. ph|4.80 PB 153 262
Boundary layer equations for two-dimensional steady
magnetohydrodynamlc flows are derived and some ,
physical problems such as the relative order of magni-
tude of viscous and magnetic terms , the velocity and
magnetic field boundary layer thicknesses . etc . are
discussed. The momentum and energy Integral equi(-
tions for magnetohydrodynamics are also cAtained.
Consideration is given to two magnetohydrodynamlc
flows . The first one is the flow over a flat plate ana-
lyzed by Greenspan and Carrier Q. of Fluid Mechanics
6, I*- ^H P' ^7''^' J"^y 5'^- ^' ** pressure ratio
p«p, Hg /^^^ J approaches one, Greenspan and
Carrier showed that the flow is plugged while the mag-
netic field is amuiled. It it shofwn in this work, how-
ever, that there exists another solution when the elec-
tric conductivity of the fluid is very large and P ■ 1 .
This solution yields the result that the flow is plugged
but the magnetic field is uniform and undisturbed. The
second flow is concerned with Jet mixing under a mag-
netic field directed along the Jet axis . The flow plug-
ging phenomenon Is also found to occur. (Author)
University of Southern California. Engineering
Center, Los Angeles.
THE STRUCTURE OF STRONG SHOCK WAVES OF
STABLE MONATOMIC MOLECULES^ by Toyoki Koga.
Technical note on Contraa AF 4 9(638)831. Oct 60,
68p. 19 r«fs. USCEC rept. 83-201; AFOSR-TN-60-
1344" AD- 247 335.
Ordjsr from LC iiil$3.90, ph$10.80 PB 153 428
Tlie present theory of plane shock waves of a mooa-
tomic gat is based on three hypothetical assumptions
according to which two series of distribution functions
are designed. There is no serious mathematical
difficulty in solving five equations of moments by
which the five unknown variables involved In an
assumed distribution function are determined. The
results are compared with those of other authors.
According to the results, the initial assumptions seem
to be plausible as long as the theory is confined in a
limited domain of interest so that moments of hi^ier
orders with respect to Cy and c^ are not involved in
the theory. (Author)
607
Vidya, Inc., Palo Alto, Calif.
AERODYNAMIO APPUCATIONS OF PLASMA WIND
TUNNELS, by Jfcu:kson R. Stalder, Frederick K.
Goodwin and others. Kept, for July-Dac 59 on Re-
search on Aerodynamic Flow Fields, Contract
AF 33<616)6704, Dec 60, 12^ 23 refs. WADD Tech-
nical note 60-1.
Order from LC mi$6.30, ph$19.80 PB 152 582
An investlgatloa has been made of the use of arc-
heated plasma wind tunnels to determine their useful-
ness in aerodynamic and thernxxlynamlc experimenu-
tion. In order cd establish the range of aerodynamic
and thermodynamic variables of interest trajectories
have been calculated for representative hypersonic
vehicles of current and future interest. From these
trajectories, thie pertinent aerodynamic and thermo-
dynamic variables have beeo calculated and ploaed.
A parametric study has been made of the character-
istics produced by arc-heated plasma wind tunnels.
These calculaticns were made for flow in chemical
equilibx-ium and for flow whose chemical composition
was frozen at scagnaticn conditions. These two cases
will bracket any case where the flow is initially in
equilibrium and, freezes in composition during its ex-
pansion in a supersonic nozzle. The vehicle charac-
teristics, in cotjunctioD wid^the wind-tunnel charac-
teristics, then permit a comparison between aerody-
namic and cheriDodynamlc variables encountered in
flight and those conditions produced by arc-heated
plasma wind tunnels operating under a wide range of
initial or stagnatioD conditions. (Author)
Hydrodynarnic*, Hydraulic*, and Hydrotfotict
irni
Army Tranaponation Research Command, Port
Bustia, Va. '
OFFSHORE DWCHARGE (PNEUMATIC WAVE
ATTENUATIOM FULL-SCALE TANK TESTS), by
Stuart N. Sherfc Engineering rept. on ProJ. 9R98-06-
Oia House Task 14.63. Dec 60. Il2p 22 refs.
TRBC Technical rept. 60-26; AD-247 470.
Order from LC!ml$6. 00. phflS. 30 PB 153 416
] •
This study covers an investigation of the practica-
bility of utilizing rising air bubbles in water to
achieve height aftenuationof ocean-size waves. Basic
wave theory, odeanographlc definitions, and operat-
ing principles of pneumatic wave attenuation are pre-
sented primarily as they apply to inshore ocean wave
areas. Specific interest in concept application is di-
rected toward iiicreasing Transportation Corps capa-
bilities in the discharge of ships' cargo in offshore
operations. Details of a full-scale tank test are
given; and, to ctxrfirm the validity of the results and
figures presented and to clarify some of the basic
coDcepcs of pneumatic ware attenuation, basic theory,
sample calculations, problems, and derivations are
shown. (Author:
Chesapeake Bsy bist. , Johns Hopkins U. ,
Baltimore, Md,
SURFACE WAVES AT SHORT FETCHES AND LOW
WIND SPEEDS. A FIELD STUDY, VOLUME 1, by
Blair IQnsman. Bept. on Contract Noor-248(20X
May 60, 191p. 50 refs. Tehnical rept. 19; Reference
60-1; v. 1; AD- 241 166.
Order from LC ml$8. 70, ph$30. 30 PB 149 891
A study of 24 point records of surface waves made at
short fetches and low wlndspeeds is reported. It Is
found that the characteristic departure of the observed
distribution of water heights from the Gaussian con-
sists of an elevation of the positive tail, a depression
of the negative tail, and a shifting of the mode toward
negative values. The deformation Is more pronounced
for shorter fetches and lighter winds. Evidences of
nonlinear Interaction are found in the wave spears,
which tend to support the suggestion that a nonlinear
theory of surface waves should be carried at least to
third order for realistic result^, h is found that for
sharply peaked spectra the equilibrium range may not
begin until frequencies are reached greater than three
times the frequency at which the maximum power it
located. (Author)
David Taylor Model Basin. Washington, D C
ON THE STATISTICAL MECHANICS OF GRAVITY
WAVES, by J. Kampe de P^rlet (U. of Lille). Jan 6a
Up. 2 refs. Rept. 1370.
Order from LC ml$2. 40, ph$3. 30 PB 154 767
This report released for sale to the public 15 Mar 61.
Methods of sutistical mechanics have been applied to
study gravity waves. The waves are assumed to be
progressing in the direction of the positive /-axis and
their elevation 7(J(, t) is considered as an almost peri-
odic function of x and the time t. Special consideratJoi
is given to the caae when the distribution of wave nun-
bers follows the Poisaon law. (Author)
Hydrodynamics Lab. , Cabf. Inst, of Tech.,
Pasadena.
THE ANALOGY BETWEEN SURFACE WAVES IN A
UQUID AND SHOCKS IN COMPRESSIBLE GASES, b)
H. E. Crossley, Jr. Memo. rept. on Experimental
Study on Wave Forms, Contraa hK)rd-96l2. Apr 49,
I5p. 2 refs. Rept. no. M-54.2.
Order from LC mi$2. 40, ph$3. 30 PB 154 745
This report released for sale to the public 16 Mar 61.
Measurements to determine wave strength and veloc-
ity should not be made too near the generator: a dls-
unce greater than 20 inches is desirable. A wave o(
given strength can be generated by a proper choice of
initial water depth in the ripple tank and of air inlet
diameter on the generator. To minimize decay of
wave strength, a large generator head and a small alt
inlet diameter should be used. Waves identical witMl
experimental error will be created by the two availa-
ble generators If the water is raised in the generators
to a height between 19 and 21 centimeters. The addi-
tion of a detergent to the working fluid results in
smoother waves and steeper wave fronts for shock
waves of Intermediate strength, but causes accentua-
tion of the oscillatory nature of weaker waves.
(Author)
608
Institute of Engineering Research, U. of CalifomlA,
Berkeley.
WATER WAVES. IV, by E. V. Laitone. Rept. on
Contiact Nonr-222(30). Nov 59, 95p. Series no. 82,
igngno. 11; AD-229 400.
OiderfromLC mi$5.40, ph$15. 30 PB 150 510
Contents:
Shallow water waves
The fundamenul equations for the first approxima-
tion
The linearized shallow -water theory
Linearized shallow -water theory applied to 2-dl'^
mensional steady flow
ItoaUnear shallow -water theory
One-dimensional non-steady, first-order, shallow-
water theory
Two-dintensional, steady, supercritical flow by
the first -order shallow -water theory
One -dimensional, steady, open channel hydraulics
and the hydraulic jump
Higher order theories and the solitary and cnoidal
waves
The first and second approximations to the cnoidal
and solitary waves
The limiting height and velocity of propagation of
cnokl*' and solitary waves
Lockheed Aircraft Corp. , Sunnyvale, Calif.
HYDROFOILS. AN ANNOTATED BIBLIOGRAPHY, by
K. D. Carroll. Sep 60, 39p. 85 refs. Special bibliog-
raphy SB- 60- 36; AD- 244 916.
Order from OTS $1.00 PB 171 502
TUs bibliography Is the result of a brief investigation
of recent developments in hydrofoil design and testing,
hems have been selected from the holdings of the
Tachnlcal Information Center Lockheed Missiles li
Spux Division, and, to some extent, the Armed Serv-
ices Technical Information Agency. The reports
iSMSd by the National Aeronautics and Space Adminis-
tntlaii were ixx exhaustively checked; however, a
■mber of these documents were selected from their
nnore recent publications that are in the LMSD Tech-
nical Information Center. (Author)
Michigan U. , Ann Arbor.
HYDRODYNAMIC STABILITY AND THE INmAL
VALUE PROBLEM, by K. M. Case. Research
iponiored by ONR. 14 Apr 60, 15p. 9 refs.
AD-240 618.
Order from LC mi$2. 40, ph$3. 30 PB 149 782
Natloaal Research Labs. , Ottawa (Canada).
ANALYSIS OF NEW BED- LOAD TJIANSPORT DATA
IN TERMS OF MEY ER- PETER -MULL ER, REGIME
"TOEORY", ANDH. A. EINSTEIN FUNCTIONS, by
Di J. Knapp. 25 Aug 60, 34p. 4 refs. Mechanical
iHlMiiii lag rept. MH-100.
(Mar from LC mi$3.00, ph$6.30 PB 154 339
Ite twofold purpose of this report is to publish new
bad- load transport dau in the form of the Meyer -
-Mailer, Regime "theory", and H. A. Eln-
analyses, ail of which are well known, and to
give an appreciatioi^ criticism and comparison of
each of these methods, particularly regarding their
application to grain size mixtures of varying specific
gravity. Of these three, the first two were found to
define the rate of transport within the narrowest
limits but neither was considered capable of exact
quantitative bed-load prediction. For each of the
three analyses these new dau have extended the range
of previous experimental observation in the direction
of the threshold of bed-load transport. (Author)
Reed Research, Inc. , Washington, D. C
RESEARCH TO WORK OUT A THRUST C«DUC-
TION EVALUATION OF THE SUBMARINE ALBA-
CORE (THE CONSTRUCTION OF THE TOTAL
HARMONIC VELOCITY FIELD AROUND A GEN-
ERAL ELLIPSOIDAL SUBMARINE WITH ONE PRO-
PELLER), by Johann Martinek, Henry de Beaumont,
and Gordon C K. Yeh. Final rept. (II) on Contract
Nonr-2192(00). 1 Aug 58, 25p. 4 refs. AD-218 852.
Order from LC mi$2. 70, pb$4. 80 PB 154 431
This report released for sale to the public 8 Mar 61.
Necessary details are given in reference to the
Green's function of first klixl pertaining to the
Dirichlet problem. Then the Neumaiui function for
the general ellipsoid is derived. Considerations of a
more general nature and interest are discussed whidi
are concerned with the construction of the most gen-
eral types of scdutions in terms of the derived Green
or Neumaiui function, which finally solves any type of
related problem. (Author)
S^ce Sciences Lab. , General Electric Co. ,
Philadelphia, Fa.
EFFECTS OF END CURRENT LOOPS CW THE
VELOCITY PROFILE IN A MAGNETOHYDRO-
DYNAMIC CHANNEL, by A. W. Carlson and G. W.
Sutton. Rept. on Contract AF 49(638)914. Dec 60. 39p.
2 refs. Technical Information Series R60SO439;
AFOSR-TN-60-1183. AD- 248 631.
Orxler from LC ml$3. 00, ph$6. 30 PB 153 835
The effect of the end current loops on the velocity
profile in a magnetohydrodynamic flow has been in-
I vestigated for incompressible inviscid flow in a rec-
tangular channel. The end current loops interact with
the applied magnetic field to produce Lorentz forces.
In the entrance region cf the ciiannel, the Lorentz
forces vary in magnitude and direction. This vari-
ation of the Lorentz forces causes the velocity of the
fluid to increase near the walls of the chaiuiel aixl to
decrease near the center. The ratio of the changes in
velocity to the initial velocitv is directly proportional
7B ^Po
to the interaction parameter * , V ■ For a value
R du
of ^ = 0. 25, the maximum diange in velocity
is I0%at the initial velocity. (Author)
velocity.
609
METALLURGY
Banelle MenDorial Inst. , Columbus, Ohio.
THE EFFECT OF HYDROGEN ON THE MECHANI-
CAL PROPERTIES OF TITANIUM AND TITANIUM
ALLOYS, by 0 A. Letmlng, C. M. Crmlghead, and
R.I. Jaffee. S4immary rept. no. 3. 1 Aug 53-
31 July 54. on Contract DA 33-019-ORD-938.
31 July 54. 99i>. 6 refs. WAL 401/79-31.
Order from iJ^ mi$5. 40. ph$I5. 30 PB 154 749
This report relleased for sale to the public 15 Mar 61.
Results are given on the effea of notches, testing
speed, and te«ing temperature on hydrogen ennbrltlje-
ment of high-purity titanium, commercial purity
titanium (A-5S). and the commercial 8 per cent man-
ganese alloy (C-llOM). The effect erf hydrogen on the^
microstructure and mechanical properties at alpha-
beta and beta Utanlum-molybdenum alloys is pre-
sented. Hydrc^en pickupof A-5S andC-llGMUtanium
alloys in sodiifn hydride and Virgo descaling and add
pickling was also investigated. The removal ot hydro-
gen by vacuun) annealing of A-55 and C-llCM titanium
was studied. (Author)
Birmingham 0. (Gt. Brit.)
RESEARCH OU ST RAIN -AGEING, HARDENING A^D
SOFTENING OF METALS BY FATIGUE. PART I.
FATIGUE OF ALUMINIUM- MAGNESIUM ALLOYS.
PART n. FAllGUB OF ZINC SNGLE CRYSTALS.
byG. W. J. Wlaldron, T. Broom, and J* M. Summer-
too . Technical (final) rept . on Contract
AF 61(514)1182. Aug 60, 88p. 26 refs . AFOSR-TR-
60-170. AD- 246 965
OrderfromL4:mi$4.80. phH3.EflD PB 153 298
As -extruded aluminium-magnesium alloys have hl^
ratios of fatigvie to tensile properties , and their S-N
curves show fttigue limits . Polycrystals of aluminium
and alumlnlun^ magnesium show hardening behaviour
after fatigue. Evidence is advanced for supposing that
the lowest strfss for fatigue failure in aluminium and
aluminium- magnesium alloys may be correlated with
the stress for Ibeglnning of cross-slip. Zinc single
crystals taive been fatigued at -196°. -78° and ■»-200C,
In push-pull tests at 100 c/s . Stresses d the order of
one hundred times the flow stress of a virgin crystal
can be reached. These results suggest that point de-
fects cootribuae to the tiardening . (Author)
I
Crucible Ste4l Co. of America, Midland. Pa.
INVESTIGATION TO DEVELOT OPTIMUM PROP-
ERTIES IN FORGED Ti-7Al-4Mo. by James E.
Hamer. Rept. for Feb 58 -June 60 on Metallic Mate-
rials, Contract AF 33(616)6122. Oct 60, 145p. 8 refs.
WADD Tecfani^ rept. 60-489.
Order frxjm OTS %2. 75 PB 171 546
The influence of six processing sequences on the
oiicroatnictur^, mechanical properties, and heat
treatment response of the Ti-7Al-4Mo alloy has been
studied Forging entirely above the beta tranaua pro-
duced a Widman-stanen type of structm-e. The creep
resistance of this structure was excellent; however,
\
heat treatment response and tensile ductility were
poor. Forging entirely below the beta transus de-
veloped an equiaxed microstnicture and generally
good properties except for reduced creep resistance.
Duplex forging. 1. e. , forging initially above the beta
tranaua, cooling to room temperature, and reheating
to below the beta transus for finish forging, produced
a nearly equiaxed microstnicture and general prop-
erty levels quite similar to all below -beta forging
but with improved creep reaiatance. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
DESIGN PROPERTIES AS AFFECTED BY CRYO-
GENIC TEMPERATURES (TI-6A1-4V, AISl 4340,
AND 7079 -T6 ALLOYS), by W. P. Achbach and
R. J. Favor. Rept. on Cootraas AF 33(616)6410 and
AF 33(616)7747. 24 Jan 61, 19p. 5 refs. DMIC
memo. 81.
Order from OTS $0. 50 PB 161 231
Defense Meuls Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
THE EVOLUTION OF NICKEL-BASE PRECnTTA-
TION- HA REINING SUPERALLOYS, byJ.G. Hoag.
[Rept. on Contract AF 33(616)7747). 6 Feb 61, Up.
18 refs. DMIC memo. 84.
Order from OTS $0.50 PB 161 234
Defense Metals Information Center. Battelle
Memorial Inst. , Columbus, Ohio.
PICKUNG AND DESCALING OF HIGH-STRENGTH
HIGH -TEMPERATURE METALS AND ALLOYS, bjr
J. A. GurklisandL. D. McGraw. (Rept. on Contraa
AF 33(616)7747). 8 Feb 61, 17p. 28 refa. DMIC
memo. 85.
Order from OTS $0, 50 PB 161 23S
The purpose of this memorandum ia to bring togettav
a partial selection of chemical and electrochemical
descaling and pickling procedures that have been em-
ployed on the high -strength, high-temperature metait
and alloys.
Defense Metals Information Center. Battelle Me-
morial Inst. , Columbus, Ohio.
REVIEW OF DEVELOPMENTS IN IRONALUMINUU-
BASE ALLOYS* by J. W. Holladay, [Rept. on Con-
tract AF 33(616)7747]. 30 Jan 61, 61p. 99 refs. DliC
memo. 82.
Order from OTS |0. 50 PB 161 232
The iron-aluminum aUoys are of interest as an akv-
native to titanium. The present memorandum rerisH
the current developments In the iron-aluminum alloj^
and Includes the essential data from two previous
memorandums.
Lincoln Lab. , Mass. Inst, of Tech. , Lexington.
ANNEALING OF OBLIQUE -INCIDENCE PERMAL-
LOY FILMS, by G. P. Weiss and D. O. Smith. Re^
on Contract AF 19(604)7400. [i960) 9p. 3 refs.
53G-0O46; AD-248 363.
Order from LC mi$l. 80. ph$l. 80 PB 153 701
610
The anisotropy of evaporated Permalloy films (com-
position near zero magnetostriction) deposited on
(lass at 45° to the substrate normal and at a sub-
itiate temperature of 2[XPC has been studied after
tmeal for several hours at 300PC. After anneal the
room temperature easy-axis of "films with positive
magnetostriction is in the original direction. How-
e»er, films with negative magnetostriction develop a
new room temperature easy -axis 90° to the original
one; at 300°C the easy-axis is in the original direc-
don. Application of a large magnetic field in any
diiection during anneal does not influence the final
inagDetic anisotropy in either case. These effects
ue qualitatively explained by assuming the anneal to
increase the tension along the long -axis of oblique -
incidence chains, a process which converts surface
energy into strain energy. Anisotropy was measured
by resonance in a coaxial bridge over the frequency
m^ 50 Mc to 2100 Mc. A recungular coaxial cav-
ity is used which can be heated to 500^C in a vacuum
cf 10'^ mm Hg; continuous angular orientation of the
Him is possible with a resolution of 1 0. 5°. Bridge
balance is good enough to permit samples of less
ctan 100 A thickness to be measured. (Author)
National Research Labs. , Ottawa (Canada).
ON THE FURNACE REQUIREMENTS FOR T«E
MECHANICAL TESTING OF MATERLVLS AT ELE-
VATED TEMPERATURE, by J. A. Dunsby. Nov 60,
3Sp. 22 refs. Mechanical engineering rept. MS- 103.
Order from LC mi$3.00, pb$6.30 PB 154 340
A review is made of the sensitivity to temperature
change of the results of tensile, creep, stress rupture
and fatigue tests on typical enj^eering meuls. The
temperature sensitivity is then used as the basis for
in examination of the temperature tolerances specified
by the existing standard codes for elevated tempera-
ture testing. Guidance is also given for tolerances for
devated temperature fatigue testing, for which ix>
standard codes exist at present. The rate at which. a
ipecimen is brought to test temperature is shown to
be of some importance and is a design parameter not
covered by the standard codes. Suggestions are made
tar suitable heating rates. (Author)
Naval Weapons Plant, Washington. D. C.
FRACTURE TOUGHNESS OF HIOl STRENGTH
WEBT metals; by Harold Bernstein and George C.
Young. Progress rept. no. 2. 28 Jan 60, 26p. 3 reft.
NAVORD rept. 6496 (Part 2); NWPW-T-35-59;
AD- 233 380
Order fromLC mi$2.40. phHBO PB 153 928-2
lUs report released for sale to the public 15 Mar 61.
Praaure toughness results on several high strength
itieet steels are presented. Crack extension force (Gc)
values now include a plastic zone correction. The data
cover the effects of heat treatment, section size, and
directionality. On the basis of the toughness data
•kjoe, the low alloy and high iilicon steels show prom-
ise of reaching the higher strength regions. There was
■0 iixlication of temper brittienes s in any of the mate-
rials examined. AMS 6434 showed a prtxiounced size
effect on fracture toughness. The fracture toughness
t«t is more sensitive to temperature than the Charpy
impact test. Fracture appearance is not necessarily
a valid measure of toughness. (Author) (See also
PB 153 928-1)
Naval We^wns Plant, Washington. Di C.
FRACTURE TOUCHINESS TESTS OF HIGH
STRENGTH SIEET METALS, by Harold Bernstein
and George C Young. Progress rept. 18 May 59,
2^. 3 rett. NAVORD rept. 6496; NGF T-7-59;
AD-219 361.
Order from LC mi$2.70, ph$4.B0 PB 153 928-1
This report released for sale to the public 15 Mar 61.
The Blgnificaixre of the fracture toug^ess test and ,
the iKXch variable are briefly discussed. Toughness
data for numerous high strength sheet steels and one
titanium alloy are presented. Tlie data cover the
effects of heat treatment, section size, welding, aixl
surface finish. (Author)
Ferrous Metals
Armour Research Foundation. Chicago. III.
IMPROVEMENT OF MECHANICAL PROPERTIES OF
STEEL CASTINGS BY PRESS FORGING, by
T. Watmough. J. T. Berry, and P. R. Gouwens.
Final technical engineering rept. for 24 Jan 58-
29 Feb 60 on Contract AF 33(600)36387. Sep 60,
116p. 31 refs. AMC Technical rept. 60-7-637.
Order from OTS $2. 50 PB 171 524
Steel castings for high performsnce aircraft and
missiles are markedly improved in strength by the
application oi a press forging operation accomplished
under controlled conditions of temperature and defor-
mation. The most suitable alloys for the technique
are low-carbon, high-alloy types of steel where the
martensite can susuin deformation. The casting
alloys of this type investigated were AMS 5363A (an
18-8 stainless), and 17-4 PH suihless steels. In the
former, strength increases of 400-600t in yield
strength and 200- 250% in UTS were obtained by press
forging at -lOOOP with 40% deformation, followed by
tempering at 650OF. In the case of the 17-4 PH steel
increases in both yield and UTS of approximately 10%
were obtained by deforming the predominantly
martensitic structure 10% at room temperature fol-
lowed by aging at 860<^. SAE 4340 is responsive to
strei^hening by warm working, prior to transforma-
tion and at the 240,000 pel strength level; the yield
point can be increased by 15 per cent and the UTS by
10 per cent. The composition of 4340 is not entirely
suited to these techniques. Utilization of the process
with the low-carbon, high-alloy steels is feasible bitt
not without certain difficulties. These involve the
design of closed dies erf adequate strength to press
forge at the lower temperatures. Selective press
forging of critical areas in castings by semi-open
die techniques, is perfectly feasible.
611
Defense Metals Information Center. BttteUe
Memorial Inst. , Columbus, Ohio.
HIGH -CTRENCTH- STEEL FORCINGS, by H. J. Henn-
ing and P W. Boulger. Rept. on Contract
AF 33(616)774(7. 5 Jan 61, 64p. 9 refa. OMIC
rept. 143.
Order from QTS) 1.75 PB ISI 102
This report lai mainly coacerned with forgings made
from martensttic steels heat treated to strengths
ranging from 240, 000 to 300, 000 psi. Forging char-
acteristics, design limitations, dimensional toler-
ances, and quality -control problems are discussed.
A considerablf amount of data on mechanical proper-
ties is also presented. In addition, the report sum-
marizes the available Information on forged, semi-
austetiitic steals. This compilation is based on pub-
lished articles, Government reports, and interviews
with producerl and users of steel forgings. (Auttior)
Engineering blv. , Air Materiel Command, Wright -
Patterson AI%, Ohio.
FATIGUE LIMIT OP CHROMIUM PLATED STEEL,
by Louis Mehr. T. T Oberg and J. Teres. 26 July 44,
83p. AP Tech^cal rept. 51 2S: ATI-29 321.
Order from L<: mlf4. 80, ph$13. 80 FB 154 759
This report released for sale to the public 16 Mar 61.
The purpose at this Investigation was two-fold: (a) A
systematic study and evaluation of the effect of the
possible variables on the fatigue limit, (b) The de-
velopment of a process which would have such a low
fatigue loss th>c the necessity for testing ol each plated
part could be dispensed with. This latter objective
was not completely realized but several desirable con-
ditions were established.
Franklin Insti , Philadelphia, Pa.
EFFECT OF SINGLE TRACE ALLOY ADDITIONS
ON THE PROICRTIES OF PURE IRON, by G. Londoq
J. L. Rutherfctd and others. Rept. for 15 Mar 57-
30 June 60 on Ititer actions. Imperfections and Alloy
Theory, Contrsa AF 33<6l6)5059. Dec 60, 72p.
11 refs. ARL Technical rept. 60-295.
Order from CTSS $2. 00 PB 171 045
I
This study cov^s the introduction at single trace
alloy additions (zero to 0. 1 per cent) into zone purl-
fled iron. The elements studied were phosphorus,
sulfur, cobalt, chromium snd nickel. Radio-active
tracer techniqiies were utlUzed as a tool to determine
relative alloy doncentratlon . Purification of the Iron
was accomplisked in 3/16 Inch diameter and 1 inch
diameter bars by a vertlcle floating zone technique
using 10 zone passes to accomplish Initial purifica-
tion. In the coacentration levels studied the specific
alloys had the saual grain refining effects on recrys-
tallization; however, even in the zone purified and un-
alloyed material, recrystallization was influenced by
the residual impurities. Alloy effects on mechanical
properties were slight except for low temperature
embrittlement and room temperature strengthening
due to phosphorus. The yield strength temperature
relationship fo4 these high purity iron differ from that
of ingot iron ar{ mild steel in tha\ the majority of the
data shows a linear relationship rather than hyper-
bolic. Only the high phosphorus material tested loitt-
cated the hyperbolic type curve usually attributed to
Iron. (Author) ■
Indiana Steel and Wire Co. , Inc . , Muncie .
INDUSTRIAL PREPAREDNESS STUDY ON NON-
NiaCBL BEARING ALLOY BRAID WIRE, byAlvinW.
Holmes and Paul R. Judy. Final rept. for 24 June 57-
31 July 58 on Contract DA 36-039- 8C-75929. [1958] 2^
AD- 201 450.
Order from LCml$2. 70, ph$4. 80 FB 154 419
Fourteen bundles (2,400 lbs .) of cleaned 1/4" Special
Alloy Steel were received from Allegheny -Ludlum
Steel Corporation . One coll was as hot rolled the
others annealed prior to cleaning . Several stringer
tests established processing for this material to veiy
much like Type 302 except cleaning must be carefully
watched to avoid excessive steel losses and final stock
size needed to be smaller because this "Special AUof
work hardens at a greater rate than average Type 303,
both of which increase overall processing costs . Piatl
stock size was determined to be .040" nominal as cos-
ductive to best finished wire by our practices . The
drawing, testing and packing of approximately
2,000 lbs. of .015" wire was completed. The wire
meets the specification requirements almost 100%, dk
only discrepancy being six torsion tests (out of seven
hundred performed) which ranged 13 to 14.5 in one
inch length versus 15 iTilnlmum specified. Wire pro-
duced would be considered brittle (compared to Type
302); while samples of all the wire produced would
wrap on one wire diameter, most of it would break oi
sharp kink test. There were no unusual difficulties K
any stage in the processing of this wire. (Author)
Light M«tali
Armour Research Foundation, Chicago, 111.
INVESTIGATION OF HEAT TREATMENT AND
WELDING CHARACTERISTICS OF 8 120 VGA
TITANIUM ALLOY SHEET, by John F. Rudy. Frank
A.Crossley, and Harry Schwartzbart. Final rept. for
28 Nov 58-28 July 60 on Contract NOa(s) 59-6054c.
[1960] 124p. ARF 2164-12.
Order from LC ml$6. 30, ph$l9.80 PB 153 56B
Aglnaexperlments were carried out between 700 sal
1000°F for durations of 2 to 400 hours. Both cold
rolling, as a pre-age treatment, and duplex aging
showed important advantages in tensile properties
over the commercially popular solution -treat -and-afe
sequence. Duplex aging cycles gave more promislof
weld metal properties than did Isothermal aging.
Magnetic stirring, a weld deposition technique in-
tended to refine the weld metal grains and to increast
weld metal homogeneity, showed improved tensile
properties in duplex-aged weldments. The aging be-
havior at the alloy after the various pre-age thermal
and mechanical treatments, and as a function of the
aging cycle per se, is discussed in terms of tensile
[jropertles, hardness, mlcroatructure. and published
TTT diagrams for the subject slloy. (Author)
612
l»ckheed Aircraft Corp. , Sunnyvale, Calif.
VACUUM MELTING OF BERYLUUM BY ELEC-
TRON BOMBARDMENT, by H. T. Sumsion and
C. 0. Matthews. Technical rept. on Contract NOrd
17017. Dec 59, 41p. 5 refs. LMDS-480485:
AD- 232 993.
Order from OTSI 1.25 PB 171 521
A process is described for melting and cilsting beryl-
lium ingots by electron bombardment, in order to
produce a beryllium or beryllium -alloy ingot for
(abrication into plate. Results are furnished of visual
iaspections, metallographic examinations, chemical
and X-ray diffraction analyses, and machinabiUty,
hardness, tensile strength, and bend tests. The
ideas of vsrisbles in both the melt stock and the
processes are reported. It is concluded that smooth,
homogeneous Ingots three inches in diameter and
essentially free of casting defects can be produced by
the process described. Vaporization loss during
melting is not prohibitive for successful production.
Ingots produced show improved cast structure and
better machinabiUty than Induction- melted, vacuum -
cast material. Oxide content is reduced but no signi-
ficant increase in ultimate tensile strength, or de-
CTMse In metallic impurities, was obtained. A
method at analysis by gamma -activation was devel-
oped and proved effective for determinations at
oxygen and carbon. (Author)
Pitman -Dunn Labs. Groiq), Prankford Arsenal,
Philadelphia, Pa.
A NEW TYPE OF UGHTWElOfr CELLULAR MA-
TERIAL, by L. Polonsky and S. Lips on. Apr 60,
66p. 3 refs. Rept. no. R-1534; AD- 242 924.
Order from OTS ♦L75 PB 161 770
A process for the production at cellular metals is de-
scribed. The process consists at preparing a refrac-
tory mold, filling the nK>ld with soluble granules
which correspond to the size and shape of the pores
desired in the metal, and infiltrating the molten
metal into this soluble aggregate. After leaching with
a suitable solvent, the metal has a void structure of
Itterconnectlng cells which correspond to the shape
and size of the soluble aggregate. The apparent den-
sity of the metal body can be ccntrolled from a maxi-
mum of approximately one-third of its base density
CO some lower density in the order of cne-flfth the
base density. In addition to process development,
which includes catting of shapes as well as billets, a
limited investigation cf the mechanical and ttiersi?)
chsracterlstics of aluminum-base cellular metal was
nede. Potential applications for materials of this
type are suggested. (Author)
Nonferrous (except light) Metals
Carnegie Inst, of Tech., Pittsburgh, Pa.
TEMPERATURE DEPENDENCE OF INTERNAL
PRICnON OF MAGNESIUM, COPPER. AND ALUMI-
NUM SINGLE CRYSTALS, by John T. Plttenger.
Docwrsl thesis. Technicsl rept. on Contrsct N6arl47,
T.O. 1. 10 Aug 51, lOBp. 30 refs. ATI-173 115.
Order from LC mi$5.70, ph^l6.80 PB 154 867
This report released for sale to the public 17 Mar 61 .
Apparatus for determining the temperature dependence
of internal friction in the kilocycle range of frequen-
cies is described. The measure of internal friction is
the logarithmic decrement. The apparatus was used
to determine the temperature dependence of the inter-
nal friction of single crystals of 99. % per cent pure
magnesium, 99. 999 per ce« pure copper, and 99.99
per cent pure aluminum. The decrement of copper
showed a minimum near 215%. A broad minimum
occurred in the decrement of noagneslum near 60*^^.
When the temperature of magnesium was changed
below lOO^C, the decrement increased. The decre-
ment then decressed to s steady value at the new tem-
perature. The decrease has been named aging. The
aging process appeared to have an activation energy
of about 7000 cal. /mole. These results permit defini-
tion of a critical temperature for each of the two
metals. Above the critical temperature the decre-
ment increased rspidly as the metal was heated.
Below the critical temperature the decrement may be
increased by small mechanical Influences or by strain
accompanying cooling. (Author)
Defense Metals Information Center, Battelle
Memorial Inst . . Columbus . OUo.
PHYSICAL AND MECHANICAL PROPERTIES OP
OOMMERQAL MOLYBDENUM-BASE ALLOYS, by
J. A. Houck. Rept. on Contract AF 18(600)1375.
30 Nov 60, 182p. 63 refs . DMIC rept. 140.
Order from OTS $3.00 PB 151 099
A compilation of the more important physical and
mechanical pn^wrties of nwlybdenum and commercial
molybdenum-base alloys is presented. Included among
theaUoys are: Mo-0.5Ti. Mo-0.5Zr, Mo-0.5Ti-
O.OSZr (TZM), Mo-0.05Zr. Mo-30W, Mo- SOW. and
Mo-1.25Tl-0.5Zr-0.15C(TZC). (Author)
Unlversal-Cyclope Steel Corp. , Brldgevllle, Pa.
MELTING, FABRICATION AND TESTING CX*
CHROMIUM BASE ALLOYS, by N. R. Harpater.
Final rept. on Contraa NObs -72042. 27 Jan 60, 38p.
4 refs.
Order from LC mi$3. 00. pll»6. 30 FB 153 592
This report released for sale to the puUic 15 Mar 61.
This report summarizes melting snd fabrication ex-
perience on chromium-base alloys containing nickel
and/or iron aa second major elentents. SmsU ingots
from all compositions, except 100% chromium, could
be forged to bar. Fabrication of wrought produa from
pnrodualon size ^ts was accomplished only with the
505t chromium - 50% nickel alloy. Limited property
tests showed the 50% chromium - 50% nickel compo-
sition had low stress -rupture strength at 1800°F and
2000°F, poor impjaa strength at room temf>erature,
limited bend formabillty and poor welding charaaer-
Istlcs. Tests conducted at the Bureau of Ships on the
50% chromium - 50% nickel and 60% chromium - 40%
Iron alloys showe^hat both had corrosion and oxida-
tion resistance superior to Type 310 stainless.
'■«
613
Structur<il Metallurgy and Corrosion
Carnegie Insu of Tech. , Plnsburgh. Au
SELF DIFFUSION IN THE IRON-CHROMIUM SYS-
TEM, by H. W. Paxton and T. Kunitake. Technical
repc. oo CoDtra^ Noor- 760(08). 1 Mar 60, 31p.
26 rets. AD-23# 184.
Order from UZ mi$3.00, ph|6.30 PB 153 742
The self diffuslcn coefficients at chromium and iron
in Che Fe-Cr system have been measured or collected
from published work. The variation of Dcr with
composition at |275°C is the largest yet obaerved in
an alloy system - ct order IC* difference in rates be-
tween pure chrpnuum and a 30 Cr - 70 Fe alloy. The
▼ariation d Dp^ is much less at this temperature
(about a factor pf 10 difference in rates over the same
compos iiicD raQge). The values ol Dq and Q for both
Iron and chromium self-diffusior show large variations
with compos itlcai. The eflect ci< compositicn is rather
complex, but isi essentially of the same form for both
elements. The currently accepted theories on the
vacancy mechaaism al diffusion provide no obvious
esplanatlon of tie results. The ccncefits at ring diffu-
sion and correlttion require more detailed theoretical
work before proper ccmparisoo can be made. Experi-
ments to shed light on diffusloo mechanisms In the
b. c. c. transition elements whicli are d very consid-
erable present and future technological importance
seem most desirable. (Author)
i
Defense Metals Information Center. Battelle
Memorial Inst , Columbus, Ohio.
PHYSICAL AND MECHANICAL PROPERTIES OF
TUNGSTEN A>ID TUNGSTEN- BASE ALLOYS, by
V. a Birth. Piept. oo Contract AF 18(600)1375.
15 Mar 60, 67p. 58 refs. DMIC rept. 127; AD- 236095.
Order from OTg $1. 75 PB 151 084
I
The mechanical and physical properties d tungsten
and tungsten-boise allays are reviewed and siaxuna-
rized. In an apt>rai8al at mechanical properties, the
effects of the ductile- brittle transition and of recrys-
tallization muse usually be taken into account.
Tensile properties of tungsten up to the melting point
have been measured. A considerable amount of work
in the field of tungsten-base alloys remains to be done.
Riysical properties erf tungsten have been fairly well
esublished as the result of developments in the lamp
and electron tufce industries. The relatively poor-
temperature oxidation resistance of tungsten may pre-
sent a problem in elevated-temperature environments.
(Author)
Metals and Caramics Lab. , Wright Air Development
Dlv. , Wright -Panerson AFB, Ohio.
APPUCABIUTY OF PRESENT CREEP PREDICTION
TECH>nQUES FOR EXTRAPOLATING VERY LONG
TIME CREEP BEHAVIOR, by K. D. Shimmln. Rept.
fOT Feb- July 60 on Metallic MaterUla. Oct 60, 21p.
16 refa. WADD Technical rept. 60-523.
Order from 01$ $0. 75 PB 171 487
A number of m<thoda of correlation and extrapolation
of creep and stiness- rupture data are reviewed and
discussed briefW. It is shown chat, of the time-tem-
perature parameter correlation methods, the Manscn-
Haferd parameter method has been most successful in
correlating existing data. Of the empirical methods
of extrapolation, the graphical method of Grant and
Bucklin, and the statistical approach reported by
Clauss are shown to hold promise as a means of pre-
dicting long-time creep data. Recommendations are
given for an experimem to provide verification and
evaluation of the methods of extrapolation of long- >
time data. (Author)
Metals and Ceramics Lab. , Wright Air Developmea
Div., Wright -Patterson AFB, Ohio.
STUDY OF RATE CONTROLLED PROCESS FOR
COMPRESSIVE DEFORMATION OF HIGH PURITY
ALUMINUM, by A. E. Rlesen. Rept. for July 58-
July 60 on Metallic Materials . Sep 60, 27p. 7 refs.
W ADD Technical rept. 60-542.
Order from OTS $0.75 P* 171 488
A unique testing technique for determining the rate-
controlling process for compressive deformation of
high purity aluminum over the temperature range of
297OK is discussed, and an attempt is made to corre-
late the activation energy for compression with some
recognized rate-controlling process for tensile defor-
mation of aluminum. It is shown that the compressive
activation energy obtained, 5,400 cal/mol. , cannot be
related to any known tensile deformation process . The
results of this study indicate a need for further experi-
mental investigations to define the compression activa-
tion energy spectrum for aluminum over a broad tem-
perature range. (Author)
Minnesota U. , Minneapolis.
THE EFFECT OF STRESS MAGNITUDE AND
STRESS HISTORY ON THE DAMPING, BLASTlCnY
AND FATIGUE PROPERTIES OF METALLIC MA-
TERIALS, by L. J. Demer and B. J. Lazan. Rept. on
Contract N8-ONR-66207. Sep 53. 64p. 53 refs.
AD- 26 069.
Order from LC ml$3. 90. ph$10. 80 PB 154 818
This report released for sale to the public 17 Mar 61.
Unnotched cylindrical test specimens of gray cast im
Sandvik steel. N-155 alloy. 24S-T4 Al aUoy, J-1 M|
alloy, and SAB 1020 steel were tested in the rotating
beam damping, elasticity, and fatigue machines. Tht
results of vibration decay tests indicate that the spe-
cific damping energy (D) increases as a power functlos
of the 8tre88(S): D - JS". where J and n are constants
depending on the material. The damping energy abovs
the cyclic stress sensitivity limit (CSSL) was depend-
ent on the stress history, but stress history had no
observable effect on damping below the CSSL. Valuss
obtained for n below the CSSL varied between 2. 0 aad
2. 6. Above the CSSL, the rate of change of damping
with stress Increased. The ratio of stress at the CSS-
to fatigue strength varied from apprbximately 0. 5 for
the Mg alloy to 1. 1 for the Sandvik steel in the quenched
and tempered condition. Data are given on the relative
damping properties. With the exception of gray ina,
none of the nutterials exhibited an average dynamic
modulus of elasticity lower than 95% of the static mod-
ulus at the respective fatigue strengths. A compariscs
of the relative damping properties for equal stress be-
low the CSSL indicates that the damping energy de-
614
creases with an increase in the fatigue and tensile
•trei«ths of the materials. On the basis of equal ratio
of stress to fatigue strength, the daniping energies
iliowed an increase with both fatigue and tensile
gtm^^. A review of prior work is given.
Naval Civil Engineering Lab. , Port Hueneme. Calif.
CORROSION SURVEY OF STEEL SHEET PILING, by
C. V Brouillette and A. E. Hanna. Final rept.
27Dec60. 66p. 21 refs. Technical rept. R-097.
Order from OTS $1.75 PB 171 501
A st^y w*B made of the corrosion of steel sheet piling
in marine environments In order to improve the design
tnd construction of future insuUatlons and to predict
the Ufe of existing structures. The effectiveness of
calhodic protection was investigated. (Author)
Naval Ei^neerlng Experiment Station. Annapolis,
Md.
INVESTIGATION OF THE MECHANICAL PROPER-
TIES AND SEA WATER CORROSION CHARACTER-
iSnCS OF NODULAR (DUCTILE) CAST IRON, by
14. R. Gross. [1952] 33p. 12 refs. E.E.S. rept.
4E(E1)101717.
Order from LCml$3. 00, ph$6. 30 PB 154 809
This report released for sale to the public 16 Mar 61.
Based on the tenaile property measurements and the
shock tests described herein, it is concluded that
fully annealed nodular iron is a suitable material for
shipboard applications. Unfortunately, the low notch
impact resistance of the material tested Imposes an
element of doubt as to the validity of this conclusion.
In so far as the tensile tests are concerned, there is
• significant variation in ductility between the outside
and center of large annealed coupons and among vari -
ous locations in the engine frame. The shock reslst-
•nce of the engine frame tends to lessen the impor-
tance of this variation, however.
Westlnghouse Elearic Corp. , Bloomfleld, N. J.
DIFFUSION OF COBALT IN M0LYBC«:NUM, by
E. S. Byron and V. F. LanrUjert. Rept. on Contract
NCh-d 10276. Jan 53, 25p. 7 refs. NAVORD rept.
no. 3072.
Order from LC ml$2.70. ph$4.80 PB 154 542
This report released for sale to the public 2 Mar 61.
The diffusion coefficients for cobalt In molybdenum
•ere determined at 900, 1100, 1275, 1500 and 1700<*C
In the equation re latltig diffusion coefficient with tem-
perature, D - Ae^/*^, the activation energy Q de-
rived was 34, 800 calories per niol, and the constant
A was determined as 2. 82 x lO'^crnvsec. (Author)
Westlnghouse Research Labs . , Pittsburgh, Pa.
THE QUAUTATIVE MECHANISM OF STRESS COR-
KXLOti CRACKING OF AUSTENITlC STAINLESS
STEELS, byD. van Rooyen. Technical rept. no. 1 on
Stress Corrosion Cracking, Contract Nonr- 2868(00).
10 Nov 59, 52p. 20 refs . AD- 236 225
Order from LC ml$3. 60, ph$9. 30 PB 150 502
Results support the electrochemical mechanism of
stress corrosiCHi crack initiation in austenitic stain-
less steel: after a period of initiation, during which
partial passivation occurs , local anodes corrode along
cenain narrow planes , resulting in cracking and ulti-
mate failure. Crack lengths gradually Increase with
time, after the onset of stress corrosion crack propa-
gation, and no cracking occurs during the initiation
suge. The cracks extend slowly through austenitic
stainless steels and a mg-base alloy, without any
steps of instanwneous advance. Crack propagation In
mild steel, placed in hot nitrate solutions, takes place
In alternating steps of rapid and slow penetration. The
rapid steps are not instanuneous . The stress cor-
rosion cracking of AI-4% Cu and Al-7% Mg alloys , In
Na Cl-Na HOO3 bicarbonate solutions , consists of al-
ternating stages of electro-chemical corrosion and
sudden physical failure. Study methods used Include
the automatic recording of electrochemical potential
change and extension of specimens , and the acoustic
recording of sound generated during cracking. Sam-
ples were tested as wires or strips; stressed in di-
rect tension, or as U-bends or arc-bends . (Author)
NUCLEAR PHYSICS AND
NUCLEAR CHEMISTRY
Bartol Research Foundation, Franklin Inst.,
Swarthmore, Pa.
ANNUAL REPORT NO. 7, by W. F. G. Swann and
C. B. Mandeville. Rept. for 1 Oct 56-30 Sep 57 on
Contract N6ori- 144(01). 30Sep57, 58p. 100 refs.
Order from LCml$3. 60, ph$9. 30 FB ISO 696
Resonance fluorescence studies; Nuclear resonance
fluorescence in A$75; The radiations of two Odd -A
isotopes of osmium; The radiations of Os^°5. -j-h^
radiations of Co^S; The nature of the photosensitivity
of Geiger counters; Cosmic Rays: balloon flights ,
shipboard neutron monitor, Thule neutron nxmitor.
satellite, emulsion studies, Theoretical Studies.
Included in the report are:
Lifetimes of the 6.91 - and 7.12-mev excited sutes of
0^^ pub. in The Physical Review 108:982-988.
ISNoRT 57
Acceleration of particles to cosmic ray energies by
electromagnetic induction, pub. In Jnl. of the Frauk-
(Nuclear Physics --and Nuclear Cbentlstry,
linlnst. 264:287-299, Oct 57
Search for a long-lived radioisotope of neodymium,
pub. in Jnl. of the Franklin Inst. 263:553-556,
June 57
Radiations from W ^ 85 and W 187, pub. in The Physical
Review 106:785-790, 15 May 57
Gamma rays of As 77 , pub . in Jnl . of the Franklin
Inst. 263:351-354, Apr 57
Sea-going cosmic-ray observatory, pub. in Jnl. of the
Franklin Inst. 263:153-159, Fe* 57
Nuclear energy levels of Osl88, pub. in The Physical
Review 104:722-727, 1 Nov 56.
615
Michigan U. Research Inat. , Ann Aiimr.
(X>a^C RAY INVESTIGATIONS. Annual progreaa
rept. on Contract Nonr-l224< 07). 31 K4ay 60. 8p.
AD- 238 168.
Order from LC|ml$l. 80. ph^l. 80 FB 148 215
Contents: '
Air shower experiment
Ionization chamber array
Cloud chamber
MIT 60-in. cltMd chamber
Direct pair production by muons underground
Eifm«ntary Particles
T
California U i Berkeley.
SOME EFFECTS OF HOLE-HOLE INTERACTIONS
IN SYSTEMS OF FERMIONS, by J Sawlckl. Rept. on
Contraa AF 49(638)327. [I960) I7p. 11 refs. AFOSR
TN-60-893; AD^243 994.
Order from LC;mi$2. 40, ph$3. 30 FB 153 032
A generalized reaction matrix o* the Bruecimer theory
is discussed inToMng the effects at hole -hole Inter-
actions in large systems of fermlons. Corrections to
the real part erf the single particle excitation energy
are estimated fbr the cases at nuclear matter and
bquld He3. The problem of the damping factor (I.e.,
the imaginary energy ahift) is discussed. (Author)
High-Energy fhysica Lab. , Stanford U. . Calif.
EXPERIMENTAL STUDY OT THE MAGNETIC
STRUCTURE Cfi' THE NEUTRON, by J. I. Friedman.
H. W. KendaU, and P. A. M.Gram. III. Rept. on Con-
tract N6onr-2S^(l6). 25 May 60. 28p. 30 refs.
HEPL-199. 1
Order from LCImi$2.70. ph$4.80 PB 148 155
A measuremenc at the ratio at the nugnetlc form
factor at the net<ron to that at the proton has been
carried out by Comparing large- and small-angle elas-
tic electron-de«teron scattering at constant four-
momentum traiWera. The experimental result for the
average value of the ratio in the range of momentum
transfers from 1.6 f-1 to 2.25 f-1 is Fin/Fp =
(0. 91 1 0. 05) 1 0. 07: the first error is a standard
deviation from experimental uncertainties, and the
second from thacretlcal uncertainties in the analysis.
Measurements at the ratio of the nucleon isotopic
scalar form factors have also been obtained from this
experiment. The average value erf F2®/Fi* for the
same range at momentum transfers has been found to
be ( +0. 06 1 0. 09)1 0. 13. The small-angle scanerlng
data have been ts«d to determine the charge form
faaor at the devteron in the range at momentum
transfers from 0. 98 f * ^o 2. 8 f ' ^ The results are
consistent with B repulsive -core model at the
deuteron. (AutHor)
Illinois U. , U^na
BEAM ANALYZER MAGNET. PART I. by Van
Bluemel and Saif imay Chacterjee. Technical rept.
no. 17 on Contract Nonr-1834<(B). 11 May 60. 48p.
4 refs. AD-240 891.
Order from LC mi$3. 30. ph$7. 80 PB 149 315
The design and operation of the magnet used to ana-
lyze the energy oif the particles accelerated by a
spiral ridge cyclotron are described. The old 16-ln.*
diam cyclotron magnet is converted to a 3CP sector
magnet by adding two wedge shaped pole pieces. The
meth6d employed to design the extra pole pieces is
described. The pole pieces and the vacuum chamber
connecting the beam tubes are so designed that a
beam can be deflected to both sides of the central di-
rection of the beam by changing the direction of the
current flowing through the coils of the analyzer may
net. The magnetic fields on the beam entrance side
and the beam exit side of the magnet have been ex-
tensively measured for various values of magnetic
field at the center of the magnet. All data are pre-
sented. The automation control circuit used for
regulating the current in the mafpnet is also de-
scribed. (Author) ;
Institute at Theoretical Physics. - Stanford U. . Calll
PRODUCTION OF PARTICLE BEAMS AT VERY HIGH
ENERGIES, by S. D. Drell. Technical note no. 28 on
Contract AF 49(638)388. Axig 60. 13p. 8 refs. APOSR-
TN-60-1136; AD- 246 635.
Order from LC mi$Z 40, ph$3. 30 PB 153 188
The physical principle that a transition amplitude has •
pole for real one -particle intermediate states Is used
to study the photoproduction of secondary beams of
high energy strongrly-interacting particles. Photons
were found to be much more effective in initiating col-
limated beams of high energy charged plons. K mesoos,
etc. , than believed; this result is at Interest in pre-
dicting and comparing yields from electron linacs,
electron synchrotrons, and proton synchrotrons in tla
multi-Bev range.
Washington U. , St. Louis, Mo.
STUDY OF SYSTEM FOR PHOTOGRAPHY OF A
LIQUID HELIUM BUBBLE CHAMBER, by Pkul AikiD
Smith, Master's thesis. Technical rept. no. 6 on
Cosmic Rays, Contract Nonr- 816(09). May 60, 62p.
41 refs. AD- 240 073.
Order from LC ml$3. 90. ph$ia 80 PB 149 087
The theory, construction, and performance of a photo-
graphic system are described for use with a small
liquid helium bubble chamber at one liter capacity.
The contrast between bubble image and background fag
on the photographic film as a function of the size of the
bubble, and the ability to distinguish between adjacent
bubblea in the chamber are discussed. A theoretical
analysis at the angular dependence of the intensity d
light scattered by helium bubbles of radii from one
micron \jf> is given, making use of 4 different compu-
tational procedures appropriate to the various portloM
of the size range. The theory of image irtensity as A
function of (1) depth of field, (2) magnification, and
(3) lighting system design parameters Is developed for
the case of dark field photography of helium bubbles la
liquid helium. An analysis is given of the comparatHt
case of photographing (1) water drops falling through
Isopentane, and (2) helium bubbles in liquid helium.
Experimental results of photography of water drops
falling through Isopentane are given. Results show
that telium bubbles having radii smaller than 5vLWlU
be difficult to photograph, while those having radii
larger than 2G|[i,will be rather easy to photograph.
Instruments and Installations
»- J I
616
Controls for Radiation, Inc. . Cambridge, Mass.
DEVELOPMENT OF A TACTICAL GAMMA NEU-
TRON DOSIMETER, by I. A. Berstein, R. C. FU
sod others. Bi-monthly progress rept. no. 1, 1 July-
Si Aug 58. on Contract DA 18-108-406-cml-198.
1 Sep 58. 6p. AD-211 296.
Order from LC ml$l. 80. ph$l. 80 PB 154 428
lUta report released for sale to the public 8 Mar 6i.
Design of equipment for automatically filling and seal
ing E-5 dosimeter ampoules was investigated. Am-
poules were sealed using a Nichrome resistance loop;
however, the seal was not entirely satisfactory. In
addition, glo -bars, (silicon carbide heating elements)
were Investigated. The commercially available glo-
bars are too large for ampoule sealing application,
and It is thought that smaller designs would be too
costly. A promising combination of glo -bars with Pt-
Rb alloys is scheduled for testing.
Controls for Radiation, Inc., Cambridge, Masa.'M.r-.-
DEVELOPMENT OF A TACTICAL GAMMA NEU-
TRON DOSIXfETER, by I. A. Berstein, R. C Fix and
ctfaera. Bi-monthly progress rept. no. 2, 1 Sep-
31 Oct 58. on Contract DA 18-106-406-cml-198.
1 Nov 58, lOp. AD-211 297.
Order from LC ml$l . 80, ph$l .80 PB 154 429
This report released for sale to the public 8 Mar 61.
An 90% Pt - 20% Rh alloy was investigated for sealing
B-S dosimeter ampoules. Very favorable results were
oteained. A number of sealing units consisting at
Pt - Rh alloy imbedded in cement were constructed and
studied. It was concluded that with minor modlflca-
tlona automatic filling and sealing equipment can be
■aMmbled and put into use. The use at RF induction
heating was also investigated. Several ampoules were
successfully sealed by this method, and further in-
vestigation is proposed. (See also PB 154 428)
Controls for Radiation, Inc. , Cambiidge, Mass.
DEVELOPMENT OF A TACTICAL GAMMA NEU-
TRON DOSIMETER, by I. A. Berstein, R. C Fix
and others. Bi-monthly progress rept. no. 3, 1 Nov-
31 Dec 58, on Contract DA 18-108-405-cml-198.
5 Jan 59. I2p. AD -209 700.
Order from LC mi$2. 40, ph)3. 30 PB 154 430
llda report released for sale to the public 8 Mar 61.
Assembling and testing of the various components and
iMtruments used in the equipment for automatically
filling and sealing E-5 dosimeter ampoules were
■tudled. Brief descriptions affiled to each component
euch as the oxygen analyzer, atmosphere gas control
■nv^ratus, pH measurement device, and water and
tzichlorethylene purifiers are given. In addition,
plHaol red purification is described, aa well as water
deaeratlon, a sealing unit temperature measuring
•ystem, and the operator equipment and instrument
platform. (See also PB 154 429),
Naval Research Lab. . Washington. D. C.
DOSMBTRY BY LUMINESCENCE DEGRADATION IN
ORGANICS. by Frank H. Attix. Rept. for Dec 57-
Oct 59 cm The Chemistry and Physics of Materials ,
Contract AF MIPR (33-616)58-21. Oct 60, 66p.
25 refs . WADD Technical rept. 60-563.
Order from OTS $1.75 PB 171 491
This report covers an investigation of the phenomenon
of photolumlnescence degradation in organic materials
due to damage by ionizing radiations . A survey of pre-
vious studies of this effect is presented. The present
work stresses reduction to a practical dosimetry sys-
tem for die 5x10^ to 5x10^ rad absorbed dose range.
It is demonstrated that pressed wafers of anthracene
and of p-quaterphenyl can be employed together to
cover the required dose range. Ultraviolet lij^
(3650 angstrom) is used to excite the photolumlnes-
cence, which is observed in a narrow band at 4420
angstrom . Some recovery of photolumlnescence with
time after X-ray irradiations is observed, and heat
treatment Is proposed as a hietbod at reducing this ef-
fect . Degradation of luminescence in blphenyl , p-ter-
phenyl , fluorene , naphthalene , and tetracene have
also been studied and are reported upon. (Author)
Naval Research Lab., Washington, D. C.
A SOUD STATE BRAGG-GRAY CAVITY CHAMBER,
by Victor H. Rltz and Frank H. Actix. Rept. for
Mar 59-June 60 on The Chemistry and Physics at
Materials. Contract AF MIPR (33-616)59-27. Oct 60,
24p. 11 refs. WADD Technical rept. 60-562.
Order from OTS $0.75 PB 171 490
An attempt has been made to construct the solid state
analogue of a Bragg Gray cavity ionization chamber.
Thin layers of materials sensitive to radiation have
been placed between walls of C , Al , Cu , Sn or Fb .
Two types of sensing agents have been employed; thin
layers of anthracene whose ultraviolet Induced lumi-
nescence degrades upon irradiation, and 6 micron
thick polyethylene terephthalate (Mylar) films whose
optical density at 3250A increases upon irradiation.
Results in a Co"" •Y"'*y Add with the anthracene disa-
gree sharply with theory, while the Mylar film yields
excellent agreement (*5%) with theory. A preliminary
attenqx to discriminate between the fast neutron and
gamma ray dose in a nuclear reactor has been unsuc-
cessful. (Author)
Radiation Research Corp. , West Palm Beach, Pla.
DOSIMETER CHARGER (RADIOACTIVE), by
M. J. Cohen. Quarterly rept. for 1 Ais--30 June 53 on
Contraa NOb8r-63046. 2 July 53, 26p. 5 refs.
AD-22 410.
Order from LC mi$2.70. phM-80 PB 154 753
Tills report released for sale to the public 15 Mar 61 .
The Type D experimemal dosimeter charger was
selected as the basis for design of the ten develop-
mental models. The layout of this model has been
completed. Assembly of 10 units is about 40% com-
pleted. A report on "Power Supply Requirements for
.Neutron Counters" has been completed and is
included. (Author)
<l
617
Nuclear Reactions
High- Energy Physics Lab. , Suutford U. , Calif.
ELECTROPRODUCTION OF F10NS FROM HYDRO-
GEN AND DEUTERIUM, by Gerald G. Ohlsen. Rept.
on Contract N6ont-25116. 20 May 60. 34p. 14 refs.
HEPL-203
Order from LC m|i J3. 00. ph$6. 30 PB 148 154
The absolute cro4s section for direct production d
pioos in electron -proton and elactron-deuteron col-
lisiooshas been measured by the detection erf inelastic-
aHy scattered electrons. Proton dau has been taken
throughout the range of q^ s 2. 6 f ^ to q^ « 10. 75
f '^, and center ct mass energy E • 1100 Mev. to
E « 1300 Mev. pata analysis has been in terms al
neutron magnetic moment distribution. Comparison
with available thepry yields a neutron rms magnetic
moment of I f, but better theoretical calculations may
change this value somewhat. No theory for the
electroproduction at pions from deuterons exists at
present. The deu^erondau is presented in terms of
absolute cross sections as well as in terms of deuteron-
procon cross section ratio. (Author)
Physics Research Lab , U of Illinois, Urbana,
THE PHOTONEUTRON CROSS ACTION NEAR
THRESHOLD. bylP Axel and J. D. Fox (Doctoral
thesis). Technic4l rept . no. 13 on Contraa Nonr-
1834(05). Feb 60J 191p. 84 refa. AD- 233 889.
Order from LC nil$8.70, ph$30.30 PB 153 140
The experimental and theoretical atudy oi photo-
neutron cross sections near threshold is described.
Photonuclear meaeurements are used to determine
such nuclear proBerties as neutron binding energies,
spins and parities of nuclear energy levels, relative
widths of differeii decay modes of states formed by
photon absorption^ and electromagnetic transition
probabilities. Thp source erf the photons was the
x-ray beam from a betatron yielding a photon spec-
trum produced by^ electrons of different energy due to
multiple scattering. The theoretical prediaions are
evaluated for the photoneutron cross section in terms
of the following parameter s: (1) the photon absorption
mechanism and tJie fraaional strengths of the various
modes (predominately El, Ml. and E2, but possibly
higher modes); (2j) the energy dependence of the cross
section for each (|f these modes; (3) the spins and
parities of the initial, intermediate, and final sutes;
(4) particle binding energies; (5) competition param-
eters affecting th^ decay of the compound state, (in-
cluding gamma r^y. neutron, and proton partial
widths); and (6) tlfe energy dependence of the com-
petition parameters.
U., A.
Pittsburgh
DISTORTED WAVE METHOD FOR ELECTRON
CAPTURE FROM ATOMIC HYDROGEN, by R. H.
Basse] (DoCToral tfiesis) and E. Gerjuoy. Technical
rept. no. 12 on Capture -Loss and Ionization Cross -
Sections of Ions aiid Neutral Particles, Contract
Nonr- 624(06). A(^ 60, 30p. 30 refs. AD- 237 494
Order from LC iTi$2.70. ph$4.80 PB 147 543
The distorted- wave method, in which distorted waves
replace plane waves in the matrix elements for the
collision amplitude, is given a rigorous formulation
for arbitrary rearrangement collisions. In atomic
collisions Involving electron rearrangement, the for-
mulation enables removal of the unphysical internu-
clear Coulomb Interaction from the "perturbation"
Hamiltonian. The procedure is applied to the problem
of electron capture by protons in atomic hydrogen,
eliminating explicit dependence on the proton-proton
interaction. Numerical results of a first-order cal-
culation are In good agreement with experiments from
35 to 200 kev. Despite this agreement and the agree-
ment of previous calculations it is felt the charge-
transfer process is still not well understood. (Author)
Sarah Mellon Scaif e Radiation Lab. , U. at
Pittsburgh, Pa.
STUDIES OF THE ANNIHILATION OF POSITRCW
IN GASES» by Milton Heinberg and Lorne A. Rige.
Final rept. for 1 Dec 55-30 Nov 56 on Research and
Development on Study of Positrooium and Magnetic
Moment of the Electron, Contract DA 36-[06l]-ORD-
515. [1956] 69p. 16 refs. AD- 128 532.
Order from LC mi$3.90, ph$10.80 PB 154 817
This report released for sale to the public 17 Mar 61.
The study of the process of positron annihilation by
measurement of the angular correlation of the two
quanta from the annihilation event has been used
successfully in solids. No precision experiment on
the angular correlation of the two quanta from the
annihilation events ^n gases has been reported pre-
viously. In this work the distribution in angle is usu-
ally limited to within ten milllradians of 180O with
particular attention to the effect of a d. c. magnetic
•nd/or a d. c. electric field on the events within two
miliiradians cf ISO"^. The pressures used were from
one to 28 atmospheres. The experiments on the mag-
netic quenching gf orttio-positranium done previously
in various gases^'^ have been extended to higher
fields. The effects on the angular correlation and
magnetic field dependence of argon by adding ther-
mallzing and/or quenching gases has been studied.
Some evidence of the n < 2 states of positronium has
been found. (Author)
Washington U-, Seattle.
AN EXPERIJWDENTAL STUDY OF CLOSE COLLI-
SIONS OF HIGH ENERGY MU-MESONS WITH
ELECTRONS, by Robert Francis Deery. Doaoral
thesis. Technical rept. on Contract Nonr-477(l2).
Apr 60, lOOp. 32 refs. AD- 236 262.
Order from LCml$5.40. ph$15.30 PB 147 306
Particles from coemic-rays were required to pass
through 14 in. lead above and 10 in. lead below the
apparatus. Knock-on electron events originating in a
target above the top section of a three section 36 in.
cloud chamber operating in a field of 1 1 , 000 gauss
were detected with the aid of two proportional counters
which sandwich the top section. Electrons and mu
mesons were identified by their behavior in traversln|
lead plates above and below the middle seaion. The
target was 23. I g/cm^ of carbon In one experiment
and 17.0 g/cm^ of paraffin in the other. Energies of
the electrons and muons were determined from track
curvature measurements, and events accepted only
618
„„Bii the electron energy was greater than 100 Mev
^ the mu energy was from 5 to 50 Bev. The distri-
btfion of electron energies waa compared with theo-
fetlcal predictions based on quantum electrodynamics
aodtfled by a one parameter form factor and cor-
ttOBi for energy loss of the electrons before reach-
|M ibe chamber. The data taken at face value would
|2gMt an exceaa of events with large momentum
^Sers (50-100 Mev). The uncertainties inherent in
this experiment and poor sutistics prevent ascribing
too much significance to this excess. (Author)
Radioactivity
General Electric Research Lab. , Scheneaady,
N Y
BLECTRON INDUCED RADIATION DAMAGE IN
PURE METALS, by R. M. Walker. Scientific rept.
00 3 on Contract AF 19(604)5557. Dec 60. 43p.
33 refs. APCRL-TN-60-1122.
Orter from OTS $1.25 PB 171 523
Electron bombardment of metals at low temperatures
provides a quantitative treatment of both production
•■d recovery processes: General features erf elec-
tnm irradiation of solida; Low -temperature electron
bombardment of high -purity copper; Recent work on
the influence of lattice imperfections on the damage
and recovery processes; New results in Al, Ag, Au.
W, and Fe; current outstanding problems. (See also
PB 144 199)
High -Energy Physics Lab. , Stanford U. . Calif.
ELECTRODISINTEGRATION OF Ta AND Au NU-
CLEI, by W. C. Barber and T. Wiedling. Rept. on
(Jootract N6onr-251l6. 26 Apr 60. 25p. 17 refs.
Rept. no. HEPL-192.
Onler from LC ml$2 70, ph$4. 80 PB 147 553
YWd curves were measured for the productiOTof
5.6-day Au^'^ and 30-second Aul95 from Aul97, and
ol8. 1 -hour Ta 180, 2. 1-hour Ta^^S, and 9. 3-mln
Tal78 from Tal8l, in foil stacks which were bom-
barded by electrons. The results were analyzed to
compare the yields resulting from the direct effect of
the electrons with those resulting from bremsstrahl-
ung from the electrons. The comparison shows the
direa effect is relatively larger than is predicted by
existing theories of electrodisintegration if the tran-
sitions being excited are entirely electric dlpole.
(Author)
Princeton U . , N . J .
STUDIES OF NATURAL AND INDUCED RADIOAC-
TIVITIES, by James R. Arnold. Final rept. on Coiwraci
DA 36-034-ORD-2163. 1 June 59. 90p. 62 refs . OOR
rept. no. 1574:5; AD-225 038.
OnlerfromLCmi$4.80, ph$l3.80 PB 154 417
Contents:
Sedimentary geochemistry of the beryllium isotopes
MetlKxls for separation and determination of beryllium
In sediments and natural waters
"Solar radioactivity" studies
Rome Air Development Center. Grifflss AFB. N. Y.
GENERATKW AND DETECTION OF PULSED X-RAY
FROM MICROWAVE SOURCES, by Anthony P.
DeMInco. Nov 60, 17p. 9 refs. RADC-TR-60-185.
Order from LC ml$2. 40, ph»3. 30 PB 153 858
In his quest for higher and higher output power from
his microwave generators, man has within twenty
years come from average outputs of ten wans to pre-
sent outputs of almost one million watts. In addition
to the consideration of microwave radiation hazards
with Increased power. X-radiatlon. another poeentlal
hazard has become evident. In order to produce in-
creased powers, bigger and better high power tubes
are required, which calls for an increase in plate
voltages and plate currents, the necessary Ingredients
for more efficient penetration and higher ionizing
intensities. Until recently, the X-radiation intensities
from Air Force electronic equipment were not con-
sidered as serious potential hazards as the r-f or
microwave radiation. This paper describes in general
the generation and detection of pulsed X-radiation
emanating from high power microwave generators.
(Author)
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Columbia U . , New York .
REPLACEMENT OF PERIOCHCALLY INSPECTED
EQUIPMENT (AN CHTIMAL OPTICWAL STOPPING
RULE), by C. Derman and J. Sacks . Technical rept.
no. 8 on Contract Nonr- 266(55). Feb 60. 21p. 6 refs .
AD- 233 902.
Ortler fromLC mi$2.70. ph$4.80 PB 153 149
The following modified problem which Involves the
efficient use of acquired Information is considered:
Suppose the equipment is such that it has a measurable
characteristic associated with it which is decreasing
in tln»e; i.e. , the equipment deteriorates . Assume
that at times t-1,2 the amount of deterioration
X(t) occurring during the interval (t - 1 . l) is observ-
able and that the sequence [x(t3 t - 1 . 2, ... Is a se-
quence of independent, identically distributed, non-
negative random variables with conunon distribution
function F. The equipment is known to fail ifSX(t)>L
(a given constant for t • 1 . 2. . . . . n. Hei»ce Z. the
service life, satisfies the inequalities k - 1 ^Z ■^k.
(Author) .
RCA Defense Electronic Products. Camden, N.J.
IMPROVED BARCUSHIONS FOR FLYING HELMET,
by Leo Weinreb. Rept. for Apr 57-Dec 59 on Contract
AF 33(616)5248. Oct 60, 31p. 6 refs. WADD Techni-
cal rept. 60-568.
Order from OTS $1.00 PB 171 493
619
An improved farcushlon has been developed for use In
flying helmets . This earcushion Is superior in com-
fort, fit, duraUlity and acoustical properties to any
prior earcushtons used in a similar application. It
employs a special drawback provision which appreci-
ably aids the user in donning and removing the helmet
And which permits him to relieve headband pressure
when in low noise. The earcushion assemblies are
provided in kit form with mounting instructions for
use with the MA- 3 high altitude helmet. However,
with minor modification they can be adapted to other
helmets . This repon presents the background and
theory underlying the approach to the development and
design a< this earcushion. Mounting techniques and
earcushion materials and their influence on acoustical
performance, comfort, fit, durability and helmet inte-
gration are diicussed. Psjcboacoustlc testing and the
calculation of articulation index are described and re-
lated test dataware presemed. (Author)
Science and Tech. Dlv. , Library of Ccngresa,
Washington, b. C.
UNDERWATEI swimming. BuUetinnos. 1-12 on
Cootraa NAonr-33-57. May 57-Mar 60. 230p.
630 refa. i
Order from Ots $3.00 PB 171 577
A bibliography .
PHYSICS
Air Force Sffecial Weapona Center, K inland, APB,
N. Mex.
X-RAY MASS ATTENUATION COEFFICIENTS IN
THE 1.49 TOl 11.9 KEV RANGE, by C E. Ehren-
frled and D. Q. Dodds. Jan 60, 62p. 17 refa. AFSWC-
TN-59-33: AI>237 572.
Order from GTS %l. 75 PB 171 527
Maaa anenuat^ coefficients at eleven metala and
three plaatics were determined for fourteen X-ray
energiea from I 49 to 11. 92 kev. The eources of
radiation were K emisaion from suitable fluorescera.
The att^nuatioii coefficients obtained for metala agree
reasonably well with the compilation at Allen. The
values for the plaatics agree within 5 percent of cal-
culated coefficients from Victoreen's data. Tables
and graphs are given which show mass attenuation
coefficients determined as well aa values determined
by aeveral oth^r inveatigatora. (Author)
Avco Corp. , Wilmington. Mass .
SCATTERING COEFFIQENTS FOR ABSORBING AND
NONABSORBINC AEROSOLS, by R. Penndorf. Scien-
tific rept. no 3 on Reaearch on Aerosol Scattering in
the Infrared, Contract AP 19(604)5743. Oct 60, 88p.
18refs. RAD-TR-60-27: AFCRL-TN-60-667.
Order fromLC ml$4.80, ph$13.80 PB 153 450
Applied problems involving light scattering by aerosols
demand reliable numerical dau at the scattering and
abaorptlon coefficients . When the size of the aerosol
is smaller thaq the wavelength of the incident light.
approximation formulas can be derived from the Mle
theory. The asymptotic expansion of the exact solutiGi
is given, where the leading term is identical with the
Rayleigh approximation. For the first time, the flnt
three terms as function of the size parameter o are
correctly derived for nonabsorbing, absorbing, and
metallic spherical particles . Next , the error of the
approximation is determined using one, two, and thret
terms . This approximation extends the useful size
range by about a factor 2 for nonabsorbing aerosols.
The new approximation allows for computing the scat-
tering and absorption coefficients for small aerosoli
simpler and faster than the Mle formula. Numerical
results are given for nonabsorbing aerosols having re-
fractive indices between n ^ 1 and n s 2 . For absoitU|
spheres , the numerical values are given for the cocfll-
cients in the appropriate formulas . (Author)
Naval Ordnance Lab. , White Oak. Md.
THE MONTE CARLO METHOD: NEUTRON RE-
FLECTION BY WATER, by Paul B, Morgan.
29 Jan 59, Mp. 37 refs. NAVORD rept. 6227;
AD- 220 676.
Order from LC mi$3.60, ph$9.30 PB 154 812
This report released for sale to the public 16 Mar 6L
The Monte Carlo Method with applications of interest
to the physicist is discussed. Papers are listed which:
(I) utilize the technique in the solution of physics prok-
lems, and (2) describe methods of increasing the ef-
ficiency of the technique. Comments are made on the
general usefulness of the technique, its limiutioos and
pitfalls. The treatment is Introductory rather than
comprehensive. The Monte Carlo Method is applied
to the problem of estimating the probability of nor^
mally impinging monochromatic neutrons scattering
back from deep circulating pure water. (Author)
Texas U. , Austin.
RELAXATION PROCESSES IN UQUIDS AND SOUDS.
by A. W. Nolle. Final rept. on Contract Nonr-375(06).
1 Apr 60, 44p. 14 refs. AD- 237 244.
Order from LC mi$3. 30, ph$7. 80 PB 147 W
The experimenul work consisted mainly of investiga-
tions of magnetic resonance relaxation, with a sll^tly
smaller qxuntity of work on relaxation processes in
ultraaonic-wave absorption. The results led to infor-
mation concerning thermally aaivated molecular
processes in high polymers, in molecular liquids, la
aqueous solutions with paramagnetic ions, and in
crystalline solids. (Author)
Acoustics
California U. , Los Angeles.
FLUID MOTION AND SOUND, by AlanBaweU. Aimd
summary rept. 1 May 59-30 Apr 60, on Contract
Nonr-233(62). May 60, 6p. Dept. of Ei^ineerlngrejt
no. 60-51; AD- 239 941.
Order from LC ml$l. 80, phfl. 80 PB 149 0»
620
Smunaries of papers on the following topics are re-
ported: Instability of Jets; Edge Tones; Aeolian Tones;
IVirlwIent Jet Noise; Boundary Layer Noise; and
Pitjpagation Problems.
paycho- Acoustic Lab. , Harvard U. , Cambridge,
PERIODIC STATUS REPORT 35. Rept. for 16 Nov 59-
15 May 60 on Contraa Nonr-i866(lS) and National
Science Foundation Grant G-2668. 15 May 60, 21p.
94 refs. PNM-87; AD-237 634.
(Jrder from LC mi$2.70, ph(4.80 PB 147 765
Ccmtents:
Auditory faciliution following stimulation at low
itfanslties
Gfe the new psychophysics
Ratio scales, partition scales, and confusion scales
The influence of inhibition on the sensation pattern of
the skin and the eye
The speaker's subjective scale of vocal effort
The binaural summation of loudneaa
Electricity and Magnetism
Avco Corp. , Wilmington, Maaa.
AN EXPERIMENTAL INVESnGATI(»i OF NEGA-
TIVE POINT- PLANE CORONA AND ITS RELATION
TO BALL LIGHTNING, by Edward T. Pierce, Richard
M. Nadile and Philip J. MclCinnon. Final rept. on
Cootraa AF 19(604)7342. 24 Oct 60, 80p. 41 refa.
Technical rept. RAD-TR-60-29; AFCRL-TR-60-354.
Order from LCmi$4. 50, ph$12. 30 PB 153 916
Existing theories of ball lightning are briefly dia-
cuBsed. Kapltaa has suggested that the energy to aua-
taln a fireball comes from resonant absorption of
radio waves of 300/mc/s. Pierce has extended
Kapltsa's theory by suggesting a mechanism for pro-
ducing this r-f energy during a corona discharge. The
oorooa diacharge from a negative point flows in a
scries of regular pulses called trichel pulses. Baaed
on the theoretical relationship between corona dis-
(Trichel pulses) and ball Lightning, an experl-
il program is developed. The main part of this
report la concerned with the description and discus-
am of the experiments. To obuln the nuximum
poaalble corona frequencies, a van de Graaff gener-
ator haa been utilized. An appUed voltage of 280,000
*oka haa produced a current of 1 25 microamperea
and a Trichel pulse frequency above 2 mc/a. This
■hort experiment has established the usefulneaa of
<Ua type of generator . The experiment, however,
baa been conducted with a snull d-c high- voltage
inarator (up to 30 kv). Pulse-repetition frequencies
of a few mc/a have been the highest attained in the
oouTK of the experiments. The results obuined are
Ikn dlacussed as they concern ball lightning. (Author)
Lincoln Lab., Mass. Inst, of Tech., Lexiagton.
EXCITATION AND BOUNDARY EFFECTS IN SPIN
WAVE RESONANCE, by R. F. Soohoo. Rept. on
Contract AF 19(604)7400. 7 Dec 60, 8p. 6 refs. '
MG-0045, AD- 248 365.
vW«r from LC mi$1.80, ph$1.80 PB 153 700
Using the general spin wave dispersion relation and
the general exchange boundary condidon, the spin
wave absorption spectrum in a Permalloy film is cal-
culated. Whereas the s pacings between the various
spin wave resonance peaks are largely depaedent upcn
the value of the exduinge constant A, tiie result of the
calculation shows that the relative intensities at the
absorptian peaks are dependent upon both A and the
surface anlsotropy energy density K^. Thus, the
value of Kg can be obtained by comparing the relative
experimental Intensities of the various peaks with the
calculated results using various values of assumed
K,. Though the resonance intensities are also depend-
ent upon the ratio of the r. f. magnetic fields at the
two surfaces of the film, an experimental configura-
tion may be devised such that the ratio d the two
fields is near unity. In this way. Kg for permalloy
films was estimated to be from 1 to 3 ergs/cm^.
(Author)
Polytechnic Inst, of Brooklyn, N. Y.
MAGNETORESICTANCE AND DC»4AIN STRUCTURE
IN THIN FERROMAGNETIC FILMS, by Richard L.
Coren (Doctoral thesis) and Hellmut J. Juretschke.
Technical rept. no. 9 on Contraa Noar-839(06).
15 May 60, 126p. 23 refs. AD- 238 066.
Order from LC ml$6. 30, ph$19. 80 PB 148 349
Magnetoresistance measurements were used to deter-
mine the magnetic doniain struaure of nickel films.
The magnetoresistance results are discuaaed in terms
of a new representation in which the resistivity com-
ponents, parallel and transverse to the current, meaa-
ured simultaneously as the a;q>lied magnetic field
varies in magnitude or direalon, are regarded as
Cartesian coordinates. Tills representation is inde-
pendent of the direction of the current relative to any
preferred orientations in the film. Marked differ-
ences are found between the measured magnetoresist-
ance and the behavior expeaed of a single domain
film. The nature of the differences indicates that
these films must at least contain a distribution ot
uniaxial magnetic regions in the film plane. A par-
ticular model having these propertiea is developed.
(Author)
Electronics
Advanced Kinetics, Inc. [SanU Ana, Calif. ]
PRODUCTION OF MILLIMETER AND SUB-MILU-
METER ELECTROMAGNETIC WAVES BY THE
INTERACTION OF PLAadA AND ELECTRON BEAMS
WITH HIGH DfFENSITY PULSED MAGNETS, by
Ralph W. Wanlek. Scientific rept. no. 1 (Quarterly)
15 July-Oa 60i on CMtract AF 19(604)7406. [1960]
?p. AFCRL-TN-60-1124; AD- 248 330.
Order from LC mi$1.80, pb^.80 PB 153 732
Theoretical studies have been initiated on the produc-
tion at bremsstrahlung radiation by electron beams
li^eaed into hlgb-fleld magnets. The first phase at
the experimental work is aimed at testing the feasi-
bility of injeaing electron beams into high-field
magnets.
hctelle Memarial Inst. , Columbus, Ohio.
INVESTIGATIOMS OF RARE- EARTH OXIDE
CATHODES, by j. BL Baker and G. E Gaines. Scien-
tific rept. no. S. 1 Aug-31 Oct 60 on Contract
AF 19(604)5691. 1 Nov 60. lip. 1 ref. AFCRL
11^-60-1152. Al>24«616.
Order from LCimi$2. 40. ph$3. 30 FB 153 823
The emiss ion properties erf A mixture erf the oxides o^ neo-
dymiumandgad4liniuiTi coated on a tantalum wire were
determined. Tile eniissicn level at 1400% was as
high as 0. 5 amp/cm^ but, in ccnunon widi cathodes
composed of th« same coating on other refractory-
metal base wires, the emission tended to beunstable
at brightness temperatures of iNxu 1300oC and below.
(Author) (See alio PB 152 538)
Boston Coll. . Chestnut Hill, Mass.
RESEARCH DIRECTED TOWARD TOE STUDY OF
THE PROPERTIES OF A PLASMA THAT MAY
LEAD TO A NEW TYPE OF EM GENERATOR, by
William G. Guitdon. Final rept. on Contract
AP 19(604)2195. 19 Sep 60, 14p. 3 refs. AFCRL
TR-60-429. AD- 248 587.
Order from LCUi$2. 40. ph$3. 30 PB 153 820
A description iii given of the major pieces of perma
nent equipment tonstructed or assembled during the
course at the work, mainly consisting of a36-kilo-
joule capacitor bank and related apparatus. A summary
description is given of the chief experiments carried
out: (1) observation of the motion of ionized gas
through a pulsed magnetic field; (2)pulsed Zeemanand
PtS(±en-Back Effect measurements; and (3) work to-
ward the development of a pulsed air-core betatron.
(Author)
[Electronic Syatema] Lab. , Maaa. Inst, of Tech. ,
Cambridge ■ |
MODULATION AND CKMODULATION WITH 'SEMI-
CONDUCTORS, by Dale P. Masher. Technical rept.
no. 2 on Contract h^5orl-a7876. 15 June 53. 59p.
9refa. AD- 16 1^1.
Order from LC jnii$3. 60, pb$9. 30 PB 154 843
Thia report rel^aed for sale to the public 17 Mar 61 .
I
Initial inveatlgafion of modulation and demodulatioa
ayatems which employ transistors was concerned with
classifying such systems in a manner which permits
logical study an<l analysis. This work led to a claal^
fication system tvhlch considered linear, time -varying
systems as first order, and nonlinear, square-law
systems as second order. Further distinction waa
made between continuous -data systems in which the
sensitivity function exhibits only discrete zero cross-
ings, and sampled-dau systems in which the sensi-
tivity function possesses some characteristic distri-
bution of finite intervals where the function is zero.
Analyses were rtiade of first- and second-order sys-
tems. The use ^ transistors as controlled- sensitivity
devices was discussed for grounded-base and -emitter
operation. Residts derived experimentally from
carrier-present and -suppressed systems which
utilize transistot'S as time -varying parametera Indi-
cated that the tr^naistor systems exhibit limited fre-
quency response because of the intrinaic nature of ths
tranaistora, and that tranaistora offer no decided ad-
vantages over vacuum tubea with reapect to linearity
and distortion -free operation but are better than
diodes in almost every operational aspect.
General Mills, Inc. , Minneapolis, Minn.
STUDY OF SPUTTERING OF MATERIALS, by
G. K. Wehner, N. Lsegreid, and R. V. Stuart. PImJ
rept. for IS Apr 59-14 Oct 60 on Contract
AF 19(604)5536. Oct 60. 75p. 40 refs. Rept.
no. 2133; AI^CRL-TR-60-418; AD- 248 045.
Order from OTS $2. 00 PB 171 513
Sputtering yield measurements for nitrogen, hydrogn
and neon ion bombardment at energies up to 1 kev are
preaented. The hydrogen and nitrogen results are
questionable. The neon yield results for 28 metala
and aemi conductor a show that an important parameter
in sputtering is the degree of filling of the d- shells of
the target atoms. Yield measurement at very low
bombarding ion energy are discussed. A new spec-
troscopic method allows the instantaneoua meaaure-
ment of spuuering yields down to 10'^ atoms/ion. Ft
waa found that yields at 10 ev bombarding energy be-
come so small that erosion effects at a satellite sur-
face ahould never pose any problems. Sputtering
effects on the moon's surface are discussed. About
40 meters of material should have been sputtered in
10^ years under solar wind bombardment. Sputtering,
provides an explanation for the smoothness of the
lunar surface on a 10 cm scale.
Lincoln Lab. , Mass. Inst. ofTe^h. . Lexington.
A SIMPLE APPROXIMATE EXPRESSION FOR CCW-
VERTING DIRECTLY FROM NOISE FIGURES IN
DB TO NOISE TEMPERATURES; by E- P. McCurley
and C Blake. Rqx. en C>)ntraa Af 19(604)7400.
8 Dec 60, 5p. 46 G-0009, AD- 248 912.
Order from LC mi$1.80. ph$1.80 FB 153 804
Sindel S. p. A., Rome (Italy).
MICROWAVE DETERMINATION OF AFTERGLOW
TEMPERATURES AND ELECTRON COLUSION FRB
QUENCIES IN NITROGEN, by D. Formato and
A. Gilardlni. Technical summary rept . no. l,SepS9-
Apr 60, on Contraa AF 61(052)39 30 Apr 60, 18p.
6 refs. AFCRL-TN-60-1136; AD-248 685.
Order from LC mi$2. 40, ph$3. 30 PB 153 807
Two hypothesis, ionization from metastables and
shock waves, were proposed in order to explain the
high electron temperature in the afterglow of a d.c.
Nitrogen discharge. Some experiments have been per-
formed to susuin or reject these hypothesis. The
electron fractional energy loss per collision has also
been measured and found in good agreement with
previous measurements by Crompton and Sutton.
(Author)
Stanford Electronics Labs., Stanford U. , Calif.
DENSITY FLUCTUATIONS IN A PLASMA IN A
MAGNETIC FIELU WITH APPLICATIONS TO THE
lONOSHlERE, by T. Hagfors. Scientific rept. no. I
on Contraa AF 19(604)7436. 5 Dec 60, 35p. 19 refs.
AFCRL-TN-60-1164, AD-248 447.
Order from LC mi$3.00, ph96.30 PB 153 824
QaBeral expressions are developed for the fluctuation
todSBSlty of electrons, ions, and charge in a plastna
In diermal equilibrium in an eztefnal magnetic field
taking only Coulomb interaction into account. The
ipectral distribution of the spatial Fourier components
(rf these fluctuations is derived from basic principles.
The fluctuations in electron density are discussed in
loroe detail, and spectra are computed under coo-
iHboBS whidi are thought to prevail in the outer iono-
f]flMre. Frequency spectra of general validity are
computed for electron density fluauations along the
magnetic field. It is shown by means of examples
dMt the frequency spectra under lonospberlc ooodi-
doBS are not much influenced by the magnetic field
mcepc for density fluctuations fairly close to perpen-
dicularity to the magnetic field. Applications to inco-
bo-ent backs cattering are discussed, and it is shown
(hat, under suitable conditions, backscatter tech-
niques can give valuable information about electron
dotsity, temperature and constituents of the lono-
spbere. (Author)
Stanford Electronics Labs. , Stanford U. , Calif.
THE EFFECTS OF INITIAL ELECTRCW VELOCI-
TIES AND SPACE CHARGE IN SECONDARY
EMISSION, by M. D Hare. Rept. on Contract
AF 33(616)6207. 31 Dec 59. 32p. 12 refs. Technical
rept. DO. 303-2; AD-232 288.
Order from LC mi$3. 00, ph$6. 30 PB 150 717
Secondary -emiss ion devices fall into two classes. (1)
Those in which the em iner- collector potential is such
that all emitted secondary electrons are received by
the collector. (2) Those in which the emitter-col-
leaor potential is such that the number of collected
secondary elearons equals the number of incident
primary electrons. For either class of device this
potential is determined by the nature of the secondary
emitter, the electrode configuration, and the primary-
electron current density. For the first class the col-
lector must always be positive with respect to the
emitter. For tlie secotid class there are cases In
which this potential will be negative and others in
which it will be positive. This paper shows howLang-
ouir's treatment of thermionic emission in ttie plane
diode can be applied to secondary emission between
parallel planes to compute the emitter-collector po-
tsntial for either class of device. This treatment
accounts for space charge and Initial electron veloci-
ties. The effects predictedtheoretically are supported
by experimental measurements. (Audior)
Molecular Physics and Spectroscopy
(imegie Inst, of Tech. , Pittsbui^gh, Pa.
INVESTIGATION OF THE REFLECTICW AND
SCATTERING OF MOLECULES BY SOLID SUR-
FACES, by Paul M. Marcus. Final rept. on Ckxitract
Noor-760(11), continuation of Contract N7onr-303.
I Apr 60, 19p. 10 refs. AD-235 795.
Older from LC mi$2. 40, ph*3. 30 PB 153 768
Colorado U. , Boulder.
ASPECTS OF MOLECULAR STRUCTURE OF
ETHYL ALOCWOL AND THE DESIGN, CONSTRUC-
TION, AND OPERATION OF A STARK MODU-
LATED MICROWAVE SPECTROGRAPH, by George
Edward Schafer, Master's thesis. Technical rept.
no. 7, pt. I, I Feb 53-30 Sep 59, on Study erf the
Wave Equation for Loosely Coupled Molecules, Con-
tract DA 23-072-ORD-1059. [1959) I69p. 32 refs.
OOR rept. 839. 10-P, AD-228 615.
Order from LC ml$7. 80, ph$25. 80 PB 150 701
A Stark modulated microwave spectrograph was de-
signed, constructed, and tested. A set of instruc-
tions were prepared to facilitate the use, mainte-
nance, and repair of the components of the spectro-
graph. This instrument was used to examine ethyl
alcohol. for Stark sensitive absorption lines in the
frequency range of 12. 4 to 26. 5 kMc/s. The fre-
quency range of 18. 0 to 26. 0 kMc/s was systemat-
ically searched at relatively high sensitivity, while
the remainder of the frequency range w'as examined
for relatively intense absorptions. A number of ab-
sorption lines had Stark components which could be
resolved, and the rotational transitions of these lines
were tentatively identified. These absorptions were
then examined again, and a tentative analysis of the
spectrum was made. Prom this analysis, the follow-
ing provisional molecular constants were determined
for ethyl alcohol; A -33, 326. 64 Mc/s, B - 9112. 85
Mc/s, C - 8019. 38 Mc/s. K - 0. 913576, u« • 1. 18D,
and ub * 1- 37D, where A, B, and C are the rotational
consunts associated with the least, intermediate,
and greatest moments ol inertia, respectively, ua
and Ui) are the components of the dipole moment
along the axes of the least and intermediate momente
erf inertia, respectively, and K is Ray's asymmetry
parameter. (Author)
(Guggenheim Jet Propulsion Center, Caltf. hst. at
Tbch. . Pasadena, Calif.
E(5UILIBRIUM EMISSIVTTY CALCULATIONS FOR A
HYDROGEN PLASMA AT TEMPERATURES UP TO
10, 000**K, by IX Olfe. Ttechnlcal rept. no. 33 on Con-
tract Nonr-220(03) and AF 18(603)2. May 60, 69p.
53 refs.
Order from LC mi$3. 90, ph$10. 80 PB 148 936
The important equilibrium emission processes In a
hydrogen plasma have been investigated in the temper-
ature range between 300OK and 10, OOOOK for pressures
up to several hundred atmospheres. Representative
emissivlty calculations have been carried out for a
transparent gas at a toul pressure at 100 atmos and a
mean beam length of 30 cm. Important emissivlty
contributions were made by the pressure- induced
fundamental vibration- rotation band and rotational
lines of H2 at the lower temperatures, 1. e. , below
approximately 4500OK. Above this temperature, the
bound-free and free-free transitions of ti»e H' ionand
the continuim and line radiation of the H atom are the
most imporunt contributors to the emissivlty. The
following emission processes were also investigated;
the bound-free transitions of the Ho ion, free-free
transitions of colliding H atoms and H'^ ions,
electronic transitions of the H2 molecule, quadrupole
vibration -routlon transitions at the H? molecule, and
vibration -rotation transitions of the HD molecule, fai
addition, the effects of the lowering of the ionization
623
potentials by the field* d plasm* Ions and of the very
broad wings at the Lyman a line have beencxnsldered.
(Author)
Harvard U. . ^mbridge, Mass.
SECOND DIFFERENCES OF MOMENTS OF INERTIA
IN STRUCTURAL CALCULATIONS: APPLICATION
TO METHYL- fLUOROSILANE MOLECULES, by
Lawrence C. Krisher and Louis Pierce (U. of
Notre Dame). Rept. on Contract Nonr- 1866(14). [196(^
26p. 12 refs. AD- 231 434.
Order from LQ ml$2. 70. phK 80 PB 153 154
An extension a^ application of the method recently
proposed by Pi«rce [J. Mol. ^)ectro8copy 3:575, 1959]
for the location of "near-axis atoms" from spectro-
scopically determined monvents of inertia is made.
Equations are derived which are required for the
application of the method to asymmetric top mole-
cules with Cg symmetry. The method Is applied to
the determination of silicon coordinates in the mole-
cules CH3SIH2F and CH3SIHF2. The experimental
results are coitibined with results of previous micro-
wave investigations of these molecules in order to
determine their structures. Addition of each fluorine
atom lowers the SiC distance. The SIF distance is
lowered on adding the second fluorine. In the case of
CHaSlHI^ the tquillbrlum conformation (staggered)
is also determined. (Author)
I
Physics , Harvard U . , Cambridge,
Lyimn Lab .
Kwss.
ATOMIC BEAM RESONANCE EXPERIMENTS WITH
STORED AT01*B. by Mark Goldenberg. Final rept.
for 15 Jan 58-14 Jan 60 on Contract DA 36-039-sc-
74976. 23 July 60, 73p. 22 refs . AD-243 052.
OrderfromLCjmi$4.50. ph$12.30 PB 153 237
The atomic beam separated oscillatory field resonance
technique was wsed to study the hyperflne frequency d
cesium as perturbed by collisions with storage box
walls . With a wall coating of long straight-chain satu-
rated hydrocar^xms , resonances are observed even
with approximately 200 wall collisions . A theory
based on the statistical nature of the collision inter-
action is described which is in qualitative agreement
with the experimental data on the frequency shifts and
line broadening . (Author)
Malllockrodt CSiemlcal Lab. , Harvard U. ,
Cambridge, Mass.
SUPPLEMENTARY FORMULA INDEX FOR MICRO-
WAVE SPECTROSCOPY FOR 1954-1958, by E. Bright
Wilson. Jr. an<i James R. Holton. Rept. 00 Contract
Nonr 1866, Talk order XIV. [1960] 19p. 346 refs.
AD- 234 157.
Ordo- from LC ml$2.40, ph$3.30 PB 154 113
Materials Research Lab. , Watertown Arsenal, Mass.
COMMENTS ON DETERMINATION OF ATOMIC
SCATTERING FACTORS, by D R. Chipman and
A. Paskin. Jul* 60, 5p. 1 ref. MRL repc. no. 88.
Order from LQ ml$l. 80, ph$l. 80 PB 150 088
Errors In a recent article by R. R RooT. Jr. are
pointed out. A possible explanation Is given for the
fact that Roof's final result Is nearly correct.
(Author)
Noyes Chemical Lab., U. of niinols. Urbana.
ELECmON COUPLING OF NUCLEAR SPINS. IV.
TEMPERATURE IMPENDENCE IN SUBSTITUTED
ETHANES, by John C Schug, Paul E. McMahon, and
H. S Gutowsky. Technical rept. no. 28 on Contract
Nonr- 1834(13). 1 Apr 60, 28p. 16 refs. AD- 237 051.
Order from LC ml$2. 70. phK 80 PB 147 775
The proton-proton coupling constant. Apjj^-, in
H-C-C*-H' groups is known to depend upon the dihedral
angle, ^ . Previous valence-bood calculations by Kar-
plus (J. Qicm. Phys. 30:11, 1959) have given the re-
sult that Aj-j. at Aq cos2 ♦ ■•- R This relation Is ussd
to estlmatetne effects upon the average coupling
constant of torsional vibrations and reorientations
about the C-C bond. For substituted ethanes, it is
found that torsional vibrations produce a modest temper-
ature dependence, of opposite sign for the trans and
gauche coupling. However, for molecules In which the
potential function. V(<^), has 3-fold symmetry, ro-
tational averaging leads to a cancellation of the vlbrt-
tlonal effects, giving a temperature Independent value,
<Aj^.> , for the average coupling. This prediction
was verified in experiments on ethyl nitrate for which
<AhH'^ was found to have a constant value of 6. 92cpi
over a 100° temperature range.
Western Ontario U. (Canada).
TRANSITION PROBABILITIES OF MOLECULAR BAND
SYSTEMS. XVll: TABULATED KLEIN -DUNHAM PO-
TENTIAL ENERGY FUNCTIONS FOR FIFTEEN
STATES OF N2. N2*, NO, 02. C2 AND OH. by
W. R. Jannaln. Scientific rept. no. 5 on Contraa
AF 19(604)4560; Scientific rept. no. 2 on Contracts
AF 49(638)640 and Nonr -2895(00). 1 July 60, 20p.
7 refs. GRD-TN- 60-498; AFOSR-TN-60-877;
AD- 247 906.
Order from LC mi$2. 4a ph$3. 30 PB 153 637
Sets of classical turning points, together with the cor-
respoodlng vibrational energies, are given for the fol-
lowing molecular states: N2, Xll+, alll . K^L.
b3JL. C3fl^; N2*. A,2JI: NO. k^V. B^fl^; Oj- a^^g.
"^g- ^2* * "u" g u u i
These numbers, which were calculated from series
formulae, represent Klein -Dunham potential energy
functions for the sutes listed. The maximum vibra-
tional quantum number varies from 2 to 14, dependlag
on avlalable experimental data. (Author)
Optics
Massachusetts U- , Amherst.
THE SCATTERING OF LIGHT BY POLYMER FlUtf
POSSESSING CORRELATED ORIENTATION FLUC-
TUATIONS. I. by Richard S. Stein and Philip R.
Wilson. ONR Technical rept. no. 18 on Contract
Nonr-2151(00) 10 May 60, 24p. 9 refs. AD- 244 444.
Order from LC mi$2. 70, ph$4. 80 PB 150 657
624
tlK acattering of light from polymer films exhibiting
jfidoni and anisotropic orientation fluctuations is
■nslyzed mathematically. The equations derived are
related to those cA Prins (Physics 22:576. 1956; iUd
2):2S3, 1957) and Peterlin (Physik. Z. 37:43, 1936) who
itudied orientation fluctuations principally as related
to the depolarization of low molecular weight liquids.
Iptbe analysis of anisotropic orientation fluctuations,
different types of orientation are discussed: including
(1)' ideal fiber-like orientation where the principal axes
are always orienuted along the line erf separation, and
(2) ideal disklike orientation where the principal axes
ire oriented perpendicular to the line of separation.
Aaual systems cannot exhibit either extreme but may
deviate from randomness in a rod or disklike manner.
The type of anisotropy is dependent on the crystalliza-
tloa mechanism.
Naval Ordnance Test Station [China Lake] Calif.
TOE DESIGN OF A VERSATILE LOW-POWER PER-
ISCOPE, by Theodore R. Whitney, Roger S. Estey,
iod Lawrence W. Nichols. 20 Mar 50, lOp. NAVORD
rept. 1222; NOTS 279.
Onier from LC ml$1.80, ph$1.80 FB 154 750
lUs report released for sale to the public 15 Mar 61.
A parlscope is described which permits an operator
to view remote-controlled operations from a position
Mdnd protective barriers. Line of sight from the
obfactive can be directed through 180 degrees hori-
nntally and 75 degrees vertically by the operator.
"Hie optical system and mechanical components are
of • configuration that permits the periscope to con-
form to many contours differing both in length of
pKfa and location of corners. Optical resolution Is
good enough to allow the reading of dial instruments
ill the object plane. (Author)
Wayne Slate U. , Detroit, Mich.
EXPERIMENTAL INVESTIGATIONS ON THE LIGHT
SCATTERING OF COLLOIDAL SPHERES. IV. SCAT-
TERING OF LINEARLY POLARIZED LIGHT AND
THE 'SCATTERING RATIO" AT AN ANGLE OF OB-
SERVATION OF 90°, by Wilfrled Heller and Richard
Tabiblan. Technical rept. no. 35 on Contract Nonr-
736(00). 1 Feb 60. 47p. 11 refs. AD- 234 486.
Order from LC mi$3. 30, ph$7. 80 PB 153 123
Light scattering of 18 monodisperse polystyrene and
pojvvlnyltoluene latlces was investigated at an angle of
9(r with respect to an incident linearly polarized beam
•hoae electric vector was, in succession, parallel and
perpendicular to the plane of observation. The ratio
of the two quantities obtained, designated as scattering
ratio, <r-- which is closely related to depolarization
•id polarization ratio - - was found to be a very useful
VMOtity for absolute particle size determinations ex-
cept for particle dlameter8< 1 /4 u (00 use of visible
Hf^). a particular advantage being the relative
isaensltivity to changes in the solid angle of the scat-
tered beam. Partial investigation of the spectra of (f
eUminated the problem of multivaluedness erf results
taherent in any measurements of lateral light scaner-
1b|. The various types of concentratiexi dependence of
9, of the individual intensities and also of scattering
from unpolarized incident light were investigated in
deuil and could be explained fully. The particle
diameters obtained from (T, evaluated on the basis of
theoretical data derived from the Mie- theory, agreed
very aatisfi^orily with electron microscopic results
(range covered: 135 pip to 824 n^i)- Except for minor
modifications, the hig^ precision apparatus was the
same as used in the preceding investigations. (Author]
Wayne State U . . Detroit , Mich .
PARTIAL TABULATION OF CT- SPECTRA FOR DETER
MINING SIZE DISTRIBUTION CURVES FRC»« UGHT
SCATTERING, by Morton L. Wallach, Marvin F.
Walden and Rodney Wu . Technical rept . no . 36 on
Contract [Nonr] 736(00). 1 Mar 60, 21p. AD-234 487.
Order from LCmi$2. 70, ph>4. 80 PB 153 757
Willow Run Labs. , U. of Michigan. Ann Arbor.
ULTIMATE SENSITIVITY AND PRACTICAL PER-
FORMANCE OF THE TELLURIUM PHOTO-
CONDUCTIVE MTECrOR. by David F. Edwards.
Rept. on Project Michigan. Contract DA 36-039- sc-
78801. Dec 59, lOp. 9 refs. Repc no. 2900-129-R;
AD- 230 703.
Order from LC ml$l. 80, ph$l. 80 PB 153 456
Calculations of the ultimate seiultlvity and measure-
ments of d)e practical performance have been made
for the tellurium phe>toconductive detector. For the
condition that detector sensitivity Is limited by fluctu-
ations of background radiation, the theoretical NEP
(noise equivalent power) at the peak of spectral sensi-
tivity (A.-3. 4>4) was calculated to be 5. 1 x 10' ^^ ^inxu
For the "best" telluriimi detector the measured value
of NEP was 3. 1 x 10"^ watt at the same wavelength
and at the optimum chopping frequency. These values
indicate that the tellurium photoconductive detector is
background limited and thus is an ideal detector.
(Author) •
Solid State Ph)rsics
Advanced Semiconductor Lab. , General Electric Co. .
Syracuse, N. Y.
APPLICATIONS OF TUNNELING TO ACTIVE DI-
ODES, by N. Holonyak. Jr. Scientific rept. no. 2> on
Contract AF 19(604)6623. Oct 60, 67p. 9 refs.
AFCRL-TN-60-1141.
Order from LC mi$3.90, ph$ia80 FB 153 873-2
This repon covers the results obtained to date in
studies of tunneling due to sutes (bands) in the
"forbidden gap" of GeAs and InP, describes a relia-
bility - failure property in GaAs tunnel diodes which
bears some resemblance and possibly relationship to
formation of 'Yorbidden gap" states, outlines a method
of regre>wing and doping GaAs (and potentially other
compounds) from an alloy-vt^xir state, and presents
some initial results in growing various Intermetallic
compounds (Including epitaxial growth of GaAs) via
reaaion with a halogen in a closed quartz tube. A
theoretical and experimental study of tunnel diode
characteristics and their relationship to circuit per-
formance has been undertaken. The circuits that have
been studied are as follows: general purpose logic,
sequential circuits, pulse generators and drivers,
memory, and active R-C filters. Results to date in-
dicate that the practical ai^lications of tunnel diodes
are limited. (Author)
625
Mlittlc Research Labt. , Aberdeen Proving Ground,
Md.
CHARACTERISTICS OF SEVERAL OIELECTRIC
MATERIALS AT HIGH PRESSURE, by George Hauver.
Oct 60. 18p. 2 refi. Technical note no. 1356;
AD- 248 025
Order from LCmi$2. 4a ph$3. 30 PB 153 649
Some plastics, when subject tohigh transient pressures,
have been found to generate an electric current that is
dependent upon the particular plastic, pressure, load
resistance, area and thickness. It is suggested that
dlpole orienutioo is the dominant mechanism responsi-
ble for the curzmt. The resistivity d sulphur has been
found to decreale to values less than 0. 04 ohm-cm
when It Is subjected to high transient pressure. Some
results are included which indicate that sulphur may
possibly be used as a pressure tranducer for measure-
ment d pressure profiles. (Author)
norit
Battelle Mem<irial Tnat. , Columbus, Ohio.
BASIC TRANSPORT PHENOMENA IN CERMANIUM
AND INDIUM ANTIMONIDE. by R- T. Bate,
S. E. Miller, and A. C. Beer. Pinal rept. on Con-
tract AF 49(638)222. 31 Oa 60. I2p. 6 refs. AFOSR-
TR-60-158; AD- 246 156.
Order from GTS $0. 50 PB 171 511
The growth of ItiSb single crystals and the transport
properties of InSb and semiconducting diamond were
studied. Summaries are given of work in: galvano-
magnetlc effects in InSb; purification and single crys-
tal growth; galvanomagnetlc effects in semiconducting
diamond; inhomogeneltles and associated galvanomag-
netlc effects in semi conductions.
Battelle Memorial Jnst. , Columbus , Ohio.
INFLUENCE OP MAGNETOCONDUCTIVITY DISCON-
TINUITIES ON GALVANOMAGNETIC EFFECTS IN
INDIUM ANTIMONIDE, by R. T. Bate, J. C. Bell, and
A. C. Beer. Technical note no. 4 on Contract
AF 49(638)222. 16 Oct 60, 30p. 15 refs. AFOSR-TN-
60-1226; AD- 246 424.
Order from LC{mi$2. 70, pl44. 80 PB 153 199
Anomalous galvanomagnetlc effects associated with
spatial discontinuities in earner concentration have
been observed In n.-type InSb. These discontinuities
result from anisotropic segregation of impurities dur-
ing crystal grol^th. An increase In the magnitude of
the Hall coeffldeni at 20.000 gauss to nearly twice the
weak-field value was observed m one case. The mag-
netoreslstance Is especially sensitive to inhomogeoe-
itles . For an ifthomogeneous sample at a particular
ntiagnetic field, the measured ^P//Oq niay be as much
as 100 bn«s larger than that for a homogeneous sam-
ple. Negative magnetoresistaoce has also been ob-
served at room temperature in inhomogeneous sam-
ples . All of iho above observations are predicted
qualiutively by considering a simple nxxiel consisting
of a loi^, thin ipecinten having a discontinuity in re-
sistivity and H411 coefficient in the current direction.
The boundary vwlue problem corresponding to tUs
case is solved |o predict the electric field and current
densities. (Aut)ior)
California U. . "Los Angeles. "
STRESS FIELD CAUSED BY SLIP IN A WORK-
HARDENlNG CRYSTAL IN AN AGGREGATE, by
T. H. Lin and D Martin. Rept. on Contract
AF 49(638)20. Oct 60. 33p. 14 refs. Dept. of Engi-
neering rept. no. 60-94; AFOSR-TN-60-1256.
Order from LC mi$3. 00, ph$6. 30 PB 153 729
The stress field of an aggregate of randomly-oriented
crystals loaded just beyond the elastic limit is com-
puted. The elastic modulus of each crystal is taken
to be isotropic. The sliding directions and planes of
different crystals are different. The initial stage of
plastic deformation, at which only the most favorably
orlenuted crystal slides, is considered. This slidiif
crystal is assumed to be of cubic shape and at the
inierior of a fine grained aggregate. The aggregate
is infinitely large as compared to the cr3r8tal. It is
shown that the plastic strain gradient is equivalent to
body force in the calculation of stress field. The
equivalent body force caused by slips in the sliding
crysul is considered to apply in an infinite elastic
isotropic medium. The known solution of the stress
field caused by a concentrated force in an infinite
medium is applied to express the stress components
in terms of slip distributions in the sliding crystal.
The increase of critical shear stress with slip caused
by work hardening is considered. The resolved shear
stress is equated to this critical shear stress in the
slidii^ region. This gives an integral equation in
terms of slips at different points. This equation is
solved numerically by the method of finite difference.
The stresses causied by these slips are then calcu-
lated and shown in graphs. These stresses caused
by slips decrease rapidly with the distance from the
sliding cryaul. (Author)
Curtiss -Wright Corp. . Santa Barbara, Calif.
STUDIES Qfti MACWETOSTRICTIVE FERRITES. by
G. S. Smith. Final progress rept. for Dec 58 -Dec 59
on Contract Nonr- 2749(00). (1959] 78p. 28 refs.
TR 59-80: AD- 234 784.
Order from LC n[U$4. 50. ph$12. 30 PB 154 095
An investigation was made of the reproducibility of tlis
properties of magnetostrictive ferrites and of the
changes in the properties brou^t about by small
changes in composition. The study was concerned pri-
marily with a correlation of properties with fxarticle
size and distribution of the raw and reacted oJtides as
Influenced by chemical composition and the forming
and firing variables. The basic compositions studied
were NiO Fe203 and NiO^i -a) CoOr.) Fe20^. Since
the properties of the ferntes variea uniformly as the
average particle size of the presintered powder, it
was concluded that the physical state of the presintered
material must be controlled in order to assure a high
degree of reproducibility. Two compositions of
NIO- FeTOs. which had average panicle sizes of 1- 52
and I. 5^ were prepared to demonstrate the effect tlat
particle size and firing schedule have on the proper-
ties. The samples were fired separately at 1400°C te
1 hr. The maximum variations were: density of
iO. 02%; resonant frequency *0. 01%, electromechani-
cal coupling of 0*0. 75%; and mechanical Q, of *l. 5%.
626
Franklin Inst. Labs, for Research and DevelofMnent,
Philadelphia, Pa.
SINGLE DOMAIN CRITERIA AND THEIR IMPLICA-
TK^iS, by Henri Amar. Rept. on Solid State Re-
■earch and Properties of Matter, Contract
AF 33(616)5041. Oct 59. 25p. 12 refs. Intexlm r^.
I.A2033-3; WADC TR-59-547; AD- 239 602.
Older from OTS |0. 75 PB 171 543
A general and critical review of the various single
domain criteria is presented in a uniform notation,
and the validity of the various treatments is assessed.
While the Stoner-Wohlfanh (S-W) theory is rigorous
and valid within its assumptions, the heuristic S-W
•iagle domain criterion (only a minor part of their
paper) is open to question. Yet on the basis of this
criterion, discrepancies have been claimed between
S-W theory and the experimental data, and alterna-
tive mechanisms (such as fanning) have been pro-
posed. Three independent and rather rigorous In-
restigations led to the same "micromagnetic crite-
rion", at considerable variance with S-W result.
Namely, the condition for a prolate ellipsoid of elon-
gation m (and semi -axes R, a =mR) to be single do-
main, (even in presence of an applied field). Is that
R^Rm= X ToDr- 1/2 where ro = A 1/2 Mg is an ex-
change length, /. a number of order unity and Dr the
transverse demagnetizing factor. In the S-W result
Ds figures instead of Dr. This implies considerable
difference in the linear sizes of the respective criti-
cal ellipsoids, and an even greater difference In the
critical volumes Vaw(ni)> ^i^m). Since the single
domain volume fraction of a powder plays a dcMninant
role in experimental measurements, the ratio>^ (m)"
fg^m)/vi^m) has been calculated for various values
of m. Assuming the single domain sphere to be the
sunt in both cases, and the micromagnetic criterion
to be the more correct of the two, it is found that the
S-W criterion may lead to an enormous overestimate
of the single domain content of a powder, and conse-
quently of the remanence and coercive force. To be
specific, it is found that the error ranges from 1(X)%
for m =1. 5 to much larger values as m increases.
(Audwr)
Oaeral Electric Research Lab. , Schenectady. N. Y.
APPLICATIONS OF TUNNELING TO ACTIVE
MODES, by R, N. Hall. Scientific rept. no. 2a on
Contract AF 19(604)6623. Sep 60, lip. 4 refs.
APCRL-TN-60-1I41. AD- 248 899
Order from LC mi$2. 40, ph$3. 30 PB 153 873-1
Blecrrlcal measurements of germanium recrystallized
frcm fai-Ga solutions are rep5Jrted. Acceptor concen-
trations between 1 and 2 x 10*0 cnf^ are (pund for
crystals grown from In containing 0. 5 to 1 weight per
cent Ga. TUnnel junctions from PbTe and PbS have
been prepared and studied. Low temperature electri-
cal measurements yield values for the long wavelength
longitudinal optical phonon energies in these semi-
conductors which are 16* • and 27 1 1 mllll-electron-
'olts respectively. Areas of investigation which are
•till in progress Include the preparation of crystals of
the lead salt semiconductors by vspor phase trans-
port, measurements of phonon and polaron phenomena
in the low temperature electrical characteristics of
haael junctions, the effect of linear elastic strains
upon tunneling current components, andelasto-
teilstance measurements on a variety of semi-
oowkicting materials. (Author) (See also PB 152 473)
General Electirlc Research Lab. , Schenectady, N. Y.
THEORETICAL AND EXPERIMENTAL WORK <M
PAST DIFFUSION IMPURITY ATOMS IN SEMIOC04-
OUCTORS, by E. M. Pell. Final rept. on Contract
AF 19(604)5551. I Dec 60, 12p. 4 reft. AFCRL-
TR-60-375. AI>248 593.
Order frcm LC mi$2. 40, ph$3. 30 PB 153 819
Summary of work and publications.
[General Milla, Inc. , Minneapolis, Minn. ].
INVESTIGATIONS OF BISMUTH TELLURIUM SUL-
FUR COMPOUNDS, by Henn H. Soonpaa. Tedmical
rept. no. 1 (Progress) on Contract Nonr- 1589(14).
7 Apr 6a 25p. 4 refs. Rept. no. 1940; AD- 235 354.
Order from LC mi$2. 7a pfa$4. 80 PB 154 097
Compounds of the composition Bi2(Te, 8)3 with the Te:S
ratio ranging from lOQO to 50:50 were studied. The
single phase crystalline compound, Bi2(Te, 8)3. with
the Te:S ratio from 54:46 to 62:38 was different from
the natural tetradymlte. X-ray powder diffraction pat-
terns were taken of all of the compounds prepared. A
table was compiled of the lattice constants, a and c, of
the different Bi2(Te, 8)3 compounda. A plot of the ratio
of the intensities of the 261 10 **^ 2e(X)15 Hoes vs the
compoaltion revealed a sharp minimum at a TeS ratio
alightly above 58:42, a new compound corresponding to
that composition was substantiated as BigTeySs. Two
compounds resulting from the mixture of Bl2Te3 and
Bi2S3 are believed to exist. The Hail mobilities and
electrical conductivities of the samples seem to be-
come very nearly the same at room temperature for
Bi2Te3, and the 56:44 and 58:42 compouitda.
General Telephone and Electronics Labs. ,
Bayside, N. Y.
ANALYSIS OF TRACE IMPURITIES IN SILICON
CARBIDB, by R. Rupp and G. Morrison. Final rept.
for 1 Nov 58-31 Oct 60 on Contract AF 19(604)4944.
31 Oa 60, 27p. 3 refs. TR 60-703. 9; AFCRL-TR-
60-357; AD- 248 258.
Order from LC ml$2. 7a ph$4 80 FB 153 682
Trace spectrographic techniques that are 2 to 3
orders of magnitude more sensitive than previous
methods have been developed. The knowledge ob-
tained has been Instrumental in the development of
three direct spectrographic methods for the determi-
nation of ultratrace impurities in high purity silicon
carbide and nickel, atxl for the determination of
traces of boron In silicon. A technical manual de-
scribing the procedure for the determination of im-
purities in silicon carbide is included. (Author)
Illinois U. , Urbana.
SELF DIFFUSION IN SILVER DURING PLASTIC
DEFORMATION IN TORSKW, by J. B. D»rt)y, Jr.
(Argonne National Lab.) C. T. Tomizuka (U. of Arizona)
and R. W. Balluffl. Rept. on Contract AF 49(638)880.
20 Dec 60. 35p. 13 refs. AFOSR-TN-60-1394.
Order from LC mi$3. Oa ph$6. 30 PB 153 899
Self- diffusion of Agl 10 in polycrysuls subjected to
simultaneous torsion was studied at 700 aivl'^8(X)^C
using the sectioning technique. The effects of straining
on diffuaion were relatively small in all cases.
627
tlllnoii U., UtUna.
A STUDY OF U)W TEMPERATURE RECOVERY OF
ELECTRICAL RESISTANCE IN COLD WORKED
COPPER CRYSTALS, by J. H. Bredt (Doctoral thetli)
anri J S. KoehJer. Technical rept. no. 2 on Contract
[Nloor- 1834(26). Feb 60. 94p. 39 refs^ AD-232 831.
OitJerfromLCmi$5.40. ph»l5.30 PB 153 138
Efforts were made to clarify the general aspects d the
behavior at point defects in the face- centered cubic
metals by sttidylng low -temperature recovery of elec-
trical resistance in cold worked Cu crystals . The
electrical resistance at every specimen actuaUy used
In the experiment was measured in a bath of liquid He.
The annealing al 99.998% pure Cu single crystals de-
formed In compression at 780K waa exceedingly com-
plex. The deiaias at the resistance recovery depended
on the exact naoire of thermal history; this dependence
extended at least as low as 7dPK.. The acUvation ener-
gies of the effective annealing processes appeared to
be distributed ipore or less continuously over a range
of approximately 0.2 to 0. 8 ev . Identification d sped
fie values was made ambiguous by the complex struc-
ture of the annealing spectrum. An attempt was made
to account for the complicated behavior produced by
complexities in the kinetic behavior of large , dense
aggregates of interstiUal atoms caused by the
deformation.
Illinois U. . Utbana.
VACANCY QUBNCHING IN GOLD (I) by Hlroshl
Pujlwara. Techsiical rept. on Contract Nonr- 1834(12).
(I960] 20p. 14 tefs. AD- 233 129.
Older from LC ml$2. 40. ph$3. 30 P8 153 772
The variations of concentrations of single and divacan-
des in gold durtng rapid linear quenching (<jjenching
rate 3 x lO^^C/sec) are quantiutlvely obtained over
the ranges from quenching temperature to room tem-
perature. In this paper, we assume that (i) only the
single and dlvacancies play a role during q^ienchlng
and annealing, (ii) total void concentration is constant
during quenching. The cases in wWch the q^ienching
temperature Tq -700OC. 800OC and 900PC for etch
case the bindinf energy of a divacancy is B =«0. 1. 0. 2
and a 3 e. y. a^e treated. Tbe results show that the
concentration of single vacancies decreases with tem-
perature and approaches a limiting value character-
istic of Tq and B near room temperature. If one as-
sumes that all dlvacancies produced during quenching
reach dialocati^ during quenching, then the fractions
of the expected resistance increase which is loat for
the case of T^ r SOOOC. are 2%. 18%, and 47% corre-
sponding to the cases of B - 0. I. 0. 2, and 0. 3 e. v.
respectively. Thermal equilibrium of the vacanci«i
I>reaks at certain temperature, from 500PC to 3O0PC
corresponding to each case. The value c# B must
therefore be n«ar 0. 1 e v. (Author)
nitnols U. [Btglneering Experiment Sution]
Urbana.
A STUDY OF THE ALLOYS OF TRANSITION ELE-
MENTS, by Paul A. Beck. Rept. for 6 Aug 56-
14 Ai« 60 on Sdlld State Research and Properties d
Matter, Contracts AF 33(616)3789 and AF 33(616)6770.
Dec 60. 17p. 12 refs. ARL Technical rept. 60-326.
Order from OTS $0. 50 PB 171 1 13
Correlation of the occurrence of various Intermediate
phases in alloys of transition elements with thelocatica
of these elements in the periodic table suggests a
strong effect of the electronic structure. Measure-
ment at the electronic specific heat in body centered
cubic alloys in the systems Tl-V, V-Cr, Cr-Fe,
Fe-Co. Cr-Mn and V-Fe lead to information regarding
the shape of the 3d band. (Author)
InaUtute at Optica, U. of Rochester, N. Y.
LUMINESCENCE OF MDCED ALKALI HALIDE
CRYSTALS, by D Dutton and K. Teegarden. Final
rept. for 1 Aug 58-31 July 60 on Contract DA 30-115-
ORD-998. [1960] 4p. 1 ref. OOR rept. 2045. 3-P;
AD- 243 75a
Order from LCml$l. 8ft ph$l. 80 PB 153 670
A method has been developed for measuring the con-
centration of iodide Ion in KQ:! crystals, utilizing the
characteristic absorption band of the I' loo In water
solution. Iodide ion concentrations of 10^5 cm-3 cm
be determined in this way in the presence of 1020 Q"
iona/cm3. The lower limit of the method is set by die
overlap of the CI* band with the iodide band at 2500 A
The exciutlon and emission spectra of a KQ cry^al
conuining about 0. 01 per cent KI have been investi-
gated using the vacuum monochromator. No lumines-
cence occurs at room temperature. At 80° K excita-
tion bands occur at 6. 73 and 7. 18 ev; these correspond
to the iodide ion abaorption bands. The 7. 18 ev
absorption band appears on the "tall" of the KCl ab-
sorption edge, but is quite distinct in the excitation
spectrum. An additional excitation band is observed
at 7. 6 ev. This is well within the strong-absorption
region of KQ. ExdtaUon In any of these bands gives
rise to a broad emission band peaking at 3. 06 ev. In
nominally pure KCl, at 80° K there is an excitation
band at 7. 6 ev. The observations have been repeated
on additional samples of KQ and KQ:! with the same
qualitative results. (Author)
Laboratory for Insulation Research. Mass. Inst, cf
Ttech. , Cambridge.
INTERACTION OF A POLAREABLE POTASSIUM
CHLORIDE CRYSTAL WITH A VALENCE- BAND
HOLE, by Slephen J. Nettel. Rept. on Contract
Nonr- 1841(10). Mar 60, 52p. 25 refs. Technical rejt
146; AD- 235 468.
Order from LC ml$3. 60, ph|9. 30 PB 153 741
The Interaction of a valence-band hole wltha potassium
chloride crystal, when crystal-hole correlations are
considered, is studied by variational means. A
crystal trial wave function is constructed which
allows for the iaiic polarizability of the crystal by
means of a correlation between the crystal configu-
ration and the motion of the hole. The expectation
value of the Hamiltonian operator for the crystal is
found by integrating over both electronic and nuclear
coordinates. The necessary matrix elements of the
electronic energy operators are taken from aprevkJUl
calculation by Howland (Phys. Rev. 109:1927, 1958X
The toul energy expectation is minimized with re-
spect to a sij^le parameter in the wave function that
measures the hole- lattice correlation. The valence
bands obtained when the crystal lattice is treated as
rigid become completely flat; a result which implies
628
tiHi die hole Is self- trapped. The roodlficatkxi that
are introduced by the addition of the elearonicpolariz -
ilifltty are studied by repeating the previous calcu-
lation with a refined wave funaion. Consideration it
, given to the energy bandwidths when the electronic but
■ttke ionic polarizability is active, since these may
be compared with experlmenul widths derived from
X-ray emission spectra. (Author)
Lincoln Lab. , Mass. Inst, of Tech. . Lexington.
ANISOTROPY IN NICKEL -IRON FILMS, by
D. 0. Smith. Rept. on Contract AF 19(604)7400.
2 Dec 60. 40p. 48 refs. 53G-0047; AD- 247 895.
Order from LC mi$3. 00, ph$6. 30 PB 153 563
The magnetic and optical aniaotroples of evaporated
nickel-Iron films deposited at an angle to the substrate
nmnal are sensitive to the rate of deposition and the
orieotadon of the nugnetization M during deposition,
k is postulated that crystallite elongation toward the
vapor beam or in the direction of M occurs.
Lincoln Lab. . Mass. Inst, of Tech. . Lexiiigton.
CLASSICAL THEORY OF THE GROUND SPIN -STATE
IN SPINELS, byT A. Kaplan, K. Dwlght and others.
Kept, on Contract AF 19(604)7400. 7 Dec 60. 30p.
26 refs. 53G-0043; AD- 248 364.
Order from LC ml$2. 70, ph$4. 80 PB 153 699
An investigation of the ground state of the classical
Hdsenberg exchange enei^ in spinels has led to sev-
eral new results. By means of a recent generalization
of the method of Luttinger and Tlsza, the ground state
has been rigorously obtained in the part of the ex-
diange parameter space defined by nearest neighbor
AB and BB interactions for tetragonally distorted spi-
nels. The regions In this space where the Neel and
Ytfet-Klttel configurations mltiimize the energy are
much smaller than predicted by the Yafet-Klttel six-
Mblattice theory. Outside of these regions, there ex-
iats a domain where the ground state is an antlferro-
mgnetic spiral similar to those recently introduced
ll the literature. In still other regions, the ground
state is a new type of spiral which is ferrlmagnetic.
(Audior)
Metals Research Lab. , Brown U.. Providence, R.I.
™E RELATION BETWEEN THE PLASTIC DEFOR-
MATION OF ALUMINUM SINGLE CRYSTALS AND
POLYCRYSTALS. by Stephen Howe and Charles
Elbaum. Final rept. on Contracts Nonr-562(12) and
Nonr-562(27). I May 60, 29p. 9 refs. AD- 238 992.
Order from LC mi$2. 70, ph$4. 80 PB 148 559
Stogie crysuls of <I00>. <lll>. and <1I0> axial
orienution, and polycrystals. both of 99.99% pure
•taminum, were deformed in tension at temperatures
ofZTOC. 200OC. 400OC and 6000c. The experiments
* **le crystals reveal that as the temperature is
tocreaaed. the shear stress -shear strain curves for
4e three orientations become more and more similar
latll at 600OC they are identical. On the other hand
the surface appearance of the crystals strained at
MOSC indicates that the mode of deformation depends
•Irtstically on orientation. Taylor's criterion for the
comparison of the stress -strain curves of single and
PoJycrystals was found to be valid at 270C. As the
temperature is raised, however, the criterion ceases
K> he applicable.
Microwave Research Inst. , Polytechnic Inat. of
Brooklyn, N Y
TRANSMISSION LINE FORMULATION FOR SEMI-
CONDUCTORS, by P. Parzen. Rept. on Contract
DA 36-039-SC-73052. 12 Mar 59. 84p. 13 refs. Re-
search rept. R -712-58; PIB-640; AD-218 374.
Order from LC mi$4. 80, pb|13. 80 PB 153 932
In the tranamlssion line method of band structure, the
crystal is divided into periodically displaced regions
bounded by crysul planes passing through atomic
sites, which contain subregions with almoet constant
potential. The Schroedinger equation is solved in the
subregions in terms of incident and scanered plane
wavea satisfying proper Bloch conditions in direaions
parallel to the crysul planes. The incident and scat-
tered waves are related via the scattering of an elec-
tron wave by the 2-dlmen8ional lattice of a crystal
plane. The plane wave amplitudes are constrained to
satisfy the Bloch condition along a lattice direction not
parallel to the crystal planes, thereby determining
energy as a funaion of wave number. Different atoms
per unit cell require the solution of appropriate scat-
tering problems which may be tabulated and used to
compute the band structure of solids built up of arbi-
trary crystal planes. The symmetry properties in-
duced by the symmetry operations (rf the two dimen-
sional lattices in the crystal plane are determined.
Detailed computations for U are given. (Author) (See
also PB 146 454)
Naval Ordnance Lab. , 'White Oak. Md.
A SURVEY OF BASIC RESEARCH IN THERMO-
ELECTRICITY, by Wayne W. Scanlon. 1 June 59.
14p. 25 refs. NAVORD rept. 6663; AD-220 241 .
Order from LCinl$2. 40, ph|3. 30 PB 154 770
This report released for sale to the public 15 Mar 61 .
The present status of research in the general area d
tfiermoelectrldty was surveyed for the purpose of
evaluating the present understanding of the phenomena
and to point out areas where additional knowledge is
needed. Thermoelectric effects were considered in
metals and Insulators as well as In semiconduaors.
As a result of this study it is apparent that even in the
simplest monatomic metals such as the alkali metals.
the theory is unable to account qualitatively or quanti-
utlvely for the observed behavior. Wide discrepan-
cies are found In some of the meuls which are gen-
erally believed to apis-oxlmate closely the ideal free
electron behavior. (Author)
Ohio State U. Research Foundation, Columbus.
AMPLITUreS OF VIBRATION AND X-RAY SCAT-
TERING OF CRY^ALUNE UTHIUM HYDRIE^
AND LITHIUM E^EUTERICC: 300°K TO 20OK, by .
C. K. Stambaugh and P. M. Harris. Technical rept.
no. 2 on Order -Disorder Transformations In Crystals,
Contract N6onr-225- 17. Jan 53, 52p. 30 refs.
AD-10 920.
Order from LCmI$3. 60, ph$9. 30 PB 154 807
This report released for sale to the public 17 Mar 6l.
Intensities of Laue-Bragg scattering from powdered
crysuls of LiH and LiD were obtained at 2CP, 77°,
1940, and 303°K with a recording G-M counter apec-
629
trometer and 4 special Dewar specimen mount. Rela-
tive crystal- structure factors and relative atomic
torm factors w»cre calculated from the intensities; ab-
solute atomic form faaors and characteristic tem-
peratures were obtained from the relative form-factor
values. Temperature coefficients and amplitude! of
Tlbraticn were calculated from the characteristic tem-
peratures. Electroo-denaity distributions for LIH,
dxained from the absolute atomic-form-factor data,
were used to calculate radial charge distributions.
Evidence was discovered which suggested a change in
tlie Ionization wate of the crystals with changes in
temperature.
Ohio State U. Research Foundation. Columbus.
A THEORETICAL STUDY OF THE SIMULTANEOUS
DIFFUSION OP TWO IMPURITIES INTO SILICON
THROUGH AN OXIDE LAYER, AND THE DIFFU-
aON OF BORON INTO SILICON THROUGH DIOX-
IDE FOR a OOl PER CBKT SOURCE STRENGTH
OF BORON, by M. O. Thurston, J. Tsai. and
K. D Kang. Quarterly technical rept. no. 6, 1 Apr-
30 June 60, on Diffusion of Impurilies Into Silicon
Through an Ontide Layer, Contract DA 36-039-»c-
83874. 2 Aug 60. 26p. Rept. 896-6; AD-244 694
OixJer from Lp inl$2. 7a ph»4. 80 « 153 603
A theoretical study of the simultaneous diffuaioo of
two impuritiea Into silicon through an Initial aside
layer to prodiice junction transistors is given in the
first part of tkis report. Relations among the diffu-
sion time and impurity surface concentrations are
given in terma of initial (xide Uyer thickness. R's
and the junction depths. As a speciAl case, the thin
base layer is considered. Possible design procedure!
are suggested No experimental data were obtained.
Experimental results at boron diffusion from a 0.001
per cent source are given in the second part of this
report. It way observed that the saturated lurtace
concentration has nearly a conaunt value and is
higher than the source concentration. This suggests
that at low ao^rce strength the saturated surftce
concentration may be independent of source strength.
It was suggested that there may be a segregation
phenomenon af. the silicon -cotide interface. On the
oatide aide at the interface boron has a slighUyhigher
coocentration than on the ailicon side. (Author)
Raytheon Co., Waltham. Mass.
RESEARCH STUDIES AND INVESTIGATIONS OF
THE SOLID STATE CHEMISTRY OF FERRITES, by
A. E. Paladiio. Jr. Final rept. for 15 Jan 58-15 Jan 59
on Contract D|A 36-039-8C-74987. [1959] 58p. 26 rcfs.
AD-213 430. ,
Order from L(C mi$3.60, ph>9. 30 PB 153 238
Phase equilib^a in the systems Fe-Nl-0 and Fe-Mg-0
have been investigated in the ferrite regions up to a
temperature of 1300<H:. A "vacuum" technique for ^
determining equilibria relationships in these systerrts
is described and data are reported for oxygen pres-
sures from one to 0.01 atnKJspheres ^ DC resistivity
measurement* have been made cm NiftxFeJ*Fej*D^,
where x variqd from 0 to 1 . (Author)
(See also PB 1137 195)
Rome Air Development Center. Grlffiss AFB. N. Y.
CERTAIN PHYSICAL PROPERTIES OF SOME INTBl-
METALUC COMPOUNDS OF Mn AND As , by
Josqjh B. Brauer. Oct 60. 60p. 30 refs . RADC-TR-
60-165: AD- 246 806.
Order from LCml$3. 60. p»49. 30 PB 153 264
The system Mn-As Is representative of a series of bi-
nary systems consisting of a transition metal and one
of the sub-group elentients . Most of these systems art
characterized by a number of definite intermetallic
compounds and present complex phase diagrams. Ua-
usual electrical and magnetic behavior of the com-
pounds and alloys in the Mn-As system and conflictin
dau reported by previous Investigators led to this
study of certain compositions within the range of 30 to
50 atomic percent arsenic . Alloys were prepared wlife
composition near that of the reported compounds
MnAs, Mn4As3. Mn3A82. «nd Mn2As . Two alloys oa
either side of me composition erf Mn3As2 were sub-
jected to dllatometrlc measurements; electrical resli-
tlvity measurements were made on the alloy approod-
mating Mn4As3; and all alloys were studied using
metallographic and X-ray diffraction techniques . Ex-
pansion and electrical resiitivity vs . temperature
curves are discussed, correlations o< the X-ray pow-
der diffraction patterns are described and photomicro-
graphs of the various alloy structures are presented.
(Author)
Synthetic Mica Co. , Caldwell, N. J.
SYNTHETIC MICA CRYSTAL GROWTH PROGRAM,
by John G. Froemel, Edgar C. Worden, and Philip S.
Hessinger. Interim technical eyigineering rept. no. 1,
16 May- 16 Aug 58, on Contract AF 33(600)36853.
[1958] 96p. 241 refs. AD- 205 707.
Order fromLCml$5.40, ph$15.30 PB 154 515
This report released for sale to the public 2 Mar 61.
Method* are being developed for growth d large
(4 * X 6") aynthetic mica crystals on a conunercial
scale. Special furnacing techniques are being evalu-
ated on an In-plant basis including progressive (step)
melting, controlled cooling schedules, seeding meth-
ods and melt super heating. In the laboratory, spedsl
crystal growing techniques such as zone melting,
crystal pulling and thermal gradient crystanizatioo
are under study on both mica melt and solutions. Tte
report describes the first plant scale progressive
melt, composition control experiments, and other
preliminary studies. Mica crystal growth theory is
discussed, and the initial design of a laboratory crys-
tal growing apparatus is presented. The experinteaisl
work being conducted on solution growth is described
aixl a comprehenaive MbUography of synthetic mica
references is Included.
Utah U. , Salt Lake Qty.
HIGH PRESSURE PHYSICS, by P. Gibba, G. S Brta
and others. Rept. on Solid Sute Research and
Properties of Matter, Contract AF 33(616)5016.
Dec 60. 47p. 11 refs. ARL Technical rept. 60-330.
Order from OTS $1. 25 PB 171 0«
630
An apparatus for producing and measuring pressures
ID 20, 000 atmospheres using a liquid or a gas en-
vironment has been constructed and tested. The
pressure chamber has a working space 1 Inch In di-
ameter and 4 inches lone and is designed for use with
iBtemal heating to 1000°C. A new type plug has been
designed and tested allowing 8 electrical leads to be
Irought into the pressure chamber. A torsional
paxkilum for measuring internal friction inside the
pressure vessel has been constructed andinstru-
BOCed. Damping measurements on '^. 06 Inch di-
■neter wire specimens can be made over a strain
amplitude range of £ - 10'^ to 10'^. Provision is
made for an Internal furnace heating the specimen
over a wide temperature range. A creep apparatus
has been construaed and tested. Preliminary re-
Ittltf on tin have shown a definite slowing down of
creep due to the application at pressure. An acti-
vation volume for the process is estimated. (Author)
Theoretical Physics
Ckm^ie Inst, at Ttech. , Pittsburgh, Pa.
ATOMIC LINE SHAPES FROM A PLASMA, by
Bernard Mozer. Technical rept. no. 3 on Contract
Nonr-760(15). [1960] 208p. 47 refs. AD- 237 043.
Order from LC mi$9. 30, ph$31. 80 PB 147 748
Several line shapes emitted by atoms in a plasma were
calculated. The free ions and electrons in the gas ,
which are responsible for broadening and shifting the
emitted radiation are considered to be classical parti-
cles. The simultaneous effect of these perturbers on
tbe emitting atom is treated by considering the ions in
the stttic approximation and the electrons in the im-
pact approximation. Strict regard is paid to the va-
lUlty at these approximations. The line shapes are
calculated by a method which assumes that the sutic
tonic electric field splits the line into its Stark com-
ponents. The impact electrons then broaden each
ccmponent causing them to overlap. Th"" resulting
line shape is obtained by averaging the broadened,
overlapping Stark components over all ionic fields
multiplied by an appropriate distribution. A theory of
impact -broadened overlapping lines developed byKolb
•as used to calculate the effect at the electrons. New
tonic field distributions which are important for hydro-
fen line shapes were calculated by a new method
•Wdi Included the correlations between the charged
particles in the gas. A calculated Balmer fi line shape
•as ta close agreement with a recent precise measure-
ment. The close agreement between these results
emphasizes the Importance o^ the electrons Indl-
realy broadening the Stark components and indirectly
nodlfying the ionic field distribution. (Author)
Btoctronics Research Lab. . U . at California,
Berkeley.
KXTRACnCW AND MODULATICW OF ELECTRON
"BAM PROM PHlUPS ION GAGE, by R. E.
LuBdgren. Scientific rept. no. 9 on Contract
AP 19(604)2270. 31 Aug 60, 74p. 23 refs . lER series
no. 60, issue no. 306; AFCRL-TN-60- 1100: AD-247 432.
Order from LCml$4. 50, pKl2. 30 PB 153 488
A cold-cathode electron source Is investigated in an
extension of the work done by Savarin in which an elec-
trode structure similar to that of the Philips Ion Gage
Is used to generate a low pressure plasma from which
a beam of electrons is extracted. In the present work
the electron beam is modulated by varying the density
of the plasma through control ot the appropriate elec-
trode volwges . Measurements were nsde to deter-
mine the extracted electron beam current as functions
of magnetic field, gas pressure, and the several elec-
trode voltages . Both dc and pulsed measurements are
diescnbed. ^jecial attenticm is paid to the properties
of the device when the two cathodes are at diflterent
potentials , and some proof is presented for a theory
expUining the negatlve-resisunce characteristics of
the asymmetrical Philips Ion Gage. The emission
efficiencies obtained for pulsed operation were com-
parable with those for a pure tungsten thermionic cath-
ode, the maximum measured being 7.2 ma/w. Al-
though insununeous emission efficiencies are low,
the average emission efficiency may be higher than
even that of an oxide-coated cathode for pulsed opera-
tion because of the necessity of supplying heatii^
power to a thermionic cathode during the time be-
tween pulses . (Author)
Free U. of Berlin (West Germany).
A DERIVATION OF BOLTZMANN EQUATION WITH
THE HELP OF AN ASSUMPTION OF DETERMI-
NACY, by GDntber Ludwig. Technical rept. no. 1 on
Theoretical Research Studies of Reacting Plasmas,
Contract AF 61(052)239. [1960J 35p. AFOSR-
TN-60-1405; AD-246 970.
Order from LC mi$3. 00, ph|6. 30 PB 153 311
Institute of Mathematical Sciences, New York U. ,
N. Y
THE GREEN'S FUNCTION METHOD FOR QUANTUM
CORRECTIONS TO THE THOMAS- FERMI MODEL
OF THE ATOM, by Gene A . Baraff and Sidney
Borowitz. Rept. on Contracts AF 19(604)4555. DA 30-
069-ORD-2581, and Nonr- 285(49). Aug 60, 37p.
12 refs. Research rept. no. CX-50; AFCRC TN-
60-464 [sic).
Order from LC rai$3. 00, ph$6. 30 PB 150 946
A systematic method is presented for deriving the
Thomas- Fermi equation for an atom and the quantum
corrections from the many body description. The
novel feature of the method is that it does not require
any a priori assumptions about the distribution of the
electrons in phase space but shows instead that the
distribution which is usually assumed is a direct con-
sequence of specifying that the many panicle system
is In its ground state. The procedure used in the
derivation is the expansion of the mixed position-
momentum representation of the Green's function in a
series of powers of h. The lowest order term is found
to correspond with the Thomas-Fermi density. The
form of the higher order terms, which are to be con-
sidered as corrections to zeroth order term, depends
OTi the approximations made in the many body equa-
tions for obtaining the Green's function. This paper
deals only with the Hartree-Fock a{>proximation, but
the methods presented here allow generalization to
631
other approximation* which can Include correUtioa
effects. (Auth
It her)
bjstliute d T^ch- , U. dl Minnesota, MinneapoUs.
C«LAY- DIFFERENTIAL EQUATIONS AND AN
APPUCATION TO A TWO- BODY PROBLEM OF
CLASSICAL ELECTRODYNAMICS, by Rodney R
Driver, Technical rept. for 16 June- 15 Aug 60 on
Problems in tha Theory at Ordinary Differential and
Deference Equations, Contract DA 11-022-ORD-3369.
July 60, 6^ llrefa. OOR rept. 2560.1-M;
AD- 243 177. J
Order from Lq nil$3.90, phfiaSO PB 153 679
A system at delay -differential equations is considered.
The equations (Jescribe the variation with time of an
n -tuple, the derivative d each component at each n-
tuple being dependent upon the n- tuple itself as well
as time and some delay fimctloos. The question con-
sidered is: what initial data is sufficient for a system
of delay-dlfferwtial equations in order that the prob-
lem al predicting the future will be well set? (Author)
Institute of Tlieoretical Physics. Sunford U. , Calif.
NEUTRCW- PROTON PAIRING INTERACTION, by
A. N. Saxena. Technical note no. 26 on Contract
AP 49<63«)388 Aug 60. 19p. 15 refs. AFOSR-
TN- 60- 11 33; AD- 246 634. „. .„ .„^
Order frxxn LG ml$2. 40. ph$3. 30 PB 153 186
■Die neutron- pBoton pairing Interaction A between the
last odd neutrcti and the last odd proton In the outer-
moat neutron «id proton shells of a nucleus has been
estimated in the regions Z >20. N > 20 and Z :> 40.
N :» 50 Behavior of i In these two regions and in the
heavy nuclei r^on Z > 82. N > 126, as estimated by
Gbothal and Staena, is discussed. Also, it Is shown
that X arises due to the Wlgner force and it is pro-
portional to (2ji* l-2z) (2j2 ♦ l-2n). where z Is the odd
number of protons in the n.itermost proton shell jj.
and n Is the odH number of neutrons In the gytgpTiost
neutron shell J^ of the odd-odd nucleus. <Au*
Institute of Tfceoretlcal Astrophysics , U . of Oslo
(Norway)
ON Plj^NE STiATIONARY SHOCK WAVES IN A
PLASMA , by IQell V^yenll . Scientific rept . no . 3 on
Contract AF 61(052)49. 1959. 85p. 25 refs.
AF06R TN-601-424; AD-236 337.
OrderfromLCmi$4.80, ph$13.80 PB 152 656
Equations for plane stationary shocks in a plasma are
developed from a general continuum description of a
fully ionized pliasnu consisting erf one type of ions and
electrons . Th« shock equations are independent of the
viscosity and the thermal and electric conductivity of
the plasma . When the magnetic field and the flow
velocity are perpendicular to the shock front , the equa-
tions are redu<;ed to the familiar form for an ordinary
gas . When the, magnetic field is parallel to the shock
front ("parallel shock"), there is a strong formal anal
ogy with the ncr - nnagnetic case. Several important re
suits may consequently be transferred directly from
the theory q^ shocks for ordinary gases . The general
case is considered where the magnetic field forms an
arbitrary anglf with the shock front ("oblique shock").
The magnetic field loses Its importance for the motifli
when the shock is strong, and a weak shock may be
considered as a parallel shock.
Institute of Theoretical Physics, Stanford U. , Oallf.
PION PARAMETERS FROM HIGH ENERGY IN-
ELASTIC INTERACTIONS, by & D Drell. Technics
note no. 25 on Contract AF 49(638)388. Aug 60. lip.
7 refs. AFOSR-TN-60-1134; AD-246 633.
Order from LC mi$2. 40. ph$3. 30 PB 153 185
The physical principle that a transition amplitude has
a pole for real one-particle Intermediate states isap-
plied to various experimental arrangements in order
to check their quantitative content and to determine
plon interaction constants.
Institute of Theoretical Physics. Stanford U. . Calif.
SPECTRA OF ODD-ODD NUCLEI, by A.deShalit and
J. D- Walecka. Technical note no. 24 on Contract
AF 49(638)388. Aug 6a 39p. 19 refs. AFOSR-TN-
60-1137; AD-246 632.
Order frocn LC mi$3. 00. ph$6. 30 PB 153 189
A general discussion of the spectra of odd-odd nuclei
is presented. For this purpose it was found useful to
develop a new method for the calculation of energy
levels. An explicit expression is derived for the dis-
tribution of the relative angle of the two panicles,
properly weighted according to the spin -dependence of
the Interaction. With the help of these expressions the
general structure of spectra of odd-odd nuclei can be
more clearly seen. In particular the modified Nord-
helm rules are seen to hold quite generally, and it Is
found that for configurations containing a half-filled
shell the lowest state has an even or odd J accordinf
to whether its parity is odd or even. (Author)
Lockheed Aircraft Corp . Sunnyvale, Calif.
A SELF -CONSISTENT FIELD THEORY OF QUAN-
TUM ELECTRODYNAMICS, by Mendel Sachs and
Solomon L. Schwebel. Technical repc. on Physics.
May 60. 5lp. 16 refs. LMSD-288254; AD-244 204.
Order from OTS $1. 50 . PB 171 533
A self -consistent field theory of quantum electro-
dynamics is developed which Is based on the postulate
that the laws of nature must be described In terms of
field variables which may be associated only with
elementary interactions. Coupled with this postulate
is a relnterpretation and reformulation of the Max-
well-Lorentz theory of electromagnetism. The theory
is deterministic and Is a field theory in the tradition
of Einstein and Maxwell. Quantum mechanics is in-
terpreted as a statistical theory of elementary in-
teractions. One consequence of this theory is the
rejection of the photon as an elementary particle and
Its replacement by a state of the particle -antlpartick
pair. The concept of a particle acting on itself ha*
no meaning in the present theory. An application of
the theory to a system of identical particles reveal*
mathematical consequences which are identical to
those obtained from the Paull exclusion principle. A
study made of posltronlum reveals in detail the
structure of the theory. Annihilation and creation
processes of partlcle-antlpanicle pairs are shown
to be states of this rwo-particle system. (Author)
632
Maryland U. , College Park.
ANALYTICITY IN THE COUPLING CONSTANT
AND BOUND STATES IN POTENTIAL THEORY, by
I. Boaco (Brookhaven h4atlonal Lab. ) and J. Sucher.
[Btpt. on Contract AF 49(638)24) Nov 60. Up.
9 refs. Dept of Physics Technical rept. no. 199;
(AFOSRJ TN-60-1434; AD-248 970.
Orier from LC ml$2. 40. ph$3. 30 PB 153 872
A method for determining the wave function In poten-
dsl acanerlng. from the S- matrix, using unitarity
and analyticity. is extended to the case where bound
itstes are present by using analytic continuation in
III* coupling constant. A numerical example Isglven,
Illustrating the passage of a pole from the second
lUemann sheet of the energy to the first sheet.
(Audior)
Pferke Mathematical Labs.. Inc.. Carlisle. Mass.
ON THE EVALUATION OF FEYNMAN PATH
NTECRALS. by Fazil Erdogan. Scientific rept. no. 1
onContraaAF 19(604)7316. 20 Sep 60. 48p. ISrefs.
AFCRL-TN-60-1109. AD-246 923
Order from LC mi$3. 30, ph$7. 80 PB 153 282
After a technical description of the Feynman path
integral formulation of quantum mechanics the report
trM* several praaical methods of evaluating path
integrals: (1) parameterization by means of
orthonormal functions, with examples. (2) approxl-
mstlon by n-parameter family of curves. The deter-
mination of normalizing factors is treated, with
illuatrative examples. Energy eigenvalues and a
quasi -classical approximation are treated In terms
of path integrals. A first crude step is taken toward
a feometrization of quantum mechanics in terms of
path Integrals in action space. (Author)
Pennsylvania State U. . University Park.
AN INVESTIGATION OF THE MACROSCOPIC EQUA-
TIONS FOR A PLASMA, by H. U and R. D. Mathieu.
Technical rept. no. 13 on Contract AF 49(638)647.
May 60. 35p. 13 refs. AFOSR-TN-60-1070.
Drier from LC mi$ 3.00, ph*6. 30 PB 153 432
The macroscopic equations for the conservation of
mail, momentum, and energy, which are deduced
from the particle viewpoint by using the classical
Boltzmann equation, are investigated (or both a non-
reacting plasma and a reacting plasma. The nK>$t gen-
eral form of these equations is presented for variable
material constants. I.e. dielectric constant and mag-
netic permeability. The resulting equations are com-
pired with equations which have been obtained from
the continuum viewpoint of a cwtrol volume and a con-
trol surface for the plasma . (Author)
^set, E. H., Associates, Inc., Los Angeles,
Calif.
COLLISION CROSS SECTIONS THEORY AND PRAC-
TICE, FORMAL THEORY FOR MSTINGUISHABLE
SPWLESS PARTICLES, by Edward Gerjuoy. Scientific
rept. no. 2 on Contract AF 19(604)6187. 17 Oct 60r
% C25-60(U)43: TR-104; AFCRL-TN-60-1153.
*der from LC mi$3.00, phJ6J0 PB 153 499
A rerlew is given of the formal theory used to com-
pute reaction rates resulting from arbitrarily com-
plicated collisions between "aggregates" of spinless
distinguishable particles, with special reference to
atomic and molecular collisions of interest in Air
Force problems. This restricted theory serves as an
introduction to the more realistic and more compli-
cated case of collisions between systems of indistin-
guishable particles possessing spin. (Author)
Stevens Inst, of Tech. , Hoboken. N. J.
INVESTIGATION OF PLASMA ACCQ,E RATION, by
K. C. Rogers. D. Flnkelstein, and G. Brucker.
Semi-annual progress rept. no. 7, 1 Jan- 10 Sep 60,
on Megatron Acceleration, Cootract DA 36-039-BC-
78097. [1960] 71p. 8 refs. SIT P-2l(10/30);
AD- 245 936.
Order from LC nU$4. 50, ph$12. 30 PB 153 934
Experimental and theoretical results on pulsed mag-
netic field shaping and high-voltage, high-current
switching are summarized. Work on plasma betatron
theory and plasma injection into plasma betatrons is
discussed. (Author)
Thermod)rna m ics
Aeronautical Research Lab. . Air Force Research
t5iv., Wr ight- Patter son AFB, Ohio.
EXPERIMENTAL STUDIES ON THE INTERACTION
OF STRONG SOUND FIELDS WITH FREE CONVEC-
TION BOUNDARY LAYERS, by E. E. Soehngen and
J. P. Holman (Southern Methodist U.). Oct 60. 79p.
108 refs. ARL Technical rept. 60-323; AD-249 104.
Order from OTS $2.00 PB 171 485
Experiments have been conducted on the interaction of
strong sound fields with free convection boundary
layers on horizontal heated cyhnders of 0. 750-inch
diameter. The Interaction effects were observed
throu^ the measurements of the total heat transfer
from the cylinders to air under the Influence of dlf-
ferent'types of sound environments. Three different
types of sound fields were employed for the experi-
ments: (1) Standing plane waves generated by loud-
speakers In an anechoic chamber; (2) Traveling plane
wave fields generated by a mechanical siren In an
anechoic duct; and (3) Constant pressure or diffuse
sound fields generated by a mechanical siren in a
reverberant chamber. In all cases the generated
sound was monochromatic. The frequencies covered
a range from approximately 1000 to 6000 cps at sound
intensities ranging from 0 to 152 DB. The tempera-
ture difference between the test cylinder and air was
varied between 20 to 2500F.. (Aurtior)
Massachusetts Inst, of Tech., Cambridge.
UQUID AND GAS DISTRIBUTION IN THE TWO-
PHASE BOILING ANALOGY, by Graham B. WalUa and
Peter Griffith. Technical rept. no. 13 on Contraaa
N5orl -07894 and Nonr- 1848(39) [slcl. 1 Dec 58. 89p.
AD-209 391.
Order from LC ml$4. 80, ph$l3. 80 PB 154 967
633
Thit report re eased for sale to the public 17 Mar 61 .
This report contains a description at the design and
operation erf an experimental apparatus for the analy-
sts of iwo-phafe flows similar to those occurring in
bailer tubes ati low pressures. Velocity and density
profiles erf air -water mixtures are determined across
a passage in which boiling conditions are simulated by
pumping air through porous walls into a water stream.
Photographs erf. the flow patterns are also presented as
a qualitative c|eck on the quantitative dau. The re-
sults obtained Bre: (1) Velocity and concentration pro-
files of the twq phases for various values of the flow
rates of each. ' (2) A classification of the flow into
several patter^is or regimes with quaotiMtive dau de-
scribing each Regime. The data is suitablerfor use in
comparing the physical phenomena with mathematical
models and fot developing a more accurate theoretical
treatment of the flow of boiling fluids in heated
channels. (Author)
Massachusetts Inst, of Tech. , Cambridge.
MEASUREMEKTS OF THE THERMAL CONDUC-
TIVITIES OF GASES AT HIGH TEMPERATURES,
by Robert G. i^ines Rept. on Contraa Nonr- 1858(25)
Sep 58. 20p. 12 refs. Proj. Squid Technical rept.
MIT-20-P; ADh205 694.
Order from Lp ml$2. 40, ph$3. 30 PB 154 432
This report released for sale to the public 8 Mar 61.
The determinition of thermal conductivities at high
temperatures Is unusually difficult because the large
heat losses produce thermal Instability In experi-
mental equipment Investigations previously carried
out in this laboratory have shown that measurements
above 500^0 atre often liable to errors of up to 205^.
In the work reported here a system of high thermal
capacity was ^ployed, and consistent and repro-
ducible resultb were obtained; it thus seems likely
that the conductivity values given are substantially
correct, and <hat reasonably accurate high tempera-
ture measureftients have been achieved. (Author)
Naval Ordtuiice Lab. . White Oak, Md.
REVIEW OF K«ETHODS FOR MEASURING TEM-
PERATURES pP TO 20,000O|C. by Harold Hurwitz.
6 July 59. 33d. 46 refs. NAVORD rept. 6680;
A£>-232 698. , , ,^^
Order from ijc ml$3. 30, ph$7. 80 PB 154 722
This report rtleased for sale to the public 15 Mar 61.
The measure^iient of high temperatures is considered
from the star^ipoint of the requirements of the NOL
high -temper at ore testing facilities. For temperatures
of test specimens, measurements by means of the
thermocouple^ radiation pyrometer, and opcical py-
rometer are discussed. Methods considered for gas
temperatureaT both in combustion flames and in elec-
tric arc plasias, include the measurement of intensi-
ties or width} of spectral lines, as well as radiance
methods utih^ng a comparison radiator. Among
tfjese latter, ja niethod is proposed for using an optical
pyrometer with a comparison radiator, cooler than
the flame beihg studied, but this requires further
development. Certain of the methods discussed are
recommended for use in specific circumstances.
(Author)
Naval Ordnance Test Station, China Lake. Calif.
GENERAL ENTHALPY -TEMPERATU RE ENTTROPY
DIAGRAM FOR IDEAL GASES AND GAS MIXTURES
UP TO 5000°K. by W. C Noeggerath. Rept. for
Sep 53-June 54. 28 June 54, lOlp. 9 refs. NOTS 882;
NAVORD rept. 3341.
Order from LC mi$5. 70. phJ16. 80 PB 154 755
This report released for sale to the public 16 Mar 61.
A method is developed for the correct presenution tt
a propeny function of a group of substances by a ■In-
gle, general set of curves. The method is applied to
the representation of entropy and enthalpy functiooa
for ideal bi- and trl -atomic gases, and general dia-
grams are presented from which enthalpy and entropy
values can be read by attributing appropriate param-
eters to individual gases and mixtures. The diagrtmi
cover the temperature ranges from 298. 16° to bCCffX
and from 2000 to 1700°K. and fulfill, for most practi-
cal purposes, the function of combined enthalpy-
entropy (Mollier) charts. The parameters for spedlk
substances have simple and constant values for the
three gases most commonly encountered (N2. H2O.
OO2). *nd are nearly constant over the nuijor part ri
the temperature range for the other bi- and tri -atomic
gaaes and for some higher -atomic gases. For moat
practical applications, constant parameters can be
used with gas mixtures to yield results within the per-
missible error. Correct parameters are presented
for H2. CO, O2. OH, NO, H, and O, and can be cal-
culated for other gases frcwn known enthalpy and en-
tropy v^ues. CAuthor)
Naval Supersonic Lab. , Mass. Inst, of Tech. .
Cambridge.
APPLICATION OF COVERT'S APPROXIMATIONS
FOR THE BINARY BOUNDARY -LAYER TO A
POROUS CONE WITH A SOLID TIP. by James P.
Moran. Rept. on Contract AF 49(638)245. June 6a
82p. 11 refs. Technical rept. 442; AFOSR-TN-
60-834; AD-247 915.
Order from LC mi$4. 80, ph$l3. 80 PB 153 lOS
Coven's approximations to the solutions to the lami-
nar binary boundary -layer equations as derived by
Baron are critically analyzed for the case of helium
injected into an air boundary layer. The assumed
constant aimilarity integrals employed by Covert are
evaluated for a helium air boundary layer by use of
the exact wedge -flow solutions of Baron and Scott.
These approximate relations are applied to the profc-
lem of a porous cone having a solid tip. The porooi
region is of such a composition that an injection di»-
tribution of the form kA^ exists when both inside
and outside walls are at constant pressures. The
solutions show that the approximations to the shear
and concentration equations give reasonable result*,
but that the approximations to the energy equation do
not. A comparison between these results and como
solutions obtained by a finite difference formulados
are presented in another report. (Author)
Research Inst. , Temple U. . Riiladelphia. H.
HIGH TEMPERATURE PROJECT, by A. V. Groiie*
J. B, Conway. Progress rept. no. 4. 1 Dec 50-
1 July 51. on Contract N9onr-87300. 31 July 51. 31^
634
3rtfi. AD-135202, -=. . -^r-
Orier from LC ml$3. 00, ph$6. 30 PB 154 842
Ihlt report released for sale to the public 17 Mar 61.
llie experimenul work was coocemed primarily with
dw following topics: (a) Centrifugal reactors for the
combustion of alumlnum.(b) The combustion of metal
powders, (c) The production of aluminum vapors.
(Author) (See also PB 137 762)
Research Lab. of Heat Transfer in Electronics,
Mass. Inst, of Tech., Cambridge.
THE INFLUENCE OF VERTICAL VIBRATIONS ON
THE RATE OF HEAT TRANSFER FROM A
HORIZONTAL CYLINDER IN AIR, by C Telekl.
Thesis Rept. on Contract AF 33(616)6076. Oa 60,
6Sp. 19 refs. WADC Technical note 59-357.
Order from OrS $1.75 PB 171 484
TUs report contains the results of an experimental
investigation of the influence of mechanical vibrations
on the rate of heat transfer from a heated horizontal
cylinder In otherwise undisturbed air. The cylinder
vts subjected to temperature potentials and uniform
sinusoidal vertical vibrations whose principal varia-
bles lay within the following experimental ranges:
frequency, f: 54 to 225 cps; amplitude, a: 0 to 0. 16";
product of amplitude times frequency, af: 0 to 1 . 1
ft/sec; temperature potential. At: 15 to ISO^F; cylin-
der diameter, D: 7/8". For the same temperature
potential, the heat-transfer coefficient was observed
to increase In the presence of intense vibrations by
u much as 2(X) per cent of its value without vlbra-
tioos. Analysis of the experimental results shows
that this increase is a function of only one vlbra-
donal parameter, namely, the product of amplitude
and frequency, af. The quantitative results are pre-
sented in the form of three graphs which can be used
to predia the coefficient of heat transfer for
leotnetrles similar to those of the present investiga-
don. (Author)
Wave PropagaHon
Dtytoo U. Research Inst. . Ohio.
CHARTS OF CORRECTIONS TO RADAR OBSERVA-
TIONS FOR REFRACTION BY TERRESTRIAL AT-
MOSPHERES, by Paul B. Taylor and Nicholas A.
Ei^er. Rept. on Contract AF 33(616)5438. Feb 60.
I48p. 15 refs. Research rept. 427-71; WADC Tech-
nical rept 59-619; AD-239 322.
Order from OTS $2. 75 PB 171 544
There are presented in chart form corrections for
ttmospheric refraction to observations of range and
•ngular altitude of targets observed by electromag-
netic radiation at either visual or radar wave lengths.
These correlations have been computed for sixteen
tjfpe atmospheres above a spherical earth. In these
•tmospheres the index of refraction anenuates expo-
nentially with height. The type atmospheres cover
1 range of base indices and exponential attenuation
«tes. (Author)
National Bureau of Sundards, Boulder, Colo.
BIBUOGRAPHY OF TROPOSPHERIC RADIO WAVE
SCATTERING, by Richard L. Abbott. Nov 60. 82p.
681 refs. Technical note no. 80.
Order from OTS %2. 25 PB 161 581
This bibllogrsphy emphasizes tropospheric scattering
of radio waves t^ turbulence-Induced inhomogeneities
of the dielectric constant (local wave velocity in the
atmosphere). Papers on related topics such as turbu-
lence theory and measurements, statistics, instru-
mentation, and some papers on sound scattering are
also included. Papers on radio meteorology are gen-
erally excluded, unless they bear directly on the re-
duction of scattering data. This bibliography covers
material up to about January 1960. Some recent pub-
lications are missing because cf the time lag between
the dates of Journals and their receipt, or because
laboratory reports of various organizations often
reach other laboratories after a year or more. Some
internal reports cannot be listed until they become
formal publications. Papers are ordered by year of
publication and indexes by author and subject are
included. Generally, publications on the same topic
will be found close together in the body of the
bibliography. (Author)
National Bureau of Standards, Boulder, Colo.
THE NBS METEOR -BURST PROPAGATION PROJECT.
A PROGRESS REPORT, by Charles E. Homback.
Louis D. Breyfogle. and George R. Sugar. Rept. on
Contracts DO (33-616) 58-16 and CSOliA 59-524.
31 Mar 60, 46p. 8 refs. Technical note no. 86.
Order from OTS $1. 25 PB 161 587
This report briefly describes a meteor-burst propaga-
tion-study program and presents some of the prelimi-
nary analysis results. Observations have been made
with scaled systems over three different paths (Long
Branch - Table Mesa. Norman - Fargo, and Barrow -
Kenai) at frequencies of 3a 50. and 74 Mc/s. The re-
corded data is processed by a combination of manual
and automatic nfiethods. The preliminary results show
about a 10 db diurnal variation in threshold for a con-
stant duty-cycle. Thresholds for a constant duty-cycle
were observed to have an approximate frequency de-
pendence relative to 30 Mc/s of 15 db lower for SO
Mc/s and 30 db lower for 74 Mc/s. There was no
statistically -significant difference observed in the
occurrence of meteor-bursts from a Poisson distri-
butioa (Author)
National Bureau of Standards, Boulder, Colo.
A THEORETICAL STUDY OF SPORADIC- E
STRUCTURE IN THE LIGHT OF RADIO MEASURE-
MENTS, by Kazuhlko TYw. Jan 61. 42p. 31 refs.
Technical note no. 87.
Order frxxn OTS $1. 25 PB 161 588
The theoretical aspects of the mechanisms of spo-
radic-E reflections are described from both the stand-
point of a thin layer aixl a scattering model. For the
thin layer model, thin dielectric layers which have
various distributions of electron density arecon-
sidered. The scattering theory for which an auto-
correlation function of the fluctuation of electron
density is given by modified Bessel functions of the
635
fourth through Che seventh order is an available model
for sporadic- B scatter. Bobs at ionization which have
a horizontal sqale at the order at 200 m and a vertical
scale at about $0 m are considered for sporadic- E
scatter. The ft-equency and distance dependences at
the oblique VHF propagation by means of the spo-
radic-E layer $re discussed by comparing the theo-
retical results {with experimenul evidence. (Author)
National Bureau of Standards, Boulder, Colo.
VHF RADIO PROPAGATION DATA FOR THE
CEDAR RAPIDS -STERLING. ANCHORAGE -BARROW,
AND FARGO -CHURCHILL TEST PATHS APRIL 1951
THROUGH JUME 1958. by George R. Sugar and
Kenneth W. Suljivan. 1 Sep 60. 262p. 5 refs. Tech-
nical note no. t9.
Order from OVB U 00 FB 161 580
The data tabulated herein are primarily the hourly
values ot systetn loss for vhf ionospheric scatter pro-
pagation (D- region scatter) over the test paths These
data do not inclpde all of the measurements made over
these test patha, but represent a homogeneous set of
results which c|in be readily interconipared since they
were all made imder similar experimental conditions.
A secondary result of the observing program was the
collection of data on sporadic- E propation at 49. 8
Mc/s over the iCedar Rapids to Sterling path for other
frequencies and other paths have not been included
since they cover rnuch shorter intervals of time and
the criteria usdd in scaling were not the same as those
used for the 49^ 8 Mc/s Cedar Rapids - Sterling Eg
data.
Physical Research Lab. . Space Tech. Labs., inc.,
Los Angeles, paltf.
THEORY OF EtECTRON DRIVEN SHOCK WAVEa
by R. G. Fowler and B. D, Fried. 16 Sep 60, 17p.
8refs. STL/TR-6O-0000-GR310.
Order frcxn LCjini$2.4Q. pb$3.30 PB 153 464
Previous calculations at the time required for ion
heating in the discharge or driver section of an elec-
trical shock tube yielded values much greater than
that in which formation and acceleration of the first
luminous front ^ observed to occur. The model at an
electron driven shock presented here shows that the
relation between shock velocity, V, and electron tem-
perature, Te> ^4hich has been established experimen-
tally over a widt range of parameters, remains valid
even though the Conventional plaure ot a shock driven
by hot ions must be abandoned. Thermal expansion of
the hot electrcHi gas accelerates the cold ions, result-
ing in a shock fi?ont or moving electrostatic double
layer. Assuming conditions behind the shock to be
coupled to those in the discharge region through a
simple rarefaction wave, it is found that MV^/kT^ Is
a universal function of W/MV^, where W is the
effective ionization potentiaL This is shown to be in
excellent agreet^ent with a wide variety erf experimen-
tal data.
RESEARCH METHODS, TECHNIQUES
AND EQUIPMENT
Case Inst, of Tech. , Cleveland, Ohio.
A BOUNDED SOLUTION TO A LINEAR DIFFER-
ENTIAL EQUATION WITH A TlXffi- VARYING CO-
EFFICIENT, by Halm Haskal. Scientific rept. no. 1|
on Contraa AF 19(604)3887. 30 Oa 60, 37p. 2 refs
AFCRL-TN-60-1139; AD-248 954.
Order from LC mi$3. 00, ph$6. 30 PB 153 876
A linear circuit containing a time varying element Is
analyzed. A nnethod Is devised to bound within pre-
scribed limits the solution of the first order dlfferca-
tial equation, the circuit current obeys. The steady-
state solution of the current is piecewise given in
terms of exponential functions over intervals selectal
to meet accuracy requirements. The transient com-
ponent at the current is evaluated within the same
limits. A formula is also derived for the steady state
direct current component. (Author)
Cook Research Labs. , Morton Grove. 111.
HYEHIAUUC SERVO CONTROL VALVES. PART 5.
ANALOG SIMULATION, PRESSURE CONTROL, AND
HIGH -TEMPERATURE TEST FACILITY DESIGN, b^
Leslie R. Axelrod, Delmar R. Johnson and Wayne L.
Kinney. Rept. on Contract AF 33(616)5136. Aug 58,
148p. WADC Technical repc. 55-29. Part V;
AD-208 266.
Order from LC ml$7. 20, ph$22. 80 PB 154 966
This report released for sale to the public 16 Mar 61.
Analog computer simulation of an electrohydraullc
servo valve, investigation of pressure control valves,
and design of a high-temperature test facility are
discussed. Analytical relations are developed wWcfc
describe the internal nonlinear operations of the valve
These equations are mechanized on an analog com-
puter and the results verified for static conditions.
The advisability of using a pressure control valve as
opposed to a flow control valve in closed loop opert-
(R^s^rcb. Methods, Techniques and Equipment,,
tion is investigated. The development of a pressure
control valve transfer function and experimental
verification at the analytical results is included. Tbe
requirements for a valve testing facility capable of
providing and utilizing oil at 750<'F, and an ambient
temperature up to I200*'F, are presented.
Massachusens Inst, of Tiech. , Ombrldge.
GQS. GENERAL SINGLE- SERVER C^UEUE- SIMU-
LA TION COMPILER, by George W. Armerding.
Interim technical rept. no. 15 on Fundamental In-
vestigations in Methods of Operations Research,
Contract DA 19-020-ORD- 2684. July 60. 61p. 17 reft.
OOR rept. 968.30-M; AD- 243 492.
Order from LC ml$3. 90. ph$10. 80 PB 153 681
A description is given at GQS, a general queue- simu-
lation compiler program constructed for the IBM 704
computer. The compiler generates a simulation
636
ftognan for any one at a number at specifiable sli^le-
lerter queuing operations. Inter-arrlval times at
(gcfa of a number of queues may be exponential.
crlaag, hyperexponential, normal, rectangular or
ooMtant. and these distributions may be assigned non-
ittonary parameters. Service-times may be chosen
from any oc these distributions, also with non- station-
ary parameters, and service-times may be com-
pounded through probabilistic chains. Priority at
larvlce may be as signed by Input queue. (Author)
Rome Air Development Center, Griffiss AFB, N. Y.
■niE EFFECT OF HIGH AND LOW-PASS FILTER-
IMG ON SPEECH INTELUGIBIUTY, by Arthur Rubin.
R. J. Christman, and George E. Renaud. Nov 60,
lip. 6 refs. RADC-TN-60-243; AD- 249 025.
Order from LC mi$2. 40, ph$3. 30 PB 153 871
This report describes an experiment on speech filter -
ii^. Speech, consisting of prerecorded, phonetically -
Nlf**^ word lists, was passed through either High-
tuaor Low-Pass filters at various cut-off frequen-
dea, and delivered through calibrated headphones to
trained listeners. FiVe subjects listened to the fil-
tered speech and were scored for number of words
heard correctly. Data are presented in both tabular
and curve form, showing the amount of intelligibility
remaining for various degrees of frequency restric-
tion. Some intelligibility may remain in the speech
sigoal when severe bandwidth Limitations ate imposed.
Bttrcme bandwidth restriction results in loss of
(Raaearch Methods. Techniques and Equipment,
"oaniraloess" and leads to possible difficulty in
speaker recognition. One-half the presently utilized
military voice channel bandwidth can result m usable
communications. (Author)
Communication Theory
Ohio State U. Research Foundation, Columbus. Ohio.
OiB-SYLLABLE WORDS- REVISED AND ARRANGED
BY ENDING SOUNDS, by Henry M. Moser. Technical
Ttft. no. 53 on Contract AF 19<604)4575. Nov 60, 153p
i ref RF proj 882; AFCCDD-TN-60-58; AD-248 933.
Order from LC mi$7. 50, ph$24. 30 PB 153 875
TUa report presents a systematic listing of the nKmo-
■yUaUc words in American English according to their
ending sounds. It represents a complete revision of
ftie- syllable Words. AFCRC TN-55-56(PB 132 061)
iB that all words have been re-examined, errors have
been corrected, a few words have been deleted, and a
number of new words have been added. The summary
charts have been revised, and charts of the beginning
<ad ending sounds with the individual vowels and diph-
tbooga have been added. Some changes have been made
'"tfce section on Inclusions. Exclusions, and Qualifi-
CMloos. For the most part, the two reports supple-
■ant aach other; the earlier repon presents an ar-
'*V|Hnent according to beginning consonant sounds.
*e present work according to ending sounds. (Author)
Rirke Mathematical Labs. , Inc. . Carlisle, Mass.
AN EXTENSION OF KAUTZS WORK ON ERROR-
CORRECTING CODES, by Hans G, Haefeli. Scien-
tific repc. no. 4 on Contract AF 19(604)3471. Sep60,
36p. 3 refs. AFCRLrTN-60-1118. AD-248 307.
Order from LC mi$3. 00. ph$6. 30 PB 153 654
Proofs of some basic theorems cxmcemlng binary and
non- binary Kautz's codes. Most of Che results had
been conjectured by Kautz for the binary case.
(Author)
Photographic Equipment
Hydel, Inc., Waltham, Mass.
THE DEVELOPMENT OF A PHOTOMEMORY, by
Emery St. George. Jr.. Carl E. Nielsen, Jr. and
Eugene P. Johnson, Jr. Annual summary rept. no. 1
on Contract Nonr- 2668(00). (1960) 106p. 13 refs.
AD-237 635.
Order from LC mi$5.70, ph$l6.80 PB 147 756
Contents:
Data storage and retrieval
The photomemory in hybrid data retrieval
The photomemory in digital data retrieval
Mechanical language translation
Characteristics of photomemory storage for
mechanical translation
Requirements for photomemory writing
Development of a reading system
Optical system
Electronic system
Demonstration system
(Research Methods- -Photographic Equipment,
Writing system development
Photographic materials
Test plate preparation
Mechanical writing systems
Electronically timed writing system
Dau input
Systems Development Corp. , Dayton, Ohio.
A METHOD FOR CALCULATING FILM RESPONSE
TO CATHOC« RAY TUBE PHOSPHORS, by John E.
Miller. Rept. on Contract AF 33(600)36195. June 59,
22p. WADC Technical note 59-97; AD-212 910.
Order from LC mi$2.70, ph$4.80 PB 154 752
This report released for sale to the public 15 Mar 61.
This report discusses the theoretical optimization of
film and phosphor combinations as used in cathode ray
tube photography. A means is derived whereby the
radiant flux energy from a phosphor can be converted
to a given density on die developed film. This method
of conversion can be used to obtain a figure of merit
for any film-phosphor combination. Several films and
phosphcH- combinations are theoretically evaluated and
comparative figures of merit are tabulated. A con-
version between the units of meter candle seconds and
watt seconds is obtained. The expression for the
637
beam current dtaslty In a cathode ray tube ia obtained
aa a function al the radar resolution capabilities, the
camera lens, and the required density on the devel-
oped film. Thi$ beam current density is compared to
the Langmulr limit for beam current densitlea in
cathode ray tubes. A meana of specifying resolution
la suggested. Bxperlmental results when available
will be pubUshed. (Author)
SCXriAL SCIENCES
Applied Mathetnatlcs and Statistics Labs . , Stanford
U., Calif.
WALRAS' EXISTENCE THEOREM AND BROUWBR'S
FIXED-POINT THEOREM, by Hirofumi Uzawa. Tech-
nical rept. no. 80 on Contract Nonr- 225(50).
28 Mar 60, 7p. tl2 refs . AD- 235 144.
Order from LCpU^l. 80. ptal 1.80 FB 153 691
The equivalence of two fundamental theorems , Walras'
existence theoram and Brouwer's fixed-point theorem,
is shown. Walrts' theorem is concerned with the exist
ence of an equilibrium in the Walrasian system of gen-
eral equilibriuni . Let an excess demand function x(p)
satisfy the foll6Wing conditions: (1) x(p) is a continuous
mapping from P into X , (2) x(p) is a homogeneous of
order 0: x(tp) « >(p) for all t>0andpCP, and (3)
Walras ' law holtotVpi*! (P) "0 'or *11 P*P- Th«>
there exists at Ijeast an equilibrium price vector ]> for
x(p). Brouwer's theorem is concerned with a continu-
ous mapping oojthe simplex. Set ^(r) be a continuous
mapping from ''linto itself. Then there is at least a
fixed -point* int.- f-^(-?).
California U. , Los Angeles.
PRIORITY FUNCnON METHODS FOR JOB- LOT
SCHEDULING, by Ross T Nelson. Rept. on Manage-
ment Sciences Research ProJ. (Contract Nonr-233(02).
4 Feb 55, 37p. piscuaslon paper no. 51; AD- 147 553.
Order from LC mi|3. 00. ph$6. 30 PB 154 423
This report released for sale to the public 8 Mar 61 .
The research reported in this paper was directed to-
ward the development of computationally feasible
methods for obtaining approximations to the solutions
al certafh Job- lot scheduling problems.
Northwestern Technological That. , Evanston, III.
INTER -TEMPORAL ANALYSIS AND OPTIMIZATION
OF BANK PORTFOLIOS, by D. Chambers and
A. Charnes. ONR Research memo. no. 27 on Tem-
poral Planning apd Management Decision under Risk
and Uncertainty^ Contract Nonr-1228(10). May 60,
30p. 3 refs. AD- 237 868.
Order from LCtni$2.70, ph$4.80 PB 148 198
A model is presented and illustrated for assisting In
the analyaia andj planning of a bank's portfolio over
several time petiods. The banker is assumed to know
the levels that Mill prevail, at various dates in the
future, of demandand time deposits, of rates al itttt-
est, and of the bank's net worth. The banker seeks to
maximize profit. He has a choice between various
kinds of earning asset (loans, government securities,
bonds issued by agencies other than the government),
and for each kind at asset he also has a choice betw—
several matioritiea. He is required to observe two
restrictions: a reserve requirement that part cf the
bank's assets must be held in cash or deposited with
the Federal Reserve, and a constraint that it maintaii
a balanced portfolio. (Author)
Princeton U. , N. J.
UNCERTAINTY AND THE EXPANSION OF BANK
CREDIT, by Daniel Orr and Walter G. Mellon. Rept.
on Contract Nonr -1858(1 6). 1 Nov 59, 14p. 18 refs.
EcoiKMnetrlc Research Program Research Memo,
no. 10.
Order from LC ml$2. 40, ph$3. 30 PB 150 469
The method of treatment suggested by Edgeworth
Onl. of The Royal Sutistical Society 51: 113-127,
1888) is developed and extended to the banking sys-
tem as a whole. When the results of this analysis
are compared with those obtained in the traditional
Phillips formulation, it will be shown that the expan-
aion at bank credit, though appreciably affected, ia
surprisingly insensitive to the presence of uncer-
tanity, at least of the type visualized. This result is
hardly obvious a priori in view of the substantial dif-
ferences between stochastic and deterministic analy-
ses of the inventory problem.
Documentation
Case Inst, of Tech., Cleveland, Ohio.
AN OPERATIONS RESEARCH STUDY OF THE
DISSEMINATION AND USE OF RECORDED SCIEN-
TIFIC INFORMATION IN THREE PARTS: I. JOUR-
NAL READING BY PHYSICISTS AND CHEMISTS. D.
THE COST OF JOURNAL PUBUCATION. III. THE
EFFECT OF CONDENSATION ON COMPREHENSION
OF JOURNAL ARTICLES. Rept. on National Science
Foundation Grant no. G-8434. Dec 60, 74p.
Order from OTS$ 2. 00 PB 171 5<B
An Intensive study of the reading behavior of chemists
and physicists was made using almost exclusively the
direct observation of behavior (rather than question-
naires. Interviews, or diaries) to determine what is
read, why they read what they do, and what dlfferencei
In reading behavior exist between the groups. An
economic analysis of Journal publication was made snd
an equation developed which expresses the average
coet (and range of coats) of publishing Journals of •
certain type as a function of The characteristics of the
Journal. In addition, by combining the cost estimates
with readership data, estimates of cost per reading
(rather than cost per page printed) were made for me
most frequently read journals in the fields and they
were compared on this basis. The third part of the
study is directed to the question of how condensadoa
affects the comprehension of scientific articles. A
pilot study was run to determine the feasibility of s
given experimenul deaign to establish the effect of
condensation. (Author)
Reniington Rand Univac Dlv. , Sperry Rand Ck>rp. ,
Philadelphia, Pa.
TUB SCAN-COLUMN INDEX. A BOOK- FORM 00-
OMXNATE INFORMATION RETRIEVAL SYSTEM,
by John O'Connor . Rept . on Contract Nonr-2297(00) .
Feb 60, 84p. 25 refs. AD-236 466.
OrderfromLCmi$4.80, ph$13.80 FB 153 160
Tbe book-form index requires no searching machine,
and tbe coordinate searching can be done by a clerical
person. Each document is entered at Just one place,
and the documents can be in almost any order. A docu-
ment entry consists of a single (or multi-) character
abbreviation for each term the document possesses ,
and a document identification. The document identifi-
CMAoa may be anything from a serial number to a
brief abstract; micro- reduced document identifications
are al^o discussed. ^)eed of searching might be any-
where from several hundred to one thousand or per-
haps more documents per minute, depending to a con-
siderable extent on the amount of space used. How-
ever, actual searching speeds are best determined in
particular applications . Some factors likely to be rel-
evant to search speed are discussed. Specinnen pages
cf a hypothetical scan-column index are given for
reader trials , and experiences of several people with
them are discussed. There is a chance of error in
searching, and fatigue limits the anxxint of searching
possible. These factors are discussed. Subsearches
are defined, their importance described, and their
performance in a scan-column index and in other non-
mechanized systems are discussed. Various questions
about producing a scan-column index are discussed.
A number of possible applications for the scan -column
index are suggested. Several possible variations of
the tcan-column form are suggested, including a very
■odestly mechanized retrieval system, and a possibly
convenient arrangement for coordinate searching of
microfilm reels . (Author)
MISCELLAh€OUS
Naval Research Lab. , Washington, D C
REPORT OF NRL PROGRESS. Apr 61.
Order from OTS $1. 25, $10. 00/year PB 171 317
Contents:
Articles:
The Elevated Duct Between San Diego and Hawaii -
Wave Propagation Branch Staff
A Brief Review and Analysis of Thermoelectricity, by
W. H. Ludte
Scientific program:
Chemistry: Surface chemical methods of displacing
water and/or oils and salvaging flooded equipment -
scHne practical applicationa
Mechanics: Effect of dimensions on fast fracture in-
staMlity of notched specimens. New technique facili-
tatea evaluation of the fracture tou^ness of sheet
materials
Metallurgy and Oramica: Crack propagation resist-
ance of aus- rolled low alloy ateel. Calibration of
new electron microscope for selected area diffrac-
tion. Effect of cold work and temperature on the
strength and structure of steel. Effect cf prior creep
in controlled environments on the low temperature
tensile strength of nickel. Removal of interstitial
impurities from niobium by zinc-niobium compounds.
Determination at alkali metala in solid propellant
rocket fuels. Cast HY 80 aa a submarine structural
material. Protective spinel films on steel: Their
corrosion resistance in aqueous media at room tem-
perature. Preliminary findings in a final investiga-
tion of the effect of minor constituents on the per-
formance of zinc aiwdes in sea water
Optics: Effect of glare on eye behavior during growth
of dark adaptation under blackout conditions
Radio: Passive receiver multicouplers. Reticular
density in cubic lattices. Int^ral grid -cathode de-
sign. Redistribution from an electron beam. Port-
able precision frequency meter and precise signal
generator
Soun± Effect of hydrostatic pressure on seven types
of magnetic core materiala
638
639
' -WV**;'
■^ '/-.
ATOMIC ENERGY COMMISSION REPORTS
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GOVERNMENT RESEARCH REPORTS. As FB numbers are not indicated, order by series and number.
These reports may also be consulted at any ABC Depository Library. A list of these libraries may be
oixsined from the U. S. Department of Commerce, Office of Technical Services, Washington 25, D. C.
Reproduction in whole or part of any report listed herein is encouraged by the U. S. Atomic Energy
Commission, subject to the approval of authors or originating sites. General inquiries from the industrial
press about AEC-developed information should be directed to the Industrial Informatlcn Branch, Atomic
Boergy Commission, Washington 25, D. C.
\.
tu
General, Miscellaneous, and Progress
Reports
Chemical processing technology. Quarterly prog-
resB report for'April -June 1960, by J. R.
Huffman anc others. Fiiilllps Petroleum Com-
pany, Atomic Energy Division, Idaho Falls,
Idaho. Dec 60. Contract AT(1 0-1)- 205. 87p.
Order from OTS. $2.00. IDO-14534
Range safety considerations of the Deacon-Arrow
sounding rocket, by C. T. Force. Sandia
Corporation , Albuquerque, N. Mex. Jan 61.
113p. Order from OTS. $2.50.
SC-4513 (RR)
1959. 51p.
ph$9.30.
Order from LC.
Mi $3. 60,
LA-I937(Del.)
Metabolism of C^^ -isoniazid in humans, by L U.
Boone and others . Loe Alamos Scientific Labor-
atory, Los Alamos, N. Mex. Mar 60. Con-
tract W-7405-eng-36. 50p. Order from LC.
Mi $3. 30, ph$7.80. LA-2420
Effect of segmenttl gut shielding on mortality from
intestlMl radladon, by J. C. Smith. Western
Reserve University, Atomic Energy Medical
Research Project, Cleveland, Olio. Oct 59.
Contract W-31-l09-Eng-78, 21p. Order from
LC. Mi $2.70. ph$4.80. NYO-2064
Final
arming and firing, project HOBO,
Sandia Corporation, Liver-
High explosives,
by R. j. Tockey.
more Laboratory, Llvermore, Calif. Aug 60.
29p. Order from LC. Ml $2.70, ph $4.80.
SC-4824 (RR)
'Proi
8 ret
^_reportforMarchJj^
by E. C. Pollard.
ogresi
1959 - May 31.
Yale University,
New Haven, Conn. 1960. Contract AT(30-1)-
568. 58p. Order from LC. Mi $3. 60,
ph $9. 30. ^ NYO-9339
Biology and Medicine
The study of sponuneous and Induced genetic
changes in mammalian cells grown in tissue
cultiu'es. Summary report for period Tune 15.
ry repor
[June ]
Long
Medical survey of R
after exposure to
yegetttion), byl^
lap people five and six years
allout (with an addendum on
1956 to June U, 1960, by H. MSJgTT
Island Biological Association, Biological Labora-
tory. Cold Spring Harbor. N. Y. 1960. Con-
tract AT(30-1)- 1944. 29p. Order from LC.
Mi $2.70. ph $4.80. NYO-9396
Conard and others. BFook-
haven Nationai Laboratory, Upton, N. Y. Sep
60. 86p. Order from OTS. $2.00.
BNL-609(T-179)
Radioisotopic cows, by W. D. Tucker. Brookhaven
National Laboratory, Upton, N. Y. 1960. lOp.
Order from LC. Mi $1 . 80, ph $1 . 80.
BNL-4908
Biological effectiveness of nuclear radiations from
The effects <rf radiations and chemical treatment
on growrfi in phleum pratenae roots
_ Progress
T. Bnimbield. Longwood college.
report, by R.
Farmville, Va. 1960. Contract AT(40-1)
1676. 17p. Order from LC. Mi $2.40,
ph $3. 30. ORO-280
The effects of radiations and chemical treatment on
growth in phleum
SB ion weapons, by P. S. Harris. Los Alamos
Scientific Laboratory, Loe Alamos, N. Mex.
Aug 55. Decl. with deletions November 25, 1959
report, by R. T.
Farmville, Va. 1960
25p. Order from LC.
ratense roots
•rumfield
Tr
88
College,
Longw
Contract AT(40-1)-1676
Mi $2. 70, ph$4.80.
ORO-281
641
The cytology a n^ genetics of radiation reaisttnce
in pacteria. magreas report for the j)eriod of
February 1, 1955 to November 1, 1955. Univer-
■ity of Oklahtmia, Research Institute, Norman,
Okla. 1955. ICkwtract AT(40-1)-1976. 50p.
Order from LJC. Mi $3.30, ph $7.80.
ORO-282
The c
e cytology an4 geoetica of radiation resistance
in Pacteria! Progress report for the perio3
of November 1. 1955 to November 1 1<
University of Oklahoma, Research Institute,
i per
Norman, Okl4. 1956.
49p. Order firom LC.
Contract AT('40-1)-1976.
Mi $3. 30. ph$7.80.
ORO-283
The
In bacteria .
ana genetica of radiation resistance
m>gre88 report for the perioS
rogress repoi
1956 to Now
oC November 1 {"956 to fJovember 1 'l957.
University of 'Oklahoma, Reaearch. Institute,
Norman. Okla. 1957. Contract AT(40-1)-1976.
44p. Order ffomLC. Mi $3.30. ph $7.80.
ORO-284
The cytology and^genetics of radiation resistance
In bacteria, n^ogrea a report for the period of
frogri
November 1, 1957 to NovemJKr
veraity of Oklahoma,
Okla. 1958.
peril
1, l9a. Uni-
Research Institute, Norman.
pontract AT(40-1)-1976. 31p.
Order from LC. Mi $2.70. ph $4.80.
ORO-285
The relationship |of skin conductance to behavior
in a vigilance task, by D. SteiT Sandia Corpor-
ation, Albuquqrque, N. Mex. Jan 61 . 51p.
Order from OTS. $1.50. SCTM-331-60-14
Radioisotopes in agriculture: Animal hiwbandry
at Teclinical loformaaon, Oak Ridge, Tenn.
Dec 60. 35p. Order from OTS. $1.00.
TID-3078
Vascular and tissue alterations induced
^ whole
body x-irradiatigo. Progress report 1959 -
1960, by B. W. Zweifach and E. Klvy-Roaenberg.
New York Uniilersity, Medical Center, New York,
N. Y. May 6a Contract AT(30-1)- 1680. 6p.
Order from LC. Mi $1.80. ph $1.80.
TID-5946
I
Biological effects erf radiation, and related biochemi-
cal and physiail studies. Semiannual progress
m
report for Noytmber 1, 1959 through Apr
l9o0. Sloan -I<^tterin2 Institute for Ca nee
progre
Aprfl 2
307
_ ttering Institute for Cancer Re^
rch. New York, N. Y. May 60. Contract
AT(3O-l)-910. 70p. Order from LC. Mi $3. 90.
ph$10.80. TID-5955
Investlgationa on the cytogeiytic dttects of radiatloB.
Promress report for June 1, 1959 to May 31,
I960. Yale University. New Haven, Conn.
1960. Contract AT(30-l)-872. 48p. Order fo
from LC. Ml $3. 60. ph $9. 30. TID-5976
The influence of radiation In altering the incidence
of mutations in droaophila. Progress report on
die past twelve montfaa and renewal propoeal for
die period September 15, 1960 to September 14.
1961. by H.J. Muller. Indiana University.
Foundation Research Division, Bloomlngton, Ind.
May 60. Contract AT(11-1)-195. 14p. Order
fromLC. Mi $2.40. ph $3. 30. TID-6042
Some effects of oxy«n on the insects, anat
5r3nnr}iri32FJ:T55?Pr7qi,
ts, anagasu
^^_^ by A.M. CUrk
and V. J. Cristofalo. University of Delaware,
Newark, Dela. and Oak Ridge National Labora-
tory. Oak Ridge, Tenn. 1959. Contract AT(30-
1)-1752. 20p. Order fromLC. Mi $2.40,
ph $3. 30. TID-6052
A program for the study of transplanution of bone
marrow, tissues, and whole organs and of
related topics in surgical research. Progress
irgic
OTC
rogre
report wiui outline cd contlnuning work, by Pr"D.
Moore. Harvard University, Medical School,
Boston, Mass. June 60. Contract AT(30-1)-
2265. 28p. Order fromLC. Mi $2.70,
ph$4.80. TID-6107
The effect of prenatal X- irradiation on ttie behavior-
al develcyment of the albino rat. Period coverwl
October 1. 1959 through September 30, 1^557
>uigh
by J. Werboff and M. iT. Sikov. Wayne Swte
University, Aninal Behavior Laboratory, Detroit,
Mich. 1960. Contract AT(ll-l)-a21. 15p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-6147
The cause and nature of an aplastic anemia of the
bovine and its relation to radiation pancytopenia.
Progress report no. 5 covering the period June
rogress
STTOT
tS:
16, 195»toJunel5, 1»60, by Kl. 0. "Schult^ and
J. H. Sautter. University of Mlnnesou, St.
P«ul. Minn. 1960. Contract AT(ll-l)-364.
56p. Order from LC. Mi $3.60. ph $9.30.
TID-6152
Uptake, transport, and effects of radioactive mateii-
als in aquatic ecosystems. Progress reporT
University of Michigan, Ann ArBor, Micii.
1959. Contract AT(11-1)-781. 5p. Order from
LC. Mi $1.80, ph$1.80. TID-6153
Immunochemical studies of radiation- induced dam-
642
Lawrence, Kan. May 60. Contract AT(1 1-1)-
83. 72p. Order fromLC. Ml $4.50, ph$12.30.
TID-6156
Mass. June 60. Contract AT(30-1)-918.
Order from LC. Mi $2. 40. ph $3. 30.
TID-6183
The chemistry of boron in plants. Technical prog-
ress reporT State University of Iowa. Iowa
City. Icwa. (ndj. Contract AT(ll-l)-59. 7p.
Order from LC. Ml $1.80. ph $1.80.
TID-6160
Ca-45 and Sr-85 metabolism in man. Progn
portforJuneiS. 1959-May20, 1960. Cr
university, Omaha. Neb
ess re-
rt for June 1 5. 1959-May 20, 1960. g:reij^ton
" " ' ■ 1960. Contract AT
(ll-l)-587. 9p. Order fromLC. Ml $1.80,
pta$1.80. TID-6219
Effects of X-rays and thermal neutrons on plant *
ntetaboltsm. Final report, by F. A. Haskins.
University of Nebraska, Lincoln, Neb. 1960.
Contract AT(ll-l)-393. 32p. Order from LC.
Mi $3. 00, ph$6.30. TID-6264
The effect of localized x-irradiatton on antibody
formation and antigen localization. The site of
antibody formatiotT Final report for June I ,
¥
1959 to June 30^ 1960, by W.
University of Chicago, Chicago, 111
tract AT(1 1-1)- 175. 30p.
Mi $3.00, ph$6.30.
Taliaferro.
1960. Con-
Order from LC.
TID-6349
Studies on hydrogen oxidation In cell-free extracts
of hydrojpnecffnonas eutropha . Final tedmicaf
report for September I9M to August 1959. by
C. L. Wittenberger and R. Repaske. University
at Indiana. Bloomlngton, Ind. 1959. Contract
AT(11-1)-251. 30p. Order fromLC. Mi$2.70,
ph$4.80. TID-6394
RadioisotCK)e exdiange *tudies in lakes
~ " Try 1960 - January" 1
versity of Wisconsui, Madison. Wis.
tope
t for
Progress
r%l Uni-
report for February 1960 - Janua
-^ ^-^ ^ f^l.
Contract AT(ll-l)-64. 2^. Order from LC.
Ml $2.70, ph$4.80. TID-6513
lations
Integratloo of the genotype in geographic popu!
at drosophila pavani, by D. Brncic. Cniie.
Universidad. Santiago and Chile. Universldad,
Santiago. Instituto de Biologla '7uan Noe. "
1958. Contract AT(30- 1)- 2465. 13p. Order
fromLC. Mi $2.40, ph $3.30. TID-6539
A quantitative amdy of lifetime sickness and
mortality and progeny effects resulting from
emoaure to penetrating irradiation! Sum ma
e^qxiaure
e to pepetratlng
B and contempUt
of
(M«itemplat»3 work program. 19c
196l. by J. W. GowenandJ. Staduer" Iowa State
University of Science and Technology. Ames,
Iowa. 1961. Contract AT(11-1)-107. 122p.
Order from LC. Mi $6. 30. ph $19. 80.
TID-6582
at
Rica.
47p. Order
TID-6594
1960. Contract AT(30-l)-2043.
fromLC. Mi $3.30, ph $7.80.
Physiological studies on congenital deformity in
mice. Mechanism of action of radiation and
radiomimetic treatments . Progress report and
sixdi renewal propoaal for Septeniber ij 1959 to
August 31, 1900, by C. P. Dagga andM. N. R
Runner. Roscow B. Jackson Memorial Labora-
tory, Bar Harbor, Me. Oct 60. Contract AT
(30-l)-1762. 23p. Order fromLC. Ml $2.70.
ph$4.80. TID-6615
Uptake of radioisotopes and their transfer throu^
food chains by marine organisms. Annual re-
ejrt. 1959-1960. by S. J. Townsley and ottiers.
niversity of Hawaii, Hawaii Marine Laboratory.
Honolulu. Hawaii. 1960. Contract AT(04-3)-56.
45p. Order fromLC. Mi $3. 30, ph$7.80.
TID-6630
Genetic effects of cumulative Irradiation in rats.
Tedinical progreas report, by A. B. Chapman
and others. University of Wisconsin, Madison,
Wis. Sep 59. Contract AT(ll-l)-697. 4p.
Order fromLC. Mi $1.80, ph $1.80.
TID-6640
Relation of ricAettsial and viral infections to radia-
tion injury. Progress report and pcxyoeed
rogram for period January 1, 19o0 to December
Program tor pe:
1,1960, by Id.
mTi
U, 1960, by D. Grelff. Marquette University,
School of Medicine, Milwaukee, Wis. Oct 60.
Contract AT(ll-l)-596. 53p. Order from LC.
Mi $3. 60, ph $9. 30. TID-6729
Rate of recovery from radiation injury and Ita
relationship to after expectation of life of mice.
Progress report for January 1 , 1960 to September
rogress repot
3. 1960. Ren
2D. 1960. Renewal period: January 1 , 1 961 to
December 31, 1961, by J. B. Storer. Roecoe
B. Jackson Memorial Laboratory, Bar Harbor,
Me. Sep 60. Contract AT(30-1)-2313. I6p.
Order from LC. Ml $2. 40. ph $3. 30.
TID-6743
643
A study (rfitrontium, calcium, and rare eartfaa ^
metabollam in Thumana. Annual repoft for
December 1, 1959 to November 30, l^RT" Ap-
pHcation for this continuation of work for Decem-
ber I, 1960 CO November 30, 1961, EyTT
Spencer . Montefiore Hospiul, New York, N.Y.
Oct 60. Contract AT(30-i)-1763. 67p. Order
from LC. Ml 13. 9a ph (10. 80. TID-6747
The bacterlologlcil aspects of radiation slckneas,
P. Miller. University of Chicago, Chica-
go. 111. 1959. Contract AT(ll-l)-46.
Order from LQ. Mi $2. 40. ph $3. 30.
18p.
TID-6855
Radiation tmiuc^d viability mutationa in the honey
bee, by W. R. Lee" University of New Hamp-
shire. Durham^ N. H. 1959. Contract AT
(30-l)-2315. i). Order from LC. Mi $1.80,
ph$1.80.
TID-6877
ibtof
Summary statemefat of flndlnga relftcd to the dis-
tribution, charjicteristicar and biological availa-
bility of fallout' debris originating from testing
DTOgnms at the Nevada test site" by K. H.
Larson and J. tf. Neel. University of Califor-
nia, School of Medicine, Loe Angeles, Calif.
Sep 60. Contract AT-04-i -GEN- 12. 40p.
Order from LQ. Mi $3. 00, ph $6. 30.
UCLA -438
Current status erf Curium inhalation ejqxjsures in
humans, by H. G. Parker and others. Univer-
sity of California, Lawrence Radiation Labora-
tory, Berkeley,, Calif. Sep 60. Contract W-
7405-eng-48. I2p. Order from LC. Mi $2. 40.
ph $3. 30. UCRL-9361
Comparative effects of glucagon, hydrocorltlsone
and epinephrine^ on the protein metabolism of the
fasting rat, byj. L. Izzo and others. Univer-
sitycK Rochester. Atcxnic Energy Project,
Rochester. N. y. May 58. Contract W -7401-
eng-49. 26p. Order from LC. Mi $2.70.
ph$4.80. UR-564
Distribution and excretion studies in dogs exposed
to an aerosol containing polonlum-210. by F. A.
Smith and odiei^. University erf Rochester,
Atomic Energy Project, Rochester, N. Y. Jan
60. Contract W -7401 -eng-49. 45p. Order
from LC. Mi $3. 30, ph $7.80. UR-566
High specific actlMjity iodlnation of gamma -globulin
"with iodine -1 31 nnoiKxAlorlde. t^ R. W. Helm-
kamp and others. University of Rochester,
Atomic Energy Project. Rochester, N. Y. Mar
60. Contract W -7401 -eng-49. 18p. Order
fromLC. Mi $i2. 40, ph $3. 30. UR-568
Biliary excretion of radium in dogs, by ]. B.
Hursh and A. Lovaas. University of Rochester,
Atomic Energy Project. Rochester. N. Y.
May 60. Contract W-7401 -eng-49. I6p. Order
fromLC. Mi $2.40, ph $3.30. UR-571
Urinary excretion of radium in dogs, by J. B.
Hursh and others. University of Rochester,
Atomic Energy Project, Rochester, N. Y.
May 60. Contract W-7401 -eng-49. 17p. Order
fromLC. Mi $2.40, ph $3.30. UR-572
Unifying OMicepts of parathyroid hormone action,
by A. R. Terepka and others. University of
Rochester, Atomic Energy Project. Rochester,
N.Y. July 60. Contract W-7401 -eng-49. 28p.
Order from LC. Ml $2.70. ph $4.80.
UR-577
Strontlum-90 and gross beta activity in the fat and
non-fat fractions of coconut crab ^Birgus latro)
liver collected at Rongelap Atoll during Mar3i
1958, by D. Chakravartl and R. Eisler. Uni-
versity of Washington, Laboratory of Radiation
Biology, Seattle, Waah. Mar 59. Contract AT
(45-l)-540. I3p. Order fromLC. Mi $2.40,
ph$3.30. UWFL-59
Potassium as an Index of naturally occurring radio-
activity in tuna muscle . by D. Chakravarti and
T. Joyner. University of Washington, Labora-
tory, of Radiation Biology, Seattle, Wash. June
59. Contract AT(45-l)-540. Up. Order from
LC. Mi $2.40, ph$3.30. UWFL-60
Potassium and ceslimfi-137 in birgus latro (coconut
crab) muscle collected at Rongelap Atoll, by
d. Oiakravarti and E. E. Held. University of
Washington, Laboratory of Radiation Biology,
Seattle, Wash. Jan 60. Contract AT(45-1)- 540.
14p. Order from LC. Ml $2. 40, ph $3. 30.
UWFL-64
The analysis of some trace elentents in fish tissues,
by T. Joyner and D. Chakravarti. University
(rf Washington. Laboratory of Radiation Biology.
Seattle. Wash. Apr 60. Contract AT(45- 1 )-
540. 15p. Order fromLC. Mi $2.40,
ph$3.30. UWFL-68
Chemical Separations Processes for
Plutonium and Uranium
Purification of reactor fuels using tiq^iid zinc, by
J. B. Knighton and others. Argonne Natimal
Laborarory, Argonne, 111. Jan 61. Contract
W-31-109-eng-38. 35p. Order from CTS.
75 cents. ANL-6223
644
Ctemical engineering dlvlalon summary report for
July. August, September, 1960, by S. Lawroaki
and others. Argonne Natinnal Laboratory,
Argonne, 111, 1960. Contract W-31-109-eng-38.
I82p. Order from OTS. $2.75. ANL-6231
Ridge,
Tnm. Sep 60. 393pL Order from LC.
Mi $11. 10, ph$63.00. CF-60-7-65
Burochemic assistance program. Pr
_^_^ listance program. Progress report
for January dirough June I960, by E. L. Nichol-
son and E. M. Shank. Oak Ridge National Labor-
atory. Oak Ridge. Tenn. July 60. 6p. Order
fixxn LC. Mi $1.80, ph $1.80. CF-60-8-2
Burochemic assistance program: Information from
Hapo on centrifuge decontamination and fuel
storage canal water clean-up, by O. F. Hill.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Aug 60. 3p. Order from LC. Ml $1.80,
ph$1.80. CF-60-8-127
Distribution of uranyl nitrate between Al^OOa
and tributyl phoeirfiate, by D. P. Ames and D. G.
Kar raker. Du Pont de Nemours (E. I. ) fc Com-
pany, Savannah River Laboratory, Aiken, S. C.
Mar 58. Decl. March 28, 1960. Contract AT
(07-2)-l. I6p. Order fromLC. Mi $2.40,
ph$3.30. DP- 275
Scavenging of ruthenium from Purex uranyl nitrate
solutiCTi, by C. A. Prohaska. Du Pont de Nem-
ours C^.I. )k Company, Savannah River Labora-
tory, Aiken, S. C. June 58. Decl. March 28,
1960. Contract AT(07-2)-l. 12p. Order from
LC. Mi $2.40. ph$3.30. DP-2%6
Behavior of technetium in the Purex process, by
T. H. Siddall, III. Du Pont de Nemours (E. I.)
k Company, Savannah River Laboratory, Aiken,
S. C. Apr 59. Decl. March 28, 1960. Con-
tract AT(07 - 2)- 1 . 1 3p. Order from LC.
Mi $2. 40, ph$3.30. DP- 364
Recovery of rare earth fission products faxMn
Purex **?^' by W. E. Prout and E. K. Didces.
E. I. du Pont de Nemours h Company, Savannah
River Laboratory, Aiken, S. C. Sep 60. Con-
tract AT(a7-2)-l. I6p. Order from OTS.
50 cents. DP-509
Complexlng fluoride ions with aluminum metal, by
h. A. Holthaus and others. Goodyear Atomic
Corporation, Porumouth, Ohio. Aug 60. Con-
tract AT(33- 2)- 1. 5p. Order fromLC.
Ml $1.80, ph$1.80. GAT-P-18
Depositloo of ruthenium activity oo the ojddizer
during head-end treatment, by C. F. Callis.
Hanford Works, Richland, Wash. Nov 50.
Decl. March 28, 1960. 7p. Order from LC.
Mi $1.80, ph$1.80. HW- 19391
Organic continuous cartridge for the Purex 2D
column, by G. M. Hesson. General Electric
Company, Hanford Atomic Products Operation,
Richland. Waah. Aug 56. Decl. June 10, 1960.
Contract W-31-109-Eng-52. 14p. Order from
LC. Ml $2. 40, ph$3.30. HW -44974
eparation of cerium from the trivalent rare
rtns usinghydrogen peroxide and sodium
state, by E. J. Wheelwrl^ and N. C. Howard.
The separation of cerium from the trivalent rare
eart
acetate.
General Electric Company, Hanford Atomic
Products Operation, Richland, Waah. May 60.
Contract AT(45-1)-1350. 18p. Order from LC.
Ml $2.40, ph$3.30. HW-62505
Multl -purpose dlssolyer Information manual, by
H. P. Simonds. General Electric Company,
Hanford Atomic -Products Operation, Richland,
Wash. Mar 60. Contract AT(4S-1)-1350, lip.
Order fromLC. Mi $2.40. ph $3.30.
HW-64172
The zirflex lyocess terniinal development report,
by P. W. Smith. Hanford Atomic Produces
C^atioa. Richland. Waah. Sep 60. Contract
AT(45-1)-1350. 48p. Order from OTS. $1.25.
HW-65979
Review of research and develcyment at the Idaho
Chemical processing plant on the electrolytic"
dissolutioo of nuclear'fuel, by C. M. Slansky
and otfaersi Riillips Petroleum Company,
Atomic Energy Division, Idaho Falls, Idaho.
Jan 61. Contract AT(10-1)- 205. 57p. Order
from OTS. $1.25. IDO-14535
Some comnients on die U^^^ and Th^^ problenns
in recycled Th - U fuels, by E. F. Welsner.
Atomics International. Dlviaicn of North Ameri-
can Aviation, Inc. , Canoga Pari:, Calif. June
55. Decl. June 10, 1960. 15p. Order from
LC. Mi $2. 40, ph$3.30.
NAA-SR-Memo-1418
Foam separation in nuclear processing. Annual
report for April 1, 1959 to June 15. I960.
Radiation Ai^lidations Inc. . New York, N. Y.
Sep 60. Contract AT(30-1)- 2384. 41p. Order
from LC. Mi $3.00, ph $6.30. NYO-2S21
645
Purex DToeess for plutoolvnn and uranium recyrery,
by W. B. Lanham and T. C. Runion. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Oct 49.
Decl. with deletions April 18, 1960. Contract
W-7405-eng-26. Up. Order from LC.
Ml $2.40, ph $3. 30. ORNL-479 (Del.)
Recovery of nltrqgen oxldea and rare gag flaaloo
products from die nitric acid dbaaoTutlon^^
Irradiated uraiilum, by A. T. Creaky. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Apr S2. Decl. with deletions February 9, 1960.
Contract W-74p5-eng-26. 83p. Order from LC.
Mi$4.80, phil3.80. ORNL- 1206 (Del.)
Operating characterlatlcai of a podbielnlak centrtfu-
H enractor, 'by). H. Morgenthaler and others,
issachusetta Institute ai Technology, Engineer*
Ing Practice School, Oak Ridge, Tenn. Aug 51.
Dele. Marches, 1960. Contract W- 7405 -eng-
26. 30p. On^rfromLC. Ml $2.70, ph $4.80.
TID-5463
). Onfcr
Separation of yttrium and the rare eardis by liquid-
by liQul<
Octobei
liquid extraction. Progreaa report for uctooer
3, 1957 to Fehiruary 7, 1958. by J. Q. Penrod.
Michigan Cheiiical Corporation, St. Louis, Mich.
Apr 58. 14p. Order from LC. Ml $1.80,
ph$1.80. TID-6420
Liquid- liquid extraction
^ril
Cnemlcal Corporadoo, St. Louis, Mich
quid extraction prooeMgs. Period covered
April 9-18, 19b7, by C. W. Clemaas. MlcSI^
Aug
lOp. Order from
TID-6424
57. Decl. February 6, 1959.
LC. Ml $1.80^ ph$1.80.
1
The separation of! the rare earths In a Llndsey con-
centrate by ion exchange. Period covered June
22. 1956 to March 30. 1957, by R. B. WIa55.
Michigan Chemical Corporation, St. Louis,
Mich. Apg57. Decl. February 6, 1959. 19p.
Order from LQ. Ml $2. 40. ph $3. 30.
I TID-6430
Longitudinal dispersion In aolvent-extractlon
columnB: Nuirierical tablea, by A. K. McMuUen.
and others. University of California, Radiation
Laboratory, Berkeley. Calif. Jan 58. Contract
W-7405-eng-4a. 31p. Order from LC. Mi$3.
Mi $3. 00, ph $16. 30. UCRL-391 1 (Suppl. )
Chemistry
Tritium productiop proceaa, by N. Chellew and
others. Argonbe National Laboratory, Argonne,
111. May 48. Decl. March 15, 1960. Contract
W-3l-109-eng-38. 25p. Order from LC.
Ml $2.70, ph $4.80. ANL-4159
ThernaocWnsnalc evaluation of materials in contact
with fluoride fuels, by R. C. Crooks and othera.
Battelle Memorial Institute, Columbus, Ohio.
Aug 54. Decl. September 9, 1959. Contraa
W-7405-eng-92. 19p. Order from LC.
Ml $2.70, ph$4.80. BMI-936
Practical methods of milking Y^, Tc^^"* and
1^32 from dieir respective parents, by W. D.
Tucker and others. Brookhaven National Labora-
tory. Upton, N. Y. Aug 60. 4p. Order from
LC. Mi $1.80. ph$1.80. BNL-4940
Chemical technology division, unit operation sectios
ninthly progress report for Tanuary 1958, by
J. C. Bresee and others. Oak Ridge National
Laboratory, Oak Ridge. Tenn. Aug 58. 41p.
Order from LC. Ml $3.00, ph $6.30.
CF-58-1-137
Measurements of amall amounts of H9O in D2O by
near-infrared abeorpdon spectroscopy, by R.E .
Biggers. Oak Ridge Naticnal Laboratory, Oak
Ridge, Tenn. Dec 58. 7p. Order from LC.
Mi $1.80, ph$1.80. CF-58-12-143
Hydrogen evolution fro«n uranluin-233 prodiict
solutions, by R. H. Ralney. Oak Ridge NatiOMl
Laboratory, Oak Ridge, Tenn. Mar 60. 9p.
Order from LC. Mi 1.80. ph $1.80.
CF-60-3-8
Transfer of uranyl Ion across a water-TBP Inter-
face, by C. V. Chester. Osk Ridge National
Laboratory, Oak Ridge, Tenn. Mar 60. 12p.
Order from LC. Ml $2. 40. ph $3. 30.
CF-60-3-119
Oxidation of hydrogen and carbon monoxide in hell-
\jn by use of CuO. I. Prelimary results, by
C. D. Scoct. Oak Ridge National Laboratory,
Oak Ridge. Tenn. July 60. 21p. Order from
LC. Mi $2. 70. ph $4. 80. CF-60-7-26
Spectrophotometrlc studies of solutions at elevated
temperatures and pressures: Status and pro-
for FY-196rand part of PV-1'^62, bpT^. E.
Siggers and J. M. Chllbon. Oak Ridge National
Laboratory^ Oak Ridge, Tenn. July 60. 13p.
Order from hC. Mi $2. 40, ph $3. 30.
CF- 60-7 -51
Comparison of weight changes of Columbium BPCtJ'
n>ena with amount of impurities as determined
by v
vacuum fusion analyses, by H. E. McCoy.
Ridge National Laboratory, Oak Ridge, Tfena.
Aug 60. Order from LC.
Mi $2.40. ph$3.30.
CF-60-8-25
646
Determination of free acid in highly radioactive solu-
tlona by remotely controlled conductometric tF
tradon, by R. E. Corcoran and othera. Oak
Ridge Nadonal Laboratory, Oak Ridge, Tenn.
Oct 60. 9p. Order from LC. Mi $1.80,
ph$1.80. CF-60-10-38
Maridme ns -cooled reactor progrann. X-r«y
atudy (« the ternary 8 yatetn U-Al-O, by L. J.
Dykstra. General Dynamics, General Atomic
Division, San Diego, Calif. Sep 60. Contract
AT(04-3)-187. 21p. Order from OTS.
75 cents. GA-1479
Phiorlne disposal using charcoal, by N. W. Houston.
Goodyear Atomic Corporation, Portsmoudi,
Ohio. July 60. Contract AT(33- 3)- 1. 12p.
Order from LC. Ml $2. 40, ph $3. 30.
GAT-T-819
Wet fluoride studies: Calcium plutonium (IV)
fluoride, by P. B. Branin. General Electric
Company, Hanford Atomic Products Operadon,
Richland. Wash. Dec 53. Decl. March 15,
1960. Contract W - 31 -1 09 -Eng- 52. 9p. Order
from LC. Ml $1.80, ph $1.80. HW-30039
The preparadon of plutonium {IV) ammonium fluor-
ide and its decoinpoeltion to plutonium tetrafluor-
Ide for aubsequeni reducdon to meal, by W. B.
ToUey. General Electric Company, Hanford
Atomic Products Operadon, Richland, Wash.
Mar 54. Decl. March 15, 1960. Contract
W-31-109-Bng-52. Up. Order from LC.
Ml $2. 40, ph$3.30. HW-31211
Continuous denitradon status of development.
anu-
Ec-
)pment, Ja
ary 12, 1955, by M. J. Szullnaki. General E
trie Company. Hanford Atomic Products Opera-
don, Richland, Wash. Jan 55, Decl. June 10,
1960. Contract W-31-109-Eng-52. 9p. Order
from LC. Mi $1.80, ph $1.80.
HW-34470(Rev.)
Tbermal decomposition of plutonium (IV) oxalate
and hydrofluorinadon of plutonium (IV) oxalate
and oidde, by M. N. Myers. General Electric
Company, Hanford Atomic Porducts Operadon,
Richland, Wash. Aug 56. Decl. April 28,
1960. Cond-act W-31-109-Eng-52. 30p. Order
from LC. Ml $2.70, ph $4.80. HW-45128
Eiamlnatlon of corrosion test coupons in Purex 101
waste storage tanks- -rm- 147, by D. H. Parks.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Apr 57.
Contract AT(45-1)-1350. 19p. Order from LC.
Mi $2. 40, ph$3.30. HW-49574
Oxygen diffusion and reacdon during gamma Irradl-
ttfiylene, by R. C. "f
CtMnpany, Hanford Atomic Products
ation ot poiyemyiene, by R. c. Uiherson. Gen-
eral Electrl
Operadon, Richland, Wash. July 60. Contract
AT(45-1)-1350. 40p. Order from LC. Ml $3. 30,
ph$7.80. HW-64305
An electrodiemical determinadon of Bubmicrogram
quandtlCT of mol^xtenum, by H. E. PalmerT
Gmeral Electric Company, Hanford Atomic
Products Operadon, Richland, Wash. July 60.
Contract AT(45-1)- 1350. 22p. Order from LC.
Mi $2. 70, ph $4. 80. HW-66057
Decladdlng of Zircaloy clad uranium dioxide fuels
by aclmc fluoride joludons, by R. F. Maness.
dieneral Electric Company, Hanford Atomic
Products Operadon, Richland, Wash. Sep 60.
Contract W-31-109-Eng-52. 14p. Order from
LC. Ml $2.40, ph$3.30. HW-66884
Pilot plant development of a process for separating
barium-140 from MTO fiel, by B. M. LigleT^ .
and others. PWllipe Petroleum Ccnnpany, Atomic
Energy Division, Idaho Falls, Idaho. Sep 55.
Decl. August 15, 1960. Contract AT(10-l)-205.
171p. Order from LC. Ml $7.80, ph $25.80.
IDO-14344
Low -cost Bridgman-type single -crysul growing ap-
paratus, byE. H. OlsonT Iowa State University
of Science and Technology, Ames Laboratory,
Ames, Iowa. Aug 60. Contract W-7405-eng-82.
51p. Order from OTS. $1.25. IS-178
Progress report on friction loss of slurries in
strairiit tubes, by G. Murphy and others. Iowa
State University of Science and Technology,
Ames Laboratory, Ames, lows. Sep 60. Con-
tract W-7405-eng-82. 99p. Order from OTS.
$2.25. IS-197
Development of the condnuous method for the re-
ducdon of uranium hexafluoride with hydrogen
process develomnent. Hot wall reactor, byS.H.
Smiley and D.C. Brater. Oak Ridge Gaseous
Diffusion Plant, Oak Ridge, Tenn. June 58.
Decl. with deledons August 21, 1959. 18p.
Order from LC. Ml $2. 40, ph $3. 30.
K-1379(Del.)
Decontamination of irradiated U-235 samples for
Isotopic analysis, by J. W. Codding and others.
Knolls At«nic Pbwer Laboratory, Schenectady,
N. Y. May 52. Decl. October 15, 1959. Con-
dract W-31-109-Eng-52. 13p. Order from LC.
Ml $2.40, ph$3.30. KAPL-M-ELZ-5
647
Electroidnetic procegsea --Nuclear >Bpect». Qu«r- The radjochemiatrr of protactinium, by H. W
terly progreaja report for February I -April 30, ICirby. Mound Laboratory, Monaanto Cher
'ly Drogreae repo
57, byV C. ^r
a; 1957, by A. C W^erner and H. Kau. Vitro
L«boratorieat Weat Orange, N. J. May 57.
Decl. June 10. I960. Contract AT(30-1)-1996.
9p. Order filoin LC. Mi $1.80, ph $1.80.
KLX-10077
Report for reaearch oo subetitute materiala for
April 2 1951 to July 2 1951. (Acdnium-227).
Mound Laboratory, Miamiaburg, Obio. Aug 51.
Decl. May 3, 1960. Contract AT-33-1 -GEN -53.
71p. Order trom LC. Mi $4. 50, ph $12. 30.
MLM-6l3(Del. 1)
Pinal safety anajyaia report of americium proceea-
ing to be perfcrmed by tlie Martin Company, by
J. Watcher. Martin Company, Nuclear DlvlskMi,
Baltimore, Md. May 60. Contract AT(30-3)-
217. 66p. order from LC. Mi $4. 50,
ph$12.30. J MND-P-2347
Methods tor analysla of polypheny I reactor coolants,
by R. T. Keen and others. Atomics International.
A Division of North American Aviation, inc. ,
Canoga Park, Calif. Jan 61. Contract AT(1 1- 1)-
CXN-8. 56p. Order from OTS. $1.25.
NAA-SR-4356
Denaity-temperyire relationahipe for irradiated
dtphenyl, by Jl.H. J. Ger eke. Atomics Intemat-
tiooal. Division of North American Aviation,
Inc., Canoga Park, Calif. Nov 57. 4p. Order
from LC. Mii$1.80, ph $1.80.
NAA-SR-MenK}-2268
Automatic apectgophotometry for chromatographic
separations, l>y R. M. Kramer. Atomic^ Inter
national. CRvlsion of North American Aviation,
Inc. . Canoga Park, Calif. July 59. 25p. Order
from LC. Mi $3.00, ph $6. 30.
NAA-SR-Memo-4188
The maximum sqlubili
solubility of water in terphenyl and
polypnenyla, ty H. Mandel. Atomics Internation-
al, Diviaion of North American Aviation, Inc. ,
Canoga Park. Calif. Dec 59. lOp. Order from
LC. Mi $2.4^, ph $3.30. NAA-SR-MenK>-4753
L
Leaat squares treatment of data involving non- linear
functional reUtionships, by I. R. Tatinenbaum
and W. A. Yoiing. Atomics International. A Div-
lalOD of North American Aviation Inc., June 60.
lOp. Order f^om LC. Ml $2. 40, ph $3. 30.
NAA-SR -Memo- 5393
The radttochemiajry of zinc, by H. G. Hicks. Uni-
versity of California, Lawrence Radiation Labor-
atory, Uvermore, Calif. June 60. 58p. Order
from OTS. 7) centa. NAS-NS-3015
Company, Mlamlaburg, Ohio.
Order from OTS. $1.00.
Chemical
Dec 59. 80p.
NAS-NS-3016
The radiochemictry of iron, by J. M. Nielsen.
Hanford Laboratories, Hanford Atomic Products
Operation, Richland, Waah. Aug 60. 42p.
Order from OTS. 50 cents. NAS NS-3017
The radiochemiatry of mangaiyse, by G. W. Leddl-
cocte. Oak Ridge National Laboratory, Oak
Ridge , Tenn. Oct 60. 23p. Order from OTS.
50 cents. NAS-NS-3018
The radiochemiatry of carbon, nitrogen, and oxygen,
by J. Hudis! Chemistry Department, Brookhaveo
National Laboratory, Upton, N. Y. Dec 60.
20p. Order from OTS. 50 centa.
NAS-NS-3019
The productioo of high-purity beryllium carbide, by
J. G. Theodore and others. Brush Beryllium
Company, Cleveland, Ohio. Oct 52. Decl.
September 21, I960. Contract AT(30-1)- 541.
20p. Order from LC. Mi $2.40, ph $3.30.
NYO-llU
Progress report of pilot plant work on UF^ produc-
tion by continuous methods;- period covered April
22. 1^50 to My 31, l»5fl, iSTe. ^. Teter.
Mallinckrodt Chemical Works, St. Loul«*, Mo.
Nov 50. Decl. March 7, 1960. 8p. Order
from LC. Mi $1.80. ph $1.80. NYO-i3l3
iphic Sununary report on the long range program for the
Inter- period May 1. 1953 to July 3lT 1953° by C. J.
ition, Kodden. New Brunswick Laboratory, New Bruns-
wick. N. J. Oct. 53. Decl. March 7, 1960.
131p. Order from LC. Mi $6.30, ph $19.80.
NYO-2043
Second annual progg-ess report to the United Sutes
Atoniic Energy Commission, by J. G. Floss.
Temple University, Research Institute, Philadel-
phia. Pa. Sep 59. Contract AT(3O-l)-2062.
29p. Order from LC. Mi $2.70. ph $4.80.
NYO-2156
Foam separation in iaotope recovery
_ Quarterly
report for the period /uly 1 to October 1 . 19w,
by R. A. Sanford. Radiation Applications Inc.,
Long Island City, N. Y. Oct 60. Contract AT
(30-l)-2384. 27p. Order from LC. Ml $2.70.
ph$4.80. NYO-2522
A study of the mechanism of radiation induced reac-
tions of organic polymers with inorganic salts
64»
and organometallic compountte. Quarterly sum-
mary report for April 1, 1960 to June 30, _1960,
Radiation Applications Inc. , Long Island City,
N. Y. Aug 60. Contract AT(30-1)- 2318. 6p.
Order from LC. Mi $1 . 80, ph $1 . 80.
NYO-2526
The standard free energy of formation of certain
rare earth carbides" Final report, by C. L»
McCabe. Carnegie Institute of Technology,
Metals Research Laboratory, Pittsburgh, Pa.
Mar 60. Contract AT(30-1)- 1825. 40p. Order
from LC. Mi $3. 00. ph $6. 30. NYO-7432
Ft»ed sodium hytlroxide. Prfye^s report for
period covered June 1, 1959 to May 31, 1960,
Dy R. P. Seward and H. W . Ono. PensylvaSla
Swte University, University Park, Pa. June 60.
Contract AT(30-1)-1881. 8p.
Ml $1.80, ph$1.80.
Order from LC
NYO-7581
Absorption and fluorescence spectra of uranium
salts and other solids; spectrs of molecules con-
Mining tritium IX. Annual report, by G. H.
Dieke" Johns Hopkins University, Baltimore,
Md. June 59. Contract AT(30-1)- 1447. 12p.
Order from LC. Mi $2.40. ph $3.30.
NYO-8098
The determination of strain and crystallite size in
CaPo powders from the data of a single x-ray dif-
fraction profile, by F. Witt and others. Frank-
lin Institute Laboratories for Research and
Development, Philadelphia and International
Buainess Machines Corporation, Poughkeepsie,
N. Y. Nov 58. Contrsct AT(30-1)-1484. 32p.
Order from LC. Mi $3.00. ph $6. 30.
NYO-8119(Del.)
Corrosion by molten fluorides. Interim report, by
L. S. Richardson and others. Oak Ridge Nation-
•1 Laboratory, Oak Ridge, Tenn. Sep 52. Decl.
May 9, 1960. Contract W-7405-eng-26. 20p.
Order from LC. Ml $2. 40, ph $3. 30.
ORNL-I491
Fbase equilibrium diagrams for fused salt systems,
byR. E. Thoma and W. R. Grimes. Oak Ridge
National Laboratory, Oak Ridge, Tenn. July 57.
Decl. May 27, 1860. Contract W-7405-eng-26.
9^. Order from LC. Mi $4.80. ph $13.80.
ORNL-2295
Phase equilibria in molten salt breeder reactor fuels
I. The system LiP-BeFo-UF4-ThF4, by CTIT.
Weaver and others. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. [ndj. Contract W -7405-
eng-26. 58p. Order from OTS. $1.50.
ORNL-2896
Survey of potential vapor -phase explosions in Da rex
and Sulfex processes, by K. S. Warren. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
(ndj. Contract W-7405-eng-26. 22p. Order
from OTS. 50 cents. ORNL-2937
Removal of silica from Darex dissolver solutions,
by A. F. Messing and O. C. Dean. Oak Ridge
National Laboratory, Oak Ridge, Tenn. [nd].
Contract W-7405-eng-26. 12p. Order from OTS.
SO cents. ORNL-3000
The solubility of wster in benzene (thesis) byR.A.
Pavia. North Carolina State College, Raleigh,
N. C. Revised on the performance of contactors
for liquid- liquid extraction. 1958. Contract
AW-1)-13M. 123p. Order from LC.
Mi $6. 30. ph $19.80. ORO-287
Extraction of uranium from incinerator ash leach
slurries, by J. C. Biery. Dow Chemical Com-
pany, tiocky Flats Plant, Denver, Colo. JulySS.
Decl. March 28, 1960. Contract AT(29-1)- 1106.
67p. Order from LC. Mi $3.90. ph $10.80.
RFP-117
Quarterly report for April 1, 1960-June 30, 1960.
Mellon Institute, Radiation Research Labora-
tories, Pittsburgh, Pa. July 60. Contract AT
(30-1)- 2310. 15p. Order from LC. Mi $2.40.
ph$3.30. RRL-43
A study of the effect of various fluoride treatments
on the properties of barium titanate and lead
zirconste tiunate polycrysulline ferroelectric
polycryst
L Wilxo
cersmics, by D. L. Wilxox. Sandia Corpora-
tion, Albuquerque, N. Mex. Jan 61. 41p.
Order from 015. $1.50. SCTM -422-60(11)
Current cornmtss ion methods for producing UOg
UF4, and UFft. Mallinckrodt Chemical Works,
St. Louis, Mo. ; National Lead Company of Ohio.
Cincinnati, Ohio; New Brunswick Laboratory,
New Brunswick, N. J. and Union Carbide Nuclear
Company, K-25 Plant, Oak Ridge, Tenn. Jan 56.
Decl. with deletions November 5, 1959. 281p.
Order ttom LC. Mi $11. 10. ph $45.00.
4: TID-5295(Del. )
Radiation stability of organic llquida. Semi-annual
report no. 6 for July 1, 1959 'to Decetnber 31,
1959, by R. M. Wagner and R. Farrand. Stan-
ford Research Institute, Menlo Park, Calif.
Jan 60. 15p. Order from LC. Mi $2.40.
ph $3. 30. TID-5635
Absorption spectroBcopy in litjuld sitfiydrotw hydro -
gen fluoride, by A. Tulun)ello.
649
slty, Lafayette, Ind. 1960.
LC. Mi $1.80, ph$1.80.
Purdue Univer-
lOp. Order from
TID-6059
Mercairy-photo<gii»ltlzed reyctlotM involvii
nitric
Hoffman and it. B. Berascein.
Michigan. Ana Arbor, Mich. June 60. Contract
AT(ll-l)-821. 42p. Order from LC. Mi $3. 30,
ph$7.80. TID-6062
oxide, nitroug oxide, and hydrogen, by
Kin. Univeraity of
itiic
Spectrophotometyic determination of allipon in
plutoaium. by'M. E. Smith. Loa Alamo* Scieati -
tic Laboratoriea, N. Mex. 1957. Decl. July 9,
1958. 17p. Order from LC. Mi $2.40,
ph$3.30. TID-6071
A rcy^ £< the detractive metallurgy of niobium,
by M. E. Sibert and others. Horizona, Inc.,
Cleveland, Ohio. [195?I Contract AT(30- 1 )-
1894. 58p. Order from LC. Mi $3. 60.
ph$9.30. TID-6100
Absorption and fluorescence apectra of NdCla and
a ta tea of the ofeodymium ion, by E. H. Carlson.
Johns Hopkins "University. Baltimore, Md. Mar
60. Contract AT(30-1)-1447. 139p. Order
frcxn LC. Mi $6. 9a ph $21.30. TID-6124
Absorption and fltioreacence spectra of uranium
aalta and othef solids spectra of moleculea con-
taining tritium! X. Annual report, by G. H.
Dleke" Johna Hopkins University. Baltimore,
Md. June 23. 1960. Contract AT(30-l)-1447.
2^. Order fiiom LC. Mi $2.70, ph $4.80.
TID-6125
The determinatioy of soluble poison concentrations
in H20. Thesja. by R. A. Mattson. Argonne
National Laboratory. Argonne. III. 1957. 64p.
Order from LC. Mi $3. 90, ph $10. 80.
TID-6143
ChemlBtry of polyvalent metal halides. A. Technl-
cal progress rieport for March 1, 1959 to Febru-
ary 29, 1960. by H. C. Brown. Purdue Research
Foundationr Lafayette. Ind. 1960. Contract
AT(ll-l)-170. 65p. Order from LC. Mi $3.90.
ph$10.80. TID-6149
Solvent extraction studies
— Z
^ An annual report, by
G. Warren^ Western State College of
Colorado, Gunhiaon, Colo. May 60. Contract
AT(ll-l)-749.i 27p. Order from LC. Mi$2.70,
ph$4.80. TID-6150
1
Progreaa report <yi removal of atrootium-85 from
miUc covering period November 1, 1959 to June 1,
1960. by W. D. Armstrong and L. Singer. Uni-
versity of Minnesota. Minneapolis. Minn. 1960.
Contract AT(1 1 -l)-838. 28p. Order from LC.
Mi $2.70, ph $4. 80. TID-6163
The graphite electrode: an Improved technique for
voltammetry and chronopotentiometry, by F. J.
Elvlng and D. L. Smith. University of Michigan,
Ann Arbor, Mich. June 60. Contract AT(1 1-1)-
70. 39p. Order from LC. Ml $3.00, ph $6. 30.
TID-6167
Calculated and experlmenul propane njaaa spectra
_ ' ' - " ..'"T^-
Technical repor^no. VIII, ty E.
rature.
dependence upon electron voltage and sample
eport nc
ing and A. L. Wahrhaftig. University of
Utah. Salt Lake City, Utah. May 60. Contract
AT(ll-l)-82. 86p. Order from LC. Ml $4.80.
ph $13.80. TlD-6170
temperai
M. Eyri
The effect of preaaure on microgravlmetric studies
In hydrogen. Scientific paper 1 1 -0807 - 1 1 - PI, by
O. M. Katz and B. A. Uulbransen. Westing -
house Electric Corporation. Research Labora-
tories, Pittsburgh, Pa. jan 60. Contract AT-
ll-l-GEN-14. 19p. Order from LC. Mi$2.40.
ph$3.30. TID-6175
Radiation stability erf organtc liquids. Semi-annual
report no. 7 for January 1, 1960-June 30. 1960,
by L. H, Towle and R. S. Farrand. Sunford
Research Institute, Menlo Park, Calif. June 60.
30p. Order frcMm LC. Mi $3.00, ph $6. 30.
TlD-6186
On the structure and thermal decompoeltion of
"ammonium dluranate. " by K. J. Nocg and other».
National Lead Ccvnpany of Ohio, Cincinnati,
Ohio. [195?) 6p. Order from LC. Ml $1.80,
ph$1.80. TID-6228
Studiea of coordination compounda conuining Olefin
and Olefin- like Uganda. Progress report from
August 1, 1959 to July 31 1960, by B. "g:
Douglas. University of Pittsburgh, Pittsburgh.
Pa. July 60. Contract AT(30-l)-2274. 12p.
OrderfromLC. Mi $1.80, ph $1.80.
TID-6242
Eighth annual report on distribution studies between
melts and solid phases using radioactive tracers,
by W. C. Orr and others. University of Connecd-
cut. Storrs, Coon. June 60. Contract AT(30-1)-
1154. 55p. OrderfromLC. Mi $3. 60,
ph$9.30. TID-6243
Technical pr
June 16, I
1
•ess report for June 16, 1959 to
, X \ii^. F. Firestone. Western
.eserve University, Cleveland, Ohio. June 60.
Contract AT(ll-l)-685. 15p. OrderfromLC.
Mi $2.40, ph$3.30. TlD-6260
650
Uboratory studiea pertalnlag to the treatment of
TNT wastes, by E.R. Madiewa and others. Loa
Alamoe Scientific Laboratory, Los Alamos,
N. Mex. [195?]. 19p. Order from LC.
Mi $2. 70, Fh$4.80. TIO-6268
-tCy
rt on chemistry for period covering
1960, Ionics. Inc.. Cambrid^.
as report or
yl6-fulyl5,
Maaa. July 60. Contract AT(30-l)-2470
Order from LC. Ml $2.70, ph $4.80.
TID-6277
22p.
Study<
"Tin
of Inorganic salts at high temperatures.
lal technical report, by R. L. Seifert. Uni-
versity of Indiana, Bloomington, Ind. July 60.
Contract AT(11-1)-410. 6^. OrderfromLC.
Mi $3. 90. ph $10.80. TID-6289
Progreaa report on radioinduced reeln grafting for
Tune 1960. Radiation Applicadona Inc. . Long
laUnd City, N. Y. Contract AT(30-1)- 2318.
4p. OrderfromLC. Mi $1.80, ph $1.80.
TID-6321
ladirect neutron absorptiometry, by W. W. Meinke.
University of Michigan, Ann Arbor, Mich. [1957].
Contract AT(ll-l)-70. 5p. OrderfromLC.
Mi $2.40, ph$3.30. TID-6325
High concentration- ratio technique: Isottye frac-
tionation at the methyl carboo in die reaction of
cyanide ion and methyl iodide. Isotope etfecT"
under conditions of equal reagent concentrations.
by K. R. Lynn and P. E. Yai^ich. Unieersity
of Illinois. Noyea Laboratory of Chemiatry,
Urbana, 111. 1960. Contract AT(ll-l)-67. 20p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-6344
Progress report on solvent extraction for period
Kwerlng July 16- August 15, 1960. Ionics, Inc.,
Cambrid^, Mass. Aug 60. Contract AT(30-l)-
2470. 15p. OrderfromLC. Mi $2.40. ph $3. 3a
TID-6357
Proon
nic
ess report on alkali ha tide purification, Tech-
cal report no. 12i Anderaon Physical Labora-
tory, Champaign, 111. July 60. Contract AT(1 1 -
I) -544. 13p. OrderfromLC. Mi $2.40,
ph $3. 30. TID-6403
Coprecipimion from homogeneous solution,
~^^^^^ .. Gordon
ititute of Technology, Cleveland, Ohio.
Annual
and others. Case
June
lOOp. Order from
progreaa report, byH
Ins ti tut
60. Contract AT(ll-l)-582
LC. Ml $5. 40. ph$15.30.
With this la a paper on the minimum ignition tem-
perature of aluminum oxide precipitatea, by O. 1.
Milner and L. Gordon. TID-6414
Determinsttoo of yttrium and rare (Miths in inix-
njurea, Period covered July 9, 1957 to July 21,
1958, by R. R. Freeman, Jr. Michigan Chemi-
cal Corporation, St. Louis, Mich. July 58. 31p.
Order from LC. Mi $3. 00. ph $6. 30.
TID-6417
Spectrographic analysis of impuritiea In pure yttri-
um oride. III. Studies on 'selective volatilization-
Period covered September 12, 1958 to NovembeF
3. 1958, by A. B. Whitehead. Michigan Chemi-
cal Conxuration, St. Louia. Mich. Nov 58. 7p.
Order from LC. Mi $1.80. ph $1.80.
TID-6419
Spectrographic analysis of impurities in pure yttri-
um oxide (revised method). Period covereo Octo-
ber 4. 1957 to December 6, 1957, by A. B.
Whitehead. Michigan Chemical Corporation,
St. Louia, Mich. Dec 57. Revised January 7,
1958. Decl. February 6, 1959. 16p. Order
from LC. Mi $2. 40, ph $3. 30. TID-642t
Evaluation of xenotime ore as a source of feed for
the rare earth plant.
h plant. Period covered July 26,
ml>er 3, 1957, by J. R. Morton.
1956 to Septei
Michigan Chemical Corporation, St. Louis,
Mich. Nov 57.
Order from LC.
Decl. February 6, 1959
Mi $1.80, ph$1.80.
TID-6422
4p.
The spectrgihotonaetric snalysiB of rare earth mix-
tu^8- Period covered Febniary 25 to August 30,
1957, by C. G. Shultz. Michigan Chemical Cor-
poration. St. Louis, Mich. Oct 57. Decl.
February 6, 1959. 6p. Order from LC.
Mi $1 . Sa ph $1 . 80. TID-6423
Determinatiai of yttrium in rare earth coooentra-
tions by x-ray fluoreacence. Period covered
Mardil3. 1^57toJuly26, 1957, by C. C.~5trulu.
Michltan Chemical Corporation. St. Louis,
Mich. Oa 57. Decl. February 6, 1959. 7p.
Order from LC. Mi $1 . 80. ph $1 . 80.
TID-6425
A spectrophotometric determination of silica in high
purity yttrium oxide. Period covered August 16?"
1 957 to September 30. 1957. Michigan Cbemical
Corporation, St. Louia, Mich. Sep 57. Decl.
February 6, 1959. ^. Order from LC.
Mi $1.80. ph $1.80. TID-6426
Spectrographic method of analysis for yttrium in
Period covered December 3
ores.
March 1, 1957, by A. B. Whitehead
1956 to
Michigan
Chemical Corporation, St. Louis. Mich. Apr
57. Decl. February 6. 1959. 14p. Order from
LC. Mi $2. 40. ph $3. 30. TlD-6431
651
The analysis erf or^a for yttrium by x-ray floures-
cenae. Period covered January 14 to April 2T,
1957 by C. G. 'Shultz. Michigan Chemical Cor-
poration, St. L0ul8, Mich. Apr 57. Decl.
February 6, I9$9. 9p. Order from LC.
Mi^l.SO, ph$1.80. TID-64a2
Spectrographic analysis of impurities in pure yttri-
purl
um oxide. Perlbd covered March I. 1957 to
May 30. IJg7 a>d July 1 1957 tojuly 15. r9S7,
by A. B. Whiteriead. Michigan Chemical Corpbra-
tioo. St. Louia. Mich. July 57. Decl. February
6. 1959. 8p. (;h:t)er from LC. Mi $1.80.
ph$1.80. I TID-6433
Pilot plant evaluatlbn erf a Brazilian yttrium concea-
trate aa rare earth plant feed, rerlod covere3"
March 5, 1957 to June 11, 1957. by J. R. Morton.
Michigan Chemical Corporation, St. Louis.
Mich. Aug 57. Revised October 23, 1957. Decl.
Febniary 6, 19$9. 2p. Order from LC.
Ml $1.80. phJi.SO. TlD-6434
Pre
ratloo erf purf europium by electrolyla.
rlod covered July 23, 1957 to July 24. r957. by
J. R. Morton. Michigan Chemical Corporadon,
St. Louis, Mid}. Aug 57. 2p. Order from LC.
Ml $1.80. ph $11.80. TID-6436
The analysis of sotne volatile phosphorus compounds
f gas -liquid cliromato^apoy, py S. H. Shipotof-
cy Includes papers: "Caa chroma cographic
by gas -liquid chromato^a
sky. Includes dapers: ~G
analysis of sony volatile
by Sl H. Shlpotifsky and H. C. Moeer. Reac-
tlona of tritium atoms witfi frozen hydrocarbons,
by R. D. Shorei and H. C. Moeer. Kansas
State Universlt]if. Manhatun. N. Y. I960. Con-
tract AT(11- 1)- 584. 22p. Order from LC.
Ml $2.70. ph $4.80. TID-6437
Effect of structure on the stereochemistry of elec-
trode reactions i Monobromo C4-dibaalc acida
and esters, by f. J. Elvlng and others. Pennsy-
lvania State UnU/erslty. University Park, P«. ,
and University erf Michigan, Ann Arbor, Mich.
Aug 60. Contract AT(30-l)-822. 25p. Order
from LC. Ml $8.70, ph $4.80. TID-6441
Diffusion -kinetics In radiation chemistry. I.
Generalized fortnulation and crltlclam of thffu-
sloo model, by X. Kuppermann and G. G. Bel-
ford. University of Illinois, Noyes Laboratory
of Chemistry. Urbana. HI. [1960] Contract AT
(11-1)-691. 5te. Order from LC. Mi $3.60,
pii $9. 30. I TID-6456
T
An Improved laborjitory cold-trap and procedure
for reducing personnel hazard, by i. G. Burke
Oak Ridge Gasebus Diffusion Plant, Oak Ridge,
Tenn. Sep 58. Revised July 15. 1960. 6p.
Order from LC. Ml $1.80, ph $1.80. TID-6470
The faradaic admittance of electrochemical
?Que
Bauer and Philip J. Elvlng
esses, nr The free
ilproc-
ncy dependence, by H. H.
University <rf Michi-
gan. Ann Arbor. Mich. June 60. Contract AT
(ll-l)-70. 17p. Order from LC. Ml $2.40.
ph$3.30. TID-6474
Thermodynamics of the monohydrogen dlfluorldes.
ni. mat capacities erf cesium, rubidium, and"
thallium monohydrogen dlfluorldes from 7 to
Westrum. Jr
oge
A. Burney and E. E.
Tlniveralty of Michigan, Ann Arbor,
Mich. [I960]. 19p. Order from LC. Ml $2.40,
ph $3. 30. TID-6509
Photogalvanlc and photovoltaic effects with anodlzed
zirconium and niobium electrodes, by W. M.
Graven and others. University erf Oregon,
Eugene, Ore. Aug 60. Contract AT(45-1)- 535.
45p. Order from LC. Mi $3. 30, ph $7. 80.
TID-6514
Analytical chemistry at low concentrations, by J. T.
Stock and M. A. Fill. University of Connecticut,
Storrs, Conn. Aug 60. Contract AT(30-1)- 1977.
31p. Order f reus LC. Mi $3.00. ph $6.30.
TID-6525
The direct measurement of local absorbed dose by
caloriroetry. Investigation of the relation be-
tween the energy absorbed In a medium exposed
phoephorus cc«npounde. In a ga
H. C. Moeer. Reac- medlun
to x-rays and electrons, die ionization prcxhiceB
In a gas cavity chamber In the aatne absorbing
um. and the oxidation of ferrous sulfateln
the frlcke dosimeter. Annual progress reponfor
lulyl, t959--]une30 1960, Eyf.
Slcian-ICetterlng Institute for Cancer Research
ogress repon
. S. Lau^lin.
New York, N. Y. Aug 60. Contract AT(30-1)-
1451. lOp. Order from LC. Mi $1.80.
ph$1.80. TID-6534
Invest!
tions relating to gas ph^se detonations.
Final report, by M. G. Zabetakls and P. C. Glb-
son. Bureau of Mines. Explosives Research
Laboratory. Pittsburgh. Pa. [ndj. 42p. Order
from LC. Ml $3.30. ph $7.80. TID-6546
Thermodynamics of the monohydrogen dlfluorldes.
I. Decompoeltion reaction, fusion, phase transi
tlon and electrical conductivity of f -potassium
ty of i-potii
M. C Davli
moqohydrogen dlfluoride, by ^. iL bavls.and
E. F. Wesmun. Jr. University of Michigan.
Ann Arbor. Mich. (195?]. Contract AT(l 1-1)-
70. 31p. Order from LC. Mi $3.00. ph $6. 30.
TID-6552
Synthesis erf organic compounda. Final report, by
H. Oilman. Iowa State University of Science
and Technology, Ames, Iowa. [1959?]. Contraa
AT(ll-l)-59. 19p. Order from LC. Ml $2.40,
ph $3. 30. TID-6586
652
A sroall-scale ui^nlum hexaflucyide plant, by S. H.
Smiley. Oak Ridge Gaseous Diffusion Plant.
Tenn. Dec 59. 6p. Order from LC. Mi $1.80,
ph$1.80. TID-6635
The effect of certain variables on the polarization
capacity of ziroanium. Technical report no.
300CIII, by A. B. Johnson and others. University
of Utah, Institute for th Study of Rate Proceases,
Salt Lake City, Utah. Oct 60. Contract AT(11-
l)-82. 22p. Order from LC. Ml $2.70,
jA$4.80. TID-6685
Coalescence and dispersion rates In aglMted liquid-
liquid systems, by J. H. Vanderveen. Oniver-
airy of California. Lawrence Radiation Labora-
tory, Berkeley, Calif. Dec 60. Contraa W-
7405-eng-48. 56p. Order from OTS. $1.25.
UCRL-8733
The cross sections for the formation of astatlna
Isotopes nade by the bombardment of Bl^P^
widiHe^ by E. T. Strom. University of Cali-
fornia. Lawrence Radiation Laboratory, Berke- >
ley. Calif. Nov 60. Contract W-7405-eng-48.
31p. Order from OTS. 75 cents, UCRL-9372
An lnterfere«netrlc etudy erf atomic mercury spec-
tral linea. by R. Berg. University of California,
LawrencxT Radiation Laboratory. Berkeley,
Calif. Dec 60. Contract W-7405-eng-48. 2^.
Order from OTS. 50 cents. UCaiL-9512
EqMllibrium consunts for the formation of poly -
nuclear tridentate 1:1 chelatea In uranyl-mailate,
-citrate, and -tartrate systems. Deformation
of the uranyl entity, by I. Feldman and otfaersT
University of Rex:nester, Atomic Energy Project,
Rochester, N. Y. Oct 59. Contract W-7401-
eng-49. 33p. Order from LC. Mi $3.00,
ph $6. 30. / UR-S59
EsBort on phase VI tests. jSpeciflcatlona]T -474945
Hydrazlpe proof test. [Specification lT-474946
afte
1
Ftux recombination proof teat, by Y. \i. Solomon
and P. Cohen. Westinghouse Electric Corpora-
tion, Atomic Power Division, Pittsburgh. Pa.
May 54. Decl. with deletions Arrll 29. 1957.
16p. Order from LC. Ml $2.40, ph $3. 30.
WAPD-CP-460(Del.)
Use of radiochemistry and mass si
le 01 radiochemistry and mass spectrometry for
Kiel depletion studies, by J. E. Hudgens. West-
inghouse Electric Corporadon. Bettis Plant,
Pittsburgh, Pa. 1960. Contract AT-U-l -GEN -
14. 14p. Order from LC. Mi $2.40. ph $3. 30.
WAPD-T-1113
Nuclear ntaterials control system (NMCS). Phase II.
Analyst performance on synthetic Purex 8anq)leB.
by H. Ginsburg and C. C. Hiomas, Jr. WesUng-
., house Electric Corporation, Atomic Power De-
partment, Pittsburgh. Pa. Jan 60. Contract
AT(30-1)-2176. 6lp. Order from LC.
^ Mi $3.90, ph $10.80. WCAP-6036
The determinatlc>n of Aettluro and uranium aa trace
impurides in beryllium tneul, by W. C.
bietrich. Union Carbide Nuclear Company^
Dlvlaion of Union Caziilde Corporation, Y-12
Plant, Oak Ridge. Tenn. Dec 60. Contract W-
7405-eng-26. 21p. Order from OTS. 50 cents.
Y-1329
Controlled Thermonucleor Processes
Quarterly report oovering the period July 1 - Sep-
tember 30, 1960, by L. Goldberg and others.
Princeton University. Project Matterhorn.
I Princeton, N. J. Oct 60. Contract AT(30-1)-
1238. 34p. Order from OTS. $1.00.
MATT-Q-12
Thermonuclear project semiannual progress report
ending July 31, 1960. by A. H. Snell
ject semiannual
for period en^ng July 31,
and e>ther8. Oak Ridge National Labora tory .
Oak Ridge, Tenn. [nd]. Contract W-7405-eng-
26. 142p. Order from OTS. $2.75.
lit
Effect of eneri
in an
ORNL-3011
degradation on Ae crlrtcal current
device, by T. K. Fowler.
Oak Ridge National Laboratory. Oak Ridge. Tenn.
[nd]. Contract W-7405-eng-26. 20p. Order
from OTS. 50 cents. ORNL-3037
Criticolify Studies
Summary listing of subcrltical measurements of
heterogeneoOffi water -uranium lattic»» made at
Hanford, by R. C. Lloyd. General Electric
Company, Hanford Atomic Products Operation.
RichUnd, Wash. June 60. Contract W -31 -109-
eng-52. 53p. Order from LC. Ml $3. 60.
ph$9.30. HW -65552
Multiplication of neutrons in small spheres of active
material, by C. Richman. Los Alamoe Scienti-
fic Laboratory. N. Mex. Apr 45. Decl. August
2, 1960. 18p. Order from LC. Mi $2.40,
ph $3. 30. LA-267
653
The Kukla prompt critical assembly. Hazarda
aununary repogt, by E. R. Chriatle and B. W.
Mar. Univerality at California, Lawrence Radia-
tion Laboratory,
Contract W-74^-eng-48
OTS. $2. 00.
Livermore, Calif. Feb 60.
86p. Order from
UCRL-6105
Critical mass stifles. Part VT, by D. CalUhan
and others. Oak Ridge Nadooal Laboratory,
Y-12 Area, Oak Ridge, Tenn. Aug 51. Decl.
with deletions June 17, 1960. Contract W-7405-
eng-26. 32p.
ph$6.30.
Order from LC.
Mi $3. 00,
Y-801(Db1.)
Engine4ring and Equipment
IN SrrU traaers project. Quarterly progri
pcHTt no. 2 for J^uie - August 1959. Jonn
(William H) Laboratories, Inc
ess re-
August 195^. Johnalon
Lafayette, Ind.
1959. Contract AT(ll-l)-650. 32p. Order
fnxnLC. Ml |3. 00, ph $6. 30. AECU-4383
Remote nnaintenance experlnaenta 1 work on a reac-
tor system Pimip, by W. B. McE)onald and othera.
Oak Ridge Natloial Laboratory, Oak Ridge, Tenn.
Apr 58. 35p. Order from LC. Mi $3.00.
phf6.30. CF-58-4-93
Study of ouMge exj>erience with selected boiler and
turbine generaror units, by M. L. Myers. Oak
Ridge National 'Laboratory, Oak Ridge, Tenn.
Mar 60. 38p. Order from LC. Ml $3.00,
I>h$6.30. CF-60-3-56
.no"
Instruction manual, mercury relay pulse generator
model q- 121 2C; by g" Pkirstein Oak Ridge
National Laboratory, Oak Ridge, Tenn. Sep 60.
lOp. Order frqmLC. Mi $2. 40, ph $3. 30.
I
CF-60-9-67
Momentum and he<t transfer to a fluid flowing
turbulently in a^pipe, by R. ]. Hefner" Dak
Ridge Natinnal Latxsratory, Oak Ridge, Tenn.
Sep 60. 79p. Order from LC. Mi $4. 50,
ph$12.30. I CF-60-9-69
Design basis for peddle pumpe, by D. S. Webster
tnd C. L. Williamson. E. I. du Pont de Nem-
ours k Company, Savannah River Laboratory,
Aiken, S. C. jiin 60, Contraa AT(a7-2)-l.
21p. Order fr<»n OTS. 75 cents. DP-451
Contlnuoua solvent washing hydraulic characteristics
of the turbine contactorT by D. S. Webster and
C. L. Williamaon. E. I. du Pont de Nemours k
Company, Savannah River Laboratory, Aiken,
S. C. Sep 60. Contract AT(07- 2)- 1. 20p.
Order from OTS. 50 cents. DP-506
Leakage o< water frcan valve stuffing boy*, by F. C.
Apple. E. I. du Pont de Nemours and Company,
Savannah River Laboratory, Aiken, S. C. Jan
61. Contract AT<07 -2)1. 12p. Order from
OTS. 50 cents. DP-538
A dynamic digital delay generator for use in neutroa
chopper e;q)eriments, by W. M. Lopez and
others. General Atomic Divlalon, General Dy-
namics Corporation, San Diego, Calif. Sep 60.
Contract AT(04-3)-l67. Up. Order from LC.
Ml $2.40, ph$3.30. GA-1585
Two-phase flow rates and preaaure drops in curved
tubes, by H. L. Polu. Goodyear Atomic Cor-
poratioD, Portsmouth, Ohio. Jan 60. Contract
AT(33-2)-l. ISp. Order from LC. Mi $2.40.
ph $3. 30. GAT-T-679
Operating manual for 105-C metal examination
facility, by J. M. Pouts. General Electric Com-
pany, Hanford Atomic Products Operation, Rich-
land, Wash. May 60. Contract AT(45-1)- 1350.
58p. Order from LC. Mi $3. 60, ph $9. 30.
HW-58220(Rev.)
Portable radiation instrumenution standardization,
by W. G. S()ear. General Electric C(Mnpany,
Hanford Atomic Products Operation, Richland,
Wash. July 60. 35p. Order from LC. Mi $3. 00,
ph $6.30. HW-60404 (Rev.)
Critical pressure ratio for a nozzle with two-phaae
fog flow, by W. J. Love. General Electric Com-
pany, Hanford Atomic Products Operation, Rich-
land, Wash. Mar 60. 13p. Order frcrni LC.
Mi $2. 40, ph$3.30. HW-64269
Time-temperature excursions of film blanketed fuel
elements as measured by diermocouples and"
voltage taps, by C. I— Gregory. Knolls Atomic
654
Power Laboratory, Schenecudy, N. Y. [1958).
31p. Order from LC. Mi $2.70, ph $4.80.
KAPL-RDTR-308(Pl. VI)
Heat transfer for 7 1/4" -pitch ribbons at low flowa,
by C. L. Gregory. Knolls Atomic Power Labori-
tory, Schenectady, H. Y. Jan 60. 96p. Order
frwn LC. Mi $5.40, ph $15. 30.
KAPL-RDTR-310(Pl. 10
Remote control equipment for plutonium meul
production, by W . C. Hazen. Loe Alamos Scien-
tiflc Laboratory, Loe Alamos, N. Mex. Oct 51.
Decl. with deletions June 9, 1960. 221p. Order *
from LC. Mi $9.90, ph $34.80. LA-l387(Del.)
A study of various types of freeze type liquid metal
Valves, byE. O. Dryer. Atomics Internationsl
DiviaiOG of North American Aviation, Inc. ,
Canoga Park, Calif. July 58. l^. Order from
LC. Mi $2. 40, ph$3.30.
NAA-SR -Memo- 2920
Ttermal cycling and leakage teaa of 12- inch sodl-
ian valves, by C.J. Baroczy. Atomics Internation-
al. Division at North American Aviation, Inc. ,
Canoga Park, Calif. Sep 59. 30p. Order from
LC. Mi $3.00, ph$6.30.
NAA-SR -Memo- 3961
Stress relieving fitting— stress evaluation, byW.F.
Anderson! Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. Aug 59. 6p. Order from LC. Mi $1.80,
ph$1.80. NAA-SR-Memo-4268
Pinal performance tests of two-coolant -region sodi-
umpump abaft freeze -sea Is, by F. O. Streck.
Atomics International. Division of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. Feb 60.
4^. Order from LC. Mi $3. 30, ph $7.80.
NAA-SR-Memo-4442
Teat of a 24-inch diameter model of the HNPF
oerrobend seal, by B. W. Admire. Atomica
International, th vision of North American Avla-
tiOQ, Inc. , Canoga Park, Calif. Nov 59. lOp.
Order from LC. Mi $2. 40. ph $3. 30.
NAA-SR -Memo-4682
Flexure teeta of a helically coiled tfaermocotq)le, by
iC. H. Dearborn. Atonilcs International. Divi-
iion at North American Aviaion , Inc. , Canoga
Park, Calif. Dec 59. 4p. Order from LC.
Mi $1.80, ph$1.80. NAA-SR-Memo-4717
Interim report on filter screening tests, by S. J.
Sawyer. Atomics International. Division at
North American Aviation, Inc. , Canoga Park,
Calif. Mar 60. 13p. Order from LC.
Mi $2. 40, ph$3.30. NAA-SR-Memo-4982
Compilation of experimental forced-convection,
quality burnout dau with calculated Reynolds
numbers, by H. Firstenberg and others. Nu-
clear Development Corporation of America,
White Plains, N. Y. June 60. Contract AT(30-
1)-2303(DC). 60p. Order from LC. Mi $3. 60,
I)b$9.30. NDA-2131-16
irch Laboratories, Pittsburgh, Pa. A{>g 60.
Contract AT(30-1)-2176. 13p. Order from LC.
Mi $2.40, ph$3.30. NYO-2899
The development of a theory of pulse column flood-
ing behavior. Progress report no. 10 on the "
pertonnsnoe of contactors for liquid- liquid ex-
traction, by F. P. Pike and E. E. Erickson.
North Carolina Sute College, Raleigh , N. C.
Apr 55. Contract AT(40-1)-1320. 76p. Onler
fromLC. Mi $4.50, ph $12.30. ORO-288
The ineaaurement of dynamic pressure drop in a
pulse column. Progress report no. 12 on die
performance of conuctors for llquld-llquid"ex-
traction, by B. E. Erickson and others. North
Carolina State College, Raleigh, N. C. Apr 55.
Contract AT(40-1)- 1320. 99p. Order from LC.
Ml $5. 40, ph $15. 30. ORO-289
Tlie development of a puiae -column sampling tech-
nique to overcome entrainment. Progress report
no. 13 on the oerfo nuance of contactors for
liquid- liquid extraction, by E. E. Erickson and
others. North Carolina Sute College, Raleigh,
N. C. Apr 55, Contract AT(40-1)-1320. 55p.
Order from LC. Mi $3.60, ph $9. 30.
ORO-290
Comparative performance of e3q)aoded meul places
in a pulse column extragor. Thesis, by J. C.
Park. Progress report ift). 16 on die performance
of conuctors for li^ild-liq^id extraction. North
Carolina State CoU^, Raleigh, N. C.
Contract AT(40-1)-1320. 151p.
LC. Mi $7.50, ph$24.30.
1956.
Order from
ORO-291
Liquid-liquid heat transfer in a pulse column.
Thesis, by S. C. Li. Progress report no. 18 on
the performance of contactors for liquid- liquid
extraction. North Carolina Sute College,
Ralel^, N. C. 1957. Contract AT(40-l)-l320.
136p. Order from LC. Mi $6. 90, ph $21. 30.
ORO-293
Agiuted liquid- liquid heat transfer. A study of the
influence of temperature driving force on tfie
heat transfer coefficient in a jHused, counter-
current, sieve-plate conuctor. Thesis, by~
R.P. Gardner. Progress report no. 21 on the
performanoe of (^tactors for liquid- liquid ex-
traction
liqul
North Carolina Sute doUege, Raleigh,
^r~1958. Contract AT(40-1)- 1320. 117p.
Order from LC. Mi $6.00, ph $18. 30.
ORO-295
Materials and process variables and their effect
on conuct resistance, by L. K. Jones. Sandia
Corporation, Albuquerque, N. Mex. May 60.
18p. Order from LC. Mi $2. 40, ph $3. 30.
SCR-190
Integrating the quality control contribution in re-
search and development operations, by L. ^[7
655
Snodgrasa. SatKUa Corporation, Albuquerque,
N. Mex. Jan 61. 17p. Osier frGm OHTS.
75ceot8. SCnM-419-60-25
The line recorder 'meM apectrometer >a >n anelyti-
cal tnatrun^nt, by W. O. Gentry. Oak Ridge
Caseous Diffusion Plant, Oak Ridge, Tenn.
Sop 58. Contract W-7405-eng-26. 42p. Order
from LC. Mi $3.30. ph $7.80. TID-6529
Progress report for research on heat transfer to
fluida flowing tliroug^ non-circular dianoels.
Period covered March to September 1960, by
B. R.G. EckertandJ. L. Novotny. University
(rf Minnesota, Heat Transfer Laboratory, Min-
neapolis, Minn, Sep 60. Contract AT(ll-l)-659.
S5p. Order frtto LC. Mi |3. 60. ph $9. 30.
TID-6566
High stability LC <|aclllator for use with a capacttlve
pressure sensing element. Theaia, by A. J.
Eldridge. University of New Mexico, Albuquer-
que, N. Mex. 1955.
Mi $4.80, ph$],3.80.
88p. Order from LC.
TID-6601
i
A versatile, horiz»iul electron diffraction unit
with inmroved t^esolving power, by ). F.
McUu^n and W. W. Harris. Oak Ridge
Gaseous Diffusion Plant, Oak Ridge, Tenn. Apr
60. Decl. October 5, 1960. Contract W-7405-
eng-26. 23p. Order from LC. Mi $2.70,
pii$4.80. I TID-6606
Green's function for a circular ring widi radiation
type boundary conditions, by]. F. Heyda. Gen-
eral Electric Ohnpany, Aircraft Nuclear Pn^l-
aion Department, Cincinnati, Ohio. Aug 60.
Contracta AF 33(600)- 38062 and AT(ll-l)-171.
lip. Order from LC. Mi $2. 40. ph $3. 30.
TID-6648
The effects of Increaaing mass spectrometer ion
accelerating voltagesT by A. Langdon and W. C.
Hart. Oak Ridge Gaseous Diffusion Plant, Oak
Ridge, Tenn. Pteb 60. 7p.
Mi $1.80. ph$l,80.
Order from LC.
TID-6679
A new saturable transformer measures direct cur-
rent through conductors in the vicintiy of large"
stray OMCoetic ijle Ida, by A. Windsor. Univer-
sity of California, Lawrence Radiatioa Labora-
tory, Berkeley, Calif. Oct 60. Contract W-7405-
eng-48. 14p. Order from OTS. 50 cents,
UCRL-9464
The E X B discharge as a aource of ions,, by K. W.
Ehlera. Univeriity of California, Lawrence
Radiation Laboratory, Berkeley, Calif. Jan 61.
Contract W-7405-eng- 48. 26p. Order from
OTS. 50 cents. UCRL-9503
Remote surface Inspection technlquea, by R. A.
betz. Westingbcxise Electric Corporation, Bettia
Atomic Power Laboratory, Pittsburgh, Pa.
1960. Contract AT-ll-l-GEN-14. 9p. Order
Irom LC. Mi $1.80, ph $1.80. WAPD-T-1176
Fundamenttls of radiography, by R. C. Barry.
Westinghouse Electric Corporation, Bettis Atoa-
fl ic Power Laboratory, Pittsburgh, Pa. 1960.
Contract AT-ll-l-GEN-14. 23p. Order from
LC. Mi $2.70, ph$4.80. WAPD-T-1177
Nuclear materials control system (NMCS) phase II
reas report for the period ending June 30
^
Westinghouse Electric Corporation, Atom-
ic Power Department, Pittsburgh, Pa. July 60.
Contract AT(30- 0-2176. 42p. Order from LC.
Mi $3. 30. ph$7.80. WCAP-6043
Geology and Mineralogy
Seiamolo^cal investlmtlons at the Hanford area,
1958-1959, by F. Neumann. General Electric
.- Company, Hanford Atomic E>roduct8 Operation,
' Richland, Wash. Nov 59. Includes reprint:
Oscillator responses to eardiquake motiotia7
Trend Engineering University, Wash. Coiitraa
- W-31-109-Eng-52. 96p. Order from LC.
Mi $5.70, ph $16.80. HW-63832
Re<x)nnats8ance tor uranium in the Uinta Basin of
Colorado and Utah, by E. A. Noble and E. C.
Annes, Jr. Exploration Division, Grand Junction
Operations Office, AEC, Grand Junction, Colo.
Jan 57. 22p. Order from OTS. 50 cents.
RME-94
A »tudy of Nevada test site wind variability, by
W. Reed. Sandla Corporation, Albuquerque,
Osier from LC.
SC-4144(TR)
T
N. Mex. Mar 58. 43p.
Mi $3. 30, ph$7.80.
Analyses d ground water from Rainier Mesa,
Nevada test site, Nye County, Nevada, by A.
Clebsch, Jr. and F. B. Barker. Geological
Survey, Washington, D. C. May 60. 23p.
Order from LC. Mi $2.70, ph$4.80.
TBI-763
Correlation and chronology of ore deposits and
volcanic rocks. Annual progreaa report no. 2,
by P. E. Damon and othera. University of "
Arizona, Geochronology, Laboratory, Tucson,
Ari2. July 60. Contract AT(ll-l)-689. 114p.
Order from LC. Mi $6. 00, ph $18. 30.
TlD-6482
656
Htyilcal properttee of salt aamplee. Final report.
" R. S. uuldo and S. E. Werner. University of
California, Lawrence Radiation Laboratory. '
Uvermore. Calif. July 60. 14p. Order from
LC. Mi $2. 40. ph $3. 30. UCRL-6069
Surrey and selected bibliography of reactor fuel
element assay syatemsr Nuclear nrkaterials
^ tay syatei
trol ayatem (NMCSy7
and D. G. Gardner.
con-
niase II, by S. L. Ruby
Wescingjiouse Electric
Corporation, Atomic Power Department. Pitta-
bur^ Pa. June 59. Contract AT(30-l)-2152.
41p, Order from LC. Mi $3.00. ph $6. 30.
WCAP-6014
Health and Safety
Environmental radioactivity at Argonne National
Laboratory. Report for the year 1959, by J.
Sedlet. Argonne National Laboratory, Argonne,
ai. Jan 61. Contract W- 31 -109- eng- 38. 50p.
Order from OTS. $1.25. ANL-6282
Preliminary studies of acayenglng ayatema related
to radioactive fallout. Letter report no. 7 cover-
ing period Apr 11 I to May 31 19W. byj. DT
StoochamandJ. Rosinski. Illinois Institute of
Technoiogy, Armour Research Foundation,
Chicago. III. June 59. Contract AT(11-1)- 626.
^ Order from LC. Mi $1.80, ph $1.80.
ARF-3127-7
Comparative nuclear effects of biomedical interest,
by C. S. White and others. Lovelace Foundation
for Medical Education and Research, Albuquer-
que, N.Mex. and the U. S. Atcxnlc Energy Com-
mission, Division of Biology and Medicine,
Washington. D.C. Sep 60. 84p. Order from
OTS. $1.00. CEX-58.8
A study of the contribution of the Rala proceaa to
atmoepherlc conamlnatlon of ORNlI by R. L.
Bradahaw and W. D. Cottrell. Oak Ridge Nation-
al Laboratory. Oak Ridge. Tenn. Nov 54. Decl.
March 14, I960. Contract W-7405-eng-26. 54p.
Order from LC. Mi $3. 60. ph $9. 30.
CF-54-11-186
Dlaaolver off-gaa and rare gas plant hazarda, by
J. M. Holines. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Nov 59. lOp. Order from
LC. Mi $1.80. ph$1.80. CF-59-11-133
Cootatnination of shipping cask and storage canal
water by fuels Irradiated in pressurized water
reactors --a review of pertinent subjects. 5y"
L J. King. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Mar 60. 21p. Order from
LC. Mi $2.70, ph $4.80. C F-60-3-49
ced RQG y»l"f* for radioiodine isotopes in
'oods, by J. H. Horton. E. L du Foot de Nem-
ours k Company, Savannah River Laboratory,
Aiken, S. C. Oct 60. Contract ATX07-2)-l.
18p. Order from OTS. 50 cents. IX*-S24
Evaluation of plastic fllma tor protective suiting,
by A. E. Symonds, Jr. E. 1. du Pont de Nem-
ours k Company, Savannah River Laboratory,
Aiken. S. C. Nov 60. Contract AT(07-2)-l.
18p. Order from OTS. SO cents. DP-S28
Health instrument divisions quarterly progress re
nment acuylties fa
Taardil»51, by H. M. Parker. Han
quai
irt on research and development acuylties for
y- Mardil»51 by hTm. Parke "
orks. Richland, Wash. Apr 51. Decl.
March 2, 1960. Contract W-31-109-Eng-52.
30p. Ortler from LC. Mi $2. 70. ph $4. 80.
HW-20666
port on
January
ford Wo
Radiological assistanoe plan, by P. Griffiths and
G. J. Ball. Idaho Operations Office, Health and
Safety Division. ABC. Idaho Falls, Idaho.
June 60. 58p. Order from LC. Mi $3.60,
ph$9.30. IDO-12013
Method of calculating lung doee received frcwn a
confined cloud of j-adlaictive gaa, by D. E.
Hankins and W. C. King. Phillips Petroleum
Conqjany. Idaho FalU, kkho. Dec 60. Con-
tract AT(10-l)-205. 27p.
SO cents.
Order from OTS.
IDO-16632
Health physloB manual of enylronroental monitoring,
by M. R. Kennedy. Kiolla Atomic Power Labor-
atory, Schenectady, N. Y. June 60. Contract
W-31-109-ENG-92. 71p. Order from LC.
Mi $4. 50. ph $12. 30. KAPL-A-HP-6
Evaluation of radioactive fallout. Interim progress
report, by L. P. Salter. 'Nuclear Science and
Engineering Corporation, Pittsburgh, Pa. Feb
60. Contract AT(30-I)-2420. 46p. Order from
LC. Ml $3. 30. ph $7.80. NSEC-22
Preliminary atudies of scavenging systems related
to radioactive fallout. Letter~report no. 4 cowr-
IngperlodOctober 1 toDeceinber 1, 1958, by
J. D. StodAam andj. Roeinski. Illinois Insti-
tute ol Technology, Armour Research Foundation,
Chicago. 111. Dec 58. Contiract AT(11- l)-626.
3p. Order from LC. Mi $1.80, ph $1.80.
TID-6117
657
Preliminary
•tucuis of
BoiyenKlng aytema rcUited
to radioactive ftillout. betoer report no. 5 caoyer-
Ing period December 1 1958 to January 3171^5^,
by J. D. Stockham and J. Roainskl. Illinoia In-
Btltute al Techqology, Armour Research Founda-
tion, CJiicago, 111. Feb 59. Contract AT(1 1-1)-
626. 6p. Ordqr from LC. Ml $1.80. phll.SO.
TlD-6118
l.^>per atxnoephere momtoring progri
" ■ iWstl. 1
as
. ^_^_^ am. Pri
rqwrt go. 9, covering period Aiyus
ifaTOugh October 31 1959, by J. ftiumatark and
odiers. General Mllla, Inc. , Minneapolis,
Minn. June 60. Contract AT(1 1-1)- 401. 4lp.
Order from LCI Ml $3. 30, ph $7.80.
TID-6207
A ahlelded ooottiner for transporting radioactive
apent fuel, by a. B. Bligs. Knouia Atomic Power
Laboratory, Schenectady, N. Y. July 60. 6p.
OrrierfromLC Mi $1.80, ph $1.80.
TII>-6395
Stiidiea of nuclear debria in precipitation. Quarter-
lyprogreaa report no. 4. laotopee, Inc.7 Weat-
wood, N. J. July eo. Contract AT(30-1)-2415.
S7p. Order from LC. Ml $3. 60, ph $9. 30.
TII>-6485
Zirconium, Zlrol»y. and hafnium safe practice
guide for shlppijiiig. storing, handling, proceseing
and acrap dlapogal. by W. W. Allison. Westing-
house Electric (tkjrporation, Bettia Atomic
Power Laboratory, Pittsburgh, Pa. Dec 60.
Contraa AT-U'-l-GBN-U. 30p. Order from
OTS. 75 cents. WAPD-TM-nOlev.)
Neutron doee calibration of indium personnel doel-
I pei
meters for proi^-crltical metal bursts, by
J. W. Wachter And L. C. Enaerson. Union Car-
bide Nuclear Company, Y-12 Plant, Oak Ridge,
Tenn. Mar 56. Decl. with deletions August 13,
1959. Contract W-7405-eng-26. 31p. Order
from LC. Ml $$. 00, ph $6. 30. Y-1092(DeL)
nstruments
A tow dead- time Mtitron- counting system, by R. J.
Epstein and D. C. Thompson. Argonne National
Laboratory, Argoooe. 111. Jan 61. Contrart W-
31-109-eng-38, 16p. Order from OTS. 50 cents.
ANL-6292
Detection of U^" buildup in separations processes
by neutron muldpiication, by A. C. Lapaley.
E. I. du Pont de Viemours k Conpany, Savannah
River Laboratory, Aiken, S. C. Dec 60.
f
Contract AT(07-2)-L lOp. Order from OTS.
50 cents. DP- 533
A tranaltofized pulae height analyzer for gamma
spectroecopy, by R. T. Graveson. NewYork~
C^ratiana Office, Health and Safety Laboratory
AEC, New York, N. Y. Mar 59. 24p. Order '
from LC. Mi $2.70, ph $4.80. HASL-59
Ana
■log and digim readout on an IBM output writer.
byR. T. Graveson. New York Uperationa Office,
Health and Safety Laboratory, AEC, New Yortc,
N. Y. Sep 60. 15p. Order from LC. Ml$2.40,
ph $3. 30. HASL-94
Studies in micromeritics. I. Particle deposition in
cooduita as a source of error In aerosol sanq)l-
Ing, by A. K. Poetma and L. C. Schwendiman.
General Electric Company, Hanford Atomic
Products Operation, Richland. Wash. May 60.
Contraa AT(45-1)-1350. 24p. Order from LC.
Ml $2.70. ph$4.80. HW-65308
Tlie development of a beu-ray particle aize analy-
zer. A new instrumental technique for automatic
particle size analyaia. C^iarterly technical
' atatua report for the period January 15- -April
15, I960, by S. Z. Lewlnatidl. Conner. Evani
Research and Development Corporation, Nefr
York, N. Y. Contract AT(30-l)-2372. 26p.
Order from LC. Ml $2.70, ph $4.t0.
NYO-2656
Thermocoiyle res«irch to 1000^ - Fina 1 report
November 1, 1957, through Tune 30, 1959. 5y
J. F. Potts, Jr. andD. LTMcBlroy. Oak Ridge
National Laboratory, Oak Ridge, Tenn. [nd].
Contract W-7405-eng-26. 155p. Order from
OTS. $2.75. ORNL-2773
Interim repwt on development <rf design criteria for
relays. This report covers the period 1 Septem-
ber to 31 October 1960, Sandia Corpora don,
Albuquerque, N. Mex. Dec 60. (Ap. Order
from OTS. $2.00. SC-4530(RR)
A homing parachute system, by M. T. Kane and
ocfaera. Sandia Corporation. Albuquerque,
N. Mex. Jan 61. 35p. Order from OTS. $1.00.
SC-4537(RR)
Safe tfiennal operation ofpower tranalBtorB under
pulsed exclcatlon, by G. R. Swain and W. W.
Cr
Ion ofpowe
Ised excltttlon, by (j. R.
rannemann. Univeralty of New Mexico, Engi-
neering Experiment Sution, Albuquerque,
N. Mex. Sep 58. Contract AT(20-l)-789. 75p.
Order from LC. Ml $4. 50, ph $12. 30.
SCDC-910
658
Tte uae of compenaaticm with directional oouplera,
5y R. A. Lincoln. Sandia Corporation, Albu-
querque, N. Mex. Jan 61. 5^. Ckder from
OR. $1.75. SCI\I-149-60-27
Measurement of the directivity of a coaxial dlrec-
donal coupler by use of a length of precision
transmission line, by W. E. Little. Sandia
Lorporadon, Albuquerque, N. Mex. Jan 61.
23p. Order from OTS. 75 cents.
SCTM-352-60-27
The Sandia Corporation 12-inch transonic wind
tunnel analog-to-dlgittl dagt gathering system,
byD. R. MacKenzle. Sandia Corporation,
Albuquerque, N. Mex. Jan 61. 47p. Order
from 015. $1.25. SCIW-371-60-71
Feasibility study of a thermistor vacuum
by J. r. Taylor. Sandia Corporadon.
"»8?
que, N. Mex.
75 centa.
Jan 61 . 2^.
Order from OTS.
SCrM-402-60-14
Nuclear materials rontrol aystem (NMCS). Phase
II. Summary and progress report to December
31, 1959. Wesringhouse Electric Corporadon.
Atomic Power Department, Pittsburgh. Pa.
Dec 59. Contract AT(30-1)-2176. 91p. Order
fromLC. Mi $5.40, ph$15.30. WCAP-6037
Isotopes — Industrial Technology
Radiation -induced nitration of hydrocarbons, by
M. J. Oestmann and others. BatteUe Memorial
Institute, Columbus, Chio. Jan 61. Contract
Wj-7405-eng-92. 14p. Order from OTS.
SOcenu. BMI-1495
Determination of the lithium isotoplc separation
factor by ion exchange in the aulfonated polysty-
rene resin - - lithium chloride system, by R, £7"
bianco and others. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. Nov 53. Decl. with
deletions June 10. 1960. ISp. Order from LC.
Ml $2.40, ph$3.30. CF-53-ll-47(Del.)
Summary report of thermionic isotoplc
rough 7une 30. 1960, by R. J. Harvey
powi
■fe
er s
IL
tern tfarc
k«artin Company. Nuclear Division, Baltimore,
Md. 1960. Contract AT(30-3)-217. 535p.
Order fromLC. Mi $11. 10, ph $91.80.
MND-P-2399
Development of a double thickness/double density
gamma gauge, by P. C. Aebersold. Nuclear
aesearon Corpora
>rporadon. Southampton, Pa.
Dec 59. Contract AT(30-l)- 2304. 36p. Order
from OTS. 75 cents. NYO-2480
The study of the potential applicadona of radioiao-
tcye tedinoloiy to waterreeource investigadona
atid udllzadoiT Quarterly report no. 1
Isotopes, Inc., Westwood, N
tract AT(30-l)-2477. 62p.
Ml $3. 90. ph$10.80.
J. June 60. Con-
Order from LC.
NYO-9037
The study of the potential applications of radioiso-
tope technolojy to water resource Investigations
and utilization. Quarterly report no. 17^
Isotopes, Inc., Westwood, N. J. Sep 60. Con-
59p. Order from LC.
NYO-9038
tract AT(30-l)-2477.
Mi $3. 60, ph$9.30.
Utilization of radioactive iaotopea in coal process
reaearcfa. Quarterly technical sums report no.
5 for May 1, i960- July 31 IW, by P. M.
Yavorsky and E. Gorin. Consolidation Coal Co
Company, Research and DevelofHitent Divlaion,
Library. Pa. Aug 60. Contract AT(30-1)- 2350.
18p. Order fromLC. Ml $2. 40. ph $3. 30.
NYO-9139
Chemistry related to the isottyic separation of
tungsten by gaaeousdiguslon, by K. E. Rapp.
Oak Ridge Gaseous Diffusion Plant, Oak Ridge.
Tenn. Oct 59. 8p. Order from LC. Mi $1.80,
ph$1.80. TID-6471
Radioisotopes in world Induatry. Abatracts of
selected foreim literature. OtHce <rf iaotopea
Development. U. S. Atomic Energy Commission,
Washington. D. C. Jan 61. 141p. Order from
OTS. $2.50. TID-6613
Isotope Separation
Theory of the simple-process flow-through centri-
fuge, by K. Cohen. Columbia Univeralty, New
York, N. Y. [1947]. Decl. February 1, 1960.
44p. Order from LC. Mi $3. 30, ph $7.80.
A-SO
Thermal phenomena in centrifugdon, by C. Skar-
Strom and K. Cohen. Naval Research Labora-
tory, Washington, D. C. and Columbia Univer-
sity, New York, N. Y. [ndj. Decl. February
1. 1960. lOp. Order fromLC. Mi $1.80,
ph$1.80,. A-51
The influence of baffles on a countercurrent ultra-
centrlfuge. by K.
NewYo^
uge. by
JrkTN.
Y.
Cohen.
[194?].
Columbia University
Decl. September 23,
6S9
n
1960. lOp.
ph $3. 30.
Order
from LX:.
Ml $2.40.
A-
52
Coocentratioo of tsotopea by fractional (ttattllatloB
In an lUtracentrifuge, by K. Cohen. Columbia
University, N^ ^rk. N. Y. [I94?l. Decl.
February 1. 1960. 43p. Order from LC.
Ml $3. 30, ph$7.80. A-54
tr
Absolute efficiencies of iaotcye separation by
counter -current centrifuges. A new counter -
current centrifuge, by K. Cohen and I. Kaplan.
Columbia University . Substitute Alloy Materials
Laboratory, htew York, N. Y. Jan 42. Decl.
February 1. I960. 37p. Order from LC.
Ml $3. 00. ph!$6.30. A-101
Cooceturatlon of the isotopes by centrlfuglng. Part
I. Flow tfaxoup;h mefl>od. Part II. Coimttr flow
n^ethod. University of Virginia, CharlotteavlTIe,
Va. Aug 42. iDecl. February 1. I960. 30p.
Or*rfromL:. Ml $2.70. ph $4.80.
A -260
Long bowl gas separator, by F. C. Rushing. West-
Ingbouse Elec&ic and Manufacturing Company,
East Pittsburg. Pa. Apr 44. Decl. February
1. 1960. Contract OEMsr -415. 29p. Order
from LC. Ml $2.70, ph $4.80. A-1911
Short bowl gaa saparator, by F. C. 'Rushing.
Westlnghouse Electric acid Manufacturing Com-
pany. East FittsbuTj^, Pa. Oct 44. Decl.
February 1, I'960. Contract OEMsr -48 9. 33p.
OrierfromLC, Mi $3. 00. ph $6. 30.
An investi
A-3113
tion of thermal diffusion separation of
U-232-(J-233 »8 an alternate to remote proceiiT
ing, byS. H. )ury. Oak Ridge National Labora-
tory. Oak Rld|e. Tenn. Mar 60. Contract W-
7405-eng-26. ,7p. Order from LC. Ml $1.80.
ph$1.80. ' CF-60-3-37
Axial diverge nee 'calculations, by D. L. Thomas.
Goodyear Atoiifiic Corporation. Portsmouth.
Ohio. Feb 60, Contract AT(33-2)-l. 5p.
Order from Lt. Ml $1.80. ph $1.80.
' GAT-C»^-819
Separation of metcury
byE. E,
excitation,
isoti
Volfand
jto-
8 by se lectl ve phot
General ElectrTc
Company. Hartford Atomic Products Operation.
Richland, Waah. Mar 59. Contract W- 31 -109-
Eng-52. I6p. Order from LC. Ml $2.40,
pll$3.30. HW- 59329
Applicability of gas centrifuge to Isotope separatloa
for elements neayler thantiunium. by]. J.
Barker. Kldde (Walter) Nuclear Laboratories ,
Inc. . Garden City, N. Y. Sep 56. Decl. Febru-
ary 1. 1960. Contract AT(30-1)- 1374. 52p.
Order from LC. Mi $3.30, ph $7.80.
NYO-7348
Separation of isotopes. Annual progress re
by R. I. Taylor. Columbia University.
rt.
sport
York. N. Y. Oct 59. Contract AT(30- 1 )-755.
179p. Order from LC. Ml $8. 10. ph $27. 30.
NYO-7763
Separation and exchange of isotopes. Annual
• • \959toJuly 1
Rutgers University.
Lnnual prog-
ress report for July 1 , 1959 to Julj
W. Spindel and others.
Newark. N. J. 1959. Contract AT(30-1)-
2250. 115p. Order froip LC. Ml $6. 00.
ph$18.30. NYO-8769
The Improved dual -temperature process for die
jroduction of heavy water (inclu "
t plant program), by
Oct49. 'Decf. july2f: i«^. (
luction of heavy water (including coat analy-
sis and pilot plant program), by J. S. Spevack.
Contract AT
(30-l)-759. 45p. Order from LC. Ml $3. 30,
ph$7.80. NYOO-85
The development of short bowl ultracentrlfuges.
Progress report, by G. Zlppe. University of
Virginia. Research Laboratory for Engineering
Science, Charlottesville, Va. Nov 59. Contraa
AT(40-l)-2400. 22p. Order from LC.
Ml $2.40, ph$3.30. ORO-2I6
Methods of calculating U-235 outputs and chargea
by use of ideal cascade theory, by A. J. Snyder.
QEflce of Operations Analysis and Forecasting,
Oak Ridge, Tenn. Feb 60. 38p. Order from
OTS. 50 cents. TID-8522
Mathematics and Computers
Calculation methods for heterogeneous systems,
by J. Chernlck. Brookhaven National Laboratory,
Upton, N. Y. Aug 60. 32p. Order from OTC.
$1.00. BNL-622(T-I89)
Evaluation of the zeros of cross -product Bessel
functions, by L. ). Laslett ana W. Lewish.
Iowa Sute University of Science and Technology,
Ames Laboratory. Ames, Iowa. Sep 60. Con-
tract W-7405-eng-82. 174p. Order frorp OTS.
$2.75. IS-189
660
r»rm |Biieral meah data, by J« A. Archibald. Jr.
~ Knolk Atomic Power Laboratory, Schenectady,
N. Y. May 60. Revised July 22, 1960, Con-
tract W-31-109-eng-52. 17p. Order from LC.
Ml $2. 40, ph$3.30. KAPL-M-JA-7(Rev.)
Electromagnetic production of pion palra, by C. D.
Zerby. Oak Ridge National Laboratory, Oak
Ridge. Tenn. [ndj. Contract W-7405-eng-26.
103p. Order from OTS. $2.25. ORNL-3033
Improvement of Monte Carlo precision, by H. D.
Brunk and G. P. Steck. Sandia Cor]x>ration.
Albuquerque, N. Mex. Dec 55. 32p. Order
fromLC. Ml $3. 00, ph $6. 30.
SCTM-248 -55-51
Solution to a glass of singular Integral equations
occurring in mathematical physics. Thesis, by
F. A. Hlnchey. Sandia Corporation, Albuquer-
que, N. Mex, Aug 60. 76p. Order from LC.
Mi $4. 50. ph$12.30. SCTM-259-60-U
Use of dual -level logic aids In block diagram devel-
opment. by R. h" Braasdi. Sandia Coi
Albuquerque, N. Mex
nt. by R. h7 Braasdi. Sandia Corporation.
Dec 60. 18p. Order
from OTS. 50 cents. SCTM-3O7-60-24
SiannMiry technical progress report. University
oflUinoia, Digital Computer Laboratory. Urbana,
Ul. Aug 60. Contract AT(11-1)-415. 373p.
Order from LC. Mi $11. 10, ph $54. 60.
TID-6495
A paper tape to magnetic tape converter, by L. F,
Flores. University of California, Lawrence
Radiation Laboratory, Berkeley, Calif. Dec 60.
Contract W-7405-eng-48. I6p. Order from
OTS. 50 cents. UCRL-9483
BRIC - an IHM-704 iwo-dlnynslonal nuclear -thernaal
depletion program with distributed void effecti^
by W, M. Jacobi and odiers. Westing^iouse Elec-
trlc Corporation, Bettis Atomic Power Laboratory,
Pittaburgh, Pa. Jan 61. Contract AT- 11-1 -GEN -
14. 26p. Order from OTS. $1,00.
WAPD-TM-208
QJRPl«»a least-squares polynomial fitting program
for the Phi 100-2000, by A. V. Pace. Westlng-
house, Electric Corporation, Bettis Atomic Power
Laboratory, Pittsburgh. Pa. Jan 61. Contract
AT-ll-l-GEN-14. Up. Order from OTS.
50 cents . WAPD-TM- 226
Inpit preparation for diffusion -depletion pr^rams
00 the Philco-2000 computer, by W. R. didwell
•nd H. P. Henderson. Westlnghouse Electric
Corporation. Bettia Atomic Power Laboratory.
Pittsburgh. Pa. Jan 61. Contract AT-ll-l-
GEN-14. 14p. Order from OTS. 75oents.
WAPD-TM-238
WANDA -5»a one -dimensional neutron dlffusloo
equation program for die Riilco- 2000 compuier,
by O.J. Marlowe and M. C. Suggs. Westing-
house Electric Corporation. Bettis Atomic
Power Laboratory, Pittsburgh, Pa. Xov 60.
Contract AT-ll-l-GEN-14. 31p. Order from
OTS. $1.00. WAPD-TM-241
Metals, Ceramics, and Materials
Fission product release: A comparison between un-
clad metal fuel and clad plasac fuel, by G. F.
Bogar and G. R. Hopkins. Westlnghouse Elec-
tric Corporation, Atomic Power Division,
Pittsburgh. Pa. Aug 56. Decl. with deletions
May 6, 1957. 2^. Order from LC. Mi $2.70.
ph$4.80. AECD-4254
Applications for lanthanon oxides and other com-
pounds in die ceramic industry, by G. L. Ploetz
and A. T. Mucclgrosso. Knolls Atomic Power
Laboratory, Schenectady, N. Y. Jan 60. 14p.
Order from LC. Mi $2. 40, ph $3. 30.
AECU-4639
A coated cast iron crucible for use with eutectic
Al -Si alloy in the temperature range 595" -
65q"C, by F. L. Yamee. Argonne National
Laboratory, Lemont, 111. Nov 57. Decl. Febru-
ary 4. 1960. Contract W-31-109-eng-38. 37p.
Order from LC. Mi $3. 00, ph $6. 30.
ANL-5673
Niobium phase diagramg. Report no. 5: Colunibl-
um- hydrogen system. Report no. 6: Colunabi"-
um-nitrogen system. Report no. 7: Columblum
roget
-nitn
oxygen-nitrogen system. Report no.
teen '
^ .^-, ■ 8: Final
inical report covering Ae period April I?r
technical report covering the period April 15,
l»57toAprin5, 1960, ^R. rBmotaadS.
Komjatfay. Illinois Institute of Technology,
Armour Research Foundation, Chicago, 111.
May 60. Contract AT(1 1-1 )-515. 74p. Order
from LC. Mi $4. 50, ph $12. 30.
ARF-2120-5 dim 8
Euratom program. "Improved zirconium alloys,"
by D. Weinsiein and R.J. Van Thyne. IllinoiB
Institute of Technology, Armour Research
Foundation, Chicago, III. Oct 60. Contract
AT(ll-l)-578. Up. Order fr<Mn LC. Mi $2.40,
ph$3.30. ARF-2198-7
^
661
Tbe boroa-carbon 9\
m lx>roa-carbon system. Quarterly report no. 1
forMay 1 t960-Iuly 31 fW). by R. T. BTIISr
and R. J. Vaa Thyne. Illinois Institute <rf Tech-
nology, ArmOur Re8earc± Foundation, Chicago,
m. Ai«60. Contract AT(U-l)-578. l^.
Order from LC. Ml $2. 40, pli $3. 30.
ARP-2200-3
Mo6l
SI2-JJO2 ceramics for hig^- temperature fuel
elements, by J. R. Gamblno ana other*. Battelle
Memorial fnatltute, Columbus, Ohio. Aug 55.
Dccl. September 1. 1960. Contract W-7405-
eng-92. 30p4 Order from LC. Ml $2.70.
phM-80. I BMI-1029
Surrey and sete^on al materials for programmatic
evaluation foy a gaa-cooled reactor e^yerlment,
by D. L. Keller. Battelle Memorial Institute,
ColumiHis. Ohio. Sep 56. Qecl. with deletions
December 4. ! 1959. Contract W-7405-eng-92.
86p. Order trotn LC. Mi $4.80. ph $13.80.
BMI-1133(Del.)
Progress relatigg 1
August 1959, bv
iss relatigg to civilian appllcatioos Airing
[ugust 1959, by R. W. Dayton and C. R. Tipton,
Jr. BatteUe* Memorial Institute, Columbus,
Ohio. Sep 59. Decl. October 8. 1959. Contract
W-7405-eng-92. 102p. Order from LC.
Mi $5.40, ph $15. 30. BMI-1377
Progress relatigg to civilian applications during
m
Progri
lo^mber IS^, by R. W. Dayton and C R.
Tipton, Jr. lattelle Memorial Institute, Colum-
bus, Ohio. I>ec 59. Decl. Febniary 10, 1960.
Contract W-7405-eng-92. 108p. Order frOTi
LC. Mi $5.70, ph $16.80. BMl-1398
ess relating to civilian applications during
amisry 1960rby R. W. Dayton and C. R. Tipton,
r. Battelle ifemorlal Institute, Columbus,
Ohio. Feb 60. Decl. April 20. 1960. Contrsct
W-7405-eng-92. 88p. Order from LC.
Ml $4. 80, ph $13.80. BMl-1409
Progress reUtlM to civilian applications dtirlng
March, 1960. by R. W. Dayton and C. R.
Uptoa, Jr. Battelle Memorial Institute, Colum-
bm. Ohio. Apr 60. Contract W-7405-eng-92.
103p. Order from OTS. $2.25. BMI-1430
Progress relating to civilian applications during
April, 196jD, by R. W. Dayton and C. R. Tipton,
Jr. Battelle Memorial Institute. Colimibus, Ohio.
May 60. Coi«ract W-7405-eng-92. 99p. Order
from 015. $G.50. BMI-1434
Pr
ogress relating to civ
feptember, 1960, by R. W."
Tipton, Jr. ^ttelle Memorial institute,
licatlons durln;
yton and C.
Columbus, Ohio. Oct 60. Contrsa W-7405-efl
92. 80p. Order from OTS. $2.25.
BMI-1469
Progre
Nov
ss relating to civilian applications during
ember, 1960, by R. W. Dayton and C. R.
Tipton, Jr. Battelle Metnorial Institute. Colum-
bus, Ohio. Dec 60. Contract W-7405-eng-95!.
76p. Order from OTS. $2.00. BMI-1480
Pri
esa relating to civilian a
member, 1
lications duri
yton, and C.
,byR.W.
Tipton, Jr. Battelle Memorial Institute, Colum-
bus, Ohio. Jan 61. Contract W-7405-eng-92.
77p. Order from OTS. $2.00.
BMI-1489(Rev. )
t
le effect at hlgfa-burnup irradiation on massive
uranium carbide, by A. W. Hare and F. A.
Rough. Battelle Memorial Institute, Columbus,
Ohio. Jan 61. Contract W-7405-eng-92. 25p.
Order from OTS. 75 cents. BMI-1491
tory. Upton, N. Y. Sep 60. I3p. Order from
OTS. 50 cents. BNL-633 (T-196)
Process developtnent<piarterly report for Aprll-
June 1958, ^ Bridgeport Brass Company, Bridge-
port, Conn. Feb 59. Decl. February 4, 1960.
Contract AT(30-l)-1405. 74p. OrJer from LC.
Mi $4. 50, ph $12. 30. BRB-47
Measurement of the dispersion of conductivity appli-
cation to two uranium oxide -aluminum oxide
samples, by D. P. Snowden. General Atomic
Division, General Dynamics Corporation, San
Diego. Calif. [195?]. Contract AT(04- 3)- 187.
12p. Order from LC. Ml $2.40, ph $3.30.
GAMD-1234
brradlation and examination of vibratory packed
UOy b^gb !'y""P Pfoy^"* ^""J.^A'^™ '■ ^ '^'^'
Sloeek andB. Weldenbaum. Vallecitos Atomic
Laboratory, Atomic Power Equipment Depart-
ment , General Electric Company. Pleasanton,
Calif. Feb 60. Contract AT(04-3)- 189. 53p.
Order from OTS. $1.50. GEAP-3108(Pi. 2)
Studies on die compstibility of hig^-temperature
carbon dioxide with suinless steels and other
OMterials. Preliminary report. General Nu-
clear Engineering Corporation, [Xinedln, Fls.
Dec 59. 29p. Order from LC. Mi $2.70.
ph$4.80. GNEC-121
662
Corrosion effects of lowering the pH in TBP waste
storage tanks, by N. D. droves. General Elec-
tric Qjmpany, Hanford Atomic ProducM Opera-
tion, Richland. Wash. Apr 54. Decl. March
24.1960. 5p. Order frc»n LC. Mi $1.80,
ph$1.80. HW-3004I
Host-Irradiation examitiation of cluster-type fuel
elements, by C. L. Boyd. General Electric
Company, Hajiford Atomic Products Operation,
RicfaUnd. Wash. Nov 56. Decl. March 16,
1960. 8p. Order from LC. Ml $1.80,
ph$1.80. HW -46472
Some new techniques in the use of ultrasonic attenua -
tion intestinguranlum fuel elements, by C. LT
Frederick. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash .
Mar 57. Decl. March 16, 1960. Contract W-
31-109-Eng-52. 17p. Order from LC.
Mi $2. 40. ph $3. 30. HW-48989
A proposed mechanism for the corrosion o< alumln-
um in water by R. L. EMllon. General Electric
CfMnpany. Hanford Atomic Products Operation,
RlchUnd. Wash. Mar 59. Contract AT(45-1)-
1350. 14p. Order from LC. Ml $2. 40,
ph$3.30. HW- 59687
Uraniuna cold extrusioo, by G. W. Riedeman. Gen-
eral Electric Company, Hanford Atomic Products
OperaUon, Richland, Wash. Apr 59. Decl.
September I. 1960. Contract W-31-l09-Eng-52.
20p. Order from LC. Mi $2. 40. ph $3. 30.
HW -60059
Thermal cycling of Plutonium. Part I. Observa-
tions of die physical damage resulting from tRer
mal cycling Plutonium throut^ its low tempera-
ture pnase transformations, by R. D. Nelson.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Sep 59.
Contract AT(45-1)-1350. 30p. Order from LC.
Mi $2. 70. ph $4. 80. HW-61681
Classification of PuOo particles, by J. B. Burnham.
General Electric Company, Hanford Atomic
Products Gyration, Richland, Waah. Jan 60.
15p. Order from LC. Ml $2. 40, ph $3. 30.
HW-63106
Studtes 00 the oxides of plutonlum, byT.D. Chlkalla.
tieneral Electric Coinpany. Hanford Atomic
Products Operation. Richland, Wash. Dec 59.
53p. Order from LC. Mi $3. 60, ph $9. 30.
HW- 63574
Metallographic observations of swelling on uranium.
Interim report, by T. B. Bier lein and others.
General Electric Company. Hanford Atomic
Products Operation. Richland, Wash. June 60.
Contract AT(45-1)- 1350. 59p. Order from
LC. Ml $3. 60, ph$9.30. HW- 63848
Comparison of the corrosion erf carbon steel, stala-
less steel. inconel-X and stellite in the KER
roockup tubes with out -of -reactor loops, by
A. P. Larridc. General Electric Conipany,
Hanford Atomic Products Operation, Richland,
Wash. Feb 60. I5p. Order from LC.
Ml $2.40, ph$3.30. HW-63872
PRTR calandria fabrication report, by L. T. Peder-
sen and M. R. Kxeiter. General Electric Com-
pany, Hanford Atomic Products Operation,
RichUnd, Wash. July 60. Contract AT(45-1)-
1350. 42p. Oitler from LC. Ml $3. 30,
ph$7.80. HW-64762
A multiple nondestrugive test station for NPR
fuel elements, by T. G. Lambert. Hanford
Atomic Products Operation, Richlaod, Wash.
June 60. Contract AT(45-1)-1350. 3^. Order
from OTS. $1.00. HW-65910
Invention report: Hermetically s«iled closure on a
sheathed thernaocoiyle, by B. S. Koeut. Gener-
al Electric Compenyi~Hanford Atomic Products,
Operation. Richland, Wash. July 60. Contract
AT(45-1)-1350. 4p. Order from LC. Mi $1.80,
ph$1.80. HW-66043
Specialized gating and forming of react! ve metal
fbapea- Period covered May 15. 1959-March3i,
1960. by T. A. Hamm. Oregon Mettllurglcal
Corporation. Albany, Ore^ Mar 60. Contract
W-31-109-Eng-52. 20p. Order from LC.
Mi $2. 40, ph $3. 30. HW-OREMET-1
Specialized casting and forniing of reactive metal
shapes. Period covered May 15, 1959-Deoember
30, 1959. byT. A. Hamm. Oregon Mettllurgl-
cal Corporation, Albany, Ore. Dec 59. Coo-
trsct W-31-109-Eng-52. l^. Order from LC.
Ml $2.40. ph$3.30. HW-OREMET-3
Specialized gating and forming of reactive mettl
shapes. Perloo covered October 19, 1959 -April
30, I960, by T. A. Hamm. Oregon Mettllurgl-
cal Corporation, Albany, Ore. Apr 60. Con-
tract W-31-109-Bng-52. lOp. Order from LC.
Mi $1.80, ph$1.80. HW-OREMET-4
Tlie structure of U
Peterson
ni7, by C. L. Void and D. T.
lowalSttte University of Science and
Technology, Ames Laboratory. Ames. Iowa.
Jan 61. Contract W-7405-eng-82. 28p. Order
from OTS. 75 cenu. IS-246
663
'<;
The application df tfrfrargd techniques to the study
of the corroeion film on Zircaloy, by H. A.
Fisch and others. General Electric Company, ^^
Knolls Atomic Power Laboratory, Schenectady,
N. Y. Jan 59J Contract W-13-109-Eng-52.
lOp. Order ftom OTS. 50 centa. KAPL-2052
Radiation effects
"HI
tipon the recovery of
» of meals, by E.TT
the mechani-
Aqua and
oai properties oC
R. J. Alllo. (feoeral Electric Company, Knolls
Atomic Power Laboratory, Schenecudy, N. Y.
Oct 60. Contract W- 31- 109-Eng- 52. 27p.
Order from 015. $1.00. KAPL-2103
Effects o< electrijcal discharge machining (elojdng)
of Zircaloy, by J. O. Mirate. Knol'la Atomic
Power La&ralory, Schenectady, N. Y. July 60.
Contract W-3l-109-Eng-52. 13^. Order from
LC. Mi $2. 4q, pb $3. 30. KAPL-M-JOM-2
Fabrication of taatalum capaulea for LAMPRE 1
reactor, by G. S. Hanks and J. M. Thub. Los
XIamos Scientific Laboratory, Los Alamos,
N. Mex. June 60. Contract W-7405-eng- 36.
64p. Order fitom LC. N4i $3. 90, ph $10. 80.
LAMS -2434
Ptiase tran8forma.tion, twinning, an anelastlc
pheoomenon associated with zirconium hydride.
by R. Chang. Atomics International. Division
of North American Aviation, Inc. , Canoga Park
Calif. Sep 60. Contract AT-ll-l-CTN-8.
15p. Order fi|>m LC. Mi $1.80, ph $1.80.
NAA-SR-5537
frpm
Post service metsllurjlcal examination of Griscom-
Russell two-tifce superfagiter. by J. P. Page.
Atomics International. Division of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. Jan 60.
Sp. Order frofn LC. Mi $1.80, ph $1.80.
NAA-SR-Memo-48S4
Ingot mold heating as a mettK>d of controlling metal
quality, by E. B. Blasch and others. National
Lead Company of Ohio, Cincinnati, Ohio. Sep
57. Dec 1. Match 30, 1960. Contract AT(30-1)-
1156. 47p. order from LC. Mi $3. 30,
ph$7.80. NLCO-697
Atomic power development associates progress
report for July|l 1954-January 31, 1955, by
R. Evans and (itfaers. Nuclear Metals, Inc. ,
Cambridge, Mm*. Apr 55. Decl. February
4, I960. Coottact AT(30-1)-1565. 25p. Order
from LC. Ml $2.70, ph $4.80. NMI-1133
Proceedings
symposium.
Nuclear
of tfJ
m, Mb
Metals, Inc
ninth annual AEC corrosion
ay 10-12 .t»60. by J. P
Perns ler.
Concord, Mass. July 60.
SSp. Or^r from LC. Mi $3. 60, ph $9. 30.
NMI-1220
Fundamental and applied research and development
in naeallurgy. Rrogress report for July 1^60. ~
Nuclear Metals, Inc., Concord, Mass. Aug 60.
Contract AT(30-1)-1565. 21p. Order from LC.
Mi $2.70. ph$4.80. NMl-2067
indamental and applied Yesearch and development
in metallurgy. Progress report for August 1960
Nuclear Metala. Inc. , Concord, Mass. Sep 60.
Contract AT(30-1)-1565. 27p. Order from LC.
Mi $2.70, ph$4.80. NMI-20e8
Fundamcnoil and applied research and development
in nietallurgy. nDgress report for September
1960. Nuclear Metals, Inc., Concord, Mass.
DcTR). Contract AT(30-1)-1565. 28p. Order
from LC. Mi $2.70, ph $4.80. NMl-20e9
The fabrication of clad massive UOo fuel elements
1
coexp-uaion. Third quarterTy* report, byJ.G.
Nuclear Meuls, Inc.,
unt and P. Loewenstein
Concord, Mass. Apr 60. Contract AT(30-1)-
1565. 26p. Order from LC. Mi $2.70,
ph$4.80. NMI-250e
Spheroldlzation heat treatment and re-evaluation of
Ziraloy-clad U-2 w/oZr alloy tube no. 28, ex-
tnisloo no. 18388, by D. F. Kaufman and others.
Nuclear Metals, Inc. , Concord. Mass. July 60.
Contract AT(30-1)-1565. 38p. Order from LC.
Mi $3. 00, ph $6. 30. NMI-4377 (3uppl. )
Power r«ctor program. Progress report for the
period March l" 1959 tfarouA March 31, 1959,
pyS. Isserow and others. Nuclear Meuls, Inc.
Concord. Mass. July 59. Contract AT(30-1)-
1565. 22p. Order from LC. Mi $2.70,
ph$4.80. NMl-4392
Power rector program. Progress report for the
period August 1° 1959 dirwgfa August 31, "T^9,
oy S. Isserow, and others. Nuclear Meuls, Inc.,
Concord, Mass. Nov 59. Contract AT(30-1)-
1565. 17p. Order from LC. Mi $2. 40,
ph$3.30. NMI-4397
Power reactor program. Jjovce
period September 1, 1959 mr
ess re
iport for the
Septembers),
^ P
jdSeptemt" ""
1959, by D. F. Kaufman and ot^rs. Nuclear
Meuls, Inc., Concord, Mass. Nor 59. Con-
tract AT(30-1)- 1565. 40p. Order from LC.
Ml $3. 00. ph$6.30. NMl-4398
Power reactor program. Progress report for the
period October 1. 1959 through Ottober 31. i^>
664
bjr R. G. Jenkins and others. Nuclear Meuls,
Idc. . Concord, Mass. Mar 60. Contract AT
(30-l)-1565. 27p. Order from LC. Ml $2.70,
ph$4.80. NMI-7221
Power reactor program. Progress report for the
period November 1, 1959 mrourii November"
1959, by W. J. Richmond and ocie
30.
rs. Nuclear
Meuls, Inc., Concord, Mass. June 60. Con-
tract AT(30-1)- 1565. 39p. Order from LC.
Ml $3. 00, ph$6.30. NMl-7222
Power reactor program. Progress report for tl^
eriod December 1 1959 mrougfa December 31,
959, by W. B. Tuffin and others. Nuclear
Meals, Inc. , Concord, Mass. June 60. Con-
tract AT(30-1)-1565. 44p. Order from LC.
Ml $3. 30, ph$7.80. NMl-7223
Power reactor
Ti
or program. Progress report for the
period Ja nuary 1 , 1 960 throujrti January 31 , 1 9<
oyH. M. Green and others. Nuclear Meula.
—/ ... — -. _•— .. — ..— __..,._. ..w^.^_» .^.«,M-».
Idc.. Concord, Mass. June 60. Contract AT
(30-l)-1565. 37p. Order from LC. Mi $3. 00,
ph $6. 30. NMI-7224
Power reactor program. Progress report for the
period March l" 1960 through March 31, I960,
by W. J. Richmond and others. Nuclear Meuls,
Inc., Concord, Mass. July 60. Contract AT
(30-l)-1565. 34p. Order from LC. Ml $3.00,
ph $6. 30. NMl-7226
Power reactor program. Progress report for the
period April 1, i»60 through AprilSO 1960,
by A. M. White and otheraT Nuclear Meuls,
Inc., Concord, Mass. July 60. Contract AT
(30-l)-1565, 36p. Order from LC. Ml $3.00,
ph $6. 30. NMl-7227
r reactor program. Progress report for the
riodMayl fe60 through May 31 . 1»60, hj
Power reactor
pgr^May^i, ivou tnrougn May
A. D. Donaldaon and others^ Nuclear Meuls,
Inc., Concord, Mass. July 60. Contract AT
(30-l)-1565. 31p. Order from LC. Mi $2.70,
Fb$4.80. NMI-7228
Power reactor program
period June 1, i960 tKri
H. F. Sawyer and others
Progress repor
rough June 30, 1
rs. Nuclear Mc
t for the
1»60, by
Meuls, Inc.,
Concord, Mass. Aug 60. Contract AT(30-1)-
1565. 34p. Order from LC. Mi $3.00,
ph $6. 30. NMI-7229
Power reactor proapram. Progress report for the
periodjuly 1, 1960 dirougfjuly 31,_ 1»60, by
P. R. Smoot, and others. Nuclear Metals, Inc.,
Concord, Mass. Sep 60. Contract AT(30-1)-
1565. 32p. Order from LC. Ml $2.70.
Ph$4.8G, NMI-7230
The development and testing of the UO2 fuel ele-
ment s^tem. Quarterly report for June 1, 1960-
August 31. 196oT Comlwjstion Engineering, Inc.,
Nuclear Division, Windeon, Conn. 1960. Con-
tract AT(30-l)-2379. 47p. Order from LC.
Ml $3.30. ph $7. 80. NYO-9009( CEND-99)
Fuel element development program for the pebble
bed reactor. Quarterly mrogress report for"
February 1, to April 30, i960. Sanderson and
Porter, New York, N.Y. 1960. Decl. May 23.
1960. Contract AT(30-l)-2378. 85p. Order
NYO-9058
Contract AT(30-l)-2378.
from LC. Mi $4.80. ph $13.80.
Thoriuni oxide infiltration of graphite spheres; by
W . E. Parker and F. Ruslnko. Jr. Speer"Car-
bon Company. Research Laboratory, Niagara
Falls, N. Y. June 60. Contract AT(30-l)-2378.
44p. Order from LC. Ml $3. 30. ph $7. 80.
NYO-9059
The electrical resistivity of liquid sodium and
dilute sodium alloys. Final report, by J. F.
Freedman and W. D. RoberttonT Yale Univer-
sity, Hammond MeuUurglcal Laboratory, New
Haven. Conn. Oct 59. Contract AT(30-1)- 1857.
45p. Order from LC. Mi $3.30, ph $7.80.
NYO-9316
Metallurgy division annual progress report for
period ending July 1, 19c0. Oak Ridge National
Laboratory, Oak Ridge, Tenn. Sep 60. Con-
tract W-7405-eng-26. 503p. Order from LC.
Ml $11. 10. ph$82.80. ORNL-2968
Columbium-clad uranium carbide fuel element con-
tract. Monthly letter report for February
1 dirough February 29, 1960, by J.J. Finley
and others. Union Carbide Meuls Company,
NUgars Falls, N. Y. 1960. Contract AT(40-1)-
2559. 5p. Order from LC. Ml $1.80, ph$1.80.
ORO-266
Synthesis and fabrication of refractory uranium
compounds, Monthly progress report no. 8 for
•11 1 through April 31 , 1
ough April 3l, 1960, by K. M. Taylor.
. Carborundum Company, Niagara
April
and others
Falls. N. Y. May 60. Contract AT(40-l)-2558
5p. Order from LC. Ml $1.80, ph $1.80.
ORO-276
Fuel beari
menu.
ass aluminum base fuel ele-
ress letter no.
11 for
ithly progi
April 1, 1960 toXprfl 30, 1^60, by R. H. Baskey.
Clevite Corporation, Mechanical Research Divi-
sion, Cleveland, Ohio. May 60. Contract AT
(40-l)-2557.
ph$1.80.
3p. Order from LC.
Mi $1 . 80,
ORO-277
665
Fuel berlng flberjgUg in aluminum bage fuel ete-
mentB. Monthly progress letter no. 12 for May
1 I960 to May 3d. [%6b. by R. H. haicey.
Clevite Corporition, Mechanical Reaearcfa Divi-
sion. Cleveland, Ohio. June 60. Coatraa AT
(40-l)-2557. 5t>. Order from LC. Ml $1.80.
ph$1.80. ORO-303
Graphite -matrix niuclear fuel elementa. latgrim
atatus report for Noveinber 1, 1959 throu^
June 30. I960. National Carbon Company, Re-
■ea rch Laboi aoor ies , Cleveland, Ohio and Na-
tional Carbon Company, Product and Process
Development Luboratory, Fostoria, Ohio.
July 60. Contract AT(40-1)- 2560. 57p. Order
from LC. Mi ^S. 60. ph |9. 30. ORO-309
Fuel bearing fibeij
Monthl
ments.
:las in aluminum base fuel ele-
irogresa tetter no]^
iS
TfWi
riodlulyl, 1^60 t5 July 31, 1960. by RTH.
akey. Cleviqe Corporation. Mechanical Re-
search Division, Cleveland, Ohio. Aug 60.
Contract AT(40-1)- 2557. 3p. Order from LC.
Ml $1 . 80, ph $1 . 80. ORO-313
Fuel bearing fiberolaa in aluminum baae fuel ele-
ments. Mondijy progress letter no. 15 for
August 1, 1960 to Auguat 31, 1960, by ITTH,
Baskey. Clevitie Corporation, Mechanical Re-
search Divisioa, Cleveland. Otto. Sep 60.
Contract AT(40-1)- 2557. 3p. Order from LC.
Ml $1.80, ph$l.80. ORO-322
Synthesis and fabtication of refractory uranium
compounds . Monthly progress report noTTO for
September 1 throurfi SMeptember 30. 1960, by
K. M. Taylor and C. H. McMurtry. Carborun-
dum Company, Research and Develc^wnent Divi-
sion. NUgara palls, N. Y. Oct 60. Contract
AT(40-l)-2558i 2p. Order from LC. Mi $1.80.
ph$1.80. ORO-331
Preferred orientation in cross -rolled uranium, by
G. R. Mallett. The Dow Chemical Company,
Rocky Flats Pl$nt. Denver, Colo. Feb 61. Coo-
tract AT(20- 1)^1 106. 41p. Order from OTS.
$1.00. i RFP-216
Advanced fabricadion develoCTnent of strut-type ele
ments, by J. A!. Ruzga. Sylvania- Corning
Nu'^lear Corporation, Bayside, N. Y. Dec 58.
Decl. June9, I960. Contract AT- 30-1 -GEN -
366. 24p. Or^rfromLC. Mi $2.70, ph $4. 80.
SCNC-258
Low cost ceramld fuel elements by isoatatic press -
ing, by J. Fugirdi and J. L. Zambrow. Sylvania
rSrning Nuclear Corporation. Bayside, N. Y.
July 59. Decl., November 18. 1959. Contract
AT-30-l-GEN-»366. 22p. Order from LC.
Mi$2.70, phjl4.80. SCNC-289
Titanium dioxide as a semiconductor. Period cover-
ed November 6, 1958 to Novemlaer 6. i')S9, by
R, Bechtel and others. University of New Mexico,
Engineering Experiment Station, Albuquerque,
N. Mex. 1959. 12p. Order from LC. Mi $2.40,
ph $3. 30. SCDC-952(l.JNM-290-l9e)
General purpoae adhesives, by H. Moore. Sandla
Corporation, Albuquerque, N. Mex. Jan 61.
lOp. Order from OTS.
50 cents.
SCTM-351 -60-25
Eoyloratory study on ultrasooic inspection of hot
ressed uranium slugs, by G. Tnomas and odiert.
ylvania Electric Prooucts Inc. , Atomic Energy
Division, Bayside. N. Y. Dec S3. Dec 53.
Decl. March 7. 1960. 20p. Order from LC.
Mi $2.70. ph$4.80. SEP-217
The determination of the equilibrium phase diagram.
zirconium-niobium. Monthly letter report iio7~
13 for May 1, 1960 to June 1. 1960, by C. E.
Luodin. University of Denver, Denver Research
Institute, Denver, Colo. June 60. Contract
AT(ll-l)-752. 4p. Order from LC. Ml $1.80,
p*i$l.80. TlD-6061
Slip casting of nuclear fuel elements. Report no.
IV, by E. H. Baron and odiers. Stevens Institute
oTTechnology, Powder Metallurgy Laboratory,
Hoboken, N. J. June 60. Contract AT(30-1)-
2258. 9p. Order from LC. Mi $1.80, ph $1.80.
TID-6090
Investigation of electrolytic processes for prepara-
tion of hidi purity niobium meul, by A. J. IColk,
Jr. aodooiers. Horizons, Inc., Cleveland,
Ohio. 1960. Contract AT(30-1)- 1894. 26p.
Order from LC. Mi $2.70. ph$4.80.
TID-6101
Effects of non- uniformities on the hardening of
crysMls. by R. L. Fleisdier. Massachuseta
Institute of Technology, Metals Processing
Laboratory, Cambridge, M^ss. 1959. Contract
AT(30-1)-1310. 22p. Order from LC. Mi $2.70,
ph$4.80. TID-6126
Easy glide and grain boundary effects In polycrysttl-
line aluminum, by R. L. Fleischer and W. F.
Hosford. Jr. Massachusetts Institute of Technol-
ogy, Meuls Processing Laboratory, Cambridge,
Mass. 1960. Contract AT(30-1)-1310. I6p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-6127
The corrosion of the Inconel HF inlet and salt outlet
line cd the MK II dissolver, by P. W."Fnac:
Battelle Memorial Institute, Columbus. Ohio.
666
July 60. lip. Order from LC. Mi $2.40,
pli$3.30. TID-6215
Study of factors Influencing ductility of iron
lU
aluminum
jn6'
'IS
2,
oys. Monthly letter report no
byF. C. Perkins and J. F*^. Nachman. Univer-
sity at Denver, Denver Research Institute,
Denver, Colo. July 60. Contract AT(ll-l)-742.
3p. Order from LC. Mi $1.80, ph $1.80.
TID-6294
Preparation of UC2-ThC2- -graphite fuel bodies
for the ^A-306 HTGR capsule irradiations, W. V.
Goeddel. General Atomic Division, General Dy-
munlCB Corporation, San Diego, Calif. Sep 59.
Contract AT(04-3)314. 24p. Order from LC.
Mi $2. 70, ph$4.80. TID-6339
Studies In nuclear spectroscopy. Technical pre
art for October 15, 1959 through June 30,
rei
gress
T960, by R. C. Pllger, Jr. University of Notre
Dame, Notre Dame, Ind. I960. Contract AT
(ll-I)-834. 7p. Order from LC. Mi'$1.80.
ph$1.80. TID-6345
Electrochemical studies of nonaqueous melts.
Annual report, by G. Derge. Carnegie Institute
of Technology, Metals Research Laboratory,
Pittsburgh. Pa. July 60. Contract ATX30-1)-
1024. 18p. Order from LC. Mi $2.40, ph$3.3a
TID-6382
Corrosion testing of metals In the liquid-liquid ex-
traction pilot unit" Period covered September
12 195fi [q March 4 1959, by P. A. Oncoln.
Michigan Chemical Corporation, St. Louis, Mich.
1959. lOp. Order from LC. Mi $1.80, ph$1.80.
TID-6418
Fuel cycle deveic
lel cycle development program monAly newsletter
•tor July 1960, by R, L. Robinson. National Car-
bon Company, Fostoria, Ohio. Aug 60. Con-
tract AT(40-l)-2560. lOp. Order from LC.
Mi $1.80, ph$1.80. TID-6463
Electrochemical studies of hafnium, zirconium and
yttrium. Qiiarterly progress report no. 10 for
January 1 i960 to March 31, 1960. Bureau of
Mines. Boukier City Meullurgy Research Labor -
• atory, Boulder City, Nev. Mar 60. Contract
AT(ll-l)-475. 5p. Order from LC. Mi $1.80.
P»i$1.80. TID-6480
Electrochemical studies of hsfnium, zirconium and
yttriuin; pure metals project: Hafnium, zirconi-
um and program. Quarterly progress report no.
n for April 1 1 960 to J une 30, ^60. Bureau of
Mines. Boulder City Metallurgy Research Labor -
•lory, Boulder City, Nev. June 60. Contract
AT(ll-l)-475. 5p. Order from LC. Ml $1.80.
ph$1.80. TID-6481
Study of factors influenci
um alloys. Monthly letter repo;
March 15, l9^to March 15, 1960, h P. C.
aluminum alloys.
.of iron-
MonSiIy letter report for
Perkins and J. F. Nachman. University of
Denver, Denver Research Institute, Denver,
Colo. Jan 60. Contract AT(ll-l)-742. 8p.
Order from LC. Mi $1.80, ph $1.80.
TID-6562
>tudy of :
alumii
irs influencing ductility of iron-
alloys. Monmly letter report no. 11
15, 1959 to March 15, 19fo, by P. t
factors influenci
luininum al
for March"
Perkins and J. F. Nachman. University of
Denver, Denver Research Institute, Denver,
Colo. Mar 60. Contract AT(ll-l)-742. 7p.
Order trom LC. Mi $1.80, ph $1.80.
TID-6564
Study of factors influenci
aluminum alloys. Monthly :
March 15. 1959 to April gO, 1960. by F. t.
_ ot tron-
Monflily letter report fOT
Perkins and J. F. Nachman. University of
Denver, Denver Research Institute, Denver,
Colo. Apr 60. Contract AT(ll-l)-742. 4p.
Order from LC. Mi $1 . 80, ph $1. 80.
TID-6565
Recrystallization and sinteritig of oxides. Progress
report for SepMinber 1, 1959 to August 31, 1960.
University of Utah, Institute for theStudy of Rate
Processes, Salt Lake City, Utah. Aug 60. Con-
tract AT(ll-l)-82. 35p. Order from LC.
Mi $3.00, ph$6.30. TID-6572
Research on metals and alloys at lo^ temperatures.
Repp" no. 5 for SeptenAer 1, 1959 to July 1,
1960, by W. F, Love. University of dolorado,
BouTder, Colo. Ai« 60. Contract AT(ll-l)-377.
50p. Order from LC. Mi $3. 30, ph $7. 80.
TID-6578
Syndesis and fabrication of refractory uranium com-
pounds, Quarterly
April 30 and July 1
report no. 4 for Mardi 1 to
April 30 and July 1 tojuly 31, I960, by K.M.
Taylor and omers" darborundum Company,
Research and Development Division, Niagara
Falls, N. Y. Aug 60. 15p. Order from LC.
Mi $2.40, ph$3.30. TID-659I
Study of x-ray effects caus«l by point defects in
"jftals. InteriiP report for June 1 to "
1960, by F. R. L. Schoning. Franklin institute
Laboratories for Research and Develt^jment,
Hiiladelphia, Pa. 1960. Contract AT(30-1)- 2585.
5p. Order from LC. Mi $1.80. ph $1.80.
TID-6651
667
>tudy erf factors ilnfluenclog ductility of tron-
tluminum •ijoys, Montfily letter report no. 4,
by G. Rauacber and J. F. Naclunan. University
o€ Denver, Denver ResearcA Institute, Denver,
Colo. Sep 60. Contract AT(ll-l)-742. 5p.
Order from tC. Kfti $1.80, ph $1.80.
TID-6691
The kinetics <rf transformatioo at niobium-base »
zirconium »l|oy8- Monthly letter report no. 4
for August 1, 1960 to Sepcember 1, 1960, "5y~
August
1. Lun<
ipcer
1 ty c
C. B. Lundla. Universfty of Denver, Denver
Research Institute, Denver , Colo. Sep 60.
Contract AT(ll-l)-752. 3p. Order from LC.
Mi $1.80, ph|$1.80. TID-6692
I
The study factors influencing ductility of iron-
aluminum allbys. Interim report, by G. Raua-
cber and others. University of Denver, Denver
Researc* Institute, Denver, Colo. June 60.
Contract AT(Jil-l)-742. 56p. Order from LC.
Mi $3. 60, phj$9.30. TID-6694
L
The metallograAic preparation of Plutonium and its
alloys at LosAIamoe, by K. Imlah and E. M.
Cramer. Loc Alamos Scientific Laboratory,
Los Alamos, N. Mex. Feb 58. Decl. September
12, 1960. I4p. Order from LC. Mi $2.40,
ph $3.30. TID-6764
Effect of temperature on yielding in single crystals
of the hexagojial Ag-Al intennetallic phase.
Technical report no. 1, by J. Mote and others.
University ot California, Materials Research
Laboratory, Berkeley, Calif. June 60. Contract
AT(11-1)-34.| 41p. Order from LC. Mi $3.30.
ph$7.80. TID-6794
The pebble bed rieactor program. Current fuel
euer
ment devejopments and their effects on the
bble bed reactor development program. ~San-
rson and Porter, New York. N. Y. May 60.
Decl. September 23, 1960. Contracts AT(30-1)-
2207 and AT(30-l)-2378. 37p. Order from LC.
Mi $3. 00. pb!$6.30. TID-6809
T
Molybdenum, niobium, tantalum, tungsten and urani-
im cadde i» tlic journal literatures of the USSR,
1955-June I960, by C.J. Wensrlch. University
of California, I Lawrence Radiation Laboratory,
Uvermore, Calif. Sep 60. Contract W-7405-
eng-48. 32p. Order from LC. Mi $3. 00.
ph $6.30. UCRL-6110
Quarxerly naetalmrgical progress report, no. 9 for
the period of October 1, 1960 to December 31,
the period of 0ctober 1, 1960
19M, byM. t Wright. U
to December 31,
_ S. Department of
Interior. Bureau of Mines, Albany Metallurgy
Research Center, Albany, Ore. Dec 60. Con-
tract AT(ll-l)-599. 24p. Order from OTS.
$1.00. i USBM-U-783
Furnace brazing of Ztrcaloy, by E. R. Slaughter.
Westlnj^iouse Electric Corporation, Bettis Plant,
Pittsburgh. Pa. Jan 59. Decl. March 30, 1960.
Contract AT(11-1)-GEN-14. 24p. Order from
LC. Ml $2.70, ph$4.80. WAPD-TM-172
Westlnghouse Electric Corpor-
Zirconium highlights _ ^_
adon, Betus Atomic Power Laboratory, Plttsbiu^
Pa. May 60. Contract AT-ll-l-GEN-14. 22p.
Order from LC. Mi $2.70, ph $4.80.
WAPD-ZH-24
Zirconium highlights . Westlnghouse Electric Corpor-
ation, Bettis Atcxnlc Power Laboratory, Pittsburgi,
Pa. Oct 60. Contract AT-ll-l-GEN-14. 40p.
Order from LC. Mi $3. 00, ph $6. 30.
' WAPD-ZH-25
Thermoelectric nuclear fuel elenwnt progress report
no. 20 for February 1960, by G. R. iGlp and
others. Westing^iouse Electric ^rporation.
Atomic Power Department, Pittsburgh, Pa. Mar
60. Contract AT(30-3)-500. I5p. Order from
LC. Mi $2. 40, ph$3.30. WCAP-1513
Thermoelectric nuclear fuel element progress report
no. 22 , by G. R. Kilp and others. Westlnghouse
Electric Corporation, Atomic Power Department,
Pittsburgh. Pa. May 60. Contract AT(3O-3)-500.
21p. Order from LC. Mi $2.70, ph $4.80.
WCAP-1565
Thermoelectric nucl(Mir fuel element monthly prog-
ress report no. 26 covering the period August
1960, byG. R. Kilp and otters. Westlnghouse
Electric Corporation, Atomic Power Department,
Pittsburgh, Pa. Sep 60. Contract AT(30- 3)- 500.
14p. Order from LC. Mi $2.40. ph $3.30.
WCAP-1630
Meteorology
Surface temperature anomalies in mountain area
weather analysis, by J. W. Reed. Sandia Corpora-
tion, Albuquerque, N. Mex. Jan 61. I7p. Order
from OTS. 50 cents. SC-4546(RR)
Particle Accelerotors and High-Voltage
Machines
Electrode damage caused by sparks in'vacuum, by
C. A. Harris. University of California, Law-
rence Radiation Laboratory. Berkeley, Calif.
Nov 60. Contract W-7405-eng-48. 31p. Order
from OTS. 75 cents. UCRL-9487
668
Physics
Some physics calculations on the performance of
large fast breeder power reactors, by S. Yiftah
aodD. Okrent. Argonne National Laboratory,
Argonne. 111. Dec 60. Contract W-31-109-eng-
38. 32p. Order fromOTS. 75 centt.
ANL-6212
A study of the diffusive motions of liquids by meana
of cijld neutron scattering experinients, by H.
Palevsky. Brookhaven National Laboratory.
Upton, N. y. 1960. 22p. Order from LC.
Ml $2. 70, ph $4. 80. BNL-4934
Utilisation of experimental magnet power supplies,
■ by W.W. Merkle. Brookhaven National libora-
tory, Upton, N. Y. Sep 60. 2p. Order from
LC. Mi$2.40. ph$3.30. BNL-5040
Method for applying transniission and ]|-vs-E
corrections' In the determination of fy^ry^ by the
Macklin-deSaussure experiment, by E. C. Halbert
andodiers. Oak Ridge National Laboratory.
Oak Ridge, Tenn. Aug 59. 45p. Order from
LC. Mi $3.30. ph$7.80. CF-59-8-85
Seine elementery results concerning escape proba-
bilities of particles of fixed ranre generated in
spheres, byM. Tobias. Oak Ridge National
Liboratories. Oak Ridge. Tenn. Sep 60. 5p.
Order from LC. Mi $1.80, pb$1.80.
CF-60-9-44
loB energy distribution, energy degradation, and ex-
ntiation criteria in a plasma formed by
beam trapping and charge'transfer, by D. J.
koae. Oak Ridge National Laboratory, Oak Ridge.
Tenn. Sep 60. 23p.
ph$4.80.
Order from LC. Mi $2. 70.
CF-60-9-112
Oak Ridge,
Tenn. 1948. Decl. September 1. 1960. Con-
tract W-7405-eng-26. 64p. Order from LC.
MI $3. 90. ph $10. 80. CNL-21(Rev. )
Prop-ess report for Janizary, February, ^March
1960 to the United States At<»iic Energy Conamia-
sion. Columbia University. Pegram miclear
Ryaics Laboratories, New York, N. Y. 1960.
Contract AT(30-l-GEN-72. 47p. Order from
LC. Mi $3.30, ph $7.80. CU(PNPL)-203
Progress report for April, May , June I960 to die
United States Atomic Energy Commiaaioin.
! -J Columbia University, Pe^am Nuclear Hiyaica
- Laboratories, New York. N.Y. 1960. Con-
' tract AT- 30-1 -GEN-72. 49p. Order from LC.
Mi $3. 30. ph $7. 80. CU(PNPL)-205
A preliminary report on nneasurements of diffusion
parameters in w»ter by the pulsed -neutron"
mefliod, byW.M. Lcyez and others. General
Atomic Division, General Dynamics Corpora-
tion. San Diego, Calif. Sep 60. Contract AT
(04-3)-167. 20p. Order from LC. Ml $2. 40.
pb$3.30. GA-15S4
Slow neittron inelastic scattering and neutron ther-
malization. by M. Nelkin. General Atomic
Division. General Dynamics Corporation , San
Diego. Calif. Sep 60. Contract AT-04-3-167.
. 48p. Order from LC. Mi $3. 30. ph $7. 80.
GA-1669
Incurrent on a black body, by J. Devooght. General
Dynamics Corporation, General Atomic Divi-
sion. San Diego. Caiif. Sep 59. Contract AT
(04-3)-314. 27p. Order from LC. Mi $2.70,
ph$4.80. GAMD-1013
Epithermal absorption by control rods of variable
blackness, by J. Devooght. General Dynamics
Corporation. General Atomic Division. San
Diego, Calif. Oct 59. Contract AT(04-3)-314.
29p. Order from LC. Mi $2.70, ph $4.80.
GAMD-IOSO
IBM 650 program for the calculation (rf capture -
scarring and total cross -sections for S-, P-
and D-wave neutrons, by C. Crafton and B.
Rooa. General Dynamics Corporation, General
Atomic Division, San Diego. Calif. Feb 60.
Contract AT(04- 3)- 187. 20p. Order from LC.
Ml $2. 40, ph$3.30. GAMD-1251
Shielding propertiea of ordinary concrete as a func-
tion~oif temperature, by E. G. Peterson. Han-
ford Atomic Products Operation, Richland,
Wash. Aug 60. Contract AT(45-1)- 1350. 39p.
Order from 0T3. $1.00. HW-65572
Measurement of negative k«»y for a graphite uranium
lattice in die PCTR, by E. Z. Block and D.E.
Wood. Hanford Atomic Products Operation,
Richland, Wash. Dec 60. Contract AT(45-l)-
1350. 24p. Order from OTS. 75 cents.
HW -67179
Leakage of neutrons from bare subcritical plutonium
systems, by B. C. Clark and J. L. Carter.
Hanford Atomic Products Operation, Richland,
Wash. Dec 60. Contract AT(45-1)-1350. I6p.
Order from OTS. 50 cents. HW-67691
669
An •ppUcatloo <|f perturbation theory to reactor
"""^tlc^-traniBfer functlona for a two- node model,
by E. C. Hatisen. Knolls Atomic E\>wer Labora-
tory, Schenectady, N. Y. Feb 60. Contract
W-31-109-E6g-52. 20p. Order from LC.
Mi $2.70. pilM.SO. iCAPL-M-ECH-4
Estimate of the'deaignageful life of die SAR-PTR
reactor preabure vessel bead. fBased on stresses
at the edge of the central hole), py F. Panlilio
and R. Eiseiistadt. KnoIIa Atoonlc Power Labora-
tory. Schenectady, N. Y. June 60. Cootract W-
31-109-eng-$2. 23p.
Mi $2. 40, pl}$3.30.
Order from LC.
KAPL-M-FP-
of radioactivity issuing from
A counter arratgement to facilitate the averaging
' " - . _ J "- ^°°^ plate or strip
like element», by G. J. Gavin and otfiera.
Knolls Atomic Power Laboratory, Schenectady,
N. Y. Feb 60. Changed frcxn OFFICIAL USB
CWLY May 3, 1960. Contract W-31-109-Eng-
S2. 17p. Order from LC. Mi $2.40. ph $3. 30.
i KAPL-M-GBG-10
Cloeure properties on oecillatlon matrices with
appUoitioos,' by G. J. Habetler and E. P.Shelly.
iCooIla Atomic Power Laboratory, Schenecudy,
N. Y. Aug*). Contract W -31- 109-Eng-52.
ISp. Order from LC. Ml $2. 40, ph $3. 30.
KAPL-M-GJH-4
BHT-M: An IBKi| digital ccmpucer program to cal-
culate boiling h»»t transfer of steam generatora,
by H. Harden. Knolla Atomic Power Laboratory,
Schenectady, N. Y. July 60. Contract W- 31 -109-
Eng-52. 32p|. Order from LC. Ml $3.00,
ph$6.30. KAPL-M-NPA-15
TCI-an auxiliary one dimensional transient conduc-
tion code for \iBe with the art, spy and ter reac-
tor deaim codes, by ). W. Millard. Knolla
Atomic Power Laboratory, Schenecudy, N. Y.
Sep 59. Contract W-31-109-Eng-52. 59p.
Order from LC. Mi $3. 90. ph $10. 80.
KAPL-M-S3G-RES-69
Collected reporft on fission cross section at U^37
in thermal neutron, intermediate neutron, an3"
degraded fisai on neutron spectra, by G. A.
Cowan. Los 'Alamos Scientific Laboratory, Loe
Alamoe, N. Mex. Jan 55. Decl. May 11. 1960.
Contract W-7405-eng-36. 66p. Order from LC.
Ml $3.90, phi $10. 80. LA-1669
I
Neutron emiaeldn probabilltlea from the interaction
of 14-Mev netitrons with Be, Ta, Bi and U^'M,
by L. Rosen 'and L. Stewart. Los Alamoa
Scientific Laboratory, Loe Alamos, N. Mex.
Jan 57. DecU May 5. 1960. Contract W -7405-
eng-36. 27p, Order from LC. Mi $2.70,
Advanced thermoelectric power system. Final
report, by R. J. Harvey. Martin Company,
Nuclear Division, Baltimore, Md. 1960. Con-
tract AT(30- 3)- 217. 20p. Order from LC.
Mi $2. 40. ph$3.30. MND-P-23S5
Development of a diermoelectric optimization code
for the BM-7W, by T. S Buatard and W. C. ~
LyoD. Martin Company, Nuclear Division.
Baltimore, Md. July 60. Contract AT(30-3)-
217. 142p. Order from LC. Ml $7.20.
ph $22. 80. MND-P-2372
Bibliography of SNAP reports
Nuclear Divlaion. Baltimore, Md
> tract AT(30-3)-217. 9p.
Mi $1.80, ph$1.80.
Martin Company,
Aug 60. Oca-
Order from LC.
MND-P-2413
SNAP programs. Quarte
rly progress repo'
for" April 1 throim^ June y, 1960. Man
pany, Nuclear Division, Baltimore, Md
Contract AT(30-3)-217. I62p.
Mi $8. 10. ph$27.30.
rt no. 3
artin Com-
1960.
Order from LC.
MND-P-3011
Consttnt-area R-F buckets In the IBM-704 pro-
ramme TTT, by R. A. Dory. Midwestiern
niversities Research Association, Madlsoo,
Wis. July 60. Contract AT(ll-l)-384. 8p.
Order from LC. Mi $1.80, ph $1.80.
MURA-578
Physics measurements on the SNAP experimental
reactor ^Uk), isy F. H. CJlark and others .
I Intern
Atomics Intemadonal. A Divls ion of North
American Aviation. Inc. . Canoga Park. Calif.
Jan 61. Contract AT(11-1)-GEN -8. 37p. Order
from OTS. 75 centa. NAA-SR-5619
Least squares determination of lattice paranieten,
by 1. R. Tannenbaum. Atomlca Intematiaial.
EMvisioi of North American Aviation, Inc. ,
Canoga Park. Calif. June 60. 14p. Order from
LC. Mi $2.40, ph$3.30.
NAA-SR -Memo -5345
Gamma ray penetratiDn in composite slabs, by
M. H. Kalos. Nuclear Development Corporatloi
of America, White Plains, N. Y. June 60. 56p.
Order from LC. Mi $3. 60, ph $9. 30.
NDA-2056-10
Neutron cross sections for deuterium, by H.
Goldstein. Nuclear Development Corporation
of America, White Plaina, N. Y. Oct 60.
Contract AT(30-1)-2303<IX). 9p. Order from
LC. Mi $1.80, ph$1.80. NDA-2131-27
ph$4.80.
LA-2111
670
tinium-233, uranium-233, beryllium, sc
protac-
ium,
Fast neutron cross sections of thorium- 232, pi
beryllium, socuii
and Iron, by M. H. Kaloe and E. S. Troubetzkoy.
Nuclear Development Corporation of America,
White Plains, N. Y. Sep 60. Contract AT(30-1)-
2303. 30p. Order from LC. Mi $2.70,
pb$4.80. NDA-2134-2
^-? scattering at low energlea, by S. W. Barnes
and others. University of Rochester, Rochester.
N. Y. Mar 58. Contract ATX30-l)-875. 2^.
Order from LC. Mi $2.70, ph $4.80.
NYO-2170
Bquilibrium configuration of a plastna in the guiding
center limit, by A. Oppenhetm. New York Uni-
versity, Institute of Mathematical Science, New
York, N, Y. Sep 60. Contract AT(30-1)- 1480.
29p. Order from LC. Mi $2.70, ph $4.80.
NYO-9353
Blectronuclear research division semiannual prog-
ress report for period encflng September 20.
1954, byF. T. Howard. Oak Ridge National
Laboratory, Oak Ridge. Tenn. Nov 54. Decl.
August 12, 1959. Contract W-7405-eng-26.
29p. Order from LC. Mi $2. 70. ph $4. 80.
ORNL-1795
A compilation of Information on gamma -ray spectra
resulting from thermal -neutron capture, by
E. Troubetzkoy and H. Goldstein. Oak Ridge
National Laboratory. Oak Ridge, Tenn. [ndj.
Contract W-7405-eng-26. 75p. Order from
OTS. fZ.25. ORNL-2904
>roup-theoretlcal treatment of time and energy-
dqpendent multiple scattering, with application
to the slowing-oown of neutrons, by E. Guth and
E. InSnll. Oak Ridge National laboratory. Oak
Ridge. Torn. Nov 60. Contract W-7405-26.
19p. Order from LC. Mi $2.40, ph $3.30.
ORNL-3010
Rainbow scattering analysis of recent heavy ion
data, by M. V. Goldman. Oak Ridge National
Laboratory, Oak Ridge, Tenn. [nd]. Contract
W-7405-eng-26. 28p. Order from OTS.
75 cents. ORNL-3025
Prop-esa report for the fifth period. Deceniber 1,
1958 to September 1. 1959^ by A. E.S. Green.
Florida State University, Tallahassee, Fla.
1959. Contract AT(40-1)-1755. 141p. Order
from LC. Mi $7.20, ph $22.80. ORO-259
Ionization and charge transfer cross sections.
Technical status report no. 3 covering the period
Warchl. 1960 to t/ay 31, 1960. by e! W.
McDaniel and others. Georgia Institute of Tech-
nology, Engineering Experiment Station, Atlanta,
Ga. 1960. Contract AT(40-1)-2591, 12p.
Order from LC. Mi $2. 40, ph $3. 30.
ORO-286
Particle motions near explosions in Halite. Final
report, by B. P. Murphey. Sandia Corporation,
Albuquerque, N. Mex. June 60. 88p. Order
from LC. Mi $4.80, ph $13.80. SC-4440(RR)
Strese-atrain characteristics of materials at hig^
strain rates! Part VI. The proMgation of
jtrain-rate-
_^ ? propagat
Slaadc waves in finite cylinders ofst
ependent material, by B. D. Tapley. University
sity of Texa&, Structural Mechanics Research
Laboratory. Austin, Tex. Aug 60. Contract
AT(29-2)-621. 144p. Order from LC. Mi $7.20.
ph $22.80. SGDC-2156
Interpretation and prediction of radar terrain re-
turn fading spectra . Progress report no. 1, by
P. D. Welch. New Mexico College of Agriculture
and Mechanic Arts, Physical Science Laboratory,
State College, N. Mex. July 60. 67p. Order
fromLC. Mi $3.90, ph $10. 80. SCR-212
Eigen coupling factors and principal components,
the thermodynamic invariants of piezoelectricity,
byH. G. Baerwald. Sandia Corporation,
Albuquerque, N. Mex. Sep 60. 9p. Order
from LC. Mi $1.80. ph $1.80. SCR-22S
Va
r pressures of the rare earths, by L. C.
avis . Sandia Corporation, Xlbuquerque,
N. Mex. Dec 60. 14p. Order from OTS.
50 cents. SCI\I-256a-60-14
Charge cylindrical tube, by T. R. Ferguson and
R.H. Duncan. New Mexico Suie University.
University Park. N. Mex. June 60. 34p.
Order from LC. Mi $3. 00, ph $6. 30.
SCTM-258-60-14
Prediction of shock response, by P.M. Barba.
Sandia Corporation, Albuquerque, N. Mex .
Nov 60. 19p. Order from OTS. 75 cents.
SCTM-335-60-14
The latest develcyment in the electroluminescent
display of time readout system, by L.C. Meyer.
Sandia Corporation, Albuquerque, N. Mex.
Jan 61. 2Ip. Order from OTS. 75 cents.
SCTM-362-60-72
SpaCT-charge studies, by R.M. McGehee. Sandia
Corporation, Albuquerque, N. Mex. Dec 60.
44p. Order from OTS. $1.25.
SCI\l-366-60-14
671
^B* ^{fL^^^^^ **^^^^°^ emlasicn. by
R. M. Mcuelaee. Samlia Corporatioa, Albuquer-
N.Mex. |J«n6l. I8p. Order from Crre.
que.
75 cents.
SCI\l-367-60-l4
Shock signatures and Bpectra from railroad awitch-
ing loads, by P. H. Adams. ^anJia riorporatifM-
Aibuquerque. |N. Mex. Jan 61. 84p. Order fron
OTS. J2.25
from
SCnXi-410-60-73
toPuUive Joa<liM of cylindrical »t»ella. by W.B
Murfin. Sandiia Corporation, *"*'^
N. Mex. Feb
Abuquerque,
61. 20p. Order from OTS. $1.00.
SCTM-433-60-71
NucJIear spectroscopy of neutron-deficient. Lu .
Ta and Re laotopes, by B. Harmatz ancTothers.
OaJc Ridge National Laboratory, Oak Ridge, Tenn.
and University of Notre Dame, Ind. 1960. 8^.
Order from LC-
Ml $4.80, ph $13.80.
TID-5666
Study erf complex beta decay spectra. Report no 4
progress for Ktay 16. 1959 -May 15, i960, by
M. H. Kurbatov and J. U. Kurbatov. Ohio State
University Research Foundatioo, Columbus,
Ohio. June 60, Contract AT(ll-l)-469. 133p.
Order from LA. Ml $6. 90, ph $21,
Quarterly
May 31
30.
TID-6080
„ eas report for March 1, 1960 to
1. 1«^, by W.P . Coodell. Jr. Columbia
arterly progress repoi
May?l,l(^, byW.F . ,..
University, Nevis Cyclotron Laboratories, Irving-
ton -on -Hudson, N. Y. June 60. Contracts AT
(30-l)-1932; At(30-l)-1019; AT- 30-1 -GEN -72;
Nonr-266(72); 8ndN6-orl-110-l. 20p. Order
from LC. Mi 12. 40, ph $3. 30. TID-6081
Method for detennining the K" spin, by P. Eberbard
«nd M. L. Gooi. College de France, Pari*.
Laboratoire de Physique Atomique ei Moleculaire;
University of Wisconsin, Madison, Wis. and
University of California, Lawrence Radiation
Laboratory. Berkeley. Calif. 1960. Contract
AT(ll-l)-64
ph$4.80
pp. Order from LC. Ml $2. 70.
TID-6157
A study of redundi nt number representations for
parallel diglMl tCTnputers. Thesis, by A
Avizienis. " Uniyersity of Illinois, Urbana. Ill,
May 60. Contract AT(11-1)-4151. 82p. Order
from LC. Ml $4.80, ph $13.80. TID-6168
r
Similarity in the asymptotic behavior of collision-
free hydromagnetic waves and water waves, "By
C. S. Gardner and G. K. Moriicawa. New York
University, Institute of Mathematical Sciences,
New York, N. Y. May 60. Contract AT(30-1)-
1480. 30p. Or^rfromLC. Mi $3.00,
Ph$6.30. TID-6184
The construction and study of a high field plasma
beutroo accelerator. Final report for May 1
1JW:Ae1L30J^. With this are bound pai^n:
Plasma beutron accelerators and A high efficiency
^P>cltor bank study, by gTC. Roger and D. — "*-
Finkelsteln. Stevens Imtltute o* Technology,
Hoboken. N. J. 1960. Contract AT(30-1)-2410
68p. Order fron. LC. Mi $3.90. ph $10.80.
TID-6204
Calculation of heat capacities and derived thermody-
namic functions from thermal data with an IBM
704 dlrital computer, by B. H. lustice. Univ«>r.
sity of Michigan, Ann Arbor. Mich. June 60.
Contract AT(ll-l)-70. 79p. Order from LC.
Ml $4. 50. ph $12. 30. TID-6206
Quantum calculations of the velocity dependence of
the differential and total cross sections for
elastic scattering of molecular beams, by R.B.
Bernstein. University of Michigan, College of
Literature, Science, and the Arts. Ann Arbor,
Mich. Aug 60. Contract AT(11-1)-321. I9p.
Order from LC. Ml $2. 40. ph $3. 30.
TID-6326
InvestigBtion (rf plasma acceleration. Quarterly
progress report no. 1 for June 30, 1956 - Sep-
tember 3U, 1958, by 1^. C. Rogers and otbera.
Stetens Institute of Technology. Hoboken, N. J.
1958. 42p. Order from LC. Mi $3. 30,
Ph$7.80. TID-6359
Radiative decay modes of the moon, by R. R.
Crittenden and others. University of Wisconsin,
Madision. Wis. and Michigan State University,
East Lansing, Mich. 1959. Contract AT(1 1-1)-
64. 45p. Order fromLC. Ml $3. 30, ph$7.80.
TID-6386
Use erf radioisotopes as a source c< x-rays to devel-
°S^ ^^y^g^gh scattering method for the anaTysIs
of high Z atoms in a low Z media . "
Quarterly
process report for the period April 1 5, toTul
1 5, 1960. Tracerlab, Inc., Wal&yim. Mass
1960. Contract AT(30-1)- 2538. 24p! Order
fromLC. Mi $2.70. ph $4.80. TID-6390
Solid state physics program. Tanperature variation
of spontaneous niagnetization in thin iron films.
lechnical report no. 8, by K. H. Rosette. <?aae
institute of Technology, Cleveland. Ohio. Apr
60. Contract AT(ll-l)-623. 40p. Order from
LC. Mi $2.70, ph$4.80. TID-6391
Radioactive decay of Pm^^3 Pm^^, and Pm^^, by
E. G. Funk. Jn and others. University of Notre
I>Bme, Notre Dame, Ind. 1960. Contract AT
(ll-l)-498. 43p. Order fromLC. Mi $3. 30,
Ph$7.80. TID-6458
672
Nuclear spectroscopy and the application of radlo-
isotopes to the study of reaction kinetics. Prog-
ress report no. 2 for August I. 1959-July 31.
I960. Includes appendixj^: The L/K-c&pture
ratio and EL /EK for Ar^\ by D. C. Conway and
A. G. Santos -Ocampo. Purdue University Lafa-
yette, Ind. and Purdue Research Foundation,
Lafayette, Ind. 1960. Contract AT(ll-l)-694.
28p. Order from LC. Ml $2.70, ph $4. 80.
TID-6476
Progre
ss report for 1959-1960. University of
ansas. Nuclear Physics Laboratory, i_dwrence,
Kan. I960. Contract AT(ll-l)-83. 80p. Order
fromLC. Ml $4. 50. ph $12. 30.
TID-6503
Summaries of fuels and materials development
programs, by D. E. Deutsch and others. Aug
60. Fuels and Materials Development Branch.
Nuclear Technology, Division of Reactor Develop-
ment. Washington. D. C. Aug 60. 103p. Order
from OTS. $2. 25. TID-6506
Annual report of project on anisotropic diffusion,
by H. B. Huntington. Rensselaer Polytechnic
Institute. Troy, N. Y. Aug 60. Contract AT
(30-l)-1044. 6p. Order fromLC. Ml $1.80,
ph$1.80. TID-6511
Studies relating to scattering of neutrons and allied
phenomena. Proposal for renewal of Contract
?nX30-l)-1679 for period January 1, 1961 -
December 31, 1961 and Annual progress report
tor 1960, by D. M. Van Patter. Bartol Research
Foundation. Swarthmore. Pa. Sep 60. 40p.
Order from LC. Mi $3.00, ph $6. 30.
TID-6609
Effect of creep on stresses in cylindrical shells
structural memo no. 51, by H. Poritsky. Gener-
al Electric Company, General Engineering Lab-
oratory. Schenectady. N. Y. Aug 60. Contracts
AF 33(600)-38062 and AT(11-1)-171. 18p.
Order from LC. Mi $2. 40, ph $3. 30.
TID-6645
Input- output modifications of gamma heating pro-
gram 0307 for a finite heterogeneous cylinder,
by M. R. Smidi. General Electric Company,
Aircraft Nuclear Propulsion Department, Cincin-
nita. Ohio. July 60. Contracts AF 33<600)-
38062 and AT(11-1)-171. I6p. Order from LC.
Ml $2. 40. ph$3.30. TID-6646
Interacting Fermi systems, by K. Harrison. Los
Alamos Scientific Laboratory, Los Alamos,
N. Mex. 1960. 94p. Order from LC. Mi $5.40.
ph$15.30. TID-6676
(S .aP) relatlveparity and the Da lie decay ol the
X^hyleron. Technical report no. 188, by J.
Sucher and G.A . Snow. University of Marybuid,
College Park, Md. July 60. Contract AF 49
(638)-24. (AFOSR -IN -60-853). 7p. Order
fromLC. Mi $1.80, ph $1.80. TH>-6699
Programme and abstracts of papers. Second annual
meeting of d>e Division of Plasm* Kiysica of ifae
American Physical Society held at GatUnburg,
Tennessee, Noveinber 2-5, I960. American
Physical Society, New York, N. Y. and Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Nov 60. 89p. Order from LC. Ml %4. 80,
ph $13.80. TID-6829
CEPTR— An IBM-704 code to solve the P-3 approxi-
matlon to the one-velocit
mauon to the one -velocity transport equatioo
in cylindrical geometry, by P. B. Dattch and
others. ComlNistion Engineering, Inc. , Nuclear
Division. Windsor, Conn. Sep 59. 41p. Order
fromLC. Mi $3.30, ph $7.80. TID-6940
Ang^e, a two dimensional, multlgnxm, neutron
diffusion reactor code for IBM 70^, by R. Stuart
and S. Stone. University of California, Radia-
tion Laboratory, Livermore, Calif. 1957. 37p.
Order from LC. Ml $3. 00. ph $6. 30.
UCRL-5019
Small-scale instabilities of the pinch and a suggeated
remedy — the levitron. byS. A. Colgate an"
H. P. Furth. University of California, Law-
rence Radiation Laboratory. Livermore. Calif.
Nov 58. Changed from OFFICIAL USE CWLY
July 20. 1960. Contract W-7405-eng-48. 27p.
Order from LC. Ml $2.70. ph $4.80.
UCRL-5392
Radial distribution of plasma in astron's E-Uyer,
by L. Tanks. Uni>«rsity of California, Law-
rence Radiation Laboratory. Livermore. Calif.
Dec 58. 3p. Order from LC. Mi $1.80.
ph$1.80. UCRL-5418-T
A note on the optical potential witfi the Pauli princi-
pie, by M. A. Mittleman. University of Califor-
mT, Lawrence Radiation Laboratory, Livermore,
Calif. July 60. Contract W-7405-eng-48. lip.
Order from LC. Mi $2. 40, ph $3. 30.
UCRL-6022-T
Cross sections and spectra for negative electron
Bremsstrahlung. by N. E. Hansen and S. C.
Fulu. University of California. Lawrence
Radiation Laboratory. Livermore. Calif. Nov
60. Contract W-7405-eng-48. 39^). Order
from OTS. $1.00. UCRL-6099
673
AmlyaU o< ttuclaDo-aucleon acatterigg experiments,
by H. P. Noyes. University erf CaUfornia, Law-
reoce Radiatiqn Laboratory, Livermore, Calif.
Aug 60. Coottact W-7405-eng-48. 32p. Order
fromLC. Mi *3. 00. ph $6. 30. UCRL-6108-T
Magnetic core
aanoaecodS
J
ts for
- --J- P"^**^ operation at 30
on^ piUae wi<fah, by G. A. Reeser. Uni-
versity (rf California, Lawrence Radiation Labor-
atory, Livermore, Calif. Aug 60. Contract
W-7405-eng-4«. 16p. Order from LC.
Ml $2. 40, pii|3.30. UCRL-6121-T
Hindrance ftctora for alpha decay, by H. V. Michel.
University of (California. Lawrence Radiation
Laboratory, Berkeley, Calif. May 60. Con-
tract W-7405-*ng-48. 26p. Order from LC.
Mi $2. 70. ph U. 80. UCRL-9229
Experiments with pulsed naagpetic cuape. byJ.P.H.
Watteau. University of California, Lawrence
Radiation Laboratory. Berkeley, Calif. Aug 60.
Changed from OFFICIAL USE ONLY Auguat 31.
1960. Contract W-7405-eng-48. 17p. Order
from LC. Mi t2. 40, ph %i. 30. UCRL-9239
r
The early antiproton work, by O. Chamberlain.
University of Chlifbmia, Lawrence Radiation
Laboratory, Betrkeley, Calif. Dec 59. Contract
W-7405-eng-4a. 34p. Order from LC.
Mi $3. 00, ph $^. 30. ' UCRL-9380
N^^ (p, p2n)N^^ reaction Induc^ by protons of eh-
ergy 0. 4 to 6. 2 Bev by L. Chang Sah. Univer-
sity of CaUfomia, Lawrence Radiation Labora-
tory, Berkeley,, Calif. Aug 60. Contract W-
7405-eng-48. |6p. Order from OTS. 75 cents.
UCRL-9394
-48. W
Charged E -hyperion pro(hiction and decay: Ener-
getics, lifetimeji, and branching ratios, by J.N.
Dyer. University of Californiar Lawrence
Radiation Laboratory, Berkeley, Calif. Nov 60.
Contract W-7406-eng-48. 89p. Order from
OTS. $2.00. UCRL-9450
int4
S- and P-wave interactions of k" mesons in hydro-
gen, by P. Nordin, Ir. University of California-
Lawrence RadiaKion Laboratory, Berkeley, Calif.
Nov 60. Contract W-7405-eng- 48. 40p. Order
from OTS. $1.00. UCRL-9489
Bibliography on twQ-phase t«ait transfer, by G. W.
Maurer. Westii^ouse Electric Corporation,
Bettis Atomic Power Laboratory, Pittsburgh,
P». Aug 60. Contract AT-U -1 -GEN -14. 19p.
Order from OTS. 75 cents. WAPD-TM-249
Measurement of Ae natural neutron source In two
cores, byW. B. Doub and S. Milani. Weating~-
house Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburgh, Pa. Nov 60.
Contract AT-ll-l-GEN-14. I6p. Order from
OTS. 50 cents. WAPD-TM-254
.■>»-\;
Radiation Effects on Materials
Summary of UO-y—stainless steel dispersion ele-
ment irradiadon experiments, by V. Q. Haynea
and others. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Mar 58. Decl. September
14, 1959. Contract W-7405-ent-26. 14p.
Order from LC. Ml $2. 40, ph $3. 30.
CF-58-2-71
Irradiation effects in cladding materials , by J. E.
Minor. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Apr 60. Decl. May 19, 1960. Contract AT
(45-l)-l350. 23p. Order from LC. Mi $2.70,
PhM.80. HW- 64688
ETR radiation damage surveillance prograi
ress repon I, by M. J. Graber and I. H
ams
iia-
Ronsick. RiiUipe Petroleum Company, Idaho
Operations Office, Idaho Falls, Idaho. Jan 61.
Contract AT(10-l)-205. 29p. Order from OTS.
50 cents. * IDO- 16628
Radiation tolerance of a select group of semicon-
ductor diodes, by C. I. Westmark. Sandia
Corporatinn, Albuquerque, N. Mex. Nov 60.
14p. Order from OTS. 50 cents.
SCTM-404-60-14
Review of Hanford radiation damage studies on
graphite, by R. E. Nightingale" General Elec-
tric Company, Hanford Atomic Products Opera-
tion, Richland, Wash. Mar 59. Contract W-
31-109-Eng-52. 5p. Order from LC. Mi $1.80,
ph$1.8 0. TID-6504
Reactor Technology
Prototype power plant gas-cooled reactor project.
2 from March 15, 1959 to
Process report noT
September 30, 1959.
. _ --■ - .-- American Electric Power
Service Corporation, New York, N. Y. Oct 59.
Contract AT(38-l)-200. 175p. Order from LC.
Mi $8. 10, ph$27.30. AEPSC-608
674
Sulfur cooled power reactor itudy
DO. 1 for period October 1, 1959 to January 1,
Quarterly report
I960. Aerojet- General Nucleonics, San Ramon,
XSB. 1960. Contract AT(04- 3) -251. lip.
Order from LC. Mi $1.80, ph $1.80.
AGN-150
Water chemistry and fuel element scale in EBWR,
by C. R. Breiden and odiers. Argonne National
Ltboratory, Argonne, III. Nov 60. Contract
W-3l-109-eng-38. I05p, Order from OTS.
$2.25. ANL-6136
Theoretical feedback analysis in boiling water reac-
tors, by A. Z. Aksasu. Argonne National
Laboratory, Argonne, 111. Oct 60. Contract
W-31-109-eng-38. 6<^. Order from OTS.
$1.50. AN L- 6221
Terminal report on the boiling slurry reactor ex-
periment'(SLURREX), by G. A. Freund and
others. Argonne National Laboratory, Argonne,
111. Dec 60. Contract W-31-109-eng-38. 97p.
Order from OTS. $2.25. ANL-6248
A lunar power plant, by R. H. Armstrong and others.
Argonne National Laboratory, Argonne, 111.
Dec 60. Contract W-3l-109-eng-38. 137p.
Order from OTS. $2.50. ANL-6261
Insybility studies widi EBR-I, Mark HI, by R. R.
Smith and others. Argonne National Laboratory,
Argonne, III. Dec 60. Contract W-31-109-eng-
38. 92p. Order from OTS. $2.00.
ANL-6266
Shield design methods for Argonaut -type reactora, 3
by J. Fagan. Argonne National Laboratory]
Argonne, 111. Mar 60. Contract W-13-109-eng-
38. 38p. Order from OTS. $1.00.
ANL-6281
Reactor develcyment prograin progr^s report, by
W. Hilberry and othera. Argonne National
Laboratory, Argonne, 111. Dec 60. Contract
W-3l-l09-eng-38. 64p. Order from OTS.
$1.75. ANL-6295
Reactor development program progress report, by
N. Hilberry and otners. Argonne National Labor-
atory, Argonne, 111. Jan 61. Contract W- 31-
109-eng-38. 66p. Order from OTS. $1.75.
ANL-6307
SM-1 research and development "task XV" zero
pCT»er experiments for SM-1 core II and SM-IA
core I, by R. A. Robinson and others. Alco
Products, Inc. , Schenecudy, N. Y. Oct 60.
Coatraa AT(30-3)-326. 92p. Order from LC.
Mi $4. 50. ph$12.30. APA£-58(Rev.)
Analysis ^ zero power emerinaents on SM-1 core
II and SM-IA core I, byS. Paluszkiewicz. Alco
Products, Inc., Schenectady, N. Y. Oct 60.
Contract AT(30- 3)- 326. 45p. Order from LC.
Mi $2.70. ph$4.80. APAE-71
SM-2 reactor core and vessel review report for
period December 15 1959 to March 18, 1960,
by H. L. Hoover. Alco Products, Inc. , Scfaenec-
Udy, N. Y. Mar 60. Contract AT(30-3)-326.
14^. With this is bound: SM-2 core materials
developinent pro-am. Battelle Memorial Insti-
tute, Columbus. Ohlor Order from LC.
Mi $7. 20. ph$22.80. APAE -Memo- 250
SM-1— research and developnaent quarterly report
for Octc^r 1 to December 31, 1959, by J. O.
Brondel and others. Alco Products, Inc. ,
Schenectady, N. Y. Apr 60. Contract AT(30-3)-
326. 91p. Order fromLC. Mi $4.50. ph$12.3Q
APAE -Memo- 251
SM-1 reactor vessel penetrated gasket deaign and
test report, by F. G. Gebbardt. Alco Products,
Inc.. Scfaeoectady, N. Y. June 60. Contract
AT(30-3)-326. 56p. Order from LC. Mi $3. 60,
ph $9. 30. APAE -Memo- 254
Vibration and collapee testing of SM-2 fuel elements.
Period covered January 1959 to January I960, fiy~
D. J. Morehouse and J. A. Christenson. XIco
Products, Inc. , Schenectady, N. Y. July 60.
Contract AT(30- 3)- 326. 53p. Order frcMn LC.
Mi $3. 30. ph$7.80. APAE-Memo-265
Thermal stress testing of SM-2 fuel elements.
Final report for January I, 1959 to July l.~l960.
by J. A. Christenson and J. D. Kormeuer. ^co
Products, Inc. , Schenectady, N. Y. Sep 60.
Contract AT(30-1)- 326. 31p. Order from LC.
Mi $2.70. ph$4.80. APAE -Memo- 268
Summary of reactor design information from three
years operation oi a small PWR, by J.~d
Gallagher. Alco Products, Inc. , Schenectady,
N. Y. Sep 60. Contract AT(30-3)-326. 43p.
Order from LC. Mi $3. 30, ph $7. 80.
APAE -Memo- 273
Striytural testing of ^-2 fuel elements, by F. G.
Coleman, Jr. and R. J. Herbert. Alco Products,
Inc. , Schenectady, N. Y. Sep 60. Contract
AT(30-3)-326. 70p. Order from LC. Mi $3.60,
ph $9. 30. APAE -Memo- 275
675
Studies (rf reactoi- ooottiranent. Summary report
no 3 covering tfte period February 1, 1960 to
Jiii2_^1^4V«J . by T. A . Zaber . A ntiSOrRiSiarch
Foundadon, Illinois Institute of Technology,
Chicago, 111. Aug 60. Cootract AT(ll-l)-528.
83p. Order faom 0T5. $2.25. ARP-4132-14
plMi
Fpint source explpaion in a soUd. by T. A. Zaker.
Armour Research Foundatioo, Illinois Institute
o# Technology, Chicago, Ul. Nov 59. Contraa
AT(n-l)-528. lOOp. Order from OTS. $2.50.
ARF-4132-6
"Hie effect of end conditions on the dynamic respon
Of cylindrical ahells. by R. L (Jilaperm »n/^
P. G. Hodge, Jr. Xrmour Research Foundation.
UUnois InstituQe of Technology, Clilcago, 111.
July 60. CoQtr»aAT(ll-l)-528. 65p. Order
from OTS. $2,00. ARF-4132-8
ise
Liquid metal fuel reactor experiment. Investigation
<y txrylllum welding techniques for reactor tcH
thimble Jolna, by P. C. Thva. Tlie Haht^^^
and Wilcox Company, Lynchburg, Va. Apr 60.
Cootract AT(30hl)-1940. 20p. Order from 015.
75 cents. BAW-UOO
Pe«»iblUty study at a high temperature Integral
jjquid metal fual reactor for low coat powefT by
Babcodc and Wilcox Con^jany, Lynchburg, Va.
Apr 60. Contract AT(30-1)-1940. lOIp. Order
from OTS. $2,175. EAW-1156-1
•r
^•■•■uapenalon reactor coolants, by D. C. Sdiluder-
berg. Babcock and Wilcox Company, Atomic
Energy Division, Lynchburg, Va. Dec 59. 27p.
Order from LC* Mi $2. 70. ph $4.80.
BAW-1182
Engineering expertence at Brookhaven Nad coal
Laboratory in handling fused chloride salts, by
C. J. Raseman and others. Brookhaven National
Ltboratory, Upton. N.Y. June 60. 27p. Order
OTS. 75<Jent8. BNL-627(T-192)
A aurvey ol bulk -bailing studies in pressurized
water reactor systems, by H. Suaskind. Brook-
haven Nadooal Laboi
60. 16p.
3ratory,
Ordet from OTS
Upton, N. Y. Aug
SO cents.
BNL-636(T-199)
ABWR PL-1 referetice design report, by F. J, Staroo
and L. M. Johnson. Combuation Engineering,
Inc. Nuclear Division. Windsor, Coon. Jan 60.
Cootract AT(10-|)-967. 121p. Order from LC.
Mi $6.90. ph$2i.30. CEND-70
Barkelew. Oak Ridge National Laboratory, Oak
Ridge, Tenn. May 53. Changed from OFFICIAL
USE CWLY October 4, 1960. 28p. Order from
LC. Ml $2.70. ph $4.80. CF-53-5-225
A preliminary study of molten salt power reactors,
by H. G. MacHiersoo and others. Oak RUge "'
National Laboratory, Oak Ridge, Tenn. Apr 57.
Decl. with deletions November 20, 1957. Coo-
tract W-7405-eng-26. I43p. Order from LC.
Mi $7. 20, ph $22.80. CF-57-4-27(Rev.XDeL)
Pei^rmance of HRT charcoal beds, by H. O.
weeren and W. J. Lee. Oak Ridge National
Laboratory, Oak Ridge, Tenn. June 57. Coo-
tract W-7405-eng-26. 21p. Order from LC.
Ml $2.70, ph$4.80. CF-57-6-120
Hi
gh flux Isotope reactor— a general description,
by T. E. Cole. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Mar 60. Contract W -7405-
eng-26. 66p. Order fr«n LC. Mi $3. 90.
Ph$10.80. CF-60-3-33
Potgot^ng and fuel cycle costs for fluid fuel reactora.
by W. D. Burch and odiers. Oak Ridge National
Laboratory, Oak Ridge. Tenn. July 60. 46p.
Order from LC. Mi $3. 30, ph $7.80.
CF -60-4-1
Studies of improvement of power density
loops, by M. L Tobias and D. R. Vondy
in ORR
^ , ■ , — , — ,. Z>ak
Ridge National Laboratory, Oak Ridge, Ttenn.
Apr 60. Contract W-7405-eng-26. Up. Order
fromLC. Mi $1.80, ph$1.80. CF-60-4-31
The shield of the 01 LNL-research reactor, by C. H.
Crttl<^llty in die HRT transfer vessel, by S. Jaye
and L. L. Bennett. Oak Ridge RaBooal Labora-
tory, Oak Ridge, Tenn. July 60. 7p. Order
fromLC. Ml $1.80. ph $1.80. CF -60-7 -81
Reactor physics calculations for the MSRB, by
C. W. Nestor, Jr. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. July 60. I4p. Order
fromLC. Ml $2. 40, ph $3. 30. CF-60-7-96
Recent developmentt in magnet design and fabrlca-
tion proce<Lres (BSR type magnett), by I. R.
Tallackson and R, T. SantoroT Oak Ridge Nadoo-
al Laboratory, Oak Ridge, Tenn. July 60. 31p.
Order fromLC. Mi $3. 00. ph $6. 30.
CF-60-7-109
HFIR respwise to void swept into flux trap, by R. S.
Stone. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Aug 60. 9p. Order frwn LC.
Mi $1.80, ph$1.80. CF-60-8-39
676
Operating manual for the Oak Ridge research reac-
tor, by S. D. Sheppard and otters. Oak Ridge~
National Laboratory, Oak Ridge, Tenn. 1960.
358p. Order fromLC. Mi $11. 10, ph $66.60.
CF-60-8-46
Summary of HRT run 18, by H. F. Bauman and
others. Oak Ridge National Laboratory, Oak
Ridge. Tenn. Aug 60. 5lp. Order from LC.
Ml $3. 60, ph$9.30. CF-60-8-152
griod April 1959 to April 1960,
ORR cyeratiOQS for pei _
J. A. Cox. Oak Ridge National Laboratory,
Oak Ridge, Tenn. Sep 60. 144p. Order from
LC. Mi $7.20. ph $22.80. CF-60-9-2
Preliminary analog computer study of the small
BGCR In -pile Joope. by 5. ]. Ball and E. G.
Beasley. Oak Ridge National Laboratory, Oak
Ridge, Tenn. Sep 60. 54p. Order from LC.
Ml $3. 60, ph$9.30. CF-60-9-118
HPni reactor vessel expansion problems, by W.R.
Gall. Oak Ridge National Laboratory, Oak
Order from LC.
CF -60- 10-7
Ridge, Tenn. Oct 60. Ip.
Mi $1.80, ph$1.80.
Deacrlption of the IEM-704 code for die calaUatioo
of coocentradon gansients in tie HRT, by H. B.
Piper and F. N. Haubenreich. Oak Ridge Nation-
al Laboratory, Oak Ridge, Tenn. Oct 60. 1^.
Order fromLC. Ml $1.80, ph$1.80.
CF- 60- 10-8
ram
Reaearcfa and development progn
reaa report for the period Octobe
quarterly
erl, 19«
prog-
i9 to
Decenaber 31. 1959," by P. G. DeHuff. Westing-
house Electric Corporatioo, Atomic Power
Department, Pittsburg Pa. Feb 60. Contract
AT(30-l)-2289. 127p. Order from LC.
Mi $6. 90. ph $21.30. CUNA-45
Coptrol rod poeltioos for cirtlMllty 0 EFPH. Core
I, seed 2. Duquesne Light Conqpany, Shipping-
"PT July 60. 20p. Order from LC.
DLCS-1490209
port. Pa. July 60. 20p.
Mi $2. 40, ph$3.30.
Periodic radiation aurvey of reactor plant container
Core I. seear
and components after shutdown.
l^ctlcn 3. Duquesne Light Company, Shipping^
'June 60. lOp. Order from LC.
port. Pa.
Ml $1.80, ph$1.80.
DLCS-1840307
Reactor and presaurizer relief valve bellows rupture
teat. Corel, seed 2- Section 1, Duquesne
Light Company, Shippingport, Pa. July 60. 8p.
Order fromLC. Mi $1.80, ph $1.80.
DLCS-3470101
Heavy water moderated power reactors. Progress
report for November 1960, by R. R. Hood and
L. laakoff. E. I. du Pont de Nemours and Com-
pany, Technical DivlBloa, Wilmingtoo, Del.
Feb 61. Contraa AT(07-2)-l. 40p. Order
from OTS. $1.00. DP-565
Heavy water nnoderated power reactors. Progress
report for December, 1960, by R. R. Hood and
L. IsakoCf. E. I. du Pont de Nemours and Com-
pany, Technical Division, Wilmington, Dd.
Mar 61. Contract AT(07- 2)- 1. 3^. Order
from OTS. 75 cents. DP-575
Maritime gas -cooled reactor program
Quarterly
March 31,
progress report for the periodending .
1960. General Dyanmita Corporation, General
Atomic and Electric Boat Divisions, San Diego,
Calif. 1960. Contract AT(04-3)-187. 135p.
Order from OTS. $3.00. GA-1259
The effects of atomic nytions on the moderation o<
neutrons, by D. E. Parks. General Dynamics ~
Corporatfon, General Atomic Diyislao, San
Diego. Calif. Oct tt. 31p. Order from LC.
Ml $3. 00. ph $6. 30. GA-1660
A fortran program for studying the core cooling
capacity of a bellum-air mixture, by R. C.
Kaeatner and R. J. Mulvihiir General Atomic
DivlaioQ, General Dynamics Corporation. San
Diego. Calif. Feb 60. Contract AT(04-3)- 314.
59p. Order from LC. Mi $3. 60, ph $9. 30.
GAMD-1224
Fuel cycle prograni, a boiling water reactor re-
search and oevelopment program. First »^-
mary report for iJlarcfa 1959-July 1960. by W. H.
Cook. General Electric Company, Ttomic
Power Equipment Department, San Joee, Calif.
Contract AT(04-3)-189. 59p. Order from LC.
Mi $5.40, ph$15.30. GEAP-3516
Hete
n-
tieous iattice fluidized bed reaccpr study
rabbit reactor. " by E. R. Astley. General
Electric Company. Hanford Atomic Products
Operation, Richland, Wash. Mar 57. Contract
AT(45-1)-1350. 24p. Order from LC.
Mi $2.70. ph$4.80. HW-48847
Effect of die PRTR hi;
recycle
igh pressure loop oo plutonlum
program qp}ectiyes. by R. E. Peterson.
General Electric Compaoy, Hanford Atcxnic
Products Operation, Richland. Wash. Oct 59.
Contract AT(45-1)- 1350. Up. Order from LC.
Mi $2. 40, ph$3.30. HW-62531
Decootaminatlon studies for HAPO high temperature
reactor recrlculation systems. Progress report
677
far June 1959 to January I960, by T. F. Demmitt
and others. General Electric Company, Hanford
Atomic Producta Operation, Richland, Wash.
Mar 60. Coqtract AT(45-1)-1350. 65p. Order
fromOTS. lil.75. HW-62806
J. il.75.
APDAC-1, A PCTR data analysis code for the IBM
709, by J. R. Lilley. General Electric Company,
Hinford Atomic Products Operation, Richland,
Wash. Sep 6C. Contract AT(45-i)- 1350. 40?.
Order from 1^. Mi $3. 00, ph $6. 30.
HW-63592
A mathematical fcnd statistical approach to the de-
sign and analysis of a reactor containment vessel
pressure test, by W. L. Nicholson. General
Electric Company, Hanford Atomic Products
Operation, Rjphland, Wash. Mar 60. Contract
AT(45-1)-1350. 21p. Order from LC. Mi $2. 70.
P*»M.80. i HW-64446
•ess report for April I to
. ■ --- /olume II. SL-1 health physics
and safety, by Cc«nbuatlon Engineering. Inc. .
Nuclear Division. Idaho Falls, Idaho. Aug 60.
Contract AT(lD-l)-967. 18p. Order from LC.
Mi $2.40, ph$3.30.
IDO-19017 (CEND-lOOOXVol. U)
Army gas -cooled; reactor systems program. In-
terim report ip-pile testa of GCRE-ffl
report ip-pile testa of GCRE-IB prototype
fuel elements, by H. T. Watanabe and others .
Aerojet-Gene eal Nucleonics, San Ramon. Calif.
Oct 60. Contract AT(10-l)-880. 69p. Order
fromOTS. %^.Q0. IDO-28552
Army gaa-coolecl reactor systems progri
Monthly progress report for July [96(57 Aerojet
General Nucle^mics, San Ramon. Calif. Aug 60.
Contract AT(ll)-l)-880. 85p.
Mi M-80.ph|13.80.
Order from LC.
IDO- 28559
Reactor »chnoloy report no.
b. T. Goldmaojand others. ~
IS, physics, by
General Electric
Company, Knolls Atomic Power Laboratory.
Schenectady. N. Y. Dec 60. Contract W- 31 -109-
Eng-52. 188p^ Order from OTS. $2. 25.
lCAPL-2000-12
A comparison betiireen experlmenul and calculated
ff ^"^" t° ?f..^^^^^ ^^°™ 68"F-550"P of an
" ' X 30" X 32" core having various weight percent
T . „ ..,
B-10 stainless steel septa" by G. D. Hickman an^
others. ICnolla Atomic Power Laboratory, Sche-
Dectady,N.Y. Oct 59. Contract W-3l-109-Eag-
52. lOlp. Or4er from LC. Mi J5. 40,
I*J15.30. lCAPL-M-GDH-2
Large •cale
rge 'cale preparatioo of hirii purity plut<
mettl try electrorefining. Preliminary ri
L.J. Mullin& and others. June 60. CoiQi
W-7405-ENG-36. June 60.
LC. Mi $2.40, ph$3.30.
ity Plutonium
report,
itract
16p. Order from
LAMS -2441
Quarterly sMtus report of the LASL plasma thermo-
couple development program for pieriod ending ~
L>ecember20 I960. Upiversity of (^iliforaia.
Loa Alamoe Scinntific Laboratory. Los Alamos,
N. Mex. Dec 60. Contract W-7405-ENG- 36.
I8p. Order from OTS. 50 cents.
LAMS-2504
Results of high-temperature strain-fatigue tests on
reactor-grade aluminum-base materials. 6y
W. F. Anderson and W. Wahl. Atomics Inter-
aational, A Division of North American Aviation,
Inc., Canoga Park, Calif. Jan 61. Contract AT
(ll-l)-GEN-8. 42p. Order from OTS. $1.25.
NAA-SR-4528
Eteslgn aivd analysis of a uranium-3. 5% molybdenum
afloy CMRE core, by B. L. Hoffman and otterT
Atomics International. A Division ot North
American Aviation, Inc. . Canoga Park. Calif.
Jan 61. Contract AT(ll-l)-GEN-8. 150p.
Order fromOTS. $2.75. NAA-SR-5I74
Design modlflcatioos to the SRE during FY 1960. by
G. E. Deegan and others. Atomics International.
A Division ol North American Aviatioa, Inc. .
Canoga Park. Calif. Feb 61. Contract AT(11- 1 )-
GEN-8. I06p. Order from OTS. $2.25.
NAA-SR-5348 (Rev.)
Kinetic enaerlmentt on water boilers "A" core re-
port. Part V - conrainment aspects of pressure
waves from initial solution exmnsion. by M. A.
Greenfield. Atomics Internanonal. A Division
oi North American Avaition. Inc. , Canoga Park,
Calif. Feb 61. Contract AT(I1-1)-GEN -8. 32p.
Or^r from OTS. 75 cents. NAA-SR-5419
Design and ^^^fn^j ap*tyaia erf sodium specialties
CCTiponents for HNPF, by w: M. Hoschouer and
others. Atomics International. A Division of
North American Aviation. Inc.. Canoga Park.
Calif. Feb 61. Contract AT(Il-l)-GEN-8.
49p. Order from OTS. $1.00. NAA-SR-5445
U^d hydrocarbon as SRE core tank protection
during core exchange, by F. W. Dodge and T. D.
Chilton. Atomics International. Division of
North American Aviation, Inc. , Canoga Park,
Calif. Nov 58. 13p. Order from LC. Mi $2.40,
I* $3. 30. NAA-SR-Memo-3291
678
Worth of enriched uranium fuel after irradiation
— "in the SRE, by R. W Woodruff. Atomics Inter-
national. Division of North American Aviation,
Inc. . Canoga Park, Calif. May 59. 3p. Order
from LC. Mi $1.80, ph $1.80.
NAA-SR -Memo- 3933
Pressure drop measurements across a mockup of
an SRE 7 -rod fuel element with an orifice plate
at the top, by R. J. Begley. Atomics Internation-
iT Division of North American Aviation, Inc. .
Canoga Park, Calif. Dec 59. 12p. Order from
LC. Mi $2. 40, ph $3. 30. NAA-SR-Menx)-4776
Summary of data on high tenipe
element materials, by A.Sti
rature reactor fuel
ly A.i»trasset\ Nuclear
Development Corporation of America, White
Plains, N. Y. Sep 56. Decl. March 25, 1960.
Contract AT(30-l)-862. I79p. Order from LC.
Ml $8. 10, ph$27.30. NDA-64-103
Piwling lattice test rig operating naanual, by R.
Schamberger and G. Poster. Nuclear Develop-
ment Corporation of America , White Plains,
N.Y. Apr 60. Contract AT(30-1)-2303(DC).
62p. Order from LC. Ml $4. 50. ph $12. 30.
NDA-2131-9
Prellniinary deaign ot the ORNL fast burst rMctca-,
by G. Breidenwch and others. Nuclear Develc^-
ment of America. White Plains, N. Y. July 60.
120p. Order from LC. Mi $6.90. ph $21. 30.
NDA-2136-1
Operational procedures and some accident analysis
for the ORNL fast burst reactor, by G. Breiden-
bach and others. Nuclear Development Corpora-
tion of America, White Plains, N. Y. June 60.
20p. Order from LC. Mi $2.70, ph $4.80.
NDA -Memo- 21 36- 3
^^
PISiT
construction, and operation of a pulaed sub-
cal uranium assembly for educadonal uses.
art. Rensselaer Polytechnic Institute,
T7 Dec 59. Contract AT(30- 3)- 294.
81p. Order from LC. Mi $4.80. ph $13.80.
NYO-9055
rinai repoi
Troy" N!y
Thermodynamiic and heat transfer analyais of the
aircraft reactor experiiasm, by B. Lubaraky"and
B. L. Greenstreet. Oak Ridge National Labora-
tory. Oak Ridge. Tenn. Aug 53. Decl. July 14.
1959. Contract W-7405-eng-26. 131p. Order
from LC. Mi $6. 30, ph $19. 80. ORNL-1535
ress rei
Oak Ri
Tenn. June 56. Decl. with deletions November
10, 1959. Contract W-7405-eng-26. 225p.
Order from LC. Mi $10. 20, ph $36. 30.
ORNL-2061 (Pts. I, U, UIXDel.)
Solid state division semiannual progress report for
period ending August 30. 1956. Oak Ridge
National Lalx>ratory, Oak Ridge, Tenn. Dec 56.
Decl. July 12, 1960. Contract W-7405-eng-26.
39p. Order from LC. Mi $3. 00, ph $6. 30.
ORNL-2189
Maritime reactor project. Annual pt-ogress report
for period ending November 30, 1965, by H.C.
McCurdy. Oak Ridge National Laboratory,
Oak Ridge, Tenn. 1960. Contract W-7405-eng-
26. 59p. Order from OTS. $1.50.
ORNL-3046
Monthly technical report for May 1960. Power
Reactor Developnient Company, Detroit. Mich.
1960. Contract AT(ll-l)-476. 12p. Order
from LC. Mi $2.40. ph $3.30. PRDC-TR-35
Monthly technical report fOT June 60. Power Reactor
Development Company. Detroit. Mich. 1960.
Contract AT(ll-l)-476. 13p. Order from LC.
Mi $2. 40, ph $3. 30. PRDC-TR-36
Heavy water power reactor parog-am monthly prog-
ress report. October_19o0. Savannah River
Operations Office. AEC. 1960. 19p. Order
from LC. Mi $2.40, ph $3.30. SRO-38
Specification for fixed in -plant radiation monitoring
for die Enrico Fermi Atomic Power Pl*Pt, by
G. C. BurkittandJ. J. Owens. Atomic Power
Development Associates, Inc. , Detroit, Mich.
Aug 59. 27p. Order from LC. Mi $2.70,
ph$4.80. TID-5686
The practical arolication of space nuclear power
in the 1960'Kfor the Interniational Astronautical
Coogrei
as, Stockholm, Swieden August 15-20."
1960, by J. R. Wetch and others. Atomics Inter-
national. A Division of North American Aviation.
Inc. . Canoga Park, Calif. 1960. Contract AT
(ll-l)-lGEN-8. 50p. Order from OTS. $1.25.
TID-6312
HTGR steam generator deaign-1, by H. N. Woebcke.
General Atomic Division, General Dynamics
Corporation, San Diego, Calif. Oct 59. Con-
tract AT(04-3)-314. 23p. Order frOTi LC.
Mi $2.70, ph$4.80. TID-6337
Program SHAG- -A monoenergetic muldreglon slab
cell correction calculation (cSi^-AKIH) tgogram"
). 518), by F. D. Wenstrup. General Electric
no.
679
Company, AUrcnft Nuclear PropulBioa Depart-
ment, Cincinnati, Ohio. June 60. Contracts
AF33(600)-38062aiidAT(ll-l)-171. 89p. Order
fromLC. Ml $4.80. ph $13.80. TID-6643
program for the prepa ration d
wiai fine energy deaill (progra
554), by J. tl.T^ooper aVl W.
Ceneral Electric Company, Al
A program for the preparatioo ati nuclear data tape
IT detail (program FINDT, ANt>NQ-
Mper and W. B. Henderson.
Company, Aircraft Nuclear
Prc^xilsion Department. Cincinnati, Ohio. May
60. Contracts AF 33(600)- 38062 and AT(1 1-1)-
171. 81p. Order fromLC. Mi $4, 50,
ph$12.30. i TID-6647
Co>ta of nuclear power. (Replaces report TID-
8506_of July mt^), by M. V. Searl and others.
Office d Opaaations Analysis and Forecasting
United Sute Atomic Energy Commission, Oak
Ridge. Tenn. Jan 61. 40p. Order from OTS.
50 cents. j TID-8531
Nuclear fuels aiid materials development. Division
of Reactor Development, Atomic Energy Ckxn-
mission, Washington, D. C. Feb 61. 171p.
Order from 0T5. $2.75. TID-11295
fetg^ »chPlaH review, by R. H. Fillnow and others.
Westioghousa Electric Corporation, Bettia
Atomic Powef Laboratory, Pittsburgh, Pa. Nov
60. ContracuAT-ll-l-CJEN-U. 97p. Order
from OTS. $|2.25. WAPD-BT-21
I
Trans
ansport flux pfeaking calculations in a fuel cell,
by J. A. Davis and E. M. Gelbard. Westlnghouse
Electric Corporation. Bettia Atomic Power Labor-
atory. Pittsburgh. Pa. Apr 60. Contract AT-
ll-l-CKN-14
ph$3.30
An accurate control rod
Palmer a
byM.K.
15p. Order from LC. Ml $2.40,
WAPD-T-1165
ition indicator si
jystem,
H, A. Morewltz. West-
Inghouse Electric Corporatlcm, Bettia Atomic
Fower Laboratory. Pittsburgh. Pi. May 60.
Contract AT-U-1-(3EN-14. 15p.
LC. Mi $2. 40. ph$3.30.
Order from
WAPD-T-1191
Dimeoaional Insttection (rf Irradiated PWR core 1
bUnket fuel, by L. D. Larson. Westlngfaouie
Electric Corporation, Bettis Atomic Power
Laboratory, Pittsburgh. Pa. Dec 60. Contract
AT-11-l-GENf-U. 17p. Order from OTS.
50 cents. WAPD-TW-262
17p. Order from LC.
Mi $2.40. ph$3.30.
WCAP-1161
poration. Atof^lc Power Deparmtnet. Pittaburgh.
Pa. Apr 59. Contract AT(30-1)- 2176. T^ak L
Carollnas Virginia nuclear power associates. Inc.
CJ^^l yoJ^ct. Monthly progress report for~
Noveinber 1959. Westlnghouse Electric Corpnr..
tion , Atomic Power Department, Pittsburgh.
Pa. 1959. 29p. Order from LC. Mi $2.70.
ph$4.80. WCAP-1354
Carollnas Virginia nuclear power associates, inc..
jJVmt PrQlect. Monthly progress report for
becember 1959. Westlnghouse Electric rnrprvr..
tion. Atomic Power Department, Pittaburgh.
P». 1959. 28p. Order fromLC. Mi $2.70.
I*f*.80. WCAP-4002
Nuclear materials control system , -
"Eiqierlmental confirmation of the
Ftiase
^^ - . ... ""^^^
of die variable loading teat reactor concept, by
J. A. Vreeland. Westlnghouse Electric Corport-
tion. Atomic Power Department. Pittsburgh, Pa.
Dec 59. Contract AT(30-1)-2176. 44p. Order
fromLC. Ml $3.30. ph $7.80. WCAP-6O40
Nuclear materials control system (NMCS). Phase
II. A nftethod for the non-destructive analysis
^ ^^1 reactor fuel elementa. by B. lennings.
Westlnghouse Electric (Corporation. Atomic
Power Department, Pittsburgh, Pa. July 60.
Contract AT(30-1)-2176. 41p. Order from LC.
Ml $3. 30. ph $7. 80. WCAP-6044
Technology — Raw Materials
Further evaluation of amines as extractants for
uranium from sulfate liquors.
Oak Ridge National Ubora-
_ _ _ -, . -J ... D. Arnold
and D. J. Crouse.
lory. Oak Ridge, Tenn. [nd]. Contract W-7405-
eng-26. 43p. Order from OTS. $1.00.
ORNL-3a30
Waste Disposol and Processing
Quarterly procreas report research and develop-
ment activities fixation of radioactive residues
July - September, 1960. by 1). W. Pearce. H
General Electric Company. Hanford Atomic
Products Operation. Richland. Waah. Oct 60.
Contract AT(45-1)-1350. 24p. Order fromOTS.
75 cents. ^ HW-67334
.'s/r- -sopj
6S0
jUilMt " (OBamark)
593
Elactroolcs Cancer.
Electric Co.,
N. Y. 558
jUtwrtKi Kinetlca, Inc .
I AM. Calif.
621
j^trrv'^ Metml* Reeearch
Corp., SomervUie, Maaa. S64
ttittt ail Semlcooductor
Lab., Ceaeral Electric Co..
%racuae. N. Y.
Mrlal Racoonalaaance
Uk., Wrlgtu Air
DilJH Olx, Wright -
rwtaraon AFB, Ohio
Aaro Sarvtce Corp. .
RiUadelphla, Pa.
Aare-Space Lalia., North
erican AviaUon Inc.,
Calif.
625
565
557
580
604
AarvMiKical Raaaarch Lab.
Raaaarch piv. ,
atteraon AFB, Cnii
wngiK nil
Mr«t« -General Corp. ,
Calil.
0 533
sn
SM
633
18
Air Crew Eoutpmnt Lab. ,
Naval Air Material Center.
fUladelphia. Pa.
Air Force Balllatlc Mlaalle
UlT. , Air Reaearcn amT
OtvelaoRieat Conunand.
CaUf.
Air Force Cambridge
Raaaarch Laba. ,
536
580
9«
sn
AlT Force Flight Teat
CoMr. Bdwardi AFB,
CalM. 561
Air Force Special Weapona
CMlar. Kirtland Al^
N. Max. 620
AlrRatfcictlonCo.. Inc.
Mimy HUl. N. ].
Ait IMtlbar Senrtca.
~ ■ O. C.
Alrhorae Inatnimenia Lab.,
Omt Parle. N. Y.
5(3
555
565
Alibarae Inatnimenta Lab.,
IMvUle. N. Y. 556
Allkarat Inatnimenta Lab.
N. Y.
Aitaaaarch Mf j. Co..
~ Aril.
Alabama Mytechmc Inai..
Auburn
566
366
StO
580
Ml
Ml
AaHrtcas Inac. tor Reaearch.
fktitattrgh. Pa
CoU.. Maaa.
LMathamatlca aad
ca Laba..Staa*ord
U., Calif.
537
538
5M
538
M7
994
9M
•M
994
994
594
594
*M
PB Number
153 646
153 399
153 732
153 653
153 873-2
154 296
153 886
153 613
153 743
150 522
171048
153 583
171 108
130 3X
171 489
154 758
154 968
155 002
153 489
194 811
154 748
1931K>6
153 591
171 527
153 551
153 659
171 509
153 888
171 504
171 508
153 616-1
153 616-2
153 825
153 826
153 2S8
153 497
153150
148 169
153 690
148 092
148 419
153139
153 144
153 688
153 689
193 MO
193 691
SOURCE INDEX
Source
Arctic Aeromadlcal Lab.
Ladd AFB, Alaaka
Argowa National Lab., Ul.
Ariaooa Sate U., Tempe
AriaooB U., Tucaon
Arkaaaaa U., Fayetteville
Armed Force* -NRC
Vialoa Committee,
Waahln^oa, D. C.
Armed Service* Technical
Information Agency,
Arlin^on, Vt.
Armour Reaearch Fouo-
datloo, Ghlcaga, Ul.
544
545
627
54S
627
949
535
533
Army Ordnance Corpa ,
Waahingion, O. C.
561
566
611
612
Ml
Ml
Ml
Ml
581
581
Army Signal Reaearch aad
Oevdopmeat Lab. , Fort
N.J.
Army Snow ice and Fenna-
froai Reaearch Eatahliah-
metc. WUmette. Ul.
Army Tranaportatlon
Reaearch Command,
Fort Euatla, Va.
566
567
567
567
565
561
608
AvcoCorp., WUmln^oa,
Avco- Everett Reaearch
Lab.. Maaa.
620
621
558
60S
Balllactc Reaearch Laba.,
Aberdeen Proving Ground,
Md. 626
Bartol Reaearch Founda-
tion. Franklin Inai..
Svarthraore. fm. 615
BaneUe Memorial Inai.,
Columtaua. Ohio 567
610
622
626
626
Bauach and Lomb Optical
Co., Rocheaier. N. Y.
Bell Aeroayatema Co.,
Buffalo. N. Y.
Bell Telephoaa Laba., lac.
Murray Hill. N. J.
Beadlx Avlatioa Corp. ,
Oatrolt. Mich.
BlophyaiceLab.,
Stanford U.. Calif.
Btrmli^iamU. <Gl. Brit.)
Bolt BaiaiMiL and Newman,
Inc. CamtaridgB. Maaa.
558
605
'596
601
949
610
602
602
iCoU.,
Cheataui Hill. Maaa.
567
622
Brooke Army Medical Cas-
ter. Fort Sam Houacoa,
Tai.
I-l
943
943
FB Number
153 374
153 370
153 839
153 233
153 839
153 827
153 755
171 518
171554
147 498
171 524
153 565
154 756
154 757
171 480
171 481
171 482
171 483
153 250
153 247
153 248
153 249
153 5M
171 514
153 416
153 430
153 916
153 »9
153 568
153 649
150 696
193 753
154 749
153 823
153 199
171 911
153 920
152 M7
153 831
154 806
152 961
153 298
153 739
153 794
153 822
193 •»
193 406
193 406
Source
Brooke Army Medical Cen-
ter. Fort Sam Houaton.
Tex. (coo.)
py.
545
545
545
Brookhaven National Lab. ,
Upton. N. Y.
Brown (J., Frovideacc, R.I.
Brnwn U. Olv. of Applied
Mathematica, Providence,
R. I.
633
550
568
594
602
602
602
602
605
Brown U. CNv. of Engineer-
ing, Providence, R.I. 603
605
Bureau nf Mlnea,
BirtlesvUle, Okla.
Bureau of Minea,
Pinafaurgh, Pa.
Bureau of Naval Peraonnel.
Waahingion,. O. C.
Buma and Roe, Inc . ,
New York
California Inat. of Tech.,
CaUlontaU.. Berkeley
Callftiraia U.. Loa Anflelea
CarBagte Inat. of Tech.
Pittaburgh. H.
Caae laai. of Tkch.
Qeveland. Ohio
549
549
536
536
560
542
549
550
550
61h
555
558
568
601
620
626
6M
568
568
604
613
614
623
631
636
6a
Centre de F1iyai<|ue
Eleccronique ei
Corpuaculaire (France)
Chemical Eiwineering Lab. .
Princeton U., N. J.
Cbeaapeakc Bay Inat., Joim
HopklnaU., Baltimora.Md
Chlcan Midway Laba.,
U. oTchicagD, Ul.
Chicago U.. Ul.
568
569
Clevlte Reaearch Ceacar.
aeveland. Ghio
Clifton Corp. ,
Waahii^coa, 0. C.
Coaaial Studiea Inat.,
Loulaiana Suta U.,
Baton Rouge
CoioradoU., Bouldar
CoiunWaU.. New York
CobuaMa U. School of
Bnglneerln^ New York
550
608
590
534
595
598
569
536
554
623
565
995
619
569
153191
153 640
153 641
153 872
154 109
153 599
153 600
147 402
148 811
14n812
1.53142
1.53 737
148 346
153 644
171 52B
153 687
153 561
153 604
153 931
194 099
153 051
153 448
153 764
153 032
153 745
153 566
149 090
154 422
149 089
153 729
154 423
153 776
171 498
153 749
154 867
153 742
153 768
147 74B
193 876
171909
153 809
148 656
171912
-149 891
171 9a6
153 492
153 664
153 669
154 941
14(999
193 799
190 701
147 946
147 947
193 149
193 796
Souro
ColumMa U- School of
ri^Miil1.riiii Yiiii
(Cm.)
Comrola for Radlatkm, liz
Cambridge, Maaa.
Cook fteaearch Laba.,
MDrron Gr<7ve, (11.
ComeLl AaronauUcaJ Lab<
lac. . BuMalo, N. Y.
CotmUU.. Ittaca. N. Y
CoraaU U. Madtcal
CoU.. New York
CorwU U. School o«
Electrical BoxtaaerliiL
N. Y.
Courtaay aadCo.,
PhiladrtpMa. Fa.
Crucible SMd Co. of
America, Midland, Pa.
CnraialJoarartiy Lab. ,
U. ornnatairgK Pa.
Curtlsa-Wright Corp.,
Sanu Barbara, Calif.
Oartmouth Coll.,
Hanover, N. H.
Oavid Samoff Reaearch
Center, Prlncetoo, N.J.
Oavfc) Taylor Model Baain
Waahlagton. O. C.
Oaytoo U. Reaearch Inai.
Oaytoc
dliio
Defenae Atomic Support
Agency, Waahlngtoa, 0. C
Oefenae Metala Informatic a
Center, Battelle Mernorl^
loat., Cotumbua, Ohio
Digital
U. of Ullnola, Ur
Dikewood Corp. ,
Albuquerque, N. Mex. 539
Directorate at Reaearch
Aaalraia, HoUoiMaa AI%,
N. Man.
Dougtaa Aircraft Co. , !■
Santa Monica, Calif.
Duke U. Medical Center.
Durham. N. C.
OHriMiiiLab., raleU.,
New Haven, Cooa.
Dualap and Aaaoclatea. la^.,
StamlDrd, Conn.
Dynamic Aaalyaia Coatrol
Lab., Maaa. teat, of Ti
Cambrldr 535
OyMmlc Stmulatlcna Lab.
Ordnance Tank-Automotfrc
Comniaad. Camer Line,
595
571
Educadoaal Teatlng SarvU e,
N. J. ^
EUal-McCuUoi^ lac.
SaaCarloa. CaUf.
M!
595
617
617
617
636
605
60S
540
569
546
r* Number
153 665
154 428
154 429
154 430
154 966
1.53 125
153 463
153 080
153 830
154 803
tMm W>*i«*T
569
154 420
561
171 510
610
171 546
546
153 490
626
154 095
557
133 «2
570
570
153 268
153 818
595
603
603
608
154 768
154 765
154 766
154 767
635
171 544
541
154 402
610
610
610
610
612
613
614
161 231
161 232
161 234
161 235
151 102
151 099
151 084
570
S9S
152 915
153 415
150 904
581
581
1S3 825
153 826
M2
154 970
539
152 837
570
171 542
571
153 758
153 202
153 562
147 363
171 492
Electrical Engineering
aearch Ltb. U. of fa
Auatln
Re-
Electronic Syatama Lak. ,
Maaa. Inat. of Tech. ,
Cambridge
Electronica Reaearch Lab. ,
U. ct California, Berkeley
Engineering Div. Air Mater-
iel Command, Wrlgla-
Paneraon AFB, Ohio
Engineering Reaearch
Aaaoclatea, lac. , St. Paul,
Minn.
Federal Aviation Aoency,
AUaatlc City, N. ].
5.59
622
571
571
i95
631
612
571
561
561
Pela Group Dynamica Center,
U. of Delaware, Newark
Pettman Reaearch Laba. ,
Ptcatlnny Aracaal, Dover,
N. J.
539
582
582
Plight Accenaorlea Lab. ,
Wright Air Development
Dfv. , Wright -Paneraon
AFB. Ohio
562
Florida U. Engineering and
Induatrial Ej^rlment Station.
GalneavUle
Fraaklla Inat. ,
PMladelpMa, Pa.
Franklin Inat. Laba. (or Re-
aearch and Devalopn
PhUadelpMa, Pa.
Pretiank Co. . Qendale, Calif.
Free U. of Berlin
(Weat Germany)
Prick Chaimcal Lab. ,
Prtacetoa U. , N. ].
Ptilmer Reaearch Inat. , Ltd.
(a. Brit.).
Gatea and Crellln Laba. of
Chemlatry, Calif. Inat. of
Tech. . Paaadena
General Electric Co. ,
Schenectady, N. Y.
General Electric Reaearch
Lab.. Sctenectady. N.Y.
GMieral l«Ua. Inc. .
Mbin.
550
612
587
627
582
582
5S2
631
550
606
550
551
551
587
General Telephone and
Electronica Laba. , Inc.
■ayalda. N. Y.
Georgia Inat. of Tech.
En^neering Experiment
AiTai
Station. Atlanta
590
Ougfenhelm let Propulalon
Center, Calif, biat. of Tech. ,
Paaadena. Calif. 623
Harvard CoU. Obeervatory.
Cainbrldfi. Maaa.
Harvard U. , Candn-ld^e,
Harvard U. DIv. of Engineer-
ing and Afiplled Phyalca,
Cambrldae, Maaa.
1-2
534
596
624
660
153 081
154 843
153 937
153 998
153 313
153 488
154 759
1S4 747
171 506
171 506
171 545
153 627
153 857
171 552
152 403
171 045
155 001
171 543
153 614-1
153 614-2
153 615
153 311
154 109
152 895
153 445
152 IQB
133 812
148 011
619
627
627
171 523
153 819
153 873-1
622
627
171 513
154 097
571
627
153 431
153 682
154 751
148 936
153 285
152 370
153 154
171 9S1
Source
Harvey Aluminum, Inc.
Torrance, Calif.
Hazeitlne Electronica Corp. ,
Utde Neck. N. Y.
Hebrew U. (larael)
High- Energy Phyalca Lab. ,
Stanford U. , Calif.
Horizona, Inc. ,
Cleveland, Ohio
Hughea Aircraft Ca ,
Culver City, Calif.
Human Reaourcea Reaearch
George Waahlnl
ahlnyon, D. C.
Office, George Washington
U. , Waah- - '" ''
Hydel, Inc.,
Waltham. Maaa.
Hydrodynamlca Lab. . Calif,
bat. of Tech. . Paaadena
nilnola Inat. of Tech. ,
Chicago, Ul.
nilnoU U. . Urbana
nilaota U. Pnflnaerlng
Experiment Station, Urbana
Inverlal CoU. of Science
and Tech. , London
(Q. Brit.)
Indiana Sieel and Wire Co. ,
Inc., Muncle
Indlaaa U. , Bloomlngton
Indiana U. School of Medicine,
ladlaBapoiia
Inatltute (or Advanced Study,
Prlncalon, N. ].
Um
FLttliii
562
171 529
572
154 418
551
1714*7
616
618
619
148 IH
1M1S4
147 ass
589
171 520
551
171 322
537
153 288
637
147 7M
608
154 74}
596
153 l«
551
585
596
616
627
628
628
152 884
171 S7»
153 I3B
149 313
153 811
153138
153 772
552
628
153 08
171 US
Inatltute (or Reaearch In
Social Science, U. of North
Carolina, Ch^iel HiU
faiatitute of Bngtnaeiing Re-
aearch, U. ci California,
Berkeley
Inatltute of Geodea^ Photo-
grammetrv and Carto-
graphy, Onio State U.
Reaearch Foundation.
Columbus
555
612
554
544
596
540
603
606
609
557
'm"*-"* of Mathematical
Sdancea. New York U. .N. Y. 572
631
Inatltute of Oottca, U. of
Rocheater. N. Y.
628
Inatltute of Polymer Reaearch,
Polytechnic (net. of
Brooklyn. N. Y. 547
Inatltute of Statladca, U.
of North Carolina, Chapel
"^ ?s
596
596
597
iMUtuie of Tech. . U. of
Mlnneaota. Mlnneapotla
597
632
bietitute of Theoretical Aatro-
phyalca. U. of OBla(Norway) 632
faHtltute of Thaoratlcal
Phyalca. Stanford U.,Callf. 616
' 632
632
632
153 9W
154 419
149 SI
153 401
153 678
147 767
153 767
153 III
ISO 510
154 118
132 7M
lS0 94i
153 670
148 7«
153 8S1
153 SB
153 8»
153 810
153 04
153 to
153679
152*86
153 lO
iMIg
153 lit
153181
» of Tranaportatlon
Ml Traffic Engineering,
U. «f California. Berkeley 562
^mtmafi\r Weather, Inc.,
IrilLiteClty. Uah 559
iMHpkva Reaearch Lab. ,
hMMjrtvanla State U. ,
IWvaratty Park 559
loaa State U. of Science and
Tech., Amaa 597
taduto di Fiaica Superlore,
Ualvcraltl dl Pavla (Italy) 552
Jiaas Forrestal Reaearch
Ca«er, Princeton, N.J. 586
Mb CarroU U. ,
^evelaad, Ohio 572
Mm Hopklna U. SchocJ of
bvlaeerlng. Baltimore, Md. 572
Laboratory for Inaulatlon Re-
aearch. Maaa. Inat. of Tech. ,
Canbridge
Uaanai Geological Obaer-
vatury. Paliaadea. N.Y.
Laiglay Porter Ncuro-
paycUatrlc Inat. , San Fran-
ctaco; CalU.
U. , Belgium
U. (France)
■b. , Maaa. Inat.
of Tach. . Lexington
Uole, Arthur D. . Inc. ,
Canbrldge. Maaa.
I nckhewl Aircraft Corp.
Suanyvalc. Calif.
Louisiana State U. . Baton
Rouge
Loaall Technolocical Inat.
rch Foundation, Maaa.
Lvmaa Lab. of Phyalca.
Harvard U., Cambridge,
McCraw-HiU Book Co. . Inc. .
Na« York
MaUlnckroA Chemical Lab. .
Harvard U. .Cainbrldge.
572
628
537
558
539
597
608
544
559
573
573
597
597
598
601
601
610
621
622
629
629
559
573
590
552
604
609
613
632
539
573
624
589
624
Marina Phyalcal Lab. ,Scrippa
laMhuUon of Oceanography,
San Diego, Calif.
Mvylaad U. , College Park
573
573
554
633
•fcaaachuaeaa Inat. of Tech. ,
Caotoidfe
547
552
583
598
598
633
634
M6
** f\ltll>f
171 507
153 635
147 532
153 668
150 063
154 104
153 775
154 483
152 128
153 741
153 076
153 075
147 561
153 307
154 767
150 607
153 698
152 970
153 803
152 956
153 0B2
152 128
153 108
153 485
153 701
153 700
153 804
153 563
153 699
153 586
153 246
171 515
171 534
153 502
171 502
171 521
171 533
153 760
153 821
153 237
171 494
154 113
154 545
154 546
153 735
153 m
152 877
153 769
153 660
153 675
153 676
154 967
154 432
153 681
'OT'tfBtCT SfiKfif
Maaaachuaetu U. , Amheret 599
624
Materials Reaearch Lab. ,
Waiertovn Araenal, Maaa. 624
NWaba, Inc, Palo Alto, Calif. 573
MeUoa iMt. . Plttaburgh, Pa. 552
604
Inc.
Macal Hydrldea
Beverley,
Metala and Ceramics Lab.
Wright Air Development
Dlv. , Wrighi-Panersan
AFB, Ohio
Metala Reaearch Lab. ,
Broan U. , Providence, R. I.
Metala Reaearch Lab. ,
Carnegie Inat. of Tech. ,
Plttaburgh, Pa.
Michigan State U. ,
Eaat Lanalng
Michigan U. , Ann Arbor
553
614
614
629
604
598
539
609
Michigan U. Coll. of
Literature, Science,
Arte, Ann Arbor
and the
552
598
SM
598
Michigan U. Reaearch Inat. ,
Ann Arbor 616
Microwave Lab. , Stanford
U,, Calif. S74
Microwave Phyalca Lab. ,
Sylvanla Electric Producta,
Inc., Mountain View, Calif. S74
Microwave Reaearch Inat. ,
Polytechnic Inat. of Brooklyn,
N. Y. 574
574
574
575
S79
S99
Minneapolia - Honeywell
RepUator Co. , Hopklna,
Minn.
Mlnneaota U., Minneapolia
Mlnneaoia U. School of
Phyalca, Minneapolis
Moore School of Electrical
Eaglaaerlng, U. of Penn -
syivania. Philadelphia
Motorola. Inc..
Scottadale, Ariz.
Narrlca Corp. ,
PhUadelphia, Pa.
National Bureau of Standarda.
Boulder, Colo.
National Bureau of Standarda,
Waahlnyon, D. C.
NaUonal ReaMrch CouncU,
Waahington, D. C.
National Reaearch Laba. ,
Ottawa (Canada)
i-»
583
581
589
593
599
599
999
614
534
575
575
601
tOI
575
S9S
635
635
635
636
590
5r
559
586
606
609
611
153 628
150 657
150 088
150 894
153 549
153 749
171 489
171 487
171 488
148 559
153 856
153 669
154 866
149 782
152 612
153 200
153 266
153 267
148 215
153 503
150 898
150 897
153 663
153 677
153 234
153 598
1S3S54
153 932
154 769
153 826
171 556
153 646
147 176
153 133
153 771
154 818
153'
171 549
171 557
171 548
171 555
153 595
171486
161 581
161 sr
161 588
161 580
171 541
153 763
154 066
154 067
153 475
154 339
154 340
Naval Civil Engineering Lab. ,
Port Hueneroa, Calif.
Naval Engineering Experiment
Station, AnnapaUs, Md.
565
615
Naval MlaaUe and Aatro-
nautlca Center, Point Mugu,
CaUf.
Naval Ordnance Lab. ,
Corona, Calif.
Naval Ordnance Lab.
WMteOak, Md.
Naval Ordnance Teat Station,
CMna Lake. Calif.
Naval Radiological Defenae
Ijt. . San Frandaco. Calif.
Naval Reaearch Lab.
Waahington, D. C.
576
601
553
576
620
629
634
583
586
625
634
585
589
542
562
576
590
591
591
617
617
639
Supe:
of Ti
Naval Supply Reaearch and
Development Facility,
Bayonne, N. ].
Naval Weapona Lab. ,
Dahlgren, Va.
Naval Weapona Plant,
Waahington, D. C.
593
583
611
611
New York Medical Coll.
Nwr York State CoU. of
Oeramlca, Alfrad U.
New York U. . N. Y.
591
N.Y. 546
591
540
553
New York U. C^cU. of
Engineering, N. Y.
Nlchda Chemlatry Lab. ,
New YorkU.. N.Y.
North American Aviation, Inc. ,
Downey, Calif.
North Carolina State Coll. ,
Raleigh
Northweatem Technoioglca]
Inat. , Evanaton, Ql.
Noire Dame U. , bid.
Noyea Chemical
ofUUnola, Ur
560
■555
599
638
Nuclear Development Corp.
of America, White Plalna,
N.Y.
Office of Oefenae Reaearch
and Engineering^
Waahii4ton.D. C.
547
624
600
f> Nmit)ff
m§if
154 746
154 809
544 153 355
153 294
150 073
154 813
154 771
154 812
154 770
154 722
153 4r
153 449
154 750
154 755
154 503
154 754
161 834
171 0S2
171 358
171 107
161 932
171 159
171 490
171 491
171 317
Inat. of Tech. . Cambridge 634 153 103
171 532
153 551
153 928-1
153 928-2
New Hanyahlre U. . Durham 534 153 878
New )eraey Ceramic Re-
aearch Station, Rutgers
State U. , New Brunawtck
150 899
153 152
171 550
153 000
150 895
560 153 643
153 567
154 808
599 153 672
148 200
141 19>
624 153 154
153 814
147 775
152 587
533 171 518
Office of Technical Servicea,
DcfX. of Commerce,
Waahinpon, D. C.
533
Ohio State U. . Columbua, Ohio 542
OrSS8-449
171 495
OWo Suta U. Rfetrch
Fw— tMlni. Columfaua
I Tmc ActlTity,
Yuma, Aiiz.
CMortU. (GL lilt.)
Parke Mghanwrtral Labi .
ioc. . CarUal*. Maaa
Pcnoairlnnta State U. .
Untvcraiiy Park
Penaavlvanla State U. Cell.
at ChenUatrv and PliyaK a,
Ualveraiiy rark
Puraf—a I Research Boar^
OWo State U. Reaearch
PouadMoa, Cotumbua
PtallUpa Pacrcteum Co. .
BardeavUle. OUa.
Physical Reaearch Lab. .
Space Tech. lac. , Loa
CaUl.
Phralcai Sciaacea Lab.
(MMBca Tairic-Auto-
— alu Co— nand, Ceatei ■
Phyalca Reeearch
U. o<l
nunala. U
Pttman-Ouiai Labe. Graq ,
Praakfcrd Araeaal, ?haf-
delpMa, Pa.
Ptoaburgh U. , Pa.
PliilK. E. a.Aaeociacei
lac; , Lob Anyelea. Calil .
PolyiaetaBlc Isat. al BrooU m.
N. Y. '
PonUflda Unlveraidade
Catotica. Rio de Janeiro
draxll)
Prtncetoo U. , N. J.
PropdatOB Lab. . WrijM Air
Oevelapinent Olv. , Wrlgli :
Paneraon AFB, OMo | S92
Paycho- Acouatlc Lab. ,
Harvard U. , Cambrtdae.
621
Purdue Reaearch Founda-
tiOB, Lafayette, Ind.
Quarter maater Pleld
Evaioackai Agency,
Fort Lee. Va.
Quarter maater Research
aad Eagtneertac Center,
Natlck, Maaa.
Radtation Research Corp.
Weai Palm Beach, Fla.
Radio Corp. of America,
HarrlaoB. N. ].
Sam fSJitttba
544
560
629
630
637
5B8
SW
633
637
i47
S«9
633
553
537
537
537
540
592
636
583
618
562
S«4
613
618
633
600
604
604
604
606
606
607
607
607
576
563
563
588
619
638
537
538
593
SS5
593
617
576
152 865
150 896
154 807
153 603
153 875
171 525
154 7M
153 282
153 654
153 686
153 661
153 432
153 811
154 836
154 837
154 838
154 835
ISO 072
153 464
153 447
153 140
154 424
153 944
161 770
147 543
153 499
153 296
147 757
153 638
153 639
150 327
150 636
153 183
153 837
153 838
148 349
1S3107
149 354
149 355
149 155
154 417
150 469
154 969
147 765
153 855
153 854
153 491
153 427
153 628
154 753
154 544
SauGI Pfa
Radio Corp. oi America,
PrIacetoB. N. J. 577
Radio Obaervatory, Calif.
iMt. of Tech., OeaM Valley 534
534
535
535
535
535
535
535
Rav-O-Vac Co. . Madlaon,
tay-(
Wia
Ravtheoa Co. , Burltaffoa.
Ray
aytheoaCo.,
Walifaam. MMa
RCA OXeaae Electronic
Producta, Canxlen. N.].
RCA Serrlce Ca ,
Camden. N. J.
Reed ReeearciL lac.
WasMaycn, D. C.
Remlngion Rand Univac
Div. , Sperry Rand Corp.
PhUadelphia. Pa.
577
577
690
619
577
577
609
Reesarch toat. ,Tern|iie U. ,
PhUadelphia, Pa.
Reaearch Lab. of Electronlca,
N4aaa. Inal. of Tech. ,
Cambridge
Research Lab of Heat Trana-
fer in Electronic*, Maaa.
Inat. cf Tech. , Can^rldge
RIAS. Baltimore. Md.
635
544
578
635
600
600
Richmond Ressarch Lab. ,
Stauffer Chemical Co. , Calif.
Robertahaw- Fulton Central*
Ca. Anaheim. Calif.
546
5*4
584
Rock laland Araenal Lab. , 01. 584
Rocketdyne, Canoaa Park,
Calif.
Rome Air Oevelapmeni Cen-
ter, Grtftlaa AFB, N. V.
Sarah Mellan Scalfe
Radtation LA. ,U. at
Pltiaburgh. Pa.
School of Aviation Medicine,
Brooke AFB, Tex.
Science aad Tech. Olv.
Library of Ccocreaa,
WMMnyon. D. C.
Slndet S. p. A. ,
Rome (Italy)
Small Croupe Reaearch Cen-
ter, Waahinaon U. ,
St. Louu. Mo.
580
584
619
630
637
542
542
543
543
620
622
540
540
Smith Coll. .
Northampton, Maaa. 538
Southern Meihodial U. .
DaUaa, Tex. 633
Space Sclencee Lab. , General
Electric Co. , Philadelphia, Pa.609
Sperling Labe. , Arllnpcn, Va. 541
1-4
153 602
147 323
147 334
147 323
147 S2S
147 326
147 327
147 338
147 329
153 935
153 230
159 238
171 493
154 516
154 844
154 431
639 153 160
tro^, N. Y.
553
171 535
607
153 262
154 842
150 607
154 190
171 484
153 413
153 710
152 rs
153 617-1
153 617-2
171 111
153 613
153 612
153 858
153 264
153 n
618 154 817
153 402
154 426
153 583
154 819
171 577
153 807
147 767
147 768
153 !50
171 485
153 835
152 902
SfiUEEf
Sparry Microsave Elac-
tronlce Co. , Clsar«ater,
Fla.
Stanford Electronlca Labe.,
Stanford U. , CaUf.
Stanford Reeearch loat.
Menlo Park, Calif.
Stanford U., Calif.
Suwiord U. School of
Madlclae, Calif.
«. of Tech.,
Hoboken, N. J.
Synthetic Mica Co. ,
Caldwell, N. ].
Syracuae U. . N. Y.
ma Corp. d A
Angelee, Calif.
Syateme Corp. d America,
Loa
Syateme Development Corp.
Dayton, Ohio
Syateme Techooiofy, Inc.,
biflewood, Calif.
Techniache Hochachule,
Craz (Auatrla)
Techniache HcclMChuie,
Vienna (Auatrla)
Telephonic* Corp. ,
Huntiagian. N. Y.
Tesaa laalrumenta. Inc.
DaUaa
U. . Auatln
Textile Reeearch Inat. ,
Princeton, N. ].
Theoreucal Chemlatry Lab. ,
U. of Wiaconain, Madlaon
Tranaportatlon Center, North-
irestern U. , Evaaaton, Ul.
Traveler* Life Inaurance Co.
Hartford. Conn.
Ultrasonic Testing aad Re-
search Lab. , Paramouat,
Calif.
United Aircraft Corp. ,
Eaai Hartford, Conn.
Unlveraal-Cydope Steel
Corp. ,BrldgevUle, Pa.
Univeraliy of Southern
California, Loa Angelea
Univeralty of Southern
California, Engineering
Center, Los Angeles
Utah U. , Sail Lake City
Vertol Aircraft Corp. ,
Morton, Pa.
ftm
578 154 I
578
602
622
623
596
578
579
591
565
543
633
630
541
584
586-
637
563
593
546
579
560
620
548
554
588
556
586
564
613
548
554
554
607
630
564
564.
564
Waahinffon State U. , Pullman
WaaWayoa U. . St. Loula, Mo.
Waahiagton U. .Seanle
Waahington U. , Seattle. Div. of
Counaeling aad Teating
Servlcea
600
540
616
600
618
148 411
149 333
153 834
150 717
153 «a
153 308
153 097
154 848
147 548
148 931
153 934
154 515
153 123
171 491
171 553
154 753
171 SSI
153 389
152 848
153 276
579 153 228
153 933
147 8M
147 170
153114
153 606
153 5S0
171 499
154 504
153 592
150 520
153 667
171530
153 438
171 0«9
153 740
153 879-1
153 879-1
Vidya, lac.. Palo Alto, Calif. 608 152 SC
Virginia Agricultural Ex-
periment Station, Blackatwrg
153 7B
153 408
149 or
147 306
541 148 610
"SR
Staia Uj , Oairolt.
Pat PB HuiBbeT
600 153 177
625 153 123
625 153 757
Sourcs
Weatem OKarlo U.
(CMada)
' Foracaatlng
rcfaCeatsr,
a«(CMcago,ai.
556
153 443
Weatlaghouse Elsctric
Corp. . Blooa«eld, N. ].
Weetlnghouae Reaearch
Laba. , Plnaburgh, Pa.
f'tf
PB Number
ta4
193 6r
615
154 542
619
190 502
•> '-tJ-
■•5i^,^
SeoEt
willow Run Laba. U. at
MlchlgBa,Ana Aibor
Wiaconain U. . MadlaiB
Wright Inatrumeau lac. ,
Vestal, N. Y.
Yate U. . New Haren,<::onn.
Itm PBNviBt>fT
625
153 496
596 153 608
579 153 243
579 153 244
557
547
601
154 7«2
147 528
153 671
'5. .
$-
bS
AMf y matnlsla
Acer leronteter*
-- Applies iiooa
--Maierul*
--SaaalQvlty
AaiiaJ cmmeraa
- -Develo|iaieat
A«lal rvcoanalasance
-A/taual tictora
Awuliriniiuc hwrtng
- -Commnneaaurea
--Theory
--Ttemal •fleet*
AaroaoU
--AbaorpooQ
Aarocte rmodiemiauy
AftsrskNi
Alrloraa
Air traSlc cxntrol syaiem i
--Bqulpmeni
ering
AlT (raffle controUera
- -Pel fui luanca
Alitraadunc combuaclon
Aircraft
--Dawcuoo
--MaxerUla
Aircraft equlpmam
--Daal^
Aircraft tlras
«0S
SM
M2
SU
S61
S61
sat
634
60S
606
m
630
590
622
633
S65
S66
561
561
590
565
610
560
563
Alrlotla
latica
60S
153 463
--Traoaaolc cteracvrlai
tca609
153 644
Alrframa
--MaMTlaU
S62
171529
Alrpiaaa ai^taB alia
--Storayt
392
154 969
Alryiaaaa
--Goatrol iratema
363
171 SSI
--Loagltudlttal itaMUty
963
171 331
AlxpoRB
--I l^lin ayatema
363
171 307
AH**
--Fbyalcal etkcta
954
133 733
AJgebra
SH
133 664
--Appllcatloaa
S74
153 663
--Theory
9M
153 678
AftaU metal hallde cryatal
1
- - Uanlneacance
623
133 670
ABcaU metal laUdee
--Spectra
332
132 612
"»>■ luli.nl cal etiecta
Altoya
--Raae atudiee
--Temperature laoora
Altracor
Al
Ifrlctlaa
Itaiparantre tactora
•lloya
CaaHiig
* -XBiBparanire factoca
Ahaninum cryatala
--Orfomatioa
t kydrtdee
•l*jr
i-lzoaaUoya
346
621
610
MS
614
613
614
613
615
610
189
532
610
610
133 966
133 449
134 424
134 424
171 906
171 506
133 569
133 103
133 566
150 636
133 912
153 490
153 446
133 107
153 499
171 509
171 504
171 906
171 510
171 510
153 448
171 509
161 231
153 933
171 552
153 132
171 113
161 231
134 296
171 4M
154 S67
171 466
161 770
190 902
161 231
146 539
171 334
161 232
153 296
171 546
171 346
171 546
161231
1S9U1
171462
SUBJEa INDEX
S^>act
Amplitude raodulauoB
--Aaalyais
AN/DFN-31(XE-1)
AN/FPS-3
AN/GllC-27
AN/PPN-l3(XE-2)
Aaalync fuoctioas
- -Oetemunauoe
--Tteory
Aoiaocropy
Aonihilatloa reacQaaa
Anoxia
--Fbyaloloclcal
--Deaivi
- -DevekjptucQt
Aaihracene cryatala
- - Luroloeacence
Aathrapologlcal daa
Antlbodtae
--Adeorpuoo
--Ftayatologlcal etiecta
AatUerroelectrlcliy
Aatmbrtllatloii
Approximjte computation
--A|ipUcauoaa
--Brrora
--Theory
Arfoa
- -Aarodynamlc diaracier-
Utica
Aacroaomlcal cameraa
--Daalyi
Aatroaamlcal data
--Racortilii( devlcea
AunueiriHie
— AiMlyala
—Arctic refiona
— Atiaauatioa
--Optical propertlea
--Preeaure
--RadUdaa
--Raflactlve etiecta
- -StaUlity
--Turtulence
AOBoeptaeric retractlaa
--Theoretical correctiooe
AOBaapherlc aoundln;
- - laatnanentatloa
Atomic bomb ezploelons
-Hazarite
Ananlc apectra
— Aaal^
--ThKjry
AtODic atnicture
- - Mathematical analyaia
Atone
--Reaoaance
- -Scene riof
Atttnidae
- -Nychutoglcal fatxora
Audk> acceaaortca
Aunmata
Artatiaa atxidenta
--Aoalyala
- -Countenneaaurea
AvlatioD peraoonel
- -Aoihrapacnetry
--C3oiliing
--ftrfomaaca
622
572
577
577
575
StO
633
576
994
596
629
616
942
579
579
617
536
543
545
591
545
620
634
593
606
533
533
560
559
559
596
556
596
599
560
635
555
599
635
596
559
541
623
631
631
634
624
536
539
579
«01
'563
561
536
619
337
S3i
561
Avlatlaa aafety
Axlally aymmetrlc floa
--LainiJiar bouodary layer 606
Backward wave ampllflara
--Developmant S71
Ball UgbtalDf 621
Balllatlc data
--Racordiaf darloae 560
1-6
n Number
154 643
154 416
154 644
154 516
153 595
153 678
153 872
153 107
153 669
153 200
153 563
154 817
154 099
133 243
153 244
153 097
171 490
153 4B9
146 931
153 640
150 899
153 370
1S3 490
153 103
153 415
153 606
152 895
130 322
190 322
153 643
154 096
153 061
153 566
153 606
153 5619
153 639
150 896
161 568
153 745
154 096
171 544
153 399
147 532
154 4(U
150 701
147 748
190*46
153 237
150 OM
153 237
153 604
154 866
171 543
153 228
171 346
171 0S2
171 90S
133 469
171 493
153 835
153 834
171 SOS
153 118
1S3 936
153 916
154 966
Sublect
Benkii^
Barium titanaiaa
--Applications 562
--Dielectric propertiea 591
Barrier grid tube 566
969
Bayes nilea 996
554
-Caribbeen lalanda
- -Deformatlan
- -Sheer atreaaea
Bearloga
--Corroalon prevention 584
Bed- load tranaport dau 609
Beozeoea
--Fhotolyala Ml
Beryllium
--Caatlnf
- -Dele rmiiiat Ion
--Melting
Beryllium hydridee
- -Syntfaeela %
Betatrooa
--Oealgn
--Drvelopmeni
602
603
613
619
613
SS3
&
Bibliography
■ -Aluminum hydridee 55^
--Coolaata 53d
--Corroaian 615
- -High apeed caatara* 560
--Hydrofolla 609
--hitermealUc campauoda591
--Maintenance 533
--Microwave apactro-
acopy 624
-•Paydtoacouatica 621
--Radlauon 560
--Radio wavee 635
--Refractory maeenala 591
--Scientific reporta 620
--Underwater awlmmlng 620
Bteberfaacfa coajccture 994
Blng theorem 598
Blamuih
--Magnetic propertiea 602
Blamuih a lloya
--Electrical propertlee 567
--Thermal propertiea 967
Blamuih compounda
--Cryaul atructure 627
BUdcbody radiation 559
Blood
--PDlarographlc analyaia 543
Blood veeeela
--Fhotographic aaalyala 544
Blunt bodlea 606
607
Bodlaa of revolutiao
- -Heet tranafer 606
--Praaaure dtatrtbudoa 607
-RanectivaaOacu 606
Boiling
-Analyaia 633
Boltzmann equation 600
631
--Dlffuelon
Boron hydrldea
- -Spectra
Boundary layer
--Mathematical analyaia
630
SS2
607
--Superaooic character -
iatlca 604
Bragg-Cray 617
Brake Ualngn "^
-MaterifU 590
Breakwatera
-Dealgn 606
Bremaatrahiung
--OetenniiMtloa 534
Brick
- -Coetlngi 990
Brl^taeea
- -Determiaatlon 543
nu
148 IN
150 46*
154 424
150 899
- 153 809
148 696
153 840
153 735
148 812
154 766
171 HI
154 339
153 612
171 521
154 417
171 521
171 4B9
153 934
153 822
153 830
171 534
OT^SB-44t
171 501
154 966
171 902
154 846
171 518
154 113
- 147 766
150 896
161 S61
154 846
149 0*9
171 577
153 13*
153 6*9
153 267
149 333
153 753
153 751
154 097
153 0*1
ISSSU
153 401
150 636
1S310
150 636
153 1*3
153 475
154 9«
152 sn
153 311
153 609
152 613
153 262
153*3*
153 741
171490
154 7a
153 416
153 444
171 107
161 •34
?»m WNuDibar
theory
cbamber
-fkBtographic analyaia
.■Mocbemlcal eftecu
iBlobate
••Olalactric propertiea
OWMHors
—Develapnieni
■ Uatrriala
— laparauon
tMbiclaa
GMIina
--Corroalon
■ -Uacfeanlcal propertiea
QMkoia ray aedloecopea
"Ihai reaulta
CMbo# ray tube acreena
-ftaugraphy
Otedaa (Electron tubea)
"MaMriaU
OHCkgr problem
OKhiMalfokda
GnUoec
I of radlaQoo
: capacltora
"T6nperature tactora
OHiaiic materiala
--AfpUcatiooa
-•Machaalcal propertlee
--Hypertlne atructure
Qaifi tranafer
Oaalcal Impuritiea
--Oieimcai effects
- iehaat propertiea
I of radiation
I alloys
--vwelapnnent
CfenMlura-lron alloya
--DUfualon
Chromium plating
—Machaalcal properties
QntUtm atructurea
□laaB
-China
- -Japan
--Korea
OoHd chanibera
--hifcrmance
Goaidal cables
Cobalt
--DtSuBlon
Cobalt-molybdenum alloya
•tudiea
--Optical propertiea
■-laeonanoe
CaaMaatorUI analyaia
-Aaatysu
j-Chrtbbeaa tolanda
(^■■Malcatian systeme
— Oavekipmem
■ -StgnsI to nolae raUo
••Thaory
OMpactlflcatiaaa
OMptai Bumbera
■-Theory
Cm$kA vanablea
-AlpUcatioaa
-Tta.,
616
616
616
543
545
54S
591
622
572
565
966
615
615
601
637
622
597
59*
5*9
5*6
535
569
571
591
590
624
54*
612
63*
SSI
546
551
613
614
612
546
555
555
555
616
567
615
615
554
625
552
593
5*6
549
550
554
635
573
539
572
593
540
603
994
153 032
149 0*7
149 0*7
153 405
153 406
153 191
1SS641
190*99
153*20
152 12*
154 746
171 525
154*09
154*09
153 4*5
154 752
153*23
153 307
153 266
154 754
154 754
147 32*
154 541
171492
171 SSO
154 751
153 237
154 74*
171 049
171 503
152 **4
152 848
171 497
153 592
153 742
154 759
153 490
153 427
153 427
153 427
149 0*7
153 24*
154 542
154 542
153 667
153 123
153 757
150 063
153 646
154 104
171 52*
153 44*
149 321
161 567
154 545
190 904
154 4*3
153 266
153 646
153 0*0
153 200
154 765
154 766
153 139
153 6*9
CoDpreaaible flow
--Boundary lamr
Coacrate
--Coatinga
Coafamal mapptag
--Applicaaooa
--Theory
Coooectora (Electric)
--Dealgn
Oacrol aysKma
--Aaalyaia
--Dealgn
--Development
--Equipment
--Human engtoeerlng
- -Mathematical analyaia
- -Syntheaia
Control valvea
--Aaalyaia
--Simulation
Oinvaji bodlea
--Thetwy
Coolanta
--Bibliography
Copper
--Imemal frictioa
Capper cryaula
--Deformation
--Electrical propertiea
Corona (Electricity)
--Analyaia
Correction clrcuita
Correlation methoda
Corroaioo
- -Bibliography
?»m WNianhar
Corroelan lohittttors
- -Bttectlveiieaa
Carvua
Coaraic radiation
--tnienalty
Coamic radltiaa abowera
--Meaauremat ^
Crab -Nebula
Crack arrestora
Creep behavior
CryofBnlca
Cryatal o««aa
-DaaicB
Cryaul phoaphi>ra
- - niototxjnductl vlty
Oyatal atructure
• - Madiematica I analyaia
Cryatal video recelvera
Cryatala
- -Drtonnaiioa
--Mechaiucal propertiea
Culture medu
- -MaierUla
Cyclonea
--Theory
Cyckxroo tnagaeta
--Dealgn
Cylindera
--Aerodynamic character-
lauca
--Heat tranafer
CyliBdrlcal ahelU
--Deformation
--Load dlstribuQon
--Pressure distribution
--Stresses
Damping
— AnalyaU
--Eflactiveneaa
--Theory
Dame
Dark adapubon
- -Meaaurement
Daa
--Procesaing
Data auvafe ayateiiu
1-7
605
590
603
60S
567
5*4
5*5
581
601
571
535
56*
574
636
636
599
533
613
62*
62*
621
570
573
615
5*1
S»4
583
615
534
616
534
5*5
614
5*2
610
573
553
629
575
603
603
541
556
616
606
633
635
604
604
604
604
602
5*9
60*
565
542
561
601
639
153 125
171 107
154 766
194 765
153 24*
171 496
171 SS3
171 4*0
171 481
171 4*2
171 483
171 54*
153 75*
153 202
153 755
149 090
153 663
193 «n
154 966
154 966
14* 200
153 771
OTSSB-449
154 867
153 138
153 13*
153 916
171 542
154 546
171 501
IS* 757
171 HI
153 487
190 696
153*78
14* 215
147 323
171 576
171 4*7
153 614-1
153 614-2
161 231
153 246
150 895
153 932
150 894
171 531
171 531
153 122
153 SSO
149 315
153 118
171 485
171 484
147 757
153 502
147 757
153 502
153 794
171 556
153 416
147 546
161 834
171 510
154 422
153 160
Subtact ^aa
Data atorage ayatama (coo. )
--Orvelopntent 560
637
Data tranamlaalcn ayateme
--Coding 637
- -Oealgn S7S
--Brrara <V
DacarhonaUan StS
Decofupres s loa
- -Padiological afieca 542
Def ruiUag equipawat 566
Denalty aenaltlve indlcatora
--Deaign S57
Dental e<|uipmeiu
-Dealgn 544
Deotal reeearcfa 542
Oeacaling UO
Detectioo (RF)
-AaalyaU ttt
DeseciDia
--Clrcuita 576
--Mathematical analyau 969
--Rdiabillty 565
Detoaatlan wavea
-Energy 553
--Propagatioa SSO
Deuterium
- -Btanbardmeot 618
- -Therapy 546
Dialectrica
--Development 572
--Propertiea 626
--Temperature tactora 569
Dlaa
-Materiala 562
Dlflerenoe equBdana 597
632
Differential equatlaaa 601
--Appllcatloaa 603
6S1
--Theory 91?
Dttterentlal geumatiy
«SS
6a«
997
600
-Theory 59*
Oifterentiaung clrcuita
- -Developmeia 570
Diffuaioo
-Theory 614
Diocotroa
Dtodea
- -AppHcaUooB
--Daal^
- -Electrical properties
S71
569
570
625
627
579
--Theory
Dlpropargyl ether
-Toxic efHfcta 561
Duplay ayatema
--Development 571
--Miliury requiretnenu 535
Documenutlon 639
Domain criteria 627
Doppler tracking ayatema
- -Development 565
Drag
- -Meaaurement 559
Ear prolBctora
--Dealgn 619
Earcuahloaa 619
Early warning radar
ayatema
-ReliablUty 577
Ecommic conditlona
- -Chile 5*7
- -Mathematical aaalyaia 638
Elaatiaty
- -Mathematical analyaia 602
-Theory 602
Electric batterlea
- -Oevelopnient 54*
Electric fluida
--Fhyalcal factora 631
Electric Inaulatora
--Electromagnetic pro-
pertiea 568
Electrical etgulpment
- -CooUi« 533
154 75*
147 756
153 654
153*03
153 654
154 746
154 426
171 SO*
171 SO*
154 762
152 865
154 426
161 235
154*43
153 294
153 736
171 509
154*13
199 44*
14* 154
153 152
152 128
153 649
154 541
171 529
153 660
153 679
153 671
153 739
153 679
153 668
153 660
153 672
153 432
153 876
153 660
153 413
152*2*
171 542
153 742
153 93*
153 736
153 26*
153 873-2
153 873-1
153 r6
152 902
153 758
153 755
153 160
171 543
171 509
153 5*6
171 493
171 493
154 844
153 763
153 691
153 739
153 794
199 002
147 74*
153 776
OTCSB-449
Btecoical equ|
CAlrborne)
tKt iri
•ply
theor
BlactroaMfBetic
- -MMfeHBaOcai ana
Btoctroaacnetic w
--OMBCUoa
- -Traoamiasiaa
Blactna accalcraion
--Dm1|
BtectrM
analyala
-MSfBMlC fK«on
-Producaan
S«0
S7(
S7S
S7«
am
ttS
S49
548
632
539
544
544
Blactroa
ciftg— I
r-Arvur* I
Blactroa capture ,
■tical aaa^yaia
leal anaiyala
- -Wave tnnaml— 1<^
Btoctroa guaa
- -AgpUcaQona
--Propeniea
Blactraa nitea
--Aaalyaia
yaU 632
576
5«8
S7S
«S3
631
S74
571
631
MS
tu
619
618
579
636
--lUUaMlUT
•-Ttaofmruur* fM:i^ra
BlectTooic drculis
- -AoalyaU
Bloctrootc aqulinwnt
--CooUi^
BtKtraaics
BlectTona
-DMstty
"BlBctncal eOMn
- -Baargy
- -MafMtlc moaienu i
--Ktaclaar raactkna
--Vclocllir
Blectroatatic BMerat^
B^attaaa of aiaM
Brrors
BauartM
* -Hyidro(ra|Ay
BllMIIOl
- -Molecular atnicti^
Ediylene polymer*
-■Efiecta of raduci($i
--Optical properuea
Evaporators
-Scale
But taziwaye
Expellani beana
ExpanmeMal dam
--Aaalyala
-Spactrograpiilc an i
"Apptlcaliana
Bxtraaerraatrlal radh
--Sourcea
By*
-teaaltlTUy
V7
sn
sn
569
571
576
533
578
622
621
622
618
579
618
623
582
SM
SM
623
617
624
565
9*1
5M
S3
549
lyala 382
sn
S74
535
9*1
962
153 933
14*411
IS3 234
153 107
155 002
190 S02
153 827
155 002
1S3 679
147 561
1S0 607
150 607
1^679
153 294
171 498
171557
133 934
153 732
153 503
153 937
153 488
171 521
141 154
171 523
147 543
153 276
153 464
133 830
153 830
190 717
133 230
153 431
171 492
154 420
171 492
193 294
OTS 98-449
154 190
147 532
133 824
133 741
153 807
154 817
153 276
147 306
130 717
153 677
153 114
133 415
149*91
IV701
171 490
150 657
154 746
171 507
150 320
153 668
154 769
153 687
153 857
154 4*3
153 677
147 322
147 326
147 32*
171 506
161 834
3>*)act
F-104C
Pacalnule tranamtaalon
- - B<|ulpa>eat
Factor aaalyala
--Theory
Ferrliea
- -Appticadooa
--Ckemlcal propertlea
- - Mlcroacructure
Ferroeleccrtc cryatala
--Croarth
FazTOOMi^Mtlc fllma
--Ikyalcal propertlaa
--Froparnae
Ferromagnetic maiertala
--Appllcanona
MagiMinr properttea
--nyalcal propeniea
Feyamaa pacfa iuafrala
FIbera
--Molecular atructurc
--Riyalcal propertlea
--X-ray aaalyala
Fire eztlaguiahlag agenu
- -Materula
Flame velocitiae
--Maaaurement
Fhunaa
-Dtfiualoa
--iaklMtioa
Flatcker'a Ice laUod
FU^tpadw
--Madanaiical aaalyala
Fllfhl almulators
--Oevclopmeai
Fhildno*
--Heat craoaler
--Mathema tical aaalyala
•SiataiUty
- -9traaaaa
--'naory
-Velocity
Fluid ■artaaica
Fhioreacent dyea
- ' Appticadoaa
Fluor Idea
--Heat o< fonnaUoa
Fluorine
--Oieiiiical reactiooa
Fhiorocarboaa
--Syndieala
Fluoroacopaa
--Applicailooa
Fluoroailicanes
--Mlcrawave apectra
--Molacular atructure
Flutter
--Taac medioda
Prae radicala
--Electroa traaaitiana
--Hyperflne structure
--Spectra
- -Scabilixation
Frequency mulliplters
--Deaign
Frlctloa brakaa
- -Maienala
Fuel caoka
--Teat reaulta
PuBctlooal aaalyala
Funcooaa
--rntW^
--Oecermloatloa
--Theory
561
570
sa
' MO
57*
630
626
591
629
601
621
621
576
627
626
633
593
589
593
562
9*2
390
3*2
557
562
to*
607
609
«0t
MO
9*8
390
590
990
5*3
624
624
MS
549
547
547
592
574
910
9M
601
997
393
596
9*7
Fuagl
--Culture 941
Fuzes
-Teat medaoda 9*3
Calaxlaa
- -Spectrographlc aaalyala 535
Camea theory 919
--AppllcatloD*
Gamma metera
- -Oevelopoieat
radiatloa
979
*17
617
153 591
153 818
154 836
14*610
193132
154 806
153 238
154 095
150 899
133 563
150 073
153 700
14* 349
154 771
171 543
154 095
153 282
153 3*9
171 520
153 389
171 532
153 769
153 764
171 532
153 482
171 0&2
134 806
134 967
153 749
153 837
149 782
153 749
'149 089
153 835
154 104
153 401
153 445
153 764
152 403
153 447
153 154
153 134
132 «*7
152 961
153 814
153 814
130 072
150 898
134 751
133 879-1
133 879-2
153 671
153 052
133 806
153 135
192 936
133 122
153 447
147 327
147 547
171 555
171 349
154 812
154 428
154 429
154 430
171 491
8i*)eet
Gaa baarlnCB
- -Ferformaaoe
--Theory
Gaa dtadiarpta
--Temperature
Gaa flow
--Mathematical aaalyala
Gaa generating aystema
--Pamei supplies
Gaa loauatlan
-Electrical eftecu
--Magnetic factora
-Temperature factors
Gaa leaka
--Dsnctlon
Caadynamica
Caoea
-Adoorptlon
-Detooaaoo
--Blactroa tranaltlana
--'ieat tranafer
- -Molecular structure
-Tempersture
--lliermal properties
--Thermodynamic pro-
pertlaa
(lyala
Gelger counters
- -Statlatlcal aai
Geodetic data
--Collecting methoda
--DMarmlnattoo
Geofropliy
--Caribbean lalanda
Cm— eiilc genua
Oaopbyalcal surreyiog
- - loatnaneatatloe
GerflMiiluDi
• -Magnetic effecu
Glaaa
--Adaorptlve propcrtlaa
--Oeveloproani
Glyclaaa
--Riyalologlcal aflecte
Cold
--Gryetal atructurc
--Daiarmaaan
--Heat treatment
Goubau line
Gravity
--Oeterml nation
Greoadloea
Gngnard reactlona
--Analysis
Gngnard reagenta
--Chemical reacriona
Group dynomica
--Payrbolngiral eflacu
- -Suttatical anaiyala
--Thaory
Group (Mathematlca)
-Thaory
Cruneky inequalltiea
Hsil
--Radaranalysia
Hawk
Head -mounted camera
Heart
--PadMlogy
Heat equation
Heat reaiaiant allocs
-Pickling
Heat reaiatani polymers
--Drvelcpment
Heat transfer
--Acouatlc factors
--ntyalcal
Heaters
--Deelfn
Helicopter bladea
-•Preaervaiion
567
587
622
606
584
631
574
606
576
607
623
550
553
548
634
60f7
634
634
554
634
594
557
557
554
598
575
626
550
590
545
619
628
628
628
575
557
554
551
551
539
540
539
540
594
600
601
595
600
594
555
5*4
561
544
545
600
610
551
586
633
635
617
561
14* «■
ISSN
15319
153 IS
159941
147 7«
iso*n
13318
171 a
191 a
153 7«
199 4«
154 *U
154 741
154 4a
issa
194 7B
194 «
199 IM
134 791
14*41*
194 m
194*11
149 a
192 a
153 M
171 HI
171 9U
171 a
159 a
147 a
153 772
153 77J
193771
171 a
154 *H
14* a
153 112
153 8U
153a
I34M
147 7C
133 a
171 M
147 a
139M
153 a
19991
I53W
159a
153 a
153M
153177
153 la
153 a
199a
171 a
199 a
199 m
139 a
i6ta
171 a
194 a
171 a
171 a
194 a
154 a
171 9M
1-8
-AffUcatlaaa
"Oialgn
•I*
9*4
9n
M9
^IMceftocts 941
n^akHade
•-MMeorology 555
■ftyelologlcalcaecta 349
Hl^ praasure laaaarcb 630
H^epaed cameraa
-MMlagrapby 5*0
■a tsaperatura raaoardi 591
-Tiat tadUtlaa
-Itatlag equipment
HHBSiapy theory
glaeenng
-MlUtary requlrementa
«96
634
998
59*
563
- -Gryetal structure 546
Hydraulic servamectaanlems
"Asalyau 636
Hydraaolc scld
"IhaMiysls 349
347
624
547
579
609
! raactkna
—Molecular atructure
uca
il analysis
tt/^vfim eabnnlemaai
i^^ogsa peroalde
--DsoampoalUoa
--8pactra
--8iaMliry
Mifersonic ftaoi
■-Aaslysia
lie (eat vohlclea
--FUgKpada
l^fparvaloctty pra(ectllea
— BaMlor balllatlca
ivtty
:pn>l
I productloa
-Ckllt
"Icaaamic aapecta
"•dMduli^
<aa
*»pUcatla«
Ideae
iitlvlty
552
390
332
•06
606
608
560
544
544
949
9*1
937
357
9*0
999
<02
639
636
626
587
588
5*7
63*
9*7
6S7
999
629
153 879-1
153 879-2
149 0*7
159 617-1
199 617-2
159 619
171 493
192 902
154 808
154 819
171 049
154 968
161 932
171 159
154 842
154 966
154 722
153 676
153 675
171 551
153 490
154 966
153 051
153 t*6
153 237
153 686
153 276
149 782
171 502
171 902
171 512
148 154
148 936
14*936
154 749
147 543
14*936
153 811
154 749
153 769
154 109
153 769
199 118
190 636
152 582
154 758
153 355
153 374
153 370
190 899
193 482
199 4*2
171 IM
171 545
148 811
148 812
193160
153 199
153 199
171 511
153 763
149 155
153 690
154 423
153 763
153 664
130 904
153 496
Infrared film
- -Development
Infrared optical mawrUla
- -Development
Infrared reaearch
Infrared spectre
--Anaiyala
Infrared apectroocopy
- -Appllcatioaa
Infrared wavea
- -Meaaureaaaot
Inorganic polyaera
Inorganic subatancaa
- - Polymerization
laaulating materia la
Integral equadoQS
Interterometera
--Anaiyala
latermetalllc compouade
"- -BlbUography
--Mechanical propeniea
--Fhyalcal propertlea
Iodine
--nucolysla
Ion beama
--Analyau
Ion bombaitbueat
--Appllcatlooe
Ion propulsion
Ionization chamfaera
--Deaign
loniuuon pgea
--AppUcatlona
knoapiwre
-AMlyaU
- -Reflective efiecu
kna
--Froductlaa
Iron
--tmpuriaaa
Iron alloy
--Physical propertlea
Iron-mckel alloys
- -Magnetic propertlea
jet englnwe
--LiAncatkMi
jet fl^Maie
- -Farter maaoe
)et mlxlag flow
--Anaiyala
Jet propulaloa
]ata
•-Anaiyala
Job aaalyala
- -BfJactlvsaeee
Joloia
--Vthratloa
Jordan curve
Journal baarlaga
•-Thtorf
Jupiter
-- Radiatloa
KauB'e work
Laminar boundary layer
--Heat tranafer
-•Methemstlcal anaiyala
Landing ftelda
- - Lifting ayatema
Landing gear
--Stability
■Laafuafft
--Aaalyala
Ltadaelealda
--Heat of formation
Laadaraklp
-Aaalyala
--DaalcB
Laaraiag
--Statlatlcal aaalyala
--•rtati
- -Blactrtcal ayetama
U*i eupport (Aatroaaute)
596
990
*20
990
990
9*2
546
546
568
595
976
591
591
630
991
9*6
*22
586
617
631
99*
559
696
607
612
612
621
•29
992
961
•07
586
607
5S7
59*
5*9
600
9*7
934
535
637
634
606
9*2
561
637
547
537
537
576
999
99*
59*
540
561
WMumber
153 920
171 526
153 450
154 109
171 515
153 857
' 154 808
152 875
152 875
153 776
153 313
153 294
154 846
154 846
153 264
152 102
190 320
171 513
150 320
171 490
199 4**
153 399
147 532
133 698
161 380
153 183
171045
171045
153 700
153 563
154 969
139 991
133 262
154 104
153*9*
199*95
153*54
171 596
153 710
199 001
147 924
147 929
153 654
153 103
ISO 927
171907
152 5*9
153*75
147 52*
154*9*
154*97
154 838
171 398
171 549
14* IM
1SS4«7
190904
153 933
171 554
SuNact
R Number
- -Scattering
--Theory
Uqulda
--Electrical properties
- -Molecular structure
--fhysical propertlea
- - Resooanoe
LldUum hydride
--X-ray aoelyela
Uthlum hydride-d
--X-ray analysis
Lithium ions
--Olfiuelaa
Loglatica
--Theory
Low temperature batteries
- -Developmeat
Lubricant addtavea
- -Effectiveaaaa
Lubricants '
- -Materiala
Lumicoo
Lionineacence
- -Measurement
Lumlneaoent materials
- -Appllcatioaa
MayKeium
--Internal friction
Magnesium alloya
- -Corroalon
Magnealum oocidea
--Thermal propertlea
ealum cltanatea
-Electrical propertlas
--Thermal properties
Magnetic amplifiers
--Clrcuitt 570
Mayietic recording
eyetema
--Design 565
--Equipment 571
Magnetic reeoaaoce
- -Meaaurement 552
620
Magnetic upea
--Developineat 565
Magneto- bydnxlynamic
609
632
--Theory 607
Majwtorealataace eftect 602
Meanematrtctloa
--Tinary 626
Megiieiuatrlctlon traaa-
duoere
--Dealffi 9**
Maintenance
-BlUlagraphy 533
MalMBaoaoe equlpmem
--Laazpacwncy 619
Maaagement eaglneering 588
--Theory 638
558
620
624
625
621
153 566
153 450
150 657
153 123
153 757
153 916
553
620
553
552
171 535
147 848
171 535
150 063
629
154*07
629
154 807
627
583
560
153 819
153 660
153 931
577
153 935
592
154 9«9
562
534
171529
159 452
617
171491
553
130 895
613
154 867
615
150 502
590
171541
552
552
133 836
153 836
-Bqulpmaat
Maoer
XAaaoory
Materiala
--Handbooka
—Heat tranafer
--Propeniea
-•Streaaea
-Tkaaile propertlea
mo
589
605
951
9*9
603
Mathematical ooopuKr (teta
•-Codlag 597
600
Mathematical ooaqMMere
--Appllcatlaaa 601
--Qrculla 601
--Devclopmaot 601
— Bqulpmem 568
- -Errors 602
•-Mathematical aaalyala 601
--Schadulli« 9**
• -Slmulatloa
--Theory
MaihlBM equattOB
601
999
171942
194 296
154 747
150 063
147 848
154 296
153 835
152 696
153 262
149 933
154 095
147 4«
171 518
153149
149 155
154 423
153 886
153 290
171 107
171 494
159 568
171 49?
153 661
148 346
153 052
152 587
159 4*5
171595
190 073
154 422
149 090
149 333
153 10*
154 057
159 962
193 6*1
159 667
171 54*
159 672
Urn
- - Inatrvimeaudaa
MadMolc*
-Amtftim
--WucIt raa<
--Producdaa
•-ScmOBiiaf
MaiaboUam
-Padiologr
Metal -ptesdc
--Teat resulu
Mecal ptBira
--Itai rMulls
•-Vlbraboa
MealorfMUc
-■Properuee
Metala
- - Bomtenlnietu
atu»
-COTTtMloa pieveuti
-Crvap
-Bflecn of rwlunoq
-Elaculcal propertlM
-Blactradieiiustry
-Fracture
-Load diatrlbuUoa
-Madiantnl profKrllea
-PtckUiW
-Ttanparature
-IMag
-X-ray ■— Ijaia
(acto^
balloo^
Me«drataglcal ctena {
--Praparadaa
S96
997
S75
9M
9M
9>*
SI
«os
MO
Ul
6I(
«33
949
SW
SO
«02
991
«22
6S9
sai
U4
619
629
610
«04
604
611
614
610
614
611
611
620
636
S«0
59*
--Etectromagnetlc pdofiertleaSTO
--lUflecnTe effecta 1 639
Mediyl balidea |
-Spectra
15SSS2
193 334
193 234
193 144
193131
193 133
193 994
193 U6
146 346
193 403
171 91S
193 032
147 306
146 194
153 1S5
193 191
171 996
193 991
193 794
171 922
171 513
194 642
194 757
171 4t7
171 523
154 770
161 235
153 »S6
153(56
154 340
154 lis
161235
154 818
171 467
154 340
154 340
171 527
161 9i7
153 643
153 606
153 290
153 818
161 S67
153 549
Mlaaltea (coa. )
--Blectrlcal ayaieBia 964
--Bqutpmeoi SIO
MolecuUr rtxatloa
--Aoalyau
Molecular apactroacopy
--Mattaemadcal analjrala
Molecular structure
--Theory
-Blactroa traaaltlana
-Baergy
-RaUabtUty ■•
--Slnwlatlaa 601
-Telemeter syatema 563
Mlxturea
--HienDodyiiainlc piiipc rtlaa 634
Molecular assoclatlaa
-BMro S<7
624
552
624
624
624
SS4
(07
613
613
613
613
622
554
556
S75
542
536
536
536
537
--Vlbratioa
Moltaa aalts
MdyMeaum
- -Mednalcal profiertlea
--niyatcal profiertlea
Molybdeoum alloy*
--Mackanlcal propertlea
--Kyalcal propertlea
--Surface coodltiaoa
Morae poceotlala
Mo*lag tarpet Indicator*
Maltlpaifa tranamtaaloa
--Mattematlcal aoalyala
--ilerhanlcal pra|)ertlea
Naval persoonel
--Job aoalyala
--MUllary requlrementa
--f^ifuiuiaace
- -Selectloa
--Teet mattwrta
Naral reaeerch
Naval abora aetahllahmeim
639
153 944
153 613
153 616-1
153 616-2
153 614-1
153 614-2
153 615
133 612
153 617-1
199 617-2
154111
194 806
193 417
154 755
159 6*6
153 7t«
153 7M
147 775
152 612
153 637
147 775
153 637
153 114
153 428
153 637
171 535
151099
151 099
151 099
151 099
171 513
153114
153 888
153 59*
171495
153 4*9
14* 555
148 555
154 836
154 837
148 555
153 604
171 317
Nttrapaa oaldae
--Chemical raaftlnaa
--Productloa
NltrofBB ozyfluoiidea
--Chemical raactloaa
Nltroua add
--leamerlam
Notae (Radar)
--Aoalyala
NoUe (Radio)
- -Martttmarlrel aaalyala
Btlcal aaalyala
Nna (laarrirrlv eestiiig
--Apptlcatloaa
Noa- linear dlflerenclal
e<riatlaoa
--AppUcadoaa
--Theory
Nuclear ptiyaica
Nuclear power planta
- -Greenland
Nuclear reactloaa
--Maitieniatlcal analyak
Nuclear aplna
--Oeaalty
Nuclei
--NaiKroa croaa aactloaa
--apactia
Nuclaaakiae
--Spectra
Nudwiddas
--Spectra
Nunberv
--Theory
Ooaaa booom
--Arctic Ocean
—Geolocy
Ooaaao^apfay
--Arctic Ocean
OSlcer peraonnel
--Performa
--That B«ettM»la
Oparatkna reeearch
--AaalyaU
Oparatora (Maihematlca)
Optical Imagea
--buaailty
Optical inatrufDaota
--Derelopmaat
Optical aysiema
--Apptlcatloaa
550
560
550
549
573
594
622
56*
571
56*
S*6
542
595
615
S«0
632
547
624
618
632
544
544
596
537
558
537
557
537
537
583
636
636
601
533
557
S*l
ISITM
15) S0
153 7M
153 011
192 n«
193 Mt
153 8M
mmt
153 NT
ISIW
171 4H
171 4H
1547(8
ISOW
153 W
153118
138 814
147 771
153 U8
151 181
193 3H
193 aas
19) 8S
ISSVI
15) «S
ISSVI
153 «
1548)1
154 8S
154 8S
IS) Ml
171 )■
15)181
15)ffl
ISO IB
19)181
15) 8S
Mediyl-d-lMUdee
--Water aupply
153 610
-Haaitnnka
S*l
171481
--Spectra
552
153 549
Naa^
171411
Majwr-taBr-MOUer r<
rtnw
53*
153 190
171411
teory
609
154 339
Neodynuum
615
150 696
17140
MIcHau
625
153 456
NautTGO ro^Miwrt
-MatarUla
581
194 7)1
Microwave ampllAera
--Pcmer et^pUee
617
194 793
154 Tjr
--Davalopment
9«*
153 250
NeutroB croaa aectlaaa
1
-SdMduUnt
583
193 W
mo
153 36*
--Aoalyels
«U
153 140
Orgaalc compounda
Ul
153 937
Neutroo meiera
--BllBcta at radiation
617
171 4N
153 98*
--Developmeat
*17
154 428
Oaclllacor*
577
153 230
154 429
-Slatlatlcal aaalyala
572
151711
hUcTOMve equlpoaM
*
154 430
nclde cadiodae
--Oaal^
tn
153 344
Neutroae
—Propertlea
622
1)8 8S
--Radladoa
U9
15315*
--Ma^ietlc nmieaia
616
14* 155
Osidea
Mlcr«>M«e oeclUawra
--Nuclear raacdana
632
153 186
"Rqwlcsl prap0Ttl#s
9*9
171 la
--Davelopmaot
S71
1SS937
153 189
Ofwrn
MtcToaa^m apectroacoi
T
--RaOectlaa
620
154 812
-•Chemical raactlooa
607
198181
-MMtotrapky
624
154 113
Nickel alloy*
--Detennlnatloo
543
193 M
--hMtnaneaiatlai
«23
150 701
- -Oevelopoieat
«0
1*1294
--niy*lolo(lcal eOecta
542
154 411
MicroMvaa
tn
154 190
Nickel nima
Oayyen (Uquld)
"Pn^iatailiM
V4
190 89*
- -MafneUc properties
621
14*349
--AppUcaaooe
9*4
193 lU
tn
153 243
Nlooalc alloye
«10
161 234
--B^ulpnaent
561
171 SH
m
153 732
Nlohe
Mi
192 3*7
Oenm oooaumpcloB
Irfiai ilii
«a5
171 544
NloUuB
- -Maaaurement
543
194819
IfhriMMra alactroalc ai
ilpOMOt
--CoatlafB
•n
161932
Oaooa
Si*
193 8*8
171 159
--Chemical raactlooa
560
19* Mr
MtaaUafUaee
NloUuni compouDda
Ikefcaclof
-Daa^
M
193 487
-rhaae atudica
9*1
161932
"MaiariaU
593
171)8
Mtoalla parao— 1
171 159
-TMtBMlhodi
5*4
171 lU
"TtaMat
atr
193 2S*
raia duraaboUa
ftliaaila uajactorlaa
--Spactrofraphlc aaalyala
9*2
153*57
- -Meaaurement
546
154 !■
--SlMladaa
9U
194 f70
NllXXI^M
hracbuie bteica
Mlaallaa
--Chemical raactloaa
560
153 567
--Tmi reeulta
9*9
171 4M
--Aarodyoamlc chara
aer-
607
153 183
592
171 4M
laQca
9*2
194 970
--kalzaUoa
622
, 153 8(r
hrachute jumping
--CaMTol ajiiii
m
194 970
--MataboUaa
1-10
9*5
15S191
-Haxartte
542
171 Ml
.AarodyMmic character-
tobca
Itl^HMadc cryatala
Ikntol dUfcreatlal equetlooa
Illicit accelerator*
Iknlcl* beama
■ -Productlaa
{Article irajectoriea
-rtaatofraphlc aaalyala
hrtlclea
— Devmuaatlae
—Mlriradyaamlc characMr-
ledca
tadcla* (Airborne)
-Undflcettoo
"ladloactlvtty
hftidoa fuoctiona
itioo progra
Tbai ceeulu
— OHerioraitaa
Deelgn
Uty leaia
Bflactlvene**
*lttvlty
I oiycfaloridea
I propertlea
■ I reaction*
film
altlvlty
IhMagiaphlc recording
"AfpUcatloaa
■Oorrotitm
tarn
"Rrfomaaoa
llHMary atmoapheree
-Aaalyala
I (Fhyalca)
-Aaalyala
-Blectrlcal factors
-MadMmalcal aaalyala
-Properties
-Theory
naela
ifllma
-AppUcatiooa
-Materials
--Optical propertlea
fhailcliy
"Maiheniatlcal aaa^rala
-Theory
-AppUcatiooa
-Diclectnc propertlea
-X-ray analyela
-rhodium alloya
BlKtrlcal propertle*
542
S73
597
too
615
616
6li
625
616
<09
633
564
541
5tO
575
97*
«t9
SM
941
995
573
570
•M
SI*
637
546
549
637
M7
«S7
S«2
630
MS
MS
9M
9M
SS4
•U
Ml
«tt
MS
623
631
633
622
«M
M7
624
603
602
in
588
626
620
S77
617
IB Number
17104*
ISO 894
153 307
153 296
ISO 696
153 IM
149 0*7
193 757
149 315
154 399
153 499
153 653
154 402
153 135
171 549
171 929
194 944
194 750
153 604
148 610
147 547
153 821
171 542
153 4H
150 520
154 752
152 848
153 051
154 752
154 752
147 756
147 756
161 834
171 049
171 503
171 SOI
171 501
171 S06
171 551
153 2*5
153 732
153 488
152 656
153 934
14*936
147 748
153 432
153 820
153 824
153 311
192 3*2
171 532
171 490
150 657
171 531
147 402
148 811
148 812
153 142
153 767
171 525
153 649
171 527
153 230
154 429
Sulfa
Pneumatic derlcea
- -AppUoatioae
Pneumatic valve*
--OaelgB
-Ttet reeulu
Pokarographlc analyala
- -AppllcaDona
Polynara
--Cryetal atructure
--Marhanical propertlea
--Molecular atructure
--Optical propertlea
--Synitaeala
--Temperature (actora
folynomlala
--Theory
ftm H Number
1
PorouB metala
--Productloa
Poaltrona
--Nuclear reactloaa
Potaaalum
--Metaboliam
nxaaauan chloride cryatala
--Electrical propertiae
--Polarlzatioa
Pmwitlal theory
- -Greeolaod
Power at^ppliae
--Dealgn
--Military requlremenu
Precipitauoo
--Radloacuvity
Preaa forging
Preaaurc
--Coacrol ayatrma
Preaaure gagea
- -Seoaitivity
Preaaure regulatora
Daal^
--Teat reeulta
Preaaure awltchea
--Development
Preaaure veaeela
--Dealgn
Probability (StaUaUca)
- - Applications
- -Determination
--Theory
Protective covering*
- -Developoient
-•Teet resulu
Protective shelter*
--Te«t results
Protons
- -Nuclear reactloaa
PscudonKmaa lafectiooa
--Therapy
hycfaoacouatica
- -Bibliogr aptly
(Quality control
--Sutiaucal analyala
Quantum mechanica
--Appllcationa
--Theory
Quartz
--Applications
Quaru cryaula
--Temperature factora
Quinones
--Lleciron tranaiciooa
Radar beacona
--Equipoienl
Radar Inierceptloa
- -Equipment
l-ll
543
548
593
620
593
546
548
575
994
9M
613
618
543
62*
628
«M
960
5*4
560
5*1
611
636
SS7
5*2
5*4
5*4
9*2
630
996
939
994
601
SM
994
999
561
S*4
9*9
632
949
621
59o
too
Ml
693
616
632
633
MK
973
949
966
973
193 416
153 613
153 616-1
153 616-2
153 613
153 616-1
193 616-2
153 5*3
147 170
153 628
147 848
153 628
152 875
147 170
153 234
153 860
152 370
153 133
161 770
1S4S17
153 405
153 741
153 741
153 872
153 931
153 944
153 933
154 402
171 924
194 966
154 762
153 615
153 617-1
193 617-2
153 612
193 614-1
193 614-2
153 615
171 049
153 831
153 840
171 545
148 419
153108
147 546
1M092
147 176
171 514
171 HI
154 503
153 186
153 189
153 640
147 765
153 146
153 782
150 946
153 499
153 032
171 533
153 2*2
153 568
153 246
152 961
171 504
171 508
190 894
SaMact
Radar navlgstioa *y*tema
--Development
Radar reflectlona
- -Angle d arrival
Radar traddag ayaiema
--E<<ulpraaai
Radar tracking ayaieme
(Airborne)
--E<|uipment
Radiation
--Bibliograpby
--C3>etnical effecta
--Inienaity
Radiation damage
--Measurement
Radiation meiara
--Applicauona
--Development
--Power auppliea
Radio aatrooomy
Radio beacooa
--Development
Radio communication
ayatema
--Equipment
--Reliability
Radio equipment
--Reliability
Radio relay systema
--Equipment
Radio signals
--Mathematical analyala
Radio wavea
--Bibliography
-Propagation
--Reflection
--Scattering
Radioactive substances
--That methoda
Radlofreiiueiicy attenuators
- -Development
Radlofrequency cables
- -Joinu
Radiofrequency flltera
--Oeaign
--Mathematical analyais
. --Productioa
1 Random walk
fRareeartha
I --Application*
t Reaction (Psychology)
--Riysiological (actors
--Teat ntethoda
--Teat reaulu
Reacoon time
- -Analyala
Reactors
--Cooling
Reading
- -Determination
Rnvlingbeada
Recordiag aystema
--Dealgn
Re-entry aerodynamica
Refractory materials
--Bibliography
--Development
--Mechanical properties
--Physical propertiea
--Temperature (actora
Regression function
Reliability
--Military requlrementa
--Sutistical analyala
Remote control ayaicma
--Development
Retina
- -Blood circulatioa
575
635
578
572
560
551
558
619
617
551
617
534
535
572
579
577
577
567
572
635
534
570
635
6)6
573
635
635
6iS
578
567
579
572
615
619
599
622
539
538
538
539
533
638
571
573
60S
591
591
591
589
590
590
597
580
594
572
544
153 599
171 944
153 203
194 418
150 896
171 497
153 569
171 523
171491
171497
154 793
147 323
147 324
147 322
147 325
147 326
147 327
147 328
147 329
154 418
^153 22*
^ 154 516
154 516
153 247
154 483
161 581
147 324
153 818
161 587
161 580
153 821
161 581
161 588
154 417
154 806
153 248
153 243
153 244
154 483
150 696
147 553
147 176
153 823
147 561
152 837
148 169
153 497
147 561
OTSSB-449
171 503
194 747
153 821
153 968
154 846
161 932
171 159
154 846
171520
171 515
171 541
171 515
152 996
154 811
148 419
154 418
153 401
-Carittoao la
ei fuels
--Basrgy
lUxtethMdB
--Productioo
locket mocora
-MBwnaU
--TiMt methods
--TMtlnt ecfiifoam
-•Tfcniei
Rocket propeiUnu
-Ukrmaoiuc umiymii
lodDBt propelled ilede
--AATodynanuc clar4cter-
ladc*
--Velocity
Rocket profwlatoB
•-Theory
Rocketa
--Appltcations
Rotor biadea
--Presenmaoa
Runway lights
-Visibility
Saliva
--Aaalysia
Salta
--Electrical propertifea
--n>yalcal propenlei
Samplinf (SutlaUca)
- -Military rec|ulreiii^D(a
SaoHrlch paoela
--BIsctnclty
--VIbrattoa
Satellite vehiclea
--Applications
- -Cootrol aysiaoM
--□•wctlon
--FUsbi paibs
Scabtaitig
Scan -column uidBt
Scheduling
- -MacheRiadcal aaal^u
-- Simula tka
--Thsory
Scientific reporta
" Bibliography
Scientific reaearck
Sea water
--Cor riwtve efWw Is
--nirtncatiao
Sealing compounds
- - Developtneoi
Search radar receiver i
--Design
Search radar scamisra
--Design
Search radar aystema
(Lbsnd)
--Equipmeac
-lUllaballtT
SecaadU7 enuaaion
--MaAemsacal aosi^la
Sedimentatioo
-Analyata
--Mathematical aasl^ia
--Radiosctivity.
Seiaoograpba
--Appllcatiaoa
Semicoaducton
- - Applicstioos
S94
an
9M
9«6
Ml
an
S99.
9U
Stt
S«2
SSS
553
S9«
604
984
SIS
SM
SM
9tS
9t9
«M
575
600
63«
567
5W
«ao
63R
an
tat
«S9
MS
s«s
590
573
578
567
577
623
«l«
«09
619
•Crysul acruajrs
-Electncal property
-Eh
-Mawrlsis
-Thaory
ittl^stian
S«9
570
632
629
629
627
629
:1c pioperTie8626
548
630
627
543
Sensory perception
--Psydiological
Se<|uentlal analyaia
--Applications
(sen rs
539
994
193 739
190 072
153 769
153 928-1
193 908-2
171 499
153 449
153 449
171 499
153 825
153 826
190 330
147 532
171 514
171 S07
194 426
171 535
171 535
193 146
199 639
153 638
153 639
153 399
171 496
171 553
171 108
171 496
171 5*3
153 661
153 160
171 549
153 782
153 681
153 690
147 363
149 089
171 503
171 503
153 160
171317
154 809
154 746
171 107
150 894
153 208
153 248
154 844
190 717
194 417
154 339
154 417
193 075
153 736
153 268
154 843
153 932
153 873-2
153 873-1
154 770
171 511
159 233
153 264
153 819
148 931
152 837
193 688
tiigsri Has
Serins cxpsanloos
- -Applicsdons aM
Serromsdinaisms
--AippUcadons 9M
-Bqulpmeot
--Thsovy ai
Sheets
- -Boundary layer 407
- -Corrosion MS
- -Deformadon Mt
--Fracture 9M
•it
- -Hsst creatmeot MS
- -Stresses MS
--Vtbrsdoo 808
Sbeher occupsncy tents 585
Shelters
--Conntrucdan 969
Ship bulls
- -Stresses 9H
Ship models
--Ttat r«aulta SM
Ship plates
--Prscture 9BS
Shock waves
- - Machema tical analyata tOJ
--niyaical effecta 552
-- Propagation lOi
--Reflecdon MS
--Theory M7
Ml
MS
- -"nuckneaa MS
Shoee
--MlUury requirementa 592
--MoUture factors 592
Short taka-oa pisnes 563
Shrouded propellers
- -Ttat results 564
SlpaU
--Oetecdon S7S
SIUCOB
- -Impurities MS
Silicon csrbide
--Impurities M7
Silicon compounds
--Oemical reactions 591
Silicon compoonda (Or^nlc)
--Conbuadon 989
SllicaBe reatas /
--Adaorptloa 587
Silver
--Dlffuaion M7
- -Oxidanon S8S
Sliver crysiala
- - Deformation MT
Single crysiala
--Deformadon 8SS
--Fracture M7
Single crysiala (Meullurgy)
-Fatigue 610
--Iniemal friction 613
Sky
-Radiation 585
Slipped crysuls 4M
Snow
--Greenland SM
--Traf^csbiUty SM
Sdcw rosds
- -Construcdon 9M
Sodtion chloride <
--Crystal atructure SSI
Sol la
--Analysis M9
Solar atmoephere
--Spectra 9S9
Solar batteries
- -Developmem 577
Solenoids
-Appllcatiaan 910
Solids
-Creep 630
- -CrysttI structure 627
--Luminescence 617
- -Molecular structure 620
1-13
rSNiaibnr
153 677
149 090
171 496
171 SS3
171 481
171 482
171 483
171 480
1SS363
171 501
153 739
153 661
153 928-
153 928-
153 568
194 765
153 638
153 639
154 303
153 596
171 576
154 057
171 576
153 438
152 612
154 745
159 475
153 183
152 656
153 464
152 895
153 491
153 491
149 354
149 355
154 504
154 545
154 546
153 603
153 682
171 522
171 938
148 788
193 839
193 827
153 839
153 729
171 543
153 298
154 867
154 808
171 531
153 556
153 556
153 556
152 884
154 339
153 081
153 603
193 613
153 616-1
153 616-2
171 049
171 543
171 491
147 848
Solids (con.)
--Scrsnsee
SohKlons
--Electrical propertisa
--Thermal properdas
Sonsr equipment
- -Maintenance
Sonar personnel
--Trsining
Sound
--ntyslcsl sCtocts
--Theory
Space chsffss
--Etnctricsl eflscfb
- -Msihemsdcsl snslfsis
Spsce night
--niyslological i
--RtflaUlliy
Spectral emittaace
Speech
--Intelligibility
Speech tranamiaaion
-BflBcdvennna
Sftema
--Reflactlve eflects
Sptn rstes
SplnsI cord t *
--Fhysiologjr
SplnaU
--Theory
Sputtering
Squid
ScablUty
--Theory
Siainleas steel
--Oorroelon
--Forgliig
--Temperature lectors
Surs
--Deisctlon
--Energy
--Idendflcadon
Siatiadcal aoalysls
--Theory
Sutisdcsl dtstrlbutiooB
Stsdsdcs
--Theory
SmI
--Corrosion
- -Extrusion
- - Pstlgue
--Forging
-- Fracture
- -Mecfaaaical properties
Smnl cssdags
-•Mechanical properties
Steel wire
--Fhyslcsl properdes
- -Substitutes
Stellar eclipaee
--Analysis
Scorsge progrsm tests
Storsge tubes
-Design
••Development
Storms
--Radar analyaia
Strangle materials
--Devclopmnnt
Stress saalysis
-•Theory
Stresses
Structuree
--Defca-ntsdon
-Design
Sturm sequence*
Jiknurine peraonoel
--Teat methoda
603
554
554
536
536
633
620
623
574
542
980
990
637
637
558
625
542
542
629
623
547
586
634
609
615
612
610
533
534
S34
535
561
595
596
597
59©
597
615
562
612
612
611
983
611
612
612
534
584
568
569
566
555
610
603
603
604
603
602
602
594
537
158 7»
171 «
mm
ISSN
153 Ml
171 «
149*1
ISOTn
issaa
I
151 <■
154111
171 U
I5SP1
151871
151871
I9SMI
ISIU
1718a
154811
153 M
171 lU
ISSW
154181
154 «
14* «
191 M
161 a
150 IB
ISIM
193 «
147 a
171 a
193 W
193 M
133 1«
IS2«
ISSW
153 M
153 n
153 111
171 a
171 a
194 7>
151 M
193 «-i
i5sa-:
issa
171 a
154 4»
1S4 4M
147 a
171 lU
ISSW
148 W
ma
171 a
issa
171 M
154a
154 a
151 la
ISlM
141 a
14IW
147 a
193 1«
194a
.-Cifscsl structure
— DMsctrlc properties
:fk>w
iry layer
adon
-^cfesdaUag
.■BMuladon
Adsorpdvc propertlea
fhysicsl properties
(Mathematics)
drcuiu
tlcal analysis
HH*pllr legic
IjiftMlc fibers
"MMksalcsl properties
: tiAricama
iU
: mica
"G(T**>"I'*"°'>
•ntlH aaginserlng
•- CiMtrtCBl propertlea
I crystsls
avlty
- MsasiiiBWwnt
IkHpsrature control
IradlBtlaa
-hihalogtcal
—ntyslcsl eflscts
Ihwasl siiiissns
-Tlsory
'IkMry
Isctrlclty
pnpertlee
-Thsor,
(Orfsnlc)
^ Wtology)
Mioipiive properties
" (actors
627
626
604
Mt
«00
MS
ass
950
623
600
576
601
575
Ml
989
992
630
961
•»3
M9
as
a4
944
983
ITS
S7f
SM
sn
637
625
634
979
SS3
SM
«7
946
989
«03
971
622
578
948
952
639
610
610
601
621
986
963
967
967
994
947
943
944
154 431
154 097
153 649
153 743
153 149
153 782
153 691
153 660
171 512
153 768
153 710
154 771
171 548
171 949
171 555
171 948
171 494
154 969
154 SIS
171 SIO
154 769
147 SS3
171 486
153 139
152 865
153 487
153 803
153 228
171 108
150 322
154 097
153 496
154 722
153 346
153 487
1S3<04
154 097
194 809
194 754
153 767
153 431
153 823
154 190
153 233
153 836
154 770
153 701
153 701
150 073
148 949
153 449
149 394
149 355
153 349
193 389
153 600
152 877
148 931
153 374
Tltanliai
- -Eunslon
--Handbooks
--Mechsnicsl properties
Titanium alloys
--Fracture
--Heat treatment
- -Mechanical propertlea
--Propertlea
-Welding
Titanium compouuda
--Chenucal reacdons
--Temperature fsctors
Titanium powders
--Combustioo
Topology
-Applicsdons
-Thsory
Trace
Trscklng
--Psyc^oglcsl tsctors
Trsnsducers
--Devekipmeiu
Tranaformatiofu
(Maihemadcs)
--Theory
Trsnalstors
--Anslysis
Trsnsidon elements
--Phase studies
Trsnsmissioo lines
--Applicstlotts
--Impedance
--Mathemadcal analyaia
- -Operation
r»m aNimhar
8ii»ct
--Theory
Traaaonlc flow
--Mathemadcal analysis
Trsnsport equstlon
Ti^ansport phenotnens
Transport plaites
- -CammuBicaDon systems
Traneportadon
--CcKOgraphical factora
Traveling wave titan
--Development
Trtdiagonal macriona
Tungaun
--Fhyalcal propertltta
Tungsten sUoys
•-Mechnnicsl properties
TlauMldkidss
TurUaes
--Cooling
Tiirbulenoe
--Mathematical analyaia
Twin triodes
--Deterioradao
Two- body problem
Ultra hl^ frequency
antennas
-Deslpi
Ultrssoaic radladon
--Abnorption
--Ananuadon
Ultraaonica
--Appllcadooa
Ultraviolet apectia
--Aaalysia
Underwater souaS
--Pressure
Undsrwsier swimming
--■tbliogrsphy
--Equipment
Upper stmosphere
-•Chemical aaalysta
--Dsnnlty
Vscuian melUng
Van der Pol equstlon
I-U
SM
Ml
610
611
612
610
»1
M2
551
548
982
994
996
997
998
«00
601
975
998
800
SM
995
957
800
S95
630
638
575
9M
629
575
968
579
608
600
636
561
968
571
994
614
614
625
627
533
6p5
576
632
567
630
572
986
944
604
630
630
940
599
619
397
171 929
194 796
154 749
153 938-1
153 565
154 749
194 796
153 969
171 522
153 233
153 627
153 860
193 678
193 640
153 267
153 413
193 710
153 671
153 234
153 266
153 675
153 676
159177
171 909
153 202
154 762
153 710
153 313
153 603
171 113
1S3S98
171 498
153 932
171 557
171 498
171 SS7
153 644
152 987
171 911
171 505
153 605
199 9a
'193 144
191084
isiosii
153 87B-2
153 873- 1
on a- 449
193 797
1S4S44
153 679
153 347
147 848
153 775
171 499
153 355
153 902
171 577
171 577
153 967
153 586
171 921
153 668
Vshlcles
— M-35E7
--M-10S
--Simula don
Verbal behavior
Vertical take-off planea
--Model teat resulu
--Stability
Very high frequency cxxn-
municatitxi systetns
•-Krformance
Vibration
- -Countermeaaurea
--niysical effects
Video Integradon
--Equipment
Vinyl compounds
--Synthesis
Vlaual percepdon
--Physicsl fsctors
Voice communicstion -
systems
-Intelligibility
Wstar
--Reflective eflscia
--Storafe
Wster filters
--Deeign
Wster Immersion
Wster supplies
--Purificstton
Wsmr vspor
--Chemicsl eflects
Water wavea
--Aanlysis
--Boundary layer
--Hydrodyaamic character-
Udca
--Mathematical analyaia
S88
588
588
568
637
564
563
636
602
635
556
547
561
561
620
565
585
542
585
590
608
609
608
608
609
609
--Velocity
Waveguide filters
--Design
Wsvnguides
--Developmenl
- -Equipment
--Mstfaemsdcsl saalysis
Weather forecaadng
-Handbooks
--Mathemadcal aaalysia
--Statiadcal analysis
Weaifaer statlona (AirboriK)
--Equipment 996
Wetghtleaaneaa
--Aysiologlcal effects 942
Wekii
--Ttet reeults
Wind
--Geophyslcsl factors
--nysical effects
Wind tunnel models
--Tant resulu
Wind tunnels
575
574
574
572
555
555
556
556
583
556
608
964
Wil«B
--Flutter
Wiring dlagrama
--Analysis
--Theory
Wood
- - Fungus deterioradoa
X-radlaUoa
itty
--Froducdon
--Scatteriag
--Souroee
X-ray apactraaoapy
Zinccoadnga
--Mstallurgy
Zinc cryatala
--Fstlcue
Zirconiinn oxidea
--Thermal properdes
80S
6»
S70
541
630
619
S52
619
629
944
553
Ml
610
990
raNuoAar
171 525
171 529
153 562
153 562
153 875
153 740
149 354
149 395
161 940
153 794
171 484
153 8M
152 877
171 906
171 505
154 812
147 546
153 610
153 402
153 UO
171 Si^^
149 891
150 510
154 745
154 767
150 510
150 510
153 598
ISO 897
150 897
153 775
153 745
153 659
153 443
153 550
153 601
193 402
153 551
153 443
149 891
194 904
192 582
152 687
153 876
192 919
153 122
171 sr
153 sa
150 899
193 8»
194 807
152 865
150 895
161932
171 199
153 2«
171541
1
r
•
.-
«1
"«*'
'
NUMBER INDEX
, ''»V
--^ .
5«5
Number
AD- 232 381
^ Nunter
995
NumbsT
AD-345 936
fit
m
AALTH-57-J9
V2 AD-237 304
AALTH-57-40
544
AD- 233 491
8B2 AO-237 572
620
AD- 246013
»
AO- 10 930
at
AD- 232 644
9N AD-237 619
547
AD- 246018
M
AD-13 8W
SSf
AD- 232 662
941 AD-237 626
594
AO- 246 099
m
AD-13911
537
AD- 232 679
9M AD-237 634
621
AD- 246 136
m
AO-16111
622
AD- 232 698
M4 AO-237 635
637
AD- 246 156
m
AO-18SI4
537
AD- 232 705
$0 AO-2S7 641
540
AD- 246 189
»
AD- 22 410
617
AD- 232 831
iOi AD-237 642
540
AD- 246 343
m
AD-26 0M
614
AD- 232 835
9H AO-297 7S7
539
AO- 246 243
SB
AD-S4 347
555
AD- 233 993
613 AO-237 829
538
AD- 246 299
m
AI>-«3 734
601
AD- 233 093
M4 AD-237 864
999
AD- 246 316
VI
AD- 106 522
543
AD- 233 129
«• AD-2S7 868
638
AO- 246 358
M
AD- lot 394
509
AD- 233 218
«M) AD-238 049
570
AD-246r2
«
AD- 1 10 027
544
AD- 233 391
9M AD-238 086
621
AD-246r3
m
AD-I15 143
540
AD- 233 292
999 AD-238 16S
- 578
AO- 246 424
m
AD- 123 629
539
AD- 233 293
S99 AD-238 168
616
AD- 246 429
a
AD-12S S32
618
AD-233 380
611 AD-238 248
557
AD- 246 440
w
AD-133 949
548
AD- 233 515
S86 AD-238 286
540
AO- 246 499
VI
AD- 139 302
635
AD-233 516
9aO AO-238 360
594
AD- 246 491
m
AD-13e891
553
AD- 233 625
9tr AO-238 983
569
AO- 246 306
M
AD-I3»e70
542
AD-233 889
6ia AO-238 992
629
AO- 246 522
m
AD-143 0S0
«01
AD-233 902
619 AD-238 995
536
AO- 216 544
M
AD-147 SS3
638
AD- 234 018
106 AO- 239 004
602
AO- 246 546
SH
AD-14»554
sn
AD- 234 060
935 AO- 239 005
602
AD- 246 623
m
AD-14BSSS
577
AD- 234 107
105 AO-299 106
547
AO- 246 626
m
AD-144 930
S78
AD- 234 157
«M AO-239 177
543
AO-246 6r
m
AD-149S04
991
AO-234 184
•14 AD- 239 181
582
AO-246 632
m
AD-tS2 443
972
AD- 234 194
mt AD- 239 322
635
AD- 246 633
m
AD-1S9 318
Stt
AD- 234 268
Sr AD- 239 602
6r
AD- 246 634
<■
AD-1S9 800
S76
AD- 234 486
6» AD-239 645
603
AD- 246 635
M
AD-1«0 0S3
5«7
AD- 234 487
MS AD-239 778
602
AO- 246 668
M
AO-160 057
587
AD- 234 494
971 AO-239 941
620
AO- 246 691
VI
AD-1«0 0«1
SC7
AO-234 555
H7 AD-299 942
568
AO- 246 763
»
AD-300 94S
372
AO-234 724
«n AD-239 963
563
AO- 246 808
Ml
AO-aoi 4»
612
AD- 234 732
9M AD-239 964
563
AO-246 880
St
AD-201 072
574
AD- 234 751
9M AD- 240 073
616
AD- 246 906
VI
AO-303S72
S«9
AD- 234 775
991 AO-340 192
377
AD- 246 923
m
AD- 204 225
974
AD- 234 784
«M AO- 240 287
394
AO- 246 923
m
AD- 206 464
564
AO-234 831
966 AD- 240 299
988
AD- 246 969
m
AD-X»SM
(01
AD- 234 910
Sn AD- 240 618
609
AO- 246 970
m
AD-205 6M
«S4
AD- 234 927
9M AO-240 734
595
AD- 246 981
m
>. AD-20S707
J AD- 306 833
630
AD- 235 OX
aU AD- 340 799
583
AD- 246 982
m
569
AD- 235 030
106 AO-240 891
616
AO- 246 986
M
AD- 207 730
573
AO- 235 081
V2 AO-240 892
589
AO- 247 033
m
AD-20S22S
Si*
AD- 235 143
mr AD-241 166
608
AO- 247 068
m
AD- 208 266
696
AD- 235 144
6M AD- 2(1 824
554
AD- 247 096
w
AI>-3M3»1
tss
AD- 235 276
9N AD- 242 171
806
AO-247 123
VI
AO- 209 TOO
M7
AD- 235 316
9M AO-242 415
565
AO-247 159
M
AD-3I0 80S
9M
AO- 235 340
951 AD- 242 437
979
AO-247 161
SM
AD-211 3M
617
AO- 235 354
•S7 AD- 242 576
997
AO-247 162
S4t
AD-211 297
617
AO- 235 428
an AO-242 660
596
AD- 247 163
sd
AO-211 414
594
AD- 235 466
9M AO-2t2 667
974
AD- 247 219
M
AD-213 910
637
AO- 235 468
im AO-242 701
574
AD- 247 232
' m
AD-213 4»
630
AO- 235 699
9B AO- 242 704
tt6
AD- 247 239
m
AD-21S »4S. no.
996
AD- 235 755
962 AO-242 747
S79
AD-247 281
SB
AD- 216 294
S«
AD- 235 769
HD AD- 242 924
619
AD^247 284
m
AD- 21 6 295
5M
AO- 235 778
am AD-243 0S2
624
AO-247 387
SB
AD- 217 682
599
AD- 235 795
639 AO-2t3 115
5a
AO-117 300
SB
AD- 218 374
639
AO- 235 849
967 AO-343 170
597
AO-247 335
■f
AD- 218 6«1
557
AO- 235 934
«09 AO-243 172
998
AO-2r 336
M
AD-21R 852
«09
AO- 236 065
916 AO-243 177
632
AO-247 337
sa
AD-219 361
611
AD- 236 095
614 AD-243 181
604
AO-247 338
SB
AD- 220 241
639
AO-236 163
9t6 AD-243 330
580
AD-247 359
SB
AD-2» 676
630
AO- 236 225
619 AD-343 351
580
AO-247 36(7
SB
AD- 2X851
575
AO- 236 262
•to AD-243 423
582
AO-247 385
SB
AD-22S033
992
AO- 236 337
tax AD-243 492
636
AD- 217 432
m
AD- 225 038
619
AO- 236 405
»9 AD-2(3 750
628
AD-247 470
m
AO-2r 147
976
AO- 236 454
tn AO-243 829
550
AO-247 517
' SB
AD- 227 703
558
AO- 236 466
609 AO-243 872
579
AO-247 5*9
SB
AD- 238 290
sa
AO- 236 467
•DO AD-243 994
616
AO-247 658
St
AD- 238 615
633
AD- 236 670
9M AO-244 087
999
AD- 347 686
SB
AD- 239 400
«09
AO- 236 729
•02 AD-244 304
632
AO-247 745
m
AO- 230 703
625
AO- 236 737
98S AD-344 236
573
AD-247 758
SB
AD- 230 765
375
AD- 236 738
9M AD- 244 298
377
AO-*r763
m
AD- 230 794
SS7
AD- 236 747
999 AD-244 390
9M
AD-247 895
m
AD- 230 814
541
AD-236 749
914 AO-244 444
624
AD-247 906
m
AD- 230 944
559
AO-236 790
93S AD-244 583
552
AD-247 915
m
AD- 230 992
556
AD-236 751
915 AD-244 694
630
AO- 248 004
■m
AD- 231 071
910
AD-236 752
•15 AD- 244 752
566
AD- 348 006
m
AD-S31 142
564
AD- 236 753
535 AO- 244 779
975
AO- 248 025
tB
AD- 231 299
588
AD- 236 754
5)5 AO- 244 788
584
AD- 248 028
m
AD- 231 346
551
AO-236 787
919 AO-144 789
564
AD- 248 045
M
AD- 231 358
579
AO-236 86S
•M AD- 244 842
552
AO- 248 067
■
AD- 231 434
624
AO- 237 043
•51 AD- 244 916
409
AO- 248 070
«
AO-231 480
«06
AO-237 0S1
•M AD-24S 160
971
AD- 248 073
m
AO-231 545
543
AD- 237 075
«4 AD-24S 161
371
AO-248 133
m-
AO-231 817
546
AD-2r 130
9H AD-345 489
972
AO- 248 140
IS
AD- 231 951
S<7
AO-237 244
•0 AO-2t5 548
SN
AD- 248 141
91
AO-2S2 180
sm
AO-237 432
m AD-24S 672
597
AO-248 154
SB
AO-232 2t8
623
AD- 237 494
•it AD-a45 802
1-14
573
AD- 248 192
SB
tD-M* 206
AD-)48 210
AD-348 228
AD-248 258
«D-248r6
40-248 280
4D-248 301
4V-2a305
t^-Mtson
«-a«8S30
AD-348 362
AD- 248 363
AD-248 364
4D-248 365
40-348 385
iD-a«8 386
J»-]48 433
il>-aa447
iD-ia 453
AD-348 484
40-344 496
AO- 348 308
4D-248 516
4D-348 517
AD-348 530
AD-248 542
AD-34S550
AO-348 554
AD-248S73
AD-348 579
AD- 24(587
AD-3a588
AD-148 593
AD-248 996
AD-2M616
AO-348 631
AD- 348 637
AO-248 655
AD-348tS7
AD-248 659
AD-248 666
AO-248 667
AD-2tt685
80-2M723
8D-2M732
8D-248 780
8D-2M899
AD-248 912
AD-348 927
AD-ia933
AD-2a9S4
AD-248 970
AD- 249 025
AD- 249 042
AD-349 103
AO-249 104
AF-TR-5125
APMBxhlUt 57-3.
IKHilUt 58-10
) (0-862
) (0-2288
l«0-48«7
> 60-5488. V. 1
1(0-6122. V. 1
) 60-6122. V. 2
APMD-TN-60-18
AnMD-TR-59-18
AFMD-TR -60-55
*nMD-TR -60-73(1)
APMD-TR -60-73(2)
4nMD-TR -60-85, v. 1
4F»4D-TR -60-85. v. 2
4PB4D-TR-60-179-1
4FV4D-TR-60-179-2
AnMD-TR-60-180
AnMD-TR-60-184
4KXa)D-TN-60-58
AK:«C-TN-58-191
*K:«C-TR-56-305
4K»C-TR-59 217
•PC«L-TN-60-257
•PC«L-TN-60-25e
•KIL-TN-60-426
••aiL-TN-eO-437
ilCIL-TN-60-464
•KtL-TN-60 498
i»Caa,-TN-60 638
••CIL-TN-60-642
•WOL-TN-60-667
•yog. -TN- 60 -668
<fCM.-TN-60-675
•jatt.-TX-60-699
•CM. -TN -60-794
•CBL-TN-60-808
596
961
805
627
590
560
«04
«00
637
621
599
610
629
621
538
537
573
622
540
624
549
604
564
564
606
581
582
552
593
581
622
5«7
6r
604
623
609
573
5to
59o
5to
607
«07
622
970
627
994
627
623
619
637
636
633
637
999
566
633
612
580
580
580
584
583
582
580
580
582
580
564
584
584
582
583
580
580
605
558
637
573
548
599
558
537
555
557
631
624
559
556
620
556
556
534
535
560
APCRL-TN-60-816
598
APCRL-TN -60-817
555
APCRL-TN-60-822
5«7
APCRL-TN-60-993
571
AFCRL-TN-60-997
579
AFCRL-TN -60-999
574
AFCRL-TN-60-1100
631
APCRL-TN-60-1106
578
AFCRL-TN -60- 1109
633
APCRL-TN -60-11 13
599
APCRL-TN-60-1113
559
APCRL-TN 60-1118
637
APCRL-TN-60-1122
619
AFCRL-TN-60-1124
621
APCRL-TN -60- 11 2500
558
APCRL-TN -60- 1136
622
APCRL-TN-60-1199
^
APCRL-TN-60-1141(a)
APCRL-TN-60-1 141(b)
625
APCRL-TN-60-1152
622
AFCRL-TN-60-1153
633
APCRL-TN -60-1 164
622
APCRL-TR-60-190
570
APCRL-TR -60-196
993
APCRL-TR-60-238
557
APCRL-TR -60- 354
621
APCRL-TR -60-357
627
APCRL-TR-60-375
627
APCRL-TR -60-410
573
APCRL-TR -60-414
534
APCRL-TR-60-416
590
APCRL-TR-60-418
622
APCRL-TR-60-419
564
APCRL-TR -60-4X
540
APCRL-TR-60-429
622
APPlt;-TN-60-10
561
APOSR-TN -59-492. r»*.
596
AP(J8R-TN-59-1299
575
APOe>R-TN -60-104
576
APOSR-TN -60-223
596
APOSR-TN-60-424
632
APOSR-TN-60-632
633
APOSR-TN-60-716
949
APOSR-TN -60-717
572
APOSR-TN -60 -756
569
APOSR-TN 60-808
538
APOKR-TN -60-834
634
APOSR-TN-60-8T7
634
AFOSR-TN-60-890
997
APOSR-TN 60-893
616
APOSR-TN -60 -953
604
APOSR-TN 60-984
996
APOSR-TN -60-985
596
APOSR-TN-60-987
596
APOSR-TN 60-992
598
APOSR-TN -60- 1018
549
APOSR-TN-60-1019
597
APOSR-TN -60- 1027
60S
APOSR TN-60-1039
600
APOSR-TN -60- 1057
540
APOSR-TN -60 -1062
598
APOSR-TN-60-1070
633
APOSR-TN-60-1071
598
APOSR-TN -60- 1097
594
APOSR-TN -60- 11 23
600
APOSR-TN -60- 11 33
632
APOSR-TN -60- 1 134
633
APOSR-TN 60-1136
616
APOSR-TN-60-1145
995
APOSR-TN-60-1162
607
APOSR-TN -60 -1164
604
APOSR-TN -60 -1178
539
APOSR-TN 60-1183
609
APOSR-TN -60- 11 88
553
APOSR-TN -60- 1197
607
APOSR-TN -60-1224
600
APOSR-TN-60-1236
626
APOSR-TN -60- 1229
604
APOKR-TN -60 -1247
605
APOSR-TN -60 -1253
550
APOSR-TN -60 -1256
626
APOSR-TN -60- 1302
550
APOSR-TN -60- 1304
600
APOSR-TN -60 1340
607
APOSR-TN-60-1344
607
APOSR-TN -60- 1394
627
APOSR-TN-60-1405
631
AFOSR-TN-60-U14
549
APOSR-TN-60-1418
596
APOSR-TN -60 -1419
593
APOSR -TN- 60- 14X
592
APOSR-TN-60-1434
633
APOSR-TN-60-1461
604
APOSR-TN-60-1479
946
APOSR-TR-59-190
992
Number
AP06R-TR -60-118
552
APOSR-TR-60-149
581
APOSR-TR-60-1W
581
APOSR -TR -60- 198
626
APOSR-TR -60-169
540
APOSR -TR -60- 170
610
APOSR-TR -60- 171
949
APOSR -TR-60- 176
903
APSAM-60-3
HB
APSAM-60-82
•••
APSAM-60-88
S«l
APSAM-290. R-1
965
APSAM-392. R-2
94>
APSWC-TN-99-33
6X
ACC-1233
948
AOC-1541
945
AGC-1941. aupp.
AIL-3689-1
•66
A1L-45X-1
996
AIL-4614-l
566
AIL-59S4-1
965
A«-314-60-IR-129
998
Alreaaarch AB-6S78-MR
re*. 3
580
Alreeevch AB-7029-MII
re*. 2
580
Alreaeerch AB-7030-MR
rav.2
980
Amaeercfa AB-7474-R
▼. 1
980
Alreaeerch AB-7474-R
». 2
580
Alreeeerch AB-7918-MII
580
Alreeeerch SC-9175. rev.3
580
AU C-61489
599
AA8C-TR -60-7 -577
5ca
AII4C-TR -60-7-637
611
AMR-1005
564
AIOC-TR-59-33(l)
560
AfOC-TR-59-33.pc 2
580
ARF-1149-4
966
ARF-2164-12
612
ARF-31 64-12
561
ARF C-164
961
ARL-TN-60-109
980
ARL-TN-60-124
604
ARL-TN-60-137
606
ARL-TN -60-138
586
ARL-TN-60-140
«06
ARL-TN -60- 145
tm
ARL TN-60-150
542
ARL-TN -60- 158
554
ARL-TR-60-282
561
ARL -TR -60-295
612
ARL -TR -60-314
600
ARL -TR -60-315
533
ARL -TR -60-323
633
ARL-TR-60-3X
6»
ARPA Order 24-59, Teak 3
949
ARPA Order 40-59. Taek 3
590
ART-TR-60-326
628
ASROL-2151
566
ASRDL-M-1924
567
ASROL-M-1926
S«7
ASROL-M-1948
507
ATI- 29 321
612
ATI-162 940
565
ATI- 173 115
613
ATI- 199 919
546
A*co RAD-TR-60-r
6X
A»co RAD-TR-60-29
631
Atc» RR-93
558
Avco RR-94
605
AWSM-105-37
555
BAC-775
601
im-632
603
BBN-727
602
ieU-9015-19-002
609
■.-11
949
BRL-TN-1356
636
Supers TB- 60- 11
536
■uPera TB-60-13
536
CAL AF-I285-A-1
605
CAL A1-U90-A-5
609
CH-19. V. 1
<08
Ca Rat. 60-1. V. 1
60S
CML-TR-P153-12
990
Caurt-29
561
cacim-tc-i
554
CU-8-60
509
CD-14-58
595
CU-17-60
569
CU-18-60
595
CWR-TR-59-80
626
CX-50
631
Number
DAC A260-<;K-I'KI-A06.0
562
DACL-8055-2
596
OASA-S01(DeI)
541
DASA-799
909
DlkeQR-3-l0O4
939
□MiC-127
614
DlflC-140
613
OikK-143
612
DMC-M-81
610
OMIC-M-82
610
DkflC-M-84
610
D8AC-M-85
610
DB/TB5- 1401/483
588
DPS/TW-eOl/15
5«8
Uri'MB-1290
«(a
DrrMB-1311
80S
orna-isTo
808
DTIiB-UlS
595
DodapTR -252-60-1
571
OURl RR-427-71
635
B-S7 93 detector
576
BB-401
969
EERL-6-39
959
EBS-1A66024
966
EBS-4B(E1)10I717
619
BP-141
999
BRP RM-10
618
BRPRM-IS
•••
FA-M60-14-1
964
PAR-1534
613
PAS-5584
562
FAATaek 59-XS.9
561
FAA Taek D/E- 1-6089
561
PI I-AX33-3
SB
PI I-A2049-10
an
PRI-R. 146/4
90
FRL-TN-9
9B>
FRL-TR-19
9K
GMI-1940
617
GMl-2133
632
Grew AP APOSR -61 -4^
TN-1
593
Gmn NSP C-642
999
Grant NSP G-7668
621
GraM NSP G-5250
604
Cram N5F G-8434
698
GreM NSF G-9903
995
Grant FHS G-M-743(CS)
541
CRDGRP-48
5a
trrELTR-60-7019
627
GTBLTR-60-704-104-
304-XS-208.2
571
Haz«i-9905
979
HB-lX-178
•56
HBrL-192
«W
HBfL-199
•16
HB«.-X3
*U
HLCrrM-94.2
HUX
an
HI5-14
an
HT-7
an
HumRRO-RR-6
5S7
lBR-X-133 »
•06
IBR-60-280
•71
IER-eO-306
•11
IBR-60-31S
an
IER-82-11
«n
IER-131-9
ILUDCL-96
m
IRL-127
an
ISMS -223. iw.
•M
ISMS-254
an
ISMS-298
an
ISMS-260
an
ISMS-261
She -266
an
LlRTR-145
an
LmTR-146
•n
LL 230-0043
an
LL 220-0046
an
LL 220-0051
LL 250-0021
•51
LL25C-0029
an
LL30G-0009
m
LL S.1O-0014
LL46G-0009
an
LL 5IC-0017
•M
LL53C-0043
LL53G-0045
•ai
LLS3C-0046
•n
LL 530-0047
LLTR-16S
588
LLUOCL-103
an
LMSD-2882S4
•n
1 .h4Sn-480 485
619
i-ia
i
NMBtor
604
Number
9«
ftanber
PB 151 099
M3
Nmter
PB 153 313
ss
LMSD-703 021
OiURF-854-1
SN
LMBD-703 ISO
S52
omntr-u3-sa
M7
PB 151 102
M2
PB 153 355
544
Lock a-«0-36
«09
aBUIlF-M6-6
MO
PB 152 102
SM
n 153 370
S«
MBDEW-RS-2-«0
S4S
arAC-RR-29
SM
IB 152 128
973
FB 153 374
544
MEDBW-RS 4-60
$43
ClTAC-RR-30
3M
FB 152 370
SM
FB 153 389
sn
MBDEW-RS-S-W
543
ofrsa-449
SM
IB 152 403
SB
PB 153 390
S«
MBDBW-tS-7-tO
545
n 143 001 rev.
9M
IB 152 582
>' ' 4Mi
PB 153 399
SH
MBDEW-RS-g-«0
545
IB 147 170
SM
IB 152 583
' »>. J '"JM
FB 153 401
544
MH-24903
M*
n 147 176
SM
IB 152 587
MD
PB 153 402
541
t*iTD-*3D<0
m»
n 147 306
Ma
FB 152 612
SM
FB 153 403
541
ML -714
Sf4
R 147 322
SM
IB 152 656
Ml
PB 153 405
543
MTL-U
574
n 147 323
SS4
IB 152 607
MS
FB 153 406
543
MRMOMRQ-M
634
n 147 324
SM
IB 152 726
fi-' S
FB 153 413
«»
MSEE eO-23
<01
ni47 32S
SM
IB 152 828
•M
PB 153 415
SW
MSRfOr-SI
Mi
n 147 326
SM
FB 152 837
'. mp
PB 153 416
(M
MSIl?RR-16
Ml
m47 3r
SS
PI 152 848
'- -hMK '
PB 153 4Z7
SK
MUPTR-t99
Ml
m47 338
5M
IB 152 865
■^'•Jlli
PB 153 428
MP
NAA-MD- 59-79
S»
n 147 329
SM
IB 152 875
" ■^' »f#
FB 153 431
571
NAA-MD-«0-329
604
n 147 363
SM
IB152r7
FB 153 432 -
6»
NAMC-ACEL-437
536
PR 147 402
Ml
FB 152 884
' ' SM
FB 153 443
SM
NAVORD-1222
62S
r« 147 498
SM
PB 152 895
MS
FB 153 444
m
NAV(»D-30f72
«1S
n' 147 528
S«7
FB 152 902
IS.
FB 153445
590
NAVORD-3341
634
FB 147 532
SM
PB 152 915
" ''• ''-mm
PB 153 447
SM
NAVORO-4366
S5S
n 147 543
Ml
PB 152 956
--«r
PB 153 448
sao
NAVCIID-S929
601
PB 147 546
5«S
PB 152 961
SM
PB 153 449
SM
MAV01U>-«076
576
PB 147 547
595
FB 152 970
sn
PB153 4SD
MO
NAVORO-6227
630
n 147 553
M«
FB 153 032
M*
PB 153 452
53t
NAVORO-64M
611
PB 147 561
SM
FB 153 051
SM
PB 153 456
625
NAVORD-6496. pL 2
tit
PB 147 748
Ml
FB 153 052
SI?
PB 153 463
MS
MAVORD-ftAM
629
M 147 756
617
FB 153 075
SM
PB 153 464
636
NAVORD-ftMO
634
PB 147 757
M«
FB 153 076
SM
PB 153 475
eo6
NAVWEPS-70S5
5»3
n 147 766
tai
FB 153 080
SM
PB 153 482
587
HAVWEPS-7152
576
PB 147 787
SM
FB 153 081
5M
FB 153 485
toi
HAVWBPS-75W
586
n 147 768
SM
FB 153 097
579
FB 153 487
SM
NK-TN-79
636
PB 147 775
tat
PB 153 103
634
FB 153 488
631
«S-TN-»
635
n 147 848
tao
PB 153 107
576
FB 153 489
536
MB-TN-86
IB 148011
X7
FB153 108
Ml
FB 153 490
SM
MB-TN-a?
6»
PB 148 092
SM
FB 153 114
SS«
FB 153 491
sn
NCBL-R-097
MS
PB 148 154
618
PB 153118
M6
PB 153 497
SSI
NCBL-R-103
MS
PB 148 155
M«
FB 153 122
541
FB 153 499
631
NMC-TM-dO-S*
544
n 148 169
SM
FB 153 123
635
FB 153 »2
604
NOLC-425
601
PB 148 198
MB
FB 153 125
60S
PB 153 503
574
NOLC-528
576
PB 148 200
9M
FB 153 132
600
FB 153 549
5S2
NCIfrS-279
635
PB 148 215
616
IB 153 133
599
PB 153 5S0
5M
NOrS-882
634
PB 148 346
U3
IB 153 135
S96
PB 153 551
SO
Nt7rS-TP-2452
583
n 148 349
Ml
IB 153 138
Ml
PB 153 554
SM
NCrrS-TP-254l
5««
FB 148 411
S7I
IB 153 139
SM
PB 153 556
SM
NP-M64
618
PB 148 419
SM
IB 153 140
618
PB 153 561
536
NRCC-LR-289
<0«
PB 148 555
SM
F« 153 142
603
FB 153 562
SM
NRCC-LR-290
559
n 148 559
M»
IB 153 144
SM
FB 153 563
69
NRCC-ha-236
586
PB 148 610
SM
PB 153 146
SM
FB 153 565
612
NRTC-MH-lOO
609
PB 148 656
SM
IB 153 149
M* '
FB 153 566
5sa
NRCC-MS-103
611
FB 148 788
S«7
IB 153 ISO
SM
PB 153 567
5M
NRL-VMO
M3
IB 148 811
M2
IB 153 152
546
PB 153 568
US
NRL-VMO
9M
PB 148 812
M3
FB153 154
6M
FB 153 569
SM
NRL-5578
SM
PB 148 931
SU
PB 153 160
6M
PB 153 583
541
NRL-VVm
PB 148 936
Ml
FB153 177
600
PB 153 586
SSI
NRL-5581
Ml
FB 149 087
MS
IB 153 183
607
PB 153 591
S«i
NRL-5593
9P*
PB 149 089
MD
FB 153 185
632
PB 153 592
611
MSP 0-5276
tu
PB 149 090
5M
FB 153 186
632
FB 153 595
S75
NSFC-9«f70
565
FB149 155
SM
FB 153 188
616
PB 153 598
S7S
ML-442
634
PB 149 315
616
FB153 189
632
PB 153 599
SM
NHtOP BR-2.S082
593
PB 149 321
S94
IB 153 191
545
FB 153 600
SM
MWL-1725
583
IB 149 333
«3
FB 153 199
636
FB 153 601
SS6
NWPW-T-7-59
611
n 149 354
SM
FB 153 200
9N
FB 153 602
sn
H1KPW-T-35-S9
611
PB 149 355
SM
FB 153 202
SM
PB 153 603
630
0<»R-«39. 10-P
633
IB 149 782
M9
FB 153 303
an
PB 153 604
511
OailR-9M.30-M
63«
PB 149 991
Ml
FB 153 221
STB
PB 153 605
SM
rX1IIR-9M. 31-M
583
PB ISO 063
SS3
FB 153 230
377
PB 153 608
SM
00IIR-I2SXX
589
FB 150 072
993
FB 153 233
SM
PB 153 610
SM
OORR-1S38.13-E
574
IB 150 073
Ml
n 153 234
s>s
PB 153 612
SM
C)0RR-1574.5
619
PB ISO 088
tat
FB 153 237
634
PB 153 613
SM
DORR - 1716. 13-E
595
IB ISO 330
SM
FB 153 238
MO
PB 153 614-1
SM
0(1RR-1833.2-M
395
PB ISO 322
533
FB 153 243
S79
PB 153 614-2
SM
OORR-1840.18-M
598
FBisosr
M*
n 153 244
S79
PB 153 615
SM
OOIIR-1837.4-M
S97
IB ISO 469
Ml
PB 153 246
573
FB 153 616-1
SM
OOIlR-l923t5-C
554
IB ISO 502
Ml
PB 153 247
587
FB 153 616-2
SM
OOIIR-XMSlS-P
62»
fV ISO 510
Ml
PB 153 248
SM
PB 153 617-1
SM
OORR-2070.1-M
601
IBIS0 5X
5«
FB 153 249
SM
PB 153 617-2
SM
nOIIR-212S.12-M
599
PBI50«r7
544
FB 153 250
SM
PB 153 627
Ml
OOItR-2a46.2-M
598
FB 150 636
«M
r« 153 262
W7
PB 153 628
Ml
OORR-2346l4-M
S»«
PB ISO 657
tat.
FB 153 264
630
PB 153 635
SM
OOItR-226S.3-E
574
FB 150 696
MS
FB 153 266
3M
PB 153 637
6M
CX)RR-23«. . . .
631
PB ISO 701
M3
FB 153 267
SM
PB 153 638
M4
CXJIIR-242Z5-M
596
PB ISO 717
MS
PB 153 268
SM
PB 153 639
M4
CX«R-2.Vin l-M
632
PB ISO 894
srs
FB 153 r6
979
FB 153 640
54S
OORR-2S«a2-M
597
IB 150 895
SM
FB 153 282
633
PB 153 641
541
ORDP-2D-305
581
FB 150 896
SM
PB 153 285
534
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I-U
U. S. DEPARTMENT OF COMMERCE FIELD OFFICES
SERVE THE BUSINESS COMMUNITY
The Department of Commerce maintains Field Offices to enable the business community to
avail itself Nxally of (iovernment facilities designed to promote commerce. Working closely with
various units in the Department and, when necessary, with other Government agencies, the Field OflTiccs
provide business services to manufacturers, wholesalers, retailers, trade publications, trade as.socia-
tions, advertising agencies, research groups, financial instittltions, and exporters and importers.
Experienced personnel will gladly assist in the solution of sj)ecific problems, explain the scope
and meaning of regulations administered by the Department, and provide practical assistance in the
broad field of domestic and foreign commerce. Field offices act as official sales agents of the Super-
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and similar business groups under which these organizaticms have become official Cooperative Offices
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be referred to the nearest Departmental field office.
Department Field Offices
Albu4u«rqu«, N. H«., O. S. Coufthouac. PhoM: ClUp«l
7-OJll.
AtUoU 3. (H.. 604 VoluntMf Bids-. 06 LucU* «.. NW.
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imgton 25, d. c.
iUl business
■>rv--
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CATMINT OF POSTAGC. tSOO
. • »•.
(woiernment
I
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^this issue:
ting for High-Temperature Service.
(PB ISl 108) /». 776
;mical Milling. (PB 171 112) />. 7W
•1 Cells. (PB 171 155) p. 699
lual for Bervllium Prospectors.
;(PB 151 105) />. 779
lymers Related to Cellulose.
(PB 171 571) /.. 69* •
*arch in Micro Flip-Flops.
[(PB 171 566) /'. 731
►p Practice Suggestions No. 3.
|(PB 171 251) p. 744
lid State Research. (PB 171 573) />. 79.^
arable Fifth Wheel. (PB 171 613) p. 7.W
eralloy Forgings. (PB 161 236) /». 776
• Qtrnpiele lisl of printed repitrts
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June 16, 1961
Vol. 35, No. 6
A monthly listing of
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available to industry
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OF MICHIGAN
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P'^^Ksa
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that the demand
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Because of the increased size of the publication, it is necessary
to increase subscription rates. Prices will now be $15 a year ($3.75
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The first issue under the twice- a- month publishing schedule will
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The new subscription price will be effective for current subscribers
when their present subscription expires.
CONTENTS
Page
PRINTED REPORTS AVAILABLE FROM OTS ANNOUNCED IN THIS ISSUE ~v
BIBUOGRAPHY 681
ASTRONOMY 681
Astrophysics. 681
BEHAVIORAL SCIENCES 682
Human Engineering 682
Personnel and Training 683
Psychology. 684
BIOLOGICAL SCIENCES. 687
Anatomy and Physiology. 688
Biochemistry 689
Medical Specialties and Equipment 690
Pathology. 690
Pharmacology and Toxicology 691
Radiobiology 691
CHEMISTRY ^ !'.!.*!!!.*.* 693
Analytical Chemistry '. 694
Organic Chemistry 694
Physical Chemistry 698
EARTH SCIENCES 704
Climatology and Meteorology 704
Geodesy.
707
Oceanography 707
Physics of the Atmosphere 708
ENGINEERING ! . ! ! 708
Aeronautical Engineering 708
Chemical Engineering 712
Civil Engineering '. 713
Electrical and Electronic Engineering ' , 718
Mechanical Engineering 735
Ordnance, Missiles, and Satellite Vehicles 736
Sanitation and Safety Engineering 742
Ship Building 744
FOOD, HANDLING, AND PACKAGING EQUIPMENT 746
Food ! ! ! ! 746
MACHINERY, FABRICATION, AND ACCESSORY EQUIPMENT 747
Engines and Propulsion Systems .« 747
Manufacturing Equipment and Processes •. 748
Transport. Traction and Hoist Facilities . 750
MATERIALS , 752
Adhesives and Sealants 753
Ceramics and Refractories 754
Fuels, Lubricants, and Hydraulic Fluids , 755
Plastics 756
Rubber and Elastomers 757
Wood and Paper * 755
MATHEMATICS 758
Computing Devices ' 764
MECHANICS 76i
Aerodynamics and Pneumatics i 769
METALLURGY 775
Ferrous 773
Light Metals .- 779
Structural Metallurgy and CorroBion 780
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY ' 781
Elementary Particles 7g2
Instruments and Installations 783
Nuclear Engineering and Power 783
Nuclear Structure 734
Radioactivity. 784
PERSONNEL SUPPLIES AND PERSONAL EQUIPMENT .785
lu
PHYSICS
Acoustics. .
Electricity and
Electrcxiics
Molecular Physfics
Optics
Pa
? 1U
• 787
Magnetism. 787
789
and Spectroscopy 790
^&
792
Solid State Phys ics 793
Theoretical Physics 799
Thermodynamif;s 800
Wave Propagatipn ,1 804
RESEARCH METHODS, TECHNIQUES AND EQUIPMENT ..../////////./.......... 805
Conununicatioa Theory 807
SOCIAL SCIENCE^ .........[........... 807
807
Documentation.
MISCELLANEOUS 808
ATOMIC ENERGY COMMISSION REPORTS 809
GENERAL. MISCELLANEOUS, AND PROGRESS REPORTS ' ] ' * 809
BIOLOGY AND MEDICINE 8O9
CHEMICAL SEPARATIONS PROCESSES FOR PLUTONIUM AND URANIUM » 811
CHEMISTRY. .\ 811
CONTROLLED THERMONUCLEAR PROCESSES 814
CRITICALITY STUDIES 814
ENGINEERINGJAND EQUIPMENT " 814
GEOLOGY AND MINERALOGY , 816
HEALTH AND SAFETY 816
instruments] 817
ISOTOPES - INCTJSTRIAL TECHNOLOGY 818
ISOTOPE SE PA RATION 818
MATHEMATICS AND COMPUTERS [ 818
METALS, CERAMICS, AND MATERIALS 819
NUCLEAR EXPLOSIONS - PEACEFUL APPLICATIONS 822
PARTICLE ACCELERATORS AND HIGH-VOLTAGE MACHINES 823
PHYSICS
RADIATION EF
REACTOR
SOURCE IhJDEX.
SUBJECT INDEX
NUMBER INCCX
t
823
't , I
RECENT CUMULATIVE INDEXES AVAILABLE
Volume 31, January - June 1959. $1.
Volume 32. July - December 1959. $1. . . j-j
Order from SiAjerintendent of Documents, U. S. Government Printing Office, Washington 25, D. C.
n»Mi^
PRINTED REPORTS AVAILABLE FROM OTS
ANNOUNCED IN THIS ISSUE
Page
BEHAVIORAL SCIENCES
Discrimination of differences in mass of weightless objects. Dec 60.
25p. (PB 171 601) 75 centa : 662
Self- maneuvering for the orbital worker. Dec 60. 28p. (PB 171 611)
75 cents 682
Sensory deprivation and perceptual lag. Dec 60. Up. (FB 171 610)
50 cents 685
BIBLIOGRAPHY
Air pollution and purification. Feb 61 . lOp. (OTS SB-448) 10 cents 744
Chinese mainland science and technology. Rev. Mar 61. 21p.
(OTS SB-442) 10 cents 681
Fuel cells and related research. Feb 61 . 7p. (OTS SB-447) 10 cents 731
High temfjerature metallurgy and heat resistant alloys. Feb -61. 36p.
(OTS SB-452) 10 cents 777
Hi^ temperature research (ceramics, gases, lubricants, plastics,
electrical and electronic equipment, etc.) Feb 61. 36p.
(OTS SB-453) 10 cents 804
Low temperature research on materials. Feb 61. 28p.
(OTS SB-451) 10 cents 753
Power supplies. An ASTIA report bibliography. Jan 61. 313p.
(PB 171 689) $5. 00 681
BIOLOGICAL SCIENCES
Cooling and rewarming under protection of antiarrhythmic agents.
Oct 60. 12p. (PB 171 602) 50 cent& 690
Effect of chronic whole -body radiation on blood enzynies. Nov 60.
44p. (PB 171 608) $1. 25 691
Effects and characteristics of increased respiratory dead space in
dogs. Dec 60. 14p. (PB 171 607) 50 cents 688
Radiological health dau. Volume 2, No. 2. Feb 61. 54p.
(PB 161 371 - 1 1) $1 . 00. $9. 00 yr 692
Radiological health data. Volume 2, No. 3. Mar 61. 58p.
(PB 161 371-12) $1.00, $2.50 yr 693
Radiological health handbook. Sep 60. 474p. (PB 121 784-R) $3.75 692
Study of the effects of ionized air on behavior. Nov 60. 24p.
(PB 171 600) 75 cents 688
Thermal and metabolic responses of the Alacaluf Indians to moderate
cold exposure. Dec 60. 49p. (PB 171 606) $1.25 688
CHEMISTRY
IV
Equilibrium polymerization of selenium. Apr 60. 15p. (PB 171 575)
50 cents ' 699
Fuel cells. Dec 60. 80p. (PB 171 155) 75 cents 699
Models of stereoregular polymers (Part I). Stereoregularity in the
free radical polymerization of vinyl acetate (Part 11). Anionic
polymeri^tion (Part 111). Dimensions of polymer chains (Part IV).
1960. 44p. (PB 171 570) $1.25 696
Organotin polymers. Feb 60. 26p. (PB 171 571) 75 cents 696
Polymers reUted to cellulose. Dec 60. 85p. (PB 171 574) $2.25 694
Stereospecificity and dielectric properties of polar polymers. Aug 60.
52p. (PB 171 563) $1. 50 697
Study of superoxiditers. Mar 60. 59p. (PB 171 255) $1.50 702
ENGINEERING
Air pollution and purification. Feb 61. lOp. (OTS SB-448) 10 cents 744
V
ENGINEERING (con.)
^
r'.
Pai
Nov 60. 78p.
736
730
740
709
An introduction to ballistic mjsailes. Volume I. Mathematical and
physical foundations. Mar 60. 243p. (PB 171 247) $3 50
An introduction to ballistic missiles. Volume II. Trajectory and
performance analysis. Mar 60. I04p. (PB 171 248) $2 50 7^
An introduction to ballistic missiles. Volume III. Design and engi'-" '
neenng of lub-systems. Mar 60. 135p. (PB 171 249) $2.75 7^
Anintroductiojj to ballistic missiles. Volume IV. Guidance techniques". '
Mar 60. 2$8p. (PB 171 250) $3.50
Desipi objectives for telemetry R-F transmission links'foV the period
1960 to 1970. Jan 61. 26p. (PB 171 690) 75 cents . . . ,
Dynamic compkessibility of solids from single experiments using
light reflection techniques. Oct 60. 35p. (PB 171 686) $1.00 7«
Electric poweped and solar powered food warming units for space'
vehicles, ttec 60. 6lp. (PB 171 605) $1.75 ., .
Evaluation tes^ model 56C and model 56D runway barrier systems
July 60. 10$p. (PB 161 914) $2. 25
Experiments oil slip damping at rounded contacts.
(PB171 5941 $2.00
Feaisibility of I lightweight air conditioner system for piston engine
driven aircraft using air as the refrigerant. Feb 61
(PB 171 257> $1.00
Feasibility tesjs of aircraft-mounted arresting hook lulv 60 77n
(PB 161 915)1 $2.00 i y^- //P
Fuel cells and Related research. Feb 61. 7p.
Human factors Iresponse during ground impact
(PB171 599) $1.00-
Investi^tlon oi thermal characteristics of TNT and other exploeives
Nov59. lO^p. (PB 171 256) $2. 50
New electrochemical system for high-voltage low-current drain appii
cations. Mar 61. 21p. (PB 171 582) 75 cents . . .
Research in mi :rofUp-nop8. Aug 60. 91p. (PB 171 566) $2 'is ' " " nZ
Sampled-data deviations in a vertical indicator with a stellar monitor "
Sep60. 155^). (PB 171 609) $3.00
Shop practice suggestions No. 3. May 60. 29p. (PB iVl' 251) '50" cenis '. ]h
Study and evaluation of portable aircraft maintenance hoisting equip-
ment. Febdl. 23p. (PB 171 614) 75 cents e m f - 700
Summary of pr^ent information on impact sensitivity of tiunium when
exposed to various oxidizers. Mar 61. 9p. (PB 161 239) 50 cents. .. . nui
Surface chemicil methods of displacing water and/or oils and salvaging
flooded equiiinent. Part I: Practical applications. Feb 61 24d
(PB 171 479) 75 cents .. ^' ' ' '
ty. 1961. lOlp. (PB 171 691) $2.50!!."!!.'!!!.'.'
738
722
Thermoelectric
MACHINERY. FABRICATION, AND ACCESSORY EQUIPMENT
Oiemical millin 5. Dec 60. 21p. (PB 171 112) 75 cents. . . .^
Development of in extrusion method for the production of wide profile
extrusions, r'olume I. Flat extrusion container. July 60. I84p.
Develqjment of in extrusion method for the production of wide profile
extrusions. Volume II. Photoelastic investigation and stress
analyses of flkt and rectangular extrusion containers. 1960 164d
(PB 171 568-21 $3.00
Steerable fifth wjieel. Jan 61 . 17p. ("re 171 6)" 3) "sO cents; .' ." .' ." ! ..W \ [ \ \ \ [ [ [ [ [ [ ] ] [ ] \ [ ['/[ ' ' ; 7 JJ
MATERIALS
90p. (PB 171
Improved vinylic
July 58. 49p
749
749
Development of c zone resistant polymers with low hysteresis. Sep 60.
578) $2. 25.
fillers for the reinforcement of GR-S type elastomers
(PB 171 579) $1. 25
Influence of high pressures and high temperatures on transformations
and coordinatuon in crystalline and vitreous ceramic materials
Nov 60. 48pJ (PB 171 595) $1.25
757
757
754
VI
Page
MATERIALS (con.)
Investigation of the fetigue properties of molybdenum under various
conditions of temperature, coatings and stress concentration.
Oct 60. 137p. (PB 171 617) $2.75 754
Low temperature research on materials. Feb 61. 28p. (OTS SB-451)
10 cents 753
Materials review (No. 8). Sep 60. 81p. (Pfi 171 612) $2.25 752
Nitrogen fluorides and their organic derivatives. A literature review.
Aug 60. 35p. (PB 171 252) $1 . 00 756
0-ring materials for Naval Ordnance applications. Aug 60. 51p.
(PB171 688) $1 . 50 753
Preservative treatment of wood for combat vehicles. Dec 60. 24p.
(PB 171 330) 75 cents 758
Study leading to the development of high temperature resistant
adheslves. 1960. 16p. (PB 171 565) 50 cents 753
Thermogravimetric analysis of the pyrolysis characteristics of poly-
mers. June 60. 17p. (PB 171 685) 50 cents 757
MATHEMATICS
Bionics symposium held in Dayton, Ohio, 13-15 September 1960.
Dec 60. 489p. (PB 171 258) $6. 00 765
Isopar, a new and improved symbolic optimizing assembly routine
for the IBM 650. July 60. 112p. (PB 161 577) $1.50 767
Sutistical development in life testing. Apr 59. 359p.
(PB 171 580) $5. 00 764
Tables of the incomplete gamma function of integral order. Nov 60.
49p. (PB 171 687) $1.25 763
MECHANICS
An analytical methocTfor the classification of flow areas of supersonic
wings. Aug 60. 109p. (PB 171 593) $2.50 770
Elastic and plastic stress equations for hollow cylinders and spheres
subjected to internal and external pressure. Feb 60. 41p.
(PB 171 684) $1. 25 768
Investigation of cone-cylinder bodies in the steady state spin mode
and magnus force effects orfa cone-cylinder body. Aug 60. 76p.
(PB 171 604) $2. 00 770
Shock spectra and design shock spectra. Nov 59. 18p.
(PB 151 932) 50 cents 769
METALLURGY
Application of high strength aluminum castings. Oct 59. 22p.
(PB 171 564) 75 cents , 777
Brazing for high-temperature service. Feb 61. 32p. (PB 151 108) $1.00 776
Design information on titanium alloys for aircraft and missiles.
Jan 61. 87p. (PB 151 104) $2. 25 779
Desulfurization by calcium inoculation improves properties of cast
steel. Jan 61. 21p. (PB 171 384) 75 cents 777
Effect of thermal-mechanical variables on the properties of molybdenum
alloys. Nov 60. 112p. (PB 171 597) $2.50 775
Factors influencing the fracture characteristics of high-strength steel.
Feb 61. 42p. (PB 151 106) $1.25 778
Heat treatment of meuls. Feb 61. 19p. (OTS SB -454) 10 cents 777
High temperature metallurgy and heat resistant alloys. Feb 61. 36p.
(OTS SB-452) 10 cents 777
Manual for beryllium prospectors. Jan 61. 40p. (PB 151 105) $1.00 779
Preliminary observations on the effectiveness of heat treatment for the
recovery of properties of irradiated steels. Feb 61. I6p.
(PB 171 188) 50 cents 778
Review of current data on the tensile properties of metals at very low
temperatures. Feb6l. 790. (PB 151 107) $2.00 776
Vll
METALLURGY (co<i.)
StatiBCical summar ' of mechanical -property data for titanium alloys.
Feb 61. 25p. (fB 161 237) 50 cents
Study of embrittlenient of high strength steels by ttie hydrogen isotopes.
Dec 60. 55p. (^ 171 253) $1.50
Si^ieralloy forgings
MISCELLANEOUS
Feb 61. 41p. (PB 161 236) 50 cents
Report of NRL Progfress. May 61. (PB 171 318) $1.25. $10.00/year
NUCLEAR PHYSICS AND NUCLEAR CHEMISTRY
Chemical effects of, radiation. Sep 60. 65p. (PB 171 572) $1.75
Gaseous xenon therinal neutron detector. Nov 60. 16p. (PB 171 616)
50 cents J
Study of tiie nature of free radicals in irradiated chemical systems.
). (IB
Nov 60. 65p.
PHYSICS
(Phase I ). Part
(PB 171 618) $6.
171 596) $1.75
Piff
779
778
776
806
784
783
781
A compendium of tke properties of materials at low temperature
Properties of fluids. Oct 60. 446p.
A compendium of ti|e properties of materials at low temperature
(Phase 1 ). Part in. Properties of solids. Oct 60. 294p.
(PB 171 619) $4.00.
A compendium of the properties of materials at low temperature
(Phase I ). Part III. Bibliography of references (cross-indexed).
Oct 60. I66p. ^ 171 620) $3.00
Field ion microecofy of iron whiskers. Oct 60. 26p. (FB 171 598)
75 cents j
Galvanomagnetic aiid magnetic properties of thin nickel -iron films.
Jan 60. Up. (PB 171 569) 50 cents
High temperature research (ceramics, gases, lubricants, plastics,
electrical and electronic equipment, etc.). Feb 61. 36p.
(OTS SB-453) iq cents
Infrared spectral emissivity of epical materials. Jan 61. 35p.
(PB171 254) $1.00
Peltier heat pumps --Application parameters and device possibilities.
Jan 61. lOp. (P$ 171 559) 50 cents..,
Prolonged space-waive fadeouts in trophospheric propagation. Feb 61.
75p. (PB161 584) $2.00.
Quarterly radio noise data, September, October, November 196Q.
Jan 61. 65p. (PB 151 377-8) $1.75,
Solid state researcl). Dec 60. lOOp. (PB 171 573) $2. 25.
Thermodynamic serial order of the metals at high temperature. July 60.
14p. (PB 171 567) 50 cents
SOCIAL SCIENCES
802
796
796
Guidelines for using
50 cents
for your convenience OTS order Wanks (Form TS-37) are available
on request from the OFFICE OF TECHNICAL SERVICES.
- i
via
U. S. DEPARTMENT OF COMMERCE
BUSINESS AND DEFENSE SERVICES ADMINISTRATION
OmCE OF TKHNtCAL SERVICES
35, No. 6
Pages 681-829
June 16, 1961
BIBLIOGRAPHY
Armed Services Technical Information Agency,
Arlington, Va.
POWER SUPPLIES. AN ASTIA REPORT BIBUOG-
RAPHY. Jan 61, 3l3p. 862 refs. AD- 249 100.
Order from OTS $5.00 PB 171 689
This bibliography contains entries from ASTIA's AD
colleaion (1953 to the present) which represent un-
classified reports without release limitation. The
majority of references are related to power supplies
for space research and technology; entries pertaining
to such areas as primary batteries for more conven-
tional application are included. A section on solar
radiation is also provided. References appear only
once although many may be related to more than one
category. Within each category, reports published by
Department of Defense contractors are hsted alpha-
betically by source, contract, and date; military re-
ports are arranged alphabetically by source and title.
(Author)
Office of Technical Services, Dept. of Commerce,
Washington, D. C.
CHINESE MAINLAND SCIENCE AND TECHNOLOGY.
Revised Mar 61, 21p. 380 refs. OTS Selective
Bibliography SB-442. i
Order from OTS JO. 10 OTS SB-442
Reports and translations are listed which deal with the
development of science and technology in China and the
effect of communism on the population engaged in these
projects. Reports are listed under the following
categories: Agriculture, Biological, Behavioral and
Social Sciences, Chemistry, Earth Sciences, Engi-
neering, Machinery, Materials, Metallurgy, [^ysics
«nd Mathematics, Research Techniques, and
Bibliography.
ASTRONOMY
Astrophysics
Harvard Coll. Observatory, Cambridge, Msss.
CLASSIFICATION OF SOLAR PROMINENCES. X.
1945, by Donald H. Menzel and F. Shirley Jones .
Scientific rept. no. 7 on Contract AF 19(604)4962.
Jan 61, 59p. AFCRL-TN-60-805.
Order from LC mi$3. 60, ph$9. 30 PB 154 585
A tabulation and analysis of the behavior classification
of prominences observed at the High Altitude Observa-
tory at Climax, Colorado, during the year 1945.
(Author) (See also PB 148 713)
Johannes Gutenberg-Universitat, Mainz (West
Germany.)
THEORETICAL INVESTIGATION ON ENERGY
GAIN BY ABSORFnON OF SOLAR RADIATION IN
CLOUDS, by Glinther Korb and Fritz MBller. Final
rept. on Contract DA 91- 591 -EUC- 1299. Nov 60,
15p. 16 refs. AD-247 839.
Order from LC mi$2. 40, ph$3. 30 PB 153 718
The transmission, absorption and reflection of solar
radiation in clouds consisting of water droplets and
soot particles is investigated. Dividing the diffuse
radiation field within the cloud into radiation fluxes ,
the equation of radiative transfer, as given by
Chandra sekhar, was simplified and solved analyti-
cally. Radiative transfer through clouds consisting
of water droplets was studied in deuil. For this pur-
pose cloud models of different thicknesses, heights
and optical properties were analysed. Computations
for clouds formed by pure soot particles or by mixed
droplets containing water and soot were started.
A brief review is given outlining the analysis of the
problem and describing the first obtained data ,
(Author)
681
BEHAVIORAL SCIENCES
Hunan Engineering
Air Force Comrro nd and Control Development Div . ,
Bedford, Mass .
DISPLAY SHARINCJ THROUGH COLOR FILTERING,
by Donald B. Devo^ and James S. Duva. Dec 60, 7p.
APCCDD-TN-60-61)-, AD- 249 788.
Order from LCmiii. 80, ph$ 1.80 PB 154 303
A method of displa i sharing through the projection of
several different d splays onto the same screen and
selecting the desirW display by viewing through an
appropriately colored filter is described, and several
applications of the [technique are discussed. (Author)
American Inst, for Research, Pittsburgh, Pa.
GUIDE TO HUMA^ ENGINEERING OF MINIATUR-
IZED EQUIPMENli by Edna M. Jones, Richard H.
Gaylord, and John p. FoUey, Jr. Final repc on
Contract DA 36-03p-sc-75054. 30 June 59, 72p.
11 rets. AIR-261-fe9-FR-202; AD- 225 306.
Order from LC mi$4.50. ph$12.30 -PB 154 522
Three interrelate^ solutions are proposed to a major
human engineering problem in miniaturization of
electronic equipment, that at providing adequate man-
machine linkage where space is extremely limited.
The solutions proposed are (a) reducing the tocal
swept volume or a^ea required for the human to use
control and displat instruments, (b) increasing the
volume available tor man-machine linkages, and (c)
reducing the number of linkages required. Section
I presents some fundamental concepts and definitions
appropriate to thejproblem. Section II describes a
procedure for hun^an engineering of miniaturized
equipment. Sectiofi III presents facts related to each
of the proposed solutions and includes aaual
measured swept areas for different type controls,
tables at data cm size recommendations, and related
specific design recommendations. (Author)
Scier ces
Behavioral
Div. , Wright -
DISCRIMINATION
WEIGHTLESS
Copeland. Rept
Dec 60, 25p. 4
Order from OTS
Lab. , Wright Air Development
AFB, Ohio.
OF DIFFERENCES IN MASS OF
by David W Rees and Nola K.
XI Human Factors in Advanced Flight.
WADD Technical rept. 60-601
75 PB 171 601
Pa tterson
OB ECTS,
r«fs
0
Absence of gravity results in the loss of many familiar
kinesthetic cues 4f weight and friction necessary to
man far object discrimination and manipulation. Man's
ability to discrimtnate small differences in mass as
opposed to small jdifferences in weight was studied.
Four weight seriis were used, each consisting of a
standard (1000. ioOO, 5000, or 7000 grams) and nine
comparison stimuli. Judgments for mass differences
were made with the same weights supported by com-
pressed air on aij air-bearing table. Thus, the fric-
tionless aspect of a weightless environment was simu-
lated. Results srow that the mean difference limen,
mean standard deviation, and Weber ratio (^S/S) for
each standard are much larger for mass than for
weight. Thus, to be detected under a weightless con-
dition, mass increments must be at least twice as
large as the weight increments required for discrimi-
nation in a normal weight-lifting situation. (Author)
Behavioral Sciences Lab. , Wright Air Development
Div. , Wright -Patterson AFB, Ohio.
SELF -MANEUVERING FOR THE ORBITAL WORKER,
by John C Simons and Melvin S. Gardner. Rept. on
Human Performance in Advanced Systems. Dec 60.
28p. 11 refs. WADD Technical rept. 60-748.
Order from OTS $0. 75 PB 171 611
Various self -propulsion and stabihzatlon systems have
been fUght-tested under weightless conditions. The
capability of these systems is reviewed. After analyz-
ing the basic motion and orientation problems of the
orbital worker, requirements for an optimum propul-
sion and stabilization system are discussed. (Author)
Biotechnology Lab. , U . of California . Los Angeles .
ARM PROSTHESIS RESEARCH. OBSERVER PRAC-
TICE. HUMAN THERMAL STUDIES. HUMAN
TRACKING, by John Lyman, Giovanni Boni and
others. Progress rept. on Contracts V1005M-2075,
Nonr- 233(49), AF 33(616)5402, and N 123(60530)
16361A. 15 June 60. 26p. Engineering Dept . rept. no.
60-50; AD -240 024.
Order from LCmi$2. 70, ph»4. 80 PB 149 444
Contents:
Fundamental studies to establish body control sites
for application to externally powered prostheses
Electromyographic studies
Surgical nerve replants
Functional isolation of muscle groups by training
Evaluation of existing externally powered pros-
theses
Physiological measurements of human thermal toler-
^ ance
Construction of a high transient rate environmental
chamber
Engineering analysis of biotechnical factors in con-
trol systems
Kinetic and kinematic analysis of prosthesis con-
trol motions
Sequential analyses of time-separated prostheses
control functions
Selected prostheses application studies
Double pectoral tunnel
Trans metacarpal amputation
Phostheses for the severely handicapped
Sensory-motor control and feedback investigations
Control engineering state of the an survey
Methods development and special design investiga-
tions
Effectiveness of elimination of displayed information
with observer practice increase
Interaction of display redundancy and display com-
plexity during training
Determination of a hierarchy of perceptual useful-
ness of geometrical cues in dial reading tasks
Development of a rationale for psychomotor tests
measuring performance decrennents in extreme
environments
Research on the perfornriance of human operators of
tracking instruments
682
Riysical Research Labs., Boston U. , Mass.
HUMAN ASPECTS OF PHOTOGRAPHIC INTERPRE-
TATION, by E. J. Robinson. Final rept, for
1 May 57-31 Aug 58 on Contract AF 30(602)1579.
Aug 58, declassified 1 June 59. 94p. 4 refs.
RADC-TR -59-27; AD-225 120.
Order from LC mi$5.40, ph$15.30 PB 150 916
The effects are considered of the variables of presen-
tation speed, target complexity, and work load on the
precisian with which the human observer is able to
decea and recognize the number of rectilinear figures
appearing in an array containing noncritical, curvi-
linear figures. The more important findings are: (1)
the system input variable at complexity of the visual
display, over which the system has little or no con-
trol, can be increased to a limit at which the system
breaks down and fails in the rapid, efficient processing
of information; (2) to a certain extent, the effects of
this breakdown can be overcome by increasing the
eaqxjsure or examination time allotted to the inter-
preter; (3) the efficiency of the system, in terms of
rate and amount of material processed, can be signif-
icantly increased by reducing the number or simph-
fying the type of discussions the initial interpreter
must make; and (4) slight increases in allotted exami-
nation time, combined with reduction in the number or
types of decisions the initial interpreter must make,
are by far the most effeaive in increasingthe efficiency
of the abstracting -processing system. A second study
is in progress to determine the optimal range of mag-
nification for detection and recognition of photographic
detail and to determine the upper limits of magnifica-
tion beyond which there is no improvement in per-
formance with respect to detection and recognition.
(Author)
Personnel and Training
Apphed Psychological Services, Wayne, Pa.
THE MEASUREMENT OF MOTIVATION AND ITS
RELATIONSHIP TO FLEET PROFIQENCY, by
Arthur I. Siegel and Douglas G. Schultz. Rept. no. 6
on Contract Nonr- 2279(00). June 60, 7lp. 9 refs.
AD-238 991 .
Onter from LC miM.50, ph$12.30 PB 148 774
In order to gain some insight into the relationship be-
tween a sailor's Naval attitudes and his fleet perform-
ance, the Sailors 's Naval Attitude (SNA) Inventory
was developed. The Inventory measures the sailor's
perception of certain job aspects purported to be im-
portant to industrial employee motivation. Five pan
scores and a total score are obtained through the in-
ventory's 61 statements . The Inventory was adminis-
tered to 414 Naval enlisted men distributed over five
pay grades and four ratings . Within the limits of the
»tudy, the following conclusions seem tenable: (1) low;
poaitive, statistically significant correlations exist
between total SNA scores and fleet performance as
measured; (2) in general, an increase in morale is
found in enlisted personnel as pay grade increases;
(3) on the average, TRADEVMEN have slightly more
favorable job attitudes than Aviation Fire Control
Technicians , Aviation Electronics Technicians , and
Aviation Electrician's Mates; (4) although there are
group differences in morale among ratings and pay
grades , there are even larger individual differences
within the various groups; (5) based on reliability con
siderations , it would be advisable to pay principal
attention to the total SNA Inventory score and to use
the part scores only for rough group comparisons;
and (6) the group differences in scores described and
the interrelationships with other variables studied
are reasonable and give some support to the con-
struct validity of the SNA Inventory. (Author)
Bureau gf Naval Personnel, Washington, D. C
DEVELOPMENT OF OFFICER CANDIDATE
BIOGRAPHICAL INFORMATION BLANK. I. VALIDA-
TION OF SOME EXPERIMENTAL INVENTORIES^ by
John J. La Gaipa. June 60, 26p. 8 refs. Technical
Bulletin 60-9; AD- 248 227.
Order from LC mi^.70, ph$4.80 PB 153 746
An attempt was made to develop a biographical infor-
mation blank to predict aspects of performance at
Officer Candidate School and at the subsequent duty
station of the junior officer. The results reported
here indicate that the performance of line officers
assigned to Shore billets could be predicted wth a
combination of two experimental inventories. While
the performance of line officers in Fleet billets could
not be predicted with the experimental inventories, it
was predicted with modest efficiency by OCS Peer
Ratings. (Author)
Carnegie Inst, of Tech. Graduate School of
Industrial Administration, Pittsburgh, Pa.
RECENT DEVELOPMENTS ON THE JOB SHOP
SCHEDUUNG PROBLEM, by Gerald L. Thompson.
ONR Research Memo. no. 69 on Planning and Control
of Industrial Operations. Contract [Nonr- 760(01)].
May 60, lip. 9 refs. AD-238 153.
Order from LC mi$2.40. ptt>3.30 PB 148 313
Current efforts on the j<* shop scheduling problem
are discussed and compared. The loading rule, the
simulation, and the heuristic methods are discussed
briefly. Emphasis is placed on the integral Unear
programming method and the Monte Carlo method.
In the scheduling problem, there are in commodities
to be produced and n facilities which perform ojsera-
tions on m during their production. The assumption
is made that the order in which the commodities are
to be processed by the machines is completely
specified.
Human Resources Research Office, George Wash-
ington U. , Washington, D. C.
THE DEVELOPMENT OF X UST OF MINIMAL
TRAINING GOALS FOR BASIC COMBAT TRAINING,
by Albert EUdn. [Rept. on Contract DA 49-106-qm-
IJ. Dec 60, 5^. 41 refs. Technical rept. 67;
AD- 248 634.
Order from LC ml$3.60, ph^.30 PB 153 865
The Basic Combat Training Program (ATP) was ana-
lyzed in relation to each of 17 supporting Army Sub-,
ject Schedules. Discrepancies between the ATP and
its referenced subject schedules were noted and
revisions suggested. On the basis of this analysis, a
list of minimum training goals was devised for each
683
subject pres«te4 In the report. These suggested
training goals corer the minimum knowledge and
skills needed by the individual basic combat
trainee. (Author
Psychology
I
Air Force Com|nand and Control Development Div. ,
Bedford, Mass.]
EFFECT OF VISUAL h40ISE ON THE JUDGMENT
OF COMPLEX FORMS, by John Coules, James S.
Duva, and George Ganem. Nov 60, 23p. 16 refs.
AFCCDD-TR-60t4O; AD- 249 423.
Order from LC rtii$2. 7a ph$4. 80 PB 154 063
Judgments of con^plexity of 20 Irregular shapes were
obtained with wai^ying visual noise and exposure dura-
tion. The number of sides of the forms account for
86^ of the rating variance. Form differences signifi-
cantly affected judged complexity scores. It may not
be assumed that irregular forms in a given polygon
category are equivalent in terms of complexity ratings;
nor can it be said that forms with the same number of
sides are necessarily equal. Visual noise affects
complexity ratings of irregular forms. The ratings
showed that form|B differentially interact with noise.
Exposure duraticti was not an important factor for
Judged complexiiv of forms. (Author)
I
Air Force Comtnand and Control Development Div. ,
Bedford, Massi
TARGET P0Sm|:»4 AS A CODING WMENSION, by
Raymond S. Nicker son and James S. Duva. Nov 60,
24p. 10 refs. Ai|CCDD-TR-60-41; AD-249 422.
Order from LC 4>i$2. 70. phS4. 80 PB 154 064
I
An experiment w^s conducted to determine the number
of discrete posit^ns of a dot in a square which can be
discriminated under a variety of conditions. The re-
sults indicate (l)[tbe number will be at least 64 when
the viewing time is 10 seconds; (2) within broad limits
this will be indepiendent of the size of the square and
the size at the dqt relative to the size of the square,
and (3) when exp^ure duration is extremely brief the
number of discritninable positions will be less and will
vary with size ofl square. Estimates are given for the
maximum numbe|- of discriminabie dot positions for
various display-^ize, exposure duration conditions.
(Author)
Applied Mathetiatics and Sutistics Labs. , Stanford
U.. Calif.
EXPERIMENTAU ANALYSIS OF A DUOPOLY SITU-
ATION FROM THE STANDPOINT OF MATHEMATI-
CAL LEARNING! THEORY, by Patrick Suppes and
J. Merrill Carlsinith. Technical rept. no. 30 on Con-
tract Nonr-225(U7). 17 June 60, 33p. 10 refs;
AD- 246 395.
Order from LC f i$3. 00, ph$6. 30 PB 149 521
A new theory of «luopoly is proposed which is derived
from recent worjc in mathematical learning theory.
The mechanism given here is formulated in terms at
the psychological notions at stimulus, response and
reinforcement, and the psychological processes of
stimulus sampling and conditioning. These concepts
yield a theory at oligopoly that has a flavor consider-
ably different from that at the theories based on con-
cepts of maximization and rational behavior. The
stimulus sampling formulation of mathematlcalleani-
ing theory employed is discussed and a simple choice
»ituation to which the theory has often been applied it
considered. The specific duopoly situation which Is
dealt with is described and the stimulus sampling
theory is applied in detail. The experimental setup is
discussed, and the results analyzed. (Author)
Applied Mathematics and Statistics Labs . ,
Stanford U., CaUf.
A GENERAUZATION OF STIMULUS SAMPUNG
THEORY, by Richard C. Atkinson. Technical rept.
no. 29 on Contract Nonr-225(17). 14 June 60, 23p.
4 refs. AD-238 823.
Order from LC nru$2. 70, ph$4. 80 PB 148 756
A natural generalization of the axioms for stimulus
sampling theory is introduced. The change leads to
a set of axioms which is equivalent to the axioms of
Suppes and Atkinson (Markov Learning Models for
Multiperson Interactions , Stanford Univ . Press ,
I960). This modification provides a context in which
experimental variables , such as reward nnagnitude
and nxKivation, can be viewed as determiners of be-
havior. Three groups of axioms are considered: (1)
the conditioning of stimuli , (2) the sampling of stim-
uli, and (3) responses .
Applied Mathematics and Statistics Labs. , Stanford
U. . Calif.
PROPERTIES OF THE ONE- ELEMENT MODEL AS
APPLIED TO PAIRED ASSOCIATE LEARNING, by
Gordon H. Bower. Technical rept. no. 31 on Contract
Nonr-225(17). 29 June 60, 35p. 5 refs; AD- 240 389.
Order from LC mi$3. 00, phJ6, 30 PB 149 522
An attempt was made to do for the one-element learn-
ing model what the Bush and Sternberg (Studies in
mathematical learning theory, Stanford University,
Press 1959) did for the single operator linear model; viz. .
derive an extens ive number of predictions from the axi-
oms. The learning model discussed Is one special case
of a large class of small element stimulus sampling
models. For this class at models, it is assumed that
the stimulus situation for the learning subject may be
represented by a small number of separate aspects or
elements and that each element Is conditioned to one or
another mutually exclusive responses available to the
subject. The Jubject is assumed to sample at random
one of the stimulus elements on each trial and makes
the response to which that sampled is conditioned. At
the termination of the trial one or another response li
reinforced and with probability ©the sampled element
becomes conditioned to the reinforced response, If it
was not already conditioned to that response. One
general consequence at these small element models U
that response probability can change only by discrete
steps, the number of steps determined by the number
of stimulus elements. The one-element model has
proved quite adequate In accounting for the data from
several experiments on paired-associate learning.
684
With the mathematic»l analysis at the one-element
model now in reasonably complete from, the ma-
chinery Is available for making detailed comparisons
at the linear model and the one-element model in their
predict kxis at experimental results. (Author)
Educational Testing Service, Princeton, N.J.
LEARNING PARAMETERS AND HUMAN ABIUTIES,
by Roger B. Allison, Jr. Doctoral thesis. Technical
rept. on Mathematical Techniques in Psychology,
Contracts Nonr-694(00). Nonr- 1858(15) and National
Science Foundation Grant G-642. May 60, 169p.
59 refs. AD- 245 523.
Order from LC mi$7. 80, ph$25. 80 PB 150 433
The Interrelationships among learning parameters
and also the Interrelationships between learning
parameters and measures of human abilities were ex-
plored. Thlneen learning situations were devised to
evaluate possible psychological organizations within
a domain of hunrian learning. The subject's perform-
ance on each learning task was expressed by a rate
parameter which described the average rate of learn-
ing, a curvature parameter which indicated whether
the learning was faster during the first or second half
of the situation, and an initial ability parameter.
Thirty-nine reference measures of aptitude and
achievement were used to assess potential relation-
ships between human abilities and learning. Two fac-
tor analytic techniques were employed to organize
the interrelationships of the variables Into more
meaningful dimensions based upon common factor
variances . The first technique was a conventional
multiple-factor analysis of the intercorrelation ma-
trix for the 28 learning parameters . The second fac-
tor analytic technique was Tucker's inter-battery
method which determined the number of factors in
common between the learning parameters and the ref-
erence measures. Two general coiKluslons were
drawn from the project: (1) the factorial organization
of the learning parameters was multidimensional;
and (2) measures of learning and measures of apti-
tude and achievement, which have generally been
treated experimentally as separate entities , have
factors m common with each other. (Author)
Louisiana State U . , Baton Rouge .
AN EVALUATION OF THE USE OF OBJECTIVE
SOOAL DATA FOR TRAINING PROBLEM-SOLVING
DISCUSSANTS, by Bernard M. Bass. Technical rept.
no. 22 on Contract N7onr- 35609. June 60, 22p. 5 refs.
AD- 237 439.
Order from LC mi$2. 70, ph$4. 80 PB 147 903
Five subjects discussed nine industrial cases on nine
succeeding weeks . During the discussions they were
given immediate public feedback on the extent each
participant agreed with each other member, how
much opinions were changed and how much individuals
accepted the group decision. Five control groups
operated in the same way except that they received
no feedback. Groups receiving feedback tended to de-
crease in initial agreenient while control groups In-
creased from week -to -week. Despite this, feedback
groups exhibited significantly greater post-discussion
acceptance of the group decision and coalescence of
opinion during discussion. These results probably
were due to the coercion produced in the feedback
group of knowing that one's opinions were to be re-
vealed to all publicly by the feedback procedure.
Following training , the members of the feedback
group teiKied to personally profit more in equivalent
test discussions than control group members show-
ing more gbin in individual accuracy but not group
accuracy. When groups composed of four untrained
and one trained subject were presented two new
cases to discuss, no significant differences between
trained and untrained subjects emerged except that
the relative successful leadership of untrained sub-
jects was greater . But , this difference depended
upon the particular problem discussed. (Author)
Louisiana State U. , Baton Rouge.
SOME ASPECTS OF ATTEMPTED, SUCCESSFUL
AND EFFECTIVE LEADERSHIP, by Bernard M. Bass.
Technical rept. no. 21 on Contract N7onr-3.5609
June 60, lOp. 4 refs; AD- 237 438.
Order from LC mi$l. 80, ph$l. 80 PB 147 902
Theorems from "Leadership, Psychology, and Organi-
zational Behavior", (Bass, 1960) provided hypotheses
for experimental tests. Experimental verification of
the following is reported: (1) a highly- significant corre-
lation of . 45 was found between initial accuracy and
relative successful leadership in 255 brief but more
effective discussions, while the correlation was only
. 07 in the 255 less effective discussiorfs: (2) a corre-
lation of 42 was obtained between esteem and relative
successful leadership in 25 groups with higher aver-
age effectiveness on the 10 problems, while the corre-
lation was . 22 in the 25 less effective groups; and (3)
those men whose self-esteem outweighed their esteem
exhibited a mean success as leaders of -. 14, while
those whose esteem was higher than their self-esteem
earned a successful leadership score at . 18. Signifi-
cant effects emerged when the differences in attempts
to lead were controlled. (Author)
Massachusetts Mental Health Center, Boston.
SENSORY MIPRIVATION AND PERCEPTUAL LAG.
bySanfordJ. Freedman. Rept. on Biophysics Re-
search, Contract A F 33(616)5663. Dec 60, Up. 9 refs
WADD Technical rept. 60-745.
Order from OTS $0. 50 PB 171 610
The effects ctf a 3- hour sensory deprivation session
upon perceived visual speed were studied with (a)
homogeneous, diffuse -light visual stimulation; (b)
blackout; and (c) randomly changing visual stimulation.
Randomizing the spatio-temporal distribution of visual
inputs greatly enhances the apparent decrease in visual
speed which Is produced by the two homogeneous con-
ditions. Regularizing the nature of the visual Input
apparently diminishes this "perceptual lag" effect.
Synchronization and de- synchronization of discharge in
the neurovisual system may be the mechanism in-
volved. Serious distortions in speed perception de-
velop in one-half hour. The effects are cumulative with
distributed exposure to sensory deprivation conditions.
(Author)
685
Psychological Lab. , U. of Southern California
[Los Angeles]
AN INVESTIGATION OF SYMBOUC FACTORS OF
COGNITIC^J AND CONVERGENT PRODUCTION, by
J. P. Guilford, P. R. iMerrifield and others. Rept.
no. 23 on Studies of Aptitudes of High- Level Person-
nel, Contract N6onr- !38(10). Apr 60, 27p. 14 ref s .
AD- 237 753.
Order from LC mi$2 70. ph$4. 80 PB 148 005
A factor -analytic study is discussed in which specific
hypotheses as to new factors were generated entirely
by the structure of intellect. The investigation was
linnited to 7 factors tlat pertain to symbolic content,
2 of which had previously been indicated but needed
confirnwtion and 5 of which were thought to be poten-
tial new factors whenithe study was initiated. Seven
reference factors wefe included in the study to help
clarify the factorial sjtructure. A banery of 20 new
experimental tests aifl 10 marker tests was em-
ployed. The correlation matrix was analyzed by
Thurstone's centroid h^ethod, yielding 15 factors, 13
of which were readilyi interpretable after onhogonal
rotations by the Zimraerman method and 2 of which
were residuals . The y reference factors came out as
expected, in relation to their respective marker
tests . The 2 symbolic factors —cognition of symbolic
relations and convergent production of symbolic
transformations werawell confirmed. Four of the
five predicted new faqtors were clearly demonstrated
— cognition of symbolic units , cognition of symbolic
classes , cognition of Symbolic implications , and con-
vergent production of symbolic systems. The failure
of the expected factor of convergent production of
symbolic units to em«rge led to new thinking with re-
gard to abilities conc(>rned with convergent produc-
tion of units , with ne\r hypotheses more closely in
line with structure-of -intellect properties . In gen-
intellect appears to serve well
as a source of hypoth<Jses of undiscovered factors
and as a means of systematic interpretation of the
abilities that can be located within its categories .
(Author)
Psychometric Lab.,
Chapel Hill.
THE DESIGN OF A
Toda (Hokkaido U,).
Contract AF 49(638)7^9
Order from LC mi$1480,
tl
Examples illustrate
ficial robots (such as
theory which synthesi
within psychology
U. at North Carolina.
'UNCUS- EATER, by Masanao
ifesearch memo. no. 7 on
Jan 61, lOp. AFOSR-256.
ph$1.80 PB 154 462
e belief that the design of ani-
the fungus -eater) will lead to a
tes many problem areas
Psychometric Lab. , U. of North Carolina, Chapel
Hill.
THE PREDICTION 0# CHOICE UNDER TWO
MODELS FOR CONTINGENT AND COMPOUND
PAIRED COMPARISONS, by James J. McKeon, Emir H
Darrf 11 Boclt. Rept. on Contract
Oct 61), 6p. AFOSR TN-60-1308.
. 80, ph$1.80 PB 154 459
Shuford, and R
AF 49(638)729.
Order from LC mill
Radiobiological Lab. , U. of Texas, Austin.
A SHOCK -AVOIDANCE APPARATUS EMPLOYING AN
INSTRUMENTAL MANIPULATORY RESPONSE, by
William H. Melching. Aug 55, 8p. 5 refs. Rept.
55-25.
Order from LC mi$1.80, ph$1.80 PB 155 575
This report released for sale to the public 19 Apr 61.
A ahock-avoidance apparatus employing an instru-
mental manipulatory response for the behavior testing
of monkeys is described. Suggestions and recom-
mendations are made with respect to the design and
function at this type of apparatus. (Author)
Small Groups Research Center, Washington U. ,
St. Louis , Mo.
MORALE AND THE COMPETENCE OF THE
LEADER IN AUTOCRATIC STRUCTURES, by
Roben L. Hamblin, Keith Miller, and James A.
Wiggins . Technical rept. no. 4 on Contract Nonr-
816(11). June 60. 22p. 15 refs. AD-241 139.
Order from LC nU$2.70, ph$4.80 PB 149 904
An experiment is reported which was designed to test
the hypothesis that in autocratic structures morale
varies directly with the relative competence of the
leader with respect to the group's task. The hypothe-
sis was supported on the basis of two analyses; first
the average correlations of several measures of mo-
rale and manipulated and perceived competence were
.38 and .37 respectively. Secondly, in a factor analy-
sis both manipulated and perceived competence were
correlated .75 with an underlying dimension of mo-
rale. It was noted however, that three intervening
variables confounded and perhaps accounted for
pan of the relationship. Finally, an unanticipated
third factor indicated what happens when a leader is
perceived as being perverse. To the extent he is
successful, he will be disliked; to the extent he will
be the object of direct aggression. These latter re-
sults give some support to the Miller-Dollard cathar-
sis hypothesis. Furthermore, they are somewhat
consistent with Bales' findings about task and socio-
emotional leadership. (Author)
Virginia U., Charlottesville.
EXPERIMENTS IN VERBAL BEHAVIOR. 1. GROUP
REINFORCEMENT OF INDIVIDUAL RESPONSE, by
Arthur J. Bachrach, Douglas K. Candland, and Janice
T. Gibson. Rept. on Contract Nonr-474 (8). Apr 60,
43p. 14 refs. AD-235 445.
Order from LC mi$3. 30, ph$7. 80 PB147.530
Attempts were made to control verbal behavior in
small group situations . Three participants , two of
whom were actually experimenters , were asked to
attempt to translate Chinese and American Indian
ideograms into English. During the discussion the
experimenters attempted to alter the resf)onse rate of
the subject with different types of reinforcement and
with different schedules . The findings indicate that
verbal behavior in a small group situation is subject
to the same laws of conditioning chat have been found
to hold for single individuals and for subhumans . The
findings also suggest hypotheses concerning the in-
fluence of the verbal behavior of different participants
686
in a small group situation on the verbal behavior,
both in terms of conformity and deviation, of an indi-
vidual participant. (Author)
Washington U. , St. Louis, Mo.
AN EXPERIMENTAL STUDY OF COMPETENCE
KUD TIME IN GROUP AS DETERMINERS OF STA-
TUS AND GROUP EXPECTANCIES, by E. P. Hollandei
Technical rept. on Variables Underlying Group Expect-
ancies and Leadership, Contract Nonr-816(12).
June 60, lip. 5 refs. AD- 239 919. i
Order from LC mi$2.40, ph$3.30 - PB 149 324
Descriptions of a person's task competence and dura-
tion of time in a group were manipulated to study
effects upon willingness to accept chat person in a
position of authority, the measure of status. One hun-
dred and fifty-one subjects at both sexes were given a
brief description of a person they were to imagine as
a member of a group co which they belonged. Eight
descriptions were created as experimental treatments
by pairing either one at the terms "been in group for
some while" or "new to the group" with just one of
four degrees of competence described by the terms
"extremely capable performer in group' s activity, "
through "capable performer, " to "average performer,"
or "poor performer. " Each subject received only one
treatment among the eight possible combinations of
terms; a response was then elicited on a seven-point
scale indicating how willing the subject would be to
have Che described person in a position at authority
within the group. Both variables yielded significance
in the predicted direction: a descending mean score for
willingness to accept authority was found to follow the
descending levels of competence, with the mean for
"been in group for some while"" uniformly higher than
chat for "new to group" at each level. In a second
phase at the experimem, subjects indicated whether
cheir evaluation oi the described person would go up
or down if that person were co display each of eighc
behaviors, one by one. These were contrived to be
nondirectional in themselves. (Author)
BIOLOGICAL SCIENCES
Florida U. Coll. of Agriculture, Gainesville.
FINAL REPORT, by Warren S. Silver. Rept. on Con-
tract Nonr- 256 1(00). 20 June 60, 32p. 16 refs.
AD- 239 476.
Order from LC mi J 3.00, ph$6. 30 PB 148 966
Examination of cells of Nitrobacter by electron mi-
croscopy has revealed that protuberance of the
daughter cell from the parent has more the appear-
ance of budding than binary fission. Ferrocytochrome
c and nitrite react aerobically at acid pH co form a
ferrlcytochrome c-NO complex. The effects of pH on
this reaction and on the inhibition of heterotrophic
respiration by nitrite are strikingly similar. Oxy-
henioglobin reacts with nitrite at acid pH to form a
hemlglobin-NO complex. Whether nitrate was also a
product of the reaction was not ascertained. (Author)
Pennsylvania U. [Philadelphia]
PROPERTIES OF BIOLOGICAL MATERIAL, by
Herman P. Schwan. Annual progress rept. for 1 Jan 59-
31 Dec 59 on Contract Nonr- 551(05). 6 June 60, 14p.
8 refs; AD-238 177.
Order from LC mi$2. 40, ph$3. 30 PB 148 219
An analysis of the internal electrical properties of
erythrocytes was conducted. It relates the erythro-
cytes internal impedance to electrolytes, proteins and
ion binding properties at hemoglobin. Instrumentation
was developed for the determination of the dielectric
properties of frozen blood. The relationship between
protein hydration and microwave conductance of
protein solutions was Investigated. Thermal do-
simeters, useful for the determination of high frequency
field fluxes, were analyzed. A theoretical study con-
cerned with the electrical properties of ellipsoids,
surrounded by confocal shells, was undertaken in re-
lation with problems ccMicerned with the interpretation
of the electrical properties of biological cells and
galvanotaxic effects of high frequency fields on micro-
organism. (Author) (See also PB 143 850)
Washington U. , St. Louis , Mo. School of Medicine.
CORTICAL ACTIVITY AND COGNITIVE FUNCTION
ING, by Laveme C. Johnson (Navy Medical Neuro-
psychiatric Research Unit), George A. Ulett and
others. Oct 60, 15p. 23 refs. AFSAM rept. 60-75.
Order from LC mi$2. 40, ph$3. 30 PB 154 593
This study was designed to investigate the effects o^
photically induced electroencephalographic disruption
on cognitive functioning. Twenty- eight male subjects
were selected for study. Fourteen of these had
shown EEC activation and 14 had failed to activate
during several previous exposures to intermittent
photic stimulation in this laboratory. All subjects
had histories which were negative for head Injury,
seizures , or seizures in other family members .
Each subject was examined twice . During , and in the
absence of, photic stimulation his performance was
evaluated on the following cognitive tasks: memory
for stories , paired associate learning, digit span,
serial 7's , and arithmetic problems. The results in-
dicated that: (1) Tne degree of EEC disruption in re-
sponse to photic stimjlation, and measured by the
electroencephalograph, was not related to quality of
performance on any of the tasks used. (2) Marked to
extreme disruption of EEG activity during the actual
learning of each task did not impair recall or mem-
ory of that material . nor did it interfere with the
cognitive processes involved in serial 7's or solving
arithmetic problems . (3) The distracting, and some-
times unpleasant, flickering light was noc associated
with consistent impairment of performance. Rather,
marked individual differences in flicker-induced im-
pairment of cognitive functioning were found. (4) Im-
pairment in test performance during photic stimula-
tion was not related co manifesc anxiety. (Author)
687
Anatomy and Physiology
Arctic Aeromediial Lab. , Ladd APB, Alaska.
CARMOVASCULAR EFFECTS OF REFEEDING
STRESS FOLLOWtNG STARVATION. IX. METABO-
UC RESPONSES TO REFEEDING IN THE RAT:
PREUMINARY SlIUDIES WITH CM-LABELED GLU-
COSE , by G . S . S^ith and B . Connor Johnson .
Nov 60. lip. I refj. Technical note AAL-TN-60-20;
AD- 249 801. I
Order from LC miE2. 40, ph$3. 30 FB 154 168
The research proj^t was undertaken to determine
what, if any, are t^ principal factors in the diet
which nny induce ^r aggravate cardlo-vascular stress
during refeeding fallowing starvation. Tills repon de-
scribes the first pliase of experimentation with a
group of ncwly-ac(Juired pigs , and summarizes some
observations of blood pressures in the rat as in-
fluenced by diet. lt\ addition, this repon summarizes
the completed asp^ts of a study concerning metabolic
responses to the stress of excessive glucose influx
and a supplemental study of the eff^ts of starvation
and refeeding upon changes of weight and gross com-
position of heart, kidneys, and livers. (Author)
North Carolina U. School at Medicine, Chapel Hill.
THE EFFECTS A^ CHARACTERISTICS OF IN-
CREASED RESPIRATORY DEAD SPACE IN DOGS, by
Thomas B. Bar netr and Richard M. Peters. Rept. on
Physiology Research, Contraa AF 33(616)6261.
Dec 60, 14p. 2re&. WADD Technical rept. 60-660.
Order from OTS $^. 50 PB 171 607
Artificial breathin| apparatus such as oxygen masks
involves added external respiratory dead space. In
dogs with permanent tracheostomies, chronic increase
in dead space has been maintained with lengths o€
0.75-inch interior diameter vinyl plastic tubing. A
dead space of 20-30 cc./kg. is not tolerated for more
than hours. The afnount of mixing and air streaming
within this tubing 4nd in tubing of 0.5-inch Interior
diameter and 1 . 5-inch interior diameter was deter-
mined. There waa very little mixing in the two smaller
tubes but, in the I4rge one, the amount of mixing was
significant. (Author)
Pennsylvania U. , Philadelphia.
THERMAL AND METABOUC RESPONSES OF THE
ALACALUF INDIANS TO MODERATE COLD EXPO-
SURE, by Harold f Hammel. Rept. on Research on
Peripheral and Central Control of Mammalian Tem-
perature, Contract AF 33(616)6306. Dec 60, 49p.
3 refa. WADD Technical rept. 60-633.
Order from GTS $^.25 PB 171 606
The oxygen consuitiption and body temperatures erf nine
adult, male Alacaluf Indians were measured while ex-
posed to moderate cold for 8 hours. The metabolic
rate o* the averagi Indian was 60 percent higher than
ti>e average BMR df the white man at the beginning at
the night and fell only slightly throughout the night. A
few bouts at shlvef ing increased the metabolism in
burats during the tight. When comparing the Alacaluf
Indiana with other ethnic groups exposed to the same
testa, three patterns appear: (a) the unaccllmatlzed
nun starts tils metabolic rate at a near basal
level and increases it markedly as his body tempera-
ture falls, (b) the Central Australian aborigine starts
with a metabolic rate near basal and slides slowly
downward as his reaal and skin temperatures fall to a
little lower values than the white man's, and (c) the
Alacaluf Indian starts with a very high metabolic rate
which declines slightly as the rectal temperature falls
following the panern at the white man, and the skin
temperatures of the trunk fall a little more than the
white man's while the foot temperature falls a little
less. (Author)
Physics, Engineering and Chemistry Corp. , Boulder,
Colo.
A STUDY OF THE EFFECTS OF IONIZED AIR ON
BEHAVIOR, by W. Dean Chiles (Behavioral Sciences
Lab. , Wright Air Development Div. ) John M. Cleve-
land, and Richard E. Fox. Rept. on Psychological Re-
search on Human Performance, Contract
AF 33(616)5839. Nov 60. 24p. 38 refa. WADD Tech-
nical rept. 60-598.
Order from OTS $0.75 PB 171 600
The effea on human behavior of an atmosphere con-
taining excesses of unipolar ions was investigated.
Fifteen subjects were tested on a complex mental task,
an additional fifteen performed a vigilance task, and
twenty subjects indicated their attitudes through
marking an adjective check list while exposed to five
levels of air ionization. The ion conditions for each
study were varied from a high excess of positive Ions
through a medium excess of positive ions, low ion
(neutral), medium negative, and low negative. None of
the differences found among the ion conditions for
these tests were statistically significant. (Author)
Pisa U. Owly)-
REPORT FOR THE ACADEMIC YEARS 1957-58
AND 1958-59. Rept. on Contracts AF 61(515)1125
and AF 61(052)107. 10 Feb 60, lOp. 50 ref s .
AFOSR-TN-60-498; AD- 242 270.
Order from LC mi$ 1.80, ph$ 1.80 PB 150 338
Brief reports are given on EEC synchronizing struc-
tures of the lower brain stem; ascending reticular
system vs. extralemniscal sensory pathways; visual
habituation and the central control of the sensory in-
flow; and the prc^Iem at adrenergic mediation in the
ascending reticular system.
Radiobiological Lab. , U of Texas, Austin.
CORRELATION OF SKELETAL GROWTH AND
EPIPHYSEAL OSSIFICATION WITH AGE IN MON-
KEYS, by Donald B. Gisler. Stephen G. Wilson, Jr. "
and Gerrit L. Hekhuls. Nov 60, 4p. 4 refs. AFSAM
rept. 61-11.
Order from LC ml$l. 80, ph$l. 80 PB 154 594
A method has been developed for estiniating age in the
rhesus monkey by skeletal radiograph. Some thirty-
five ossification changes have been used as age -esti-
mating criteria. Females generally meet the matura-
tion criteria 3 to 5 months earlier than males. Data
presently available relate to monkeys up to 48 months
of age; however, the study will be followed until com-
plete skeletal maturation takes place. (Author)
688
School of Aviation Medicine, [Brooks AFB] Tex.
A (COMPARATIVE STUDY OF THE BEHNKE AND
THE HARVARD STEP- UP TESTS FOR PHYSICAL
FITNESS, by Peter V. Karpovich. Ai^ 53, I5p. Proj.
no. 148, rept. no. 1;AD-135 602.
Order from LC mi$2. 40, ph$3. 30 PB 155 486
This report released for sale to the public 19 Apr 61.
Portions at this report will not reproduce well.
Sunford U. School of Medicine, Calif.
THE INFLUENCE OF MAGNESIUM AND PYROGENS
ati TEMPERATURE REGULATION, by Victor E.
Hall, Ronald Grant and William J. Whalen. Rept. on
The Metabolic Activity of the Central Nervous Sys-
tem as it Affects the Thermostatic Activity of the
Body, Contract W33-038-ac-14986. Aug 51, i26p.
121 refs. AF Technical rept. no. 6682.
Order from LC mi$6.30, ph$19.80 PB 155 297
This report released for sale to the public 31 Mar 61 .
Magnesium chloride depresses body temperature by
iftcreasing heat loss in warm environments and by de-
creasing heat production in cold environments . This
action is exerted directly on the temperature regulat-
ing centers of the anterior hypothalamus . Sodium
fluoride in low doses raises the body temperature.
Sinre magnesium activates and fluoride inhibits the
enzyme enolase, the reaction catalyzed by this
enzyme in the cells of the hypothalamic centers ap-
pears the most likely possibility for a "key metabolic
reaction" which our hypothesis postulates to be a fac-
tor in temperature regulation. Pyrogenic substances
evoke fever, not by a specific "resetting of the body
thermostat" , but by a general disturbance of auto-
nomic lunctions , including those concerned with ten>-
perature regulation. Elevati'on of the osmotic pres-
sure of the plasma raises the level at which body
temperature is regulated. This mechanism may play
tn imponant role in the genesis of dehydration fever.
(Author).
Biochemistry
Aviation Medical Acceleration Lab. , Naval Aii*
Development Center. Johnsville, Pa. '
™E ISOLATION AND PARTIAL PURIFICATION OF
A PROTEIN- BOUND ENDOGENOUS SUBSTRATE
FOR OXIDATIVE PHOSPHORYLATION FROM LIVER
MITCX>10NDRIA. by H. W. Shmukler and B. David
Mis. Rept. no. 13 on Task MR005. 15-0002. 7.
31 Dfec 60. 18p. 9 refs. NADC-MA-6026.
Order from LC mi$2. 40, ph$3. 30 PB 154 468
Preparations of crude mitochrome under certain con-
ditions were found to accelerate oxidative phospho-
rylation in mitochondria. This property was contained
in a heat stable factor bound to the mitochrome. The
factor was separated from the protein moiety and
partUlly purified. (Author)
Massachusetts Inst, at Ttech. . Cambridge.
SYNTHESS OF PEPTIDES, by John C. Sheehan. Prog-
ress rept. on Contract Nonr- 1841(15). June 60, 9p;
AD- 237 967.
Order from LC ml$l. 80 ph$l. 80 PB 148 214
By the use of_N, N]-dlsopropylcarbodimide8 oriso-
butyl-chloro-formate (as cyclizing agents), the cycli-
zing agents), the cyclizatlon of N;trityl-L-8erli^ (I),
phthaloyl-L-threonine (II), and phthaloyl-D, L-p-hy-
droxyvallne was effected readily at room temperattirv
to give the p- lactones (III), (IV) and (V); (C^Hg]^
^^-CH-C0-0-C"2 <'°)- P»»N-CH-00-0-CH-C"3
(IV. PhN-cH.co-0-C <^>2 <V). ^^e^-^ I* '
phthaloyl. Cyclization at I with N-N'-dilsopropyl-
carbodiimide at room temperature led to III in 15%
isolated yield; the mol wt of III, by the Rast method,
was 309 (theory = 329). eliminating the symmetrical
anhydride as a possible structure. Cyclization re-
actions of I at concentrations varying between 2 and
0. 5% gave no Improvement in yields of IIL T^^atment
of III with benzylamine gave benzylamide in 93%yield.
Upon treatment of III with L-alanine methyl ester
hydrochloride in the presence of triethylamine,
N-trityl-L-seryl-L-alanine methyl ester was obtained
in 66% yield with no sign of racemizatlon, cyclization
of II to IV was readily effected in 40% yield by the use
of isobutyl chloroformate. The IR spectrian of IV was
in accordance with the p- lactone structure. Bands at
1775 cm-1 and 1725 cm-' (characteristic of a phthal-
oyl group) and at 1820 cm-^ (assignable to the p- lac-
tone carbonyl) were evident. The mol wt of IV de-
termined by Isothermal distillation was 245 (theory-
231). Treatment of IV with dry methanol led to the
corresponding methyl ester. Identical in every re-
spect (IR, mp, mixed mp and optical rotation) with an
authentic sample. Attempts were also made (1) to
form an amide bond by reacting an isonltrile, carboot-
ylic acid, and amine and (2) to cyclize etamycin acid
to etamycin.
Naval Missile and Astronautics Center, Potet Muni.
Calif. ^
STUDY OF METAL ION BINDING OF MONO-
NUCLEOTIDES, OLIGONUCLEOTIDES AND POLY-
NUCLEOTIDES by W. C. Gillchrlest. 1 Dec 60. lip.
21 refs. Technical memo. no. NMC-TM-60-63.
Order from LC mi$2. 40, ph$3. 30 PB 153 844
The nucleosides and nucleotides (mono, di, and tri-
phosphates) have been studied in the ultraviolet region
of the electromagnetic spectrum for base-base and
base- "small ion " interactions such as proton, alkali,
alkaline earth, and transitional cations. The results of
the study demonstrate that the alkali and alkaline earth
elements do not influence the ultraviolet spectrum of the
nucleosides and nucleotides at any given pH. The
transitional elements give specific transitional species*
and purine base interactions at specific pH's. The re-
actions of specific transitional elements which gave
precipitates with nucleotides were observed with a given
polynucleotide and found not to precipitate but to give a
hypochromic effect for the specific cations considered.
689
iiJ
M^icai Specialties and Equipment
School at Aviarti>n Medicine, Brooks APR Tex.
APPLICATION OF MINIATURIZED ELECTRONIC
MVICES TO THE STUDY OF TOOTH CONTACT
IN COMPLETE VENTURES, by Allen A. Brewer and
Donald C Hudsoi. Oct 60, lOp. 3 refs. rept. 61-12.
Order from LG nji $1.80, ph $1.80 PB 154 263
Previous attempti to study, by electrical current, the
Incidence of tootn contact in chewing were handicapped
by wires leading from the mouth. A small radio trans-
mitter, built intojcomplete dentures to send a signal
when teeth of opposing arches meet, eliminates this
problem. Varioup occlusal schemes and relationships
are tested over ling periods. The signal is recorded
continuously so t|at masticating and nonmasticating
contacts, both wiping and sleeping are monitored.
These are compared relative to time sequence, du-
ration, and characteristics. The contact at teeth
varies with the iridividual, the type of occlusal surface,
the articulation, pnd the type of food. (Author)
Medicine [Brooks AFB, Tex.]
OF PRODUCTS OF HUMAN
AND THEIR POSSIBLE
DENTISTRY . by David F . Mitchell .
refs. Proj. no. 410, rept. no. 6;
School of Aviation
AN INVESTIGATION
BLOOD FRACTIONATION
USE IN
28 July 45, 6p
AD- 21 1 267.
Order from LG iiu$l .80. ph$l .80
This repon releiised for sale to the public 31 Mar 61
tians
Surgical extrac
nwlars were
foam and thromb i
wounds , and i
materials were
cellaneous ext
thrombin in this
to the patient
and is particularly
to excessive
operative swe
series , but thes
Thus , the value
tions of consi
the thirty cases
alveoalgia. The
not appear to be
ucts in this shor
contraindication
sulfonamides in
bin, but the va
questionable
tlu;
Birmingham U
PROTEIN
Annual technical
14 Nov 60, on
6p. 3 refs; AD-
Order from LC
PB 154 427
involving impacted lower third
on thirty individuals . Fibrin
n were placed in the resulting
closure was effected. These
o employe^ following sixteen mis-
The use of fibrin foam and
series was not in any way injurious
hemostatic effect is remarkable
useful in those individuals prone
True evaluation of post-
and pain is impossible in this
factors do not appear to be reduced.
i)f such a procedure following opera -
trauma maybe limited. Five df
were treated for "dry socket" or
incidence of such occurrences did
influenced by the use of these prod-
series . There was apparently no
to the use of penicillin and various
:onjunciion with the foam and throm-
of these drugs in this series was
r)
per formed
mbin were
mniediate
2 Is
ractions
Tie
henorrhage.
jlliiig
i(
ider able
(A lithoi
'athology
(Gt. Brit. )
ABSOIItPTION IN SPRUE, by J. M. French,
status rept. A. 1/1960, 15 Nov 59-
C^mract DA91-591-EUG-1322. [I960]
48 232.
ini$1.80. ph$1.80 PB 153 714
Contents:
General background of '^N protein absorption studies
Studies with ^N labelled protein with adult coeliac
patients
Studies with patients with pancreatic dysfunction
Boston U. School of Medicine. Mass.
COOLING AND REWARMING UNDER PROTECTION
OF ANTIARRHYTHMIC AGENTS, by Evangelos T
Angelakos and Albert H. Hegnauer. Rept. on Physi-
ology of Flight, Contract AF 33(616)6767. continuation
of Contract AF 33(616)3805. Oct 60. 12p. 12 refs.
WADD Technical rept. 60-617.
Order from OTS $0. 50 , PB 171 602
Certain antiarrhythmic compounds previously effective
in preventing ventricular fibrillation (VF) during pro-
gressive hypothermia were tested for overall protection
during cooling and subsequent rewarming. Cardiac
failure occurring during rewarming was completely
prevented by previous rapid digital ization. Sympatho-
mimetic amines were also effective in this respect.
The phenothiazines, chlorpromazine and mepazine, and
the new antiarrhythmic, amoiriphene, were testedfor
their activity against hypothermic VF. Only chlor-
promazine exhibited a significant effect, but this was
not superior to that of quinidine. (Author)
Royal Hospital for Sick Children, Edinburgh (Scot. )
STUDIES IN THE PO^ TRAUMATIC PATIENT.
SODIUM BALANCE STUDIES NITROGEN UTILISA-
TION FAT ABSORPTION ASCORBIC ACID REQUIRE-
MENT, by Anne B. Sutherland, Christine G. Colver
and others*- Annual technical status rept. for
1 Nov 59-31 Oct 60 on Contract DA 91-591 -EUC-1313.
1 Nov 60, 45p.
Order from LC mi$3.30, ph$7.80 PB 153 720
School of Aviation Medicine, Brooks AFB, Tex.
SOME THEORETIC ASPECTS OF THE USE OF
INERT GASES IN SEALED CABIN ENVIRONMENTS,
by Emanuel Roth. Nov 59, 19p. 40 refs. Rept. 59-152;
AD- 239 975.
Order from*LC mi$2.40, ph$3. 30 PB 155 574
This report released for sale to the public 19 Apr 61.
The physical analysis of decompression bubbles within
the body was reviewed in an attempt to provide a
working model for seleaion erf several inert gas com-
binations in sealed cabins. The maximum bubble size
and symptom frequency after decompression appear to
be proportional to a gas factor (solubility in oil^ x dif-
fusion coefficient in oil / solubility in water). The
inert gases - helium, neon, argon, krypton, xenon,
and nitrogen — were compared with this relationship in
mind. Helium appears to be 4 times and neon 1 4
times more effective than nitrogen in minimizing
symptoms after decompression. Review of the litera-
ture on diving and experimental studies vfiih inert
gases corroborated the advantages of helium and neon
over the others. The side effects of these gases and
logistic considerations were discussed and over-all
factors governing the use of inert gases in (^rational
sealed cabins were outlined. (Author)
690
Texas U. Medical Branch, Galveston.
FINAL REPORT, by C. M. Pomerat. Rept. for
1947- 196a on Contracts N6onr-266, T. O. 5 and
Nonr- 1598(01). 15 June60, 12p. 34 refs . AD-239 361 .
Order from LC mi$2. 40, ph$3. 30 PB 148 415
Brief summaries are given of research in antiorgan
sera, cellular responses to microbial agents, cellu-
lar responses to chemical injury, cytopathology of ait
pollution and radiation, and basic cell physiology and
pathology.
Pharmacology and Toxicology
Army Chemical Research and Development Labs
Army Chemical Center , Md .
ACUTE TOXIOTY OF A MIXED AMINE FUEL, by
Maurice H. Weeks, Sidney Rothberg, and Theodore
0. Downing. Oct 60, 15p. 11 refs. CRDLR 3033
Order from LC mi$2.40, ph$3.30 PB 153 845
Range-finding toxicity tests of MAF-1 indicate that
its vapor is similar in toxicity to 1 .1-dimethyldydra-
zine (UDMH). MAF-1 produced effects similar to
UDMH in exposed animafs and produced death at
about the same concentration levels . MAF-1 is con-
sidered to be slightly less hazardous than UDMH be-
cause of its lower volatility. Cutaneous application
of MAF-1 showed that large amounts would be re-
quired to cause death. However, very low doses
caused irritation of exposed skin areas . Futhermore.
MAF-1 caused severe eye damage and permanent cor
neal opacity . The precautions and safety practices
now in use for handling UDMH should be supplemented
by additional measures to prevent any skin or eye ex-
posures to MAF-1. (Author)
Army Chemical Research and Development Labs.,
Army Chemical Center, Md.
CHRONIC TOXICITY STUDIES ON 2-PAM AND
EA 1814 IN DOGS AND RABBITS, by James W. Cook,
Joseph L. Colbourn and others. Sep 60. 19p. 18 refs.
Technical rept. CRDLR 3026.
Order from LC mi$2.40, ph$3,30 PB 153 841
Chronic toxicity studies on 2-PAM and on EA 1814 have
been made on dogs and rabbits. These oximes were
administered intravenously, 5 times a week, over a
period of 6 to 8 weeks. No toxic signs or hematolog-
ical changes were observed in the animals, and no
lesions were found after gross and microscopic
pathologic examination. Three hours after injection of
2-PAM (30 mg/kg)and EA 1814 (10 mgAg) the
oximes were no longer present in blood plasma of dogs.
Skeletal muscle analyses for these oximes were
negative 20 hours after the last injeaion. (Author)
Army Chemical Research and Development Labs
Army Chemical Center, NW.
ESTIMATED SPEED OF ACTION OF GB VAPOR
FOR DEATH AND VARIOUS DEGREES OF INCA-
PAQTATION IN MAN, by Paul Cresthull, Milton K.
Chnstensen, and Fred W. Oberst. Jan 61, 47p.
« refs. CRDLR 3050; AD-249 116.
Order from LC mi$3.30, ph$7.80 PB 154 438
691
Human estimates for the speed of action of GB
(isopropyl methylphosphonofluoridat'e) vapor have been
derived, based on experiments in six animal species
over a range of responses from 1% to 99% of the popu-
lation. Families of curves estimating the speed of
action of GB vapor at various Ct exposures for death
and various degrees of incapacitation in man, ex-
posed for 30 seconds , 2 minutes , and'lO minutes are
presented. Using these curves , one may read the
cumulative per cent effect at any time of occurrence
for any particular Ct exposure. The total expected
response at any Ct may also be read from these
curves. (Author)
Army Chemical Research and Development Labs. ,
Army Chemical Center, Md.
RESEARCH STAFF CONFERENCE. HEALTH
HAZARDS OF MILITARY CHEMICALS, ed. byKeithH.
Jacobson. Oct 60, 26p. 11 refs. CRDL Special pub.
2-34; AD-246 155.
Order from LC mi$2. 70, ph$4. 80 PB 153 843
This report realeased for sale to the public 4 Apr 61.
The discussion at a research staff conference on Health
Hazards of Military Chemicals held on 17 June 1960 is
reviewed. Investigations reviewed were: cardiotoxicity
of boron hydrides, oxygen toxicity, toxicopathology of
pyrotechnic fumes, skin sensitization by military
chemicals, and hygienic standards on brief exposure to
propellant vapors. Some of the individual discussions
represented progress reports on studies not yet
completed. (Author) (See also PB 146 460)
Washington U. [St. Louis, Mo. ] School of Medicine.
THE EFFECT OF METHAMINODIAZEPOXIDE ON
ACTIVITY, FOOD AND WATER CONSUMPTION,
BODY WEIGHT, HEART RATE AND RESPONSE TO
STIMULATION, by John A. Stern, David G. McDonald,
and William W. Hahn. Technical rept. on Contract
Nonr-816(06). June 60, 14p. 3 refs. AD-240 721.
Order from LC mi$2.40. ph$3.30 PB 149 336
Investigations were conducted on the acute and chronic
effects of methaminodiazepoxide. Results indicated
that the drug produced following effeas: (1) resting
heart rate in drug animals was higher than in controls
after acute injeaions, but was generally lowered by a
series of chronic injeaions; (2) heart rate and stabi-
limeter responses to bell stimulation tended to be de-
creased by acute and chronic injections; (3) open field
and activity wheel measures of activity level were
both lowered by acute and chronic injections; and (4)
water intake was increased in both conditions, whereas
body weight was increased by acute and decreased by
chronic injections. No effea on food intake was noted
^Author)
Radiobiology
Armour Research Foundation, Chicago, III.
EFFECT OF CHRONIC WHOLE -BODY RADIATION
ON BLOOD ENZYMES, byErvinJ. Hawrylewicz.
Rept. for 1 July 59-30 June 60 on Health Hazards of
Materials and Radiation, Contraa AF 33(616)6491.
Nov 60, 44p. 17 refs. WADD Technical rept. 60-662.
Order from OTS $1.25 PB 171 608
The objective of thil program was to determine the
effect at radiation exposure on the activity of plasma
enzymes and coenzymes. Young, adult, nule,
Spragtje-Dawley racs were exposed to four levels of
cotMh-bO gamma radiation ranging from 0. 3 to 300
r/week for 26 weeks. During this time the rats were
bled by heart puncture six times and their blood ana-
lyzed for enzyme activities. The mean activity d
each enzyme from $t least five rats at each level was
statistically compated to the nriean activity erf a simi-
larly treated, nonirradlated control group and the
change noted. Oet; the 26-week exposure the serum
activities of coenzyme A, aldolase, gluco«e-6-phos-
phate dehydrogenasfe decreased and those of glutamic
oxalacetlc transaminase and diphosphopyridlne
nucleotide from rats radiated with 30 and 300 r/week
Increased. Change* in the remaining enzymes and
coenzymes measured, namely, catalase, lactic acid
dehydrogenase, carbonic anhydrase, cocarboxylase,
and flavin adenine (jinucleotide. did not follow statis-
tically significant trends. Red and white blood cell
counts and hemoglcfcln determinations at the specified
periods throughout the 26 weeks showed typical radia-
tion response. (Author)
Chesapeake Bay Inst. , Johns Hopkins U. [Annapolis]
Md.
SOME RESULTS OF STUDIES ON THE UPTAKE
OF RADIOACTIVE WASTE MATERIALS BY MA-
RINE AND ESTUAiUNE PHYTOFLANKTON ORGAN-
ISMS USING CONTINUOUS CULTURE TECHNIQUES,
by W. R. Taylor. Mpt- on Contracts AT (30- 1)1477
and Nonr- 248(54). |une 60. 76p. 21 refs . Technical
rept. no. 21; Refeifence 60-3; AD- 243 974.
Order from LC ml$4.50, ph$12.30 PB 150 654
The advantages of ^he use of continuous culturing techi
niques for the studi of the uptake of radioactive ma-
terials by phytoplaikton organisms were discussed.
The chemostat, a system in which the cell population
as well as the chertiical environment can be main-
tained constant, appears to be ideally suited for this
purpose. A brief summary of the theory of the opera-
tion of the chemosipt was presented. (Author)
\4ae»i
Naval Medical Research Inst. , Bethesda, Md.
THE USE OF SMALL LABORATORY ANIMALS IN
MEDICAL RADIATION BIOLOGY. PART 1. APPLI-
CATICW OF A 2O0 K.V.P. X-RAY THERAPY UNIT
TO LETHAL OOSf. STUDIES, by Friedrlch ElUnger,
Jasper E. Morgan, | and Francis W. Chambers, Jr.
Vol. 10. p. 145-1^. 30 Apr 52. 34p. 5 refs. Re-
sewch rept. on Prbject NM 006 012.04.43.
Order from LC mi$3.00, ph$6. 30 PB 155 374
This report released for sale to the public 10 Apr 61 .
A critical study of irradiation techniques and appara-
tus has been undertaken, with particular reference to
the effective appliqation at conventional X-ray therapy
equipment. Major ^emphasis has been assigned to de-
tails ot accurate p^slcal dosimetry, with the goal d
consistently repro^cible inter- laboratory comparison
at experimental data. By automatic regulation of input
Une voltage fluctuations to less than 1 . 0%, plus mix! -
mum care in nunupl control and timing, individual
calibration readings are reproduced by the same
Victoreen chamber to the order of * 0. 5%. Approxi-
mately uniform simultaneous exposures are obtained
in animal containers designed for twelve mice, and
for two guinea pigs. The radiation quality is variable
from H. V. L. of 2.3 mm. Al to 1.8 mm. Cu. The
incident backscaner becomes constant in each case
after approximately a 10 cm. thickness of Masonlte,
while the harder radiations approach an H. V. L. near
0. 25 nun. Cu after traversing large thicknesses of
Masonlte. (Author)
Naval Medical Research Inst. , Betheada, Md.
THE USE OF SMALL LABORATORY ANIMALS IN
MEDICAL RADIATION BIOLOGY. PART II. CORRE-
LATION OF PHYSICAL FACTORS WITH THE BIO-
LOGICAL EFFECT PRODUCED IN TOTAL BODY
IRRADIATION, by Friedrlch Ellinger, Jasper E.
Morgan, and Francis W. Chambers. Jr. Vol. 10,
p. 181-206. 15 May 52, 24p. 6 refs. Research rept.
on Projea NM 006 012.04.44.
Order from LC mi$2.70, ph$4.80 PB 155 375
This report released for sale to the public 10 Apr 61.
Studies have been performed on the effects of two
types of X-rays (200. 140 K.V.P. ) on male albino
Swiss mice of the Institute strain. Physical data pre-
sented in the first part of this work were the guiding
principles for the various exposures. By applying a
quarantine period at at least 14 days prior to the use
of animals in these experiments, meticulous after-
care of irradiated animals, precise recording of all
pertinent data, and rigid control o* exposure condi-
tions, it became possible to accomplish a high degree
of accuracy of biological dau. As indicated in the
paper, at the LD50 level, even dose differences of
±2. 5 per cent could be distinguished biologically
under special conditions. Good agreement between
physical data and biological effeas has been demon-
strated by means of a study of the influence of back-
scatter on mortality rate and in the comparison of
two types of irradiation. Preliminary results are
presented indicating that the exit dose appears as a
suitable parameter for evaluation of the relative
lethality of two different types of X-rays in one
animal species. (Author)
Public Health Service. Washington, DC.
RADIOLOGICAL HEALTH HANDBOOK. Rev. ed.
Sep 60. 474p. 54 refs. PR 121 784-R
Order from OTS $3. 75 ™ ^^^ ^^* ^
Contents:
Glossary
Physical, chemical, and mathematical data
Radioisotope, decay, and radioassay dau
Radiation protection data
Table of isotopes
References and index
PubUc Health Service, Washington, D. C.
RADIOLOGICAL HEALTH DATA. VOLUME 2,
NO. 2. Monthly rept. Feb 61, 54p. 8 refs.
Order from OTS $1.00, $9.00 yr. PB 161 371-11
692
Contents:
Section I. - Air
Public Health Service radiation surveillance network
Naval Research Laboratory radioactivity measure-
ments
Seaion II. - Food, other than milk
The annual and geographical influences on the
strontium -90 intake in Japanese diet
Seaion III. - Milk
Public Health Service milk monitoring program
Section IV. - Water
Public Health Service national water quality network
Section V . - Other data
External gamma activity (September 1960)
Radioactive contamination of jet aircraft
Off-site animal investigation project
Human bone sampling program of the Canadian radio-
aaive fallout study program
Long term training activities of the Division of
Radiological Health
Environmental levels of radioaaivity at Atomic En-
ergy Commission installations
(See also PB 161 371-10)
Public Health Service, Washington, D. C.
RADIOLOGICAL HEALTH DATA. VOLUME 2,
NO. 3. Monthly rept. Mar 61, 58p. 2 refs.
Order from OTS $1.00, $2.50yr. PB 161 371-12
Contents:
Seaion I. - Air
Public Health Service radiation surveillance network
Radioactivity measurements in air
Seaion II. - Food, other than milk
High consumption of foods
Seaion III. - Milk
Public Health Service milk monitoring program
Radioaaivity in milk (July-August 1960)
Seaion IV. - Water
Public Health Service national water quality network
Seaion V. - Other data
External gamma aaivity (Oaober 1960)
Soil data
Environmental levels of radioaaivity at Atomic
Energy Commission installations
Factors contributing to the occurrence of radio-
nuclide levels market milk
Michigan survey of medical radiation exfxraure
during pregnancy
Natural lead- 210 content of man
Radiation intelligence network
Radiation survey report
(See also PB 161 371-11)
Radiobiological Lab. , U. of Texas, Austin.
INACTIVATION OF AQUEOUS SOLUTIONS OF
LACTIC ACID DEHYDROGENASE BY IONIZING
RADIATION, by Clyde M. Williams (School of Aviation
Medicine) and George M. Krise. Apr 58, 9 refs.
AFSAM rept. 58-76.
Order from LC mi$1.80, ph$1.80 PB 155 576
This report released for sale to the public 19 Apr 61.
The activity of rabbit muscle laaic acid dehydro-
genase was reduced by Co^ gamma rays - the in -
•alvation was found to be an exponential funaion of
the radiation dose. At 2 x 10"8 molarity the G value
was on the order of 0. 02. With increasing concentra-
tion the G value increased continuously to about 0. 2 in
the range of 1 x 10"5 to 8 x 10"5. No effect on the G
value was obtained either by oxygenating or deoxy-
genating the solution before irradiation. (Author)
School of Aviation Medicine, Brooks AFB, Tex.
PROMPT EFFECTS OF HIGH-LEVEL IRRADIATION
ON ANIMAL METABOLISM, by James P. Ellis, Jr. ,
Robert T. Qark, Jr. and others. Jan 60, lOp. 12 refs.
AFSAM rept. 60-17; AD- 233 167.
Order from LC mi$l. 80, ph$l. 80 PB 154 592
Blood acid -base related components and free amino
acids in plasma, spinal fluid, and five tissues were
measured in rhesus monkeys given whole-body irra-
diation doses of 500, 2, 500, 5, 000, 10, 000, 20, 000.
and 30, 000 r. All samples were collected within 4 hr
following the exposure. A trend of a more acid blood
pH was found in animals receiving 5, 000 to 20, 000 r,
and this became more apparent in the 30, 000 r group.
A rise in blood lactic acid seemed to parallel the
change in blood pH. A consistent change was not found
in blood pyruvate. A correlation of the more acid
blood pH and the rise in blood lactate with reductions
in the arterial CO2 tension and plasma CO2 content
indicated that a metabolic acidosis was greater than a
respiratory alkalosis resulting from increased pul-
monary ventilation. A reduction in plasma glucose
and an increase in plasma uric acid occurred in the
irradiated animals. A definite relationship was found
to exist between these altered levels, the postirradia-
tion interval, and the total dose given. A twofold in-
crease in the free amino acid content of plasma was
found in animals receiving 5, 000 r. Of the 7 amino
acids detected in spinal fluid, an elevated glutamine
level appeared to be the only consistent change and
was primarily responsible for the net increase found
in the total amino acid fraction. (Author)
CHEMISTRY
Minnesota U . School of Chemistry, Minneapolis .
FINAL REPORT, by William N. Lipscomb. Final
rept. on Contract Nonr-710(23); continued on Contract
Nonr- 1866(42), [1960] 3p. 12 Refs. AD- 233 781.
Order from LC mi$ 1.80, ph$ 1.80 PB 153 784
A summary of work on molecular structure of boron
compounds .
Rochester U., N. Y.
THE INTERNATIONAL INSTITUTE ON QUANTUM
CHEMISTRY, by Alben Gold. Rept. no. 7 on Con-
tract AF 49(638)432. Sep 60, 15p. 51 refs. AFOSR-
TN- 60- 1392; AD- 248 801.
Order from Ldmi$2. 40, ph$3. 30 PB 153 903
693
Anot ^al Chemistry
Naval Ordnance Ijest Station, China Lake, Calif.
RAPID DETERMINATION OF ACETONE IN
PENTAERYTHRIT(t)L TRINITRATE BY GAS CHRO-
MATOGRAPHY, by] Everett M. Bens and Donald H.
Stewan. 24 Nov 5^. 16p. 7 refs . NOTS TP 2371;
NAVORD rept. 70l(4; AD- 231 855.
Order from LC mil 2.40. ph$ 3. 30 PB 154 210
A ra^d gas chromAtographic method has been de-
veloped for the quafititative determination of acetone
in pentaerthritol trinitrate in which errors due to
water and other components in the sample are elimi-
nated. Accurate allquots of the viscous pentaerythri-
tol trinitrate can b^ taken after dilution with absolute
ethanol. Since the nonvolatile penuerythritol trini-
trate is retained within the Injection system, suitable
corrections for thei solubility of acetone with increas-
ing amounts of pen|aerythritol trinitrate retained in
the instrument are made. Although this requires fre-
quent standardization between determinations and
periodic cleaning of the injection system, the method
requires only ten minutes per sample in a* series of
determinations . Samples of pentaerythritol trinitrate
containing up to 2% acetone have been determined with
a standard deviatioi of ± 0.05%. (Author)
Pennsalt Chemicals Corp. , Wyndmoor, Pa.
IX4PROVED METHODS OF USING THE CHEVENARD
THE RMOBA LANCE TO MTERMINE THERMAL
STABILITIES, by jj R. Soulen and I. Mockrin. Tech-
nical rept. no. 12 (in Contract Nonr- 2687(00).
4 Feb 60, 20p. 8 r^fs. AD- 232 942.
Order from LC mii2.40. ph$3. 30 PB 153 163
Several piroblems i^i evaluation at thermal stability <rf
materials using the| Chevenard thermoba lance are dis-
cussed. These are} Maintaining an inert atmosphere,
prevention of cond^sation on the crucible support
which results in false weighing, determination of the
true decomposition
temperature and measurement of
true sample tempei ature. Solutions to these are pre-
sented. (Author)
School of Aviatior Medicine, Brooks AFB, Tex.
MODIFICATION OF THE TRIHYDROXYINDOLE
METHOD FOR THp ESTIMATION OF EPINEPHRINE
AND NOREPINEPH^NE IN URINE, by Ralph P.
Feller, Aug 60, SpL 13 refs. Rept, 60-71.
Order from LC miil.80, ph$l .80 PB 154 264
A procedure developed from existing technics for the
estinution of epinephrine and norepinephrine in urine
has been described;. The precision of the method,
based on the average difference between rwenty-eight
sets of duplicate daerminations , indicated a coeffi-
cient of variation of 8.0 percent (S.D. , .058) for epi-
nephrine and a coe^icient of variation of 9.1 percent
(S.D., .148) for nqr epinephrine. Essentially, quanti-
tative recoveries resulted from the addition of a mix-
ture of known anxxints of epinephrine and norepineph-
ieries of 45 normal subjects , a
.82; range, 0.1 to 3.7) and 0.6
(S.D., .28; range (k.2 to 1.4) gamma per hour was
found for norepinephrine and e^Hnephrine,
respectively. (Author)
rine to urine. In a
mean of 1.5 (S.D.
Organic Chemistry
British Co«on Industry Research Association.
POLYMERS RELATED TO CELLULOSE. Final tech-
nical rept. no. 3, 1 Dec 59-30 Nov 60, on Contract
DA 91 -591 -EUC- 1341. Dec 60, 85p. 24 refs.
Order from OTS $2. 25 PB 171 574
The effect of pH and temperature on the condensation
of oxycellulose with aqueous urea has been examined.
Under the most favorable conditions about 1.5 mole-
cules of urea are introduced per anhydro-oxyglucose
unit, initial uptake of urea being rapid. The reaction
is acid -catalyzed and reversible. Variations in 'bak-
ing' conditions have also been studied for the high-
temperature reaction previously reported. Condensa-
tion of oxycellulose with thiosemicarbazide is cata-
lyzed by acid, but complete substitution cannot be
achieved even at 50*^. Both nitro-aminoguanidine and
m-nitrobenzhydrazide react with oxycellulose. Thio-
semicarbazones of periodate-oxidized methyl 4, 6-0-
benzylidene-a-^-gluco8ide (OMBG), adipaldehyde, and
glutaraldehyde have been prepared. Two compounds
of unknown structure resulted from reaction erf OMBG
with urea in ethanol, one containing two, and the other
three, molecules erf combined urea. Structural in-
vestigations on the product obtained by treating OMBG
with phenylhydrazine have shown it to be methyl
4,6-6-benzylidene-3-deoxy-3-phenylazo-D-glucoside
(or -D-alloside), a new kind of sugar derivative. The
rate of oxidation of trans-cyclohexane-l. 2-diol in
mixtures of water and dimethylformamide decreases
sharply when the latter constitutes more than about
50% by volume of the solvent system. (See also
PB 145 240) . . '
Bureau of Mines , Bartlesville, Okla.
INFRARED SPECTRA OF ORGANIC COMPOUNDS IN
THE REGION 15-35 MICRONS: THIRTEEN
ORGANIC OXYGEN, NITROGEN, SULFUR, AND
SlUCON COMPOUNDS, byC. A. Frenzel. D. W.
Scon, and J. P. McCullough. Technical note on
Contract CSO 59-9. Nov 60, 19p. Rept. of Investiga-
tions 5658; ARPA Order no. 24-59, Task 3;
AFOSR TN-60-1221; AD-246 090.
Order from LC mi$2.40. ph$3.30 PB 153 036
This report presents the sjjectra of the following
thirteen compounds: Tetrahydrofuran, l-methyl-
pyrrole, piperidine, 2-methylpyridine. 3-methyl-
pyridine, 2-propanethiol , cyclopentanethiol .
2-methyl-2-buunethiol, 3,3-dimethyI-2-thiabutane,
cyclohexanethiol , cyclopentyl-1-thiaethane, 2,4-di-
methyl-3-thiapentane, and hexamethyldisiloxane.
(Author)
Cornell U.. Ithaca, N. Y.
NONIONIC DETERGENTS IN NONAQUEOUS SOL-
VENTS 2: CRITICAL OPALESCENCE OF BINARY
UQUID MIXTURES: THE SYSTEM POLYSTYRENE-
CYCLOHEXANE, by P. Debye and H. Coll. Technical
rept. no. 3 on Contract Nonr-40I(17). 30 June 60,
21p. 10 refs. AD-240 631.
Order from LC ml$2. 70. ph$4. 80 PB 149 895
A study was made of the theory that the critical opal-
escence of polymer solutions is analogous to the be-
694
bavior of systems of small nralecules near the coiiso-
lute point. The interaction range is related to famil-
iar parameters such as the radius of gyration of the
coiled- up molecule; other related factors include co-
hesive densities . Solutions of polystyrene fractions
in cyclohexane exhibited appreciable dissymmetries
d scattered intensity even when there was no critical
opalescence. The residual dissymmetfy was much
greater than could be accounted for by the size of the
polymer molecules , suggesting the presence of an
impurity. In a preliminary experiment, attempts
were made to establish the temperature at which
phase separation occurred in the polystyrene solu-
tions . Solutions were sealed in glass vials and sub-
merged in a water bath. Lowering the bath tempera-
ture caused an increase of turbidity, until finally
distinct schlieren indicated the point of phase separa-
tion. Generally, the phase separation changed only
with concentration so that this method was not suit-
able for finding the critical (consolute) concentration.
The latter was obtained from the dissymmetries of
scattered intensities , measured as a function of con-
centration at fixed temperature. Curves obtained in
this manner exhibited distinct maxima which defined
the critical concentration.
DePaul U., Chicago, HI. '
THIATRIAZOLES: AZIDO AND TWO GROUPS
ATTACHED TO THE SAME CARBON ATOM, by
Eugene Lieber and Cornelius B. Lawyer. Final tech-
nical rept. on Contract AF 49(638)474. 1 Dec 60,
119p. 40 refs . AFOSR-TR-60-163; AD-248 622.
Order from LC mi$6.00, ph$18.30 PB 154 269
Studies were made of the chemical and physical prop-
erties of 5-(disubstituted) amino-1 ,2,3,4-thiatri-
azoles . Comparisons are made with 5-amino and
5-(monesubstituted) thiatriazoles . Derivatives of the
thiatriazole ring system were synthesized by (1) the
reaction of nitrous acid with thiosemicarbazide and
its 4-alkyl or 4-aryl substitution products, and (2) the
reaction of aryl and alkyl isothiocyanates with hydra-
ffllc acid. The objectives of this investigation were
to examine synthetic routes to 5-(disubstituted)
amino- 1,2, 3, 4- thiatriazoles and to study the varia-
tions in properties with changes in the nature of sub-
itituents in aminottoiatriazole structure. A method
for the study of the pyroltic decomposition of the
thiatriazoles was developed. From the data obtained
comparisons were made relating the effects of sub-
itituents on the thiatriazole system. The relative
order of subilities decreased, In the following de-
scending order: (CH3)2N-; H2N-: (C6H5CH2)2N-;
(C6H5)HN-; and (CH3)HN-. Accordingly, the 5-(mono-
lubttituted) aminothiatriazoles appear less stable
than the disubstituted ones . The compound 5-chloro-
1,2,3,4-thiatriazole fl) was synthesized by the re-
action of thiophosgene and sodium azide. It was iso-
lated at 0 degrees and exploded violently when sub-
jected to shock. I was soluble in most common or-
ganic solvents and insoluble in water. It decomposed
generally around 5 degrees with HCL evolution.
Feltman Research Labe., Picatinny Arsenal, Dover.
N. J,
PREPARATION AND ANALYSIS OF PETRIN ACRY-
LATE, POLY -(PETRIN ACRYLATE), AND PEDN
MACRYLATE. by Delbert J. Cragle. jan6l, 2lp.
13 refs. Technical rept. FRL TR-15.
Order from LC mi$2. 70, ph$4. 80 PB 150 730
Petrin acrylate and pentaerythritol dimtrate diacrylate
(PEDN diacrylate) were prepared by the acrylation of
petrin and PEDN, respeaively. Poly -(petrin acrylate)
was prepared by the emulsion polymerization of the
monomer. A comprehensive source of analytical data
on petrin acrylate, poly-(petrin acrylate), and PEDN
diacrylate has been obtained and compiled. This data
Includes (1) a method of analysis of produaion -grade
petrin acrylate, (2) x-ray diffraaion data on petrin
acrylate and its polymer, (3) infrared spectrograms,
(4) physical constants, and (5) solubility data on the
three materials. In addition (6) impact, (7) explosion
temperature, and (8) stability data on petrin acrylate
and its polymer is included. (Author)
Florida State U. , Tallahassee,
SOME EXPERIMENTS WITH ORGANOBORON COM-
POUNDS, byj. E. Leffler, B. G. Ramsey, and
L . Todd . Technical rept . no . 1 on Contract Nonr-
2560(00). 1 June 60, 23p. 17 refs . AD- 239 043.
Order from LC mi$2.70, ph$4.80 PB 148 937
Dimesitylboron azide was prepared by the addition of
dimesitylboron floride (I) to NaNa, AICI3, and tetra-
hydrofuran. Hydrolysis of the reaction mixture pro-
duced a considerable quantity of mesidine via the
azide. Attempts to prepare dimesitylbenzylborane by
the reaction of I with p-methoxybenzylmagnesium hal-
ide resulted in 4,4' -dimethoxydibenzyl and mesityl-
borinic acid. The only identified products from at-
tempted preparations of dimes ityl(p-methoxybenzyl)
borane were 4, 4' -dimethoxydibenzyl and mesityl-
borinic acid. The Grignard reagent corresponding to
l-bromo-2methylnaphthalene was reacted with boron
trifluoride etherate in attempts to form bis(p-methyl-
a-naphthyl)boron fluoride. A white solid product was
obtained with a boiling point of 8OO to 85^/2. 5mm.
A mixture of mesitylboron mono- and dichloride was
obtained in the preparation attempt of dimesityl
azidoborane by the reaction of mesitylmagnesium
bromide and an ethereal solution of BCI3. Attempts
were made to obtain B-to-C and B-to-N rearrange-
ments by (1) the reactitwis of diazomethane with tri-
phenyl boron , diphenyldiazomechane with triphenyl
boron, and phenylboronic acid vrith hydrazoic acid,
(2) preparations of the triphenylazidoborate ion and
tri-_-naphthyIboron .
Florida State U. , Tallahassee,
SOME EXPERIMENTS WITH ORGANOPHOSPHORUS
COMPOUNDS, by I. Forsblad, U. Honsberg and
others . Technical rept. no. 2 on Contract Nonr-
2560(00). 1 June 60. 20p. 9 refs . AD-239 044.
Order from LC mi$2.40. ph$3.30 PB 148 938
The triphenylmethyl azide-triphenylphosphine com-
plex when decomposed (in the absence of air) in a
melt or in inert solvents at high temperatures gives
a tar from which only small quantities of crystalline-
materials can be isolated . Phenylazide reacts with
the complex to give N-phenyl triphenylphosphine to
give this phosphineimine. The complex in solution
has a strong IR azide band. Acids decompose the
complex at room temperature; the reaction is fast in
polar solvents in the pressence of the solid complex
but is slow when both the complex and the acid are in
solution in a non-hydroxylic solvent unless excess
acid is used . When the solid complex is dropped intp
an organic solvent containing low concentrations of
695
an mcid or iodine at toom temperature , there is a
rapid evolution of nitrogen . The decomposition of the
complex in acetic aqld is very rapid and has a half
life of Just a few miriutes at room temperature, even
though the azide itself doea»not decompoae. The de-
composition of the c^plex in dilute solutions of ace-
tic acid in chlorofortn, acetone, or benzene at their
reflex temperatures was too slow for convenient
measurement.
Florida U. Engine Ting and Industrial Experiment
Fla.
Station, Gainesville
FLUOROCARBON N
and R . D. Dresdner
I Oct- 31 Dec 60,
ARPA order no. 40-
AD-249 444.
Order from LC nu$ !. 40, ph$3. 30
F COMPOUNDS, by J. A. Young
Quarterly technical rept. no. 6,
on Contract DA 01-009-ORD-772 and
59, Tasks. [1961) 20p. 13 refs.
PB 154 251
Both NF3 and N2F4 vere reaaed with C2F5SF5 in a
flow system over Ni F pellets at atmospheric pressure
and at temperatures in excess of 500°C. Varying
yields of C2F6, SF4, SF6,*C4Fio, and C2F5NF2 were
noted in the NF3 rejctions depending on the
NF3/C2F5SF5 ratio^ while no C4F10 was found when
N2F4 was used although NF3 showed up as a reaction
product. Attemptedj reactions erf fluorocarbon amino
disulfides with flucnrjinating agents or with metals indi-
cate that these compounds tend to decompose by a re-
action which is the ieverse of their synthesis, giving
RpCN and SF4. Wlti HgF2, *n addua somewhat
similar to that founi with RfN-CF2 may be formed. A
fully acylated hydratine containing a seven -membered
ring has been made by reaaion of the mercury deriva-
tive of N, N'-hia<tri^uoroacetyl) hydrazine with
perfluoroglutaryl cliloride. Preliminary results on the
pyrolysis of {CF 3,COUN2 indicate that at 425° the re-
action probably proceeds via intermediate CFsCO-
radicals, which decompose to give mainly COF2 and
(-CF2-)n rather thap C2F6 and CO. (Author) (See also
PB 152 403)
Harvard U, Cambridge, Mass.
ORGANCTIN POLYMERS, by Rokuro Okawara and
Eugene G. Rochow., Technical rept. on Contract
Nonr- 1866(1 3). Feh 60, 26p. 15 refs. AD- 234 057.
Order from OTS $0 75 PB 171 571
Products of the rea<tion of dialkyltin dlhalides with
yxlium Silicates: A study was made of the precipitate
formed from the reaction of aqueous solutions of di-
methyltin dlchJorid^ and Na2Si03. The investigation
included a determination erf the nature of the larecipi-
tate, the effea of different organotin cations on its
properties, and the possibility of varying the size d
the silicate polyaniOn by varying the Si:Na ratio of the
Na 28103. Organostannosiloxanea from the co-hydrol-
yais of organotin and organosilicon halides: Attempes
to produce molecules with a simple Sn-O-Si backbone
by combining the units (CH3)2SnO and (CH3)2SiO re-
sulted in gradual pttecipitation of a highly dispersed
material thought tolbe organotin oxide. Dimethyltin
salts of carboxylic acids: Formic add did noe react
with dimethytin dichloride (I), but (CH3)2SnCKOOCH)
and (CH3)2Sn(OOCH)2 *ere obtained by the action of
sodium formate. Alcetlc add and I gave
(CH3)2SnCKOOCCH3) in poor yield; this compound
was obuined in better yield by using acetic anhydride.
Dimethyltin diacetate could not be obuined, but the
dimeric compound, tetramethyl-l, 3-dlacetoxydi-
stannoxytin and dlmethylchloroacetoxytin gave tetra-
methyl-l, 3- dichlorodistannoxane by hydrolysis. The
reverse reaction could be conducted by cleaving the
dichlorodistannoxane with formic or acetic acid. IR
spectra showed the presence erf carboxylate ions in
the solid state.
Instituto de Quimica Fisica (Spain).
THERMOCHEMICAL INVESTIGATIONS OF METHYL
SUBSTITUTED BENZOIC ACIDS, by M. Colomina.
R. Pferez-Ossorlo and others. Final technical rept.
no. 2, 1 Jan-31 Dec 60,on Contract DA 91-591-EUC-
1364. [1961] 33p. 30 refs.
Order from LC mi$3. Oa ph$6. 30 PB 154 465
The full series of the methylsubstituted benzoic acids
includes three mono-, six dl-,' six tri-, three tetra-,
and one penta - methylbenzoic acids. This report is a
continuation of study on the first nine members of tWa
series of compounds and contains the thermochemical
dau for five trl- and two tetramethylbenzoic acids.
Malllnckrodt Chemical Lab. , Harvard U. .
Cambridge, Mass.
CHEMISTRY OF THE METAL CARBONYLS. VIII.
PERFLUOROACYL AND PERFLUOROALKYL C«RIV-
ATIVES OF MANGANESE AND RHENIUM, by
H. D. Kaesz, R. B. King, and F. G. A. Stone. Rept.
on Contraa AF 49(638)518. Jan 61. 6p. 14 refs.
AFOSR-TN-60-1486; AD- 250 104.
Order from LC mi$l . 80, ph$l . 80 PB 155 453
Malllnckrodt Chemical Lab. , Harvard U. ,
Cambridge, Mass.
SPECTROSCOPIC STUDIES ON ORGANOMETALUC
COMPOUNDS. III. INFRA-RED SPECTRA OF
PERFLUOROVINYL METAL COMPOUNDS, by S. L.
Stafford and F. G. A. Stone. Rept. on Contract
AF 49(638)518. Jan 61, 19p. 23 refs. AFOSR-TN-
60-1485; AD- 250 104.
Order from LC mi$2. 40, ph$3. 30 PB 154 262
Tbe infra-red spectra al the compounds CF2:CFBF2.
CF2:CFBCl2, (CH3)2Sn(CF:CF2)2. (CH3)2Ge(CF:CF2)2.
(C2H5)2Si(CF:CF2)2. (CF2:CF)4Sn, (CF2:CF)3As,' and
(CF2:CF)2Hg have been recorded in the region
650-3500 cm.'* Most otthe observed absorption fre-
quencies have been assigned by correlation with known
spectra. (Author)
Mellon Inst., Pittsburgh, Pa.
MODELS OF ^TEREOREGULAR POLYMERS (PART
I). ^TEREOREGULARITY IN THE FREE RADICAL
POLYMERIZATION OF VINYL ACETATE (PART II).
ANIONIC POLYMERIZATION (PART III). DIMEN-
SIONS OF POLYMER CHAINS (PART IV) by R. D.
Spencer, MB. Fulton and others. Technical rept.
no. 3, I Sep-29 Feb 60 on Contract Nonr -2693(00).
(1960) 44p. 5 refs. AD- 234 483.
Order from OTS $1.25 PB 171 570
696
pennsalt Chemicals Corp. . Wyndmoor, Pa.
PHOSPHORUS- NITROGEN SYSTEMS. PART 1. THE
STRUCTURE AND AMINOLYSIS OF SOME PHOS-
PHORYL AZIDES, by F. L. Scott, R. Rlordan, and
p. D. Morton. Technical rept. no. 15 on Contract
Nonr- 2687(00). Apr 60, 23p. 20 refs. AD-237 151.
Order from LC mi$2.70, ph$4.80 PB 147 841
Some representative phosphoryl azides have been
synthesized and they possess infra-red absorptions
consistent with acyclic rather than cyclic structures .
The aminolyses of some such azides have been ex-
plored. In refluxing aniline tetraethylphosphordia-
midic azide (IX) undergoes extensive P- N bond cleavage,
with scission not only of the azide moiety but also
with loss of one diethylamine function to yield N,N'-
dlphenyl-N",N"-diethylphosphoric triamide (XII).
Tetraethylphosphordiamidic chloride undergoes a
comparable reaction in refluxing aniline to yield (XII).
With diethyl phosphoryl azide (H), again in aniline at
185°, not only does P-N bond cleavage occur but also
alkyl-oxygen scission, the unexpected product being
N-phenylphosphoramidic acid OQV). A similar syn-
thesis of XIV is achieved when diethyl phosphorcx;hlo-
rldate (XV) is used as the aminolysis substrate, and
also when 0,0-diethyl N-phenylphosphoramidate
(XVI)-- the nxjst probable intermediate in the aniline
solvolyses of XI and XV -- is employed. These re-
actions constitute a new route to N-arylphosphora-
midic acids . The mechanism of the process is dis-
cussed. (Author)
Pennsylvania State U. , University Park.
RADICAL REARRANGEMENTS IN BROMOALKYL
RADICALS, by Philip S. Skell. Technical rept. on
Contract AF 49(638)457. 2 Feb 61 , 4p. 7 refs .
APOSR-60. AD-250 896.
Order from LCmi$ 1.80, ph$ 1.80 PB 154 564
Plastics Lab. , Princeton U: , N. J.
STEREOSPECIFICITY AND DIELECTRIC PROPER-
TIES OF POLAR POLYMERS, by H. H. Zabusky and
H. A. Pohl. Rept. on Contract DA 36-039-8C-78105.
15 Aug 60, 52p. 50 refs. Technical rept. 59A;
AD- 243 746.
Order from OTS $1.50 PB 171 563
A method of determining stereoregularity in polar high
polymers by dilute solution dielectric measurements
is Investigated on polyvinyl isobutyl ethers, polyethyl
acrylaies, and poly-p-chlorostyrenes of differing
steric forms. In all cases no significant differences
were found in the dielectric constants or dlpole mo-
ments of the different steric forms of the same poly-
mer. This was generally true erf the relaxation times
»nd distribution of relaxation times of the polymers
also. The results are compared to those on poly-
methyl methacrylates where differences were found,
and it is concluded that the degree of hindrance to ro-
tation about the carbon -carbon bonds of the main chain
and the degree of steric repulsion to positioning of
side groups are the determining factors as to whether
differences in dielectric properties will be observed.
A simple and approximate method of predicting rela-
tive polarizations and dipole moments of stereospe-
dfic vinyl polymers based on dipole -dipole and repul-
sion energies is presented. It is concluded that the
method ol determining stereoregularity In polar poly-
mers by dilute* solution dielectric measurements is not
generally applicable, but the method is a valuable tool
for gaining insight into the flexibility of polar polymer
chains. (Author)
Technische Hochschule, Karlsruhe (West Germany).
CATALYTIC ISOMERIZATION OF PARAFFIN BASE
HYDROCARBONS IN THE C10-C20 RANGE, by
Helmut Pichler. Final technical rept. no. 1, 1 Nov 59-
31 Oct 60, on Contract DA 91-591-EUC-1307.
28 Nov 60, 47p. 4 refs . AD- 247 838.
Order from LC mi$3. 30, ph$7. 80 PB 153 717
TTie relative retention times of normal and isoparaf-
fins containing 8 to 16 carbon atoms p)er molecule
were investigated by using a Perkin Elmer Fractom-
eter. Separation of the paraffin by gas chromatogra-
phy was accomplished by also using a Linde 5A molec-
ular sieve. 2,5-Dimethyl paraffins were prepared
with 10 to 16 carbon atoms per molecule. Cloud
points were determined for mixtures of paraffins and
ist^raffins with 15, 16, and 17 carbon atoms . Cata-
lytic isomerization tests were made with n-cetane;
the reaction was analyzed by gas chromatography,
with a n- paraffin- urea extract and a Kogasin fraction,
and with catalysts of Ni, Co, Pi, and Pd on carriers
such as silica-alumina cracking catalyst, pure silica
gel, and activated alumina. A small bomb, 500- ml
autoclave, and continuous flow reactor were used for
the reaction. Pure catalytic isomerization and mild
hydrocracking were closely related reaction types .
The caulytic combination of metal on silica-alumina
gave the best results .
[Technische Hochschule, Vienna (Austria))
THE MECHANISM OF THE EMAZOTISATION OF
AROMATIC AMINES IN NON AQUEOUS SOLVENTS,
by Hermann Schmid. Final technical rept. for
1 Dec 59-1 Dec 60 on Contract DA 91-591-EUC-1311.
[1960] 70p. 39 refs. AD- 249 588.
Order from LC mi$3. 90, ph$10. 80 PB 154 157
The kinetic investigation of the diazotisanon of aniline
was extended to the solvent 1,1', -Dichloroethane. TTje
experiments had to be interrupted, because the method
of coupling and stopping in one operation, was not ap-
plicable. They will be continued after the development
erf a new method. In methanol solution the diazotisation
could be investigated by the method of stopping and
coupling. It was observed that in this medium the re-
action is very sensitive with respect to the ionic con-
centration and, the dependence of the velocity on that
concentration was determined. If the ionic concentra-
tion through the reaction remains at a constant and
suffidently high level, which is supported by foreign
ions or even by th^ reacting chloride ion, the velocity
of the reaction is proportionate to the concentration of
the anilinium ion, to the nitrous acid and to the chlo-
ride ion. At low ionic concentration and so with a con-
siderable change of it, there appears a kinetic irregu-
larity, according to the functicMial dependence of k on
(c), where c is the total ionic concentration in the so-
lution: k equals Ac to the -0. 445th power. The reaction
velocity depends now on the square root of the chloride
ion concentration (approximately). The theoretical in-
terpreution of the above stated equation needs further
697
infoTTiMtlons, for which purpose the experiments will
be extended. The temperature coefficient <rf the dlazo-
tlMtion rate In metkanol was determined at different
levels of the ionic cbncentratlon. (Author)
I
WashingtcMi U . , Settle.
THE REACTION Of TRIFLUOROMETHYL HYPO-
FLUORITE WITH $ULFUR TRIOXIDE AND SULFUR
OlCOaDE, by Wayn« P. Van Meter and George H.
Cady. Technical rebt. no. 26 on Contract Nonr-
477(16). 1960. 10p,7refs. AD- 234 837.
Older from LC mi^l. 80, ph|l. 80 PB 154 118
Trifluoromethyl hy|ofluorite reacts with sulfur tri-
oxlde in the temperature range 245° to 260° to form
trifluoronieihyl perpxyfluorosulfonate, CF3OOSO2F,
• substance which rpelts at -117° and boils at 12. 9° .
Trifluoromethyl hyiofluorite reacts with sulfur di-
oxide in the range l|750 to 1850C. to yield many prod-
ucts . The crude mixture of products has been sepa-
rated into its components by fractional codistillation.
Nuclear magnetic resonance, infra-red, and mass
spectra have been i^sed to establish the structures of
the new compounds. Differences in ease of hydrol-
ysis by aqueous sodium hydroxide have been corre-
lated with the proposed structures . Vapor pressure
curves and gas andlliquid densities have been meas-
ich of th^
ured for each
substances . (Author)
Physical Chemistry
Amherst Coll. , Mass.
THERMODYNAMtd PROPERTIES OF THE ELEC-
TRICAL DOUBLE l^YER. CAPACITY OF THE
MERCURY -SOLUTION INTERFACE IN TENTH-
NORMAL AQUEOUP SOLUTIONS OF METALUC
CHLORIDES AT 2$^ AND DERIVED PROPERTIES.
by David C Grahaihe. Technical rept. no. I on Con-
9 Mar 50. 28p. 9 refs.
PB 154 872
traa N8onr- 66903.
ATI -86 858
Order from LC mi«.70. ph$4.80
This report released for sale to the pubUc 24 Mar 61
The differential capacity of a number of tenth-normal
aqueous solutions df metallic chlorides were meas-
ured as a function if potential. The results are inter-
preted to mean that the solvent sheaths on the positive
and negative ions ate displaced as the ions approach
the interface. New explanations are given for several
well known phenomena connected with the double layer
The electrocapillaijy maxima at the solutions investi-
gated have also be^ deternuned, and the surface
charge density and integral capacity of the non-diffuse
part of the electrical double layer have been calculated
from these data. The ratios of the differential capaci-
ties are found to a^oach unity at potentials where
the concentration df cations within the double layer Is
at a maximum. Tliis result can be used to establish
liquid junction potcintials between the solutions
investigated.
Amherst Coll. , Mass.
THERMODYNAMIC PROPERTIES OF THE ELEC-
TRICAL DOUBLE LAYER. POTENTIAL OF THE
ELECTROCAnLLARY MAXIMUM IN AQUEOUS
SOLUTION AT 25 C. by D. C. Grahame, E. M. Coffin,
and J. I. Cummings. Technical rept. no. 2 on Con-
tract N8onr-66903. 11 Aug 50. 30p. 19 refs.
ATI -86 039.
Order from LC mi$2.70, ph$4.80 PB 154 873
This report released for sale to the public 24 Mar 61.
Six new methods for the determination of the elearo-
capillary maximum (e.c. max) are described. These
methods, together with a seventh, have been used to
determine the potential of the e.c. max for represent-
ative types of aqueous solutions at 25^0. The thermo-
dynamic and physical significance of the results are
discussed. It is found that the properties of the com-
pact part of the double layer are practically unaffected
by the valence <rf the cation. Th*" properties ol the
diffuse double layer, on the other hand, are strongly
affected by the valence of the cation. Precise meas-
urement at the potential of the electrocapillary maxi-
mum is indispensable to the evaluation of other prop-
erties of the electrical double layer and holds out
fwomise of providing a method for the determination of
liquid junaion potentials to within the accuracy al-
lowed by the principles of thermodynamics.
Amherst Coll. , Mass.
THERMODYNAMIC PROPERTIES OF THE ELEC-
TRICAL DOUBLE LAYER. I. THEOREM CON-
CERNING THE EFFECT OF DISCRETE CHARGES
IN THE ELECTRICAL DOUBLE LAYER. II. THE
APPARENT ANOMALY IN THE RATE OF CHANGE
WITH CONCENTRATION OF THE POTENTIAL OF
THE ELECTROCAPILLARY MAXIMUM, by David C.
Grahame. Technical rept. no. 13 on Contract N8onr-
66903. Jan 54. 22p. 11 refs. AD- 24 718.
Order from LC mi$2.70, ph$4.80 PB 154 874
This report released for sale to the public 24 Mar 61 .
Theoretical considerations are presented which show
that a uniform array oi discrete oriented dipoles gen-
erates a potential difference no different from that as-
sociated with 2 uniform layers of charge having the
same average charge density. According to the argu-
ment presented, it is not possible to explain a sup-
posed anomaly in the rate of change of the potential of
the elearocapillary maximum with concentration as
an effea attributable to the discrete charaaer of the
charges which go to nuike up the adsorbed layer of
anions in the electrical double layer. This is in con-
tradiction to a theorem advanced by Esin and Shikov
(Zhur. Fiz. Khim 17:236. 1943). An analogous argu-
ment is presented for the case of a charged sphere
carrying a discrete layer of oriented dipoles. The
anomalous variation with concentration of the potential
of the electrocapillary maximum is shown to be as-
sociated with zero or negative values erf T^+ (where ' +
is the transference number of the cation in the elec-
trical double layer). These variations In turn are as-
sociated with the presence of chemical forces (bonds)
aaing between the metal and the chemisorbed anions.
These bonds give rise to dipoles lying between the
698
metallic surface and the inner Helmholtz plane, and
they are the source of the extra potential which has
heretofore been neglected. The resolution of this
anomaly has made the possibility of evaluating the
potential V* of the inner Helmholtz plane more
promising.
Applied Physics Lab. . Johns Hopkins U. . Silver
Spring, Md.
MOLECULAR DIFFUSION STUDIES IN GASES AT
HIGH TEMPERATURE. RESULTS AND INTERPRE-
TATION OF THE He-A SYSTEM, by R. E. Walker
and A . A . Westenberg . Rept . on Contract NOrd-
7386. Aug 59, 20p. 6 refs. CM-958; AD-227 659.
Order from LCmi$2. 40, ph$3. 30 PB 154 538
Experimental measurements are presented of the bi-
nary diffusion coefficient of He-Ar obtained by the
point-source technique over the temperature interval
300-llOOOK. The dau include the extremes of the
concentration dependence from D^e-Ar measured at
298°K . Interpretation is made in terms of a purely
repulsive interaction between the atoms; the concen-
tration dependence is included in the theoretical anal-
ysis . Comparison is made with the He-Ar interaction
obtained from other sources . At the highest tempera-
ture, the measurements overlap the range of validity
of diffusion coefficients predicted from the potential
obtained by Amdur et al Q. Chem. Phys . 22:1071-74,
1954) from small-angle scanering experiments ;
Good agreement is shown to exist between the two
types of experiments, which further substantiates the
validity of predicting high -temperature transport
properties from scattering potentials . (Author)
Army Research Office, Washington, D. C.
FUEL CELLS, by B. R. Stein and E. M. Cohn. Sutus
rept. no. 2. Dec 60. 80p. 38 refs. ARO rept. no. 2.
Order from OTS $0.75 PB 171 155
This report covers recent literature, government and
private programs on fuel cell R&D. Government ex-
penditures have virtually doubled since the first sur-
vey. Government inhouse and contract work ranges
from research to systems development including power
for portable packs, ship propulsion, and regenerative
systems for space satellites. Industrial work also in-
cludes this range but concerns mostly organic fuels
tnd oxygen or air as oxidant. Despite recent demon-
strations of a fuel-cell powered tractor and a small
car. many basic problems concerning fuels, elec-
trodes, and electrolytes must be solved before de-
pendable, long-lived systems can be mass-produced
ecoBomlcally. (Author) (See also PB 151 804)
Army Rocket and Guided Missile Agency. Redstone
Arsenal. Ala.
EXPERIMENTS IN OSCILLATORY COMBUSTION, by
J_W. Connaughton, W. W. Wharton and others. fl960l
37p. 20 refs.
Order from LC mi$3. 00, ph$6. 30 PB 153 619
Ceruin experiments on oscillatory combustion phe-
nomena are described. The objeaives of this program
"e: (1) to understand the mechanism erf initiation of
oscillations and the amplification of oscillations in
combustion sysiiams, (2) to understand the mechanism
of coupling of combustion energy into oscillatory en-
ergy, and (3) to determine the effects of oscillations
on combustion kinetics. TTie results of experiments oo
combustion oscillations which occur when flames prop-
agate in tubular duas are presented. The effeas of
flame propagation velocity on initiation of oscillations
in tubes are described. The effects of addition or re-
moval of gas from the boundary layer as the flame
propagated down the tube are interpreted in terms of
boundary layer theory. The effects of driven oscilla-
tions on combustion in a tubular duct are also de-
scribed. Results erf heat transfer measurements are
presented and interpireted and the effect erf driven
oscillations on combustion kinetics is described.
(Author)
Frlck Chemical Lab . . Princeton .N.J.
A COMBINED FLASH PHOTOLYSIS AND SHOCK
WAVE METHOD FOR THE STUDY OF BROMINE
ATOM RECOMBINATION OVER A WIDE TEMPERA-
TURE RANGE, by George Burns and D. F. Homig.
Technical rept. no. 1 on Contract Nonr- 1858(26).
28 June 60. 23p. 24 refs . AD- 240 036.
Order from LC mi$2.70, ph$4.80 PB 149 085
A combined flash photolysis shock wave experiment
is described in which bromine is first flash photo-
lyzed. then compressed and heated by a shock wave "
and finally allowed to recombine at the high tempera-
ture. Some of the problems connected with working
in a shock tube used as a photolysis vessel are ana-
lyzed. The apparatus was used to measure recombi-
nation rates with argon as a third body at room tem-
perature and to obwin a preliminary measurement of
the recombination rate of bromine in the presence of
argon at 950OK. (Author)
Frlck Chemical Lab. . Princeton U. , N. J.
EQUILIBRIUM POLYMERIZATION OF SELENIUM,
by Adi Eisenberg and Arthur V. Tobolsky. Rept. on
Contraa Nonr- 1858(07). 15 Apr 60, 15p. 13 refs.
ONR Technical rept. RLT 29B; AD- 235 940.
Order from OTS %0. 50 PB 171 575
A theory of the ring-chain equilibrium in liquid
selenium is presented, which is mathematically iden-
tical to a previously developed theory for polymer
equilibrium in liquid sulfur [}. Am. Chem. Soc. 81:780,
1959]. The numerical treatment is based^on: (a) the
entjopy and ent{^lpy of the propagation reaaion
(Se^ + SegF^ Sep + g. the star denoting a diradical)
which were calculated from values of the Seg concen-
trations in the liquid as given in the literature, and
(b) the enj-opy and enthalpy of the initiation reaction
(Seg^s^Seg) which were estimated by comparison to
the sulfur values. The "transition" temperature for
the appearan<:e erf polymer in the liquid state is calcu-
lated as 830G(1340 below the melting point of sele-
nium), and the chain length at the melting point is
estimated as ca 1300 Seg units. (Author)
699
Institute for Fluid jDynamics and Applied Mathe-
matics, U. at Martyland, College Park.
SOME STUDIES OH ARGON, HELIUM AND CARBON
DIOXIDE WITH AN INTEGRATED- SCHLIEREN IN-
STRUMENTED SHOCK TUBE, by Jerome Daen and
P. C T. de Boer. %ept. on Contract AF 49(638)401.
Dec 60, 45p. 16 refk. Technical note BN-225:
AFOSR-139; AD-2i^675.
Order from LC mlfp. 30, ph$7. 80. PB 154 509
!
Using integrated- schlieren instrumentation, an in-
vestigation has been made of shock waves in argon,
helium and carbon cHoxide. bi argon and helium a re-
sidual signal has been observed, which is ascribed to
to curvature at the $hock front in the vicinity at the
wall. A discussion Is presented at the way in which
the curved shock sa^sfies the boundary conditions,
and al the resulting iflow panem. which includes a
"pressure adjustment region". Preliminary measure-
ments on the variation al the apparent "zone thick-
ness" with density dfnd shock speed in these gases are
reported. The importance al the observed shock
curvature in measurements of the vibrational relax-
ation time for gasel like carbon dioxide is considered.
Preliminary results; for the vibrational relaxation
times al dry CO2 Aije reported for temperatures up to
ca. 900^, and arej compared with results obuined
by others. (Author)
Institute for the Srtidy of Rate Processes, U. of
Utah, Sak Lake Cty.
KINETICS OF CHEMICAL REACTIONS, by George
Richard Hill. Final rept. on Contract AF 49(638)28.
30 NOV 60, 75p. 30refs. AFOSR-114.
Order from LC mi$M.S0, ph$12.30 PB 154 709
The research has consisted of two fundamental kinetic
studies, the kineticj and mechanism of diborane
CB2H6) pyrolysis an4 kinetics of carbon monoxide-
borane (BH3CO) pyrblysis.
Institute de Quimita Fisica (Spain).
KINETICS AND MECHANISMS OF THE THERMAL
DECOMPOSITION OF ACETALS, by M. J. Molera.
J. Morcillo and others. Annual technical rept. no. 2,
1 Nov 59-31 Oct 6al on Comract DA 91 -591 -EUC- 1183.
[1960] 57p. 18 refs.l AD- 249 167.
Order from LC mi$l3. 60, ph$9. 30 PB 153 91 1
I
The influence of several inhibitors upon the thermal
decomposition of m^hylal and dimethyl acetal was
studied in a high vatuum apparatus. The reactions
were followed by observing the change of pressure in-
side the reaction veissel with time and by quantitative
analyses with an inured spectrometer. N202 had a
transitory action asi an inhibitor of the decompoBition
of methylal and of ctmethyl acetal. After being re-
duced to a limiting value, the rate increased steeply
again when the N202 was completely consumed. The
apparent order was close to I for the inhibited decom-
position of both acetals, with a transition towards 2 at
the lower pressure^ of acetal. The corresponding
activation energies are 76. 6 and 61 kcal/mol for
methylal and dimetfcyl acetal, respectively. The pres-
sure increase -time curves of the methylal decomposi-
tion were lowered 1^ the action of ethylene or propyl-
ene below the limit ! reached when N202 was used as in-
hibitor. Moreover, at the greater olefin pressures
used, the curves became partiaily negative owing to a
reaction of the olefin induced by the radicals from the
acetal. Ethylene or some of its products remaining
adsorbed on the surface of the reaction vessel were
believed to have a specific influence upon the decom-
. position of dimethyl aceul. Toluene and cyclohexene
were efficient inhibitors of the decomposition of the
two acetals. (Author) (See also PB 144 239)
Louisiana State U. , Baton Rouge.
FARADAIC RECTIFICATION AND ELECTRODE
PROCESSES, by Paul Delahay, Mitsugi Senda, and
Carl H. Weis. Technical rept. no. 41 on Contract
Nonr- 300(00). June 60, 50p. 25 ref s . AD- 243 487.
Order from LC mi$3. 30, ph$7. 80 PB 150 967
A general theory of faradaic rectification was
developed and it was shown that both the mean and the
alternating components of potential and/or current
must be controlled. Transients due to charging of the
double layer and to rectification by the double layer
are quite essential in the interprewtion of rectifica-
tion voltage measurements . The difficulties associ-
ated with the double layer capacity and ohmic drop in
other relaxation methods are largely eliminated in the
application of faradaic rectification to very fast re-
actions . The method has^wo unique features in that
(a) conditions in which thOKell alternating current is
primarily c^trolled by the double layer capacity do
not prevent measurement of Ig and o but in fact are
desirable (A. V. control), and (b) frequency discrimi-
nation by means of a low pass filter in the measure-
ment of Afi«o eliminates the difficulty resulting from
a large ohmic drop and allows the determination of
Ij and a even when the cell resistance is very much
larger than the charge transfer resistance. An upper
limit of the k§'s which could be determined can be
set only after further evaluation but it appears that
values of kj up to 10 to 100 cm . sec . ' ^ could be
measured. The upper limit is based on the assump-
tion that frequencies up to ICX) mc can be used. The
question arises at very high frequencies whether
formulas derived from Pick's equations for diffusion
still apply since motion can no longer be regarded as
completely randomized. Such considerations , how-
ever, need not be introduced below 100 hk since the
average path of a diffusing particle (D« 10'5
cm?sec:l) for t - 10"^ sec is still quite large in com-
parison with molecular dimensions . (Author)
Massachusens Inst, of Tech. , Cambridge.
HYDROGEN PEROXIDE LABORATORIES, by
C. N. Satterfleld. Quarterly periodic status rept. on
Contract Nonr- 1841(11). 30 June 60. lOp. AD- 241 238.
Ortler from LCmi$ 1.80, ph$ 1.80 PB 150 031
Porous Walled Reactor Studies: Experiments were
conducted in stainless steel and Pyrex reactors with
and without injection of inert gas, using the technique
of introducing the main stream gas near the center of
the reactor. In the suinless steel reactor, under cer-
tain flow conditions, the H2O2 decomposition rate con-
stant dropped to a very low value, about 0. 1 of the
value with no injection. Similar results were obtained
in the porous Pyrex reactor. These phenomena were
due primarily to the peculiar flow and mixing pattema
700
ctitained with the type of injection. Decomposition of
H2O2 Vapor on Catalytic Surfaces: The decomposition
studies of H2O2 on Ag and Cu indicated that mass
transfer is a decisive factor under the experimental
conditions studied; the ratio of the decomposition rate
to the rate predicted by mass transfer conditions was
about 0. 5 Decomposition of H2O2 Vapor on Relatively
Inactive Surfaces: H2O2 vapor decomposition on 304
•uinless steel was studied up to 460^^. The decom -
position rate was higher than the mass transfer rate
of laminar flow above 4000c. A corresponding mass
transport controlled rate was observed. Both 0 and N
gave similar rates when used as carrier gases. (See
alsoPB 153 769)
Massachusetts U.., Amherst.
THE MEASUREMENT OF DYNAMIC BIREFRIN-
GENCE, byS. Onogi, D. A. Keedy, and R.S. Stein.
Technical rept. no. 1 on Grant AF AFOSR-61-28.
Ijan61,6p. AFOSR 78; AD-248 744.
Onler from LC mi$ 1.80, ph$ 1.80 PB 154 518
Bffon was made to measure birefringence of a sample
subjected to forced periodic strain. The equipment
includes a 1/4 hp motor, a Graham model No. 125
variable speed transmission, a gear reduction drive
and eccentric to drive a reciprocating lower clamp at
between 0 and 1 .3c. The core of a Shaevitz linear
variable differential transformer is fastened to the
clamp. The output of this LVDT is rectified, ampli-
fied by a Sanborn nrxxlel 150-1500 low-level preampli-
fier and recorded on one channel of a Sanborn nnodel
152-lOOB two channel recorder, and serves to moni-
tor the strain. A filtered parallel, monochromatic
Hg vapor light is polarized at 45 degrees to the
stretching direction, passed through the sample,
through an analyzer oriented perpendicularly to the
polarizer, and detected by an IP21 photomultiplier
tube. Tbe recorder reading is a function of the bire-
fringence and is calibrated against it using a Babinet
compensator. The strain and birefringence of a
1.3 mil Spencer polymorphous polyethylene film was
studied at room temperature as a function of fre-
quency. The strain and birefringence varied with no
perceptible phase difference. The variation with fre-
quency of strain-optical coefficient, defined as the
ratio of birefringence (in refractive index units) to
strain (in units of fractional increase in length), was
plotted. The decrease in coefficient with increase in
frequency is apparent, indicating that the response
mechanism is time dependent and is in contrast to the
negligible birefringence relaxation at longer times .
Naval Civil Engineering Lab. . Pon Hueneme, Calif.
CONSTANT CURRENT DEVICE FOR ELECTROPHO-
RESIS APPARATUS, by W. A. Bowen.Jr. andG. D.
Carpenter. 10 Feb 54, 9p. Technical note N-171.
Order from LC mi$ 1.80, ph$ 1.80 PB 154 659
A system for closely regulating the direct current
flowing in an electrolytic cell was devised and con-
structed for use with a Perkin- Elmer, Model 38,
Electrophoresis Apparatus . A substantial increase in
current stability was gained through the use of a light
spot galvanometer, phototubes , amplifier and associ-
ated circuitry. A current subility at 5 ma. of the
order of ±0.004% was obtained as compared to the
±0.05% obtainable from the unmodified instrument.
(Author)
Noyes Chemical Lab. , U. of Illinois. Urbana.
TEMPERATURE E«PENDANCE OF PROTON RE-
LAXATION TIMES IN AQUEOUS SOLUTION OF
PARAMAGNETIC ION& IL Craq, by Thomas H.
Brown. Roben A. Bemheim, and H. S. Gutowsky.
Technical rept. no. 30 on Contract Nonr- 1834(13).
16 June 60, bp. 3 refs; AD- 241 421.
Order from LC mill. 80, phW. 80 PB 150 133
Proton relaxation times of the "blue" modification of
the CrQq solution were found to depend on its thermal
history, indicating structural change of the solvate
with temperature. At least 2 sets of reactions and
chemical equilibria are associated with thermal
hysteresis. One, above room temperature, involves
times the order of days; the atixevo at lower tempera-
tures, occurs in the order of minutes. After equili-
bration at room temperature, reproducible results
were attained for the temperature dependence of Ti
and T2 in an aqueous solution containing 3 x 10^^
Cra3 molecules/cc. Log Tj and log T2 were
measured as a function of reciprocal temperature and
thermal history for protons at a magnetic resonance
frequency of 20 mc/sec. The Tj value increased as
much as 20 to 30% when a solution having initially a
normal Tj remained at a given elevated temperature
for several hours. This suggests changes in species
concentrations and thermodynamic equilibrium at the
higher temperature. When the Tj of the high temper-
ature solution was measured rapidly at lower temper-
atures, the values were systematically larger than
those of the normal solution. The Ti of a low-
temperature solution was less than that of the normal
and the rime scale of the hystersis was in the order of
minutes instead of hours. Random observations of the
thermal hysteresis of T2 Indicated an analogous
situation. (See also PB 144 432)
Ohio State U. Research Foundation, Columbus.
THE REACTIONS OF 8293(1) AND CARBON AT
ELEVATED TEMPERA "fmES, by P. M. Rentzepis
and David White. Technical rept. no. 1 on Cbntract
Nonr-495(12). Jan 59, 15p. RF ProJ. 691;
AD-210 804.
Order from LC mi$2. 40, ph$3. 30 PB 154 959
This report released for sale to the public 28 Mar 61.
The reaction of 8202(1) ■► C in the temperature range
1350-1650°K has been investigated in an effort to es-
tablish at least a lower limit for the heat of formation
of B202(g). Combining the existing data in the litera-
ture, which probably represents an upper limit for the
heat of formation of B2O2. together with the value re-
ported here; AH8f (8202(g)) is considered reliably
in the range -108± 3 kcal per mole.
Ohio State U. Research Foundation. Columbus.
STUDY OF SOLID VAPOR EQUILIBRIA IN THE
RARE EARTH - RARE EARTH METAL SYSTEMS,
by David «Vhiie. Final rept. on Contract AF 18(600)1545
Oct 6a 13p. 12 refs. RF proj. 653-Final;
AFOSR -{TR) -60- 177; AD- 249 224.
Order from LC mi$2. 40, ph$3. 30 PB 154 156
A list of the various rare-earth oxide systems investi-
gated is given. The phase equilibria, the composition
701
of the solid and vapor phases, at elevated tempera-
tures, are given. This table demonstrates the com-
plexity of the phase equilibria, which were defined, for
the first time in tbfl program. Such an extensive in-
vestigation was nec^sary before any thermodynamic
analysis of these s^lstems could be made. The rates
of vaporization for the 17 systems were measured by
the Knudsen effusioli technique. These results com-
bined with the phase equilibria data provide the basis
for the thermodynaBiic analysis of the various rare
earth-oxygen systems at elevated temperatures.
(Author)
Olin Mathieson Cnemical Corp. , New Haven, Conn.
STUDY OF SUPERPXIDIZERS, by F. Martinez. Rept.
for 5 June 58-20 Ma|r 60 on Energy Transfer Research,
Contract AF 29(60Dll667. Mar 60, 59p. 60 refs. Tech-
nical rept. OMCC-4038-G1R-2; AFMDC-TR-60-18;
AD- 250 918.
Order from OTS $1| 50 PB 171 255
Results are presented of studies on (he investigation of
methods for the prejparation and characterization of
higher oxides of hydrogen (superperoxides). The meth-
ods investigated inqlude a study of the reaction of hy-
drazobenzene and h)droquinones with ozone, the re-
action of hydrogen items with ozone, the reaction of
hydrogen atoms with oxygen, the condensation of the
product of the dissciciation of wacfer and hydrogen per-
oxide by glow discharge and the photolysis of dilute
aqueous solutions of hydrogen peroxide. The reaction
of ozone with the oijganic materials did not give rise to
a superperoxide. G|ther reactions gave rise to a ma-
terial which contaiiis two superperoxides. The reaction
of hydrogen atoms with ozone at -196°C gives water
and a mixture of suberperoxides as the sole condensed
products. The conclensation of dissociated water at
-19(PC and the reaction of hydrogen atoms with oxy-
gen give a mixture bf water, hydrogen peroxide and
two species of supet^roocide as the condensed prod-
ucts. (Author)
Pennsylvania State U., University Park.
STABILITY RELATIONSHIPS AMONG THE RARE
EARTH DIPICOUNATES, by Ingmar Grenihe. Tech-
nical rept. no. 2 oq Contract Nonr-656(24).
13 June 60. I6p. lOjrefs AD-239 54«.
Order from LC mi1|2.40, ph$3.30 PB 148 932
Step-wise stoichioi^etric formation constants have
been determined foj the complexes between copper,
yttrium, the rare earths and the dipicolinate ion. The"
measurements havq been made in an aqueous per-
the ionic strength |i » 0. 5 M at a
(Author)
chlorate medium of
temperature of 20°
Polytechnic Inst, of Brooklyn, N. Y.
A THEORY OF SOLVENT EFFECTS ON ELEC-
TRONIC TRANSTIpN, by Y. Ooshika. Technical
rept. no. 3 on Contract Nonr-839(22). 15 June 60,
24p. 10 refs. AD-2P9 108.
Older from LC mi^2 . 70 , ph$4 . 80 PB 1 48 473
A theory developed jto treat the solvent effects upon
the absorption spectra as a continuum was extended
to take into account the fact that the separation be-
tween energy levels of the solute molecule might not
be large compared with the solute- solvent interaction.
A simple nxxiel was used in which the solute mole-
cule exists in an ellipsoidal cavity In a uniform di-
electric and bodi the permanent and induced charges
in the solute molecule have quite the same distribu-
tion as that of a uniformly polarized ellipsoid confo-
cal with the ellipsoid of the surface of the cavity.
This treatment completely agreed with that of the
R.A. Marcus non-equilibrium polarization theory,
which assumes that the differences between the
energy levels of the solute molecule are infinitely
small compared with those of the solvent. The pres-
ent treatment was applied to the 2- resonance- struc-
ture model of dye molecules . With an increase in the
dielectric constant of the medium, the dipole mo-
ment of the solute molecule in the solution may in-
crease abruptly at a certain value of the dielectric
constant, though the wavelength of the absorption al-
ways varies continuously.
Princeton U. , N. J.
THE EFFECT OF DISSOLVED KBir, KOH OR HCl
ON THE RAMAN SPECTRUM OF WATER, by
William R. Busing and Donald F. Hornig. Technical
rept. no. [6] on Contract Nonr- 1858(27). 25 June 60,
33p. 33 refs; AD-239 262.
Order from LC mi$3. 00, ph$6. 30 PB 148 747
One unpolarized and 2 polarized, spectra of a sample
at KBr, HCl, and KOH, and water solutions were ob-
served in the region of the OH stretching fundamental
(I) and also in the lower frequency bending and combi-.
nation region. The solution of either KBr or HQ in
H2O produced a considerable increase in the total
Raman scattering intensity of the H2O in region I. In
both cases the low frequency component at 3250 cm-'
decreased In intensity while the intensity of the high
frequency component at 3450 cm"^ increased strik- !
ingly. The effect on both bands was more marked with
KBr; this fits the notion that the structure breaking
effect of the large ion, BR", is greater than that of
Cl~. HQ solutions also had a broad low frequency
band attributed to OH3+; as the concentration of HCl
was increased its intensity grew at the expense of
both of the H2O bends. KOH solutions had only a
steady intensity decrease of the water bands as the
concentration was increased. At the same time the
Intensity of the OH' stretching band as well as that of
the broad low frequency band attributed to H2O mole-
cules coordinated to OH' grew steadily.
Rochester U., N. Y.
THE PHOTOLYSIS AND FLUORESCENCE OF DI-
ETHYL KETONE AND CMETHYL KETONE -
BIACETYL MIXTURES AT 3130 A AND 2537 A, by
David S. Weir. Rept. on Contract AF 49(638)679. ^^^^
14 Nov 6a 22p. 29 refs. AFOSR TN-60-1381.
Order from LC mi$2. 70, ph$4. 80 PB 154 374
The photolysis of diethyl ketone and the photolysis and
phosphorescence of diethyl ketone -biacetyl mixtures
have been studied aj 3130 A and 2537 A. The addition
of biacetyl at 3130 A decreases the photodecompositioa
of diethyl ketone and increases the phosphorescence of
702
biacetyl. An energy transfer from excited triplet di-
ethyl ketone to biacetyl is proposed and there is evi-
dence that the propionyl radical formed from the sing-
let sute at 3130 A is sufficiently "hot " to dissociate.
Into an eth^ radical and carbon nKinoxide. At 2537 A
disaociatfon appears to occur from the initially formed
upper singlet state and there is no evidence that the
triplet state intervenes. A detailed mechanism is pre-
sented for th^ primary process in diethyl ketone and
for the energy transfer between diethyl ketone and
biacetyl. (Author)
Rutgers State U. School of Chemistry, New
Brunswick, N. J.
EXPLORATORY STUDIES ON THE SURFACE
ACTIVITY OF POLYSOAPS. by Helmut E. Jorgensen
(Doaoral thesis) and Ulrich P. Strauss. Technical
rept. no. 6 on Contract Nonr -404(05). 1 June 60, 18p.
26 refs. AD-238 255.
Order from LC mi$2.40, ph$3.30 PB 148 400
Among the materials studied were several polysoaps
and a polyelearolyte derived from poly-4-vinylpyri-
dine by quaternization with ethyl and n-dodecyl bro-
mides, a sulfonic acid polysoap and its sodium salt,
and a polysoap prepared by quaternizing poly-2-vinyl-
pyridine with 3-bromopropylbenzene. The poly-4-
vinylpyridine polysoaps showed the following proper-
ties: (1) In the absence of simple electrolyte the sur-
face aaivity was very small, which supports the con-
clusion that under similar conditions micelles of ordi-
nary soaps and detergents are not significantly ab-
sorbed at interfaces. (2) In the presence of KBr, the
polysoaps depressed the surface and interfacial ten-
sions markedly, but the polyelectrolyte did not. (3)
Equihbrium was reached rapidly. (4) The d-dodecyl
group content and the molecular wei^t at the poly-
•oap had no effea on the surface activity. (5) Solu-
UUzation of dlphenylmethane decreased the surface
tension substantially. (6) The depressing effect of the
polysoaps on the interfacial tension was considerably
greater than on the surface tension. The sulfonic
acid polysoap and its sodium salt had very little effea
00 the surface and interfacial tensions, even in the
presence of simple electrolyte. In contrast to the
other polysoaps, the poly-2-vlnylpyridine polysoap
depressed the surface tension significantly in the ab-
sence of simple electrolyte, and several hours were
necessary to reach surface equilibrium. The surface
tension depression increased with increasing tem-
perature, indicating that the surface aaivity was due
to entropy forces. (Author)
University of Southern California [Los Angeles).
■NUCLEAR COMPLEX IONS. UI. FORMATION OF
PBROXO AND CYANO BRIDGED COMPLEXES BY
OXIDATION OF THE PENTACYANO COMPLEX OF
Co (II). by Albert Haim (doctoral thesis) and
W. K. Wilmarth. [Rept. on Contract N6onr-238,
T. 0. 4]. [1960] 28p. 25 refs . AD-238 035.
Order from LC mi$2. 70, ph$4. 80 PB 148 075
^nuclear ions have been prepared by oxidation of the
pentacyano cortiplex of Co (II) with O2 and Fe(CN)6"^.
The mechanism of formation of the various complex
ions is discussed in terms of outer sphere and
bridged activated complexes .
University of Southern California [Los Angeles]
BINUCLEAR COMPLEX IONS. V. AN INVESTIGA-
TION OF THE MECHANISM OF OXYGENATION OF
THE Cr(in ION IN AMMONIACAL SOLUTION
USING OI8 LABELLED OXYGEN, by T. B. Joyner
(Doctoral thesis) and W. K. Wilmarth. [Rept. cm
Contract N6onr- 238, TO. 4). [1960] 16p. 6 refs.
AD-238 036.
Order from LC mi$2. 4a ph$3. 30 PB 148 076
A study has been made of the extent of the labelling of
the bridging oxygen atom of the [(H3N)5Cr-0-
Cr<NH3)5]<*lon, formed by oxygenation of the Cr<II)
ion in ammonical solution. Under all conditions the
labelling was extensive but never complete. The per-
centage labelling varied only over the range 40-705J
despite an 80° variation in reaction temperature and
a considerable variation in [jH and Cr(II) concentra-
tion. On the basis of these results and other available
information it is possible to deduce a plausible path
for the oxygenation process. In this mechanism the
binuclear [(H3N)5Cr-02-Cr(NH3)5}** ion and a
Ci<IV) complex, the [(H jN)5Ci<CW)]3* ion, both play
important roles as transient intermediates in the
overall reaction. (Author) (See also PB 148 075)
[University at Southern Calif omiiQ Los Alleles.
STRUCTURE AND STABILITY OF CCKiPLEX IONS,
by W. K. Wilmarth. Final technical rept. on Con-
tract N6cHu-238,T. O. 4[l960]7p. 19 refs; AD-238 034.
Order from LC mi$l. 80. ph»l. 80 PB 148 077
Research on the' structure and stability at complex icms
included the following studies; (1) the catalysis of
homogeneous reactions by Cu(I) complexes; (2) the
base- catalyzed exchange of molecular H and protonic
solvents; (3) the structure and properties of binuclear
complex ions; (4) the sodium salts at tri-o-naphthyl-
boron; (5) the catalytic conversion of parahydrogen by
paramagnetic complex ions; (6) the magnetic suscepti-
bility of iodine dioxide; (7) the mechanism of oxygen-
ation of Cr(Il) and Co(lI) complexes; and (8) a cry-
oscopic study of Mn(VlD and Cr(IV) compounds in con-
centrated HjSO^. (See also PB 148 076)
Virginia U. , Charlottesville.
APPLICATION OF MOLECULAR BEAM TECH-
NI(5UES TO THE STUDY OF INELASTIC MOLECU-
LAR COLLISION PHENCMENA IN GASES, by John
E. Scott. Jr. Rept. cm Project Squid, Contraa
Nonr- 1858(25). June 60. 23p. 18 refs. Technical rept.
UVA-l-P; AI>242 445.
Order from LC ml$2. 70. ph$4. 80 PB 150 535
Wayne State U. , Detroit, Mich.
COAGULATION AND STABILIZATION OF COL-
LOIDAL SOLUTIONS WITH POLYELECTROLYTES,
by Thomas L. Pugh and Wllfrled Heller. Technical
rept. no. 37 on Contraa Nonr- 736(00). 1 June 60, I6p.
5 refs. AD-238 481.
Order from LC mi$2. 40, ph$3. 30 PB 148 406
Polyelectrolytcs are found to be powerful agents for
colloidal solutions at concentrations as low as 10*^
moles per liter and excellent stabilizing agents at
703
soRiev^t higher cincentrations (in and excess erf 10'^
moles/liter). This applies if the polyions have a
charge opposite to that dt the colloidal particles. If
polyions and oolloi<lal particles have like charges, the
stability of the collloidal solutions is only slightly
altered, primarily in the direction of sensitization.
The investigations Were carried out with FeOOH-sols
(positively charged particles), gold sols (negatively
charged particles), sodium polytryene sulfonate and
polyvinyl benzyl - timethyl ammonium chloride. The
stability was tested by means of a modified Au -jiumber i
(Au-sols) or by considering the rate of coagtiium for-
mation (FeOOH-sols). The stabilizing effect is la-
terpreted as being both electrostatit and steric.
(Author) (See also ^ 148 407)
also t^ 148
Wayne State U. , t>etroit, Mich.
"STERIC" STABILIZATION OF COLLOIDAL SO-
LUTIONS BY ADSORPTION OF FLEXIBLE MACRO-
MOLECULES, by Wilfried Heller and Thomas L. Pugh.
Technical rept. no,i 38 on Contract Nonr- 736(00).
1 June 60, 25p. 17 refs; AO-238 423.
Order from LC ml^. 70, ph$4. 80 PB 148 407
Studies were made Irf the stabilizing effect of polyethyl-
ene glycol on Au hydrosols. It was thought that stabli-
zation was caused l>y the adsorption of the polymers at
the colloidal particles and the extension of segments of
the polymer into thf surrounding medium. The inter-
penetration of the pblymer chains would separate col-
liding particles, miking the van der Waals interaction
energy insufficient to cause coherence. The degree of
stabilization achieved by addition of polymer to the Au
sols increased with the time elapsed before the sub-
sequent addition of toagulatlng electrolyte particularly
during the first hour. The stabilization increased with
polymer concentration and with the molecular weight of
the polymer. (See ^Iso PB 148 406)
West Virginia U. [Morgantown].
RESEARCH AND DEVELOPMENT ON METAL ION
COMPLEXES OF OXYGEN SUBSTITUTED AMINES,
by James L. Hall, final technical rept. for 1 June 57-
31 May 60 on Contria DA 36-061 -ORD-579, continua-
tion of Cortract DA '36-061 -ORD- 541. 15 June 60,
14p. OOR repc. 16flK:l2-C; AD-239 453.
Order from LC mi$p. 40, ph$3. 30 PB 153 662
Preliminary, tentative results are now available on
complexes formed qetween nickeKII) ion and 2-amino-
2-(hydroxymethyl)-l, 3-pn-opanediol, (2) the prepara-
tion of a number of new solid complexes of copper(II)
and nickeKII) salts trith the alkanol- substituted mono-
amines and (3) a stijdy of the infra-red spectra of a
number of copper(II| complexes of mooo-. dl- and
triethanolamine .
EARTH SCIENCES
r
Coastal Studies Init. , Louisiana State U. , Baton
Rouge. I
INTERNATICWAL GEOGRAPHICAL UNICW COM-
MISSION ON COASTAL SEDIMENTATION, BIBUO-
GRAPHY 1955-19581. Rept. on Contract Nonr-
1575(03). 1 June 60^ ISSp. 1337 ref s . Contribution
60-2; AD-239 8%.
Order from LCmi$^. 50. pl424. 30 PB 149 216
A bibliography was compiled on scientific coastal re-
search and emphasizes the following fields: beach-
drifting measured by isotope indicators; over-nouri-
ished and undernourished beaches in relation to sup-
ply of material; the sources of beach material; evolu-
tion and classification of shorelines; ebb- and flood-
scour dynamics , and the topography of the tidal area;
delta sedimentation and.isostatlc movements; the pos^
glacial eustatic rise of sea level; coordination of
levels of abrasion terraces and of accumulation ter-
races in river valleys and indications of quaternary
changes of sea level; mangrove coasts , topography
and development; salt marshes and their development,
coordination of levels and vegetational stages; the
solvent action of sea water in limestone cliffs and
abrasion planes; coral reef geomorphology , topogra-
phy, and development; the standflat in f jord regions:
classification systems of shorelines; investigations of
the offshore by means of aqualung methods; and beach-
rock observations .
Washington U. , Seattle.
ENERGY EXCHANGE MEASUREMENTS ON THE
BLUE GLACIER, WASHINGTON, by E. LaChappelle.
Semi-annual progress rept. on Crysul Fabrics,
Contract fNonr-477(18)]. 1 June 60. lip. 1 ref.
Order from LC mi$2. 40, ph$3. 30 PB 148 233
The Blue Glacier has been characterized by the studies
to date as a temperate alpine glacier situated in a
strongly maritime environment, where the winter
energy deficit is due almost entirely to accumulated
ice mass, and where the principal source of heat for
sununer melting comes from insolation. Sensible heat
transfer from the atmosphere plays a well-defined but
secondary role in the ablation. Sub- surface snow melt
plays a significant part in the daily energy balance.
Weizmann Inst, [of Science] (Israel.)
PROPAGATION OF A SEISMIC PULSE IN A
LAYERED SCfLVD HALF-SPACE, by Q L. Pekeris,
Z. Alterman and others. Quarterly rept. no. 16,
Apr-June 60, on Contract Nonr-2189(00) [and>
Quarterly rept. no. 19, Apr-June 60, on Propagation
of Rayleigh Waves In the Earth, Contract
Nonr- 1823(00). 1960, 3p.
Order from LC mi$l. 80, ph$l. 80 PB 149 775
Climatology and Meteorology
Air Force Cambridge Research [Labs. ] Bedford,
Mass.
STRONG VERTICAL WIND PROFILES AND UPPER-
LEVEL MAXIMUM WIND SPEEDS OVER VANDEN-
BERG AIR FORCE BASE, by H. A. Salmela and
N. Slssenwine. Additional note. May 60. 15p. 3 refa.
GRD Research notes no. 35; AFCRC-TN-60-411.
Order from LC ml$2. 40. ph$3. 30 PB 155 089
This report released for sale to the public 24 Mar 61 .
This note reports on a very strong wind shear that was
observed with only moderately strong wind speeds
704
over Vandenberg AFB, and also reports on the investi-
gation of wind soundings over southern California that
followed. The study reveals stronger-than-anticipated
•hears of two distinct types: (a) the type rn which there
are relatively strong winds through a deep layer and
where there is high correlation between shear and
wind speed; and (b) the type that has very light wind
speeds in the lower levels with a sudden increase in
wind speeds around 9 km. Also included are recom-
ntendations for missile designers. (Author)
Army Signal Research and Envelopment Lab. ,
Fort Monmouth , N . J .
BOUNDARY LAYER WIND SMULATOR, by
Abraham Golden. Nov 60, 13p. 1 refs . USASRDL
Technical rept. 2159; AD-249 109.
Order from LC mi$2. 40, ph$3. 30 PB 154 533
An experimental nKxJel of a meteorological simulator
is described which solves the equations of motion in
two dimensions . Simulator solutions are given for
three test problems . Use of the simulator for deriva
tion of austausch coefficients is explained. (Author)
Army Signal Research and Development Lab. , Fort
Monmouth. N. J.
A CONTRIBUTION TO A SIMPLE THUNDERSTORM -
WARNING DEVICE, by Lothar H. Ruhnke. Oct 60,
20p. 4 refs. USASRDL Technical rept. 2158;
AD-249 108.
Order from LC mi$2. 40. ph$3. 30 PB 154 532
Detection and tracings of lightning during a thunder-
storm were made. Results indicate that the wave
form of a return stroke and the corresponding fre-
quency spectrum is derived theoretically under con-
sideration of the influence of the finite length of the
radiator. The probable accuracy of determining the
distance of a lightning stroke by field measurements
of the return stroke is treated by theory and experi-
ment. A proposal is made to increase the accuracy of
the thunderstorm -warning device described previ-
ously. (Author)
Army Signal Research and Development Lab. .
Fort Monmouth, N. J.
ON THE THEORY OF WIND- SHEAR MEASURE-
MENT, by Abraham Arnold. Nov 60, I2p. 5 refs.
USASRDL Technical rept. 2155; AD-249 107.
Order from LC mi$2. 40, ph$3. 30 PB 154 531
An examination was made of the mathematical as-
■umptions underlying a technique of wind-shear meas-
urement. Results indicate that the measurement is
defective even excluding the effect of error in track-
ing equipment. Under conditions where the wind
varies markedly in a measurement layer, such as
occurs in the vicinity of the jet stream, the current
technique is most liable to yield faulty values.
(Author)
California U . , Los Angeles .
THE INFLUENCE OF TERRAIN AND THERMAL
STRATIFICATION ON FLOW ACROSS THE CAU-
FORNIA COASTLINE, by James G. Edinger. Final
rept. on Contract AF 19(604)5212. 30 Nov 60, 67p.
7 refs. AFCRL TR-60-438.
OrderfromLCmi$3.90, ph$l0.80 PB 154 447
The manner in which terrain and thermal stratifica-
tion influence the air flow across the California coast
during the summer is investigated. In the first
section, using rawins from Oakland and Santa Maria,
the disturbances to the flow below, in and above the
inversion are examined relative to the orientation and
magnitude of neighboring relief. The second section
is concerned with the acticm of adjacent sea-breeze
regimes . Here, the characteristics of the vertical
motions generated at the confluence in the San Fer-
nando Valley of the Oxnard and Los Angeles sea-
breezes are determined from a dense array of upper
wind data. And described in the last section is an ob-
servational technique,' involving rapid response air-
borne thermometers , that was developed to provide
detailed descriptions of the thermal fields in the vicin-
ity of terrain features . Included are analyses of the
field test data demonstrating the capabilities of the
technique and at the same time revealing the some-
times elaborate temperature structure adjacent to
coastlines and coastal ranges . (Author)
General Mills , Inc . , Minneapolis , Minn .
THE REVERSAL OF STRATOSPHERIC WINDS OVER
NORTH AMERICA IN 1957, by Arthur D. Belmont.
Scientific rept. no. 2 on Contract AF 19(604)6618.
1 Dec 60, 87p. GMI rept. 2145: AFCRL TN-60-836;
AD-249 452.
Order from LC mi$4-80, ph$13.80 PB 154 163
The spring and fall reversal of prevailing strato-
spheric zonal wind direction during 1957 is described
and compared to the normal pattern. On both east and
west coasts of North America the zonal wind became
easterly sooner and more extensively in the spring of
1957 than nornwlly. The fall reversal was essentially
normal except for westerlies near Balboa from Aug to
Oct. (Author)
General K^Us, Inc., Minneapolis. Minn.
THE REVERSAL OF STRATOSTHERIC WINDS
OVER NORTH AMERICA IN 1958. by Arthur D.
Belmont. Scientific rtspu no. 3 on Contract
AF 19(604)6618. 9 Jan 61, 86p. GMI rept. 2154;
AFCRL-220.
Order from LC mi$4.80, ph$13.80 PB 154 376
The spring and fall reversal of prevailing strato-
spheric zonal wind direction during 1958 is described
and compared to the "normal" pattern previously
presented. In 1958 the major currents along both
profiles were more strongly developed, both with
respea to persistency and zonal component, than in
the nornuds or in 1957. The 1958 spring reversal
along 80OW was later than normal and was not quite
completed even by the second half of May. The
remaining reversals were normal. (Author)
705
Hawaii but. cf Geophysics, Hoooiulu.
OBJECTIVE WIND FORECASTING OVER THE
TROPICAL PACIFI<i by R. L. Lavole and
C. J. Wiederandersj Scientific repc. no. 1 on
Contraa AF I9(604t7229. Dec 60, 43p. 19 refs.
AFCRL-TN-60-832.
Order from LC mi|3.30, phS7.80 PB 154 566
The results at a study ot the pocentialitles at two
simple objective techniques for wind forecasting over
the tropical Pacific $ie presented and discussed. The
investigation revealed that objective extrapolation ci
the winds does not provide a usable forecast. A
simple statistical r^ression technique, however,
which yields a forecast composed o£ a weighted com-
bination at the persistence wind and the "normal"
wind, does produce « useful improvement upon cur-
rent forecast accuracy. The study further shows that,
although it is difficult to anticipate the optimum
weighting parameters without laborious computation,
the technique can be applied immediately in the field
for Z4-hr forecasts.; This is due to the fortuitous
circumstance that a simple average at persistence and
the long term mean wind does as well as the optimum
weighted combination at the two for a 24-hr forecast
evaluated over the ajfea as a whole. (Author)
High Altitude Obs^vatory, Boulder, Colo.
THERMALLY DRIVEN CIRCULATIONS IN A ROTAT-
ING FLUID SYSTEM, by B Haurwitz. Scientific rept.
no. 2 on Contract Af 19(604)5488. Jan 61, 34p. 2 refs.
AFCRL-TN-61-201;IaD-249 817.
Order from LC mi$i. 00, ph$6. 30 FB 154 275
Some simple modelg of thermally driven atmospheric
circulations are conpidered. The rotation of the fluid
system (for insunc^ the effea of the earth's rotation
in the case of the atmosphere) which was not taken into
account-in an'earliet report is now included. Its
principal effea is to deflect the motion so that the ve-
locity component paf aUel to the temperature gradient
is small, while a mikii larger velocity component nor-
mal to the temperatikre gradient develops. If friction
is not included in th« model the velocity component
parallel to the temperature gradient now tends to zero
as time increases while the normal velocity component
increases without liout because of the continuing en-
ergy input into the niodel. Contrary to the case of no
rotation the temperature gradient is now also increas-
ing without Umit because of the reduction of the ad-
vective term caused by the deflective effect of the
rotation at the syste^. If the friction is introduced
into the model the velocity components and the tem-
perature difference ^end to finite values, as in the
models without rotatjion. The ratio of the final ve-
locity components inj the direction of and normal to the
temperature differ eiice is that ol the Coriolis parame-
ter and the frictionaj coefficient. The kinetic energy
approaches asymptotically the same value as in a
non-rotating model. The final temperature gradient is
larger than in the noti- rotating model because of the
reduction of the advictive term by the rotation of the
model. (Author) I
Laboratory of Climatology, Centerton, N- J.
MEASUREMENT OF VERTICAL WINDS IN TYPICAL
TERRAIN, by C. W. Thomthwaite and W. J Superior.
Quarterly progress rept. no. I, 1 July-30 Sep 60 on
Contract DA 36 - 039 -sc- 84940. continuation ot Contract
DA 36 -039 -8C -78 168. Oct 60. 15p; AD- 245 359.
Order from LC mi$2. 40, ph$3. 30 PB 154 527
A study of the vertical winds over different typical
terrains is made. The study is divided into three usks:
instrumenution, site selection, and data analysis.
Work involved manufacture, testing and calibrating of
measuring instruments, assembly of instrument masts,
and the drawing up of plans for a mobile instrument
trailer. A number of observation sites were studied
and certain sites having markedly different terrains
were selected for future use. (Author)
Mount Washington Observatory, Gorham, N. H.
A STUDY OF PREQPITATION SYSTEMS BY MEANS
OF SNOW CRYSTALS, SYNOPTIC AND RADAR
ANALYSES, by Joachim P. Kuettner, Luis Aldaz and
Roland J. Boucher. Final rept. for 15 Nov 56-
30 June 58 on Study of Relationship Between Snow
Crystal Type and Weather Phenomena , Contract
DA 36-039-8C-73153. 30 June 58, 97p. 3 refs.
AD-215 454,
Order from LC mi$5.40, ph$15.30 PB 150 848
During the winters of 1956-57 and 1957-58, simultane-
ous snow crystal replicas using the Schaefer tech-
nique, were made at three stations: Mount Washington
and two nearby valley points . The synoptic implica-
tions derived from the morphology at snow crystals in
time and space were compared with usual synoptic and
radar analyses. The snow crystal analysis was found
to reveal not only the gross features of the synoptic
scale but many lesser scale phenomena not detectable
by conventional methods of analysis . Micro crystals
with maximum dimensions ranging from 20 microns
up were frequently found with evidence of their forma-
tion at temperatures as high as -9C.
New York U. Coll. of Engineering. N. Y.
A SERIES OF SEA BREEZE OBSERVATIONS IN THE
NEW YORK CITY AREA, by John Frizzola and Edwin
L. Fisher. Quanerly progress rept. no. 1. 1 July-
30 Sep 60. on Local Wind Circulations, Contract
DA 36-039- sc -84939. [I960) 80p. 5 refs.
Order from LC mi$4. 50, ph$12. 30 PB 154 570
A series of pilot balloon observations provided data
for the analysis of vertical cross -sections of the wind
field in the lowest 3500 feet of the atmosphere during
three sea breeze situations in the New York City area.
The days were chosen for different superposed flow
conditions. The progress of the sea breeze was also
followed by hourly surface observations and surface
maps. The following were noted: (1) The sea breeze is
frequently found to have frontal chifiracteristics in New
York City. (2) Opposing gradient flow caused the sea
breeze to be shallower; have lower velocities; and
form later in the day, while retreating seaward earlier
in the evening. (3) During two days, an increase in the
706
landward component of the sea breeze was found in
the very lowest layers near the coast line about sun-
set. This phenomenon had also been observed in a set
at earlier observations at Block Island, Rhode Island.
(Author)
Pennsylvania State U. Mineral Industries Experi-
ment Station, University Park.
STRUCTURE OF TURBULENCE AND MEAN WIND
PROFILES WITHIN THE ATMOSPHERIC BOUND-
ARY LAYER, by Alfred K. Blackadar, Hans A.
Panofsky and others . Final rept . on Contract
AF 19(604)5231. 31 Oct 60, 94p. 31 refs. AFCRL-TR-
60-422.
OrderfromLC mi$5.40, ph$15.30 PB 154 562
Wind profiles observed at various locations are com-
pared with wind profiles predicted by Ellison on the
basis of similarity theory. It is shown that theory and
observation agree well for near neutral and unstable
•ir. However, in stable air factors not considered in
the similarity theory appear to become important .
The range of usefulness of the log- linear wind profile
is shown to be small. The variance and spectrum of
the velocity component at right angles to the mean
wind are summarized from observations at four dif-
ferent places . The sp)ectrum of the lateral velocity
component can be separated into two quite different
regimes: the mechanical regime extending from very
short wavelengths to about 100 m or a little longer;
and the convective regime which extends down from
several kilometers to below 200 m. The breakdown of
surface inversions at night at Brookhaven is closely
associated with the occurrence of strong winds above
300 ft, and becomes almost a certainty when the wind
at 355 ft exceeds 8 m sec" 1 . The occurrence of turbu-
lence below 400 ft is sensitive to the Richardson
number, which in the layer from 100 to 300 ft appears
to have a critical value slightly larger than 0.25.
Texas A. and M. Research Foundation, College
Sution.
IMPROVEMENT, EVALUATION, AND EXTENSION
OF CAPABILITIES OF METEOROLOGICAL SIMU-
LATION (DALLAS TOWER PROGRAM) by William H.
Qayton. Quarterly rept. no. 1, I June- 15 Sep 60 on
Contract DA 36-039- sc-84942, continuation of Con-
tract DA 36-039-SC-.74975. Sep 60, 30p. Reference
60-19T; AD- 248 203.
Order from LC mi$2. 70. ph$4. SO FB 154 528
A review is made of the initial problems and solutions
Involved in the organization of an 11 station mesoscale
meteorological network designed to provide evaluation
data for a special purpose analog computer (Low Level
Meteorological Simulator). (Author)
Weather Bureau, Washiivon, Di C.
SEASONAL MEANS OF HEIGHTS; TEMPERATURES
AND RELATIVE HUMIDITIES FOR STANDARD
LEVELS AT GREENLAND AND SURROUNDING
STATIONS^ by P. Putnins, W. Schallert, and
M. Oboate. q^terly rept. for 1 Nov 59-31 Jan 60
«> Contract DA 3-99-00-500. Mar 60, 55p.
(kikt from LC mi$3.60, ph|9.30 PB 153 715
Geodesy
Clark U. , Worcester, Mass.
LANDFORM MAPS. A METHOD OF FREPARATI(»J,
by Erwin Raisz. Final rept. part 1, on Contraa
Nonr- 2339(00). Nov 59. 39p. 7 refs. AD-235 539.
Order from LC mi$3. 00, ph$6. 30 PB 150 489
Particular attention is given to techniques for pre-
paring the Landform Map of Mexico.
Institute of Science and Tech. , U. of Michigan,
Ann Arbor.
PHOTOGRAMMETRIC TECHNIQUES FOR EKTER-
MINING THE SPATIAL ORIENTATION OF AERIAL
PLATFORMS, by WendeU E. Young. Rept. on Proj.
Michigan. Contraa DA 36-039-8C-78801. Dec 60.
24p. 4 refs. 2900-230-R; AD-249 189.
Order from LC mi$2.70, ph$4.80 PB 153 915
The general problem of determining the spatial orien-
tation of an aerial platform by photogrammetric means
is discussed. Both the stereo and analytical solutions
are included. The photogrammetric range, which
provides a major portion of the input data, is treated
in detail. Five such ranges were construaed. With
these ranges and a calibrated metric camera, the X,
Y , and Z coordinates of the camera station can be
obtained with a probable error of one foot for flying
altitudes of 10.000 feet. (Author)
Oceanography
Arctic Inst, of North America, Washington, D. C.
OCEANOGRAPHIC OBSERVATIONS ON ICE ISLAND
T-3 IN THE SUMMER OF 1959, by Kou Kusunoki.
Scientific rept. no. 5 on Contract AF 19(604)3073.
Apr 60. 21p. Research paper no. 5; AFCRC-TN-60-
417.
Order from LC ml$2.70, ph$4.80 FB 154 551
Marine Physical Lab. , Scripps Institution of Ocean-
ography, San Diego, Calif.
SUMMARY OF AN ENGINEERING DESIGN OF A
REMOTE UNDERWATER MANIPULATOR. Rept. on
Contracts Nonr-2216(07) and Nonr-266(66). 1 Mar 60.
14p. SIO Reference 60-11; ARTEMIS rept. no. 6;
AD- 235 0S9.
Order from LC mi$2. 40. ph$3. 30 PB 153 781
A tracked vehicle, called remote underwater manipu-
lator (RUM), was designed to perform specific work
functions on the ocean floor down to a depth of 20, 000 ft .
The RUM is a remotely controlled, dual tracked
vehicle equipped with a hydraulically operated mechan-
ical manipulator and a vertical lift appendage. The
manipulator will perform work functions of transpon-
ing, assembling, and installing instrumentation assem
blies on the ocean floor. The vertical lift appendage
will consist of a large lifting rotor mounted on a verti-
cal axis to a wheel -shaped structural frame. When
atuched to the tracked vehicle by a system of cables.
707
cbe lift appendage wilf provide the vehicle with an ex-
tended obstacle climting capability for traversing
rugged terrain. A ccfisole panel will consist ct control
circuitry for sonar, ^losed-circuit television, lights,
navigational devices, and instrumentation. The RUM
vehicle with the mechanical manipulator in place will
be capable of carrying a 1000- lb payload in the water
without exceeding a vfehicle ground pressure of 1 . 20
psi of projected trad^ area. Emergency braking in the
event of an electrical' or hydraulic system failure will
be automatically perfbrmed by a spring -actuated fric-
tion brake. The vehicular body will consist of a
welded, tubular, aluifiinum chasis mounting 6 rubber-
tired wheel assemblies with bolted-on axle shafts. The
dual tracks will be the standard 4-pitch, 30-in. -wide,
rubber-band type U8e«l on Army M-76 amphibious
vehicles.
Oregon Sute Coll. Corvallis]
BIOCHEMISTRY OF ^RINE't)RGANlSMS, by
Vernon H. Oieldelin,' Tsoo E. King and others.
Annual progress rept; for 1 Jan-31 Dec 59 on Contract
>4onr- 1286(06). 7 /iHif 60. 2p.
Order from LC mi$l. 80, ph$I. 80 PB 148 079
See also PB 144 256
Physics
ofih«
Atmosphere
Stanford Research |nst. . Menlo Park, Calif.
DISTRIBUTIONS OF ATMOSPHERIC RADIATIVE
HEATING AND COCtiNG, by K. L. Coulson and
P. M. Furukawa. Scientific rept. no. 2 on Contract
AF 19(604)5965. Noi| 60, 83p. 40 refs . SRI ProJ.
2994; ARPA Order n<i. 26-59; AFCRL-TN-60-835.
Order from LC mi$4j. 80, ph$13. 80 PB 154 556
The time variation d the atnwspheric radiation
regime is investigated for a selected synoptic situa-
tion. Elsasser's grajphical method shows the diurnal
variation of the upwaird- directed long-waye flux to be
in phase with surface temperature changes , but no
such change of downward flux was found. Clouds re-
duce the upward fluxiabove the cloud tops and increase
the downward flux bqlow their bases . Long-wave
radiative cooling is greatest above cloud tops and at
upper surfaces of intersions . Ground surface tem-
perature is shown to be very important in the long-
wave regime. Short wave molecular scattering and
surface reflection aie evaluated for a model atmos-
phere by Chandraseknar's exact method and are
adapted for the synoitic situation. Water vapor ab-
sorption, ozone absorption, and the effects of atmos-
pheric dust are approximated. Surface reflection,
water vapor absorptiion, and absorption by particu-
lates in a polluted atmosphere all play dominant roles,
while the effects of r x}lecular scattering and ozone
absorption are relatii^ely minor in the over-all energy
regime. (Author)
Vienna U. (Austria).
EXPERIMENTAL INVESTIGATION OF THE CARBON
DIOXIDE CONTENT OF THE AIR AND AN ANALY-
SIS OF ITS GASEOUS AND COLLOIDAL PHASES, by
G. Stetter. Final technical rept. no. 2, 1 Oct-
31 Dec 6ft on Contract DA 91 -591 -EUC- 1377. con-
tinuation ct Contract DA 91-591 -EUC-1012. [1961]
63p. 5 refs. AD- 249 715.
Order from LC mi$3. 90, ph$10. 80 PB 154 155
Attention was given to the elimination and identifica-
tion of the lightsensitive nuclei or substance(s) of C02
after experiments with physical methods (URAS and
the Kempt ron- Ring Balance) were carried out, which
also should show the particulars of the presence and
structure of the colloid. For the chemical tests sepa-
rations with filters and later separations with the
thermal -sediment -tube were carried out. Following
this, all substances, which were separated in this
manner should be identified and only after that a
grouping accordiiig to special points of view are made.
A general view of the tests and results is given.
(Aulttor) (See also PB 145 947)
ENGINEERING
Aeronautical Engineering
Aeroelastic and Struaures Research Lab. , Mass.
Inst, of Tech.. Cambridge.
RESPONSES OF PLATES AND SHELLS TO INTENSE
EXTERNAL LOADS OF SHORT DURATION, by
Emmett A. Witmer, Walter Herrmann and others. •
Rept. on Atomic Weapon Effects on Aircraft Systems,
Contraa AF 33(616)6373. Apr 60, 145p. 128 refs.
WADD Technical rept. 60-433; AD- 246 364.
Order from LC mi$7. 20, ph$22. 80 PB 155 090
This report released for sale to the public 24 Mar 61.
The problem is examined of predicting the damage in-
curred by simple single-material shell structures such
as cylinders and spheres when subjeaed to intense
distributed external loading of extremely short dura-
tion. A tentative analysis of the intense stress wave
propagation and spelling problem was formulated. The
equations were programmed for solution on an IBM 704
digital compuer and are currently being studied. An
approximate analysis was formulated for the prediction
of buckling type damage to circumvent the enormous
complexities of an exact calculation. This analysis
consists of an energy method employing assumed pat-
terns or modes of deformation for an unspalled shell
or the unspalled portion of a shell which has undergone
spelling immediately prior to experiencing the subjea
buckling damage. C^namic and static loading tests on
spherical shells have provided data which show the
ap>proximate analysis to afford encouraging results.
Further work is required to investigate the importance
erf strain rate, strain hardening, and elastic energy
effeas, to permit accurate analytical energy-deforma-
tion predictions, and to provide further guidance for
the selection erf appropriate assumed deformation
modes for vArious shell geometries. (Author)
7Qt
Aeronautical Instruments Lab. , Naval Air Develop-
ment Center , Johnsville , Pa .
RADIATION EFFECTS STUDIES ON OPERATING
AIRCRAFT INSTRUMENT SYSTEMS OR COMPO-
NENTS BY FAST NEUTRONS AND GAMMA RADI-
ATION, by M. S. Bergmann and E. ]. Rickner.
Rept. on ProJ. TED ADC AE-70001. 31 Dec 59, 51p.
5 refs. Rept. no. NADC-AI-5957.
Order from LC mi$3.60, ph$9.30 PB 154 535
Some typical aircraft instrument components are
damaged when subjected to an integrated fast flux
above 4(10)^2 m/cm2.
Air Proving Ground Center, EgUn AFB, Fla.
DRAG DATA FOR MC-3, MC-5A, TDU-4/B, AND
TDU-IO/B AERIAL TOW TARGETS WITH VARIOUS
TOWLINES> by Karl D. Kirk, Jr. Dec 60, 39p.
2 refs. APGC-TR-60-65; AD-248 708.
Order from LC mi$3.00, ph$6.30 PB 153 861
This technical report presents drag and altitude
separation data for MC-3, MC-5A, TDU-4/B, and
TDU-IO/B aerial tow targets using various types ot
towlines. These data provide mission planning infor-
mation agd criteria for design of future target and
tow sxifems. In addition, information concerning
:;apabilitles and limitations at items being
djwas obtained. (Author)
U^
Airborne Instruments Lab., Mineola, N. Y.
AN OPERATIONAL EVALUATION BASED UPON
ORNION SURVEY OF RVR AND ALCH AS APPLIED
AT NEWARK AIRPORT, by M. A. Warskow and
W. H. Smith. Rept. on Task 4 of Contraa AMB-16.
Sep 58. 31p. 1 ref. Rept. no. 5791-4.
Order from LC mi$3.00, ph>6.30 PB 154 743
An operational evaluation, based upon the opinions ol
pilot and operational personnel, has been conducted
on the system of measuring terminal weather in effect
at Newark Airport- -that is, Runway Visual Range
(RVR) and Approach Light Conuct Height (ALCH).
Opinion has been obtained from pilots completing an
estimated 518 to 693 approaches out of 2851 ap-
proaches made during the test period- -1 May 1957
through 20 August 1958. Pilot and operational person-
nel decidedly approve the RVR/ALCH system. They
believe it generally gives them a more accurate pic-
ture of terminal weather. Sixty-three percent of the
pilots indicated that the system is "extremely helpful"
and 33 percent indicated "fairly helpful," which
ewers 96 percent of the pilots polled. (One percent
indicated "slightly helpful" and 3 percent did not
answer. ) (Author)
All American Engineering Co. , Wilmington, Del.
EVALUATION TESTS MODEL 56C AND MOCCL
56D RUNWAY BARRIER SYSTEMS, by Mark].
Connor and William R. Schlegel. Final rept. oo Con-
tract FAA/BRD-37. July 60. 105p.
Order from OTS $2. 25 PB I6I 914
This report discusses the program to investigate the
feasibility of utilizing either of two arresting barrier
■jrstems. These barriers are for use in coojuoction
with an emergency arresting gear to prevent overrun
accidents of commercial jet aircraft. The barriers
investigated are Model 56C (Pull-Up) and Model 56D
(Pop-Up) types. Test results (rf actual engagements
with a vehicle simulating a full size aircraft at speeds
up to 60 miles per hour are used to predict perform-
ance up to 120 miles per hour. (Author)
All American Engineering Co. , Wilmington. Del.
FEASIBILITY TESTS OF AIRCRAFT-MOUNTED
ARRESTING HOOK, by M. K. Grevatt. Final rept. on
Contract FAA/BRD-37. July 60, 77p. 2 refs.
Cfrder from OTS $2. 00 PB 161 915
This repon discusses the testing of a tail hook-
equipped transport aircraft under actual arrested land-
ing conditions. The arresting hook installation and the
operation are explained, and the arresting system used
for the tests is described. The test data for both the
static pull test and the actual landing engagements are
presented in both tabular and graphical form and are
analyzed concisely.
Army Transportatian Research Command, Fort
Eustis, Va.
AN ANALYSIS OF THE RESULTS FROM ARMY-
SPONSORED VTOL RE^ARCH AIRCRAFT, by
George I. Schuck. Interim rept. on Proj. 9R38-01-015.
Jan 61, 24p. 5 refs. TREC Technical rept. 61-3;
AD-250 924.
Order from LC mi$2.70, phM-BO PB 154 580
Results of flight tests of several research aircraft are
discussed, with emphasis on handling charaaeri sties
and flying qualities. An attempt is made to relate
characteristics to basic concepts or configurations, as
the case may be. The conclusion reached is that VTOL
fligfit may be achieved by several different methods,
but present controllability is too low for the perform-
ance of any missions assigned to such aircraft.
(Author)
Army Transportation Research Command, Fort
Eustis, Va.
STUDY AND EVALUATION OF PORTABLE AIR-
CRAFT MAINTENANCE HOISTING EQUIPMENT, by
Joseph A. Blanco. Final rept. on Projea 9-38-01-00,
HT-12.103. Feb 61, 23p. TREC Technical rept. 61-7.
Order from OTS $0. 75 PB 171 614
This report covers the testing of a portable tripod
gantry hoist that was designed to aid in the disassem-
bly and assembly of Army aircraft and their major
compjonents. It is a universal-type piece of support
equipment that can be used for maintenance opera-
tions by other technical services. The tripod gantry
hoist is lightweight and portable, is easily erected by
two men, and has a 2:1 safety factor. In addition to
its use as an assembled gantry, each tripod can be
used independently as a hoist. The assembled gantry,
as well as each tripod, has a rated capacity of one
ton. It can be used in sand, mud, clay, and soil.
(Author)
709
Aviation Medical Acceieraticn Lab. , Naval Air
Development Center, Johnsville, Pa.
EXPUaT EXPRESSICWS FOR THE ANGULAR
ACCELERATIOTJS AND LINEAR ACCELERATIONS
DEVELOPED AT A POINT OFF CENTER IN A
GONDOLA MOUNTED WITHIN A THREE GIMBAL
SYSTEM. Oti THE END OF A MOVING CENTRI-
FUGE ARM, by Richard J. Crosble and Robert A.
Hall. Repc no. 7 Oi ProJ. MR005. 15-0005.6.
17 Oct 60, 1^. 4 refs. NADC-MA-6034; AD-248 216.
Order from LC mii2.40, ph$3.30 PB 153 695
A gondola mounted Within a controllable three gimbal
system on the end df a moving centrifuge arm has
the capability of providing a more realistic flight
simulation than is possible with a two gimbal system.
The Human Centrif^e is being modified to provide a
third glmbel (yaw) |o its present roll and pitch gimbal
system and the pro|iosed centrifuge also envisions a
gondola mounted within a three gimbal system. The
present two gimbal system is capable at providing
three degrees at freedom and therefore requires
three control paraiieters; i. e. , the three linear
acceleration command signals ax, ay, az. The third
gimbal will provide) a fourth degree of freedom which
will necessitate an additional control parameter,
presumably an angillar acceleration. The problem d
controlling this extra degree ot freedom has not yet
been satisfactorily resolved. Although no direct solu-
tion to the control i^oblem is offered, equations are
provided which will enable one to calculate both the
angular acceleratiOis and linear accelerations devel-
oped at a point off Renter of the gondola as a con-
sequence of variou$ combinaticxis of gimbal motions
superimposed upon the centrifuge motion- (Author)
Cornell Aeronautical Lab. , Inc . , Buffalo, N. Y.
DESGN OF AN EXPERIMENTAL FAQUTY AND
TEST PROGRAM TO EVALUATE THE EFFECTIVE-
NESS OF PROXIMITY WARNING INFORMATION,
by E . G . Rynaski and W . J . White. Rept . on Contract
FAA/BRD-15. Feb 59, 66p. 10 refs. Rept. no. JA-
1266-S-9.
Order fromLC mi»3.90, ph$10.80 PB 154 744
The specifications have been completed of an experi-
mental program to obtain information on the effective
ness with which a pilot can utilize proximity warning
information. The Experimental equipment required
for this program i( specified in this report. Provi-
sion is made to experimentally evaluate specific
proximity warning
devices . A preliminary statistical
progfam is outlinejd
Fairchild Aircrat [and Missile) Dlv. , Hagerstown,
Md.
ANALYSIS OF THE POWER REQUIREMENT OF A
BLOWING AIRFOIL WITH SLOTTED FLAP, by
H. B. Hebnbold. Rept. on Contraa Nonr- 22 26(00).
22 Apr 58, 58p. slrefs. Engineering rept. R246A-002:
AD- 209 045. , ^
Order from LC m|$3. 60, ph$9. 30 PB 155 146
Thla report released for sale to the pubbc 30 Mar 61.
SUn friction, turdulent mixing, and pressure varia-
tions along the flap cause considerable changes of the
Jet properties from blowing slot to trailing edge. In
the present experiments the Jet momentum flux was
always decreased whereas the jet stiffness was in-
creased under certain favorable conditions. The Jet-
induced lift results from the vorticity of the mixing Jet
sheet downstream of the trailing edge and from the sink
effea of the mixing jet along the flap. Because of nux-
ing the stiffness of the jet sheet increases downstream
from the trailing edge toward infinity. Thus, the con-
tribution of jet -sheet vorticity to the jet -induced lift
becomes greater than predlaed by the theory of the
blowing wing with non-mixing jet. The analysis was
restriaed to states erf flow where the flow was fully
attached to the flap. Under these conditions losses of
wing-circulation Uft are caused by leading-edge sepa-
ration. Reattachment of the flow separated at the lead-
ing edge is, however, favored by the sink effect of the
mixing Jet on the pressure distribution over the suaioo
side of the main airfoil, resulting In an alleviation of
the losses of wing-circulation lift. The influences of
flap-deflection angle, angle of attack and blowing- slot
width ratio on the lift -power relationship are studied
and represented by empirical formulae permitting
extrapolation of this relationship over the range of
power coefficients attainable in the present
experiments.
Fhght Control Lab. , Wright Air Development Div. ,
Wright -Patter son AFB, Ohio.
ANALOG COMPUTER MECHANIZATION OF A TILT-
WING VTOL AIRCRAFT, by Edward B. Balsink and
Donald M Sovine. July 60. llOp. WADD Technical
note 59-344; AD-246 530.
Order from LC mi$5.70, ph$l6.80 PB 155 255
This report released for sale to the public 31 Mar 61.
The techniques used in simulating a tilt -wing Vertical
Takeoff and Landing (VTOL) aircraft are summarized.
A "cockpit" from which the pilot could "fly" the air-
craft was included. Both longitudinal and lateral modes
were used, and wing-tilt was possible. Relatively few
of the usual linearizing assumptions were made, thus
it was possible to "fly" the aircraft throu^ the transi-
tion from hover to normal flight and back to hover .
(AuthOT)
Forest Products Lab. [Madison, Wis.]
SUMMARY OF RESEARCH BY FOREST PRODLfCTS
LABORATORY ON SANDWICH CONSTRUCTIONS
FOR AIRCRAFT, by Donald G. Coleman. Annual
rept. no. 6, Aug 56- -Aug 57, on Rubber. Plastics,
and Composite Materials , Contract AF 33(616)56-9.
Oct 57. 15p. WADC Technical rept. 52-184. suppl.5;
AD- 142 102.
Order from LC mi$2. 40. ph$3. 30 PB 154 955
This repon released for sale to the public 24 Mar 61 .
The approach has been in general to derive design
criteria mathematically and then to check by test.
Seven technical reports issued during the fiscal year
are abstracted. (Author)
710
HlUer Helicopter Corp. . Palo Alto, Calif.
VTOL IX)WNWASH IMPINGEMENT STUDY SUR-
FACE EROSION TESTS, by A. Morse and H New-
bouse. Rept. on ProJ. 9R38-01-017-29, Contract
DA 44-177-TC-655. continuation of Contract
DA 44- 177- TC- 500. Oct 60, 186p. Hlller engineering
rept. no. 60-84; TREC Technical rept. 60-67;
AD-248 356.
Older from LC mi$8. 40. ph$28. 80 PB 153 642
A mobile test rig, mounting a rwo-foot-ducted pro-
peller, capable of providing disk loadings up to 145
Ui/sq ft, was used to provide a cold air jet. This jet
was allowed to impinge upon surfaces which might be
considered unprepared landing sites. The range of
duct exit height above the surface was from one- half
to three diameters, and thrust angle Inclinations of 0,
30 and 60 deg. Surfaces with light vegetation or hard-
packed soil surfaces show little erosion from disk
loadings to 145 Ibs/sq ft. The hard-packed surfaces
normally have fine loose dust on top, which produces
■ large dust cloud even at very low disk loadings. In
general the loose material surfaces erode rapidly,
■nd large holes are formed in a short time. The
gravel, with a mean particle size of about seven mm
and large particles to forty mm, was eroded at a rate
of 150 lbs/sec at a disk loading of 145 Ibs/sq ft. Wet
sand showed minor erosion under the same test con-
ditions. Over water the surface spray started at disk
loadings between eight and fifteen Ibs/sq ft. Between
the disk loadings of thirty to sixty Ibs/sq ft the spray
pattern changes from a radial surface spray to one in
which there is considerable vertical motion and in-
gestion into the duct inlet. (Author)
Kellett Aircraft Corp. , Willow Grove, Pa.
STABILITY AND CONTROL HANDBOOK FOR HELI-
COPTERS, by A. A. Perlmutter. Eugene Kisielowski
and others." Rept. for July 59-June 60 on Contract
DA 44- 177 -TC- 599. Ai« 60, 446p. 54 refs. KACrept.
no. I59A-90-1; TREC 60-43; AD-248 268.
Oixler from LC ml(Il. 10, ph|68. 10 PB 153 851
Methods are presented for the determination of the dy-
aamic stability and the control response character-
istics of single and tandem rotor helicopters. The
methods utilize calculation procedures that are con-
sklerably simplified through the extensive use of infor-
mation plotted in graphs and charts. The effects of de-
sign parameters on the stability characteristics are
discussM in detail. Stability augmentation devices are
surveyed and methods for the evaluation of their
effects are presented. Current military and civil
specifications of handling qualities of helicopters are
incorporated. (Author)
Lift Support Systems Lab. . Wright Air Development
Div., Wright -Patterson AFB, Ohio.
HUMAN FACTORS RESPONSES DURING GROUND
IMPACT, by Robert N. Headley, James W. Brinkley
•ad others. Rept. for 1959 on Biophysics at Fhght.
Nor 60, 35p. 10 refs. WADD Technical rept. 60-590.
Order from OTS $1.00 PB 171 599
Forty-six vertical impact experiments were coixliicted
ualng a simulated B-70 escape capeule and eleven
seated human subjects (-f Az). Three drops are re-
ported. Impact velocities rang^ from 9. 8 to 30ft/bec.;
a crushable paper honey comb material was the impact
attenuator. Three restraint systems were tested. Ac-
celerometer data revealed mean rates of onset of de-
celeration as high as 1620 g/sec. with max g- loads to
35 g. The only noteworthy finding of pre- and post-test
clinical examinations was one case at microscopic
hematuria lasting one month. The conclusion was that
impaa decelerations of 24 g with a velocity change of
30 ft /sec. and a 500 g/sec. rate of onset can be
tolerated by using a proper body restraint system,
good upper torso support, proper torso and neck
positioning, and by eliminating all possible elastic
recoil components. (Author)
Minnesota U. , MlnneapoUs.
EXPERIMENTS OH SUP DAMPING AT ROUNDED
CONTACTS, by L. E. Goodman and G E Bowie. Rept.
for 30 June 58-31 Dec 59 on Metallic Materials. Con-
traa AF 33(616)6828. Nov 60, 78p. 11 refs. WADD
Technical rept. 60-161, Parti.
Order from OTS |2. 00 PB 171 594
This report describes an apparatus for studying slip
damjping at the cootacts of a sphere with two flat paral-
lel plates. A load of constant magnitude is apphed
normal to the plates and the sphere is driven in a di-
rection tangential to the plates by an electrostrictive
device operated at 60 cycles per second. Experimental
results obtained with a one half inch diameter type 316
stainless steel sphere pressed between flats of the
same material are pjresented. They are in fair agree-
ment with theoretical predictions by R. D. Mindlin et al
Results for pyrex glass differ from those for stainless
steel and are not compared with theory . Suggestions
are made for future work on conua problems.
(Author)
National Research Lab«. , Ottawa (Canada).
WIND TUNNEL AND STATIC THRUST MEASURE-
MENTS ON A FOUR- BLADE CONSTANT CHORD
PROPELLER, by R. H Wlckens. 20 Oct 60. 47p.
8 refs. Aeronautical rept. LR-29I.
Order from LC ml$3. 30. ph$7. 80 PB 154 549
Experiments have been conducted in order to evaluate
the cruising and static performance of a high solidity
model propeller. The results of the investigation re-
vealed that the propeller was not highly efficient in
the cruise (V * 0. 72) when compared with current
full-scale designs. Static thrust data indicated high
performance at small blade angles and low tip speeds.
Measurements made in the wind tunnel of slipstream
total pressure and flow rotation indicated evidence of
tip stall and significant slipstream rotation. A simple
theory for the calculation of slipstream flow angle
shows fair agreement with experiment. (Author)
Santa Barbara Dlv. , Curtiss- Wright Corp. . Calif.
VZ-7AP AERIAL PLATFORM RESEARCH, by Walter
R. Wolf, Jr. Pinal engineering rept. 17 July 57-
31 Aug 60, on Contraa DA 44-177-tc-397. Aug 60,
148p. 36 refs. S8D rept. no. TR 60-37; TREC-60-59;
AD-248 716. •
Order from LC ml$7. 20, ph$22. 80 PB 153 859
711
The VZ-7AP has detnoostrated the feaaibiUty of the
4 rotor vehicle cx)n4ept as applied to the over -all
military aerial jeeii concept. Test results indicate
that: (1) it is highly maneuverable, (2) it can be flown
by a relatively inexperienced pilot, (3) it is easily
controlled about all 3 axes without use of subility
augmenting equipment, (4) it can hover either in or
o\X. of ground effectj (5) it can translate in any direc-
tion, (6) it can fly af. speeds comparable to ground
vehicles, (7) it can carry a substantial payload, and
(8) it is both ruggec and reliable. (Author)
Standard Pressed 5ieel Co. , Jenklntown, Pa.
BERYLLIUM FASTENERS, by Edward F. Gowen, Jr.
Final technical engineering repc. for 12 June 59-
29 Jan 60 on Conlrafct AF 33<600)39728. Aug 60. 70p.
AMC Technical repi. 60-7-807; AD-247 525.
Order from LC mi«. 90. phJlO. 80 PB 155 086
This report- released for sale to the public 24 Mar 61.
Lighter structures [for high performance aerospace
vehicles may be possible through the use of shear type
bolts made from beryllium. On a strength -to- weight
basis, beryllium b^lts are stronger in all respeas but
more costly than sqeel or titanium bolts of suitable
configurations for iimilar applications. Room tem-
perature double sh4ar strength of bolt shanks was over
60, 000 PSl (65% of ^he strength of the base material
tensile strength for beryllium versus 60% for steel and
titanium) which is ^uivalent to 400, 000 PSI steel and
200. 000 PSI titaniuii bolts on a strength-to-weight
basis. However, beryllium is not reconrunended for
tension type faAen^rs because erf its high degree of
notch sensitivity. $est bolt properties were otxained
by upset forging pure extruded beryllium bar stock
at l450O-1500°F with subsequent rolling of threads
corresponding to t^e MIL-S-7742 thread profile modi-
fied for a rounded root. Best thread depth to the point
of tangency of the foot was 55% of the theoretical
depth. Aluminum $ut8 were superior to steel nuts and
could be reused m4ny times. Bolts with rolled threads
had tensile strengths 50% higher than equivalent ma-
chined threads. Sliear properties two to three times
superior to those of ground (12 microinch finish) bolts
resulted from surface treatment to 27 microinch
finish by etching iil a chromic-phosphoric -sulfuric
acid bath. Exhaus^ systems are necessary when
machining and griiiding so as to prevent machine
operators from being exposed to beryllium and
beryllium oxide pafiicles. (Author)
Whittaker Contrcts, Los Angeles, Calif.
LIQUID OXYGEN TANK. VENT AND RELIEF
VALVES. byVem'Smith. Final rept. on Contract
AP 04(647)162. 29' Sep 59. 263p. Rept. no. 2000-11;
includes rept nos. D-122206-(l-4); AFBMD Doc
no. 9-10.272.
Order from LC m^ll. la ph»4J. 10 PB 153 611
The purpose of thei program was to develop a valve
which represented' an advancement in the 8tate-o*-the-
art in design, perlormance. methods of fabrication,
and methods of teeing. Simultaneously, the valve was
to be compatible With the requirements for an existing
missile to permit flight -test following development.
Chemical Engineering
California U . , Los Angeles .
THERMODYNANQC AND ECONOMIC CONSIDERA-
TIONS IN THE PREPARATION OF FRESH WATER
FROM THE SEA. by Myron Tribus , Robert Asimow
and others . Rept. on Sea Water Research. Sep 60,
169p. Dept. of Engineering rept. 59-34.
Order from LC mi$7.80. ph$25.80 PB 154 245
This Tepon is concerned with the following problenw:
Given the unit costs for various pieces of equipment
and for differing sources of energy, how should the
items of equipment be combined to produce fresh
water from sea water at the lowest possible cost?
How sensitive is the cost of fresh water to separate
changes in unit costs of equipment and energy? What
are the lowest attainable costs for water using avail-
able technology and current unit costs? The answers
to these questions appear as equations , in which the
cost of fresh water is expressed in terms of unit costs
and conventional operating parameters for engineering
equipment. Each supposition upon which the cost
figure is based thereby stands clearly revealed and
accessible for discussion. The attainment of simple
equations is only made possible by drastically simpli-
fying, the analyses. The results of these studies show
relations annong the value of resources and the cost d
the water produced .
Naval Civil Engineering Lab. , Port Hueneme. CaHf.
ENVELOPMENT OF AN EXPERIMENTAL CHLO-
RINE INFUSER AND CHEMICAL FEEDER, by
J. R. Dawes, H. Hochman. and J. J. Doman.
21 Aug 56, 23p. Technical memo. M-113.
Order from LC ml$2. 70. ph$4. 80 PB 154 615
A six per cent chlorine hypochlorite slurry can be
made from liquid chlorine, dry chemical, and water
by using a simple device built around an educator. No
power is required other than that necessary to supply
100 psi of water at a nomianl rate of 25 gpm. Under
these operating conditions the discharge produced is
suitable for direct spraying. (Author)
Naval Civil Engineering Lab. . Port Hueneme, Calif.
ELECTROLYSS OF SEA WATER, byT. Roe. Jr.
and H. Hochman. 10 May 57, 15p. Technical note
N-300.
Order from LC ml»2.40. ph$3.30 PB 154 679
Two electrolytic cells for the production of sodium
hypochlorite from sea water were designed and fabri-
cated. Data from their operation under varying condi-
tions of flow rate and current density showed that both
are capable of producing 2000 ppm available chlorine
from sea water in a single pass . Addition of 1 lb per
gal of salt to sea water gave more than twice as much
available chlorine In the effluent as sea water at com-
parable flow rates and current densities . Multiple
pass runs of the effluent increased the available chlo-
rine concentration to a maximum which was related
to the temperature rise. Recommendations are made
for Improved cell design and use of cooling equipment
to lower the rate of decomposition of the sodium hypo-
chlorite produced . (Author)
712
[Naval Engineering Experiment Station. Annapolis,
Md.l
EFFECTIVENESS OF THERMAL SHOCK FOR
SCALE PREVENTION IN LOW PRESSURE EVAPORA-
TORS. byG. R. Garber. 30 Sep 55, 16p. Evaluation
rept. 010058M.
Order from LC mi$2. 40, phJ3. 30 PB 155 565
This report released for sale to the public 19 Apr 61.
A comparison was made of thermal shock treatment
and Navy boiler compound-starch-thermal shock treat-
ment (Navy standard) to determine scale preventive
characteristics in low-pressure sea-water evapora-
tors. When judged on the basis of shell vacuum, the
controlling factor, standard Navy treatment was
significantly better than thermal shock alone. Both
were markedly better than no treatment. (Author)
Naval Research Lab. . Washington. D. C
SURFACE CHEMICAL METHODS OF DISPLACING
WATER AND/OR OILS AND SALVAGING FLOOCCD
EQUIPMENT. PART I: PRACHCAL APPUCATIONS,
by H. R. Baker, P. B. Leach and others. Interim
rept. 23 Feb 61, 24p. 19 refs. NRL rept. 5606.
Order from OTS $0. 75 PB 171 479
The effectiveness of surface -active substances in dis-
placing Navy Special fuel oil and water from soUd sur-
iicea has been demonstrated. A general mechanism is
outlined for the rapid displacement of one liquid by
another as a result of unbalanced surface forces. Two
formulations have been developed, one for the dis-
placement of fuel oil and the other for the removal of
water from electrical, electronic, or mechanical
equipment. Both formulations are relatively harmless
to most electrical and electronic insulation. The fuel-
oil-cleaning emulsion retards rusting ot the ferrous
metals with which it comes in contact, while the water
displacing composition leaves a persistent and effec-
tive rust inhibiting film over the surfaces of the equip-
ment. Electrical and electronic components which had
been submerged in a mixture of Navy Special fuel oil
and sea water were effectively salvaged by treatment
with the fuel-oil-cleaning emulsion and the water-
displacing composition. An integrated procedure is
outhned for the recovery of electrical, electronic, or
mechanical equipment after such submersion. A
method of sealing the insulated parts of electromotive
equipment against the penetration of flooding water is
also presented. (Author)
Office of Scientific Research and Development.
Dlv. 9.
PREPARATION OF CHLOROAMIDES S-46I, S-328,
S-330, S-426, S-222, S-300, S-22I, S-436, AND
DECONTAMINANT 40, by R. T. Major, W. H, Engels
■ttl others. 17 Oct 45. declassified 1 June 58. 107p.
OSRD-6111: ATI-30 719.
Order from LC ml|5.S0, ph$l6.80 PB 154 875
This report released for sale to the public 27 Mar 61.
Ibe results at latxnratary development, pilot plaot,
■ad chemical engineering studies d preparation at
S-461, S-328, S-330, S-426. S-222. and S-300 as well
as S-221, S-436, and Decontamlnant 40 are summa-
rized, llie possibility of using S-461 in ointments and
protective clodiing led to the pilot plant study. The
process for producing S-328 was develc^ied for the
purpose of securing an impregnite other than CC-2,
which mi^t be used in the solvent system at impreg-
nation. A study of the process for producing S-330
from benzil and ur6a was investigated. S-426, S-222,
and S-300 are produced from the same starting mate-
rials as is S-330. It is shown that S-436 produced
from benzontrile and cyandiamide was more attractive
than any other chloramide for protection against the
nitrogen mustards.
Civil Engineering
Naval Civil Engineering Lab. , Port Hueneme, Calif.
CHEMICAL STABIUZATION OF BEACH SAND, by
C. V. Brouillette. 1 Dec 54, rev. Sep 56. 61p.
Technical memo. M-096.
Order from LC mi$3.90. ph$10.80 PB 154 632
A description of the diamine modification of the
aniline-furfural (Formulation X-72) method of pro-
ducing roadways in beach sand is given. This memo-
randum was prepared for use by amphibious person-
nel and includes personnel requirements and safety
precautions . An alternative formulation (S-1) is
discussed. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
DEHUMIDIFICATION OF ACTIVE WAREHOUSE BY
MEANS OF SELECTIVE VENTILATION AND
COMFORT HEATING, by Warren Viessman.
30 Apr 51, 6p. 10 refs. Technical note N-021.
Order frxjm LC mi$l. 80, ph|1.80 PB 154 638
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
DESIGN, DEVELOPMENT AND EVALUATION OF A
20- FT BY 48- FT STRAIGHT -SIDED. GABLED-
ROOF, PREFABRICATED STEEL BUILDING, by
W. R. Masonand J.E. Schroeder. 10Dec53, 48p.
8 refs. Technical memo. M-080.
Order from LC mi$3. 30. ph$7. 80 PB 154 628
The 20-ft by 48-ft straight-sided, gabled-roof, pre-
fabricated steel building was developed to fulfill the
need for a standard building. Evaluation of the design
included a study of packaging and crating; erection;
weathertightness; and structural adequacy for speci-
fied snow, wind, and floor loadings . The building was
satisfactory with the exception of the structural inade-
quacy of the floor sills . A redesign was initiated to
correct this deficiency and to have the building com-
ply with the criteria established by the Defense Sup-
ply Management Agency for a standard building for all
services . An eight-foot section of the new floor de-
sign was fabricated and tested and found to be struc-
turally adequate. The redesigned building proved to
be low in shipping cube (202.0 cu ft), low in steel
weight (62(X) lb) and able to be easily and rapidly
erected. (Author)
713
Naval Ovil Engineering Lab. , Port Hueneme, Calif.
DESIGN, DEVELOPMENT AND EVALUATION OF A
25- FT BY 48- FT, DISA^ER SiELTER, by
W. R. Mason and J. E- Schroeder. 3 Apr 53, 29p.
4 refs. Final tecimlad memo. M-08L
Order from LC ml$470, ph$4.80 PB 154 629
The 25-ft by 48-ft Disaster Sielter was designed,
developed, and evalu«ted to fulfill the need for emer-
gency shelter in the «vent of a major disaster. The
design and developing included a close analysis and
revision of the exlstltig criteria and thorough studies
at materials. The evaluation included erection studies,
weathertightnes s tescs, and structural tests to deter-
mine its adequacy fo^ withstanding the specified loads.
The building was scn)aurally adequate, boch simple
and rapid to erect, essentially weathertlgbt. and
economical in cost a^ use d materials. (Author)
a^
Naval Civil Engineering Lab. , Port Hueneme, Calif.
DEVELOPMENT OF AN IMPROVED PONTOON
SYSTEM, by W. R. Mason and R. C. Towne. 3 Aug 55,
69p. 17 refs. Technical memo. M-106.
Order from LC ml|3^ 90. ph$10. 80 PB 154 614
Description of an improved pontoon system, con»-
parable both structuually and operationally to the
present design, is given. The improved design is less
costly, easier to fabricate, requires fewer parts, and
is more quickly assembled Report Includes also an
analysis of present pontoon gear and a study d manu-
facturing problems apd costs. (Author)
Naval Civil Engineering Lab . , Port Hueneme , Calif .
DEVELOPMENT OF AN INSTRUMENT PILE TO
MEASURE LATERAl. THRUST EARTH PRESSURES,
by R. J. Lowe. Interim memo. 31 May 51, 48p.
4 refs. Technical mfmo. M-036.
Order from LCmi»3, 30, ph»7. 80 PB 154 623
To obtain the in-place properties of deep soil deposits
in relation to pile foundations , a test instrument pile
for measuring the e4rth'8 reaction along the embed-
ded length of a pile Subjected to lateral loads was de-
veloped , fabricated .; and tested . The Mark I instru-
ment pile consisted Of a 41-foot, boxed, lightweight-
steel I-beam with eight pressure and deflection gage
stations at 5-foot in^rvals on each of the wide faces .
The bottom of the pi|e was fitted with a 1-foot-long
driving shoe, and the upper end was open. The first
sand embedment test was unsuccessful because of
lack of adequate waterproofing. Test results of the
second sand embedr^ent test were erratic , anribuied
primarily to flexibility and narrowness of the basic
section and inefficielKy of the pressure gages .
Different subsurface deflection curves were obtained
by increasing the lateral movement of the pile at the
surface, however, d» sinusoidal curve assumed in
theory was approach as the surface movement was
increased. (Auihorjl
Naval Civil Ei^lnerrlng Lab. , Port Hueneme, Calif.
DEVELOPMENT OI* EVALUATION PROCEDURE
FOR LOAD TRANSFER CCVICES, by J. R. Keeton.
Interim rept. for F^b 57 on tavestlgation d Load
Transfer In Paveme<it8. 30 Apr 57, 55p. 4 refs.
Technical note 299.
Order from LC mi». 60, ph|9. 30 PB 154 678
The results herein reported Indicated that the radius
of relative stiffness (L) as measured by the extent of
slab deflection under load is considerably greater dian
would be expected from a theoretical analysis at the
slab. This appears to indicate a need for re-exami-
nadon of the basic design equations for joints. The
results also show that in all probability an evaluation
procedure for load transfer devices can be developed
with relative slab deflection under load as the princi-
pal criterion. (Author)
Naval Civil Engineering Lab. . Port Hueneme, Calif.
EVALUATION OF "HUENEME BUILDING, ' A 20- BY
48-FT STRAIGHT- SIDED, GABLEr>ROOF. PRE-
FABRICATED STEEL BUILMNG, by J. E. Dykins.
1 June 55, 34p. 6 refs. Technical memo. M-104.
Ortler from LC mi$3. 00. ph$6. 30 PB 154 613
This memorandum covers the evaluation of a pro-
duction model of "Hueneme building, " including a
study of packaging and crating, erection, weather-
tightness, and structural adequacy for specified snow,
wind, and floor loadings. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
EVALUATICW OF LARGE PONTOON (10' X 20' X6'X
by J. V. Sulcup. Interim rept. 25 May 56, 15p.
Technical note N -267 .
Onier from LC mi$2.40. ph»3.30 PB 154 672
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
EVALUATION OF THE STANDARD 40- FT BY
100-FT, ARCH RIB, METAL UTIUTY BUILDING,
by J . E . Dykins . 1 Feb 54 , 25p . 2 ref s . Final techni-
cal memo. M-048.
Order from LC nu$2.70, ph$4.80 PB 154 625
The Standard Arch Rib. 40- ft by 100-ft, Prefabricated
Metal Utility Building was evaluated to determine its
adequacy for advanced base use. The evaluation in-
cluded a study of packaging and crating, ease of erec-
tion, and structural adequacy for the specified snow
and wind loadings . It was found by test and observa-
tion that the building can be packaged for overseas
shipment in 386.80 cu ft with a gross weight of
21 ,853 lbs; erection of the building was accomplished
in 398 manhours , using a six man crew , a crane with
operator, and a large pneumatic tired fork lift as an
erection aid. The building was found structurally in-
adequate under the structural loadings specified by
Military Specifications . (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
EXPERIMENTAL ARCTIC OPERATION . HARD TOP
II, 1954, by W. R. Reese. Rept. on Snow Compactioa
29 Dec 55, 364p. 46 refs. Technical rept. R-007.
Order from LCmi$ 11.10. phJ56. 10 PB 154 619
HARD TOP II was a continuation of HARD TOP 1 .
The camp was rehabilitated and enlarged and a run-
way system of main and auxiliary runways was con-
structed using several variations of pulvimixer- roller
technique. Successful C-47 operational tests were
conducted. Further evaluation was made of logistical
problems , camp construction , maintenance and
human factors , and a mechanical process for cm
itiuction runways by compacting snow. (Author)
con-
714
I
Naval Civil Engineering Lab . , Pon Hueneme , Calif.
FIELD ASSEMBLY AND TRAFFIC LOADING TESTS
OF A PORTABLE, PRESTRESSED TIMBER ROAD-
WAY, TEN -TON CAPACITY, DESIGNATED AS
MODEL X-2, by P. J. Rush. 19 Oct 54, 37p. 6 refs.
Technical note N-202.
Onler from LC mi$3.00, ph$6.30 PB 154 663
A portable roadway of prestressed timber was de-
signed for the purpose of supplying a traffic -way capa-
ble of susuining vehicles up to 20, (XX) lbs gross
weight in passages over so-called impassable terrain.
One hundred and fony-four linear feet of this portable
roadway, designated as Model X-2, was emplaced at
an area of extremely low-bearing soil at Laguna
Mugu, California. Over five hundred traffic passes
and more than fifty static loadings , of wheeled and
tracked vehicles of gross weights ranging up to
74,125 lbs , were made on the portable roadway. No
serious structural damage was evident during or after
the field tests . Deterioration of the supponing soil
was apparent during and after loadings in excess of
50,(XX) lbs . Assembly methods employed during the
field tests were not rapid enough for tactical purposes
A portable roadway development program based on
the prestressed timber principle and concerned with
increased load capacity, reduction of soil deteriora-
tion, and rapid assembly procedures is continuing
and will be the subject of future reports . (Author)
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
nBLD TESTS ON LATERALLY LOADED INSTRU-
MENT PILES, FIXED-HEAD LOADINGS IN SAND,
FREE- HEAD LOADINGS IN CLAY, by H. G. Mason.
15 Oct 56, 27p. 2 refs. Technical note N-276.
Order from LC mi$2. 70, ph^4. 80 PB 154 673
Details of the instrumentation used to obtain a fixed-
head loading condition for static and repetitive testing
•re described . The effect that the degree of fixity has
op the pressure and deflection patterns is discussed.
A comparison is made between the measured deflec-
tions and pressures and the theoretical deflection and
pressure patterns as developed from the Palmer-
Thompson theory. A method is presented by which the
Navy facilities may have lateral thrust pile problems
solved by IBM calculations at nominal costs . Also
presented are details of the instrumentation used in a
pile embedded in 40 feet of clay soil , including a new
electronic pressure cell. Results of the "at rest"
pressure studies are presented. (Author)
Naval CSvll Engineering Lab. , Pon Hueneme, Calif.
HEATING AND VENTILATING ARCTIC HUTS, by
R. P. Uw. 1 June 53, 38p. Technical note N-145.
Order from LC ml$3. 00, ph$6. 30 PB 154 653
The purpose d this investigation was to improve the
overall efficiency of the heating and ventilating system
<leveloped by the Laboratory during the winter of
1951-1952 under project Polar Camp Heating and
Ventilating, and to establish standard procurement
■pectflcations for Its components.
Naval Civil Engineering Lab. , Pon Hueneme. Calif.
HEATING SYSTEM FOR A PERSONNEL WANIGAN.
by K. B. Edwards and Warren Vies s man. Interim
memo. I Feb 52, 22p. 8 refs . Technical memo.
M-033.
Order from LC mi$2. 70. ph$4. 80 PB 154 621
Two under-floor, warm-air heating systems are pro-
posed for use in arctic wanigans . One system utilizes
an atomizing forced -air burner and a circulation fan,
and the other makes use of a vaporizing pot burner in
a selective gravity or forced-air heating system. In
the latter system, forced-air circulation would be
available when required by the weather and air-tem-
perature stratification conditions . In the event of
power failure, sufficient heat for survival would still
be available. Both systems have supply ducts and re-
turn plenums below the floor level . Using typical
wanigan wall and roof constructitm, 55,000 Ekuh is
expected to provide 24 per cent is excess of the heat
requirements to house twelve men comfonably when
the out-side temperature is -40 F, and 2.5 per cent
In excess when It is -65 F. (Author)
Naval Civil Engineering Lab. , ft)rt Hueneme, Calif.
IN-SERVICE TEST EVALUATION OF 20- BY 48-FT
STRAIGHT- SIDED, GABLED ROOF, PREFABRI-
CATED STEEL, "HUENEME" BUILMNG, by J. E.
Dykins . 15 Nov 55, 20p. Technical note N-232.
Order from LC nu$2.40, ph$3.30 PB 154 666
Buildings were procured for in-service testing within
the Navy establishment. The using agencies were to
complete the questionnaires furnished them covering
the receiving and handling, erection, and performance^
phases of their buildings . This repon covers the eval-
uation of the "Hueneme" building from the data com- /
piled from the in-service test questionnaires .
Naval Civil Engineering Lab. . Pon Hueneme, Calif.
INSTRUCTION MANUAL FOR ALL WINTERIZED
EQUIPMENT, by E. J. Beck. Rept. on Proj . Deep-
freeze. 22 Nov 55, 22p. Technical note N-244.
Order from LCmi$2. 70. ph$4. 80 PB 154 669
The wlnterlzatlon equipment as described below has
been developed to facilitate the operation of conven-
tional equipment under low temperature conditions
with a minimum of special techniques , training, and
changes to the equipment .
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
INSTRUCTION MANUAL FOR SKID- MOUNTED
LUBE OIL CARRIER (500-GALLON), by E. J. Bedc.
Rept. on Proj. Deepfreeze. 19 Oct 55, 19p. Techni-
cal note N-255.
Order from LC mi$l. 80. ph$l. 80 PB 154 671
The Arctic LiAe Oil Carrier Is a portable, insulated
supply tank for storing, heating and handling viscous
lubricating oils at very low temperatures. (Author)
Naval Qvll Engineering Lab. , Pon Hueneme, Calif.
INSTRUCTION MANUAL FOR SLED-MOUNTED
WATER CARRIER (1000 GALLON). i)y K. N. Tlnkle-
paugh. Rept. on Proj. Deepfreeze. 19 Oct 55, lOp.
Technical note N-249.
Order from LC ml$l. 80, ph$l. 80 PB 154 670
/•
715
The Water Carrier \i an insulated, sled-mounted,
1, 000 gallon tank, \«^th pumping and heating equipment
to allow: (1) pumpin| a tankful at water frcan an out-
side lake or tank; (^ heating at the water during
transit or standby; <p) snow melting to obtain water.
Naval Civil Engln^ring Lab. , Port Hueneme, Calif.
INSTRUMENTATION OF SAN NICOLAS DIESEL
ENGINE POWER PLANT ENGINES WITH BOILING
CONDENSING COOLING, by Earl J. Beck. Supplemen
lal rept. 7 May 58.lrev. 16 June 58. 28p. 2 refs .
Technical note N-3j7.
Order from LC miM.70, ph$4.80 PB 154 683
The initial instrumantation was designed primarily to
detect possible sealing ring problem areas , but
allowed partial analysis of the heat transfer and tem-
perature distribution in the area of junction of cylin-
der and head, including the ui^r ponion of the piston
ring travel. The analysis, with isothermal plots un-
der four conditions pf loading and cooling is given, in-
cluding one run with forced circulation of low temper-
ature coolant . A prpposal for simple but more pre-
cise instrumentatioi of one of the two 8-cylinder en-
gines to be installed on San Nicolas Island is made.
From the tests mad^, it was concluded that probably
critical metal temperatures were well within estab-
lished safety limits i (Author)
Naval Ovll Engin^ring Lab. , Port Hueneme, Calif.
INVESTIGATION OF GLARE PROBLEM, BUILDING
253, SAN FRANCiaCO NAVAL SHIPYARD, by D. R
Wright. 10 Apr 52
TN-086.
Order from LC mljfe. 40, ph$3
19p. 16 refs. Technical note
30
PB 154 647
Naval Civil Engineering Lab. . Port Hueneme, Calif.
JACKETING OF TIMBER PILES: INTERIM REPORT
OS JACKETS WITrtiN THE TIDAL RANGE, byP. H.
Ftetersen. 19 Jan 56. 16p. Technical note N-241.
Order from LC miJjZ. 40. ph$3. 30 PB 154 668
The primary objectives al this phase erf the study
were: (a) to observ^ the problems relating to forming
and placing the jacket, (b) to obtain a comparison o*
tbe beiidi/% strengtll at the jacketed portion at pile with
that at a sound pile,, and (c) to compare the relative
costs at each methqd.
Naval Civil Engfintering Lab. , Port Hueneme, Calif.
OIL- SLICK REMOVAL BY THE ABSORPTION
METHOD, by S J. Weiss and C- W. Davis, Jr.
1 Aug 52, aC^ Tedinical note N-106.
Order from LC mli2.70, ph$4.80 PB 154 648
An oil-slick removil machine employing an endless
felt belt was desigaied and constructed. Operational
tests of this machine have demonstrated that this
method of utilizing ^e absorption charaaeristics of
felt is not an effective manner of oil-slick removal,
primarily because 0ie wave action set up by passing
water-borne traffic causes surging of the belt and
repulsion of the oil^slick. No further action is recom-
mended. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
PORTABLE ROADWAY, MODEL X-3, PRESTRESSED
TIMBER, SIXTY-TON CAPAQTY, by P. J. Rush.
21 Mar 55, 47p. 5 refs . Technical note N-216..
Order from LCmi$3. 30. ph$7. 80 PB 154 665
This note describes the design, fabrication, field test-
ing, and analysis of a prestressed timber roadway
structure intended to support the heaviest combat ve-
hicle traffic across soils whose bearing capacity
would not support the weight of a walking man. In
field tests 160 lineal feet of roadway were placed, and
many passages of wheeled vehicles up to 46 tons gross
wei^t and tracked vehicles up to 57 tons gross weight
were performed. No deterioration of the structure
occurred. Some soil deterioration was apparent at
the greater magnitudes of loadings , mostly occurring
at a point where a water channel passed beneath the
structure. Assembly time in the field was at a rate of
34 lineal feet per hour; although assembly rates of 82
lineal feet per hour were accomplished in practice on
firm, irregular ground. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
PORTABLE ROADWAY, X-4, 60-TON
CAPAQTY, FOR UNSTABLE-TERRAIN AREAS, by
P. J. Rush. 19 Jan 56, 25p. 6 refs. Technical note
N-240.
Order from LC mi$2.70, ph$4.80 PB 154 667
This note describes the development of a prestressed
timber roadway structure intended to support 60-ton
traffic loadings across so-called impassable areas of
mud or other extremely low-bearing-capacity soils.
Assembly of the structure was performed at the rate '
of 73 lineal ft p^r hr by a crew of 18 men. Sixty
traffic loadings with heavy wheeled and tracked vehi-
cles were performed. A static loading test employing
a weight of 90 tons upon a simulated 60-ton unk tread
was performed. No structural deterioration of the
roadway occurred as a result of the loading tests .
Displacement of the supporting soil occurred under
loadings greater than 50 tons , resulting in a settle-
ment of the structure but in no impairment of its load-
carrying ability. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
SIDE LAUNCHING OF PONTOON STRUCTURES, by
R. C Towne. Supplemental rept. 14 Jan 57, 20p.
3 refs. Technical memo. M-122; Supplement to Tech-
nical memo. M-110; AD-136 863.
Order from LC mi$2.40. ph$3. 30 PB 154 682
The amount of barge reinforcement which would be re-
quired to assure two successful side launchings using
a 3 X 12 pontoon barge mounting an 02D or 06DH pro-
pulsion unit on the outboard string was investigated.
Launchings at 4-ft to 8-ft heights were specified. This
report describes 14 side launching tests at 4-ft to 8-fl
heights of two 3x12 pontoon barges: seven tests using
a barge assembled with P-1 and P-2 pontoons and an
equal number using a barge with T6B and T7A assem-
bly. In all of the tests a simulated 06DH unit was
mounted on the center of the cutboerd strings. The
test results show that (I) a barge carrying apropulslpo
unit on the outboard string can be reinforced to with-
stand the impaa of two side launchings and still be
716
operable, (2) damage to the structure will consist of
indentation of the pontoon bottom plates and minor
buckling of the deck plates directly under the propul-
sion unit, (3) subsequent launchings eventually will
cause the pontoons to leak by failure of pontoon corner
seams, and (4) the present 06DH propulsion unit does
not appear to be capable of withstanding, without dam-
age, the forces caused by the large decelerations oc-
curring during side launching. (Author) (See also
PB 128 226)
[Naval Civil Engineering Lab. , Port Hueneme,
Calif. 1
SLAB FLOORS ON PERMAFROST A MODEL
STUDY, by J. M. Stephenson. 29 Sep 60, 61p. 4 refs.
Technical note N-392.
Order from LC ml|3. 90, ph$10. 80 PB 154 700
Building foundations which will remain stable for the
life of their superstructure are difficult to construct in
permafrost areas. At present, as one example of pro-
ducing stability, buildings are raised several feet on
piles set in the permafrost. Conventional slab floors
were studied as a substitute for piles in a model test
environment built to simulate a permafrost area and
its seasonal soil and air changes. Dimensional analy-
sis appropriately scaled the time, temperature and
linear dimensions. A small refrigeration coil, placed
under the slab of the model building, attempted to
keep constantly frozen soil beneath the model. The
test was mainuined for 43. 5 days, equivalent to 3
years of full scale slab, and soil temperatures were
taken under and around the model floor. The results
showed too much thawing at the soil and a slight rise
in floor elevation. (Author)
f4aval Civil Engineering Lab. , Port Hueneme, Calif.
SLIPPAGE OF SPUT-RING CONNECTOR JOINTS IN
UNSEASONED LUMBER, by P. J. Rush. 14 May 53,
31p. 4 refs . Technical note N-149.
Order from LC mi$3.00, ph$6.30 PB 154 654
Two groups, comprising sixteen specimen joints in
each, were subjected to sustained loadings for periods
of 60 days and 90 days , respectively. Specimen lum-
ber for the 60-day test period was unseasoned Dou-
glas Fir stock obtained from a commercial yard;
while specimen lumber for the 180-day test was ob-
tained from fresh cut Douglas Fir logs brought from
Oregon. Control specimens, of seasoned Douglas
Fir lumber obtained from the Construction Battalion
Center yard, were used in both 60-day and 180-day
tests . Both sets of specimens were instrumented to
provide information regarding temperature and humid
ity fluctuations , nwisture content changes , dimen-
sional changes , and displacements in joints . Data ob-
uined from the experiment is presented in tabular
and graph form . (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
SNOW-COMPACnON EQUIPMENT, SNOW PLANES,
byE. H. Moser. Jr. Final rept. 9 Feb 61, 34p.
ISrefs. Technical rept. 110.
Order from LC mi$3. 00, ph$6. 30 PB 154 463
Two sizes of snow planes were developed for leveling
and grading snow in the construction oif compacted-
snow areas by the Navy cold-processing techniques.
One has a 40-foot span and the other an 80-foot span.
(Author)
Naval Civil Engineering "Lab. , Port Hueneme, Calif.
STUDY OF THE MOBILITY OF VEHICLES AS RE-
LATED TO TRAFFICABILITY OF TRACTION
MECSA, by S. J. Weiss. 15 Jan 54, 30p. 16 refs.
Technical memo. M-084.
Order from LC mi$2. 70, ph$4. 80 PB 154 630
This report is a summary erf the work conducted in re-
lating the external performance of off-the- road vehi-
cles to measurable characteristics of the terrain.
The importance of the shear strength cf the soil to its
ability both to support vehicle loadings and to allow
the creation of tractive effort for the propulsion of the
vehicle has motivated consideration of a portable, di- ,
rect shear apparatus as a trafficability instrument.
Presented herein is a possible form of such an appa-
ratus and an approach to performance prediction made
possible by its utilization. Over-all success in
achieving the ultimate objective of reliably estimating
the soft ground performance of vehicles by these
methods and techniques will depend upon continued
theoretical development of the fundamental relation-
ships between soil and vehicles. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
T6B PONTOON ASSEMBLY PROCEDURE FOR AD-
VANCED BASE P-10 COMPONENT, by W, R. Mason
and R. C Towne. Rev. 21 Sep 56. Technical memo.
M-102.
Order from LC ml|3. 60, ph|9. 30 PB 154 633
Naval Civil Engineering Lab. , Port Hueneme, Calif.
TEMPORARY PROTECTIVE SHELTER: CONSTRUC-
TION AND PERFORMANCE TESTS. byE. P. Donoghue,
E. H. Moser and W. Vies s man. 1 Aug 50,
declassified. 83p. 10 refs. Technical rept. R-002.
Order from LCmi$4.80. ph$l3.80 PB 154 617
A project was established to develop a portable,
readily erected, prefabricated structure as a shel-
ter against biological and chemical attack. Accord-
ingly a standard ammunition hut was selected for
trial as a suitable basic structure to which some
modification would be made. It was equipped with
utilities, air conditioning, and collective protectors
to provide fresh clean air under pressure to make
it suitable for occupancy. The data, results and
recommendations contained in* this report deal with
the mechanical test, the evaluation of the structure
and equipment , and the results obtained by
pressurization.
Naval Civil Engineering Lab. , Port Hueneme, Calif.
TEST OF A 120- FOOT SECTION OF PRESTRESSED
TIMBER LKHTWEIGHT ROADWAY AT POINT MUGU
MUD FLATS, by R. A. Brechenridge and T. L.
Johnston. 10 Dec 51, 17p. Technical note N-081.
Order from LC mi$2. 40, ph$3. 30 PB 154 645
^
717
A 120-foot section of prestressed timber lightweight
roadway was subjec5ed to field tests to determine its
suitability as a mea^s at traversing semi-fluid marsh
areas of minimum bMrlng capacity. The basic design
principles at this ty^ at roadway are sound, and
modifications of this design can be developed to permit
higher load capacities along the lines proposed in the
recommendations contained in this report.
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
TIME STUDIES ON THE ERECTION OF THE
U. S. NAVY STANDARD ARCH RIB PREFABRICATED
yrEEL, 20-FT BY i48-FT BUILDING, byC. B.
Schaeffer. 5 Mar 53, 18p. I ref . Technical note
N-139. I
Order from LC mi$i.40, ph$3.30 PB 154 652
The investigation waB divided into two parts; the first
consisted of establis|hing the number of men required
for the njost ecooontical erection team, and their re-
quired training; the lecond consisted of establishing
normal times for tht erection of the building using
repetitious erectionf for each component and overall
erection manhours . i
Naval Civil Englneisrlng Lab. , Port Hueneme. Calif.
USE OF THE SOIL TRUSS MARK 2 IN DETERMIN-
ING THE SHEARING STRENGTH CHARACTER-
ISTICS OF A SNOW COVER, by S. J. Weiss.
23 Jan 52, 23p. 6 re<fs. Technical note N-075.
Order from LC mi$t. 70. ph$4. 80 PB 154 644
Tests at the Soil Trtiss Mark 2 at the U. S Naval
Sierra Test Site. th0 cold weather station, have
demonstrated the ability at this instrument to classify
the shearing streng^ at snow by means at technique
similar to that usedi in soil, aassiflcation at the snow
cover in conjunction with planned quantitative vehicle
mobility tests will ^ord a basis for the analysis d
performance in snolir. (Author)
Electrical ano Electronic Engineering
?., dii
Admiral Ccmt). , Chicago, fll.
EVALUATION AND| DEVELOPMENT OF
MIL-C- 14157 CAPACITORS FOR NUCLEAR RADI-
ATION ENVIRONMENT, by E. R. P«aif. Scientific
rept. no. 6 on Contfaa NObsr -77612. Feb 61, 38p.
Order from LC mii3.00, ph$6.30 PB 154 241
i
Capacitors impregnated with inhibited FC-43 and
Inhibited bis(pheno:4Th^y^) ^^^ dielectric fluids
failed during gamma irradiation after 63 and 235
hours respectively., Cross -Unked polystyrene capaci-
tors that were irracjiated at room temperature failed
in 377 hours. The Standard- CPM08 capacitors sur-
vived 1000 hours of irradiation at room temperature.
Capacitors subjected to post irradiation environmen-
tal tests survived. Six erf twelve at the Bendix
Scintilla (E-200) capacitors survived the elevated
temperature gamm4 irradiation test. The E-200 units
are thus the most rtdiation resistant capacitors that
have been tested thi|s far. Capacitors are being man-
ufactured with isocfanate treated Mylar, cyanoethyl-
ated Kraft paper, and the radiation resistant dielectric
fluids. (Author) (See also PB 153 096)
Air Force Inst, of Tedi. , Wri^t -Patterson AFB.
Ohio.
SAMPLED- DATA DEVIATIONS IN A VERTICAL
INDICATOR WITH A STELLAR MONITOR, by
Thomas Michael Pienkowakl . Master's thesis. Rept.
for Oct 59- Aug 60 on B-70 Strategic Bomber. Sep 60,
155p. 26 ref 8. WADD Technical rept 60-674, super-
sedes AFIT GGC-60-11; AD-249 269.
Order from OTS $3.00 PB 171 60»
The use of a digital computer or a star tracker in a
vertical indicator results in a sampled-data system in
contrast to the usual continuous -data system. The use
of sampled dau instead of continuous data causes
deviations in the vertical error. These deviations are
explained, computed, and presented in accurate graph-
ical form for use as a design aid. Additionally, the
linear analysis of a sampled-data vertical indicator
causes deviations from the vertical error existing in a
physical (non-Unear) sampled-data vertical indicator.
This second variety at deviations is also explained,
computed, and presented in accurate graphical form.
(Author)
Airborne Instruments Lab. , Melville, N. Y.
NONLINEAR ANTENNA STUDY, by C. Ball and
M. Deckett. Rept. on Contract AF 30(602)1873.
July 59, 44p. 1 ref. Rept. no, 5341 ^TN- 4;
RADC TN-59-294; AD- 226 476.
Order from LC mi$3.30, ph$7.80 PB 150 901
Several different nonlinear antenna systems are de-
scribed. The characteristic that is common to all of
these systems is their susceptibility to continuous or
near-gaussian interference. In the case of communi-
cation circuits, their principal application is, there-
fore, in those environments where the principal
Interference is due to signal sources other than the
intended source and where all signal sources have
low duty cycles. In these circumstances all at the
antennas discussed have characteristics that either
(1) cannot be obtained by linear arrays, or (2) can be
obtained only by linear arrays with many more
elements. In the first class are the space integration
antenna, which has high a-c gain, and the spatial-
coincidence antenna, which has spatial selectivity.
The single- lobe antennas are theoretically in the
first class but realizable current distribution prob-
lems make linear antennas with such gains unfeasible.
The first-order correlation arrays, which have high
angular directivity, are in the second class.
(Author)
Airborne Instruments Lab., Mineola, N. Y.
APPUCATION OF SEMICONDUCTOR DIODES TO
LOW-NOISE AMPUFIERS, HARMONIC GENERA-
TORS AND FAST- ACTING TR SWITCHES, by
R. Gardner, J. C. Greene and others . Quarterly
progress rept. no. 1 on Contract AF 30(602)1854.
Sep 58, 83p. 28 ref s . Rept. 4589-M-l; RADC-TN-58-
353; AD- 206 047.
Order from LC ml$4.80, ph$13.80 PB 155 258
This report released for sale to the public 31 Mar 61 .
718
Study and investigation are reported of the use of
semiconductors as low-noise amplifiers, hannonic
generators , and fast-acting TR switches . The use of
the nonlinear reactance of a reverse-biased P-N junc-
tion diode as a low-noise sum-frequency amplifier is
analyzed in detail. Experimental results obtained on
turn-frequency amplifiers constructed for use at
1 Mc and at 400 Mc are described . The problem of
using semiconductor devices as fast-acting TR
switches is outlined, and an analysis of pertinent TR
system parameters in terms of the series resistance
of the semiconductor diode is presented. The power-
handling capability of presently available semiconduc
tor devices most suited to this application is dis-
cussed briefly. The use of the nonlinear reactance
of a reverse-biased P-N Jmiction diode as a harmonic
generator is examined theoretically, and preliminary
experimental results on a low-frequency prototype
hannonic generator are given.
American Electronic Labs . , Inc . , Philadelphia , Pa .
ANTENNA GROUP OA-1315( )/GL; COMPONENTS
OP ANTENNA CONTROL EQUIPMENT, by R. New.
Final progress rept. for 1 May 57- June 60 on
Contract DA 36 - 039- sc- 73263. [1960] 11 8p. 14 refs .
Technical rept. 57033- F.
OiderfromLC nil$6.00, ph$18.30 PB 153 594
The efforts expended in the' development of efficient
coupling networks to be inserted between existing
antennas and communication receivers are described.
The coupling networks consist of three sections: an
antenna matching network, a bandpass filter, an
active impedance transformer, and a cathode follower.
These networks , together with the necessary switching
circuits , are contained within coupler units which are
located near their associated antennas . Typical per-
formance characteristics of the coupling networks are
presented, indicating the net effect of their inclusion
into the receiving system. An investigation was made
of the purposeful use of ferromagnetic material in
application to electrically short antennas . Thepreti-
cal analyses are presented which mathematically
measure the worth of the nwgnetic and dielectric en-
closure concept. Experimental verification of the
theory has been accomplished and is described by a
series of experiments . Equipnvent was developed
utilizing ferromagnetic material in tuning circuits
located between the antenna and the receiver as
opposed to its use as an enclosure for a shon elec-
tric antenna . (Author)
Amphenol Electronics Corp. , Chicago, 111.
MINIATURE AUDIO CONNECTORS, by C E. Witt.
Pinal rept. on Contract DA 36-039-sc-71184.
31 Mar 58. 98p. 3 refs; AD- 205 151.
Order from LC mi$5. 40, ph$15. 30 PB 150 849
The development and experimental investigation of the
Miniature Audio connectors is directed toward materials
and designs of plugs and receptacles of a type to en-
gage and disengage rapidly, to reaist water and mois -
ture In the mated and unmated conditions, to be suf-
ficiently rugged to withstand military portable and
vehicular radio communication usage. This report In-
cludes data and information covering the period of the
whole project, and summarizes discussions of the
operational and technical problems.
Armour Research Foundation, Chicago, 111.
HIGH POWER TRANSDUCERS, by a & Karplus and
R. R. Whymark. Quarterly rept. no. 3 on Contract
[Nonr] 2900(00). 14 Mar 60, 4p. ARF 1149-3.
Order frtim LC mi$l. 80, ph$l. 80 PB 153 777
See also PB 147 498. PB 152 140
Automatic Mfg. Div. , General Instrument Corp. ,
Newark, N. J.
DESIGN METHODS FOR HICXl FREQUENCY
TRANSFORMERS, by Allan M. Hadley and John P.
Tucker. Final rept. for 1 July 53-30 Nov 55 on Con-
traa DA 36-039-8C-52679. [1955] 366p. 56 refs.
AD-200 706.
Order from LC mijll. 10, ph$4l. 10 PB 155 159
This report released for sale to the public 29 Mar 61.
Bartol Research Foundation, Franklin Inst. ,
Swarthmore. Pa.
RESEARCH INVE^IGATION OF CATHCOE EMIS-
SIVE MATERIALS, by W. E. Danforth. Scientific rept.
no. 10 on Contraa AF 19(604)3904. 15 Oct 60, 26p.
2 refs. AFCRL-TN-60-1142; AD-248 947.
Order from LC mi$2.70, phM 80 PB 153 907
Studies have been continued regarding comparison of
thermionic effects of a thorium monolayer on poly-
crystal and single crystal tungsten. An apparatus for
growing single grain tungsten ribbons has been com-
pleted. A study erf the thermionic properties of
ZrC gg. UC 20 ^° been made. Life tests on thorium
Impregnated tungsten matrix cathodes show that op-
erating lifetimes of 15000 hours or greater can be
expected. (See also PB 152 040)
California U. , Los Angeles .
BILATERAL SWITCHING USING NONSYMMETRIC
ELEMENTS, by Masanao Aoki and Gerald Estrin.
Rept. on Contract Nonr- 233(52). May 60, 55p. 3 refs
Dept. of Engineering rept. no. 60-37; AD- 240 400.
Order from LC mi$3.60, ph$9.30 PB 149 816
Magnetic core memory elements characteristically
require bipolar affiled fields . The vanishing inner
diameter of toroids and the loss of the third dimen-
sion entirely in deposited thin films demands mini-
mization of the number of wires . A configuraticm
which has been investigated and applied in a word
organized memory is illustrated. It consists of a
pair of mutually inverted and parallel connected
transistors. The transistors are not in general sym-
metrical. Some of the system considerations which
determine the important design parameters is dis-
cussed. Methods for location of regions of satisfac-
tory operation in the many-variable space of the in-
verted transistor pair are described. Although a
particular design problem is discussed, attention is
focused on the question, "What classical and new
procedures can we use to reduce the number of di-
mensions in such design problems?" The power of
computers as a design tool is crucially dependent
upon such processes . (Author)
719
Callfomia U. , Lot\ Angeles.
STOCHASTIC TIME OPTIMAL CONTROL SYSTEMS;
by Masanao Aoki. Rppt. on Coocract hkaor- 233(52).
May 60. 19p. 11 re*$. Dept. d Engineering rept. no.
60-35; AD- 239 653.
Order from LC ml$^.«. ph$3.30 PB 149 137
Control systems whjjch are designed in such a way
chat the control syst^ outputs catch up with the con-
trol system Inputs ia the minimum amount at time are
known as time optimal control systems. In other
words, a time optimal control system is such that,
given Che final desired state at the system, it moves
from the initial stat4 to the final state in the mininium
time. Sbice rather ^sential compbcatians enter into
the problem when the desired state erf a control system
is a function d time, only che problem wich Che origin
as Che desired scateiwill be considered in this paper.
CBS Electronics Di v.
tem, Inc. , DanverjB,
, Columbia Broadcasting Sys-'
Mass.
INVESTIGATION 0!^ ULTRA -HIGH RESOLUTION
FLYING SPOT SCANNER AND READOUT FOR
PHOTOGRAPHIC RBEXJCTION, by PhiUp N. Hambleton,
Clifford C. Cain, and J. Brendan Forrest. Final rept.
on Contract AF 30(602)1908. Sep 59. 76p. 5 refs.
RADC TR-59-170; AD- 228 399.
Order from LC miM. 50, ph$l2. 30 PB 150 912
Equipment requiredlfor che invescigacion ot an ultra-
high resolution flying spot scanner is described. The
design, constructioil, and operation of this equipment
is discussed for dupiucating printed charaaeristics,
photographs, and documents. Document reductions of
100:1 and 200:1 were reproduced electronically oo
photographic paper {xwitives with the breadboard
equipment. A slow $can tin»e at one second per frame
and a flying spot scanner with P-16 phosphor were
uaed. The readout 91 monitor tube used a long per-
siatance P-12 phoepliar Although the P-16 ultra -high
resolution flying sp0t scanner is capable at 1000 TV
lines per inch and should be the ultimate limiting
aperture of the system, in practical applications the
resolution erf the av4ilable commercial lenses were
limiting the resolutijon performance of the equiprfient
and system. The cii-cultry ot the system described.
An analysis of the 14ns charaaeristics and perform-
ance is given. The resolution of the readout or moni-
tor tube using P-12 ptioaphar had resolutions at
1500 TV Unes pjer ii)ch and exceeded the resolution erf
the fl)ang spot scaniier tube and insured no loss in
resolution between the cwo systems other than me-
chanical linutationa,o< the lenses. (Author)
Compagnie G^n^ralle de Tgl%raphle Sans Pil
(France)
FEASIBIUTY AND iRE^ARCH ON A NEW TYPE OF
ENDFIRE ANTENNA "SAUaSSON ANTENNA", by
Erich Spitz. Final tjechnical rept. for I Jan-30 Sep 60
on Contract DA 91-$91-EUC-1376. [1960] 62p. 5 refa.
AD- 248 235
Order from LC mi$fe.90, ph$10.80 PB 153 719
The development is described of a new type at eodfire
antenna called "Sau<;isson Antenna". It consists
essentially of a rwo«wire line surrounded by a wire
helix. The principla of operation is explained by the
transformation at tqe excited anti symmetrical mode
Into the symmetrical radiation mode. The influence cf
different geometrical parameters is investigated and a
scale model of a 350-600 mc range antenna working in
the S band was built . A gain of about 20 db was
achieved in the whole band with secondary lobes lower
than 16 db. For a 16 db gain -antenna the secondary
lobes are lower than 20 db. (Author)
Cook Research Labs. , Morton Grove, 111.
HYDRAUUC SERVO CONTROL VALVES. PART VI.
RESEARCH ON ELECTROHYDRAUUC SERVO
VALVES IKALING WITH OIL CONTAMINATION.
UFE AND RELIABILITY. NUCLEAR RADIATION
AND VALVE TESTING, by W. L. Kinney, E. R.
Schumann and P. A. Weiss. Rept. on Contract
AF 33(616)5136, Nov 58. 146p. WA DC Technical
rept. 55-29; Part VI; AD-211 733.
Order from LC mi$7.20, ph$22.80 PB 155 147
This repxjrt released for sale to the public 30 Mar 61 .
This report is divided into four sections. Design and
operation at a test fixture intended for analysis ot
servo valve operation under various levels of oil con-
tamination are described. Information on servo valve
life and reliability, as obtained from valve manufac-
turers and users, is presented, and the various design
features influencing reliability are discussed. Design
and construction of a valve -actuator assembly for use
in a nuclear radiation environment are described, and
test results on this unit under gamma radiation are
presented. A series erf evaluation tests was run on one
unit each of three new types of valves, and the test re-
sults are presented and discussed. (See also
PB 154 966)
Curtiss-WrightCorp, Quehanna, Pa.
ANALYTICAL AND EXPERIMENTAL INVESHGA-
TION OF COMPACT CHARGE IONIZATION, by
E. N Petrick. O. K. Husmann. and H W. Szyma-
nowski. Final rept. on Contraa Nonr- 2886(00) and
ARPA order no. 5-58. 1 June 60, 182p. 77 refs.
CWR 700-10; AD-240 709.
Order from LC mi$8. 90. ph$28. 80 PB 149 847
Diffusion flow rate tests with Inert gases and ioniza-
tion tests with cesium were conducted using emitters
of sintered porous tungsten, electro-formed molybde-
num screen, and micro- perforated platinum plate.
Excellent correlation was demonstrated between meas-
ured ion current and the predicted value based on dif-
fusion dau. The effect of surface diffusion flow was
shown to be negligible. Cesium corrosion tests dem-
onstrated the high-temperature long-term suitability
at various materials, Including tungsten, molybdenum,
and aluminum oxide. In regard to fabricatidn 0* the
ion source, a pronrUsing technique of brazing the sin-
tered porous tungsten emitters into a molybdenum
holder was developed. The generation of cesium
within the fuel supply system was investigated in order
to reduce fuel storage and handling problems. A
cesium recovery of 89% of theoretical was measured.
Dau are Included on the various phases of the Investi-
gation and specific recommendations are presented.
(Author)
720
David Sarnoft Research Center, Princeton, N. J.
GENERATION OF "COOL" ELECTRONS FOR LOW-
NOISE MICROWAVE TUBES, by F. M. Johnson and
W. Knauer. Semi-annual rept. no. 2, 1 Jan-
31 July 59, on Contract DA 36-039-sc-78l51.
31 Aug 59, 28p. 5 refs. AD- 228 558,
Order from LC mi$2.70, phHSO PB 154 523
Development was accomplished of a practical lithium
ion emitter to replace the earlier unsatisfactory
cesium source. The construction of a plasma test
tube was completed; this test tube will aid in investi-
gating the rf-characteristic of the plasmas used for
cooling. A theoretical analysis predicts a noise
reduction in such plasmas which may make cooling
unnecessary. (Author)
David Samoff Research Center, Princeton. N.J.
HGH-TEMPERATURE, IMPROVED-EFFIQENCY,
PHOTOVOLTAIC SOLAR ENERGY CONVERTER, by
J. J. Wysocki. J.J. Loferski, and P. Rappaport.
Triannual progress rept. no. 4, 15 July-15Nov 59,
on Contract DA 36-039-sc-78184. 30 Nov 59, 32p.
AD 230 412.
Order from LC mi$3.00. ph$6.30 PB 154 525
Current work describes attempts to achieve higher-
efficiency GaAs solar cells by fabrication improve-
ments. Best results; 5% overall conversion efficiency
on cells 1/4 cm2 in area . Surface erosion of GaAs is
one cause of low efficiency. Diffusion of phosphorus
and nickel did not lead to appreciable improvement.
An analysis of the spectral response of a photovoltaic
cell is presented with some experimental examples
showing how it can be used to study the lifetime in a
finished cell. Improvements in spectral response are
described using post diffusion processing. (Author)
(See also PB 153 602)
David Sarnoff Research Center, Princeton. N.J,
HIGH-TEMPERATURE , IMPROVED- EFFIQENCY,
PHOTOVOLTAIC SOLAR ENERGY CONVERTER, bjt,.
J. J. Wysocki, J. J. Loferski and others . Triannual
progress rept. no. 5, 15 Nov 59-15 Mar 60, on
Contract DA 36-039-sc-78184. AD-236 973.
Older from LC mi$3. 30. ph57, 80 PB 154 526
A new type of zinc diffusion process for GaAs using an
open furnace has yielded cells up to 5.2% in efficiency
This process is promising since present surface con-
centrations are a tenth of what they should be. Prog-
ress has been made on improved ohmic contacts .
Spectral response curves show that lifetime is the
limiting factor in the GaAs solar cells . The use of
spectral response curves in determining lifetime is
also discussed. Spectral response on n andy> sur-
face layer silicon cells a^e presented. An analysis of
the PEM effect as a solar energy convener is pre-
sented showing it to be an inefficient conversion proc-
ess with efficiencies of the order of 10' 3%. This has
been verified experimeritally. (Author) (See also
PB 154 525)
David Taylor Model Bisin, Washington, D. C.
DESIGN CCTAILS AN^ OPERATING PROCEDURE
FOR THE TMB NETWORK ANALYZER, by John H.
Kenney and Ralph C Leibowitz. Apr 59, 29p. 1 ref.
Rept. 1272.
Order from LC mi$2.70, ph$4-80 PB 155 577
This report released for sale to the public 19 Apr 61.
This report describes the physical characteristics,
components, and instrumentation of the TMB Network
Analyzer, and gives the layout arrangement and some
construction details. The procedure for setup and
operation erf the network analyzer is explained suffi-
ciently to permit the reader to utilize the facility. A
brief desen-iption of the methtxls and techniques em-
ployed in calibrating the components used with the
analyzer is included. (Author)
Developmental Engineering Cenrp. . Washington. D. C.
REUABLE HIGH-FREQUENCY CC»^MUNICATIONS.
by R. E. Ankers, B. G. Hagaman, and G. F. Leydorf.
Final rept. for 1 Dec 54-31 Aug 58 on Contraa
DA 36-039-8C-64486. [1958] I22p. 45 refs;
AD-207 217.
Order from LC mi$6. 30, ph$l9. 80 PB 155 025
This report released for sale to the public 27 Mar 61.
The application of tapered aperture amplitude distri-
bution to horn antennas greatly increases their useful-
ness in many applications. The TAHA combines the
charaaeristics of directivity, effealve side- lobe sup-
pression and exteneled banchwidth. The TAHA has un-
usually stable vertical -plane radiation c:haraaeristics.
The variation of the vertical angle of maximum re-
sponse with frequency is very moderate. A prelimi-
nary study indicates polarization chversity may be in-
corporated in the TAHA antenna. Radiation panern
charaaeristics. bandwidth, and seconelary-lobe sup-
pression are maintained in both polarizatieins. Polari-
zation diversity in a single antenna will result in in-
creased reliability, reduaion in over -all cost, and
conservation of space. The 4 -wire, 300-ohm. 4 -con-
ductor Une described in AD-207 218 represents a rec-
ommendation for a balanced high-power, low-loss,
open-wire line. The over-all anenuation of the line is
cuamputed to be less than 0. 2 db/1000 ft and therefore
the losses from this line will be small when used with
a 500 kw system. The propt)sed 300-ohm line, to-
gether with the CCCO-type balun, offers a complete
system for feeding a balanced 300-ohm load, such as a
TAHA antenna, from a 50-e)hm (unbalanced) exit put erf a
transmitter with a minimum erf losses. The design
criteria for a high-power transmission line should
consider the relationship of the cost of line construc-
tion to the cewt of generating ackied RF pewer to cotn-
pensate for line losses so that the highest operational
economy may be achieved over the life span of the
installation. (Author)
721
Diamond Ordnance Fuze Labe. , Washington, D. C.
EFFECT OF DC IN A MAGNETIC RECORDING
HEAD, by J. C. Hoidlcy. 31 May 60. 16p. 1 ref.
Technical rept. TR-848; AD-240 514.
Order from LC mi$t 40. ph$3. 30 PB 155 618
The effect erf direct Current in a magnetic recording
bead is nteaaured. The point of occurrence (with re-
spect to the signal) <Jf maximum noise can be con-
trolled; unidirection*] signal -handling capability can
be increased. The direct current does not increase
dynamic range, does not increase average si^ul-to-
noise ratio, and the Jow-frequency response is
redtxred. (Author)
Diamond Ordnance Fuze Labe . , Washington, D. C
A NEW ELECTROCtlEMlCAL SYSTEM FOR HIGH-
VOLTAGE LOW-CuilRENT DRAIN APPUCATIONS.
by William J. Pauli. 10 Mar 61, 2lp. TR-883.
Order from OTS $0. ^5 PB 171 582
A new battery system has been designed for miniature
high-voltage, low-cii-rent drain applications. The
battery, a stack at cius that are 1/2 in. in diameter
and 0.0I3-in. thick, brovldes 60 v/in. of length. The
capacity is 5 coulomps and the drain rate 0. 1 to 10 pa.
The unit operates ov^r the temperature range -650F
to + 165°F; several ^ored at ■♦•125°F for more than a
month showed very ailight loss in output voltage when
subjected to -65°F operation. (Author)
Dunlap and Associ^es, Inc. , Stamford, Conn.
CODING OF EQUIPMENT FOR EA^ OF MAINTE-
NANCE, by Charles ;E. Van Albert, Norman B. Hall,
and Jerome H Ely. iRept. on Contract AF 30(602)1895.
Oct 59. 14p. RADCJTR-59-l60;*AD-227 821.
Order from LC mi%t 40. ph$3. 30 PB 150 91 1
Background information for this study was obtained
through field tripe tci various Airways and Air Commu -
nication Service sitep. Electronic equipment was ex-
amined, technicians were observed while performing
preventive maintenance checks and trouble-shooting,
maintenance manual^ were reviewed, and technicians
and supervisory personnel were interviewed. As a fol-
low-up. a questionnajire type survey was conducted
among fifteen AACS pites. From these observations, a
set of four recommendations was developed. Design
details for each recommendation are given. These
recommendations wdre tested by incorporating them on
an oscilloscope. Thfa coded scope was compared with
an identical uncodedione in terms of the time required
by technicians to locate malfunctions. The average
trouble -shooting tim^ for the coded equipment was ap-
proximately one-hatfl that of the uncoded equipment.
The recommendaticniB appear to be most useful in
helping relatively unskilled technicians identify diffi-
cult malfunctions. (Author)
Dunlap and A ssociajtes. Inc., Stamford, Conn.
RECOMMENDED EOUIPMENT CODING TO FAQU-
TATE MAINTENAn4:E, by NcM-man B. Hall. Charles
E. Van Albert, and^romeH. Ely. Rept. on Contract
AF 30(602)1895. Sep
AD- 227 820.
Order from LC mi$3|. 00.
59. 36p. RADC-TR-50-159;
ph$6.30 PB 150 910
A study was initiated to (a) determine what types of In-
formation to place on prime ground-based electronic
equipment, and (b) develop techniques for displaying
this information, in order to assist Level 3 and Level
5 technicians In performing both preventive and cor-
rective maintenance. A set of four recommendations
was developed concerning information to be displayed
on prime electronic equipment. Specifically, it was
recommended that the following information be dis-
played: (1) designation of functional groups of equip-
ment; (2) Identification of signal paths; (3) identifica-
tion of test points and indication, when appropriate, of
sequence in which they should be used: and (4) pre-
sentation of historical data displaying periodic read-
ings taken at each test point when equipment was
operating satisfactorily. These reconunendations were
tested.by incorporating them on an oscilloscope. This
coded scope was compared with an uncoded one In
terms at the time required to locate and identify mal-
funaions. The results showed that the average
trouble- shooting time for the coded equipment was
approximately one-half that of the uncoded one.
(Author)
Electron Physics Lab. , U. at Michigan, Ann Arbor.
LARGE-SIGNAL ANALYSIS OF CROSSED-FIELD
DEVICES, by 0. P. Gandhi and J. E. Rowe. Final
rept. for 1 Sep 58-30 Sep 60 on Contract DA 36-039-
sc-78223. Sep 60. 62p. 16 ref s. 2820 5-F;
AD-247 721.
Order fromLCmi$3.90. ph$10.80 PB 154 501
Large-Signal Crossed-Field Amphfiers. A set of non-
linear partial-differential integpral equations was de-
rived to describe the operation of the large -signal
crossed -field amplifier, and these are used to study
the effects of such parameters as magnetic field,
space -charge forces, injection velocity parameter,
and electron stream thickness on the efficiency and
gain. The interaaion is studied for Brlllouin streams.
nonslipping laminar streams, and nonlaminar streama
Large-Signal Backward-Wave Oscillators. The large-
signal backward-wave interaction equations are
studied for both thick and thin streams with and with-
out the acceleration terms in the equations of motion.
Premodulated Crossed-Field Streams. The effect of a
premodulation on an electron stream in a crossed-
field environment is investigated by using the small-
signal equations. One at the principal reasons for
studying this configuration Is that a drift region can be
used effectively in the middle of an r-f device struc-
ture to absorb the initial heavy electron collection and
hence reduce the power dissipation requirement of the
structure. Positive-Sole Crossed-Field Interaaion.
When the positive-sole crossed-field device is ana-
lyzed, it is found that beating velocity waves are
excited on the stream. The complementary behavior
of positive -sole crossed-field interaction with normal
(negative -sole) interaaion is established on the basis
of small-signal equations. (Author)
E lear on Physics Lab. , (J of Michigan, Ann Arbor.
RESEAROI ON CROSSED-FIELD ELECTRON DE-
VICES, by O. P. Gandhi, R. W. Larson and others.
Quarterly progress rept. no. 7. 1 June-1 Sep 60. on
Contraa DA 36- 039 -sc -78260. Sep 60, 54p. 7 refs.
2854 8-P; AD- 246 785.
Order from LC mi$3. 60, ph$9. 30 PB 154 502
722
Further calculations are carried out on nonlaminar
M-type streams and the propagation constants fw
■pace-charge waves on a nonlaminar beam are pre-
sented for two different beam thicknesses, corre-
sponding to a thin and a thick stream respealvely.
Experimental information on the energy distribution
cfaaraaerl sties at various points along the sole elec-
trode for a space -charge -limited cathode In theM-type
scream analyzer is presented and analyzed. The ap-
pearance of coherent r-f output from the analyzer is
correlated with the appearance of high-energy elec-
trons at the various sole probes . A number of possl -
ble elearode configurations for M-type Injeaion sys-
tems are presented and analyzed with respea to their
abilities to produce laminar electron trajeaories in
the circuit -sole region. One particular geometry is
analyzed in some detail. The minimum -energy method
is applied to the solution of the input boundary value
problem for thick-stream M-type backward-wave
oscillators. Expjressions are derived for the calcula-
doo of the excited wave amplitudes and the start -
oscillation conditions are derived. The small-signal
and large- signal solutions for multiple -stream M-type
devices are compared and the dlscrepMncies in the
excited wave amplitudes are explained. The effect of
cyclotron waves is also explained. (Author) (See also
PB 147 968)
Electron T^ibe and Microwave Lab. , Caltf. Inst, of
Tech. , Pasadena.
THEORY OF PARAMETRICALLY-PUMPED LONGI-
TUDINAL-FIELD ELECTRC»4 BEAMS, by Dbnald C
Forster. Technical rept. no. 14 on Contraa
Nonr-220(13). June 60, 164p. 39 refs; AD- 238 142.
Order from LC mlf7. 80. ph$25. 80 PB 148 323
The general equations describing elearon beams which
have been excited by both a moderately strong pump
source (or local oscillator) and a weak signal source
•re formulated in terms at coupled modes, including
coupling to slow- wave circuits, and solved numerically
for four problems of interest: (a) space-charge pumped
kingltudlnal parametric amplifiers, (b) circuit -pumped
longitudinal parametric amplifiers, (c) papametrlc
cooling at slow space -chaise waves, and (d) traveling-
wave tubes with pump space- charge waves excited on
the elearon stream. Emphasis is placed on the para-
metric amplifier solutions, and realization at noise
temperatures as low as 55°K are Indicated. Ampli-
fiers with this noise temperature and with gain of about
20 db per plasma wavelength should be realized by in-
creasing the phase velocity of the pump wave through
the use of circuit pumping. Reasons for the poor per-
formance at the space-charge-pumped parametric
■mplifier are established. A discussion at the form at
the general equations leads to new concepts about the
coupling d positive and negative energy carriers
through the action at parametric pumping. Experi-
mental results are presented which tend to verify
^llutlvely some of the theoretical predialoos for
the behavior at the parametric amplifiers. (Author)
Electron Tube Research Lab. , U . of Minnesott .*
Kflnnea polls .
STUDIES ON BASE NICKELS FOR OXIDE -COATED
CATHODES, by D. E. Anderson. Scientific rept.
■0. 9, 15 Apr- 15 July 60. on Contract AF I9(604)389a
11960] 118p. 12 refs. AFCRL TN-60-1154.
OrderfromLC mi|6.00, ph»18.30 PB 154 450
Cathodes . based on 0.2% and 0.08% Al-Ni aUoys ,
have been operated at 1093OK in excess of 13.000
hours . Emission levels of over 11 amps/cm^ are 'ob-
served. Experiments are described on the effect of an
extensive atriKwphere of Ba vapor on the emission
pr(^)erties of oxide cathodes . Results on the activa-
tion of oxide cathodes in the presence of heated Ti
anodes indicate the enhancement of emission is caused
by hydrogen released from the heated Ti . Experi-
ments designed to investigate the optical properties
of BaO thin film coatings are discussed. (See also
PB 152 735)
Elearonic Defense Lab. . Sylvania Electric Produas,
Inc. , Mountain View, CaJif.
VACUUM TUBE PULSE MODULATOR ANALYSIS, by
Henry Nenesheim. Rept. on Contraa DA 36-039 -sc-
78281. 25 Jan 60. rev. 29 Nov 60. 109p. 8 refs. Tech-
nical memo. no. EDL-M226; AD-236 758.
Order from LC mi$5.70. ph$16.80 PB 154 213
This report released for sale to the public 27 Mar 61.
The development of high power, high duty faaor pulse
transmitters is of great importance to transmitter
design engineers. As higher-power transmitting tubes
become available, it becomes increasingly difficult to
build modulator circuits capable of operating at a high
duty faaor into capacitive loads while still maintaining
optimum pulse shapes. This memorandum presents a
compendium of current "hard tube" modulator circuits,
together with a detailed analysis of their circuit char-
aaeristics -- rise and fall times, droop, charge
storage, and power -handling capacity. The following
circuits are considered: transformer -coupled,
common cathode RC- coupled, common cathode direa-
coupled, grounded cathode RC -coupled, and gated
modulators. From the detailed mathematical analysis
presented, virtually all circuit design parameters can
be computed for any desired modulator. (Author)
Elearonics Research Lab. , U. of California,
Berkeley.
ANALYSIS OF NONLINEAR SAMPLED-DATA SYS-
TEMS VflTH PULSE-WIE« MODULATORS, by T. T.
Kadota. Rept. on [Contraa Nonr- 222(53)] 30 June 60,
69p. 28 refs. Series no. 60, issue no. 290;
AD-241 278.
Order from LC mi$3. 90. phJlO. 80 PB 150 109
The inherent noplinearities of pulse-width modulated
systems arising from the modulation scheme present
a serious analytical difficulty, which has led to vari-
ous types of approximations of such systems. Throt^
the method of 3 -function expansion, an exact expres-
sion for the output of the pulse- width modulated sys-
tem is obtained, and is interpreted into a block dia-
gram which clearly indicates the type of nonlinearltiet
involved in such a system. On the bans of the above
method, two commonly used approximations are ex-
amined and their validity is established under more
severe conditions than have hitherto been assumed.
(Author)
723
Electronics Research Lab. , U. of California,
Berkeley. I
(QUARTERLY PROGRESS REFT. Rept. for 1 J«n-
31 Mar 60 on Contracts Nonr-222(53, 54, 57, 74).
30 Apr 60, 24p. IE| Series no. 60 [issue] no. 28.
Order from LC ini$t. 70, ph$4. 80 PB 148 098
Summaries of work on back-scanering from cones-,
scattering from multiple targets , scattered fields
from anisotropic m^ia , radiation from a modulated
ferrite traveling-wakre antenna, microwave para-
metric amplifiers , ferrite field-displacement device for
slot-coupling control, network theory, electronic cir-
cuits research, antenna arrays from a data-process-
ing viewpoint, infortnation theory, solar emission and
absorption, researci in high- temperature semicon-
ductor devices , and magnetic amplifiers .
i%\
Electronics Research Lab. , U. of California,
Berkeley.
SYNTHESIS OF NEtTWORKS
R. W. Newcomb.
dation Contract G
Series no. 60, lssu<
Order from LC mi
R«pt
-1!
PASSIVE ATp by
on National Science Foun-
142. 14 Sep 60. 31p. 7 refs.
no. 317; AD-247 892.
00. ph$6. 30 PB 153 705
If a network N has energy output q greater than or
equal to zero at p fop- time equal to zero, then it is
known that N is passive at P (o). If N is a two-port or
a member of a genei-al class at n -ports, it Is shown
that there exists a finite passive network N(P) such
that N and N(P) hava the same admittance matrix at
p(o). A simple testlfor q. greater than or equal to 0
is given, for most H, and it is shown that the complex
transformer isn't passive when Re p<o) is greater
than a (Author)
U. at CaltfornU,
Electronics Research Lab
Berkeley.
SYNTHESIS OF PA
WORKS ACTIVE A
on National Science Foundation Contract G-12142.
VE NETWORKS FOR NET-
Po, by R. W. Newcomb. Rept.
11
14 Sep 60, 54p
AD- 248 151.
Order from LC mijfe. 60. ph$9. 30
refs. Series no. 60, issue no. 316;
PB 153 704
If a one or two- port network. N, has the product ci q
lub ♦ and p sub o ii less or equal to 0, synthesis
methods are given mr passive embedding networks
which yield a natural frequency at p sub o. The
synthesis is based qn the Y matrix. However, the
synthesis is general, since N's with Z are treateddu-
ally, and a procedure is given for converting those N
without Y or Z to oi^es which have a Y or Z while
leaving q sub > unchanged. A synthesis for some
n-ports is also givefi which uses the one or two-port
synthesis after shoeing appropriate ports. (Author)
Electronics Resea rch Lab. , U. of California,
Berkeley. i
TRANSISTOR MAGIMETIC INVERTER FOR SPEED
CONTROL OF AC MOTORS, by N. llynski .
15 June 60. 55p. IER series no 60, issue no. 286;
AD-243 021 .
Order from LC mi$b. 60. p*i$9. 30 PB 150 792
The design and operation of a power transistorized
inverter supplying a single-phase reluctance motor ii
reported. Transistorized power inverters were suc-
cessfully used in many cases because of their high
efficiency, small sizes , lack of moving parts , and re-
liability. Different inverter circuits were studied;
the inverter was designed and built. The main char-
acteristics of the inverter with different kinds of load
(resistive, inductive) were obtained . The influence of
the inverter parameters on its characteristics was
investigated. Characteristics of the reluctance motor
were obtained when it was supplied from a sine volt-
age source and from the inverter. (Author)
Erie Resistor Corp. , State College. Pa.
ENERGY STORAGE CAPACITORS. HIGH DIELEC-
TRIC CONSTANT. Final development rept. for
14 Jan- 23 Dec 60 on Contract NObsr- 77554. [19601
78p; AD- 248 545.
Order from LC ml$4. 50. ph$l2. 30 PB 153 723
Twelve sample capacitors were made using the stacked
plate method and tested according to contract specifi-
cations. Degradation of the ceramic under high tem-
perature - high voltage conditions caused the units to
fail life test. The degradation was traced to an elec-
trochemical reduction of the ceramic and subsequently
high leakage. TTie ability of the ceramic to withstand
high constant voltage conditions at elevated tempera-
tures during earlier testing indicates that the constant
pulsing of the voltage was the cause of failure, but
also indicates that the ceramic can be Improred to
withstand the additional stress engendered by the
pulsing. Xhose units which were not subjected to life
test met the remaining electrical tests reasonably well
in moet instances. In those (;ases where failures oc-
curred or questionable results were obtained, the dif-
ficulties appeared attributable to the types of Jacketing
materials employed. The use of rigid jacketing com-
pounds appears unsulted to this type of unit unless
provisions are made to closely match the coefficient of
thermal expansion of the jacket material to that of the
ceramic over the operating temperature range. The
use of plasticized materials of flexible materials
would be probably more desirable. (Author) (See also
PB 144 254)
Ford Instrument Co. , Long Island City, NY.
BASIC DESIGN CONSIDERATIONS FOR REDUCED-
TIME FACSIMILE SYSTEMS, by T. Erb, R. Banow
and others. Technical note no. 2 on Contract
AF 30(602)1864. 24 Feb 59, 91p. 19 refs. RADC-
TN-59-83; AD-211 435.
Order from LCml$5.40. ph$15.30 PB 150 900
Contents:
Possible time reduction '
The scanning and display problem
The mechanical drum scanner and printer
The flat -bed mechanical scanner and printer
The electronic scanner
Photographic input and output with an electronic
scanner
Electroluminescent scanning and display devices
Scanners using other physical principles
Digital position control of electron beams in flying sprt
scanners and printers
Flying spot scanners
724
Horizontal scanning
Vertical deflection coocrcri
Modifications of this method
Flying spot recorders
Positioning d flying spots by coding plates
Problenu of spot size, shape and brightness
Other applications for digiully controlled cathode
ray tubes
Coding
Outline of a facsimile transceiver
The transmissioa link
General Bronze Corp. , Garden Qty, N. Y.
RESEARCH ON LOW SILHOUETTE ENDFIRE AR-
RAYSk by Bruce F. Bogner and Robert A. Rhodes.
Final rept. no. 1 on Contract AF 19(604)5710.
1 June 60. 73p. 8 refs. AFCRC-TR-60-165;
AD- 248 590.
Order from LC mlK 50, ph$l2. 30 PB 153 864
b the design at arrays of end-fire elements, the
characteristics of the individual element both in free
space and in the array are of importance in determin-
ing the array configuration and performance. The
free space performance characteristics of disc-on-
rod elements and the nature of the mutual coupling and
gain and pattern degradation of elements when placed
in arrays was studied. Usiqg this dau, general de-
sign equations for various fan and pencil beam arrays
of dlsc-on-rod endfire elements were developed.
Onptiasts was placed on the design of a sii^Ie disc-
oa-rod element that wcxild allow an array of six such
elements lying In a common plane to nneet a specific
gain and side lobe requirement. An alternate so-
lution to this requirement was also reached by re-
moving the restriction that the elements all lie in one
plane, and this latter arrangement resulted in the
smallest array size to n^eet the requirement. The
effects of launcher design and launcher coupling upon
array performance, and the bandwidth characteristics
of elements and arrays, were also investigated, kis
coocluded that the specific gain and side lobe require-
ment can be met by a six element single plane array,
and further that arrays of end fire elemenu show
considerable promise in antenna design. (Author)
General Electric Co. , Syracuse, N. Y.
WIRE SONIC DELAY LINES, by S. W. Tehon. Rept.
on Contraa AF 30(602)1710. 14 Apr 59. I35p. 8 refs.
lADC-TR -59-62; AD-214 596.
(Jrderfrom LCmi$6.90, ph$2l.30 PB 155 073
This report releaaed for sale to the public 27 Mar 61 .
An investigation of wire sonic dalay lines is described.
With the broad goals of reducing insertion loss, reduc-
ing apurioua response, increasing bandwidth and in-
creasing frequency of operation. Insertion losa and
frequency response are discussed for steady state op-
«t«tion. from the viewpoint of equivalent circuit analy-
•ia. Tranaient and steady state response are discussed
far a nianber of transducer types and configurationa,
Ukwing a novel method of analysis. Practical eon-
KmuioB methods were applied in the following fin-
ished Unes: (1) 500 kc. 2. 780 fitec delay; (2) 1 mc,
2j780 paec delay; and (3) 1 nK. 10, 000 usee delay.
n«oelectric ceramic transducers were developed for
low insertion loss, wideband operation. Operation was
extended to high frequendea, indicating that high fre-
quency limitations are imposed by the delay wire at-
tenuation and dispersion. Low anenuation delay wire
was developed, with a mechanical Q sufficiently high
to extend the previous limitations on the delay band-
width product. Practical limitations on line perform-
ance are discusaed. as determined by transducer
coupling coefficient, delay wire attenuation, disper-
sion, aad assembly techniques. (Author)
General Electronic Labs. , Ik. . Cambridge, Maas.
VHF-UHF RECEIVER FRCWT ENDS. Final repi. for
1 July 54-31 Mar 5S on Contraa DA 36-039- sc- 64457.
[1958] ll6p. Srefs. E- 131 -F; AD- 210 287.
Oder from LC mi$6. 00, ph$18. 30 PB 150 847
The results of this work are a series of ac -powered
receiver front ends wtucfa are continuously tunable over
the frequency raage 20 >^ 1000 mc, and a series of
banery-powered front ends covering 70 to 500 mc.
This report includes a brief history of the study phase
and detailed descriptions of the mechanical and elec-
trical properties of each of the developmental front
ends. Different techniques are required by front ends
in different portions of the wide tuning range. The
range 20 - 70 mc is covered by a conventional L-C
tuner employing a ganged variable capacitor. The 70-
to 200-nic tuner employs helical lines in a double-
cavity resonator. The 200- to SOO-noc range is tuned
bjr a capadtively loaded coaxial resonates-; the 500- to
1000-mc tuner ia similar, except that it employs a
triple-cavity reaooator rather than a double-cavity
resonator. (Author)
Georgia Inst, of Tech. EngineeriiH Experiment
Station, AtlJaau.
HIGH TEMPERATURE RESSTORS FOR PRINTED
aRCUITS, by Richard B. Belser and Douglas W .
Robertson. Final rept. for 1 Apr 59-1 July 60 on
Contract AF 19(604)5519, continuation of Contracts
AF 33(616)3870 and DA 36-039-$c-42453. 30 June 60
104p. 80 refs AFCRL TR-60-372; AD- 249 826
Order from LCmi$5. 70, phH6. 80 PB 154 166
Films of the semi -refractory and refractory metals
have been deposited on fused quartz substrates by
sputtering and examined in Y«£Ufi for temperature
coefficient of resistance (TCR) over the range 25^0
to600OC. Selected specimens were subsequently tem-
perature cycled in air and the temperatures at which
*"*v*"ible changes in resistance occurred were re-
corded. The metals examined fall into three genera]
classes: members of the platinum family, platinum,
osmium and ruthenium; the semi -refractory metals ,
titanium, zirconium, vanadium and niobium, and the
refractory metals, molybdenum, rhenium and tung-
sten. The metals of the platinum family with the ex-
ception of osmium exhibited TCR values in the approx-
imate range 1/4 to 1/2 the TCR of the bulk meul but
were too high to be of value as normal resistor units
On the other hand, similar films were utilized with
success as resistor thermometers . The group
titanium, zirconium vanadium and niobium were
attacked by residual gases during the sputtering
action to form ne tal compounds , nitrides of oxides .
Films of these materials gave negative TCR values .
72S
The refractory metils , molybdenum, rhenium and
tungsten exhibited low TCR values and high stabilities
Studies of the protection provided 42 films of tung-
sten or rhenium by overcoats of silicon monoxide, sil
icon or chromium were conducted. In some instances
protection for five 6r more cycles to 600°C In air
were observed without fllm damage and power dissi-
pation tests to apprbximately 90CPC were performed
succetsfUlly .
Giannini Controls Corp. , Duarte, Calif.
PRESSURE TRANSDUCING AND INSTRUMENTATION
TECHNIQUES. VOLUME I. BOOK I. GENERAL IN-
TRODUCTION AND PART A TRANSDUCING TECH-
NIQUES. Rept. on Contract AF 33(616)6186. 1 Aug 6a
3lOp. Giannini Controls rept. na BR 00000-56;
WADD Technical r^pt. 59-743, Vol. I, book I.
Order from OTS m|$ll. 10. phM7. 10 PB 155 568-1
I
This report releasad for sale to the public 19 Apr 61.
An engineering study and evaluation of pressure trans-
ducing techniques abd related transmitting and indicat-
ing syatem techniqiles is presented in two volumes of
four books. Volume I. consisting of Books 1, 2. and
3. gives a general Introduction and covers the current
state of the art. '
Giannini Controlal Corp. , Duarte. Call/.
PRESSURE TRANSbuONG AND INSTRUMENTATION
TECHNIQUES. VOLUME I, BOOK 2. PART B. TRANS-
MITTING TECHNIQUES. Rept. on Contract
AP 33(616)6186. 1 Aug 60, 370p. Giannini Controls
repc no. BR 00000-56; WADD Technical rept. 59-743,
Vol. I. book 2. I
Oixler from LC mlill. la pfa$56. 10 FB 155 568-2
This report releas^ for sale to the public 19 Apr 61.
SeePB 155 568-1
Q*^"««"< Controlal Corp. . Duarte. Calif.
PRESSURE TRANSDUCING AND INSTRUMENTATION
TECHNIQUES. VOtUME I, BOOK 3, PART C NU-
CLEAR RADIATION EFFECTS. Rept. on Contract
AP 33(616)6186. 1 Aug 60. 1 17p. Giannini Controls
rept. no. BR 00000-56; WADD Technical rept. 59-743
Vol. I. book 3.
Order frotn LC mlt6. 00^ V^^- 30 PB 155 568-3
This rafwrt releaa^ for nle to the public 19 Apr 61.
See PB 155 568-2 |
Giannini Controls Corp. . Duarte, Calif.
PRESSURE TRANSDUQNG AND INSTRUMENTATION
TECHNIQUES VOLUME II, PART A. IMPROVE-
MENTS TO CURRENT PRESSURE TRANSDUCING
AND TRANSMITTUJG TECKNIQUES; PART B.
UNIQUE TECHNIQUES AND PART C. REFERENCES.
Rept or Contract AF 33(616)6186. 1 Aug 60. 172p.
235 refs. Giannini Controls rept. no. ER 000(X)-56;
WADD Technical r^. 59-743. Vol. U.
Order frxjm LC mifS. Itt ph$27. 30 PB 155 569-1
This report released for sale to the public 19 Apr 61.
Volume II include improvements, if miniannization and
new techniques in addition to a reference section. (See
alaoPB 155 568-(l-3)
Gulton Industries, Inc. , Metuchen, N. J.
RESEARCH INTO SOLID STATE TRANSDUCING
TECHNIQUES, by Walter Welkowitz, Rudolph Downs
and others. Rept. on Contract AP 33(616)6359. Feb 6a
238p. 50 refs. WADC-TR-59-742.
Order frtm LC ml$ia 20. phJ36. 30 PB 155 567
This report released for sale to the public 19 Apr 61.
The effort was directed toward the measurements of
pressure, acceleration, temperature, and heat flow.
The ma}or areas d investigation were the following:
piezoresi stance, roagnetoreslstance. plezocapocitance.
heat transfer measurement using thermetric films,
and heat transfer measurement using ultrasonic pulse
techniques. In addition, preliminary investigations
were carried out on the use of magnetic transitions foi
temperature measurement, measurement of tempera-
ture using the pyroelectric phenomenon, measurement
of heat transfer using a transverse thermomagnetic
effect, the acoustoelerrric effect, and elastic ppm-
poslte piezoelectric materials. In the area of plezo-
resistance, in addition to background work, a minia-
ture piezoresistive pressure gauge was built and
t^ted. (Author)
Howard Industries . Inc . , Racine, Wis .
RESEARCH AMD DEVELOPMENT OF HAND
DRIVEN GENERATOR G-50 ( ) /G (XMl) UGHT
WEIGHT (FOR USE WITH RECEIVER-TRANS-
MITTERS RT-66/GRC, RT-67/GRC, AND
RT-68/GRC) by W. Arthur Ernst. Technical rept.
(final) 1 May 56-1 Dec 57. on Contract DA 36-039-sc-
72335. [1957] 61p. AD-158 529.
OrderfromLC mi$3.90, ph$10.80 PB 150 846
Hughes Aircraft Co. , Malibu, Calif.
INTERPOLATION TECHNIQUES APPLIED TO PAT-
TERN SYNTHESIS, by A. Ksienski. Scientific rept.
no. SR 3508/8 on Contract AF 19(604)3508. Oct 60,
23p. 7 refs. AFCRL-TN-60-1178; AD-250 937.
Order from LC nai$2.70. ph$4.80 PB 154 595
A pattern synthesis method is presented that has ap-
proximative charaaeristics similar to that of a
Fourier series but is computationally much simpler,
and consequently results in a higher over -all accuracy.
Error estimates and convergence measures are pre-
sented, which compare the above synthesis to the
Fourier approximation and the Woodward method.
(Author)
Hughes Aircraft Co. , Malibu, Calif. f" -'^
A METHOD FOR SYNTHESIS OF OPTIMUM ClREC-
TIONAL PATTERNS FROM NON-PLANAR APER-
TURES, by J. H. Harris and H. E. Shanks. Scientific
rept. no. 3508/10 on Contract AF 19(604)3508. SepW
31p. 4 refs. AFCRL-TN-60- 1168; AD-250 938.
Order from LC ml$3. 00. phJ6. 30 PB 154 596
726
Tlie scalar radiation problem la considered for radiat-
ing surfaces of arbitrary shape. The source distribu-
tion which produces an optimum directional pattern is
determined. Examples are included for apertures in
planes and spheres. (Author)
Illinois U.. Urbana.
A PROTON PROBE FOR MEASURING MAGNETIC
FIELD, by Van Bluemel and Santimay Chatter)ee.
Technical rept. no. 16 on Contract Nonr- 1834(05).
22 Apr 60. 15p. 6 refs. AD- 235 942.
Order from LC nil$2. 40, ph)3. 30 PB 154 114
This report provides a brief general description of the
prcton resonance device used for measurement of
bomogeneous magnetic fields from 3 kilogauss to
15 kilogauss.
Johns Hopkins U , Baltimore, Md.
REPRESENTATION AND ANALYSIS OF SIGNALS
PART VII. SIGNAL DETECTION IN A NOISY WORLD
bf W. H. Hugglns. Rept. on Contracts AF 19(604)1941
andNonr-248(53). 15 Sep 60, 92p. 21 refs. AFCRC
TN-60-360; AD- 245 887.
ft-der from LC mi$5. 40. ph$15. 30 PB 152 965
Many of the in^trumematlon principles used in elec-
tronic equipments today coauln the tadi assumption
that it Is possible to sort out the desired signal from
the undesired signal by simple linear filtration. How-
ever, when interfering signals and nrtse of unpredicta-
ble form and widely varying intensities are present,
linear filtration la no longer adequate. It is then neces
sary to accept or rejea the signal on the basis of its
ti^ature or waveshape, and this requires the meas-
arament of many coordinates. This problem is dls-
eoMed In terms of the geometrical notions of a signal
•pace and shows how signal energy, waveshape, and
baw^ridth are related respectively to the length, direc-
tion ajK) angular velocity of a signal vector in this sig-
nal space. Attention is directed to the practical prob-
lem of relating these abstraa ideas to engineering
practice and to designing an efficient signal analyzer
wUch will measure the principal components of a slg-
MI ensemble so that each signal may be adequately
characterized by specifying the fewest number of
coordinates, thus simplifying the data -processing
^oWem. The phase -principle <rf algnal detection is
icneralized to be applicable to signals of arbitrary
wve-form and it is shown that a particular reaUzation
Of a phase detector using super Umiters requires about
5 <lb more S/N than does a conventional matched -filter
•mplltude deteaor for the same detection and false -
utrm probabllliles. (Author)
lincoto Lab., Mass. Inst, of Tech., Lexington
AN S-BAND SYSTEM FOR MEASUREMENT OF
SCATTERING FROM HYPERVELOCTTY MODELS, by
H. G. Pascalar and D. E. Crook. Rept. on Contraa
AF 19(604)7400. Oct 60. 36p. 312G-0002;
AD-250 799.
OriStT from LC ini$3. 00. ph$6. 30 PB 154 589
ve
The microwave system described has as its object!,
the meaaurement of both the amplitude and phase of
ne backward and forward scattering compooenta from
the ioolzed trails following miodels fired from a hyper -
velocity gun into a tunnel evacuated to upper atmos-
phere pressures. Preliminary calculations indicated
backscattering voluss reflection coefficients on the
order of 10*3 to 10"*; consequently the requirement
for amplitude sensitivity of the system to refleaed
signal, i.e. backscaner, was set at 10"5. The antici-
pated magnitude variation of the signal transmitted
through the ionized trail was on the order of a few db,
so that the detector and indicator for the transmitted '
component was required to indicate clearly minimal
amplitude changes of 0. 1 db. In addition to measuring
the amplitude of both the refleaed and transmitted
components, phase dau was desired on both compo-
nents. This phase requirement necessitates detectors
which are phase coherent with the signal source The
phase coherent detector used here is a crysul con-
trolled superheterodyne receiver. (Author)
Lincoln Lab., Mass. Inst, of Tech. . Lexington.
TRAVELING-WAVE TUBES IN RADIOMETER^ by
David Karen. Rept. on Contract AF 19(604)740a
28 Dec 60, 28p. 47G-0011; AD- 249 572.
Order from LC mi^.70, ph^SO PB 154 061
Existing low-noise traveling -wave tubes have been
used radier extensively in radiometers and radar
receivers. Certain effects pertaining to the perform-
ancb of these tubes such as intermodulation and
phase modulation are at times neglected. An investi-
gation was made into the causes of these effects and
a quantitative evaluation of die performance of these
tubes, specifically as applied to radiometers. All
measurements and experiments reported were per-
formed on three RCA type 6861 low-noise S-band
tubes and the results are the average characteristics
of these three tubes. The individual characteristics
of all tubes were quite similar and the results "may
diferefore be applied to individual specimen. (Author)
Material Lab., New York Naval Shipyard. Brooklyn,
N. Y .
PRIMARY REFUCA SOURCES FOR MEASURING
UGHT OUTHJT OF CATHODE RAY TUBE
SCREENS, by Milton Adelman . Final rept. 22 July 59
23p. 14 refi. Lab. ProJ. 5032-B-15.40.
Order from LC ml$2.70. ph$4.80 PB 155 320
This repon released for sale to the public 3 Apr 61 .
Primary replica sources developed for light output
measurements of cathode ray tubes are described for
screen types PI, P2, P5, PU, P12, P14, PI 9 and P25.
The utilization of these replica sources for screens
having a long phosphorescent decay, and the develop- >
ment of limits for specific screen types are recom-
mended fof ioclution in MIL-B-1 electron tube speci-
fications. (Author)
Michigan U. Research tost. , Ann Arbor.
ONE-CaMENSIONAL TRAVELING- WAVE TUBE
ANALYSES AND THE EFFECT OF RADIAL ELEC-
TRIC FIELD VARIATIONS, by Joseph £. Rowe.
Technical rept, no. 30 on Contract AF 30(602)1845.
July 59, 59p. 9 reft. 2750 9-Tj RADC TR-59-124;
AD- 226 006.
Order f^pm LC ml$3.60. ph$9.30 PB 150 902
727
The equivalence at the differencial equation and inte-
gral equation approaches to the solution al the non- -
linear traveling -wave amplifier problem Is shown
rigcHXMJsly. The eqi^tions can be transformed one
into the other withoi* making any additional assump-
tions. The space-charge expression developed on the
basis at considering the electron distribution in phase
space is shown to give the same form for the space-
charge weighting fiosctioa as a space-charge escpres -
slon based on the electron distribution is space. Effi-
ciency calculations are compared for the 2 methods
and the agreement is excellent. The effect al radial
electric field variations due to the circuit is con-
sidered and it is shown that the efficieDcy for large
streams is reduced In direction proportion to the
square at ttie field reckiction function. (Author)
Microwave Research Inat. , Polytechnic Inst, at
Brooklyn. NY.
CARRffiR FREQUElfCV NETWORKS, by Gerald
Weiss. Rept. on Co^traaAP 30(602)1648. 12 Jan 59,
I92p. 37 refa. Research rept. R-701-58: PIB-629;
RADC-TN-59-33; AO-210 112.
Order from LC mlM. 70. ph$30. 30 PB 155 160
This report released for sale to the public 29 Mar 61.
A unified theory is presented at analysis and synthesis
of linear carrier frequency networks, based on the
work of various auttvirs in the field. The response d
the network to the modulation envelope is character-
ized by an envelope response function, a doubly-com-
plex expression, which depends on 2 independent pa-
rameters, the carritr frequency and the carrier phase
resolution angle. The poles and zeroa al the envelope
transfer function are derived from the polea and zeroa
of the conventional network reaponse function. Practi-
cal synthesis requires that the desired function be ap-
I^oxlmxed by a realizable one. A logical approxima-
tion procedure ia selected which leads to results iden-
tical to those otatainad by the conventional low-paaa
band-paaa transformation, ft is shown that the con-
>enCloiial R-C notch necworks uaed in ac aervomecha-
niams are merely R->C realizationa al the knr-paas
band- pass transfornwtion for special pole locationa. A
simple, practical method Is described for the design o<
ac lead networks, particularly bridged-T's and paral-
lel-T's. directly from the pole - zero specificacioas.
ReaUzabtlity of thesa structures requires a aacrifice
of zero frequency gain. A simple formula comparea
the gains of the various networks. The desired net-
work can be realized by doubUng the value of the
specified zero. (Author)
Microwave Research Inst. , Polytechnic Inat. of
^ooklyn, N. Y. I
COMPENSATION OP NONLWEAR FEEDBACK SYS-
TEMS BY MEANS OF AN INEXACT MODEL, by
Kenneth R Kaplan and John G Truxal. Rept. oa Con-
tract DA 30-0W-ORD-1560. 8 Jan 58. 24p. 5 refa.
tept. 11-636-57: PIB-564: AD-153 917.
Order from UC mi$2. 70. phM- 10 PB 154 S04
A cotiditionally stable system exhibiting sustained
oscillations la the presence (A an amplttude-dependeiK
nonliaearity waa us4d to iUustrace the shortcomings of
exact compenaatlon. as well as the design and jH-aai-
cability of an Inexact model. In general, the experi-
mental results served to substantiate the theoretical
prediaions. The system with exact compensation did
yield a very small output when driven with a ramp.
The inexact model provided stability, and greatly en-
hanced the properties of the system.
Microwave Research Inst. , Polytechnic Inst, at
Brooklyn, N. Y.
DISTRIBUTED PARAMETER NETWORK SYNTHESIS
USING THE POTENTIAL ANALOG CC»4PUTER. by
Alfonse Acampora. Rept. on Contraa AF 30(602)1709.
6 Apr 59. 49p. 8 refs. Research rept. R-719-59;
PIB-647; RAIX-TN-59-182; AD-216 434.
Order from LCmi$3. 30, ph$7. 80 PB 150 906
la the past, a computer utilizing a potential analog haa
been used In lumped-element circuit synthesis. A pre-
scribed immittance amplitude and phase response was
approximated with a rational function of the complex
variable P > cr -t- )a). Since the computer is capable of
yielding only rational function solutions, anempta to
extend ita use to approximate distributed parameter
loads in terms al transmission lines and resistors lead
to complicationa. Driving point and transfer impedance
as well as scattering coefficients of such approximating
networks are, in general, not expressible as rational
functions of P, but are usually transcendenul in nature
In this thesis, a transformation of the complex
variable, termed a lambda tranaformation (A- Z-t^jA).
ia described and used whereby networks consisting of
lossless commensurate, transmission lines and re-
sistors are directly expreasible as rational functions
al the tranaformed variable X. The computer can be
used to achieve networka which approodnoate a pre-
scribed amplitude and phase response of a certain nee
work function over a defined range d real frequency.
The distributed parameter approximating structure ia
arbitrary ui form and number of elements except that
it conaists of lossless commensurate lines and reals-
tor a. The structure ol the resulting networks is spe-
cifically prescribed at the oUset of the approximatioa
procedure. In the latter case, the particular networki
considered are caacaded, loaaleas-Iine, two-ports
terminated in pure resistance. (Author)
National Research Labs. , Ottawa (Canada).
LOW TEMPERATURE PERFORMANCE OF LEAD
ACID BATTERIES^ by T. R. Ringer. Sep 60, 38p.
2 reCs. Mechanical engineering rept. MD-45.
Order from LC mi$3.00, ph$6.30 PB 154 550
The discharge characteristics of two lead acid
bstteries al 100- and 4S-ampere-hour capacity were
determined for a range of current discharge rates
over a ten^erature range of ■fZS^'P to -60OF.
(Author)
Naval Avionics Facility. IndianapoUs, Ind.
ELECTRICAL HOOK-UP WIRE, FUNGUS RESIST-
ANCE OP, by Paul H Guhl. Feb 58, 44p. Materials
rept. no. 54; AD- 200 088.
OrderfronLCnriOaO. ph$7.80 PB 154 487
Thia report released for aale to the public 27 Mar 61.
728
In the search for a reliable, accelerated teat pro-
osdure for the determination of fungus resistance of
hook-up wire insulation, results obtained from experi-
ments conducted on wire specimens were compared to
results obtained on like specimens exposed to the en-
vironment of a tropical locale. Two test procedures
were followed: the petrl dish culture method of specifi-
cation MIL-I-631 and a surface insulation resistance
method similar to that of specification MIL-W-S086.
Test specimens of hook-up wire were sent to the
Tropical Exposure Site in the Panama Canal Zone
where siu-face insulation resistance values and visual
fungus growth were determined periodically. Neither
test method was infallible; the resulta obtained by the
petri diah culture method w&e much more reliable in
the prediction of fungus resistance of hook-up wire.
(Author)
Naval avil Engineering Lab. , Port Huenone. Calif.
CORROSKM OF LEAD CABLE SHEATHS AT
KOOIAK. ALASKA, by B. R. Holden and W. A.
Bowen, Jr. Final memo. 5 Feb 51, 26p. 6 refs.
l^schnical memo. M-042.
Order from LC mi$2. 70, phR 80 PB 154 624
Lead-sheath corrosion of the underground telephone
and electric power cables at Kodiak, Alaska, has
been investifpated. Potential, resistance, and current
measurements were made between the sheath and a lead
thig which was pulled through an adjacent duct. Vari-
ous other electrical tests were conducted. pH ami
resistivities were determined on water and soil
samples. Corrosion products and other materials
were analyzed. The data and visual observations show
ikK serious electrolytic corrosion is takii^ place and
ttmt chemical corrosion also is occurring, but to a
lesser extent. The electrolysis of lead is attributed
primarily to galvanic currents arising from the bond-
ing of a copper ground to the lead sheath. The infor-
mttlon secured indicates that the chemical corrosion
it caused by alkaline materials which are heii^
leached from the concrete.
Naval Ovll Engineering Lab. . tort Ifaeneme, Calif
DBVELOI*IENT AND EVALUATION OF A KNOCK-
DOWN ANTENNA MAST, by J. E. Schroader and J. J.
TYaffalis. Final rept. 5 Sep 57, 2lp. 4 refs. Technics
KXe N-319.
Order from LC mi12. 70, ph$4. 80 PB 154 681
Ihe laboratory was authorized to develop a suitable
mast tor use as rhombic and strongback antenna insul-
iMioas. This report covers the design criterU, a de-
*crl|icion of the developed mast, test procedures, and
conclusions reached from the evaluation of test results,
k is recommended that the developed mast be accepted
for advanced base use. (Author)
Maval Civil Engineering Lab. . Port Hueneme, Cslif
reRPORMANCE OP THE AN/URM-37 FOR RADIO
WTBRFERENCE MEASUREMENTS, by D. D. Hughea
Z)MayS7. 3 refs. Tectnical note N- 302.
Older from LC mi$2. 70. ph$4. 80 PB 154 680
T^ AN-URM-S7 wsa found to lack the! required sea-
■Wvliy for the direct correlation with standanl con-
formance testing equipment and procedures given in
BUSHIPS Specification MIL-I-16910A. It was also de-
termined that nKxlerately high ambient levels of radio
frequency energy, modulated at an audio frequency
rate, can prevent operation of this type of equipment.
The AN-LJRM-37 does exhil^t desirable characteristics
when used as a broad-band voltmeter. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
RADIO INTERFERENCE RADIATION TESTS ON AN
ALTERNATING CURRENT POWER SYSTEM FOR
AUTOMOTIVE EQUIPMENT, by D. B. Wright.
15 Jan 52, 18p. Technical note N-071.
Order from LC nU$2.40, ph$3.30 PB 154 643
Naval Civil Engineering Lab. , Port Hueneme, Calif.
RAUO INTERFERENCE SUPPRBSSICM OF A PROS-
PERITY NO. 2C-Jr. LALWDRY WASiER. by
A. M. Intrator and B- D. Penler. 20 Feb 53, 14p.
Technical note N-128. ■
Order from LC mi$2. 40. ph$3. 30 PB 154 651
An investigation was made to determine a practical
method of suppressing radio interference generated by
operation of a 25 -lb wringer-type laundry washer, type
2C Junior. Measurements indicated that approximately
every twenty seconds (the time point at which the
motor waa reversed), narrow high -intensity pulaea
were radiated from the laundry washer. The magni-
tude of the pulses was of the order of 10* microvolts
per meter at frequency of 200 kc to 20 mc, measured
5' from the machine. Interference of a higher repeti-
tion rate and a lower level was observed continually
throughout the above frequettcy range. This continual
low level interference was filtered and shielded to a
point where it was not detectable but the narrow high
intensity pulses were not satisfactorily reduced by
these standard suppression techniques. The high in-
tensity pulses were caused by transients resultii^
from switching of the reversing contactors. The
switching transient interference does not lend itself to
elimination by the methods presently used in radio
interference suppression. The use of lossy lines and
non -linear resistors was considered. Only the latter
waa considered to have promise.
Naval Civil Engineering Lab, , Port Hueneme, Calif.
SOME THEORETICAL CONSIDERATIONS CONCERN-
ING RADIATION FROM OVERHEAD TRANSMISSION
LINES, by A. M. Intrator. 28 June 53, 36p. 14 refs.
Technical rept. R-003.
Order from LC mi$3.00, ph|6.30 PB 154 618
An experimental program to investigate methods of
suppressing radiation from overhead power lines
called for the use of some new techniques. To undo:-
stand the problem more fully and to obtain information
useful in planniag die tests, a review of the theory of
radiation from overhead lines was made and the
theory used co compute values and construct curves of
the radiation field panern within 3000 meters of a
3 -wire transmission line 2(XX) meters long with ground
return through the earth. It is assumed that the line
aas as a horizontal transmlniqg antenna and that
both the transmitting snd receiving antenna are rela-
tively dose to the ground. Only die surface wave
729
need be considered uitder these coDdltlooi. It Is
CGOcluded chat radiation from power lines Is direc-
tional along the axis ol the line and that the field
strength decreases rapidly with distance from the
line. Interference caused by the coupling d spurious
energy to power lines will be slight at very high
frequencies. Radiatl|» will more likely be greater
from transmission lines with grounded -neutral, wye-
ccnnected transfarm*rs at both ends than from other
systems. (Author)
Naval Civil Engineering Lab. , R»rt Hueneme. Calif.
TELEPHONE BATTBRY BOX, by A. M. Intrator.
23 July 51, 28p. Technical note N-029.
Order from LC ml» 70. ph$4. 80 PB 154 639
At the request at the Bureau of Yards and Docks, the
Laboratory has studied the possibility at designing
a battery ba» for use with Telephone Set YfcD Stock
No. 3K15-4 and Rii^er Box YiD Stock No. 3K14-1.
A laminated plastic model was prepared forarrange-
ment.and dlinensional studies, which led toa general
molded-plastic design suggested for quantity
production.
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
UNIVERSAL PREFABRICATED WIRING HARNESS,
by E. D. Pettier. 30 July 53, lOp. Technical note
N-158. ;
Order from LCmi$l. 80, ph$ 1.80 PB 154 656
The problem resolvels itself to one of designing an
electrical distributioin harness that will require a
minimum of tools an^ can be applied to the structure
with as little exertioi on the part of the mechanic as
possible. This harness should be so designed as to
be universal for aU ^Izes and shapes of structures.
A polarized plug-in System is used to make it possi-
ble for Inexperienced personnel wearing arctic cloth-
ing to easily install this type erf wiring system by sim-
ple written instructions chat would accompany the
component pans . M<>8t of the components are pre-
wired with the conductors insulated with a relatively
inexpensive compounp. It is expected that the cost of
such a system will bt economical , as all of the com-
ponent parts are now, presently available on the mar-
ket and need to be only slightly modified to meet the
requirements of the tUniversal Prefabricated Wiring
Harness." i
Naval Ordnance Lab. , Corona, CaHf.
DESIGN OBJECTIVES FOR TELEMETRY R-F
TRANSMISSION UMCS FOR THE PERIOD 1960 TO
1970, byT. B. Jack4on. I Jan 61. 26p. NAVWEPS
rept. 7161: NOLO rept. 538, supersedes NOLO tech-
nical memo- 73-48; AD- 249 937.
Order frort OTS JO. 175 PB 171 690
Performance charac<erl8tia«, design Urnitariona. and
special operational features required In a general -
purpose UHF telemetry transmission bnk are pre-
sented. Separate cofisideration is given to the trans-
mitter, receiver preamphfier- converter, distribution
amplifier, main recover, and receirhig antenna por-
tions of the link. Fltxlbtllty of operation and provision
1
for adapting the ground station complex to other thaa
the presently assigned UHF telemetry bands are
emphasized. (Autbotr)
Naval Ordnance Lab. , White Oak, Md.
A FREQUENCY MODULATION PLAYBACK SYSTEM
WITH WOW AND FLUTTER COMPENSATION, by
Victor & Newton. 1 Av% 59, 22p. 3 refs. NAVORD
rept. 6633; AD- 231 113.
Order fron LC ml$2. 70, phK 80 PB 154 814
Magnetic tape recordhig systems which use an FM
carrier are subject to noise caused by variations in
tape speed. This report describes a playback system
which operates on a sampling principle to reduce this
noise electronically. The noise is removed by divid-
ing th* data frequency by the reference frequency.
By doing this the degree at compensation is main-
tained Independent of data frequency, thus overcoming
a disadvantage of earlier systems. The systemialso
features improved daU handling capacity and sliij-
pliclty. (Author) .. u-jl
Naval Research Lab. , Washington, D. C.
THERMOELECTRICITY, by J. W. Davlsson, Joseph
Pasternak and others. Status rept. no. 6, Dec 60-
Jan 61. [1961] lOlp. 14 refs. NRL memo. rept. 1127.
Order from GTS $2. 50 PB 171 691
Results are summarized of research (1) on principles
for selecting thermoelectric (TE) materials. (2) on
the development at new semiconductor materials for
converting heat to electricity from 800° to 1600OK, (3)
on the correlation betweenthe semiconducting proper-
ties of CuGaTe2 and tellerium vacancies in the lattice,
(4) high -temperature measurements of TE materials
(especially alloys of AgSbTe2 and AgBiTe2) for power
conversion, (5) on structural investigations of TE ma-
terial (e.g., Bi4SbioSeTe25). (6) on refractory ga<k>-
Hnium and hafnium compounds, (7) on (Cr, Mn)Sl2
p-type and on (Co, Fe)Si n-type systems, (8) on the
Seebeck -coefficient and dc-resistivity measurements
on LaMnOs and LaFe03 with SrO additions and on ZnO
with AI2O3 additions. (9) on the effect erf oxidizing and
reducing atmospheres on the differential Seebeck co-
efficient of liquid N«20- 6V2O6, (10) on the physical ,
properties of solid solutioos. aad compounds pf meuls
with tungsten trioxide, and other semiconductor ma-
terlaia, (11) on the thermal conductivuy of cuprous
sulfide, (12) on the preparation of and the transport
processes in inorganic anxx-phous aolids (e.g. , the
systems As:Se:Te and A8:S:Te), (13) on the prepara-
tion of compositions wjth 20% AlAs. and (14) on the
electrical properties of ytterbium nitride. It is an-
nounced that a figure of merit of 45 x 10" ^ at SOO^C
has been obuined for Gd2Se3 and that a 2-stage
thermocouple has operated with an overall efficiency
of I3|jt. (See also PB 161 977)
New Mexico U. Engineering Experiment Station.
Albuq^rque.
TRANSACTIONS OF THE 1959 SYMPOSIUM ON
RADAR RETURN. 11-12 MAY 1959. PART 1. UN-
CLASSIFIED PAPERS. Repi. on Contract N123-6C)630-
18138A. (1959) 455p. 78 ref8.^K>TS TP 2338;
AD- 244 937.
Order from LC mi$ll. la ph$69. 50 PB 155 079
This repon released for sale to the public 29 Mar 61
730
Contents:
What radar can do for you
Sea clutter at high depression angles with applications
to the ground clutter problem
Factors influencing the enhanced radar reflectirity of
thunderstorms - > ^;-i
A photographic method for analyzing radar osdllo-
acope photographs
Airborne terrain return measurements
Radar terrain return: A theoretical approach
Ground and sea return signal characteristics of
microwave pulse altimeters
An automatic amplitude distribution recorder
Radar altimeter -ocean wave profiler
Radar backscatter as a tool for siting communication
terminals
Radar design using acoustical simulation aa a tool
Some doubts concerning the specular -plus -scatter ' '"*
theory of radar return
Back -scattering characteristics of land and sea at
X-band
Radar cross section of terrain near vertical Incidence
at 415 mc, 3800 mc. and extension of analysis to
Xband
Note on an FM altimeter based on phase dlscrimina-
doo
Gutter spectra for an airborne CW doppler radar
Office of Technical Servicea, Dept. of Commerce,
Washington, D. C.
FUEL CELLS AND RELj\TED RESEARCH. Feb 61,
7p. 82 refs. OTS Selective Bibliography SB-447.
Order from OTS $0. 10 OTS SB-447
Reports are listed whidi deal with fuel cells or related
research when it was done leading to the development
of fuel cells. Also included are reports on subjects in
the general fields of batteries. ele<itrical power
sources and electrochemistry which Include Informa-
tion on fuel cells.
Ffcge Communications Engineers. Inc. , Washington,
Q C
IONOSPHERIC- SCATTER FAQLITIES AND PER-
FORMANCE OF ANTENNA SYSTEM. Rept. no. 1
(Final) on ProJ. Test Rai^e. Contract AF 30(602)1756.
S«>59, 131p. PCE-R-6901A; RADC TR-59-175:
AO-228 181.
Order from LCmi$6. 90. ph$21. 30 PB 150 914
Qootentt:
Circuit description
New site requirement
Circuit parameters
Site characteristics
Facilities and equipment
AflCenna system performance measurements
Measurements and tests
Transmission line and antenna feedllne measurements
Antenna element symmetry measurements
Antenna radiation pattern measurements
Vertical polarization measurements
JVrformance of modified Collins 15-101 filters and
paralleling networks
Receive filters
Transmit filters -^. .4
ftrallellng networks
PhllcoCorp. , Philadelphia. Pa.
RESEARCH IN MICRO FLIP-FLOPS, byT. V. Slkina.
Quarterly status rept. no. 6, 25 June 60-24 Aug 60,
and Final technical rept. 25 Mar 59-24 Aug 60 00
Contract AF 19(604)5537. 24 Aug 60, 91p. 16 refa.
Philco no. 2218-F.
Order from GTS $2. 25 PB 171 566
The feasibility of applying thin-film techniques to
microminiature circuit plates or functional circuit
blocks has been demonstrated. This unified approach
consisted of both active and passive elements fabri-
cated by solid-state techniques on a sihcon substrate.
The active component, or transistor, which was uni-
laterally constructed, was found fully compatible with
the one-sided approach to microminiaturization. Ex-
cellent switching characteristics were achieved with
this active device. Even further improvement in
switching times should be attainable. GaAs tunnel
diode arrays were hi^y reproducible for the peak
curretit range of 10 to 20 ma. The best uniformity of
characteristics and reproducibility of diodes was
achieved by the "forced alloying" technique. Two
methods were developed for achieving the desired
peak and valley current. There were (1) controlled
electrolytic etching, and (2) temperature controlled
re-alloylng.
Polytechnic Research and Development Co. , Inc . ,
Brooklyn, N. Y.
RESEARCH AND DEVELC»»MENT OF EXTREMELY
BROADBAND WAVEGUIDE COIvIPONENTS, by
Christian D. Berger. Semi-annual rept. for 15 Mar-
14 Sep 56 on Task 2, Contract DA 36- 039- sc- 64588.
[1956] 29p. AD- 129 932.
Order from LC mi$2.70, ph$4.80 PB 154 957
This report released for sale to the public 24 Mar 61 .
An engineering survey is being conducted on single-
ridged waveguide fabrication methods to determine the
most suitable method of fabrication. Tw6 waveguide
sizes permitting operation in the 3.75- to 15%mc and
the 10- to 40-kmc ranges are included. The over-all
lengths of the waveguides considered are 3 to 5 ft,
with semicontinuous lengths of over 5 ft. The ap-
pearance of the first 18-in. sample length of ridged
guide produced by the Standard Metal Corp. appeared
to promise ultimate success in providing at least one
practical method of n«king uniform ridged waveguide
in long lengths . Experiments by the Makeplece Co.
indicated that the process of extruding and drawing
will ultimately prpve feasible . An electroformlng
process was also considered, but after evaluation It
no longer appeared to warrant consideration . Ade-
quate techniques for measuring the internal cross -
sectional dimensions of ridged waveguides were made
available by the application of wedges in the design of
special gages for measuring these dimensions .
Polytechnic Research and Development Co. , Inc. .
Brooklyn, NY.
RESEARCH AND DEVELOPMENT OF EXTREMELY
BROADBAND WAVEGOTDE COMPONENTS, by Paul
Schlffres. Final rppt. on Task 1, Contraa DA 36-
039-8C-64588. 1 Sep 57, 87p. 11 refs. AD- 200 649. ,
Order firom LCmiM.80, ph$13.80 PB 154 956 .
This report released for sale to the public 27 Mar 61.
731
A study was made to determine the relative levels erf
the higher order TEno modes that may be set up and
propagated in extremely broacftjand flat waveguide* and
waveguide component*. Measurement of the relative
levels was restricted to the case where the flat guide
is terminated in a matched load for all modes. Two
approaches to the noecisuring problem were considered:
(1) the use or small, movable voltage probes to meas-
ure the maximian and minimum at the voltage standing
wave between two TE^o nriodes and (2) a flat -guide
resonant cavity, ser^- coupled to the transmission
line which, at a'particular frequency, is resonated for
one TEno mode at a time. The second ap^o^oach was
more promising. The anticipated loaded Q's and rela-
tive output voluge arc calculated theoretically for the
restricted case at T^iq- «nd TEaQ-mode propagation
in the 9- to IS-kmc range. All possible degenerate
resonance positions are found, and the manner in
which they affect the use of the instrument is dis-
cussed. The scheme for calibrating the cavity as a
mode-measuring insfrumeitt employs zero-thickness
inductive dlscontinulcies d knowrn excitation character-
istics to generate higher modes. The mode measuring
instrument is suitable for meaauriag the relative TEqo
mode amplitudes in f)at waveguides only to an accu-
racy o# a few cto. Nevertheless, the multimode flat-
guide cavity provided a convenient and rapid means erf
determining the presence and order d magnitude of
TEno modes.
Polytechnic Research and Develo(jment Co. . Inc. ,
Brooklyn. N. Y.
RESEARCH AND CaVELOPMENT OF EXTREMELY
BROADBAND WAVEGUIDE COMPONEKTS. by
E Lampner. Final rept on Contraa DA 36-0^9-8C-
64588 1 Sep 57. 75f. 12 rels. Repi. no. 9.04;
AD- 200 650. „ ,^„
Order from LCmiV^. 50. pMl2. 30 PB 155 259
Thla report released for sale to the public 30 Mar 6l
The purpose at this fjroject is to make an engineering
study al possible nMfhods of fabricating single-ridged
waveguide and to detiermine the most suitable method
of fabricating the twp sizes of waveguide designed for
the 3.75-to-l5-kmc and lO-to-40 kmc frequency
ranges respectively. The fabrication of lengths o< 3 to
5 feet and lengths owfer 5 feet are both considered.
Radio Corp. at Anaeric*. Somerville, N. J.
108-mc. 10-WATT SILICON TRANSISTORS, by
W. A. Bosenberg. quarterly repc. no. 1, 15 June-
1 Sep 59. on eontratt DA 36 - 039 -sc- 78325 (19601 Up.
2 refs. AD- 229 236. _
Order from LC m4J- 40. p»i$3. 30 PB 154 479
Tbe design of the IGB-mc, lO-watt sUicon tran^ator
is given. An NPyN structure has been selected. Tlie
Comb -Structure geometry «nd the impurity distribucion
are shown. No difficulty is expected in meeting the
electrical specification. However, heat spreading may
be a problem. Two diffusion runs have been started.
Tbe first one is finished and sliovs • relatively low
collector breakdofwn voltage. Most at the problems
involved with the photolithographic precision printing
lectmiques have beer solved. An appreciable amount
of prtjgress has been made in developing suitable nt>et-
allizii^ techniques. Silver looks to be the most prom-
isii« material for metallizing. A new apparatus for
thsrmocompression bonding has been constructed.
TWs apparatus considerably shonens the time of mak-
ing contacts to tbe active areas of the device. (Author)
RCA Service Co. , CsnKlen, N. J.
ECTABUSHMEm- OF METHODS AND PROCEDURES
OF TESTING FOR REUAHLITY IN GROUND ELEC-
TRONIC EQUIPMEKT, by R. A. Miles. Interim engi-
neering rept. on Co«raa AF 30(602)1623. 1 Dec 57.
56p. 10 refs. R-5-57; RADC-TN-58-70, AD- 148 627.
Order from LCml$3. 60, ph$9. 30 PB 155 152
This report released for sale to the public 29 Mar 61
Methods are described for establishing laboratory tests
to determine the reliaWUty of ground electronic equip-
ment inclufUng radar, communications, and naviga-
tional aids. The tests are designed to determine the
mean life of equipments prior to their use in the fiekl
through tbe measurement of equipment charaaeristics
as a means of monitoring equipment performance deg-
radation and failures. The test procedure followed
for an AN/GRC-27 Is presented as an illustrative ex-
ample. Estimates of inherent reliability for the
GRC-27, tbe GPS- 3, and the GPX-20 are summarized
as, respectively, 488, 83, and 456 hr.
RCA Service Co. , Camden. N. J.
METHODS OF FIELD DATA ACQUISITION. REEXK:-
TION AND ANALYSIS FOR GROUND ELECTRONIC
EQUIPMEKT REUABIUTY MEASUREMEKT, by
N Merlock. Interim engineering rept. o« Contract
AF 30(602)1623. 1 May 58, 71p. 5 refs. R-l-58;
RADC-TN-58-183; AD- 148 801.
Order from LCmi$4. 50, ph$l2. 30 PB 155 151
This report released for sale to the public 29 Mar 61.
This report describes the methods of acquisition.
processing and analysis of field data for reUaWlity
measurement on three classes of Air Force Ground^
Electronic Eqjuipments. The Held study was designed
to acquire sufficient controlled data for comparison
with theoretical reliability predictions and laboratory
tests that have been concurrently performed on the
same equipments. The equipments observed are as
follows: Rsd*r<AN/FPS-3). Navigation(AN/GPX-20).
and Commimications(ANA3RC-27). A sample of equip-
ments of each type above waa selected for observation
from four operational squadrons within the Central Air
Defense Force. The program at each site consisted of
the following elements, described in detail in tbe re-
port: (1) Indoctrination of Radar and Communications
Personnel; (2) Collection of general information about
the ske, including equipment, operation and mainte-
nance procedures; (3) Measurement of equipment en-
vironment; and (4) EstabHsbment of controlled dsts
collection. The contrcdled dsta collection phase has
extended over a period of about one year Dsta proc-
essii^ ststistical and engineering analysis techniques
are described. To illustrste the variety of informatiw
available and tl^ methods of sccess, s sample nnacfaiae
rim-off tabulation for the FFS-3 is presented. (Author)
(See slso R 155 15^0
731
g^esrch Lab. of Electronics , Mast . Inst, of
Tech., Cambridge.
IHASE STABIUZATICW TECWNQUES FOR ELEC-
TMOMCALLY SCANNED ARRAYS, by R. S. Badessa
V. J. Bates and others . Technical rept. on Contract
AF 30(602)1862. 4 June 59, 86p. 13 refs . RADC-TR-
59-144; AD- 228 707.
Onlerfrom LCmi$4.80, ph$13.80 FB ISO 913
The result* are summarized of a one- year study of
closed-loop phase control techniques and their appli-
cation to electronically scanned arrays . The require-
ments imposed upon the excitation accuracy for these
arrays are briefly reviewed. Closed-loop control
provides a means for substantially reducing the most
troublesome source of excitation error, phase insta-
bility. In phase stabilized systems incorporating
rapid variation of the transminer frequency, tian-
fient exciution errors may be present, and their
effects are considered in some detail. Two phase
error detector circuits capable of maintaining preci-
sion over a wide frequency band and in the presence
of environmental changes are discussed. Experi-
mental equipment developed to demonstrate closed-
loop phase control at UHF is described. The re-
sponse times and phase accuracies achieved were
l.5-5u«ec and 1-2 degrees , respectively. In order
to demonstrate feasibility at microwave frequencies ,
phsse control was applied to a reflex klystron oscil-
lator aitd to a traveling-wave amplifier. Response
time* of l-1.5psec were observed. Phase accuracy
for the TWT system was demonstrated to be 4 l". It
is concluded that closed- loop phase control is feasi-
ble, and effective in maintaining phase accuracy over
a significant band of frequencies and in the presence
of environmental changes . (Author)
Research Lab. of Electronics, Mass. Inst, of Tech.,
Cambridge.
QUARTERLY PROGRESS REPT. NO. 53 FOR PE-
RIOD ENDING 28 FEBRUARY 1959, by J. B Wiesner.
G. G. Harvey, and H J. Zimmermann. Rept. on Con-
tract DA 36-039-8C-78I08. 15 Apr 59, 224p.
115 refs.
Order from LC mi$9.90, ph$34.80 PB 154 198
This report released for sale to the public 24 Mar 61 .
ConteiKs:
Physical electronics
Microwave gaseous discharges
Plasma dynamics
Solid state physics
Thermoelectric processes and materials
Microwave spectroscopy
Nuclear magnetic resonance and hyperfine structure
Microwave electronics
Atomic beams
Sutistical communication theory
Process analysis and synthesis
Processing and transmission of information
Anificial intelligence
Statistical thermodynamics
Physical acoustics
Speech communication "
Mechanical translation
Communications biophysics
Netirophysiology
Signal detection by human observers
circuit theory
Noise in electron devices
Shop notes
Research Lab. of Electronics. Mass. Inst, of Tech.,
Cambridge .
QUARTERLY PROGRESS REPT. NO. 54 FOR PE-
RIOD ENDING 31 MAY 1959. by J. B. Wiesner, G. G.
Harvey, and H. J. Zimmermann. Rept. on Contract
DA 36-039-SC-78108. 15 July 59. 217p. 104 refs;
AD- 225 974.
Order from LC mi$9. 60. ph$33. 30 PB 154 199
This report released for sale to the public 24 Mar 61.
Contents:
Physical electronics
Microwave gaseous discharges ''
Plasma dynamics
Solid state physics
Thermoelectric processes and materials
Microwave spectroscopy
Nuclear magnetic resonance and hyperfine structure
Microwave electronics
Statistical communication theory
Process analysis and synthesis
Processing and transmission of information
Statistical thermodynamics
Physical acoustics
Speech communication
Communications biophysics
Neurophysiology
Circuit theory
(Author)
(See also PB 154 198)
Sunford Electronics Labs . , Stanford U . . Calif .
ELECTRON DEVICES RESEARCH. Consolidated
quarterly status rept. no. 12. 1 Oct- 31 Dec 59, on
Contracts DA 36-039-8C-73178, AF 33(616)6207.
AF 19(604)5480, Nonr-225(40). and Nonr- 225(24).
[1960] 83p. 32 refs . AD-234 541 .
Order from LC mi$4.80. pt4l3.80 PB 148 332
Summaries are given of research on depressed coUec
tor. current flow in plasmas , traveling wave ampli-
fiers . backward-wave amplifiers , traveling-wave
tubes , broadband master amplifiers , solid state
masers , microwave devices , parametric amplifier*,
traveling-wave and backward-wave oscillators .
crossed field devices , electrolytic -tank studies . par»
metric circuits for frequency conversion and mixing,
helitron oscillator, ferrimagnetic filter and resona-
tors . floating-drift-tube kiystron, beam focusing,
ferrite frequency doubler. (See also PB 147 014)
Stanford Elearonics Labs. , Stanford U. , Calif.
ERROR CORRECTING CODES FROM LINEAR
SEQUENTIAL aRCUTTS, by N. M. Abramson. Rept.
on Contract Nanr-225(24). 13 June 60, 23p. 25 refs.
Technical rept. no. 2002-1; AD-239 777.
Order from LC mi$2. 70, ph$4. 80 PB 149 235
This report is divided into three main sections. In the
first part a tutorial exposition of the theory of binary
correcting codes is presented in terms of matrices^
which may be related to linear binary circuits. The
second part shows how this approach may be used to
relate several different classes of codes. In the third
part the properties of optimum codes are discussed,
necessary conditions for the existence of optimum
burst error correcting codes are obtained, and opti-
mum codes are found lor burst lengths of three.
(Author)
733
Stanford Eleccronicy Labs . , Stanford U. . Calif.
INVESnCATlONS Of NaSE REDUCTION IN ELEC
TRON BEAMS BY MEANS OF LOW -POTENTIAL
REGIONS, by A. W . Shaw. Rept. on Contract Nonr-
225(24). 25 May 60, K)9p. 44 refs. Technical rept.
DO. 401-2; AO-238 1^.
OzderfromLCmi$Si.70. ph|16.80 FB 148 398
Research concerns a mechanism of noise reduction in
traveling- wave and backward-wave tubes . The noise-
reduction comes aboMt when an electron beam is
passed through a low*- potential region of the appro-
priate shape directly in front of the cathode. An anal-
ysis of a beam drlftiqg at a low potential, and an ex-
perimental X-band tube in which a noise figure of 4.5
db was obtained, areiboth discussed. The analysis
uses the denslty-func^on method. (Author)
[Stanford Electroni<is Labs . , Stanford U. , Calif.]
(A RAOAR SYSTEM BASED ON STATISTICAL ESTI
MATION AND RESOLUTION CONSIDERATI(»«, by
B. Elpas . Rept. on Qontract N6onr- 251(32).
15 Dec 58]. Declassi^ed. 159p. (pases i-iii onutted)
30 refs. [Technical itept. no. 361-lJ. AD- 207 896.
OrtlerfrDm LC mi$7.50, ph$24.30 PB 155 260
This report releasedjfor sale to the public 3 Apr 61 .
Contents:
The basic concept of matched-filter radar
Fundamental limitations on radar resolution
A matched- filter radar receiver based on sutistical
estimation theory
System resolution peHormance
System engineering considerations
Complex -signal representation: sampling theorem for
r-f band- limited fui|ctions; noise probability density
Representation of nujiring target echoes
The combined complex correlation function in delay
and doppler shift
Pseudo- random binaty nrxxlulation functions .
Stanford Electronic^ Labs . , Stanford U . , Calif.
STATISTICAL ANALVSS OF AMPUTUDE -QUAN-
TIZED SAMPLED-DATA SYSTEMS. byB. Widrow.
Rept. on Contract Noor- 225(24). 10 May 60. 62p.
12 refs. Technical rax. no. 2103-1; AD-239 776.
Order from LC miJ3l90, ph$10.80 PB 149 236
Contents :
The statistical theory! of amplitude quantization
First-order probability density distribution of a
quantizer output I
First-order probability density of the quantizadon
noise {
Second-order proba|>ility density distribution of a
quantizer output i
Second-order proba|>ility density of the quantization
noise i
On the satisfaction (|f the quantizing theorem;
quantization of the Gaussian signals
Systems applications
Sheppard's corrections for grouping
Interpolation of the fiiat-order distribution deristiy
from the histogram:
Recovery of autocorrelation function from roughly
quantized process samples
Analysis of quantized sampled-data feedback
systems
Linearization of quantized feedback systems by in-
jection of external dither
Stoddart Aircraft Radio Co. , Inc. , Hollywood, Calif.
CORRELATION STUDIES OF INTERFERENCE
MEASUREMENT TECHNIQUES. VOLUME I, by
G- Whiting and B- R. Byerley. Final rept. for
2 Feb 59-15 June 60 on Contract NOb8r-77528. [1960]
117p. 7 refs.
Order from LC ml$6. Oa ph$18. 30 PB 154 412-1
This report released for aale to the public 28 Mar 61.
This repon contains the results of comparison studies
at interference testing techniques over a frequency
range of 14 kilocycles to 1000 megacycles.
Contents: %
Task deacriptions
General factual data
Present-day conducted interference testing techniques
(14 KC - 250 KC)
General problem of lead radiation
Use of current probe for measuring interference
Special applications of the current probe
Correlation studies of characteristics of radio test
sets AN/PRM-l and ANAJRM-3
J-
Stoddan Aircraft Radio Co. . Inc. , Hollywood, Calif.
CORRELATION STUDIES OF INTERFERENCE
MEASUREMENT TECHNIQUES. VOLUME II. Final
rept. for 2 Frf) 59-15 June 60 on Contract NObsr-
77528. [1960] 63p.
Order from LC mi$3. 90, ph$10. 80 PB 154 412-2
This report released for sale to the public 28 Mar 61.
Contents:
Investigation of increasing AN/URM-47 sensitivity
Performance comparisons between radio test sets
ANAJRM-l^A and ANAJRM-17 (XN-3), and Empire
Devices RI-FI meter NP-105
Antenna comparison stixlies
Study of AN/PRM-l shielding AC versus battery
operation
Evaluation of ancillary devices for use with AN/PRM-l
International meeting on vehicular interference
measurement
Recommendations for changes and additions in MIL-
I-1691QA
Recommendations for conducted measurements
Recommendations for radiated measurements
Recommended types of calibration
Recommendation for use and study of new devices
Recommendations for use of special techniques for
making certain types of interference measurements
Recommendations of new frequency and interference
Umits for MIL-M691QA
Recommendations for automatic interference -meas-
uring and dau- processing devices
(See also PB 154 412-1)
734
Systems Development, Inc. , Binghamton, N. V. '
LIGHT WEIGHT HYDRAUUC DRIVE FOR RADAR
AZMJTH CONTROL. Final engineering rept. on
Contract AF 30(635)2810. Oct 58, 28p. RADC-TR-
59-3; AD- 208 292.
Order from LC mi$2. 70, ph$4. 80 PB 150 903
This repon describes the development of the ideas
and specifications , the design of the unit , the con-
struction, the testing, the subsequent redesign, re-
construction and final testing of the unit. (Author)
Westinj^ouse Elearic Corp. , Youngwood, Pa.
COMPARISON OF NW TRANSISTORS AND NPNP
DEVICES AS TWENTY AMPERE SWTTCHES. by
H. W. HenkelstfndF. S. Stein. [Rept. no. 6] on High
Current High Temperature Semiconductor Switching
Devices, Contract AF 33(600)35067. 17 Oct 58, 28p.
AD- 212 748.
Order from LC nii$2. 70, ph$4. 80 PB 155 321
This report released for nale to the public 31 Mar 61 .
Weston Instruments , Newark, N. J.
STUDY OF SOUD STATE PHYSICS APPROACH TO
DEVELOPMENT OF PREQSION, VARIABLE RE-
SISTORS. Interim development rept. for 1 July-
30 Sep 59 on Contract NObsr-77548. phase U . [1959]
40p.39refs.AD-232 486. p^ ^^^ 3^
This report released for sale to the public 1 1 Apr 61
Examination of magnetoresi stance as a phenomenon
is continuing. Very receiu research in this field is
surveyed and critically reviewed. Experimental and
theoretical aspects are weighed and a comparison
sought among the results of simillar researches by
different groups of workers . Special attention is
paid to three materials , viz, indium antimonide,
indium arsenide and graphite . Physical properties of
general importance in resistive device work are
appraised. Piezo- resistance is also looked into
briefly as a possibly useful phenomenon. Indium anti
monide, indium arsenide and selenium are of inter-
est. In addition, the possibility of utilizing photo-
conductivity as an alternative is studied . (Author)
Mechanical Engineering
Aeronautical Engine Lab. , Naval Air Material
Center, Philadelphia. Pa.
FEASIBILITY OF A LIGHTWEIGHT AIR CONDI-
TIONER SYSTEM FOR PISTON ENQNE DRIVEN
AIRCRAFT USING AIR AS THE REFRIGERANT, by
R. J. Lynch. Final rept. no. 5. 27 Feb 61, 36p.
11 refs. NAMC-AEL-1675.
Order from OTS $1.00 « 171 257
The system is feasible for use in piston engine driven
aircraft: however, the power requirement is from
(hree to six times greater than that needed for a sys -
teni employing Freon as a refrigerant. In comparison,
the dollar cost of the air cycle system would be higher
(ban a Freon system, but the overaU weight should be
laM. (Author)
David Taylor Model Basin. Washington, D. C
MATHEMATICAL ANALYSIS AND DIGFTAL COM-
PUTER SOLUTION OP NATURAL FREQUENCIES
AND NORMAL MODES OF VIBRATION FOR A
COMPOUND ISOLATION MOUNTING SYSTEM, bjr
Leon Katz. Jan 61, 2lp. 7 refs. Rept. 1480;
AD- 250 665.
Order from LC mi$2. 70, ph)4. 80 PB 154 507
The mathematical analysis and solutioo of the natural
frequencies aixl normal modes at vibration for a com-
pound isolation mounting system by McGoldrick's
method are discussed. The system consists of an
assembly supported by a set of isolation mountings
carried by a cradle which is, in turn, axjpported by
another set of isolation mountings attached to the hull
of a ship. The solution for a single, resiliently
mounted, rigid body is presented as a special case of
the two-body system. Instructions for obtaining com-
putation service at the Applied Mathematics Labora-
tory, David Taylor Model Basin, and specifications
for requisite data are included. (Author^
David Taylor Model Basin, Washington, D. C.
VIBRATION ISOLATION WHEN MACHINE AND
FOUNDATION ARE RESILIENT AND WAVE EF-
FECTS OCCUR IN THE MOUNT, by Alan O. Sykes.
Sep 60, 106p. 14 refs. Rept. 1404.
Order from LC mi$5.70, pfa$l6.80 PB 155 064
This report released for sale to the public 24 Mar 61 .
The problems of estimating the effectiveness of isola-
tion mounts in reducing vibration are discussed.
Massless spring-dashpot mounts, arbitrary two-
terminal mounts having mass as well as stiffness and
dami^ng. and a special case of this second type, the
continuous mount, are all treated. Curves, data, and
formulas are presented for estimating the charaaer-
istics and effectiveness of both rubber and helical
spring mounts. (Author)
National Research Labs. , Ottawa (Canada).
LOW TEMPERATURE OPERATION OF A CATA-
LYTIC COMBUSTION HEATER, by T. R. Ringer.
Oct 60, 18p. 2 refa. Mechanical Engineeriag
rept. MD-46.
Order from LC ml$2. 40. ph)3. 30 PB 154 7K
Starting and operating tests using two fuels were con-
ducted on a catalytic heater over a temperature range
from ■f70**F to -60^ . The fuel consumption rate was
found to be a function of ambient temperature. An
aliphatic solvent fuel resulted in a hig^r heat output
at all temperatures than that obtained with naphtha.
(Author)
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
DEVEUOPMEHT OF A TRANSIENT PRESSURE
CELL, by R. K. Steele. 16 Mar 51, 9p. 1 ref. Tech-
nical note N-008.
Order from LCmlfl. 80, pfa$ 1.80 PB 154 634
A transient pressure cell is required to measure
blast pressures on buildings, compression in engines <
735
and surges in hydraidic systems . The cell, as de-
signed, was deveioptd to measure the braking pres-
sure of the piston in la Symroo Diesel Pile Hammer ,
but can be adapted ta other uses by merely redesign-
ing the diaphragm of the cell for the working pres-
sures expected.
Naval Civil Engineering Lab. , Port Hueneme, Calif.
A DISCUSSION OF EVAPORATIVE COOUNG AP-
PUCATION, by R. f. Law. 15 Jan 54. 36p. Pinal
technical memo. M-053.
Order from LC mi J 3. 00, pM*. 30 PB 154 626
This report is a summary of selected information on
evaporative cooling Application, problems , and design
considerations , and presents map* indicating areas
where the use of evaporative cooling is recommended .
(Author)
Ordnance, Missiles, and Satsllito V«hicl«t
[Aero- Space Lab. I North American Aviation, Inc.
Downey. CaUf.] 1
DESIGN, CfiVELOIWENT, AND TESTING OF AD-
VANCED PNEUMATIC SOLENOID VALVE (SINGLE-
PASSAGE) PART N0. 4683-59302, by Charles P.
Bacha. Supplementan-y rept. Subcontract to Rocket-
dyne. Contract AF 04(647)160. Sep 60, I47p. Rept.
MD 60-98; AFBMD TR-60-203; Supplement to AFBMD-
TR-59-18: AD- 249 079.
OrderfrpmLCmi$^.20, p»i»22.80 PB 153 870
Results at tests witi RP- 1 , liquid nitrogen, liquid
hydrogen, and helium (at liquid hydrogen temperature
are reported, and design improvements incorporated
durii« fabrication of a second lot (A valves are de-
scribed. Previously published documents , including
the equipmeitt specification, test procedure, lapping
and assembly processes , liquid and low -temperature
test requirements . pnd the solenoid specifications are
included. (Author)
Air Force Ballistic Missile DIv. , Air Research and
Development Command. Los Angeles, Calif.
AN INTRODUCnOW TO BALLISTIC MISSILES.
VOLUME I. MATHEMATICAL AND PHYSICAL
FOUNDATIONS, ed; by Sally F. Anderson, Robert F.
Kiddle and others. Rev. 1 Mar 60, 243p. 22 refs.
AD- 240 177. ^
Order from OTS $3^ 50 « 171 247
In chapter 1, 2, ani 3 are a brief treatment of differ-
ential equations and a review of topics in analytic ge-
ometry and calculus, special attention being given to
conic sections. Chapter 4 outlines vector analysis and
explains divergency in terms of hydrodynamical source
strength. Chapter 5 utilizes Newton's laws ci motion
and the concepts of kinetic energy, conservative
forces, and potential in a discussion of the mechanics
of particles. d'Alefnberts principle and Lagrange's
equations are presented. Chapter 6 takes up the prob-
lem of the mechanics of rigid bodies and considers at
length the reUted subject of orthogonal coordinate
transformations. Other topics discussed are the vec-
torial nature of angular velocity, angular momentum,
moments and products of Inertia, principal axes, the
laws of motion in moving systems, Euler's equationa,
and precessional and nutational motion. Chapter 7 de-
scribes graviutional attraction and potential and ob-
tains the gravitational potential of a homogeneous
sphere and a homogeneous sphere fitted with a heavy
equatorial ring. Chapter 8 preseiws an introduction to
the theory of servomechanisms.
Air Force Ballistic MissUe Dlv. , Air Research and
Development Command. Los Angeles, Calif.
AN INTRODUCTION TO BALLISTIC MISSILES.
VOLUME II. TRAJECTORY AND PERFORMANCE
ANALYSIS, ed. by Sally F. Anderson. Robert F-
Kiddle and othera. Rev. 1 U^ar 6ft 104p. 9 refa.
AI>-240 17*. ^*.,^,..v -
Order from OTS $2. 50 « 171 248
Ctepter 1 treats the motion of a projectile, the effecta
of launchii^ errors on range, and the effects on ur-
geting of errors in the initial parameters, and the
deviation of the earth's gravity from spherical sym-
metry. A geodetic analysis is given In Chapter 2 of
the eanh's gravity and the determination of exact po-
sitions on the eardi'a surfiice. Chapter 3 deals with
the re-entry problems of aerodynamic heating of the
nose cone, aerodynamic forces and moments acting oo
the nose cone in high-speed flow, and simplification
of the re-entry trajectory Parameters of burnout and
variables associated with miaalle design are discussed
in Chapter 4. (See also PB 171 247)
Air Force Ballistic Missile Dlv. , Air Research and
Development Command, Los Angeles. Calif.
AN INTRODUCTION TO BALLISTIC MISSILES.
VOLUME III. CCSIGN AND ENGINEERING OF SUB-
SYSTEMS, ed. by Sally F. Anderson, Roben P. Kiddle
and others. Rev. 1 Mar 6a 135p. 15 refa; AD- 240 179.
Order from OTS $2. 75 PB 171 249
Three aspects at a ballistic missile are discussed.
Chapter 1 presents the conalderations involved in the
construction and operation of rocket propulsion sys-
tems. Chapter 2 discusses aerodynamic forces and
loads which affect the missile structure and trajectory.
CSwpter 3 analyzes attitude perturbations and dis-
cusses missile control systems, including the auto-
pilot. (See also PB 171 248) .^ .
Air Force Ballistic Missile Div. . Air Research and
Development Command, Loe Angeles. Calif.
AN INTRODUCTION TO BALLISTIC MISSILES.
VOLUME rv. GUIDANCE TECHNIQUES, ed. by SaUy
F Anderson. Robert F. Kiddle and others. Rev.
1 Mar 6a 238p. 15 refs. AD- 240 180.
Order from OTS $3. 50 PB 171 250
Chapter 1 presents the main functions of a guidance
system and gives the general features of radar (or
radio) and all-inertial guidance. Concepts of guidance
compuution and the function of guidance equations are
introduced. Radar techniques used to measure range,
ai^e, or velocity of the missile are described in
736
Ctmpter 2. Analyses are given of two means of deter-
minii* missile velocity: the differentiation of position
d»ta, and the use of Doppier techniq^ies to establish
rti^e rates and angular rates. Chapter 3 discusses
inertial navigation, including gyroscopes, accelerom-
ecers. stabilized platforms, and airborne computers.
Chapter 4 summarizes the relative merits of analog
tod digital computers for use in ballistic missile
guidance systems and includes a short description of
digital computer arithmetic. (See also PB 171 249)
Air Force Missile Development Center, HoIIoman
AFB, N. Mex.
PREDICTION OF IMPACT POINT FOR BODIES
EJECTED FROM CARRIER ROCKETS, by Hermann
0. F. Scharn. July 60. 5Ip. AFMDC-TR-60-13.
Order from LC mi$3. 60, ph$9. 30 PB 153 731
This investigation sought a means for facilitating re-
covery of bodies ejected from carrier rockets at
altitudes between 100,000 and 500,000 feet with initial
velocities in the interval 500 S Vi i 5000 fps. The
location of the velocity vector of the ejeaed body at
the time of the ejection is assiBned to be known. With
these parameters as initial conditions, the horizontal
range of a body is calculated with variable gravita-
tional acceleration without regard for the effects of
the curvature and the rotation of the earth. The effect
of air drag in the atmosphere is assumed to be ap-
preciable only up to an altitude of 100, 000 feet, and H
calculated for spheres with different specific weights.
The results of these calculations are presented in
graphs, which in combination with a graphical deter-
mination of the azimuth angles, allow, without further
calculations, the prediction of impact points or areas.
(Author)
Allied Research Associates , Boston. Mass.
LAUNCHING OF AIRBORNE MISSILES UNDER-
WATER. PART VII. HYDRODYNAMIC INERTIA
OKFnaENTS FOR A SLENDER BODY WITH A
SAIL, by Theodore R. Goodman and Ralph Greif .
Rept. on Contract Nonr- 2343(00). 15 June 60, 23p.
B refs. Rept. no. ARA-823; AD-237 631.
Order from LC mi$2.70. ph$4.80 PB 148 216
The inertia coefficients of a two-dimensional body
with one fin is calculated. This result has application
to the calculation of the hydrodynamic forces acting
00 a submarine with a sail . (Author) (See also
PB 153 161)
Army Ballistic Missile Agency. Redstone Arsenal.
Ala.
SECULAR PERTURBATIONS DUE TO THE SUN AND
MOON OF THE ORBIT OF AN ARTIFIQAL EARTH
SATELLITE, by C C Dearman, Jr. 23 Nov 59, 20p.
7 refs. Rept. no. DSP-TR-5-59; AD-232 446.
Order from LC mi$2. 40. ph$3. 30 PB 153 947
New formulas are derived for calculating first order
secular perturbations, due to the Sun and Moon, of the
orbital elements of an artificial earth satellite. The
formulas include the effects of both orbital inclinations
and eccentricities of the perturbed and perturbing
bodies on all the orbital elements of the perturbed
body (earth satellite) moving around a central body
(Earth). (Author)
[Army Ballistic Missile Agency, Redstone Arsenal,
Ala.]
SOME ASPECTS FOR THE DESIGN OF AN
ELECTRIC DRIVE MOTOR OF A FLYWHEEL RE-
ACTION iV^TTlTUDE SYSTEM, by Walter Haeusser-
mann. 3 Sep 59, 5p. Rept. no. DG-IN-4-59.
Order from LC mi$l. 80, ph$l. 80 PB 155 251
This report released for sale to the public 31 Mar 61.
Armv Ballistic Missile Agency (Redstone Arsenal.
Ala.]
THE SPHERICAL CONTROL MOTOR FOR THREE
AXIS ATTITUDE CONTROL OF SPACE VEHICLE, by
Walter Haeussermann. 23 Oct 59, 18p. 4 refs. Rept.
no. DG-TN-59-59; AD-244 034.
Order from LC mi%2. 40. ph$3. 30 PB 155 252
This report released for sale to the public 31 Mar 61.
A spherical reaaion member for a three-axis attitude
control is described and compared with the common
one-axis flywheel system. Special problems are con-
sidered; such as, control of the space vehicle with the
spherical reaction member. t<M-quing the sphere,
supporting it by a bearing, and measuring its speed.
(Author)
Arnold Engineering Development Center [Tullahonw,
Tenn.]
DEVELOPMENT OF INSTRUMENTATION FOR HY-
PERVELOQTY RANGE, by P. L. Clemens and
M. K. Kingery. Rept. on ARO, Inc. Contract
AF 40(600)800. Dec 60, 54p. 11 refs. AEDC-TN-60-
23a AD- 248 572.
Order from LCmiJ3. 60, phJ9. 30 PB 153 846
Recent progress in the development of optical and
radiotelemeiry instrun>eniation for a hypervelocity
range is discussed. High speed, visible- light and
X-ray shadowgraphs are described, and typical
shadowgrams resulting from their use are shown. A
completely transistorized, dark-field, shadowgraph
trigger which uses an optical cavity has been devel-
oped. Circuitry and construction techniques devel-
oped have produced miniaturized, active, telemetry
packages which have performed satisfactorily after
having survived peak launching accelerations of the
order of 150,000 g. Telemetry receiving and minia-
ture transmitting antennas suitable for use within nae-
tallic range walls and within meigllic models have
evolved. Pressure transducers have been developed
which are capable of withstanding gross launching
accelerations. Telemetered pressure data resulting
from in-flight, expenmental tests are compared with
their corresponding theoretical values . Other in-
strumentation equipment used in support of a hyper-
velocity pilot range is also briefly discussed.
(Author)
Arnold Engineering Development Center.
rTiiUahoma, Tenn. ]
DEVELOPMENT OF TELEMETRY FOR A HYPER-
VELOCITY RANGE, by M. K. Kingery, R. H.
Choate, and R. P. Young. Progress rept. on ARO,
Inc. Contract AF 40(600)800. Dec 60, 83p. 10 refs.
AEDC-TN-60-214; AD-248 019.
Order from LC ml$4. 80. ph$I3. 80 PB 153 648
737
Resetrdi concerns khe development of a multl -channel
telennecry system for measurement ct heat transfer
rates, pressure distributions, and accelerations ex-
perienced by free-flight models launched from a hy-
perveloclty gun. Telemetering of pressure data from
a gun- launched modfel In free flight after being sub-
jected to accelerations from 100. 000 to 550, 000 g
was investigated. An ultimate acceleration capability
of one million g 1$ ttelng sought. Several types of
circuitry were evaluated for telemetering pressure
data. Of the types oested, the model with a variable-
capacitance transducer gave the best results. The
telemeter circuitry occupies a cylindrical space one
Inch In diameter by 1. 2 inches long. Experimental
data are presented which demonstrate chat teleme-
tered data can be opined after initUl launching ac-
celerations up to laS, 000 g with less than 15- percent
error. Tliia 125, OOO-g limlutloo was attributed to
the variable -capaciltance transducer Simple RF
oscillators were bqilt using the same circuitry with-
out the transducer. These oscillators survived Initial
acoeieratioos up to 550, 000 g and transmitted during
flight with a frequeticy shift of 0. 02 percent. As a re-
sult of these experiments and the solution of many
prtJtolems involved tn the development of a practical
system, it appears! that direct measurement of aero-
dynamic paramet«»s of gim-launched models in free
flight Is feasible. ^Author)
Bureau of Mines, Pittsburgh, Pa.
INVESTIGATION OF SUSCEPTIBILITY TO DETO-
NATION OT PROPELLANTS. by C M. Mason. F. C
Gibson and others. I Final sumnary rept. 3734,
1 Oct 57-30 Sep 58. on Contract NOrd-03159. [1958]
26p. 3 refs; AD- 2^9 592.
Order from LC ml$2. 70, phK 80 PB 152 022
A medrod, based oi the variation of electrical re-
sistance in a wire element introduced into the charge,
has been developed for the continuous measurement of
burning and detonation rates in ofMque materials. The
method has been used to obtain dau on non-steady-
state phenomena ii» high explosives, in composite pro-
pellants and in liquid fuel-solid oxidizer mixtures.
Composite propelUnts were found to be readily deto-
nable when modified by the introduction of voids.
Studies on liquid fuel- solid oxidizer mixtures, with
bubbles of inert g»$ as well as voids, gave similar
results.
Colorado School Of Mines, Golden.
INVESTIGATION OP THERMAL CHARACTERISTICS
OF TNT AND OTHER EXPLOSIVES, by James O.
Milmoe, James P Kottenstette. and Fred L. Smith.
Technical rept. on Contract AF 29(601)1215. Nov 59.
104p. 16 refs. AF$WC-TR-59-34; AD-230 993.
Order from OTS %\. 50 PB 171 256
Investigations wer^ made on the effects of heat on
military explosives, mainly TNT. X-ray methods in-
dicate no 8tnictur«i changes in cycled TNT of various
crystal sizes, in iJNT heated to high temperatures at
normal pressures pr under vacuum. Infra-red spec-
troscopy of these ^mples showed no measurable
chemical changes. Differential thermal analyses of
TNT, REK and Composition B revealed no unexpected
phase changes. Other thermal reactions were Investi-
gated. Detonation temperature increases with lncrea»
ing heating rates. Cycling the TNT does not signifi-
cantly effect the detonation temperature. Effect of
temperature cycling on solidification point la dis-
cussed. Pressure -temperature relationships are in-
vestigated. A differential equation describing thermo-
dynamic and thermochemical behavior of TNT -Addi-
tive n\ixtures was solved. Experiments showed that
both silica powder and halocarbons raise the thermal
detonation point and increase delay time in powdered
TNT but that the latter only raised the detonation point
In cast TNT. Temperature cycling and aging of re-
cycled pure TNT increase impact sensitivity without
effecting detonation velocity. Silica powder increased
impact sensitivity and detonation velocity. Physical
and chemical properties of TNT were investigated and
the influence of heat discussed. (Author) |.. ' r.
Dymmic Simulations Lab. , Ordnance T^nk- Auto-
motive Command, Center Line, Mich.
DIGITAL COMP[JTER PROGRAM FOR SUPERELE-
VATION CAM DESIGN, by Mary Archambault.
18 Nov 60, 83p. Rept. no. RR-31; AD-248 569.
Order from LC ml$4. 80. ph$13. 80 PB 153 866
A digital computer program is presented for the rapid
calculation of manufacturing data essential to the de-
sign of preproductlon cams which are utilized in bal-
listic computers of tank fire control systems. The
cam profile generated Introduces the superelevation
angle required by tank main armament for a particular
type ammunition. (Author)
Peltman Research Labs. , Plcatlnny Arsenal,
Dover, N. J.
A RELIABLE INSENSITIVE ELECTRIC DETONATOR,
by J. V. Richard Kaufman. Nov 59, declassified
1 Nov 60, 13p. 2 refs. Technical rept. 2658;
AD- 229 041.
Order from LC mi$2.4D, ph$3.30 PB 153 022
It has been found possible, by following a specific pro-
cedure, to prepare quantities of ah insensitive elec-
tric detonator having the desirable attribute erf excel-
lent reproducibility. Since the explosive contained in
the detonator is penuerythritol tetranltrate (PETN), a
marked reduction In handling hazards is attained. In
comparison with standard types of detonators, which
usually contain primary explosives. The principle
upon which the detonator functions is the interaction
between an exploding wire and a loosely packed charge
of controlled-panicle-slze eatploslve. To avoid cor-
rosion, a pure gold wire is used. Reaction times of 5
microseconds have been obtained with detonators pre-
pared by the technique described, with a maximum
standard deviation of .03 nUcrosecond. The method
of preparation is simple and lends itself well to exist-
ing methods for the manufacture of detonators.
(Author)
73t
prebank Co. , Glendale, Calif.
(THE DEVELOPMENT OF ADVANCED CRYOGENIC
PRESSURE SWITCHES FOR BALUSTIC MISSILES]
VOLUME III. by Ernest A. Lament. Rept. on
Contract AF 04(647)158. Mar 60, 253p. 7 refs.
[AFBMD] 60-%8-5; [AFBMD] Doc. no. A60-5488.
vd. 3; [AFBMD TR-60-85. v. 3] AD-243 568.
OnJer fromLC ml$11.10. ph$39.60 PB 154 289-3
Contents:
Speciflcatlon: Ballistic missile medium fluid pressure
switch
Demonstration and limits of operation test specifica-
tion - medium fluid pressure switch
Demonstration and limits of operation test report -
medium fluid pressure switch
Salt spray, shock and acceleration tests on Frebank
P/N 158-286 medium fluid pressure switch, to
Prebank specification RkD 158-16
158-286 medium pressure switch and all details
Specification - Ballistic missile low fluid pressure
switch
Dennonstration and limits of operation test report -
low fluid pressure switch
Acceleration, salt spray and shock test on Frebank
P/N 158-400 low fluid pressure switch, to Frebank
specification RkD 158-81
158-400 low fluid pressure switch and all details .
Lincoln Lab. . Mass. Inst, of Tech. , Lexington.
WEST FORD PRIMARY PRINT PROGRAM, by
J. D. Drlnan. Rept. on Contract AF 19(604)7400.
24 Jan 61, lip. 21G-0024: AD-250 958.
Order from LC mi$2. 4a ph$3. 30 PB 154 588
Antenna position information and other Interesting data
will be recorded on magnetic tapes In IBM format at
each of the West Ford sites. These dau will permit
all interested persons to obtain a general idea about
what happened on a particular test day. Additionally,
the data may afford insight into specific aspects of the
eotperiment such as belt formation, belt growth, belt
deterioration, etc The Primary Print program was
designed to assist in the implementation of the West
Ford experiment by affording a detailed printout of the
site-produced binary magnetic tape. The amount of
output and the items to be printed are governed by a
variety of sets of control parameters. (Author)
Naval Ordnance Lab. , White Oak, Md.
TIC DYNAMIC COMPRESSIBILITY OF SOLIDS
FROM SINGLE EXPERIMENTS USING UGHT RE-
FLECTION TECHNIQUES, by N. L. Colebum.
31 Oa 60, 35p. 11 refs. NAVWEPS rept. 6026.
Order from OTS $1 . 00 PB 171 686
An experimental technique has been developed to
determine in a single experiment the dynamic com-
presslbihty of a solid over a relatively large pressure
rai^. The method consists of observing with a ro-
tatlng-mlrror smear camera, the behavior of the free
surface of a wedge of the test material shortly after
the opposite wedge surface has been struck by a plane,
explosive-driven shock wave. Reflected light, shock
luminescence, and the spallation of plastic films from
shocked wedge surfaces are employed. Using ooe-
dlmenslonal geometry, shock and free -surface veloci-
ties are measured as a function of a wedge thickness.
The dau are treated with the pertinem hydrodynamlc
equations to obtain the compressibility curve. The
results al measurements on the compression of
aluminum and Plexlglas in the pressure region of 70
to 300 kil(43ars are presented. (Author)
Naval Ordnance Lab. , White Oak, Md.
THE SPHERICAL TAYLOR WAVE FOR THE GAS-
EOUS PRODUCTS OF SOLID EXPLOSIVES, by
Morton Lutzky. 19 May 60, 32p. 4 refs. NAVWEPS
rept. 6848.
Order from LC ml$3. 00, ph$6. 30 PB 154 578
The results of nnachine computations of the Taylor
Wave for the gaseous products of various spherical,
solid explosives are presented. The explosives con-
sidered include TNT, pentolite. cyclotol 65/35, cyclo-
tol 60/40. TNETB, RDX, tetrjd, and nitroguanidine.
The compuutions were based on the equation of state
E ' PV/y-1 for the explosion products. Numerical dau
are given that may be used as initial dau in a calcula-
tion of the effects of the detonation of a spherical ex-
plosive charge on the surrounding fluid. Results of a
calculation designed to check the energy balance are
presented, in which the heat of detonation calculated
from the dau is compared with the accepted heat of
detonation calculated by means of the Brlnkley-Wilson
mechanism. A description of the machine program is
also given, so that similar compuutions may be made
for any arbitrary explosive. (Author)
Naval Ordpance Ttest Station. China Lake, Calif.
A COVOLUME EQUATION OF STATE OF GASES AT
DETONATION CONDITIONS, by P. A. Longwell.
Sep 60. 19p. 8 refs. NOTS TP 2535; NAVWEPS rept.
7565; AD-248 367.
Order from LC mi$2. 40, ph$3. 30 PB 153 730
Molal covolumes, activity coefficients, and the In-
crease In internal energy due to gas imperfection have
been calculated from available theoretical equaticm of
sute dau and tabulated on a reduced basis. The range
of temperature and pressure covered Is that en-
countered in the detonation of condensed explosives.
(Author)
Naval Ordnance Test Sutkn, China Lake. Caltf.
SHAFT- ANGLE DIGITIZING AND RECORDING SYS-
TEM, by E. Nadalln. 1 Nov 60, 65p. NOTS TP2567;
AD-248 071.
Order from LC ml $3. 90, ph$10. 80 PB 153 647
A system is reported for recording simultaneously in
digiul form the range, azimuth, and elevation pa-
rameters of urget position in relation to radar posi-
tion together with range timing, on magnetic upe in
an IBM- 709 upe format. The parameters are digi-
tized by means of shaft -angle encoders. This dau is
stored In a magnetic -core memory by means of tran-
sistorized logic circuitry and then shifted onto mag-
netic upe. The dau is now In a format for direct en-
try Into the IBM- 709 computer. (Author)
739
[Naval WeaportB Lab. ] Dahlgren, Va.
PROCEEDINGS OF THE U. S. NAVY SYMPOSIUM OH
AEROBALUSnCS (NO. 4] SPONSORED BY THE
BUREAU OF ORDNANCE, THE DEPARTMENT OF
COMMERCE AUDrrORIUM, WASHINGTON, D. C,
12-14 NOVEMBfiR 1957. VOLUME I. 1 May 58, 297p.
75 refs. NAVOtD rept. no. 5904; NPG repi. mo. 1599;
AD- 201 225.
Order from LC inl)l 1.10. ph$45. 60 FB 155 296
This report released for sale to the public 31 Mar 61.
North American Aviation, Inc. [Downey, Calif.)
SPRING MATERIALS: HIGH-AND LOW-TEMPERA-
TURE APPLICATIONS. 16 Sep 57, 254p. 265 refs.
AL-2606; AD-14p 811.
Order from LC ini$ll. 10, ph$39.60 PB 155 148
This report reletased for sale to the puMic 29
6i.
Wire materials which consisted of ferrous, nonferrous.
and special alloys were selected for evaluation with re-
spect to limited ^se from -40° to 300*^ and from -40°
to 800°F for application in the design of special valve
springs; high- apd low-temperature tensile properties
were determined The materials evaluated were music
wire, type 302 stainless steel, Ni Span C. 17-7PH and
17-4PH steels. 9e-Cu (alloy 25), Caroga (AISl 6152).
A-286. Thermokl J, and Inconel X (15% cold reduced).
Results showed that 17-7PH and Thermold J wire mate-
rial were superiior with respect to ultimate strength
and yield stress <0. 2% offset). The tensile proportional
limit stress values for tests conducted at high and low
temperatures w^e too scattered to draw conclusions
for design use. |A sample consisting of at least S spec-
imens would be inore satisfactory to determine propor
tional limit. Fof spring design, where proportional
limit and modulus of elasticity become important.
Armco 17-4PH wpre a^wed superior properties. At
room temperatuie. 165°, 300°. and 800°F. the pro-
portional limit stress for 17-4PH was above those of
the other materisls. An average modulus of elasticity
value was deteri^ned as 30. 200. 00° psl at room tem-
perature and 26.1800, 000 psi at 800OF.
[Office of Defer ise Research and Engineering,
Washington, D.| C. )
PROCEEDINGS (j>F THE STATISTICAL TECHNIQUES
IN MISSILE EVALUATION SYMPOSIUM HELD AT
THE VIRGINIA |<DLYTECHNIC INST.. BU^CKSBURG.
VIRGINIA ON 5H8 AUGUST 1958, ed. by Boyd Harsh-
barger. [I958)2fc6p. 103 refs. AD- 209 620.
Order from LC iiii$l 1 . 10, ph$41 . 10 PB 155 145
This report relei sed for sale to the pubUc 29 Mar 61 .
Contents:
Sessions 1 and 2
Session 3.
Session 4.
statistics
Sessions 5 and 6 _
Session 7. Teler^etry, trajectories
[H'ocesses.
System component reliability
Life tiesting
Non-j^rametric methods and order
Design and analysis of experiments
and stochastic
REF Mfg Corp , Mineola, N. Y.
ELECTRIC POWERED AND SOLAR POWERED FOOD
WARMING UNFTS FOR SPACE VEHICLES, by Mortos
H. Rochman. Herbert S. Siegel, and Robert A Landes.
Rept. on Equipment for Life Support in Flight Opera-
tions. Contraas AF 33(616)6199 and AF 33(616)6909.
Dec 60. 6lp. 19 refs. WADC Technical rept. 60-620.
Order from OTS$ 1.75 PB 171 605
Two general classes of food warming methods for use
aboard a space vehicle were studied; one class using
electrical energy, the other using direct thermal
energy. Electrical hating method investigated were
electromagnetic, ultrasonic energy electrically-pro-
duced, and electrical resistance; direct thermal
energy sources evaluated were nuclear, solar, chemi-
cal, and a heat pump system. Electrical resistance
heating, utilizing direct Bonductanoe to transfer heat
to the food, was considered the most feasible of the
electrical methods, and solar heat -sink the most
feasible of the direct thermal methods . Each preferred
method appeared to be the most compaa, reliable,
economical, and safe in relation to the energy source
employed. The development and final design features
of an electric powered food warmer and a solar
powered food warmer are covered in Part II.
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus. Ohio.
SUMM^JIY OF PRESENT INFORMATION ON IM-
PACT SENSITIVITY OF TTTANIUM WHEN EX-
POSED TO VARIOUS OXIDIZERS, by W. K. Boyd.
(Rept. on Contract AF 33(616)(7747] 6 Mar 61, 9p.
3 refs. DM IC memo. 89.
Order from OTS $0. 50 PB 161 239
This review summarizes the present status of the
compatibility of titanium with LOX (liquid oxygen) and
with other oxidizers such as N20^, Fj. and QF«.
Considerable experimental evidence has been ob-
tained which indicates that, under certain conditions
at impact, titanium and its alloys may ignite in strong
oxidizers at the type used in rocket and missile pro-
pulsion systems. However, only in the case of LOX
does there appear to be danger that the reaction will
propagate and completely consume the titanium. In
most cases, even though ignition occurs, the damage
is not significantly greater than that occurring as a
result of the impact alone. The data also suggest that
the chance for a reaction can be minimized if the ti-
tanium surface in contact with the oxidizer is smooth
and surgically clean. In spite of its impact sensitivity,
titanium appears to have some areas of application
where it can be used in contact with such strong oxi-
dizers as LOX. fluorine. N2O.. C10»F, and H-O,.
(Author)
Rocketdyne [Canoga Park. Calif.]
DESIGN, DEVELOPMENT, AND TESTING OF AD-
VANCED HELIUM PRESSURE REGULATOR PART
NO. 551302. VOLUME 1, byR. L. Kenyon. Rept. on
ContraCT AF 04(647)160, July 60, 263p. R-2356; Doc.
no. 60-6186. vol. 1; AFBMD-TR-60-74; AD-242 962.
Order from LC mi$ll. 10. ph$41. 10 PB 154 290-1
740
The ability of the 551302 regulator to meet the re-
quirements of the model specification was demon-
gtrated by the successful completion of the Perform -
»Dce. FUght Rating, and Qualification Tests. The in-
ability to effeaively damp the controller sensor led to
die development of a vibration -tolerant pilot valve to
mlninuze the errors introduced into the controller by
environmental random" and sine wave vibration. The
bleed regulator vibration error was minimized by a
metal -to -metal coulomb Action damper to simulate
tbe damping usually obtained from O-rings and sliding
teals in conventional designs. Meul-to-meul cou-
lomb friction damping was also effectively adapted to
die piloted inlet valve. The extreme ambient and gas
temperature range forced the use of metal -to- metal
fstve seats, which proved thoroughly reliable under
ail conditions tested. Temperature compensation over
a SOO^F range was achieved with an adjustable com-
pensator utilizing the difference in the coefficients of
linear expansion of two materials. Compensation for
farces exerted on tbe controller sensor due to accel-
eration was successfully achieved using a counter -
weighted beam. Pressure energized seals with seal
farces that vary in inverse proportion to the applied
pressure to provide sufficient force to seal at low
pressures and to prevent destructive loading at high
pressures were designed. A packing type seal was
also developed for low [iressures to seal the regulator
adjusting screw and at the same time permit freedom
of adjustment. (Author) (See also PB 153 612)
Rocketdyne [Canoga Park. Cahf. 1
DESIGN. DEVELOPMENT, AND TESTING OT AD-
VANCED HELIUM PRESSURE REGULATOR PART
NO. 551302. VOLUME 2. Rept. on Contract
AF 04(647)160. July 60, 551p. R-2356 (includes
R- 1962-1); Doc. no. 60-6186. vol. 2; AFBMD-TR-
60-74; AD-242 963.
Order from LC mi$ll.lO, ph$84.90 PB 154 290-2
Complete detail and assembly drawings of tbe oompo-
nent are reproduced. The original test data taken
during the Performance,. Flight Rating, and Qualifica-
tion Tests are reproduced, and test setup schematics
and photos are included. Specifications defining the
component requirements, assembly and service pro-
cedures, and official tests performed are also
presented. (Author) (See also PB 154 290-1)
Vitro Engineering Co. [Washii^on, D. C ]
MEASUREMENT AND TELEMETRY SYSTEMS FOR
MISSILES Rept. on Contract DA 30-069 -ORD- 2331.
20Oa59. 96p. 11 refs. Vitro-2331-2-59; AD-232098.
Order from LC mi$5. 40, ph$15. 30 PB 153 890
This report released for sale to the public 28 Mar 61.
This document is intended to familiarize personnel
both at ABMA and throughout the missile industry with
recent efforts being made by ABMA in themeasure-
ment and telemetry field. It describes'measurement
and telemetry systems developed in accordance with
ABMA's philosophy of flexibility, which contemplates
continuing improvements in adaptability, accuracy,
and compactness. A brief historical background of
Mme phases of the effort is included to highlight the
major advances in recent years. The complete
systems from sensing device to telemetry sigiul
transmission are discussed, including their use in
measuring and monitoring the many variables in-
volved in the flights of missiles, satellites, and other
payloads. Environmental, propulsion, attitude and
trajectory, flight sequence and other types of
measurements are included. Also, future trends in
telemetry, necessary to accommodate the increasing
complexity of missile systems, are briefly described.
(Author)
Watertown Arsenal Labs. . Mass.
NONDESTRUCTIVE TESTING. AN INVESTIGATION
OF SIGNALS FROM THE MAGNETIC FLAW DETEC
TOR FOR GUN TUBES, by R D. Kodis. Rept. on
Cannon Tubes. Progressive Stress Damage In.
15 Jan 51. 3lp. Rept. no. WAL 732/114-3.
Order from LC mi$3. 00. ph$6. 30 PB 155 059
This report released for sale to the public 31 Mar 61.
Thin-walled tubes were examined, using the flaw de-
tector developed at Watertown Arsenal, at selected
times during the life of the tube. The tubes were hy-
droatatically fatigued until failure occurred by crack-
ing through the wall. A study was made to find any in-
dication on the records of the tubes, prior to fatiguing,
which would correlate with the point of failure caused
by the fatiguing operation. One tube was examined in
detail by other methods: X-ray, magnetic particle test,
and by sectioning to measure crack depth. Another
tvte was plastically deforme^d by cold-bending and
straightening. It was then tested magnetically to
demonstrate the sensitivity of the method to local
stress concentrations induced in the above manner. A
section of one tube was studied by metallograpiiic
techniques. (Author) (See also PB 155 058)
Watertown Arsenal Labs. , Mass.
NONDESTRUCTIVE TESHNG. INDUSTRIAL EVALU-
ATION AND OPERATION OF THE CRACK DETEC-
TOR FOR TUBES MODEL II, by George Darcy, Jr.
Final rept. on Cannon Tubes, Progressive Stress
Damage In. 1 June 51 33p. Rept. no. WAL-732/114-7
Order from LC mi$3.00, ph$6. 30 PB 155 061
TWs report released few sale to the public 31 Mar 61 .
The Automatic Crack Detector for Tubes, Model II,
was used to examine a number of tnrifled gun tubes
being manufactured at Watertown Arsenal., The results
of the Automatic Crack Detector are compered to the
results of the horoscope inspection. Operational
instructions and shop procedure for use of the instru-
ment are given. Instructions with regard to the
evaluation of records produced from tubes are
(M-ovided. (Author) (See also PB 155 060)
Watertown Arsenal Labs. , Maes.
NONDESTRUCTIVE TESTING. CRACK DEPTH
MEASUREMENT IN POWDER CHAMBERS IN CAN-
NON, by C. H. Hastings, G. A. Darcy and P. C.
McEleney. Rept. on Metal Testing Methods. I July 53,
26p. Rept. no. WAL 732/123.
Order from LC mi$2. 70, ph$4. 80 FB 155 062
This report released for sale to the pubhc 3! Mar 61.
741
A nondestructive tnagnetic teat method and inatrumen-
ution for the stud^ of progreasive streas cracka in
155 mm howitzer powder chambers are described.
Studies of typical chambers are also described, as
performed, using the magnetic test equipment and
visual examination A calibration of the magnetic test
equipment for crack depth determJnation is presented
and discussed in Comparison with visual and pullover
gauge techniques for evaluating the status at 155 mm
howitzer tube life, (Author) (See also PB 155 061)
Watertown Araetal Labs. , Mass.
NONECSTRUCriVE TESTING. THE APPLICATION
OF THE INDUCTION METHOD OF CRACK CCTEC-
TION TO RIFLED TUBES, by R. D. Kodis. Rept. on
Cannon Tubes, Prtogresalve Stress Damage In.
12 Feb 51, I3p. |ept. no. WAL-732/114-5.
Order from LCn$$2. 40, ph$3. 30 PB 155 060
This report released for sale to the public 31 Mar 61 .
Sections ot rifled lubes, some having cracks in the
rifling and some ♦hich were crack-free, were exam-
ined by the magnetic induction technique developed at
Watertown Arsenal. Records obtained from these ex-
aminations were compared with sections cut from the
defective tubes. The applicability of the magnetic
method used is discussieid with regard to correlation
with the cut seaions. (Author) (See also PB 155 059)
rseiial
Watertown Arsehal Labs. , Mass.
NONDESTRUCTIVE TESTING. THE DEVELCTMENT
OF A FLAW DETECTOR FOR THE BORE SURFACE
OF GUN TUBES, by Carlton H. Hastings. 14 Aug 46,
26p. 1 ref. Expefimenul rept. no. WAL 732/114-1.
Order from LC n1i$2.70. ph$4.80 PB 155 058
This report relea^ for sale to the public 31 Mar 61 .
After due consideratiOD of existing inspection tests, a
principle new to tjie field of flaw detection has been
assayed with regard to possible utilization for the in-
spection of the bore surfaces of gun tubes. This
principle, concerning the behavior of a ferrous cored
coil under the influence of combined A.C and D.C.
magnetic fields, las been used successfully in the
laboratory for bofe inspection. An instrument has
been developed which is considered to be applicable to
production inspection on a wartime scale. Plans for
evaluating the instrument by comparison with the op«i-
cal borescope as fin inspection tool are being
completed. (Author)
Watervliet Arsetial, N. Y.
A NEW APPROACH TO THE AUTOPRETTAGE OF
HIGH STRENGTH GUN TUBES. Rept. on Cold Work
o€ Gun Barrels. Apr 59, 75p. 7 refs.
Order from LC nkU 50, ph*12. 30 PB 154 207
I
This report released for sale to the public 28 Mar 61.
The usual methodi of autof rettage for gun tubes utilizes
hydraulic pressuile applied directly to the bore in
order to plastically deform the wall of the tube in such
a nuumer as to pioduce favorable residual stress pat-
terns. An alternt te method of autof rettage requiring
reduced hydrostatic pressure is developed and de-
scribed. This method consists of passing an oversize
mandrel through the tube to plastically deform the
walls of the tube. All specimens were made from a
modified 4340 steel, and heat treated to the various
strengths involved.
Sanitation and Safety Engineering
Industrial Test Lab. , Philadelphia Naval Shipyard,
Pa.
COMBUSTION HAZARDS RESULTING FROM SHIP-
BOARD FIRES, by M. S. Gabls and M. Anmuth.
Sep 58, 20p. 3 refs. Development repc. no. A211S:
AD- 203 696.
Order from LC ml$2. 40. ph$3. 30 PB 155 250
This report released for sale to the public 31 Mar 61.
In connection with the proposed use cd a high impact,
rigid, polyvinyl chloride plastic pipe aboard ship an
evaluation has been made of the comtxistion hazards
resulting from shipboard fires. Tests were conduaed
to simulate shipboard fires involving. In one case, the
conventional materials usually found in a typical berth-
ing space and in another, the conventional materials
plus lengths of the plastic pipe. Gas analyses of the
resultant fumes and aninuil exposure tests were per-
formed. The results al test show that the conventional
materials emit fumes which are toxic to test animals
and that the addition of plastic pipe does not introduce
new toxic hazards; also the use oif the pipe does not
aggravate the toxic gas hazards which already exist in
the event o* a fire aboard ship. (Author)
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
BUILDING PROTECTION AGAINST BIOLOGICAL
WARFARE ATTACK, by Warren Viessman and E. N.
Hellberg. Interim memo. 1 Feb 52, 23p. 6 refs.
Technical memo. M-035.
Order from LC ml|2 . 70 . ph$4 . 80 PB 1 54 622
Since results of tests conducted on a small temporary
shelter indicated that it is practical to protect build-
ings from bacteriological and chemical attack by pres-
surizing the interiors with filtered air to jjrovide exfil
traiion of air at all leakage points , plans have been
formulated to evaluate the efficiency of BW and CW
protective measures as applied to larger semiperma-
nent buildings . A suitable frame building has been se-
lected and nfKxlification and instrumentation have
commenced.
Naval Civil Engineering Lab. , Port Hueneme, Calif.
FORMALDEHYDE AS A POSSIBLE COMPONENT IN
CATCHMENT WATER FROM ASPHALT RUNWAYS,
by G. E. Sanford and R. L. Alumbaugh. 11 Jan 52,
I5p. 16 refs. Technical note N-070.
Order from LC mi$2.40, ph$3.30 PB 154 642
The current study reviews important aspects in the
toBiicology ai formaldehyde. A method for the investi-
gation d formaldehyde in the field has been checked,
and evidence indicates that it can be adapted to such
742
use. Preliminary studies on the removal of formalde-
hyde from water show tn general terms the feasibility
of removal ci formaldehyde on a large scale when and
tf desirable. It is concluded that water containing up to
and including 5 ppm al formaldehyde will not be
rijected on the basis at taste or odor, in the absence
of objectionable residual chlorine. (Author)
Nival Ovil Engineering Lab. , Part Hueneme, Calif.
PORMALC«HYDE DISPERSAL, by R M. Domldson.
31 July 53, declassified. 13p. 9 refs. Technical noce
N-157.
Oitler from LC mi$2. 40, ph|3. 30 PB 154 655
A study was made of both chemical and physical
■MM of dispensing formaldehyde for interior disin-
iMloa. A commerciaUy available insecticide sprayer
(Mlcrosol Fog Generator (Model 202) was studied for
Its ability to spray formaldehyde. Preliminary studies
indicate that the oommercial model can be adapted to
Naval 9K>re Establishment use and readily adapted to
spray directly from five-gallon storage cans. Chemi-
cal methods were studied for ease and safety.
Methods which involve the use or possible use of
standard Navy stock chemicals were screened for
possible utilization. (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
PACKAGING OF FORMALDEHYDE FOR DECON-
TAMINATION, by A. L. Fons. 13 Nov 53. declassi-
fied. 9p. 2 refs. Technical note N- 160.
Order from LC mill . 80, phjl .80 PB 154 657
A Kudy was made of the important factors in packaging
and shipping of 405^ aqueous formaldehyde solutions.
The results of this study constituted the basis of for-
mulation of minimal sundards for packaging and
shipping specifications of such solutions. (Author)
Ni?al Civil Engineering Lab. , Port Hueneme. Calif
PROTECTION OF BUILDINGS AGAINST BIOLOGI-
CAL WARFARE, by Warren Viessman, E. N. Hell-
berg, and a M. Whlppo, Jr. 10 Dec 53. 68p. 19 refs.
Technical memo. M-074.
CWer from LC mi$3. 90. ph$10. 80 PB 154 627
A protective shelter was pressurized by the Labora-
tory. Attacks using BW simulants were made against
the building and evaluated. The data indicate that a
pressure of 0. 1 in. of water will give adequate pro-
tection. It is recommended that further tests be con-
tacted to confirm this fact. Investigations have pro-
Aiced a group of sealing materials which can be ap-
plied easily to the Inside of structures for protection
against infiltration of contaminants and for
(Rvssurization.
Nival Civil Engineering Lab. . Port Hueneme, Calif.
RADIOLOGICAL TEST OF DECONTAMINATION
SIOWER WASTE WATER REaRCULATION, by
W. R. Nehlsen. 4 Oct 56. 9p. Technical note N-281.
Order from LC mi$l. 80. ph$l. 80 PB 154 675
This project requires the development of a portable
arctic d«x>ntamlnation shower unit incorporating a
waste water treatment and recirculation system. An
experimental unit was devised using sedimentation and
chlorination as a basis of waste treatment. This sys-
tem was recently tested with a radioactive fallout
simulant. Results indicated that over 99 per cent of
the simulant was removed from the waste water and
was deposited in the shower sump and waste treatment
tank. It is concluded that a waste water treatment and
recirculation system should be included In the unit
design. (Author)
Naval Civil Engineering Lab. , Pcmi Hueneme, Calif.
REVIEW OF ECCONTAMlNA-nCW SHOWER UNIT
TESTS AND PLANS, by W. R. Nehlsen. 13 Mar 57.
13p. 3 refs. Technical note N-297.
Order from LC mi|2. 40. ph$3. 30 PB 154 677
An attempt has been made to develop a portaMe arctic
decontaminaticm shower unit in corporating a waste
water treatment and a recirculation system. An ex-
perlmenul unit was devised using sedimenution and
chlorination as a basis of the waste treatment. This
system was tested with a biological warfare simulant
and a radioactive fall out simulant with favorable re-
sults. No testing was done with chemical warfare
simulants but technical information was recelvedfrom
the Army Chemical Warfare Laboratory which indi-
cates tiiat this simple wane treatment scheme was not
adequate for chemical warfare use. In this interim
report the test data and the technical iirformation are
summarized and problems associated with various
applications are discussed. (Author)
Naval Civil Engineering Lab. . Von Hueneme. Calif. "
SHELTER HABIT ABILITY STUDIES: THE EFFECT
OF ODOR IN A SHELTER AND VENTILATION RE-
QUIREMENTS, by James S. Muraoka. 22 Nov 60, 20p.
26 refs. Technical note N-354.
Order from LC mi$2. 40. pl43. 30 PB 154 669
Inside closed rooms, tobacco smoke and body odors
affect the health of occupants by causing a lessening of
food and water Intake, disturbing sleep, promoting
nausea and vomiting, and mental disturbance. TotMcco
smoke is much more offensive to man than noxious
body odors. The foul smoke and body odors are es-
pecially disturbing to individuals entering an already
occupied shelter from the outside. The number of
persons (smokers and non-smokers) occupying a shel-
ter and the fresh air supply are two Important factors
affecting the quality of the air. The outdoor air tem-
perature and humidity at the time of shelter occupancy
and the number of persons occupying a shelter will
influence the amount of fresh air supply needed to
maintain comfortable climatic conditions. The follow-
ing methods were found to be effective in reducing the
concentration of body odors and tobacco smoke in
closed rooms: fresh outdoor air supplied through a
simple ventilation system, recirculation of indoor air
through charcoal filters or through a spray-type de-
humidifier, use of deodorants, and increasing the
temperature and humidity of a room. (Author)
743
Naval Ovil Engineering Lab. . Port Hueneme. Caltf.
VENTILATION SYSTEM PROTECTION AGAINST
BW AEROSOLS, by W. R. Nchlsen. 27 >jne 56, lOp.
Technical note M-277.
Order from LC itii$l. 80. ph$l. 80 PB 154 674
Since many buildings are equipped with air-handling
and filtering equipment that may offer some degree d
BW defense, ventilation air filters and air-supply sys-
tem components have been tested with O- to 5- micron-
size dust. DOP smoke, and a BW slmuUnt organism to
assess the protection available against BW aerosols.
Results show thai a high percentage a€ particles below
three microns in diameter will penetrate anair-con-
ditionii^ system equipped with panel -type ventilation
air filters. During a one-hour BW aerosol test on a
test shelter, ani)-per cent penetration of the air-con-
dltlonlr^ system) was experienced, but the aerosol
concentration ingide the shelter only reached a level
of about 50 per Oent of the outside concentration be-
cause of recircjation and dilution. This degree d
protection is too low to be of much practical value for
BW defense. The dust test results are valuable for
providing information for the application of panel -type
ventilation filter^ as prefilters for collective pro-
tectors. (Authof)
Office d Tech»ical Services. DepC. of Commerce.
Washington. C| C . .^
AIR POLLUTlOfJ AND PURIFICATION. Feb 61. lOp.
123 refs. OTS Selective Bibliography SB- 448.
Order from OTf JO. 10 OTS SB-448
A bibliography if reports listed in the two OTS monthly
abstract journals: U. S. Government Research Re-
ports and Technical Translations. This is a selective
listing of reports dealing with air pollution by non-
radioactive fumps, industrial gases, smokes aero-
sols, etc. Oio^ical warfare agents were excluded.
Ship Building
Bureau of Shida, Washington, D. C.
HULL IMPEDANCE AND NOISE REDUCTION, by
D. W. Saltus jlesearch and development rept.
1 Jan 58, I2p. Repi. no. 375-N-29; AD-158 023.
Order from LC|mi$2. 40. ph$3. 30 PB 155 413
This report released for sale to the public 10 Apr 61.
This report discusses the concept of mechanical imped-
ance and demoristrates the manner in which the con-
cept can be applied to the problem of reducing radi-
ated noise from submarine machinery Considerable
attention is gjvtn to the basic analogy between elec-
trical and meclianical impedance, and the overside
noise level due to a small fan la computed as an ex-
ample of the method. The example choaen is simple
enough that the 'basic principles of the method are no»
obscured by details. The full complexity of the gen-
eral problem ii indicated in the concluding sections of
the report whei e a description of the problems still to
be solved may » found. The advantages anticipated
in the future arte also discussed. (Author)
Bureau of Ships, Washington, D. C.
SHOP PRACTICE SUGGESHONS NO. 3. May 60, 29p.
Order from OTS $0. 50 PB 171 251
Suggestions included are: salt spray fog test; fuel oil
burner lead gaskets; mobile welding unit; weld spaner;
steam chest repairs; water closet plug valves; coating
audigage crystals; fork -truck platforms; colored label
plates; hijfh temperatxire alarm switches; cable instal-
lation dau; propeller ahaft coupling dutchman; Tran-
slte pipe for electric heat-treating; improved method
of cleaning bolter tube holes; scrap rivet sack; lateral
stiffening; portable overhead hook; masking valve hand
wheels; AN/GRC-27 contact pins; reconditioning ab-
raaive-vaJve body; lighting calculator; sea chest
valvea; lettering on plana; AU/WU-l radar transmit-
ter gear; AN/SPS-28 grid coonectiai; economizer
access doOT; catapult cylinder support brackets;
burner tile drain holea; ECM-mast cable conneaiona;
bulkhead stiffeners; degaussing- cable hangers; porta-
ble extension lights; thread- rechasing unit; butt-
welding aluminum; use of non-ferrous material on
diesel exhaust-terminals Shipalt-94K; gage for kick-
pipe and atuffing-tube installation; access trunk vent
spool: flush-type deck drain; extruding pipe branches;
pipe lagging method; vacuum testing of tanks; water-
tight test for welded Joliits; submarine flood-valvea;
removing galvanizing from cast -in straps; adjustable
stanchion tops; Teflon O- rings machined; layout
templates and transfer punch; pipe hangers; shaft roll-
ing machine; wiring color scheme; insulation and
shielding of joints; ring for economizer; superheater
outlet header drain; welding- nozzle cleaner; propul-
sion shafts machined in place; paint -baking oven; tur-
bine control-valve head; adjustable rule-target; W. T.
cover design: cable-banding tool and buckle; breakage
of non-icing windows; ribbon pipe-aealant; 5'754 firl«|
cams; salvage ot antenna connectors; main-deck wire-
ways; adjustable pressure base; scunle hinges; poly-
ethylene gasket-punch blocks; quad rings in Ueu of
"O" rings; submarine -battery cell handling; jig for
X-raying welds. (See also PB 171 024)
David Taylor Model Basin, Washington. D. C
A GUIDE FOR THE SELECTION AND APPLICATION
OF RESIUENT MOUNTINGS TO SHIPBOARD EQUIP-
MENT, REVISED, by Francis F. Vane. Feb 58, I59p.
17 refs. Rept. 880. _ ^^ ^,
Order from LC ml$7. 50, ph$24. 30 PB 155 253
This report released for sale to the public 31 Mar 61.
Contents:
Nature of the transmission of noise, shock, and
vibration
Information required for calculating natural frequencies
Calculation of natural frequencies of resillently
mounted equipment
Transmissibillty and isolation theory
Numerical examples
Experimental determination of moment of inertia with
a trifilar suspension
Report form for resiUent mounting charaaeristics
Derivation trf equations of motion and frequency forms-
las for a resillently mounted rigid assembly
Practical arrangements of inclined mountings
Beslgn work sheets for common cases of mountings
744
David Taylor Model Basin, Washington, D. C.
METALLURGICAL INVESTIGATION OF TITANIUM
ALLOYS FOR APPUCATION TO DEEP-DIVING
SUBilARINES, by A . R. Willner and V. E. Sullivan.
Progress rept. for 1 July 59-1 Oct 60. Dec 60, 50p.
17 refs. Rept. 1482; AD- 248 393.
Order from LC mi$3. 30, ph$7. 80 PB 153 707
To determine the practicability of titanium alloys for
M«as a submarine hull material, the mechanical
properties and notch- sensitivity of five iHgh-strength
tltaaium alloys and a commercially pure titanium
were evaluated. Of the high- strength titanium alloys
the MQ or MSM-821 alloy exhibited the least sensiti-
vity to rate of loading, and the greatest resistance to
fractures as determined by Charpy V-iwtch, drop-
weight, and explosion crack-starter tests . A tenu-
tive criterion for determining the nil-ductility transi-
tion temperature by the Charpy V-notch test has been
established. (Author)
Divid Taylor Model Basin. Washington, TX C.
RESISTANCE AND EHP OF A PLANING CATAMA
IAN AS PREDICTED PROM TESTS OF MODEL
«36, by Richard A. Cumming. Nov 60. 25p. 3 refs.
Icpt. 1478; AD- 248 148.
Order from LC mi|2. 70. ph$4. 80 PB 153 706
The powering characteristics for a catamaran - type
kull were determined. Wetted lengths, running trims,
•ad resistances were measured on the model for a
umber of speeds, displacements, and initial trims,
b addftion, the effect on performance of changes in
hull spacing, planing area, and spray rails was de-
termined. A test was also made with a step on the
roef of the tunnel. The results are presented in di-
nenstonless form and also in the form of EHP curves
lorTO-ft, 105. 400- lb boat. Dsta indicated that for
hull a wide spacing is of so advantage from a re-
point of view. The spray rails on the final
eorfiguration increased the drag slightly on the full-
itnd boat. The best configuration was not as gcxxlas
• good conventional planing hull, due to a large
nt of air drag. (Author)
Dsvid Taylor Model Basin. Washington. D. C.
RUDDER -EXCITED HULL VIBRATION OJ USS
FORREST SHERMAN (DO 931); (A PROBLEM IN
HYDROELASTICrrY)by R. T. McGoldrick. June 60,
49p. 33ref8. Rept. 1431; AD- 240 379.
C^der from LC mi$3. 30, ph$7. 80 PB 149 745
The vibration phenomenon on USS Forrest Sherman
(IX> 931) was quite unlike the usual cases of ship
vibration in that the hull was set into a three -noded
horizontal vibration whose frequency remained con-
Kant over a considerable range of speed. The Boston
Naval Shipyard traced this vibration to the twin rud-
ders and ehminated it by reversal of the rudder toe-
Ufle aening. No simple explanation of the pheiKxne-
■on waa apparent at the time of Its occurrence, but It
'P!**red that any mechanism producing such a condi-
tion would necessarily involve hydroelastic effects.
This problem falls within the spheres of interest of
hoifa the Hydroelastidty Panel of the Hydrodynamics
Committee and the Hydro- Struaure Vibration Panel of
the Hull Structure Committee. While officially the
projea waa handled under strictly naval jurisdiction,
these panels maintained an interest in its progress be-
cause of representation of the David Taylor Model
Basin in their memberships. The author explores
several conceivable explanatlona, and, while acknowl-
edging contary opinions, accounts for the phenomenon
as due to a sub- critical coiurol- surface flutter condi-
tion. (Author)
Naval Civil Engineering Lab. , Port Hueneme. Calif.
ACCELERATED TESTING OF WATER LEVEL AND
I»AFT INEMCATORS, by D. B. Wright. 3 Jan 55. 40p.
4 refs. Technical note 212.
Order from LC ml$3. 00, ph$6. 30 PB 154 664
Numerous reports and complaints frcrni field activities
indicate a general unreliability in the performance of
the water-level draft indlcatora on floating drydocks.
The currrait phase of the investigation is the systems -
test phase and involvea five commercially available
water-level-systems and one commercially available
telemetering aystem. Subsequent to an extensive re-
view of manufacturers literature atxl recommendations
of field represenutives concerning the various pro-
ducta, these systems were chosen as those which most
nearly fulfilled the requirements. Of those systems
tested, one is recommended for nxxUfication and in-
service testing on an active dock. Further investiga-
tion is recommended for one other system and a de-
velopment program for obtaining a transducer element
for the telemetering system. (Author)
Naval Qvll Engineering Lab . , Port Hueneme , Calif .
CATHODIC PROTECTION APPUED TO THE AFDL-
12, LONG BEACH, by W. A. Bowen, Jr. 15 Nov 51,
41p. 11 refs. Technical note TN-060.
Orxler fromLCml$3.30, ph(7.80 FB 154 640
Cathodic protection was applied to the underwater hull
of the AFDL-I2. a floating dry dock, on 3 November
1950. Its state has been continuously monitored with
semiweekly surveys . A six months' study shows that
protection can be achieved with a single properly
placed anode and as little as eight amperes or thirty-
five wans of electrical power .
Naval Civil Engineering Lab. , Pon Hueneme. Calif.
DECK LAUNCHING TESTS OF A 3x12 PONTOON
WARPING TUG, by R. C. Towne. 6 Mar 57, 29p.
2 refs. Technical memo. M-123.
Order from LC mi$2.70, pJi*4.80 PB 154 616
To determine the feasitnlity of deck launching a fully
rigged pontoon warping tug from the deck of an LST,
tests were conducted from 15- , 20-, and 25-ft
heights . Successful launchings were made from
heights up to 20 ft in calm water; the effect of waves
or rolling of the LST on the launching could not be de-
termined in these tests . A launching height of 25 ft
was determined unsatisfactory. (Author)
745
Naval avtl Enfineerlng Lab. , Port Hueneme. Calif.
ERECTION AND TEST OF 100-TON CAPACITY
FLOATING CRANE, by J. J. Hromadlk and
R. C. Towne, 14 Jan 54, 35p. Technical note N- 175.
Order from LC ^$3.00, pti$6.30 PB 154 660
fnlj
Naval Civil Englpeering Lab. , Port Hueneme, Calif.
EVALUATION OF A SWP MOTION METER FOR
MOOREO VESSELS, by J. T. O'Brien, R. E. Jones,
•ad 0.1. Kucheareuther. Rept. on Response of Ships
to Waves . 19 Fefc 57. 48p. 2 refs . Technical note 292
Onler from LC fni$3.30, ph$7.80 PB 154 676
The Ship Motion IMeter was operated to measure the
forced motion of a 4x2 NL pontoon barge. The motion
measured by the Meter is contrasted with that ob-
tained using conventional surveying techniques . It is
indicated that thf surge-sway pickup Is accurate to
0.3 foot anywhere within Its range. For a particular
case where the tidal range and normal distance from
the instrument t© ship's hull is 4 feet, a surge of
approximately lO feet and sway erf 4 feet can be meas-
ured . Both roll and pitch pickup* are found to be
satisfactory in that they are accurate to 1/4 degree in
5 degrees and the yaw pickup unsatisfactory in that its
accuracy is only 3 degrees in 5 degrees . Results o<
studies to obtain* yaw by use of two surge-sway pick-
up* are presented and such a method declared satis-
factory. It is concluded that the Meter, where two
surge-sway pickup* are used to measure yaw, is
satisfactory although not nearly the ultimate for fur-
ther work in obtaining prototype measurements .
Recommendations as to the design of a superior
Meter are preseKited. (Author)
Naval Civil Engineering Lab. , Port Hueneme. Calif.
PONTOON TIE-ROD YOKE, by F. N. LeDoux.
11 Aug 52. lOp. Technical note N-109.
Order from LCtnl$ 1.80. pb$ 1-80 FB 154 649
A test was mada of experimental type pontoon yokes .
A-14-X1 and AX-2. to determine the relative
strengths as compared with the sundard yoke, A-14.
The yokes were tested in tension and the load was
applied by A- 10 bolts in a manner corresponding to
their normal arfangement in a pontoon string.
Naval Civil En«neering Lab. . Pon Hueneme, Calif.
TESTS OF BUSWIPS ANCHORS DM MUD AND SAND
BOTTOMS, by Ri C Towne and J. V. Stalcup.
5 Ak« 54, 54p. 1 ref. Technical note N-195.
Order from LC mi|3. 60. ph$9. 30 PB 154 662
The purpose of (he tests was to provide comparative
holding power data of several Lightweight and Navy
Stockless anchors presently being utilized by the
Bureau of Ships.
Naval Weapon*! Lab. . Dahlgren. Va.
EXPLOSION BULGE TESTS OF 2-1/2 " HY-80 STEEL
SUBMARINE BULKHEAD PLATES WELDED WITH
HEAT- TREATABLE AND NON- HEAT- TREATABLE
ELECTRODES, by W. H. Hall. Final rept. 20 Dec 60,
54p. 2 ref*. NWL rept. no 1726; AD-249 080.
Order from LC |ni$3. 90, ph$10. 80 PB 153 904
The MIL- El 1018 elecfrotJe. ofdlharily u*ed fn weld-
ing HY-80 steel, forms weW metal which is not heat-
treatable. Since the bulkheads, after forming, mu»t
be heat-treated (quenched and tempered) to required
propertle*, the problem was to obuin a weld which
would have as nearly as possible the same mechanical
properties as the plate material. From the results of
explosion bulge testing of the three groups of speci-
men*. It was concluded that the weldments produced
with heat-treatable electrode* were superior to those
made with non-heat- treauWe electrode* In the as -
heat-treated condition or in the replaced and untreated
condition.
Netherlands Ship Model Basin, Wageningen.
RESEARCH ON THE "NOZZLE ♦SCREW" PROPEL-
LER (DUCTED PROPELLERS). Final Technical rept.
for 1 Oct 59-30 Sep 60 on Contract DA 91-591-EUC-
1294. [1960] 30p. 4 refs. AD-249 192.
Order from LC mi$2. 70. ph$4. 80 PB 153 725
Research i* presented on a nozzle ♦screw propeller.
The effectiveness of a screws nozzle propeller (ducted
propeller) partly depends on the thrust of the nozzle,
which can be obtained. From this point of view a high-
lift nozzle profile might be reconunendable . Separa-
tion of the flow might occur at the leading inside pan
of the nozzle or in the diffusing part . A high loading
of the screw blades near the tip will prevent to a cer-
uin degree this separation of flow by boundary layer
control Systematic experimental test series were
carried out to study these phenomena . Three varia-
tions of the nozzle profile with four different radial
pitch distributions of the screw were tested in the
open water condition and in a cavitation tunnel with
uniform flow (Author)
FOOD, HANDLING. AND PACKAGING
EQUIPMENT
Food
Illinois U. Coll. (A Medicine [Chicago].
POSSIBLE CARaNOCXNIOTY OF IRRADIATED
FOODS, by Harry Monsen. Progress rept. for
15 Mar-15 Oct 59 on Contract DA 49-007-md-794.
[19591 5p.
Order from LC mill. 80, pW 1.80 PB 155 566
This report released for sale to the public 19 Apr 61.
Pennsylvania U. School of Medicine. Philadelphia.
EFFECT OF FOOD PRESERVED WITH IONIZING
RADIATION ON RESTORATION OF ENZYME
ACTIVITY AND TOTAL PROTEIN OF RAT LIVER,
by Otto Rosenthal and Vincent J. Pileggi. Progress
rept. no. 3. Sep 58-Mar 59 on Contract DA 49-007-
md-861. [1959) 14p. AD-218 570.
Order from LC ml$2. 40. ph$3. 30 PB 155 414
This report released for sale to the public 10 Apr 61.
Irradiated becf-cootainlng rations were fed to proteia-
depleted young adult male Wistar rats after partial
hepatectomy. The restoration of protein content and
746
tOJtat activity of the livers was studied. Tliree
types of beef were compared: (a) non- irradiated
fxoKa beef, (b) beef irradiated with 5. 6 megarad and
itored frozen, and (c) irradiated beef incubated 3 wk
in the unopened can and then refrozen. Groups of
rat* were sacrificed at the 8th and 14th postoperative
^. The following 4 liver enzymes were assayed at
ptrtlal hepatectomy and at sacrifice; cyanide -senai-
tive and cyanide -resistant alkaline phosphauses,
g|iicose-6-monopho8phatase and rhodanese. In the
group receiving heated irradiated beef for 12 days
the rate nf restoration of liver protein was 15% lower
than in the two other dietary groups. Experiments
tre in progress to study the effect <^t longer periods
of realimentation with heated Irradiated beef on
restoration of protein content and enzyme activity c(
tte liver after protein depletion and partial hepatec-
tomy. In addition to the two alkaline phosphatases
•■drbadanese. glutamic -oxalacetic acid trans-
aminase of the liver is being assayed. (Author)
MACHINERY, FABRICATION, AND
ACCESSORY EQUIPMENT
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
AN INVESTIGATION INTO THE USE OF CONDUC-
TING LUBRICANTS FOR THE REDUCTION OF
SHAFT-BEARING NOISE, by A. M. Intrator. Final
rept, 25 Apr 52. 16p. 3 refs . Technical note N-085.
OrderfromLCmi$2.4G, ph$3.30 PB 154 646
Radio Interference has been observed to originate in
the shaft-bearing area of some rotating machinery
•Dd was attributed to erratic discharge through the
shaft lubricant of the static charge developed between
the shaft and bearing. A laboratory test set up was
designed to study the effectiveness of various con-
ducting lubricants in reducing such Interference.
None of the lubricants tested offered a sufficiently
low inqwdance path for complete elimination of the
noise voltages , although the graphite grease mixtures
did lower the measureable noise somewhat.
Naval Civil Engineering Lab. . Pon Hueneme, Calif.
OPERATING INSTRUCTIONS FOR PILOT MODEL
RJMPING UNITS, by R. D. Kase. 5 Jan 51, 17p.
Technical note N-012.
0ninrfromLCmi$2.40, ph$3.30 PB 154 635
The pumping units are Peerless Pump Company volute-
type, single-stage, centrifugal pumps , mounted on a
ihd base with a Hercules Model JX40 gasoline power
uait. They are capable of furnishing 1000 gallons of
•ater per minute at a total dynamic head of 1 IS ft .
Thli rating is with a 15-fl suction lift. The pump la
cooaected to the power unit through a disc -clutch,
direct-drive power take-off. The power unit and
pump are enclosed in sheet-metal compenments with
*ccess doors provided for operation and maintenance,
•ad screw-type nnountlng bases for attachment of
•cceasorte* .
Engines and Propultion S)fst«mt
Aerojet -General Corp, , Azusa. Calif.
CHARGED- COLLOID PROTULSION SYSTEM, by
R. B. Edmonson. C. B. Kretschmer, and W. C. Miles.
Quanerly rept. no. 2. 1 Oct -31 Dec 60, on Contract
AF 49(638)656. Jan 61. 14p. Rept. no. 0290-01-2;
ARPA Order no. 6-58. Task 8; AFOSR-228.
Order from LC mi$2. 40. pti$3. 30 PB 154 454
This repon summarizes research on the electrostatic
spraying of microscopic droplets of oil. The research
is directed toward an understanding of the mechanisms
of charge accumulation and electrostatic spraying in
high electrical fields. The work during this period has
been directed primarily to the measurement of oU
droplet size, and to the design and construction of
equipment for the measurement of individual panicle
change-to-mass ratio. (Author)
Jet Propulsion Center, Purdue U. , Lafayette, Ind.
AN EXPERIMENTAL INVESTTCATION OF HIGH
FREQUENCY COMBUSTION PRESSURE OSCIL-
LATWNS IN A GASEOUS BIPROPELLANT ROCKET
MOTOR, by J. R. Osbom and R. M. Schlewe. Interim
rept. on Contract N7<»r 39418. June 58, 87p. 15 ref*.
Rept. no. 1-58-1; AD- 161 563.
Order from LC mlK 80. ph$13. 80 PB 155 149
This repon released for sale to the public 29 Mar 61.
An experimeittal investigation was concerned with the
initial phases of a research program for determining
the manner In which certain basic variables influence
the high frequency combustion pres*ureo*cillations In
a rocket motor. The investigation was conducted with
a gaseous bipropellant rocket motor which simplified
the experimental work by eliminating several variables
which enter Into the combustion proce**: atomization.
vaporization, mixing, etc. The cainbu*tlon pressure
oscillations observed had frequencies ranging from
550 to 1725 cycle* per second for a transverse mode.
The combustion pre**ure oscillations were measured
with a cathode ray oscillograph. The effects of com-
bustion chamber geometry, the nozzle configuration,
the heat -release rates of the propellants, the com-
bustion pressure, and the equivalence ratio upon the
combustion pressure oscillation* were Inveatigated.
(Author)
Marquardt Corp. . Van Nuys. Calif.
TESTS OF THE MARQUARDT SERIAL 5081 (TORY
II-A) HEAVY-DUTY ENGINE, by C. D. Hartman.
Rept. on Contract AF 33(616)6214. 22 Mar 60, 53p.
24 refs. MR 60-109.
Order from LC mi|3.60, ph$9.30 PB 155 383
This repon released for sale to the public 12 Apr 61.
A series of twelve runs was made, consisting of
twenty-one minutes of air time at airflows up to 520
pounds per second and nine minutes of burning time at
exit temperatures exceeding 3500°F, during which the
structural, aerodynamic and heat transfer perform-
ance of the engine was demonstrated. (Author)
747
KGcrotech Resaarch Oo. , Cambrl^Ke. Mast.
VAPOR CYCLE POWER PLAhfTS FOR LOW POWER
MOBa.E APPLICATIONS, by J. K. Sparrell, J. C
ClMto and others, Rept. on Contract DA 44-177-
tc-60L 31 Dec 59. 169p. 43 refs. Rept. no. 172.
Order from LC i^l|7. 80, ph$25. 80 PB 153 847
Optimum vapor c^cle power plants are selected for six
specific low power mobile applications. The study
subjects many working fluids to comparative cycle
analyses and establishes relative component equip-
ment sizes for the various cycles. The final selection
d the optimum q^les is based on several criteria
with Che emphasis being placed on overall nwight and
volume (including fuel required for the specified
mission). For e^ch at the specified applications the
working fluid for the optimum cycle is water. The
disadvantages of water as a working fluid (1. e. lubri-
cation and freezltig) are considered and preliminary
solutions to these problems are suggested. Each at
the specific applications considered are described and
the resultant vapor cycle power plants are briefly
summarized. In all applications except the 175 HP
truck, the optimum prime mover is a turbine. In the
case d the truck; the optlmim prime mover is a
double expanslot^ engine. The tabulated values for
weight, volume, and specific fuel consumption re-
sulting from this study are established for compara-
tive purposes only (1. e. the selection at optimum
cycles) and may be considered somewhat conserva-
tive (high). A detailed optimization involving the ac-
tual design al equipment, necessary to refine these
values, lies beyond the scope of this study. (Author)
Naval Civil Eng;ineent% Lab. , Port Hueneme. Calif.
COMPARISON or ARMY AND NAVY SPEQFICA-
TIONS WITH PARTICULAR REGARD TO IGNITION
INTERFERENCE, by A. M. Intrator. 29 Mar 51, 8p.
Techmcal note N»019. —
Order from LC mi) 1.80, pb$ 1.80 FB 154 637
nu$1.80.
PkMHMdyne Corp. . Santa Ana, Calif.
A PREUMINARt ENGINEERING EVALUATIC*! OF
ADVANCED SPACE PROPULSIC«M SYSTEM. VOL-
UME I; GENERALIZED PROPULSION SYSTEM
ANALYSIS AND MISSION RECJUIREMENTS, by Paul
S. Masaer. RuaaellJ. Page and Willis Stoner. Rept.
on Contraa AF 33(616)5709. 25 Mar 59, 60p. 51 refa
P-1FR039-5709; AFWADC-TR-59-l»9(I).
Order from LC ftii(3. 60, ph)9. 30 PB 155 345-1
This re^xjrt released for sale to the public 10 Apr 61.
A generalized prppulaion system analysis relates the
"optimum" speci|ic irapuiae to (1) the mission charac-
teriatic velocity, (2) available propulsion time, and
(3) the ratio ot pt^er source weight to Jet power, for
the cases of ane,{ three and an Infinite ruaaber at
round trips. Tba optimom specific impulse is found
to be mainly set by the ratio of propulsion time to
power source spflci/ic weight with less effect cauaed
by changes in cb^acteriatic velocity. The analysis
include* "off-optbnoin- specific Impulse performance
A iBilque method of presenting the results which is
particularly adapted to •t^^erpoaition of miaaioa re-
quirements haa bteii devised. Representative re-
quirements have been determined for several aatel-
Ilte, one Moon and one Mars missions to indicate
propulsion aystem choice. Emphasis was placed on
insuring the accuracy of compariaon of different
propulsion systems. (Authcs-)
Mcmufoctufing Equipfn*r>t and ProcassM
Applied Mathematics and Sutistics Labs. , Staitford
U. . Clalif.
STATISTICAL TOLERANCE LfMITS, by W. Grant
Ireson. Barnard E. Smith, and George J. Resnikoff
(DllDois hst. d. Tech. ). Tecfairfcal manual no. 1 on
Contract N6oar-25126. 18 May 60. 45p. 22 refs:
AD- 237 432
Order from LC mi$3. 30, ph$7. 80 PB 148 095
A study is presented to illustrate the application of a
statistical technique to the problem of setting speci-
fications to be held in the manufactureof an industrial
product. A means of directly determining ooe-slded
and two-sided tolerance limits is discussed «4ien the
characteristic under study is appraximately normally
distributed. A otie- sided upper limit Is such that the
probability isP that at least a proportion of the popu-
lation P Is less than the limit. A one-sided lower
limit is such that the probability- is P that at least a
proportian P of the population is gr^er than the
Ibnit. IVo-sided limits are a pair of limits such diat
the probability is P that at least a proportion P of the
papulation falls within the interval Included by the two
limits, if the population mean and the population
standard deviation were known tolerance, intervals
would be formed by adding to and subtracting from the
mean a ceruin multiple K of the standard deviation.
The factors K are determined in such a way that in a
large series of samples, a certain proportion T of
the resulting intervals will Include P or more of the
population.
Aviation Medical Acceleration Lab. , Naval Air
Development Center, )ohnsviIle, ?m..
AN ANALYSIS OF THE MAGNAFLUX INSFBCTDN
RECXmO OF WELDED pINTS ON THE 50- FT.
CENTRIFUGE, by Fred Ck>llub. Rept. no. 6 on ProJ.
MR 005. 15-0005. 6. 19 Oct 60, 13p. NADC-MA-6027.
Order from LC mi|2. 40, phf3. 30 PB 153 694
An approodmate local of 60 stnictural cracks weredit-
covered by seven magnaflux inspections from the
periods at Jine 1956 to July 1959 inclusive. The rea-
sons for these structural failures are discussed and
reoonunendations made for any future arm modifi-
cation. (Author)
Carnegie ln*t. of Tech. Graduate School of
Industrial Administration, Pittsburgh, Pa.
THE EFFECTS OF AN AUDIT (A STATEMENT OF
THE PROBLEM AND A PROGRAM PORRESEARCHt
by Neil Cfaurcbill and Louis TeiteUMum. ONR Re-
search memo. no. 68 on Plaaning and Control of In-
dustrial Operations. Contract [Nonr-760(01)] ktey 60,
24p. 19 refs.
Order from LCmi$2. 70, phM-M) PB 148 787
Fonlons at tMs report wiU not reproduce areli .
74B
Carnegie Inst, of Tech. Graduate Scbotd of Indus-
trial Administration, Pittsburgh, Pa.
pORBCASnNG SALES BY EXPONENTIALLY
WBICHTED MOVING AVERAGES, by Peter R.
Wiawrs . (WR Research menx>. no. 62 on Planning
and Control of Industrial Operations , Contract
[14oor 760(01)]. Mar 59. 37p. 2 refs. AD-218 886.
OnierfromLC mi$3.00, pb)6.30 PB 154 869
This report released for sale to the public 24 Mar 61 .
Methods are presented for forecasting sales of Individ
utl products for inventory control and production
scheduling. The forecasting techniques discussed do
not predict with a behavioral nwdel of sales , but use
u analysis of the sales time -series taken out of
ccntext, i.e. , the only input is the past history of the
tales of the item . Three forecasting systems , in-
cluding the exponential model, are used; each in a
ilmilar way to predict sales for 3 different products .
A comparison of ability to predict is presented .
Omegie Inst, of Tech. Graduate Schocri of bidus.-
trial Administration, Pinsburgh. ?•..
HEURISTICS IN JOB SHCff> SCHEDULING, by William
S, Gere, Jr. 04R Research Memo. no. 70onPlan-
gii^ and Control of Industrial Operations [Contract
NdK-76O(01]. June 60. 21p. 17 reft; AD- 240 134.
Order from LC mi$2. 70. phf4. 80 FB 149 068
Iflgersoll Kalannazoo Div . , Borg- Warner Corp. ,
kAch.
FABRICATldN OF LARGE DIAMETER TITANIUM
PRESSURE VESSELS BY THE SPIRAL WARP
METHOD, byR. E. Angennan. Rept. no. 1.
1 July-31 Dec 60. on Contract DA 20-018-ORD-22890.
[1961] 55p. 13 refs. AD- 250 501.
Order from LC mi$3. 60. pb|9. 30 PB 153 917
Eighteen specimens were fabricated of stainless steel
strip and were bonded with a nitrile phenolic adhesive
for vibration and aging testing. An analysis of the
hcadbif problems incurred with AM 355 metal strip
is Included. The result of axial compression loading
of tubular sections is presented . The titanium alloy
strip for the fabrication of 20^ diameter specimens is
oa order.
Loewy-Hydropress Div.. Baldwin Lima -Hamilton
Corp. , New York.
DEVELOTvlENT OF AN EXTRUSION METHOD FOR
THE PRODUCTION OF W1C« PROFILE EXTRU-
SKNS. VOLl^E L FLAT EXTRUSON CON-
TAINER, byA. H. Tesmcn, W. H. Stocker, and
A ZandeL Final technioU engineering rept. for
29 Aug 52-1 Apr 60 on Contract AF 33(600)21525.
July 6a 184p. AMC Tecfanical repi. 60-7-257:
AD- 243 792.
Oniar from OTS $3.00 FB 171 568-1
Wide, flat, thin-prcfile aluniinum extrusions for high
porformance aircraft and missile application can be
readily and economically extruded by means of a
ractnfular (flat) billet container in conventional ex-
tnslon presses rather than being extruded front
conuiaers in "V or round sh^es requiring
subsequent flattening. A rectangular container
proved s uperior to the round container in that thinner
sections are possible and greater unit pressure
effeaed more efficient metal flow. The necessity
for converting the extruded section from "V" or
other shapes which resulted from previously used
round containers was eliminated. In use, die rectan-
gular container made possible an extrusion pressure
of 109, 000 psi on die billet. An integrally stiffened
panel of 7075 aluminum alloy, 18 inches wide, with
web thickness of 0.037 inches, having eight stiff ener%
each one inch in height by 0.100 inches chick was
successfully extruded to a length cf 25 feet and with
excellent surface condition. Specific die entrance
angles and sturdier die design were necessary to
withstand the higher extrusion pressures. (Author)
Loewy-Hydropress Div. . Baldwin- Lima- Hamilton
Corp. , New York.
DEVELOPMENT OF AN EXTRUSION METHOD FOR
THE PRODUCTION OF WIDE PROFILE EXTRUSIONS.
VOLUME n. PHOTOELASTIC INVESTIGATION AND
STRESS ANALYSES OF FLAT AND RECTANGULAR
EXTRUSION CONTAINERS. Final technical engineer-
ing rept. on Contraa AF 33(600)21525. 11960) 164p.
[AMC TR-60-7-257J AD- 243 793.
Order from OTS $a 00 PB 171 568-2
A study of models by the photoelastic method was sat-
isfactorily uaed to determine the stress distribution
that would exist in the prototype containers intended
for the extrusion of rectangular billets. For the con-
ventional round container, it was shown that the distri-
bution of stress and pressure from the billet opening
to the container was dependent on the cavity shape and
insert srrangetnent. The most effective insert ar-
rangement from the stanctpoint of minimum stress
concoitration was to give a rectangular billet opening
which is the shape most duicable for the extrusion oA
the greatest variety of wide aectiona. A study of the
effect of a multiplicity of rings indicated that a 2 piece
assembly, apart from inserts, gave the least stress
concentration. A construction entailing the use of in-
serts, liner, and container was adopted for the proto-
type flat and recungular comainer designs. The opti- .
mum conuiner shape consistent with slm{de and fea-
sible fabrication methods was rectangular with certain
relative proportions between the height, width, and
the round opening into which the inserts are assem-
bled. Dau were developed which were tranalated into
design curves which enabled a designer to select the
desired container design for different conditions.
Consideration was given to the stresses and design of
auxiliary tools which are necessary for flat extrusion
and to a deaign chart covering a wide range of preases
(See also FB 171 566-2)
Watervliet Arsenal, N. Y.
CISMICAL MILUNG, by C. H. Rose. Rept. on
Induatrial Preparedness Measure 80304231 -03-46400.
Dec 60, 2lp. 5 refa. Teclmical rept. WVT-Rl-6001-1
Order from OTS $0.75 Pfi 171 112
A process study, outlining the capatalities and limiu-
tioM of chemical milling, the materiala for which it
is suitable, the accuracies and surface finiabes ex-
peaed; derived from a study of the available literature.
749
and visits to us^rs at the process, are made to deter-
mine the applicability of the method to the pilot pro-
duction requiretnents of Watervliet Arsenal. Forty-
two pouDds at 4M0 steel were removed from a 90rnm
M41 breech ring in 61 hours by chemical milling.
Surface finish vfaa 62 mlcrolnches. Metal removal
rate was . 0007 inch per minute. (Author)
Transport, Traction and Hoist Facilititts
Army Transp^ation Research Command, Fort
Eusiis, Va. 1
STEERABLE FtFTH WHEEL, by John E. Thomas and
Ralph L. SchulKer. Final rept. on Project 9R98-
05-007, House oask 5. 23. Jan 61. 17p. TREC Tech-
nical rept. 61 -i.
Order from OT^ $0. 50 PB^7l 613
I
This report coviers the testing and evaluation of a
device that was designed and constructed for the
purpose of evaliiating the principle of transverse fifth-
wheel motion a^ a method of facilitating steering in
truck -tract CM- semitrailer or shuttle -traaor opera-
tions. The test^ proved that the equivalent of all-
wheel steering tan be accomplished through trans-
verse movement of a fifth whieel mounted on a truck
tractor. (Authcl-)
Davidaon Labi, Stevens Inst, at Tech. . Hoboken,
CC»ITROL SYStEMS FOR HIGHWAY TRAINS, by ,„
J. P. FinelU an^ C. J. Nuitall, Jr. (Wilson. NuttaU.
Ralmond Engineers, Inc.). Final rept. on Phase 1.
Contract DA 44|-177-tc-390. Sep 60, 81p. 23 refs.
Rept. no. 801 (Includes note no. 600) AD- 248 040.
Order from LC|ml$4. 80. ph$l3. 80 PB 153 713
Efforts are being made to develop feasible systems for
the simultaneous control at multiple engines. These
systems are to be suitable for application to highway
trains consisting of several 4-wheel units, each with
its own powerplant. It was concluded chat an ideal
multiple -engine^ control system would: (1) permit op-
eration of indeplendent units after separation from the
train. (2) permit all controls to be centralized in the
lead unit, (3) permit any unit to be used as the lead
unit, (4) enable the train to develop its maximum trac-
tive tttan, (5) Minimize compressive drawbar forces
that lead to jacltknifing (in all possible circumstances)
without sacrifiqing the ultimate ability of elements to
as«ust one another when necessary, (6) divide normal
driving load more-or-less equally among the engines,
(7) control and limit wheel slip for maximum traaion
or braking, (8) include engine over -speed protection,
and (9) be as simple, reliable, readily operated, and
inexpensive as possible. The following basic systems
are considered feasible: (1) thronle position control.
(2) engine rpm control (far use with open converter
only), (3) drawbar control, and (4) thronle poeition
control with drawbar modulation. (Author)
George Washington U. , Washington, D. C.
ESHMATING MERCHANT SHIP REPAIR LOADS
AND REPLACEMENTS UNDER CONVOY AND NON-
CatiWOn CONDITIONS, by R. B. Hunt and Erling P.
Rosholdt. Rept. on Logistics Research Project,
Contract Nonr-761(05). 31 Mar 60. 39p. 6 refs .
Serial T- II 1/60; AD- 234 560.
Order from LC ml$3. 00, ph$6. 30 PB 153 736
This paper has four objectives: (1) Points out the
major defects in the present repair policy used for
determining merchant ship requirements to meet a
prescribed lift schedule. (2) Proposes a new and more
accurate repair policy for planning purposes . (3) De-
scribes a method for (a) using the proposed repair
policy to derive estimates of the number of ships
going into overhaul each time period (which provides
a repair load schedule); and (b), to derive estimates
of the number of repair replacement ships needed to
supplement the "pure" ship requirements of the pipe-
line. (4) Provides illustrative examples of the use of
the preceding method and graphically compares the
current and new policies by showing tiieir effects on
sample pipelines . The repair policy proposed for
planning purposes may be stated thusly: (A) Under
non-convoy conditions , each ship will be as sunned to
receive an average of 18 days per year for major re-
pairs (overhaul). (B) Under convoy ccmditions , each
ship will be assumed to receive an average at 47 days
per year. This shall include the normal overhaul
period (non-convoy condition) of approximately
18 days and the remainder shall be for possible ex-
traordinary repairs , e.g. , battle damage. (Author)
Land Locomotion Lab. , Ordnance Tank -Automotive
Command. Center Line. Mich.
EVALUATION OF CONDUAL TIRE MODEL, by
E . Hegedus . Rept . on Contract DA 20-089-ORD-39246.
Mar 60, 30p. 7 refs. Rept. no. RR-17; LL-60.
Order from LCmi$2. 70. ph$4. 80 PB 152 006
Investigation of experimenul tires indicates that in
most types of soft ground the concent ricdual (condual)
tire producing a long, narrow contact area developes .
considerably less slippage and more drawbar pull
than a conventional dual tire having a wide contact
area. The condual tire has been investigated in a
number of soil types , and the discussed advantages
given by that tire form have been found in a reason-
able agreement with theoretical predictions . In this
report the computations aixl tests were performed for
very thin walled, elastic, small scaled tires, but re-
cent theoretical evaluations for full size tires also in-
dicate the superiority of the condual tire concept over
conventional tire forms . (Author) (See also
PB 152 004) ^
Land Locomotion Lab. , Ordnance Tank -Automotive
Command , Center Line , Mich .
MOBUTY STUDIES, by W. L. Harrison,^. Janosi
and others . Rept. on Contract DA 20-089-ORD-
39246. Dec 59, iOp. 5 refs. Rept. no. RR-5; LL-59.
OrderfromLCml$4.50, ph»l2.30 PB 152 OM
750
Xtti report was prepared to fill a requirement for
the mobility evaluati£in of a group ol existing v^iicles
and vehicle concepts , and the effect of steering on off-
niMl performance. The study consists o€ both analyti
cal evaluations of existing vehicles and vehicle con-
cMts , and experimental evaluation of the effect of
steering on off- road performance. The experimental
evaluation of Ackermann and articulated steering can
only be considered as tentative, since an extended
pngram has been initiated to fully evaluate the
steering mechanics of articulated type steering. Ini-
tial studies Indicated the qualitative improvement in
performance. A truck-family concept initiated by the
Land Locomotion Laboratory is evaluated by an ana-
lytical process . The concept is based on the train"
principle utilizing large dianneter wheels . The con-
cept Is essentially a system of powered primary and
secondary units that can operate coupled or or un"
coupled to achieve a high degree of flexibility cover-
iiy load capacities from one to fifteen tons . (Author)
Land Locomotion Lab. , Ordnance Tank -Automotive
Command. Center Line, Mich.
ON THE STATISTICAL ANALYSIS OF THE MO-
TION OF SOME SIMPLE TWO-MMENSIONAL LIN-
BAR VEHICLES MOVING ON A RANDOM TRACK,
byP. KozinandJ. L Bogdanoff. Rept. on Contract
DA 29-089 -ORD- 39246. Apr 60, 32p. 8 refs. Rept.
no. RR-l9;LL-66; AD- 244 099.
Onler from LC mi$3. 00, ph$6. 30 PB 152 007
The influence of the length parameters; base length,
idealised tire spread and track roughness spread; on
the assumed "ride" criterion of some simple two-
dimensional linear vehicles is examined. This exami-
sation is made under the assumption that the vehicles
more with constant horizontal velocity on a weakly
■udonary random track in such a way that contact is
maintained with the track throughout the motion. It is
found chat base length and track roughness spread have
a pronounced influence on the ride criterion chrough-
out Che range of interesc in chis paper. However, che
idealized tire spread only produces a marked effect
OB the ride criterion if the base length has been badly
chosen. As the analysis is based upon second order
statistical properties, a knowledge of all of the joint
probability distributions of che random crack is not
t«|Uired. (Author) (See also PB 152 006)
L4ind Locomotion Lab. , Ordnance Tank-Automotive
Command . Center Line , Mich .
ON THE STATISTICAL ANALYSS OF THE MO-
TION OF SOME SIMPLE VEHICLES MOVING ON
RANDOM TRACK , by J. L. Bogdanoff and F . Kozin.
Rept. on Contract DA 33-088-ORD-1738. Nov 59.
96p. 5 refs . Rept. no. RR-20; LL 65i AD-244 094.
OrdcrfromLCmi$5.40. pb$15.30 PB 152 008
A summary is presented of a statistical analysis of
the motion of one and two degree of freedom point
follower linear vehicles moving with constant horizon-
tal velocity along a track whose elevation vs . horizon-
tal disunce is a stationary second order random func-
tion. Vertical displacement and vertical acceleration
of the mass , vertical and horizontal components of
the force exerted by the follower on the track and
borlzonul force required for towing are considered.
It Is shown that for the symmetrical two degree of
freedom vehicle and a fairly general form for the
power spectral density of the random function repre-
senting the track the follower base length has a pro-
nounced influence on the peak value of the pjower spec
tral density of the vertical acceleration of the mass
center. Criteria for maximum vehicle velocity based
upon rider comfort are also discussed. (Author)
Land Locomotion Lab. . Ordnance Tank -Automotive
Command, Center Line, Mich.
A SIMPLIFIED METHOD FOR THE DETERMINA-
TION OF BULLDOZING RESISTANCE, by Ervin
Hegedus. Rept. on Ccwitract DA 20-089-ORD- 39246.
May 60, 31p. 7 refs. Rept. no. RR-22; LL-61.
Order from LC ml$3. Oa ph$6. 30 PB 152 009
The resistance caused by bulldozing the soil at the
front f)ortion of a track or wheel id of great import-
ance. The problem of calculating bulldozing resist-
ance has been solved first by M. G. Bekker. His
method is baaed upon curved rupture surface assump-
tions. Because of the complexity of Bekker' s method
and the difficulty in the evaluation of the factors in-
volved a simplified mechod has been escablished and
tested. This paper presents the simplified derivation
of an equation based upon theassumptions of Coulomb's
passive earth pressure theorem for the compuution of
the bulldozing force. The basic Coulomb assumption
is chac the surface of rupture is plane and that the
direction of the forces is known. Experiment* show
that the plane rupture surface assumption is a good
approximation and the error involved is relatively
small for most of the practical cases. (Author)
Land Locomotion Lab . , Ordnance Tank- AutomotlTe
Command , Centex Line . Mich .
TRlAXIAL TESTS ON SATURATED SAND AND ON
SANDS CONTAINING SOME CLAY, by R. J. Evans.
Rept. on Contract DA 19-020-ORD-4566. July 59.
22p. 8 refs. Rept. no. RR-14; LL-64; AD-244 098.
Order from LCrol$2. 70, ph|4. 80 PB 152 005
The paper describes several series of irlaxial tests
on sand and sand/clay mixtures of low clay content.
Tests were run with both axial compression and axial
extension. The .Results obtained are discussed in the
light of various limiting equilibrium stdutions for
which the stress distributions in the specimen are
,non- homogeneous . (Author)
r--
Naval Civil Engineering Lab. , Port Hueneme, Calif.
MODEL STUEXBS OP TRAMWAY CABLE TENSION
CONTROLLERS, by W. F. Buii:art and D. A. Crane.
15 Oct 53. I8p. 5 refs. Technical note N-168. .^
Order from LC ml$2. 40, ph$3. 30 PB 154 658, ,
This technical note reports further model studies in
which attempts were made to control the line tension
usiii«; (1) an electric differential drive; (2) an electro-
magnetic, dry fluid clutch; (3) a counterweight; and
(4) a cable anchorage independent of the simulated sWp-
No attempts were made to evaluate components of the
systems for durability and dependability. ^
751
Southwest Research Inst. , San Antonio, Tex.
TRACKING MECHANISMS AND COUPUNGS FOR A
COMBAT SUPPORT TRAIN CONCEPT. PHASE I,
CURRENT STATE-OF-THE-ART TECW^OLOGY,
by Fred jindra. Final technical rept. on Contract
DA44-177-tc-631.Nov 60. 80p. 157 refs . SwRl rept.
no. BE- 384: Ti^C Technical re|ic. 60-68:
AO- 248 445.
Order from LCmi$4. 50. ph$12. 30 Ft 153 703
A comprehensivie survey is presented of literature
pertaining to anilytical and expenmencal evaluation
of trailers and trailer components and of letters pat-
ent related to foiir-wheel steering of trailers . Upon
defining the functional requirements for tracking sys-
tems of a train-type vehicle, practical concepts on
tracking ntechai^isms are proposed. Future work aad
development a r0 outlined. (Author)
f
TERIALS
AppUed PsychoQogical Services, Wayne, Pa.
AIRCRAFT DETECTABIIJTY AND VISIMLTTY: II.
TACHISTOSCOPIC THRESHOUDS FOR FLUORES-
CENT AND ORplNARY PAINTS, by Kenneth Grain and
Arthiarl. Siegel| Rept. on Pro). TED NAM AE -42222,
Parts. Contract* Nl 56 -38581. I Nov 60, 25p. 2 refa.
NAMC-ACEL-444; AD-247 539.
Order from LC <ni$2.70. ph$4.80 FB 153 900
An experiment designed to provide basic infcrmatioo
about the relative effectiveness of fluorescent and
ordinary paints ss stimuli was performed. Fluorescent
red-orange, ye How -orange, and blue and matching
ordinary colors were compared through tachistoscopic
threshold determination methods. Under each of two
luminance conditions two thresholds were determined:
(1) Che point at which the stimuli could be first identi-
fied as objects regardless of whether or not their color
was identifiable (first seen threshold), and (2) that
point at which th^ color of the stimuli could be re-
ported (true color threshold). For both luminance
levels investigated, with the exception of fluorescent
blue, the first s«en thresholds of the ordinary paini
stimuli were loiter (faster recognition times) than
those of the fluorescent stimuli. On the other hand,
the true color thresholds at the ordinary palms were
higher (slower recognition times) than diose for the
fluorescent paints. (Author)
Army Chemicail Research and Development Labs. ,
Army Chemical Center, Md.
MATERIALS RBVIEW (NO. 8), by Arthur Lyem.
Rept. for 4 Jan-$ July 60. Sep 60, Sip. 263 refs.
CRDL Special pMb. 4-22; AD- 246 153.
Order from GTSIJ2. 25 PB 171 612
Contents:
High polymsrs ,
Chemistry (including macromolecular ctemiacry)
Technology (including polymerization)
Physical and chemical cbaraaeriacics
Plastic materials
Engineering and methods
Materials of construction types
End-product behavior
Nuclear aspect^ (radiological and thermal)
Medical and biological considerations
Conunercial and military applications
Synthetic fibers
Manufacturing techniques
Textile wet -processing
Properties
Industrial applications
Metals and inorganic materials
New concepts
(See also PB' 161 971)
Army Signal Research and Development Lab. , Pen
Monmouth, N. ].
EFFBCTS OF IRRADIATION AND THERMAL
TREATMENT ON THE DIELECTRIC DISPERSIONS
IN NYLON, by Marvin N. Stein. Nov 60, 94p. 53 r«ft
USASROL 'Technical rept. 2149; AD- 248 864.
Order from LC mi$5. 4a ph$15. 30 PB 154 529
The effect at irradiation and thermal treatment on the
dielectric properties of aeveral long chain polymers
waa studied in the temperature region from -160 deg
C to *%0 deg C for frequencies from 0. 1 to 100 kc.
The dielectric data show one or more dispersion re-
gions whicb were correlated with the onset of varioua
modes of internal motion within the polymera. The
changes in dielectric propertiea are interpreted in
terms of the alteration in stmcture produced by irra-
diation, absorbed moisture and thermal treatment.
The concept of radiation damage as a themval spike
phenomenon ia introduced to explain the aimllar re-
sults produced by thermal quenching and Irradiation.
The two low temperature dispersion regions in nylon
were studied extensively and are diacussed in detail.
(Author)
Department of the Navy, Washington. D. C.
MANUAL FOR SOURCE INSPECTION AND ADMIN-
ISTRATION OF NA\fT PROCEDURE. APPENDIX A.
26 Feb 60, I3p. 1 ref. Navy Procurement Directives
NAVEXOS P-1034.
Order from LC mi$2. 40. pfa$3. 30 PB 155 311
This repnt released for sale to the public 10 Apr 61.
Geographisches Inatitut der Universitlt ZUrich
(Switzerland).
INTERPRETATION OF AERIAL PHOTOGRAPHS, by
Haas Boesch. Pinal technical rept. no. 1. 1 Nov 57-
31 Oct 58. on Contraa DA 91 -S08-EUC-240. 31 Oct H
24p. 7 refs. AD- 207 400.
Order from LCmi52 70. pli$4. 80 PB 155 431
Thia report releaaed for aale to the public 12 Apr 61.
Effort is made to find a suitable method which allowt
a systematic air photo interpretation of the Swiss
agricultural landscape. Such a method requires the
implication of all formal qualities characterizing a
land uae unit on the photograph, such as site, form.
size, gray tone, texture, and stereoscopic appearaaoe.
The value of site, form and size for the interpretatioa
is quite evident and needs no investigation in detail.
The uaefulnees of (pialities like gray tone and texture
ia very much diaputed and requires a careftil study.
The atudy of the gray tone impUcatea the evaluation of
7S2
its behaviour as function of day time, angle of observa-
tion, flight altitude (scale), photographic process, and
teason. If, for instance, the variation scales of two
different crops overlap at given conditions, it is
hardly possible to distinguish these crops only by
meaas of the gray tone. If, however, they do not over-
lip, identification is possible. (Author)
Hawker Siddeley Nuclear Power Co. , Ltd.
(Ci. Brit.)
THE PRODUCTION OF MATERIALS BASED ON
GRAPHITE WITH REDUCED PERMEABIUTY AND
WITH IMPROVED OXIDATION AND EROS^LON RE-
aSTANCE. Final technical rept. for 1 Aug 59-31
July 60 on Contract DA 91-591-EUC-1176. Nov 60.
53p. Technical rept. T. R. 3^1960; AD-249 571.
Ofdsrfrom LCmi)3.60. ph|9.30 PB 153 914
An investigation of the techniques of impregnating
graphite with silicon and titanium is described. The
impregnants were SiCl4, and TiCl4. The in:^>r^na-
tion processes were investigated by "the pressure
gradient technique" and the "diffusion technique" .
With the pressure gradient technique deposition of
silicon with good penetration could be niade to occur
at a temperature of 950OC. Experiments carried out
using Che diffusion technique were inconclusive.
Naval Qvll Engineering Lab. , Port Hueneme, Calif.
ALTERED ANORTHOSITB, by John A. Bishop.
24 Apr 51 . 7p. 9 refs . Technical note N-015.
Older from LCmi$ 1. 80, p»4 1.80 PB 154 636
This paper describes altered anorthoslte, and reports
the findings of various invescigacors who have made
some qualitative tests on the proposed material.
Naval Civil Engineering Lab. , Port Hueneme, CaUf .
PLEXURAL AND END-BLOCK STRAINS IN A PRE-
STRESSED CONCRETE BEAM, by J . R . Libby . Interim
Bsmo. ISepSl, 31p.6 refs. Technical memo . M-030.
Order from LC mi$3.00. ph$6.30 PB 154 620
In order to determine the structural properties of
prestressed concrete, an I-shaped. post- tens ioned,
prestressed concrete beam was constructed and
cested. Prestresslng with large-size cables equipped
with swaged terminals seems to be advanMgeous over
MXhcidi commonly used in Europe, since (I) pre-
ttrctting can be accomplished with a smaller number
d movements of the prestresslng Jack, (2) no special
hardware is needed to secure the end of the cables
after tensioning, and (3) no specially designed pre-
stresslng Jacks are required. TTie beam failed on a
■Mtiy horizontal plane through the end block when it
was subjected to a design load of 149 per cent, ladi-
catiag the existence of excessive tensile stresses .
Prom the standpoint of flexural strains , the results of
'*"• expennnent show a close agreement with the theo-
retical analysis of prestressed concrete. The results
also indicated that prestressed beams are capable of
wH^tanding relatively high shear stresses without
•^•rte effects . (Author)
Office of Technical Services, Dept. of Commerce,
Washington, DC.
LOW TEMPERATURE RESEARCH ON MATERIALS.
Feb 61, 28p. 316 refs. OTS Selective Bibliography
SB-451.
Order from OTS $0. 10 OTS S8-451
Lists PB reports, ABC reports, and translations added
to the OTS collection during 1950 to February 1961.
Includes cryoscopic bibliographies, data books, meas-
urements and measuriiig devices; low temperature
effeas on tensile, ductile, thermal, electrical, and
superconductivity of metals; low temperature effects
on plastics, elastomers, gases, lubricants, and hy-
draulic fluids; low temperature batteries, digiul sys-
tems, transistors, and semiconductors. (Author)
AdhesivM and Sealants
Borden Chemical Co. , Philadelphia, Pa.
STUDY LEADING TO THE DEVELOPMENT OF
HIGH TEMPERATURE RESISTANT ADHESVES, by
Jack Oickstein. Quarterly progress rept. no. 1,
22 June-22 Sep 60, on Contract DA 36-034-ORD-
3316-RD. [1960] I6p.
Order from OTS $0. 50 PB 171 565
Many heat -stable phenylene- and triazine -containing
polymeric systems were prepared in large quantities.
The softening points of these systems ranged from
250° C. to greater than 600° C. The polymers were:
(1) Polypheny lenes, (2) Poly 2,6-X> lenols, (3) Melon.
(4) Condensation polymer h'om benzoluanamine and
diphenyl carbonate, (5) Self condensation polymer of
2-amiiK>-4, 6-dipbenoxytriazine, (6) Condensation
poljrmer from benzoguanamine and cyanuric chloride.
Infrared and "loes on heating" studies showed the good
thermal stability of these polymers. The poly 2, 6-J^-
lenol polymers were oxidized to carboxylic add de-
rivatives. These acid polymers were soluble in alkali
and retained the good heat resistance of the poly
2,6-xylenols. Anempced chloromethylation of the
polyphenylenes led to products containing about 4%
chloromethyl groups. The reaaion of phosphorous
pentachloride on the condenaation polymer from
benzoguanamine and diphenyl carbonate led to a high
melting product which is under inveacigatian.
Naval Ordnance Lab. , White Oak. Md.
O-RING MATERIALS FOR NAVAL ORDNANCE AP-
PLICATIONS, by Doris V. Steele and A. R. Tintmins.
1 Aug 60. 5lp. 13 refs. NAVWEPS rept. 7284;
AD- 248 647.
Order from OTS $1.50 PB 171 688
A study was made of 0-ring materials conforming to
Military Specification MIL-P-5516A to determine their
suitability for pneumatic applicationa in Naval ord-
nance. Two typea of silicone elastomers were also
included in the atudy. Results indicate that MIL-
P-5516A O-rings may be suitable for many applica-
tiona but that low temperature stiffening at -54 C
(-65 P) could permit leakage or breathing of ordnance
under adverae conditions. It ia recommended that
753
MIL-P-5516A Offings be lubricated with DC-55 ■lU-
cooe pneumatic grease (M1L-L-4343A) to otxain 0(«i-
mum a^ng prop«rtie8. Parkone No. 2 slUcone 0-ringt
•re not reconuntnded for Naval ordnance appllcatioos
Linear ZB-70 siUcxine.&iring? are suitable for static
seals. This laaer material is resilient at tempera-
tures as low as -73 C (-100 F). Silicone O- rings are
not recommendad for dynamic seals because of their
low abrasiai aai tear resistances. (Author)
Caramics and Refractori«s
Battelle Memorial Inst. . Columbus, Ohio.
INVE^riGATlOM OF THE FATIGUE PROPERTIES OF
MOLYBDENUM UNDER VARIOUS CONDITIONS OF
TEMPERATURE. COATINGS, AND STRESS CONCEN-
TRATICW, by Alexander A. Minenbergs, Dean N.
Williams and otlers. Rept for July 58-Mar 60 on
Ceramic and Cermet Materials, Contraa
AF 33(616)5915. Oct 60, I37p. WADD Technical rSpl.
60-427; AD-249770.
Order from CT^ $2. 75 PB 171 617
Fatigue behavlot of unalloyed arc -cast molybdenum
was investigated in tension-tension fatigue loading oo
uncoated and coated, unnotched and notched sheet
specimens at ISpO F, room temperature, and -40 F.
Three oxldation'reslstant coatings were evaluated
under fatigue loading. Static tensile tests were also
conducted on specimens ci the four surface conditions
at the three temperatures. The fatigue strength of un-
protected molybbenum at 1800 F was In the same range
as the fatigue strength at some other high-temperature
materials at thi^ temperature. At room and low tem-
peratures, the (fatigue strength of unprotected speci-
mens was relatively high. The notch sensitivity of un-
protected molybdenum was low at 1800 F, but rather
high at room an<l at low temperatures. All coaUngs
lowered the fatigue strength of molybdenum at all three
temperatures. The loss of fatigue strength was higher
in the notched specimens. The coatings investigated
did not prove to] be completely reliable for high -tem-
perature applications under continuous fatigue loading.
Far short-life high -temperature fatigue loading, how-
ever, utilizatiod of coated molybdenum appeared to be
possible with proper precautions. Further research is
suggested on prbtective coatings and on molybdenum -
base alloys. (Aythor)
General Electric Researth Lab. . Schenectady, N. Y
THE INFLUENCE OF HIOI PRESSURES AND HIGH
TEMPERATURBS ON TRANSFORMATIONS AND
COORDINATION IN CRYSTALLINE AND VITRECXJS
CERAMIC MATERIALS, by W. P. Claussen, R. C.
Devries. and J. D. MacKenzie. Rept. on Metallic
Materials, Contraa AF 33(616)6295. Nov 60, 48p.
19ref8. WADDTechnlcal rept. 60-304.
Order from Ol% $1 . 25 PB l7l 595
The effea of hl|h pressures and temperatures oo
densificatlon of vitreous silica and germania and on the
polymorphism df crystalline Al^SiOs was investigated
by using the higr- pressure techniques developed for
diamond synthesis. Germania glass of a density ap-
proximately eqMivalent to that of the quartz-form
germania was loftde by this techiiique. A shift of IR
reflection bands at 1110 cm-^ for Si02 and 895 cm-^
for Ce02 suggested that the densificatlon of the glasses
is a result of the decrease of the M-O-M angle, but the
over -all spectra for both compressed vitreous Si02 «ail
Ge02 are imchanged, from the correspondingly less
dense glasses. High temperatures and pressures study
of the system AI2SIO5 established that high -pressure
form kyanite melts to 0-AI2O3 plus liquid. When
kyanlte is "hot-pressed" in its stability region, the
grains show complex slip and kink pattern; but kyanite
found under the same conditions from andaluslte or
sillimanlte have simple grains possibly due to twinning.
No region of liquid immlscibiUty was found in this sys-
tem as might be expected. (Author)
New York State Coll . of Ceramics . Alfred U .
PHASE EQUIUBRIA BETWEEN B2O3 AND REFRAC-
TORY OXIDES: THE SYSTEMS BeO-B203 AND
Th02-B203, byD. E. Rase. Summary repc. for
1 June 59-31 Aug 60 on Contract AF 33(616)6545.
Aug 60, 15p. 10 refs i AD- 245 466.
Order from LC mi$2. 40, ph$3. 30 PB 152 980
The system BeO-B203 contains only one stable inter-
mediate phase having the composition 3BeO-B203.
The beryllium borate nwlts at a temperature higher
than 1445°C. Selected interplanar specings and some
optical properties characterizing this phase are pre-
sented. A tentative phase diagram for the system
Th02-B203 is presented. The system is character-
ized by extensive liquid immiscibility, one intermedi-
ate stable phase (Th02B203). and two eutectics .
Thorium borate appears to melt at 1483 ± 5oC to fonn
two immiscible liquids . (Author)
Philips Labs., Inc., Irvingion-on-Hudson, N. Y.
RESEARCH INVE LIGATIONS OF MAGNETIC MATE-
RIAL, PERMANENT CERAMIC TYPE, by Frank G.
Brockman, Paul W. Beck, and Reina A. Hutner. Quart-
erly progress rept. no. 5, 1 July -30 Sep 53, on Con-
tract DA 36-039-SC-42503. 30 Sep 53, 2lp. 3 refs.
Order fromLC mi$2.70, ph$4.80 PB 155 239
This report released for sale to the public 31 Mar 61.
The magnetic properties of the strontium oxide -Ir 00
oxide material were determined at various tempera-
tures from -69° to * 97°C. Investigation of the reU-
tionship between coercive force and particle size was
continued. Experiments were begun in order to pro-
duce barium oxide -iron oxide magnetic material pos-
sessing a high degpree of orientation. (Author) (See
alsoPB 113 554)
Philips Labs. , Inc. , Irvlngton-on-Hudson. N. Y.
RESEARCH INVESnGATIONS OF MAGNETIC MATE-
RIAL, PERMANENT CERAMIC TYPE, by Frank G
Brockman and Paul W. Beck. Quarterly progress re^.
no. 6, 1 Oct -31 Dec 53, on Contract DA 36-039- sc-
42503. 31 Dec 53, 18p. 2 refs.
Order from LC ml$2. 40, phJ3. 30 PB 155 24©
This report released for sale to the pubUc 31 Mar 61.
muw 1
754
lafMCigstlOffoTtfie relationship between coercive iforce
sod particle size was continued. An air elutriator is
beiag applied to the separation cA sub- sieve size parti-
cles. Means of determining particle size distributions
in this range are being investigated. Experiments
were 'continued to produce oriemed samples of the
barium oxide-iron oxide material. (Author) (See also
n 155 239)
Philips Labs. , Inc., Irvlngton-on-Hudaon, N. Y.
RESEARCH INVESTIGATIONS OF MAGNETIC MATE
RIAL. PERMANENT CERAMIC TYPE, by Frank G.
Broclonan and Paul W. Beck. Quarterly progress rept
no. 7, 1 Jan-31 Mar 54, on Contraa DA 36-039-sc-
42503. 31 Mar 54, 20p. 3 refs.
Order firom LC ml$2.40, ph$^. 30 PB 155 241
This report released for sale to the public 31 Mar 61 .
Advances were made in the determination d particle
■Ize distribution in the finely powdered barium com-
pound. Even though well -sintered polycrysialline ma-
terial has been reduced to an average particle size of
•bout 2 microns, the coercive force was found to be
only 1900 oersteds. Two fraaions were obulned from
the air elutriator. Some part of the period was con-
sumed in overcoming the experimental difficulties ex-
perienced In preparing crack-free test samples. Sev-
eral kilograms of raw materials were prepared and
•tudies were begun with final raw material for
orienting which contained no added calcium carbonate
and 1/4% and 1/2% by weight of calcium carbonate.
The highest energy produa obtained was 2. 7 x lO'^.
Preliminary evidence suggests that a second phase is
imrolved In the development of the permanent magnet
properties of the unoriented material (and presumably
also for the oriented material) (Author) (See also
PB 155 240)
Philips Labs., Irvington-on-Hudson, N. Y.
RESEARCH INVESTIGATIONS OF MAGNETIC MATE-
RIAL. PERMANEhn* CERAMIC TYPE, by Frank G.
Brodonan, Paul W. Beck and Walter G. Steneck, Jr.
Progress rept. no. 8 (Final) 1 Apr-31 July 54, on Con-
traa DA 36-039-SC-42503. 31 July 54, 55p. 8 refs.
Order from LC mi$3. 60, ph$9. 30 PB 155 242
This report released for sale to the public 31 Msr 61 .
The objective of producing a ceramic permanent mag-
net of the composition type M^kyi^FejO-^t^ with an en-
ergy product, (BH)niax. exceeding 3 x 10 ^ gauss oer-
steds has been achieved. The best sample had an en-
ergy produa of 3. 5 X 10^. That a second (non-mag-
netic) phase is present in high energy permanent mag-
nets of this composition has been demonstrated. A re-
cording fluxmeter which can be applied to the automatic
registration of field strength versus induaion dsta was
completed. With X-ray laboratory assistance beoomlng
again available, a return was made to the study of the
chemical reaaions involve in the synthesis erf the
oompoMod, BaO (Fe203)6. The particle size dlstrlbu-
tlOBS aad coercive farces of two BaO- 6 Fe203 powder
aamples separated by air elutriatlon were determined.
It wsa shown that pre -fired powders have coercive
'**^ much higher than powders of the same particle
■*» prepared by grinding well-sintered discs. The
coercive force of s flne-grsined BaO 6 Fe203 disc is
decreased by grinding to s powder. (Author) (See also
re 155 241) ^ ^
Fuels, LubHcants, and Hydraulic Fluids
Air Force Flight Test Center, Edwards AFB. Calif.
DETERMINATION OF HYDRAZINE-1, 1-DIMETHYLf
HYDRAZINE MIXTURE, by Hugh E. Malone.
Jan 60, 16p. 15 refs. AFFTC-TN-59-38; AD-231 372.
Order from LC mi$2.40, pfa$3.30 PB 154 716
Mixtures of hydrazine- 1 , 1-dimechylhydrazlne are
blended to obtain certain desirable properties of each
rocket fuel. A method for analyzing these mixtures
utilizing the selective action of hydrazine with sali-
cylaldehyde to form the neutral salicyialdazine is
presented. The 1 , 1 -dimethylhydrazine also reacts
with salicylaldehyde; however, the dinnethylsalicylhyn
drazbne formed is basic. The reactions are carried
out in acetic acid solvent system. Of the solvents
investigated, only in the acetic acid system did the
dimethylsalicylhydrazone display basic properties
Attempts to analyze monomethylhydrazine in mixture
with hydrazine and with 1 , 1 -dimethylhydrazine were
unsuccessful. The hydrazine- 1,1 -dimethylhydrazine
mixtures were analyzed within an average difference
of 0.24 and 0.30 percent . Water (computed as the
difference between 100 percent and the sum of hydra-
zine percentages) was determined within an average
difference of 0.26 percent. The method is simple
and can be used successfully by untrained personnel
using a minimum of equipment . (Author)
Army Ballistic Missile Agency, Redstone. Arsenal,
Ala.
STUDIES ON U-C«TA. by Wilbur A*. Riehl. 7 Oa 60,
49p. 5 refs. Rept. no. RP-TR-2-6(): AD-245 021.
Order from LC nii$3. 30, ph$7. 80 PB 155 085
This report released for sale to the public 27 Mar 61 .
U-Deta is a term used by the Army Ballistic Missile
Agency to denote a special liquid mixture of 60% (by
weight) Unsymmetrical Dimethylhydrazine (UDMH) in
Diethylene Triamine (DETA). Copper, brass, cad-
miuin and zinc were found to xeaa with U-DETA.
Tests indicated that cadmium or zinc plated hardware
could be used far short-time exposure to U-DETA
vapors, but not for liquid contact. Silicone rubber,
type AMS 3305, was found the most nearly satisfaaory
elastomer in preliminary trials. A butyl rubber com- j
pounded by ABMA has been found even better . Tests
indicated that an air blanket is probably satisfaaory
for temporary storage or pressurizing of nxisaile fuel
Unk9, but a nitrogen blanket is advisable for long
term storage and reduces the flanrunability hazard.
Autoignition temperature is comparatively high, 270OC.
in air. Charts of specific gravity and viscosity of
U-DETA as a funaion of composition are presented.
Decontamination of equipment after contaa with
U-DETA can be accomplished chemically by Chlorox.
For large tanks, draining the liquid and decontamina-
tion with dilute acetic acid (vinegar) is recommended.
(Author)
755
Linle, Arthur p. , Inc., Cambridge, Masa^
INVESTIGATION OF PARAMETERS AFFECTING
AIRCRAFT AND MISSILE FUEL FILTRATION. Repc.
or Petroleum Servicing and Handling Equipment, Con-
traa AF 33(616)6386 68p. WADD Technical
rept 60-263; AO- 243 251.
Order from LC tu$3. 90, ph$10. 80 PB 155 256
Thia report released for sale to the public 31 Mar 61 .
A study was AMe at parameters which affect fil-
ter/separators. The work was directed toward the
development at standard procedurea (or evaluation d
such equipment Information was obtained on the effect
at qualified fuel additives on water separation, varia-
bles affecting coalescence at dispersed water, and
variables affecting solids removal . Standard teat
methods and procedures are proposed for various
aspects of filter /separator evaluation including: (l)a
standard three -camiponent particulate contaminant
having both hydrophillc and hydrophobic fractions, (2)
a method at ctispersing contaminant to its ultimate
particle size involving vacuum degassing and subee-
cpjent treatment In a Waring Blender, (3) a method at
injecting contaminant into the test facility, (4) a method
of sampling fuel streams and analyzing for concentra
tion of particblate maner by passing the sample stream
directly through a Millipore Filter so that liquid sam-
ples need not be taken, (5) a method of sampling fuel
streams, and analyzing for amali amounts of water.
The method involves the use at a mutual solvem to
accomplish solution erf free water, a novel sample
transfer system, and a Karl Fischer titration in spe-
cial apparatus, (6) a highly refined keroaene as a
standard fuel. Cow interfacial teosioaa may be pro-
duced by using a particlar corroeion inhibitor additive,
and (7) a procedure for evaluation of filter /separation
equipment incorporating separate ruia for removal at
water and solids singly and in comNnatlon for both
high and low intttrfacial tenaioa fuels. (Audior)
Lockheed Alrctafi Corp. , Sunnyvale, Calif.
NITROGEN FLUORIC«S AND THEIR ORGANIC
DERIVATIVES. A LITERATURE REVIEW. byC J.
HoCman and R G. Neville. Technical rept. on Chem-
istry. Ai« 60, 3Sp. 98 refs. LMSD- 703005;
AD- 246 047.
Order from OTS $1 . 00 PB 171 252
The study of tiqutd and solid rocket propellaixs has
stimulated widespread interest in compounds contain-
iog nitrogen-fluorine bonds. The reasons for this in-
terest are twofold. First, the N-F bond is at kw en-
ergy and easily broken. Second, N-F compoiaida pro-
vide an alternative source of fluorine, obviating the
neceaaity of handling the element itaelf . Apart from
its importance to rocket technology, the subject is at
interest in its c^n right since the chemistry at N-P
compounds is conpar stive ly new, the moat significant
advances having, been made during the past decade.
This review covers only binary inorganic N-F com-
pounds and organic compounds containing N-P bonds.
The literature covered has been critically reviewed
from 1928, the date of discovery at nitrogen trifluo-
ride, the first N-F compound, to September 1960.
(Author)
Propulsion Lab. , Wright Air Development Oiv. ,
Wright -Patterson APB. Ohia
PROPERTIES OF JP-4 JET FUEL, by James C Henry.
Rept. on Contract AP 33(616)5677. Jan 60. 24p. WADD
TR 60-57, AO-238 922.
Order from LC mi$2. 70, ph$4. 80 PB 155 083
TMs report released for sale to the public 24 Mar 61.
Statistics on the properties of JP-4 purchased by the
Air Force were compiled and are presented in this
report. A cursory aaalyais of these statistics was coa-
ducted by determining the maximum, minimum and
mean values and by constructing frequency distributioo
curves. (Author)
Rock Island Arsenal Lab. . III.
DEVELOPMENT AND EVALUATION OP CERTAIN
ECTERS FOR USE AS LUBRICANTS, by S. Fred
Calhoun. Rept. no. 9 on Greases. Automotive and
Artillery. 25 Sep 53. 39p. 31 refa. RIA Lab.
no. 53-3762.
Order from LC mi|3.00. pii)6.30 PB 155 082
This report released for sale to the public 27 Mar 61.
Thirteen esters of pelargonic acid, three at citric, and
one at succinic have been prepared and evaluated in
this Investigation. Their identity has been estabUshed
by means at molecular weights, molecular refraaions,
and parachora. Theii; viscosities, viscosity indices,
pour points, flash and fire points, ASTM slopes, re-
fractive indices, specific gravities, and evaporatioa
rates have been determined. Their lubrlcadve char-
acteristics were evalxiated by nteans of the Shell Four
Ball, the Falex Load Bearing, and Cincinnati Stick
sup Testers. (Author)
Pkisltcs
Naval Or(hiance Lab. , ,White Oak, Md.
DIFFERENTIAL THERMAL ANALYSIS OF POLY-
EPOXIDES, by Hugh C Anderson 31 Aug 59. 17p.
NAVORD rept. 6675; AO-232 010.
Order from LC mi$2.40. ph$3. 30 PB 154 721
Differential thermal analyses (DTA) have been per-
formed on several typical polyepoxides, having differ-
ent chemical struaures. Both the uncatalyzed snd
catalyzed epoxides were subjeaed to DTA The DTA
curves sre seen to be quite characteristic at the dif-
ferent systems. It is shown how the rate of heating,
the concentratjoo of the curing agent and the extent of
cure can alter the DTA curve for a particular system.
It is slso shown that the shapes and positions at the
DTA peaks are dependent on the epoidde. as well as
on the curing agent. The DTA determinations, in
conjunction with ultimate percentage weight loss of the
santplea. gave a qualitative picture of the relative re-
activltlea, as well as of the thermal staUUties of the
various sy«ems. (Author)
7S*
Iitoval Ordnance Lab. , White Oak, Md.
EXPERIMENTAL BEHAVIOR OF REINFORCED
PLASTICS SURFACES IN CONTACT WITH HOT
GASES, by H. A. Perry, H. C. Anderson, and P. A.
Mlhalow. 16 Nov 59, 25p. 5 refs. NAVORD rept.
6244; AD- 232 445.
Order from LC ml$2. 70, ph%4. 80 PB 154 719
TWi report describes recent experiments formeasur
ing the thermal diffusivity, thermal conductivity,
(tensity, and heats of pyrolysis of reinforced plastics
iBKler conditions of ablation. Two methods are recom-
mended for further study - a method for determining
the steady- state ablation rate and apparent thermal
diffusivity profile in one-dimensional, constant heat
flow, and a method for detcro'. .ning the weight- loss
rate and apparent specific heat of pyrolizable ma-
terials at very high heating rates. Means are set
forth for calculating the thermal conductivity profile
from the data obtained from these twomethoids.
(Author)
Naval Ordnance Lab. , White Oak, Md.
THERMOGRAVIMETRIC ANALYSIS OF THE PYROL-
YSIS CHARACTERISTICS OF POLYMERS, by Hug^ C.
Anderson. 3 June 60, 17p. 14 refs. NAVORD
rept. 6774; AD- 249 196.
Order from OTS $0. 50 PB 171 685
The pyrolysis charaaeristics of Teflon, ix)lyvinyl
chloride, polyester, epoxy, and silicone were studied
by thermogravimetric analysis. Percentage weight
loss curves and kinetic data were reconcilable to the
basic chemical structures of the polymer. The spe-
cific rate data for Teflon were in good agreement with
literature values obulned by other methods. The
mechanism of pyrolysis probably consists of (1) initia-
tion by random splitting of a C-C bond to form a pair
of free radicals, (2) deipropagation by stepwise ejec-
tion at monomer molecules from the radical ends, and
(3) termination by blmolecular reaaion of the radicals
Polyvinyl chloride decomposed in 2 distinct steps, th«
splitting out of HCl by a free radical mechanism, and
the cross-linking of the conjugated unsaturated struc-
tures followed by chain scission. A one-step decom-
position was noted for a polyester in the 300-to-400-
degree C region. The silicone polymer decomposed
gradually. The ultimate weight loss was only 60^ for
the silicone as compared to 100% for the other
polymers. (Author)
Wttertown Arsenal Labs. , Mass.
THERMAL CONDUCTIVITY OF TEFLON, KEL-F,
AND DUROID 5600 AT ELEVATED TEMPERA-
TURES, by A. W. SchultzandA. K. Wong. Mar 58,
22p. 15 refs. Technical rept. WAL TR 397/10.
Order from LC mi$2. 70, ph$4. 80 PB 155 572
This report released for sale to the public 19 Apr 61 .
The thermal conductivity values of the fluorocarbon
plastics. Teflon, Kel-F, and Duroid 5600, were deter-
mined at mean specimen temperatures ranging from
•pproxlmately 1850F to their respective gel-points.
Measurements were obtained utilizing a comparative
method technique based on unidirectional steady -state
heat-flow theory. The materials under investigation
were of commercial quality and were annealed prior to
testing to insure dimensional stability. For the range
of temperatures within which the materials were in-
vestigated, it was found that Teflon consistently ex-
hibited higher values than Kel-F and lower values than
Duroid 5600. At 350°F, the thermal conductivities ob-
tained were: Teflon - 2.37 BTU/hr/ft^/op/in. ;
Kel-F - 1.72 BTU/hr/ft2/OF/ln. ; Duroid 5600 - 3.58
BTU/hr/ft^/Op/in. The thermal conductivities were
found to increase with increasing temperatures .
(Author)
Rubber and Elastomers
Burke Research Co. , Pompano Beach. Fla.
DEVELOPMENT OF OZONE RESISTANT POLYMERS
WITH LOW HYSTERESIS, by F. C Bruce. BPHunt
and others. Rept. no. 11 (Final) for 18 Mar 58-
19 Sep 60 on Contract DA 20-018-ORD-17071.
1 Oct 60, 90p.
Order from OTS $2. 25 PB 171 578
Tests were made on 6 experimental tires with threads
of SBR latex to which vinylic filler was added. The
tires had lower thermal conductivity, lower power loss,
and higher abraision loss than tires with treads made
with conventional HAF carbon black fillers. TSwenty
additional experimental tires were constructed from a
combination of 35 parts vinylic filler and 25 parts
Dixie clay as a reinforcing material.
Burke Research Co. . Warren, Mich.
IMPROVED VINYLIC FILLERS FOR THE REIN-
FORCEMENT OF GR-S TYPE ELASTCMvIERS, by
O. W. Burke. Jr. . J. D Sharkey and others. Final
technical rept. for 24 May 57-18 Mar 58 on Contract
DA 20-01 8 -ORD- 18081. 15 July 58, 49p. 1 ref.
Order from OTS $1.25 PB 171 579
The work covered by the present report represents
advances made in developing good hot tensile proper-
ties, while maintaining low heat build-up. by surface-
treating the vinylic filler particles in latex form (pre-
pared with polymeric emulsifiers) to form vulcaniza-
tion accelerating groups or compounds on the surface
of the vinylic filler particle. The work of this repon,
therefore, should make possible the production of
vinylic filler-elastomer stocks for manufacture of
tires.
Institute of Rubber Research, U. of Akron, Ohio.
STUDY OF BALLOON LATICES, by Irja Piirma,
Vernon Allen and Howard Stephens . Final rept. tor
1 May 56-30 Apr 58 on Contract DA 36-039-sc-72339.
[1958] 94p. 15 refs. AD-201 159.
Order from LC mi$5.40. ph$15.30 PB 150 844
A study has been carried out on the effect of chemical
modifications of the structure of polychloroprene on
its low-temperature behavior. These modifications
have included the following: (1) Addition of thiols , (2)
Addition of thioacids , (3) Acrylate graft copolymeri-
zation , (4) Amine vulcanization . Tlie modified poly-
mers were subjected to one or more of the following
measurements: melting point, crystallization tate.
Temperature Retraction Test, Gehman Flex Test,
low -temperature elongation.
757
Inacttute at Rubber Research, U. al Akron, Ohio.
STUDY OF BAL»LOON LATICES, by Maurice Morton.
Supplement to final rept. for 1 May 56-30 Apr 5% on
Contract DA 36 ^039 -sc- 7 2339. 24 Feb 59. lOp.
AD- 212 889.
Order from LC
U$l
80. ph$1.80
PB 150 845
This supplementary report contains the test data re-
ceived from the Kaysam Corporation laboratories on a -
aeries ol experimental polychloroprene latex polymers
submitted by thi» laboratory during the Spring oi 1958.
These were obtained too late for inclusion in the Final
Report on this projea. The test data showed that all of
the polymers (which were subnrutted as cast films),
"froze" at -bCfC- This was quite surprising, since
previous tests h^d shown that similar nMterials, spe-
cifically the 60^. polychloroprene and thiol -modified
polychloroprene, had successfully withstood this tem-
perature, despiOe the fact that controls of standard
Neoprenes had npt. Hence, it is concluded that the last
aeries of tests vias entirely inconclusive, based on the
following factory: (a) Long storage time and no heat-
treatment of the dry films before testing, both favoring
the well-known (lardening of polychloroprene. (b) Ab-
sence of control I samples of commercial Neoprene
films. (See alsq PB 150 844)
W< KxJ and Paper
Aberdeen Proving
Coating and Oiemical Lab.
Ground, Md.
PRESERVATIVli TREATMENT OF WOOD FOR
COMBAT VEHICLES, by John P. Hill and Richard M.
Nichols. Rept. k>. 3. 20 Dec 60, 24p. 6 refs.
CCL ^99 I
Order from OT^ $0. 75 « 171 330
Seventy-five sirtulated truck floors were treated with
wood preservatives at controlled retention and maxi-
mum penetratioii. sixteen were pressure treated to
refusal, and fiv^ were untreated. These specimens
were finished with two coat finishing systems consist-
ing at a new experimental alkyd oil, olive drab wood
primer plus various topcoats. Early exposure results
indicate that boiti the controlled retention and maxi-
mum penetratiod treatment cycles and the experi-
mental primer (Jontribute to a substantial improve-
ment in outdoor {durability. Exposure results covering
three years wor^ on this project are alsodiscussed.
(Author) I
Material LabsJ . Puget Sound Naval Shipyard,
Bremerton, wish.
MARINE LAMINATING PROPEBTIES OF SELECTED
WOOD SPECIES, TRUE HICKORY (CARYA SPEQES)
UNTREATED AND TREATED WITH WATER-BORNE
PRESERVATIVES, by R. F. England and E. Stahl.
Dec 60. 30p. ujrefs. RkD final rept. E-412-8;
AD- 250 202. I
Order from LC bii$2. 7a ph$4. 80 PB 154 281
I
Full scale lamiiUted beams were employed in a study
of the laminatin* propenies of both untreated and
preservative treated hickory (Carya spp). Laminates
included boch short and long assetnhly periods using
three brands of resorclnol phenol adheslves. Accel-
erated delamination. block shear and outdoor exposure
tests showed hickory whether treated or untreated is
difficult to bond and will require development of spe-
cial laminating procedure. (Author)
Naval Civil Engineering Lab. , Pon Hueneme, Calif.
CHEMICAL CONSTITUENTS OF CREOSOTE, by
G. E. Sanford. I Feb 54, 30p. 32 refs. Technical
note N-176.
Order from LCmi$2. 70, ph$4. 80 PB 154 661
In accordance with a request for factual data leading
to the inhibiting of nwrine borers , a research pro-
gram on marine borer deterrents has been instituted.
This repon covers a literature survey made on the
physical and chemical properties of creosote, the
most common marine borer inhibitor now in use.
Creosote may be defined as: (1) A high -temperature
coal tar distillate. (2) A distillate that stans boiling
at about TOOPC and has at least a 125<>C continuous
boiling range. (3) The fractions boiling up to 315^0
contain at least 1 per cent tar acids (phenols and
homologs). (4) All fractions between 235°C and
3150C have a specific gravity of 1 .025 at 38^ com-
pared to water at 1 5. 5^0 , or greater. Chemically
creosote is a mixture of possibly thousands of com-
pounds . Some 220 of these compounds have been
identified and are shown in this report . The com-
pounds are predominantly aromatic , 90 per cent or
more, containing mainly hydrocarbons, phenols and
homology , and nitrogen bases . (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
PRELIMINARY STUDIES OF THE USE OF CON-
CRETE AS A JACKETING MATERIAL FOR TIMBER
PILES, by L. J. Walker. 19 Aug 52, 18p. 34 refs.
Technical note N-Ul.
Order from LC nu$2.40, ph$3.30 PB 154 650
This report considers the feasibility al rehabilitatioa
by jacketing the individual piles with concrete. The
cost at such work is dependent upon conditions at the
site and upon the method used: in actual practice the
cost has r^ged from $4.00 to $34.00 per lineal foot of
pile. The survey consists of two parts, namely: (a)
composition al the jacketing material, and (b) methods
of application of the jacket.
MATMEMATICS
Stanford
Applied Mathematica and Statistics Labs.
U. Calif.
CONSTRAINT QUALIFICATIONS IN MAXIMATION
PROBLEMS. II. by Kenneth J. Arrow and Hirofumi
Uzawa. Technical rept. no. 84 on Contract Nonr-
225(50). 23 May 60. 17p. 7 refs. AD- 237 455.
Order from LC mi$2.40, ph$3.30 PB 147 844
758
An Investigation of the interrelationship between varl -
oufl conditions under which the classical Lagrange
method remains valid for maximization problems sub-
jea to inequality constraints is considered. First, the
Kuhn-Tucker Constraint Qualification [Nonlinear Pro-
gramming, in J. Neyman (ed) Proceedings of the Sec-
ond Berkeley Symposium on Mathematical Statistics
and Probability. Berkeley and Los Angeles: University
of California Press; 483, 1951] is slightly weakened so
that the meaning of the qualification becomes more
straight -forward. The Lagrangian method is shown to
be applied to those constraint maxima for which the
present version of the Constraint Qualification is
satisfied. The Constraint Qualification in the present
formulation is also shown to be the weakest require-
ment for the Lagrange method to be applicable. If the
Lagrange method is justified for any dlfferentiable
maximand, then the constraint function is proved to
satisfy the Constraint Qualification provided the con-
straint set is convex. The Constraint Qualification is
shown to be implied by the condition that the constraint
functions corresponding to a certain set of indices are
convex. (Author)
Applied Mathematics and Statistics Labs. , Stanford
U., Calif.
AN IMPROVED CRITERION FOR TIGHTENED IN-
SPECTION UNDER THE DOUBLE SAMPLING PLANS
OF MIL-STD-IOSB. by BamaVd E. Smith. Technical
manual no. 2. on Contract N6onr- 251(26). 20 May 60.
lip. 1 ref.
Order from LC ml$2.40, ph$3.30 PB 148 782
This is addressed to the quality control man. the de-
sign engineer, the process engineer. All develop-
ment mathematics are omitted. Step-by-step instruc-
tions are provided to made these methods conven-
iently available for dally use.
Applied Mathematics and Statistics Labs . .
SunfordU.. Calif.
ON THE EIGENVALUES OF VIBRATING MEM-
BRANES [AND] TWO MORE INBQUAUTIES BE-
TWEEN PHYSICAL AND GEOMETRICAL QUANTI-
TIES. byG. P6lya. Technical rept. no. 88 on Con-
tract Nonr-225<ll). 9 May 60. 41p. 17 refs
AD- 237 925.
Order from LC mi$ 3.30, phj 7. 80 PB 148 420
Applied Mathematics and Sutistics Lab«. , Stanford
U., Calif.
ON THE STEADY- STATE SOLUTIONS OF THE
NAVIER- STOKES EQUATIONS, III, by Robert Finn.
Technical rept. no. 89 on Contract Nonr-225(ll).
20 June 60. 91p. 16 refs; AD- 240 087.
Order from LC mi$5. 40, ph$15. 30 PB 149 534
Tht relations are studied which connect a solution of
the Nivier- Stokes equations with the values achieved
hjr the solution on the boundary of the region of defi-
nition, and jRTlth the magnitudes of certain energy inte-
frtls which appear naturally In the theory. A bound
U ohuined for the Dirichlet Integral. The bounds on
the Dirichlet Integral are applied in order to obtain a
priori estimates on any possible solution and on its
first derivatives, depending only on prescribed dau.
An elementary proof is given that the solutions with
finite Dirichlet Integral are necessarily continuous at
infinity. The existence of a solution corresponding to
prescribed boundary data is proven. The manner in
which the solutions of the Navier- Stokes equations
transform into those of the Stokes equations are
studied as the prescribed data tend to zero. The
classical uniqueness theorem is Improved for suf-
ficiently small solutions in a finite region by showing
that this result can be given in an a priori formu-
lation, depending only on boundary data.
Applied Mathematics and Statistics Labs . ,
Stanford U., Calif.
OPTIMAL POUCY FOR DYNAMIC INVENTORY
PROCESS WITH NON- STATIONARY ^OCHASnC
DEMANDS, by D. Iglehart and S. Karlin. Technical
rept. no. 44 on Contract N6onr-25126. 6 June 60.
52p. 8 refs. AD- 240 159.
Order from LC mi$3. 60, 1^9.30 PB 149 558
A study is presented of an inventory model where the
demand is a stochastic process (called the demand
process) in which the distributions of demand in suc-
cessive periods are not identically distributed and,
in general, are correlated. A single commodity is
considered. A sequence of ordering decisions is
made at the beginning of each of a number of dis-
crete time intervals of equal length. The cumulative
demand in each period is a random variable whose
distribution chahges from period to period . A cost
structure is superimposed on this inventory model,
and an algorithm is developed for calculating the
critical numbers characterizing the optimal policy.
Three cost functions are incurred: an ordering cost,
a holding cost, and a shortage or penalty cost. The
computational algorithm involves solving recursively
for the unique root of k.' transcendental equations .
A similar algorithm for the case of time lags in de-
livery is also presented . Some numerical examples
are g^ven for the case k - 3 and special choices of
the cost factors . A proof of the optimality of the
ordering rule is then presented.
Applied Mathematics and Sutistics Labs . ,
Stanford U., Calif,
REGRESSION ANALYSIS OF CONTINUOUS PARAM-
ETER. TIME SERIES, by Emanuel Parzen. Technical
rept. no. 33 on Contract Nonr-225(2I). 27 June 60,
43p. 24 refs . AD-240 520.
Order from LC mi$3. 30, ph$7. 80 PB 149 750
The problem of regression analysis of time series is
treated, using Hilben space techniques , in a manner
which applies simultaneously to discrete and contin-
uous parameter time series . In order to extend the
practical usefulness of the approach to statistical
estimation via reproducing kernel inner products , the*
question is discussed of approximately evaluating the
reproducing kernel inner product corresponding to a
stationary (discrete or continuous jsarameter) time
series observed over a finite interval of time. An
approximate evaluation of the reproducing kernel
inner product is given which (1) provides a conveni^i
small sample expression for minimum variance
759
linear unbiased (^1a^kov) estimates of the mean value
function, (2) shows how to take account of estimates
of the spectrum of an observed stationary time series
in forming Markov estimates , and (3) shows clearly
when naive least squares estimate will coincide with
Markov estimates .
Brown U. Dlv. jof AppUed Mathematics,
Providence, R, I.
INDEPENDENCH AND DEPENDENCE, by M. Roeen-
blan. Technical rept. no. 1 on Coniraa Nonr-562(29>
June 60, 26p. larefs. AD- 240 Oil.
Order from LC inl$2.70, ph$4.80 PB 149 165
i
A stochastic prdcess Is used as a model in studying
the behavior of 4 random system through time. The
stochastic procdBS {xj), discrete in time
t « . . . . - 1 , 0, 1 , , . . , is considered. Attention is re-
stricted to processes that are stable through time,
i.e., stationary processes. For such processes, the
probabilities of events shifted through time remain the.
same. Limited results are presented and discussed
for the following problems: (1) reasonable notions al
asymptotic independence and what types of processes
satisfy them, and (2) charaaerization of those proc-
esses {xt] that ^n be constructed out erf independent
processes by a |iaiction and its shifts.
Columbia U. . 'itew York.
ON LINEAR ESTIMATION OF A SINGLE PARAME-
TER OF A MEAN FUNCTION UNDER SECOND
ORDER DISTURBANCE, by N. Donald Ylvisaker. Rept.
on Contract Nonr-266<59X [I960] 24p. 8 refs.
CU- 16-60; AD-2|34 445.
Order from LC lni$2. 70. phK 80 PB 154 098
The linear estimation d a single parameter is dis-
cussed where the loss function Is chosen to be squared
error. The formal properties al linear estimates are
considered as they arise in the Lj space, 1 - 2, as
Cauchy sequences over the observations. Methods are
employed which arise in the reproducing kernel space
representation ($ the processes and in the generalized
Integral equariof formulation. Pertinent theorems
from the theory of reproducing kernel spaces are
stated and a restriction is imposed on the general
problem to Insui-e a well-behaved structure. A lower
bound on the risk funalon al a linear estimate Is ob-
tained and a clais at problems which allow consistent
linear estimate) is characterized. Results concerning
imbiased linear estimates is considered. A method is
given for reducing the problem, under certain coo-
ditiontf, to the 9|olution of a generalized integral
equation. ,
Cornell Aeronautical Lab. . Inc. , Buffalo, N. Y.
THE NUMBER QF ORTHANTS IN n-SPACE INTER-
SECTED BY AH S-DIMENSIONAL SUBSPACE, by
Roger David Josieph and Louise Hay. Technical memo,
no. 8 on Project Para [Contract Nonr- 2381(00)] [1960]
12p. 4 refs. AD-236 735.
Order from LC mi$2.40, ph$3.30 PB 147 559
In Euclidean n-^pace, an orthant (generalized "quad-
rant") is a set qonsistlng of all points whose coordi-
nates agree in ^ga. An orthant is considered to be
an open set , that it , if a point has at least one coordi-
nate equal to zero, it will not be a member of any
orthant. The problem of how many orthams are inter'
sected by the space spanned by the r-t- 1 vectors is
shown to be equivalent to the problem: into how many
unbounded and how many bounded regions can r- space
be divided by n hyperplanes . An upper bound for the
number of orthants achievable is derived. The bound
is a least upper bound since there exist sets of r ♦■ 1
vectors whic^ do achieve this number of orthants .
(Author)
Dugway Proving Ground, Utah.
ON THE STRUCTURE OF HYDRODYNAMIC AND
ELECTRODYNAMIC FIELDS PART IL EHSTRI-
BUTION OF TTPE (b) SINGULARITIES IN THE EU-
CLIDEAN COMPLEX PLANfi, by Keith Leon McDonakl
May 60, 49p. 14 refs. Technical rept. 240.
Order from LC mi$3. 30. ph$7. 80 PB 148 212
The present work is a study al the topology al the two-
dimensional vector field of an analytic function of a
complex variable. There Is presented an analysis
treating on the existence and distribution of type (b)
singularities (stationary points), as defined in Part L
at {>oints of the Euclidean complex plane. Branch
points and branch cuts are also discussed. Vector
field structures in the neighborhoods of these points
are pictorial ly elucidated by means of figures showing
the orthogonal systems of conjugate u, v families of
curves. (Author) (See also PB 145 697)
EJectronics Reaearch Lab. , U. of California,
Berkeley.
TRANSFORM METHODS AND TIME -VARYING SYS-
TEMS, by W. H. Wattenburg. 23 Sep 60. 25p. 9 refs.
DER Series no. 60, issue no. 321; AD-246 766.
Order from LCmi$2. 70. ph$4. 80 PB 153 211
A method is given for defining a transform which will
be convenient for the solution of a given class of equa-
tions Miu(t) ■ f(t). where all operators Mi in the class
can be expressed as functions of some basic operator
L. The method is applicable to any well-defined op-
erator L. The transform T/ for a particular operator
L is defined in terms of a linear scalar product and
the eigenfunaions of the adjoint operator L*. Two
important properties erf any T/ transform are given.
The T^ transform is derived for the special cases
L -^ d/dt and L - t(d/dt) which results in the Laplace
transform and the Mellin transform, respectively. In
the applications the Ti transform Is also derived for
the operators Li » a(t) (d/dt) and L2 - (d/di) a(t)
where a(t) satisfies certain restrictions. Two ex-
amples involving time-varying systems are given as
illustrations of the use of these two transforms. Be-
cause of the relationships between the two transforms
and the Laplace transform it is shown that the solu-
tion of systems described by Li and L2 can be
carried out using only Laplace transform tables.
(Author)
fto
lostiaite for Fluid Oyiiamics and Applied Mathe-
matics , U . of Maryland . College Park .
AN ITERATIVE SOLUTION OF LARGE SCALE
SYSTEMS OF SIMULTANEOUS UNEAR EQUATIC»4S^
by Fred J. Bellar. Rept. on Contract AF 49(638)228.
May 60, Up. 3 refs . Technical note BN-211; AFOSR-
TN-60-550; AD- 237 435.
Order from LC mi$2. 40. ph$3. 30 PB 147 904
in algorithm proposed by Lanczos Q. Soc. Indust.
Appl. Math. , V. 6, no. 1 , Mar 58) for the generation
of an approxinrtate solution of a large scale system of
iimultaneous linear equations is improved so that the
number of iterations required for a desired degree of
accuracy IS minimized. (Author)
Institute of Plight Structures , Columbia U . ,
New York.
DISCONTINUITIES IN INTEGRAL-TRANSFORM SO-
LUTIONS, by Bruno A. Boley. Technical rept. no. 16
on Contract Nonr-266(20). May 60, 20p. 6 refs.
CU-16-60-ONR-266(20)-CE; AD-244 798.
Order from LC ml$2. 70, ph$4. 80 PB 150 994
Criteria are derived for the determination of the
magnitude and the location of discontinuities of solu-
tion in the form of definite integrals obuined by
means of Integral -transform techniques . The types
of integrals arising with the Fourier sine or cosine
transforms and those arising with the Laplace trans-
forms are considered. Applications of the theory
•rise in problems of wave propagation, where in-
terest is centered on the location of wave fronts and
the magnitude of Jumps. Two illustrative examples of
luch problems relating to Timoshenko beams are in-
cluded (Author)
Institute of Mathematical Sciences , New York U. .
N. Y.
OH THE FOUNDATIONS OF STATISTICAL INFER-
ENCE. I. BINARY EXPERIVENTS, by Allan
Birabaum. Rept. on Contract Nonr-285(38). May 60,
Mp. 5 refs . lMM-NYU-267. AD-239 063.
Order from LC mi|3. 90, phJlO. 80 PB 148 906
For experiments concerning two simple statistical
hypaheses, the canonical forms of experiments and
their panial ordering are discussed. Every experi-
ment is proved to be a mixture (in a probability sense)
of simple experiments whose sample spaces each con-
ain only two points . This result is used, with stand-
»rd frequency interprewtions of probabilities , in an
•ntlysis of the foundations of sutistical inference.
This analysis establishes the likelihood function as
the appropriate basis from which sutistical infer-
ences can be made directly, for informative
inference . For the numerical values of the likelihood
function, this analysis provides (iirect interpretations
in terms of probabilities of erroj-s . These probabili-
ties admit frequency interpretations of the usual kind ,
but they are not defined with reference to the specific
experiment from which an outcoirie is obtained: they
eipress intrinsic objective properiies of the llkell-
hootl function itself, which are shoWn to be relevant
•nd useful for informative inference. TTie relations
of the problems of informative inference to problems
of testing statistical hypotheses, d^ is ion -making,
conclusions , and Bayesian treatments of inference
problems are discussed. (Author)
Institute of Mathematical Sciences , New York U . .
N. Y.
TWO EXPOSITORY NOTES C*I STATISTICAL IN-
FERENCE: GENERAUZED MAXIMUM UKEUHOOD
METHODS WITH EXACT JUSTIFICATIONS ON TWO-
LEVELS: [and] CONFIDENCE CURVES: AN OMNI-
BUS TECHNICJUE FOR ESTIMATICW AND TESTING
STATISnCAL HYPOTHESES, by Allen Bimbaum.
Rept. on Contract Nonr- 285(38). May 60, 26p. 6 refs .
IMM NYU -269; AD-239 064.
Order from LC ntil$2. 70, ph$4. 80 PB 148 907
GENERALIZED MAXIMUM UKEUHOOD METHODS
WITH EXACT JUSTIFICATIONS ON TWO LEVELS:
The central positicm of the likelihood function is ex-
hibited as the objective basis for efficient statistical
inference. New practical techniques of statistical in-
ference are given. CONFIDENCE CURVES: AN OM-
NlflUS TECHNIQUE FOR ESTIMATION AND TEST-
ING STATISTICAL HYPOTHESES: A technique of es -
tlmation by confidence curves is described, which in-
corporates the techniques of testing along with those
of point estimation, and estimation by confidence
limits and confidence intervals at various levels .
Institute of Statistics , U . of North C:arollna ,
Chapel Hill .
THE CANONICAL CORRELATION OF FUNCTIONS
OF A RANDOM VECTOR, byE. J. Hannan. Rept.
on Contract Nonr- 855(09) . Apr 60, 17p. 7 refs.
Mimeograph series no. 250; AD-248 653.
Order from LCmi$2. 40. pti$3. 30 PB 154 088
The classical theory of canonical correlation is con-
cerned with a standard description of the relationship
between any linear combination of p random variables
X and any linear combination of q random variables y
insofar as this relation can be described in terms of
correlation. Lancaster extended this theory to in-
clude a description of the correlation of any functions
of X and y (which have finite variances) for a class of
joint distributions of x and y which is very general .
Lancaster's results are now derived in a fashion
which lends itself easily to generalizations to the case
where p and q are not finite . In the case of Gaussian .
stationary, processes this generalizaticm is equiva-
lent to the classical spectral theory and corresponds
to a canonical reduction of a (finite) sample of data
which is basic. The theory also then extends to any
number of processes . (Author)
Institute <rf Statistics, U. of North Carolina,
Chapel Hill.
A CENTRAL LIMIT THEOREM i?OR SYSTEMS OF
REGRESSICW, by E. J. Hannan. Rept. on Contract
Nonr -855(09). Mar 60, lOp. 8 refs. Mimeograph
series no. 247 AD-248 651.
Order from LC mi$1.80, ph$l.80 PB 154 123
The theory of regression on fixed variables, when the
residuals are generated by a stationary process, was
illuminated by the introduction of certain restrictions
on the r^ressor vectors. These restrictions are
designed to concentrate attention cm cases where
consistem estimates of the regression coefficients
exist and the asymptotic properties of these estimated
may be investigated by Fourier methods. The
761
restrictiODS are latisfied m most cases at regression
CO functiors of time as well as in cases where the
fixed variable is generated by some stationary
process fox whid> the sample serial correlatioiis coo-
verge with probal^ly one. Conditions are shown which
are (together witb certain restrictions on the nature
at the process goierating the residuals) sufficient to
ensure that the estimates at the regression coetflci-
encs are asymptcCically normal. (Author)
Institute of Siatiktics, U. ol hJorth Carolina, Chapel
Hill. 1
EFFiaENT FITTING OF LIh4EAR MODELS FOR
CONTINUOUS STATIONARY TIME SERIES FROM
DISCRETE DAT4, by James D^rbin. Rept. on Con-
tract Nonr-855(04). Mar 60, 16p. 14 refs. Mimeo-
graph series no 249; AD- 248 652.
Order from LC mi$2. 40. ph$3. 30 PB 154 124
Consideration is given to the problem ct estimating the
parameters of th# rational spectral density function of
a continuous process given in observations eq^ii-
spaced in time, f^ estimates are derived by assum-
ing the observations to be normally distributed. How-
ever, it must notjbe thought that the properties of the
estimates dependl critically on this assumption. If the
distribution is noti- normal, the estimation process
can be thought of as arising from a son of generalized
least -squares method. The joint distribution of the
equi- spaced observations is considered, and the rele-
vant parameters jaf this distribution is estimated first.
These are then converted to estimates of the param-
eters of the spectral density. The estimation of the
parameters of th^ underlyii^ stochastic differential -
equation model 14 also considered. (Author)
Institute of Statistics, U. of North Carolina. Chapel
Hill.
THE FITTING QF TIME-SERIES MODELS, by James
Durbin (U. of Lohdon). Rept. on Contract Nonr-
855(09). Dec59,'22p. 12 refs. Mimeograph series
no. 244; AD-230!528.
Order from LC i|il$2. 70, ph$4. 80 PB 154 094
Methods of efflcijent estimation of the parameters are
reviewed in som^ of the models commonly employed
in time- series analysis. The models considered are
the following: (1)1 the autoregresslve model, (2) re-
gression on fixe4 x's and lagged y's, (3) regression on
fixed x's with autoregresslve disturbances. (4) the
moving-average model, and (5) the autoregresslve
model with nrwvihg- average errors. (Author)
Institute of Te<h. , U. of Minnesota, Minneapolis.
ON THE DIFFEBENTIAHLITY OF FUNCTIONS OF
SEVERAL VARtABLES. by James Serrin. Rept. «n
Contraa AF 49(e.38)262. 20 Jan 61, 25p. 14 refs.
AFOSR-7; AD-2fcO 199.
Order from LC iniU- 70, ph$4. 80 PB 154 452
Let u :. u(x) - u(|ti Xq) be a real valued locaUy
summable funalon defined on an open region R of the
n dimensional number spaced". The differentiabiUty
of u is investigated when the gradient <rf the distribu-
tion associated frith u Is a measure. (Author)
Lincoln Lab., Mass. Inst. ofTech., Lexington.
A METHOD FOR LOCATING THE MAXIMUM OF A
FUNCTION OF A SINGLE VARIABLE IN THE PRES-
ENCE OF NOISE, by Richard C. Norrls. Rept. 00
Contract AF 19(604)7400. 20 Oct 60, 37p. 22G-0035.
Ordex from LC ml$3.00, Bh$6.30 PB 152 957
This paper considers method for locating the maxi-
mum at a function at one variable when additive noise
is present. The function in question is considered to
be a performance function which is unknown, ana^
method is desired which will not only yield the opti-
mum parameter setting in the limit, but will also
yield fast initial convergence toward the region of op-
timum perforinance. The noise is assumed to be su-
tionary and independent at the value at the function
parameter, and its variance is assumed to be unknown
but finite. The method discussed is one which
employs logical decisions rather than iterative tech-
niques in its operation. For functions with only one
nuiximum, a modified bisection method is used.
Points are evaluated nrwre than once, in general, in
order that averaging may be used to reduce noise
effeas and so that an estimate may be made at the
noise variance. Comparisons between the relative
magnitudes of measured points and the expected dif-
ferences due to noise alone (by means of the esti-
mated noise variance) determine the operation of the
logic. When it is assumed that the function has
more than one maximum, a search routine is used
to locate the region of the highest peak, and the
single maximum routine achieves convergence in the
limit. Since this method stores and utilizes the
magnitudes at previously measured points and does
not use slope measurements in its operation, it
very quickly limits itself almost exclusively to
regions of high return, and "remembers" poor areas
Tests were conducted using both the single maxi-
mum and muki- maximum routines and both exhibited
a fast rate initial convergence and showed a good
degree of convergence after many observations.
(Author)
Laboratory of Statistical Research, U. of
Washington, Seattle.
MULTIVARIATE CORRELAllON MODELS WITH
MIXED DISCRETE AND CONTINUOUS VARIABLES,
by 1 . Olkin (Stanford U .) and R. F . Tate (Michigan
State U.) Technical rept. no. 35 on Contract Nonr-
477(11). 12 May 60. 33p. 15 refs. AD- 237 643.
Order from LC nru$3.00, ph$6.30 PB 147 847
A model which frequently arises from experimenta-
tion in psychology is one which contains both discrete
and continuous variables , x and y. respectively.
Point-blserial correlation, which is the ordinary prod-
uct-moment correlation between x and y was used as
a measure of association. A multivariate extension
is considered, in which x« x*. i« 0,1 k, has «
multinomial distribution, ana the conditional distribu-
tion of y - yj , J ■ I p. for fixed x is multivariate
normal. For convenience of developnnent as well as
clarity, the following cases are considered sepja-
rately: (l)k=l,p>l. (2)k>l, p.l, and(3)k>l,
p>l.
LiBcobiLab. , Mass. Inst, of Tech. , Lexington.
THE SHORTEST PATH THROUOl MANY POINTS OF
A SET OF MMENSION a, by John R. Kinney. Rept.
onCtJOtraa AF 19(604)7400. 1 Dec 60, 7p. 5 refs,
55G-003a AD- 247 667.
Order from LC mi$1.80, ph$1.80 PB 153 486
Lockheed Aircraft Corp. , Sunnyvale, Calif.
A MULTIVARIATE k-POPULATION CLASSIFICATION
fROBLEM. by B. E. Ellison. Sep 60. 213p. 23 refs.
LMSD- 703006; AD-248 063.
Order from LC mi$9. 60, ph$33. 30 PB 154 349
Contents:
Formal problem, heuristic solutions and discussion
The principle of invarlance
Bayes procedures and admissibility
Invariant Bayes procedures
Normal a priori distributions
A priori distributions over hyperellipsoids
Consistency
Distance risk function rules
UnUasedness and the minimax f)roperty
Naval Ordnance Lab. . White Oak, Md.
TABLES OF THE INCOMPLETE GAMMA FUNCTION
OF INTEGRAL ORDER, by Robert Ryswlck and
George Weiss. 18 Nov 60, 49p. 3 refs. NAVWEPS
rept. 7292.
Order from OTS $1 . 25 PB 171 687
These tables contain values of the function
2
+ ■
G„(x)-e"''(l*x+-^ +■•• ^ij-j
for n. 0(1)5, x . 0(0.05) 13(0. 10) 20
n. 6(1)10 X. 0(0. 10) 5(0.05)20
n. 11(1)20 X. 0(0. 50) 5(0.10)20(0.05)50
The tables are given to 6 decimal places with a
possible error of one unit in the la.ax. place. (Author)
Naval School of Aviation Medicine, Pensacola, Fla.
A SIMPLIFIED METHOD FOR MACHINE CALCU-
LATION OF THE COMPONENTS USED IN THE
FORMULAS FOR BISERIAL AND PC«NT BISERIAL
CORRELATION COEFFiaENTS, by Woodbury
Johnson. 28 Jan 53, 7p. 1 ref . Rept. no.
NM 001 058.25.02.
Order from LC mi$1.80, pti$1.80 PB 155 087
This report released for sale to die public 27 Mar 61.
A flmplified method of obtaining the necessary com-
ponents for the formulas for biserial and point biserial
ooaffidents at correlation has as its major advantage
the fact that all components are generated during a
tingle run of the cards, and no summary punch is
Meded. Its prime limitation is that for efficiency it
i* restricted to two digit numbers in the variable.
(Audnr)
North Carolina U. (Chapel HiU]. '
MODIFIED SQUARE ROOT METHOD OF MATRIX
INVERSION, by Ahmed E. Sarhan. Eleanor Roberts,
and Bernard G. Greenberg. Technical rept. no. 3,
15 Jan-1 Feb 57. on Estimatlctn of Parameters of Dis-
tributions by Order Statistics, Contract DA 36-034-
ORD-2184. [1957] I4p. OOR prx)j. 1597; AD-121 716.
Order frtMn LC mi$2. 40. ph$3. 30 PB 155 088
This report released for sale to the puMlc 24 Mar 61.
The square root method of inverting a matrix involves
the determination of a triangular matrix, finding its
inverse, and multiplying the last two results to obtain
the final inverse. The present modification omits the
determination of the inverse of the triangular matrix
and proceeds directly from the triangular matrix itself
A more reliable check column is also furnished by
working backward from the sum erf the entries in the
TOWS rather than carrying a check column forward as
in conventional methods. (Author)
Princeton U. , N. J.
STATISTICAL PROJECTION. AN INVESTIGATION
OF THE ROLE OF ORTHOGONAL PROJECTORS IN
REGRESSICW THEORY, by S. N. Afriat. Rept. on
Contract [Nonr- 1858(16)]. 10 June 60, 78p. 24 refs.
Econometric Research Program Research Menu>.
no. 16; AD- 238 786.
Order from LC miK 50, ph$12. 30 PB 148 748
The following topics are discussed: factors and
measurement, experiment, components, span, pro-
jectors, orthogonality, incidence, orthogonal inci-
dence. Inclination, inclusion, im itat ion and dependence,
configuration coefficients, parallelipiped volumes,
multivariance, projection and r^resslon, principal
reduction, reciprocal and reflexive directions, proper
angles, reciprocal vectors, rank and multiplicity,
orthogonality relations, Isogonality, total reduction,
analysis at configuration, normal form, sutlonary
variation, canonical statistical analysis, oblique pro-
jections, split orthogonal projectors, multiply spilt
projectors, partial regression. Inversion and par-
tition, experimenul uniformity and mean values,
multiple regressions, multiple configurations, limits
at association, distribution characteristics, orthogo-
nallzatlon. Intersection, canonical pairs of bases, In-
version and partition, quadratic decomposition, sepa-
ration and Inclusion, determinantal inequalities, dis-
sociation, and a generalization in Hilben space.
Radiation Lab. , Johns Hopkins U. , Baltimore. Md.
DERIVATIVES. ZEROS, AND OTHER DATA PER-
TAINING TO MATHIEU FUNCTIONS, by MarcU J
King and James C Wlltse. Rept. on Contract
AF 33(616)3374. Dec 58, 85p. 5 refs. Technical rept.
no. AF-57; AD- 211 303.
Order from LC mi$4. 8a ph$13. 80 PB 154 961
This report released for sale to the public 28 Mar 61.
762
763
Values and graphs are tabulat«d for the first deriva-
tives of the pericxlic Mathieu functions (SeJ^(8, v) and
So^(8. v)] and th« radial N4athieu functions of the first,
second, and thinJ kinds. [Jen(8. u). JOn(8. u). Nen(8.u).
h4o;,(8. u), He(l)| (s, u) and Ho(l)* (s. u)] for orders
zero, one, and flwo. and for \^rlou8 positive and/or
negative values trf the parameter s. Tables of the first
and second zeros of the radial functions, ]e^(s. u) and
JOn(8, u). and th« first zeros of the first derivatives of
these functions f re also included. In addition. cupniB
and data for the periodic functions Se2(s. v) and -
So2(s, v) are given for various negative real values of
the parameter s
Radiation Lab. , Johns Hopkins I' , Baltimore, Md
VALUES OP THE MATHIEU FUNCTIONS, by James
C. Wiltse and M»rcia J. King. Rept. on Contract
AF 33(616)3374 Aug 58, 88p. 6 refs. Technical rept.
no. AF-53; AD-201 524.
Order from LC |nij4. 80. ph$13. 80 PB 154 960
This report released for sale to the public 28 Mar 61.
This report contains tabulated values aad curves for
some of the Mathieu functions. Included are the peri-
odic Mathieu funaions Sen(s. v) and SOn(6. v) for inte-
ger orders 0 < r< < 2 and various positive and negative
real values of the parameter s. Also Included are the
radial Mathieu functions Jen(s. u), Jo^Cs, u), NCpCs. u),
and Non(8. u) with s positive real, and He0)(8, u) and
Ho(l)(8, u) with » negative real, f or 0 < n integer)
< 2 and 0 ^ u ^2| in each case.
<u <_2Ji
Rutgers State U . , New Brunswick, N.J.
ON THE DISTRIBUTION OF FIRST SIGNIFICANT
DIGITS, by Rogfr Pinkham. Repc. on Contract
Nonr-404(16) [1$60] Up. 12 refs. AD-238 529.
Order from LC ^2.40. ph$ 3. 30 PB 148 561
This paper is a theoretical discussion of why and to
what extent this |So called "abnormal law" must hold .
The only distribution for first significant digits which
is invariant und^r scale change of the underlying dis-
tribution is logip(n* 1). Contrary to suspicion this Is
a non-trivial mathematical result, for the variable
n is discrete. '
Virginia Agricultural Experiment Station,
Blacksburg.
THE DEVELOPMENT OF STATISTICAL METHODS
FOR EXPERIMENTAL DESIGNS IN QUALITY CON-
TROL AND SUtVEILLANCE TESTING, by
R. A. Bradley, R. J. Freund and others. Summary
rept. for period! ending 30 June 60 on Contract Nonr-
2352(01). 30Jun(e60, 12p. 33 refs.
Order fr«n LC ml$2. 40, ph$3. 30 PB 148 535
A list of technlckl reports and puUicatlons.
Wayne State U.! , Detroit, Mich.
ABSTRACT HOMOTOPY THEORY, by Srfjsstlan S.
Koh. Technical jKXe no. 11 on Contract AF 49(638)179.
Dec 60, 2l3p. 6|ref8. AFOSR TN-60-1223;
AD- 250 732.
A detailed exposition of the abstract homotopy theory
Is given in terms of complete seml-simpllcial com-
plexes satisfying an extension condition. (Author)
Wayne State U , Detroit, Mich.
STATISTICAL DEVELOPMENTS IN UFE TESTING,
by Benjamin Epstein. Technical repts. 1-5, 1 June 57-
2 Apr 59. on Contract Nonr- 21 63(00). 2 Apr 59. 359p.
79 refs. AD- 155 353.
Order from OTS $5. 00 .. . PB 171 580
Contents:
Tests for the validity of the assumption that the under-
lying distribution of life is exponential
The exponential distribution and its role in life testing
Testing of hypotheses
Problems ot estimation
(Superseded Technical reports 1-5, PB 134 345,
PB 140 703, PB 144 401, PB 145 341. PB 150 725)
Order from LC
iii$9.6a ph$33.30
PB 154 456
Computing Devices
Benson- Lehner Corp. , Santa Monica, Calif.
THE DESIGN AND DEVELOPMENT OF AN
(AN/APD-4 FILM EDITOR) READOUT REDUNDANCY
REDUCER, QRC-60(T), by Arthur R. Bergen. Rept.
on Contraa AF 30(602)1784. 25 June 59, 23p.
RADC-TR-59-142: AD- 227 460.
Order from LC mi$2.70, phJ4.80 PB 150 909
The design and development is reported at a film
editor used to simplify the recognition and annotation
erf trace data occurring at periodic intervals on 35nun
AN/APD-4 film, and to provide a visual readout erf
the time separation between two events. Traces are
annotated with an alpha-numeric or binary code with
175 combinations and can be edited at the rate at
15-30 points per minute. The film is advanced in
incremental steps, the length at which can be set to
correspond to the distance between traces. The error
in the incremental step is less than . 0025 in. or one
part in 2(XX) whidiever is greater. A 4 digit display
provides a visual readout of the time separation be-
tween traces. (Author)
California U. , Los Angeles.
COMPUTER DESIGN USING INDEX ARITHMETIC, by
Avlezrl S. Fraenkel. Rept. on Contract Nonr -233(52).
May 60, Up. 9 refs. Dept. c< Engineering rept.
na 60-52: AD- 239 652.
Order from LC ml$2.40, ph$3.30 PB 149 138
A system in which the two numbers I, 2 entering a
multiplication are transformed into indices is consid-
ered. These indices are added in their own number
system. The sum, when converted back, gives the
product. Multiplication is replaced by the faster proc-
ess erf addition; a" may be computed by the single oper-
ation of multiplying the index of a by n. Using indices,
which are integers, the product is exact, which is net
generally true for logarithms. The difference of two
indices corresponds to the quotient only when the
latter is an integer. No easy way has been found for
performing division in other cases. Properties erf
indices corresponding to Mersenne Primes are derived
and used to save mechanization or storage require-
764
joeais for the conversion of numbers into Indices and
rtce versa. For a computer with a large word length,
itie required storage is still extensive. (Author)
David Taylor Model Basin, Washington, D. C.
PROBLEMS SOllVED ON HIGH-SPEED COMPUTING
BtJUIPMENT OF THE APPLIED MATHEMATICS
LABORATORY, by H. Smith and L. Aaon. Jan 59,
68p. Rept. 1295.
Order from LC mi$3.90, phJlO.BO PB 155 578
Tlila report released for sale to the public 19 Apr 61 .
A toul of 118 problems have been programmed for
•olutlon on hi^- speed calculating equipment. These
problems fall into two general categories: naval
eogtneering, and management data analysis. This re-
port contains a complete list and brief description of
these problems. It is made available in the hope that
mne of the programs developed may be applicable
directly or adapted to the solution of other problems.
Digiul Computer Lab., Mass. Inst, of Tech. .
Cambridge.
INFORMATION SORTING IN THE APPUCATION OF
ELECTRONIC DIGITAL COMPUTERS TO BUSINESS
OPERATIONS, by Harold H. Seward. Rept. on Proj.
Whirlwind, Contract AF 19(122)458. 24 May 54, 68p.
21 refs. Rept. R-232; AD-35 462.
Order from LC mi$3. 90, ph$10. 80 PB 155 376
This report released for sale to the public 10 Apr 61 .
Treatment is given of both digital sorting and sorting
by merging. In the majority of cases, sorting may be
achieved most economically with punched-card ma-
chines or magnetic -tape devices. In a system incor-
porating a general -purpose computing element, it is
generally faster and more economical to use special-
purpose sorting equipment. For applications involving
large amounts of information and requiring rapid
sorting, high-speed, high-density photographic stor-
age may be praaical. However, the processing time
of the photographic medium should not be more than
several seconds, and the information should be of
such volume that the medium -processing time is not
significantly large in comparison with the total read-
record time .
Directorate of Advanced Systems Tech. , Wright Air
Development Div. , Wright -Patterson Air Force Base,
Ohio.
BIONICS SYMPOSIUM HELD IN DAYTON, OHIO,
13-15 SEPTEMBER 1960, by Joan C. Robinette, ed.
Rept. on Living Prototypes, the Key to New Technol-
ogy. Dec 60, 489p. 373 refs. WADD Technical
rept. 60-600.
Order from OTS $6.00 PB 171 258
The introductory session discusses the background
from which bionics arose, the military and general
need, attitudes toward intelligent machines (a major
produa of bionics) and a survey of current research on
Uvlng prototypes . The four technical aessions deal
with current work in stages successively closer to
practical devices. This begins with logic derived from
the contemplation of neurones but applicable to the de-
sign of electronic networks of increased capacity and
reliability. It continues with discussion of theories,
devices, and techniques based on or simulating visual
and auditory perceptual processes . The final tech-
nical session contains five papers on the mechaniza-
tion of higher functions, such as learning, self-pro-
gramming, pattern recognition, decision making, and
heuristic programs. The report concludes with dis-
cussions of the potential value of bionics, its present
status, procedural methods and difficulties, and
possible social consequences. (Author)
Hermes Electronics Co. , Cambridge, Mass.
IMPROVEMENT OF ELECTRONIC C«^1PUTER RE-
LIABILITY THROUGH THE USE OF REDUNDANCY,
by J. Tlerney and R. Wasserman. Rept. on Contract
Nonr -21 33(00). 15 Apr 60, 38p. 2 refs. Publication
#M-828: AD- 236 453.
Order from LC mi$3. 00, ph$6. 30 PB 154 087
Within certain reasonable bounds, the use of redundant
elements uninterrupted complex digital systems can
Improve reliability substantially. In particular, a
"majority" typfe of redundant design can Improve the
reliability of a logical net under certSin reasonable
physical restrictions. The digital systems to which
this paper is directed operate under the following con-
ditions: (1) Operating interval is sufficiently long or
the system is so complex that the probability of suc-
cessful operation is less than that called for by the ap-
plication. (2) The system is unserviceable during the
pertinent time interval for economic, physical, or
strategic reasons. (3) Equipment cost and size are of
secondary design importance (although order oi mag-
nitude increases are certainly undesirable). (Author)
bitemational Business Machines Corp. , Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW-I). VOLUME I:
THE PHOTOSCOPIC MEMORY SYSTEM. Final rept.
on Contract AF 30(602)1823. 20 June 59, reprfaited
29 Aug 60. 31p. RADC-TR-59-llO; AD-220 201.
Orxler from LC mi$3. 00, ph$6. 30 PB 150 086-1
This report released for sale to the public 31 Mar 61.
An initial working system for translating Russian to
English utilizes a large capacity photoscopic memory
with fast access time as the primary tool. The re-
quirements for real-time translation of Russian
technical literature are discussed and the degree is
indicated to which the present, or Mark I, system is
capable of meeting these. The overall operation of
this system is described stressing the logic of the
search procedure and other design features of the
memory which make the system workable. Since the
translating power of the memory depends upon the
dictionary information stored within it, the techniques
and devices for preparing this information and loading
it onto the storage disc are also described. A
summary is given at the work performed during the
contract period to bring the equipment to its present
operational level. (Author)
765
IntematloDal Business Machines Corp. , Yorktown
Heights, N. Y.
COMRJTER SET AN/GSQ-16 (XW-1). VOLUME IL
THE FILM MAIONG UNIT. Final rept. on Contract
AF 30(602)1828. 20 June 59, ISOp. RADC-TR-59-110:
AD- 220 202.
Order from LC p»i$8. 10. ph$27. 30 PB 150086-2
This report released for sale to the public 31 Mar 61.
The process at ^xxiverting information on paper or
magnetic tape requires a combination of electronic,
optical, and mechanical systems, each presenting
separate design problems. Parameters are derived
for the Individual systems and their relationship to the
overall system function is defined. The actual equip-
ment designed and constructed to embody these pa-
rameters are described In deuil. Instructions forad-
Justii^ and opeitating this equipment are also provided
and supplemented by pertinent mechanical and electri-
cal drawings, (^uthor) (See also PB 150 086-1)
faitemational BMsiness Machines Corp. , Yorktown
Heights. N. Y,
COMPUTER SET AN/GSQ-16 (XW-1). VOLUME ffl:
THE DISC MAKING UNIT. Final repc. on Contraa
AF 30(602)1823. 20 June 59, 126p. RADC-
TR-59-110; AI>220 203.
Order from LC kniJ6. 30, ph$19. 80 PB 150086-3
This report rel^sed for sale to the public 31 Mar 61.
The fllm-to-dlsf transfer process involves a con-
version of the information tracks to circular form and
a minification d approximately 55. Both film and disc
must be run sm^xxhly in synchronization to keep the
information maJks from varying in width as they are
laid down. Becaiuse d the smallness and density of
the spots, optical specifications are also extremely
stringent, as are those for processing the disc after
it is exposed. Requirements with regard to me-
chanics and optScs are defined in detail. The equip-
ment built to meet these requirements Is then de-
scribed and its performance discussed. Instructions
for making and processing a disc as well as for
maintaining the jsystem are included along with a set
0* pertinent me<Jhanical drawings. (Author) (See also
PB 150 086-2)
International business Machines Corp. , Yorktown
Heights, N. y1 _
CCMPUTER SET AN/GSQ- 16 (XW-1). VOLUME IV:
THE DISC READER. Final rept. on Contract
AF 30(602)18234 20 June 59. 181p. RADC-TR-59-110;
AD- 220 204.
Order from LC mi$8. 40, ph$28. 80 PB 150 086-4
This report released for sale to the public 31 Mar 61.
The general priiciples Involved in the use of a CRT
spot to scan iirfprmation densely stored in an
emulsion on a rotating glass disc are discussed at
length and follo»»ed by a description of the special
features of the pearch in the AN/GSQ-16 system. In
the system, th<S spot is focused by a lens which can be
moved trans veUsly across the information tracks.
This motion extends the apparent field of view of the
lens in the lateral dlreaion (and consequently the
amount of information that can be scanned) by an order
of magnitude. A track following servo system control!
boch the lens and the spot deflection. Signals pro-
duced in a photo-multiplier tube by passage of the
spot through the disc are recognized in a digit de-
tector and converted to binary form for use in the
comparator where they are matched against the coo-
tents of the iaput roister. Boch time response and
circuitry are explained in full and the error problem
is analyzed. (Author) (See also PB 150 086-3)
International Business Machines Corp. . Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW-1). VOLUME V:
THE SEARCH SYSTEM. Final rept. on Contract
AF 30(602)1823. 20 June 59, 285p. RADC-TR-59-110;
AD- 220 205.
Order from LC mi$ll. 10. ph$44. 10 PB150 086-5
This report released for sale to the public 31 Mar 61.
The search system consists of circuitry that controls
the flow of lexical information through the system and
the logical operation of the disc reader. A computer
set, which is the main component of the system, coo-
tains the low and high speed electronics required to
accomplish the desired functions. The low speed cir-
cuits order the transfer of information upon oonunand
from the terminal devices and also provide for trans-
literation and format control. The main function of
the high speed system is to compare the informatioo
delivered by the disc reader with that stored in the
input register. Instructions are supplied to the disc
reader to direct the search until a match is detected;
upon a match, signals are generated to activate the
read-out circuitry. The logic is described through
which all the above functions are accomplished and
the electronics for carrying this logic out. Also de-
scribed are the pow^r supplies and the input-output
device insofar as these relate to the computer oper-
ation. A set of test instructions and pertinent sche-
matic drawii^s are included to assist in operation
and maintenance. (Author) (See also PB 150 086-4)
International Business Machines Corp. , Yorktown
Heights, N. Y.
COMPUTER SET AN/GSQ-16 (XW- 1). VOLUME VI:
INFORMATION COMNG AND FORMAT. Final rept.
on Contract AF 30(602)1823. 20 June 59. 66p. 1 refs.
RADC-TTl-59-110; AD- 220 206.
Order from LC mi$3. 90. ph$10. 80 PB 150 086r6
This report released for sale to the public 31 Mar 61.
The form and content of the store, with the form of in-
formation as it enters, passes through, and leaves die
translation system is discussed. All symbols and
codes used are described and located on the encoding
devices. The make-up of word list entries is next dis-
cussed, particularly as it re ates to the look-up
scheme. This scheme also requires that the entries
be ordered in a particular way, and the word list pro-
cessing required to achieve this order on the storage
disc is described. The conventions that govern infor-
mation transfer throughout the system are given and
766
followed by a description of the translation procedure.
(Author) (See also PB 150 086-5)
Lincoln Lab. . Mass . Inst, of Tech. . Lexington
DEVICE REQUIREMENTS FOR A LARGE CRYOSAB
liffMflRY. by R. C. Johnston. Rept. on Contract
AF 19(604)7400. 27 Dec 60 , 9p . 3 ref s . 53G-0051;
AD- 249 057.
0nlerfromLCmi$1.80, ph$l.80 PB 153 905
Lincoln Lab. , Mass. Inst, of Ttech. . Lexington.
WALLC«>S ISLAND PRELIMINARY PROCESSING
COMPUTER PROGRAMS, by S. M. Ornstein and R, J.
Saliga. Rept. on Contract AF 19(604)7400. 23 Jan 61.
lupersedes same of 13 Jan 60 and rev. #1 of 25 July 60,
2*). 3 refs. 21G-00O3. rev. #2; AD-250 959.
Order from LC mi$2. 70. phH 80 PB 154 587
A portion of the data processing system used to re-
duce Instrumentation data from the Wallops tracking
radar is described. Three dau acquisition systems,
(primary, backup, and teletype) are processed by the
7090 Computer in a manner which produces a standard
format IBM magnetic tape. This tape is then available
for such further processing as may be arranged by
odier groups. In addition, two preliminary output
systems, (printed output and plotted output) are de-
scribed which employ the standard format IBM tape as
an ioput and employ other programs to obtain print-
outs and plots . This instrumentation data and the set of
preliminary programs for reducing it has the code
name SPLAT. (Author)
National Bureau of Sundards, Boulder. Colo.
ISOPAR, A NEW AND IMPROVED SYMBOLIC C*n-
MEING ASSEMBLY ROUTINE FOR THE IBM 650, b>
H. Herbert Howe. 19 July 60, 112p. Technical note-
BO. 76.
Order from OTS $1. 50 PB 161 577
Naval Ordnaupe Test Station, China Lake. Calif.
COMPUTATION OF COMPLICATED COMBUSHON
E(JUIUBRIA ON HIGH-SPEED DIGITAL COMPUTER,
by D. S. Villars. Rept. for Sep 58-June 59 on Explora-
tory and Foundational Research in Chemistry
6 Nov 59. 29p. 3 refs. NOTS TP 2354; NAVORD
rept. 6611; AD- 230 716.
Order from LC ml$2. 70, ph$4. 80 PB 153 930
A reliable and rapid procedure of successive approxi-
mations is described which does not require any quan-
atitive estimates of final answers as input data, Cur-
rent values of concentrations are used to calculate all
equilibrium constants. That reaction showing greatest
fraaional discrepancy between calculated and given
equilibrium constant is seleaed by the program to be
computed on the assumption of negligible Interactions
with the other equilibria. The process is repeated
until the maximum discrepancy has been reduced to a
value less than an error specified as a parameter of
the problem. The program will accept any number of
reactions and species. A matrix nuuiipulatlon may be
made to check that the chemical equations are in
balance. The machine is then fed a list of chemical
equations to be considered for a particular problem.
It condenses the original matrix into a smaller working
matrix cohsiating of rows and columns corresponding
only to the actual elements and reactions and the actual
chemical species to be involved in that particular
problem. Speed of convergence is enhanced by trans-
forming the chemical equations to reaaioos of forma-
tion of the various species from components existing
at maximal concentrations at equilibrium. After
checking that a proposed set of components is tenable,
the program conducts the transformation to the new
set of chemical equations and obtains the correspond-
ing equilibrium consunts. The program is also
provided with a capability of computing enthalpies and
entropies of the individual species for given tempera-
tures and of the corresponding equilibrium mixture.
Stanford Electronics Labs. , Stanford U. . Calif.
NEURISTOR. by H. D Crane. Rept. on Contract
Nonr- 225(31). 16 Mar 60, lip. Technical rept. no.
1506-1' AD- 233 959.
Order from LC ml$2. 40, ph$3. 30 PB 153 785
A novel device and Its properties are hypothesized and
possible digiul systems employing it are briefly out-
lined. The .devices, termed Neuristors, may be us© 1
to synthesize all dlglul logic functions, so that any
digital logic system can be realized using arrays of
neuristors only. (Author)
Stanford Research Inst. . Menlo Park, Calif.
RESEARCH ON MULTI- APERTURE MAGNETIC
LOGIC DEVICES, by D . R . Bennion . Technical rept . 1
on Contract Nonr- 27 12(00). May 60, 95p. 13 refs.
SRI Proj. 2697; AD- 238 000.
Order from LC mi$5. 40, ph$15. 30 PB 148 231
Methods are presented for describing and measuring
the properties (static and dynamic) of magnetic ma-
terials, devices, and circuits. A new approach to the
development of practical switching models is intro-
duced, for use in the analysis of flux transfer in all-
magnetic circuits. Various means are discussed for
realizing an OR- NOR logic module with one or more
multl- aperture devices, alone or. in conjunction with
toroids. One such module makes use cf a pair of
PLUS- MINUS devices (components that can be wired
for either direct or complementary transfer of infor-
mation). A particular design for a device of this type
was singled out for more deulled study. Ultra-
sonically fabricated units were tested Individually and
in operating circuits. Drive current ranges of 15% to
45% were obuined for the various modes of operatloo.
The device design Is diagnosed and possibilities for
substantial Improvements are indicated. It is con-
cluded that this particular approach to all-magnetic
logic is a sound one. (Author)
767
MECHANICS
Brown U. EXv. jl Applied Mathematics, Providence,
R. L
NON-ANALYTid RELATIONS IN RHEOLOGY, by
William Prager. ; Technical rcpt. no. 55 on Contraa
Nonr-562(10). A^r 60. 15p. 14 refs. Cll-55;
AD- 235 042
Order from LC i|ii$2. 40. ph$3. 30 PB 154 120
Brown U. DIv. fcrf Applied Mathematics.
Providence, R. _
ON THE PLASTIC ANALYSIS OF SANDWICH
STRUCTURES, ky William Prager. Technical rept.
no. 57 or Contract Nonr- 562(10). Apr 60. 16p. 1 ref.
CI 1-57; AD- 235. 043.
Order from LC lDi$2. 40, ph$3. 30 PB 154 121
Brown U . Div . jof AppUed Mathematics . Providence,
R I
PROPAGATION bP A PLANE WAVE IN AN ISO-
TROPIC ELASTIC MATERIAL SUBJECTED TO PURE
HOMOGENEOUS DEFORMATION, by M. Hayes and
R S Rivlin. Technical rept. no. 62 on Contract
Nonr-562(10). May 60. I3p. 2 refs. CU-62:
AD- 239 007. «...oo,.
Order from LC Ui$2.40. ph$3. 30 PB 148 813
The theory of tl^ superposition of infinitesimal defor-
mations on finitf deformations in an isotropic elastic
material is analkrzed. This theory Is applied to the
study of the propagation of a plane wave of small am-
plitude in an infinite body of the material which is sub-
jected to a statit. pure homogeneous deformation. It
is seen that the (secular equation for the determination
of the square of' the velocity of propagation in a given
direction has three real eigen-values and correspond-
ingly three real mutually perpendicular eigen-direc-
tions . Provided' these three eigen-values are all posi-
tive, travelling waves may be propagated in the body
in the direction'considered with linear polarisations
along each of trtese eigen-directions . If one or more
of the eigen-values is negative for any direction of
propagation, the body is inherently unstable in the
state of pure h<*nogeneously deformation considered,
(Author)
Brown U. Div
at Engineering, Providence, R. L
PLASTIC AND VISCOUS DEFORMATION OF RE-
DUNDANT STRUCTURES. PROTOTYPES FOR A
GENERAL THEORY, by R Paul. Technical rept. no.
19 on Contract Honr-562(20). June 60. 64p. 20 refs.
Nonr-562(20)/lP; AD- 242 974.
Oder from Lp ral$3. 60. ph>?. 30 PB 150 739
LCji
A systematic n^ethod is presented for the analysis <rfa
wide class of rigid, strain -hardening structures, sub-
jected to arbitnarily prescribed independent loads.
The behavior d such struct\ires is described geomet-
rically by means at a yield polyhedron and associated
flow law in a suitably defined space d generalized
forces. The structures are prototypes for a very
general theory lof piece- wise linear plasticity. The
basic postulate* of the general theory are deduced. In
the case of the prototype structures, from extremely
simple assumptions. The relationship between the
theory expounded and that d the kinematic hardening
theory is discussed. A close analogy Is shown to exist
between the behavior at linearly vt«tai»- structures and
that 0* linearly strain -hardening structures. Non-
linear or piece-wise linear viscous structures are
shown to possess many features In common withanalo-
gous plastic structures. (Author)
Dlinois Inst, of Tech. [Chiogo]
BOUNDARY VALUE PROBLEMS IN PLASTICITY, by
Philip G. Hodge. Jr. Rept. on Contract Nonr- 140604.
Feb 60. 72p. 50 refs. DOM IIT rept. no. 1-10;
AD- 235 027. «..„.,.
Order from LC mi$4. 50. ph$12. 30 PB 153 124
The distinctive features at plasticity boundary value
problems are discussed. Detailed solutions are
given for a three- bar truss and a Circular plate to
Illustrate elastic effects, strain hardening, and geo-
metrical chaises. Problems in limit analysis of ro-
tatlonally symmetric shells under distributed and con-
centrated loads are considered. (Author)
Illinois U. . Urbana.
THE ENQNEERING BEHAVIOR OF STRUCTURAL
METALS UNDER SLOW AND RARD LOADING, by
J. M. Masaard and R. A. CoUina. Final technical
rept. on Contract Nonr- 1834(01). Oct 58. 218p.
41 refa. AD-210 240.
Order from LC mi$9. 60. ph$33. 30 PB 154 958
This report released for sale to the public 24 Mar 61.
An investigation was made of the behavior of a few
structural metals under a range of stress conditions
applied in times that correspond to the responses
which might be excited in ship structures by under-
water explosion or air blast loading, or in building
structures by earthquake shock or the explosion of a
large scale weapon. The engineering aspects of mate-
rial behavior are emphasized. The tests included uni-
axial stress applied in either tension or compression,
and flexural stress produced by third -point loading of
small beams of rectangular section. The rise times of
the loadings were varied from a few milliseconda to
several minutes. An attempt is made to correlate the
results obtained in the uniaxial stresa tests with dioae
obtained in flexure. The applicability of the resultt of
this investigation to the general problem of determin-
ing the behavior of structures under transient dynamic
loadings producing extensive inelastic deformations !•
discussed.
Naval Ordnance Lab. . White Oak. Md.
ELASnC AND PLA^HC STRESS EQUATIONS FOR
HOLLOW CYUNDERS AND SPHERES SUBJECTED
TO INTERNAL AND EXTERNAL PRESSURE, by
V C. D. Dawson. 4 Feb 60. 41p. 5 refs. Ballistica
research rept. 18; NAVORD rept. 6786.
Order from OTS $1.25 PB 171 684
The equations used to design high-pressure vessels,
both cyUndrlcal and spherical, are given. Where
stren^ requirements are not severe, the elastic
768
equations, together with the distortion energy theory
of failure, are used. For chambers having Idgh-
pressure requirements, it is necessary to resort to a
shrink fit or autofrettage construction. The equations
for these processes are derived herein. A short dis-
cussion of bursting strength of high-pressure cham-
bers is also included. (Author)
Naval Research Lab. . Washington. D. C
SHOCK SPECTRA AND DESIGN SHOCK SPECTRA.
byG. J. OHara. Interim rept. 12 Nov 59, 18p. 6 refs.
NRLrept. 5386.
Order from OTS $0. 50 PB 151 932
For some time workers in the field of mechanical
•hock have been plagued with difficulties when com-
bining sets of shock spectra to obtain curves which
might be used for design purposes. The reason for
this trouble is the present practice of using all points
on all the available shock speara when making a com-
binatorial analysis. A few simple examples have been
worked out which show that such an approach cannot
yield the proper design spectrum curve. These ex-
amples demonstrate that, because of interactions with
Donrlgld foundations, the values of interest in a shock
spectrum tend to he in the valleys of the plot rather
than upon the peaks, even when the natural frequency
of the foundation coincides with a natural frequency of
the syfttem as a whole. Thus an analysis based on the
envelope of a set of speara is not valid, since the high
values determine the envelope. (Author)
Aerodynamics and Pneumatics
Aeronautical Research Lab. , Wright Air Develop-
ment fDlv. 1 Wright- Patterson AFB, Ohio.
INCOMPRESSIBLE POTENTIAL FLOW ABOUT AXI-
ALLY SYMMETRIC DUCTED BOWES, by Phillip
Levine. Rept. on TXirbomachlnery Cascade Investi-
gations. Ai«57, 144p. 24 refs. WADC Technical note
57-287; AD- 130 967.
Order from LC ml$3. 60, ph$9. 30 PB 155 144
This report released for sale to the public 29 Mar 61.
The velocity potentials and stream functions for a
point source, doublet, ring source, ring doublet, disk
source, disk doublet, ring vortex and line source are
derived for die case at axlally symmetric incom-
pressible potential flow in an Infinitely long duct d
constant diameter. Methods for the development of
arbitrary body shapes in uniform ducted flow are pre-
sented. Several practical applications are indicated.
(Author)
Arnold Engineering Development Center fT^illahoma,
Tfenn. 1
HYPER VELOaTT ARC- TUNNEL INSTRUMEN-
TATION, by W. T. Earheart, Jr. and D S. ^num.
Rept. on ARO, Inc. Contract AF 40(600)800
S/A 11(60-110). Dec 60, 33p. 3 refs. AEDC
TN-60-227; AD- 247 564.
Order from LC ml$3. 00, ph$6. 30 PB 153 553
Instrumenwtion developments necessary to instru-
ment the arc discharge or hotshot type tunnels at the
AEDC are presented. Force, pressure, and heat
transfer measuring devices and systems, as well as
the complete data readout system, are discussed. A
three- component balance Is described. Also, a slx-
compooent balance system, currently under evalu-
ation, including techniques at calibration and dynamic
response on both balances, is presented. Both com-
mercially available transducers and those developed
at the AEDC are discussed along with the calibration
techniques. Heat transfer transducers capable o*
measuring heat transfer rates up to approximately
300 Btu/ft^/sec are discussed. A unique transient
heat transfer calibration device which employs an
oxy-acetylene torch as a heat source is presented.
Some at the problems encountered with the trans-
ducers specifically the zero drift of the variable re-
lucunce transducers resulting from the magnetic
field associated with the Hotshot 2 inductive power
supply, are discussed. (Author)
Bell Aircraft Corp. . Buffalo, N. Y.
A MANUAL FOR DETERMINING AERODYNAMIC
HEATING OF HIGH-SPEED AIRCRAFT VOLUME
I, by Richard J. H*rm«t Craig M. Schmidt andothers.
Rept. on Contract NOas 58-614-c. June 59. 292^.
73 refs. Rept. no. 7006-3352-001; AD- 229 434..
Order from LC mijll. 10, ph$45. 60 PB 154 215-1
This report released for sale to the public 28 Mar 61.
The importance of aerodynamic heating to the design
at modem high speed aircraft has created the need for
a manual which provides a convenient and complete
source of information necessary for the prediction d
aerodynamic heating rates. The present report at-
tempts to satisfy this need and to present equations
and working curves useful for the designer. Where
possible the report has been prepared in such a form
that a large part of the analysis can be carried out in
a very routine manner. This report contains: (1) an
Introduction to and description of aerodyhamic heating,
(2) a cursory review of the history and present state-
of-the-art of aerodynamic heating methods (3) a
presentation of correlations between theory and ex-
periment, and (4) a discussion of many d the problem
areas that exist for practical aircraft designs, which
are not readily amenable to solution, together with
suggestions of how they might best be analyzed. The
emphasis is placed on methods d computing aerody-
namic heating rates although the relationship erf these
heating rates with structural temperatures is also
treated jn some deuil. Working curves were pre-
pared for velocities up to 30, 000 ft/sec and altitudes
to 300, 000 feet, with emphasis on the range 2000 Co
10, 000 ft/sec and sea level to 150, 000 feet. They
apply to flat plates at angle of attack and cones for
laminar and turbulent flow and to stagnation points d
spheres and swept cylinders. (Author)
Bell Aircraft Corp. , Buffalo, N. Y.
A MANUAL FOR DETERMINING AERODYNAMIC
HEATING OF HIGH-SPEED AIRCRAFT. VOLUME
II, by Richard S Bartle and Arnold J. Hanawalt. Rept.
on Contract NOas 58-614-c. June 59. 78p. 1 ref. Rept.
no. 7006-3352-001; AD-229 435.
Order from LC miK 50, ph$12. 30 PB 154 215-2
This report released for sale to the public 28 Mar 61.
769
Volume n present^ tables of equilibrium temperatures
for a flat plate, sptiere, and cylinder through a range
in altitude d sea l^vel to 100, 000 feet and a range In
Mach number of 1. 0 through 10. These tables are pre-
pared for several Values erf emlsslvlty, angle of attack
or sweep, and dismnce from the leading edge or di-
ameter. Also presented in this volume are transient
"thin" skin temperature curves for a flat plate at
constant flight conilitlons, namely, at altituded frcm
sea level to 100, 0(K) feet at 10, 000 foot intervals and
velocities from 3000 to 10, 000 ft/sec at 1000 ft/sec
intervals. The results are restricted to the 2-ft
station. i° angle cf attack, and an emissivity d 0. 9.
A method for applying these curves to determine
approximate temperatures for transient flight con-
ditions Is also presented herein. (Author) (See also
PB 154 215-1)
Convair, San Diefeo, Calif.
RESEARCH ON COAXIAL JET AIR MIXING, by
John W . Shue and Jbhn K . Stauffer . Final rept . ,
Phase I. on Contrafct Nonr- 2854(00). June 60, 27p.
10 refs . AD-242 997
Order from LC mi»2. 70, ph$4. 80 PB 150 866
An experimental research program on the subsonic
turbulent mixing o^ an unhealed free jet of air with
surrounding moving stream under imposed longitudi-
nal pressure gradients is presented. The program is
divided into three fhasesr (1) investigations of pre-
vious work performed in the field, including construc-
tion of the test set jup and the experimental develop-
ment of a mixing tdbe imposing a constant longitudinal
static pressure; {2\ experimental investigations to ob-
tain velocity, pressure, and turbulence parameters
which characterize this subsonic turbulent mixing:
and (3) experimental investigations to obtain the above
parameters for rw<| other mixing tubes , one imposing
an increasing pressure gradient, and the other im-
posing a decreasing pressure gradient. A mixing
tube configuration Imposing a constant longitudinal
static pressure ov^r a length of approximately 40
primary nozzle diaineters Pp« 0.70") was experi-
mentally developed. The primary nozzle is the
smaller driving jeti. This jet pump configuration has
an initial velocity ^tio, a 'Vs/Vp "0.0719 and a cal-
culated initial area! ratio, ^ * ^p/As = 0.0104 based
on experinnental results . The contour producing the
constant longitudinal static pressure exhibits a linear
area variation ove^ the mixing region. (Author)
Cornell Aerwaut^cal Lab. , Inc. , Buffalo, N. Y.
ON LOCAL FLAT-PLATE SIMILARITY IN THE
HYPERSONIC BOUlJDARY LAYER, by F. K. Moore.
Repc. on Contract Nonr -2653(00). June 60, 36p.
12 refs. Rept. no. AF-1285-A-2; AD-240 025.
Order from LC mi: 3. 00, ph$6. 30 PB 149 328
A study is made at Lees' local flat-plate similarity
rule for the hypersonic laminar boundary layer. This
rule is shown to bel exact under assumptions invoked in
the inviscid theory of hypersonic flow. From this
theoretical basis, a modified local flat-plate simi-
larity scheme is derived. Involving separate rules for
velocity and enthaliy profiles, and is compared with
exact similarity soiutions and with the existing theory
of hypersonic leading-edge interaction. (Author)
Flight and Engineering Test Group, Wright Air
Development DIv. , Wright -Patterson AFB, Ohio.
AN INVESTIGATION OF CONE- CYLINDER BODIES
IN THE STEADY STATE SPIN MODE AND MAGNUS
FORCE EFFECrrS ON A OONE-Cryi.INDER BODY,
by George W, Loptlen. Rept. on Contract
[AF] 29(600)1694. Ai« 60, 76p. 6 refs. WADD
Technical note 60-76.
Order from OTS $2. 00 PB 171 604
The aertxlynamic characteristics of cone-cylinders
In a steady-state spin are presented for angles -of-
attack from 45° to 135° and spin helix angles,
2V ( 12 ) ' '''°™ ^ *° ^- *^- ^' ""y given angle-of-
attack an increase of spin rate within the limits tested
did not increase drag. However, spinning may pro-
duce a high angle-of -attack, where high drag occurs.
Aerodynamic and Magnus force data are presented for
a rolling cone-cylinder at anglM-of-ajxack from 0°to
90° and surface speed ratios, -Jk (W^ from 0 to
0.20. Results indicate positive Magnus forces which
increase linearly for angles -of -attack up to about
40°. At angles greater than 40°, the Magnus force is
nonlinear and becomes negative for most Reynolds
numbers, with maximum negative Magnus force at
approximately R " 400,000. (Author)
Flight (Control Lab. , Wright Air Development Div. ,
Wright -Patterson AFB, Ohio.
AN ANALYTICAL METHOD FOR THE CLASSIFICA-
TION OF FLOW AREAS OF SUPERSONIC WINGS, by
Frank M Mallett. Aug 60, 109p. WA DC Technical
rept. 58-669; AD-247 248.
Order from OTS $2.50 PB 171 593
The application of digital computer methods to the cal-
culation of dynamic stability of supersonic aircraft
presents the problem of devising a method of comput-
ing certain aerodynamic characteristics of the wing or
tail alone. These characteristics are necessary in the
calculations of wing-body-tail combinations and are of
interest in other aspects of airplane design. An analy-
sis was made resulting in the complete numerical
classification of 4 basic types of wing planform, of the
geometrical cases in each type, and of the subcases
resulting from the various patterns of Mach lines
within the planform. These cases and subcases are
presented together with the analysis that determines
them. The analytical techniques can be employed in
the classification of other types of planforms. (Author)
General Electric Co. , Evendale, Ohio.
A HIGH TEMPERATURE TUNNEL USING PLASMA
GENERATORS, by J. F. Cassidy. F. Martinek and
M. L. Ghai. Rept on Contract AF(638)243. Dec 60.
46p 7 refs AFOSR TN-60-1412; AD 250 782.
Order from LC mi$3. 00, ph$6 30 PB 154 572
Experimental investigations developing a high temper-
ature heat transfer tunnel using a plasma generator
are described. Conventional and continuously oper-
ating wind tunnels have been limited to temperatures
below 35O0°F. The technological development, re-
sulting in a wind tunnel capable of continuous oper-
ation at temperatures as high as 8000°F, is presented.
770
Ihe discharge flow of a gas stabilized plasma gener-
ator was investigated with thermocouple probes and
photographic techniques such as schlleren systems,
ihadongraphs and high speed photography. "Die re-
sults indicated that the flow was unsteady and non-
uniform even though plenum chambers and a gas
itabllizing tunnel were used. Advances in arc gener-
ation technology eliminated the objectionable flow
characteristics and satisfactory temperature and ve-
locity profiles were obuined. Development of high
temperature sensing instrumentation was accomplished
by advancing the capabilities of refractory thermo-
couples where only wire calibrations had previously
been known. A probe system which will determine the
temperature and velocity profiles in a gas stream at
temperatures of 5100°F is presented. Also, various
techniques and results derived for calibrating com-
plete probes are presented and discussed. (Author)
Ludwlg, Gunther.
BOUNDARY LAYERS IN HYPERSCWIC FLOW AND
KINETIC THEORY OF MSSOCIATING GASES; by
CJunther Ludwig. Final technical repc part 1 for
1 June 59-30 Sep 60 on Contract DA 91-591-EUC-1148.
[1960] I50p. 54 refs. AD- 248 233.
Order from LC mi$7.20, ph$22.80 PB 153 658
Problems in hypersonic flow are considered. The
diermometer problem with radiation is treated for the
laminar flow around a blunt body. For numerical cal-
culations dissociation equilibrium is assumed and the
transport coefficients calculated by Hansen (NACA
Tteh Note no. 4150 and 4359; 1958) were used. At
high external temperatures and hig^ cooling rates the
empirical formula given by Fay and Riddel (J- Aero.
Sci. 25:73-85, 1958) for the heat transfer gives erro-
neous results if it Is applied to the radiation cooling
in hypersonic flow for extremely high velocities.
Prom a theoretical standpoint the theory of compress-
ible turbulent boundary layers is very unsatisfactory.
The more or less empirical basis is the Reynolds
analogy. Some critical remarks are given. TTie nor-
mal shock wave in a dissociating gas is coittidered.
With regard to the dissociated nonequilibriura state,
DO agreement is found with shock tube experiments.
Detailed calculations are given. The kinetic equations
(or the dissociated gas are given. They are the basis
for the calculation of the transport coefficients of dia-
tomic gases at high temperatures which is performed
using the results of Grossmann (Freie Universitat
Berlin, 1960) for the cross -seaion. A modified
Karmann-Pohlhausen method is given for the beat
transfer problem in hypersonic flow.
Massachusetts bist. of Ttech. , Cambridge.
APPARATUS FOR LECTURE DEMONSTRATIONS IN
AERODYNAMICS, by Erik Mollo-Christensen. Re-
search sponsored by ONR. June 60, 26p. Fluid Dy-
namics Research Group rept. no. 60-2; AD-240 656.
Order from LC ml$2. 70. ph$4. 80 PB 149 778
An apparatus used for lecture demonstrations of aero-
dynamic phenomena is described. It is built around a
slide projector and a.vacuum cleaner. In place of the
sliJde holder a duct is used, with a bellmouth on one
•ide and the vacuum hose on the other. Test sections
may be Inserted in the duct, and the flow around vari-
ous shapes projected on a screen by the slide projector.
Manometers, which are holes bored in the sides of the
test sections, display the pressure distribution.
(Author)
Mississippi State U- [State College].
THEORETICAL AND EXPERIMENTAL INVESTI-
GATION OF A HIGH PERFORMANCE JET PUMP
UTILIZING BOUNDARY LAYER CONTROL, by
William Graham Wells. Research rept. no. 30 on
Contract Nonr-978(01). 1 June 60, 37p. 11 rrfs;
AD- 238 294
Order from' LCmi$3. 00, ph$6. 30 PB 148 395
By examining the processes through which mixing
losses occur within a subsonic Jet pump, it was possi-
ble to apply boundary layer technology to improve in-
ternal aerodynamics. A peak efficiency of 41% was
attained as contrasted against conventional jet pumps
having less than 10%. The high performance jet
pump incorporates features to exploit the Improved
mixing which occurs in a favorable pressure gradient
and to overcome the adverse effect which is en-
countered during diffusion. A theoretical expression
is derived for ideal efficiency of mixing in a favorable
pressure gradient which shows agreement with ex-
perimental results. (Author)
Mississippi State U. [State College]
A UNIVERSAL DESCRIPTION OF TURBULENT
BOUNDARY LAYER PROFILES WITH OR WITHOUT
TRANSPIRATION, by Joseph Jenkins Cornish. IIL
Research rept. no. 29 on Contract Nonr-978(01).
1 June 60, 103p. 35 refs; AD- 238 068.
Order from LC mi J5. 70, ph$16. 80 PB 148 317
Seme of the fundamenUl laws governing the behavior of
turbulent boundary layers on smooth impervious
surfaces were combined and presented in the form of a
single parameter description of the turbulent profila,
utilizing two universal functions, .\ and"' , of the
relative height in the boundary layer. In the develop-
ment of this relation, an additional outer wall function
was included in the profile description. A relation be-
tween the skin friction coefficient and the boundary
layer Reynolds number was derived and expressed in
terms of the parameter, ^t^ This relation was ex-
tended to include the interdependence of the shape
parameter, H, and the limits Imposed upon this re-
lation by the laminar sub- layer were delineated. In
addition, the concepts used in the development of a
description of the profile on impervious surfaces
were extended to cases of transpiration at the
surfaces and a relation which describes transpiratioo
profiles was developed. (Author)
Naval Ordnance Lab. , White Oak, Md.
HIGH TEMPERATURE TESTING OF CERAMICS FOR
RE-ENTRY BODY APPLICATIONS, by F. J. Koubek
and A. R. Timmins. 12 June 59, 53p. 10 refs.
NAVORD rept. 6298; AD- 227 641.
Order from LC mlJ3. 60, ph$9. 30 PB 154 815
A number erf ceramic coatings were evaluated for pos-
sible application as thermal insulating coatings on heat
771
sink type-re-encr^ bcxlies. Heat shock and thermal in-
sulation charactei*istic8 were studied in an oxyacetyl-
ene test apparatus and in a supersonic hot air Jet. The
outstanding materials for the purpose were found to be
stabilized zirconit and fused silica because of their
ability to suppress the flow of heat and to resist
thermal destructi^. At heat fluxes of the order of
300-500 BTU/ft2/tec (80-135 cal/cm2/sec). siabUized
zirconia coatings, 20 to 40 mils (.5 - 10 mm) thick.
suppressed the tefnperature rise of a copper substrate
by a factor of 2 tol 3 when compared to an uncoated
■ubetrate. Simila^ results were produced by fused
silica. It was concluded that both stabilized zirconia
and fused silica would make excellent candidates for
further investigation as insulating, refractory coatings
for heat sink type re-entry bodies. (Author)
Naval Ordnance Lab. , White Oak, Md.
RANGE STUDIES OF BOUNDARY -LAYER TRANSI-
TION OF 8" HEKflSPHERE CYUNDERS, by
J. B JuainoandA^ A. CSiamberlin. 10 Mar 59, 18p.
6 refs. Ballistic Deaearch rept. 9; NAVORDrept. 6182;
AD- 225 874.
Order from LC in^$2. 40. pb$3. 30 PB 154 816
Firings were maqe in the aerodynamics range at the
Naval Ordnance Laboratory using 8-in. diam hemis-
phere cylinders t(> determine boundary- layer transi-
tion. The purpose of the program was to obtain ex-
perimental evidenpe of boimdary- layer transition on a
spherical nose at high Reynolds numbers and subsonic
Mach numbers. Tfhe velocities obtained were high sub-
sonic (M - 0. 8) and the Reynolds numbers were ap-
proximately 4 X 106. Boundary- layer transition was
observed from di»ea spark shadowgraph piaures.
The observed transition point varied from 52° to 106°
on the cylinder aa measured from the model geometric
stagnation point. The Reynolds number at transition
based on boundarf- layer momentum thickness varied
between 392 and 1J13S. (Author)
Polytechnic Inst^ of Brooklyn, N. Y.
AXIALLY SYMM8TR1C FREE MIXING WITH
SWIRL, by Mamq H. Steiger and Martin H. Bloom.
Technical rept. o$ Contract AF 33(616)7661 . Nov 60,
31p. 3 refs . PIBA|- rept. no. 628; ARL Technical
note 60-163; AD-?48 373.
Order from LCmt$3. 00, ph$6. 30 PB 153 848
The momentum litegral method is employed to investi-
gate the problem of laminar free ifiixing with nvader-
ste swir! NonsiiHilar solutions in closed form, for
incompressible and compressible flow are derived for
both the rwirling pake and Jet. It it shown that swirl
in the Jet decays «t a fatter rate than in the wake and
for both cases the^ swirl decay is faster than the de-
crease in steamwise velocity defect. An analysis by
which large swirl can be treated is given. (Author)
Princeton U. [N. J. ]
HYPERSONIC FLOW OVER CC»4ES, by Stanley A.
Berger. Rept. on iContract AF 49(638)465. Sep 60,
79p. 13 refs. Re^. 523; AFOSR TN-60-1214..
Order from LC m l$4. 50. ph$12. 30 PB 154 583
The Tkylor-Maccoll equation for the supersonic flow
of an ideal gas about a right circular cone with an
attached shock wave is solved for the two cases of
infinite and finite free stream Mach numbers. The
solution for the former is given in terms of an ex-
pansion in the limiting density ratio across the shock,
^X. and the solution to the latter in terms of a
double expansion In the actual density ratio, £ , and
5^ The results are compared with a Taylor series
solution to the Taylor-Maccoll equation and also with
the exact values of Kopal for air and Mueller for
helium. (Author)
Princeton U. , N. J.
AN INVESHGATION OF THE FLOW AROUND
SLENECR DELTA WINGS LEADING EDGE ^PARA-
TION, by Andrew J. Bergesen and James D. Porter.
Rept. onContraaNonr-1858(14). May 60, 98p.
16 refs. Rept. no. 510; AD-239 830.
Order from LC mi$5. 40, ph$15. 30 PB 149 214
*
A low speed investigation of the flow over aspea ratio
one delta wings of varying thickness was nruide to
better understand the relation between the vortices
produced by leading edge separation and the non-line-
arity 0* the lift curve. The formation and the position
of the vortex cores were determined by means of
smoke flow visualization techniques: Lift curves of
the models were obtained from the wind tunnel. It was
found that at the same angle of attack the vortex cores
moved outward on the wing as wing thickness in-
creased. Downstream of the trailing edge, the vortex
cores followed a helical path which is believed to be
related to the "vortex explosion" phenomenon. An
empirical equation was developed which predicts the
lift curves for sharp leading edged delta wings of
various thicknesses and of aspect ratios from one to
two. (^uthor)
Princeton U. [N. J.]
SELF-SIMILAR FLUIDS, by Myron S. Wecker and
Wallace D . Hayes .' Rept . on Contract AF 49(638)465 .
July 60, 16p. 4 refs . Rept. 528; AFOSR TN-60-894;
AD- 250 980. ^
Order from LC mi$2.40, ph$3.30 PB 154 582
Self-similarity is defined for a fluid medium, and
equations of state of the form f(p,v,T) F(S) are
found which are self-similar under various invariant
transformations of the equations of motion. The
Hugoniot relation is used to further restrict the equa-
tions of state; the resulting restriction is that F(S)
must be consunt if shock waves are present in a flow.
(Author)
Princeton U. , N. J.
SHOCK LOADING OF RECTANGULAR STRUCTURES,
by Walker Bleakney. Rept. on Contract N6orl-105,
T. O. 2. 10 Jan 52, 64p. 12 refs. Technical
rept. 11-11; AFSWP-140: ATI-163 038.
Order from LC mi$3.90. phJlO.80 PB 155 080
This report released for sale to the public 24 Mar 61.
The shock loading of two-dimensional reaangular
blocks has been investigated as a function of length to
772
height ratio, shock strength, and time after impaa. A
iliock pressure ratio erf about 1 . 95 was used for dif-
(raalon experiments on blocks having length: height
.1:8 (thin wall), 1:1, 3:1, and •:1 front and back (step
up and step down). In addition, the 1:1 block was
(tudied at shock strengths of 1. 26, 1.48, 3.05, and
Jr. 00. Pressure distributions are also given for these
tame strengths, and 1. 12, for the step up and step
down at times so early that signals from the corner
bave not yet reached a boundary, this case being
designated the «:•. A peaked shock having a pressure
ratio (rf 1 . 48 has been obuined in the shock tube, and
although the pressure drops only to about half of its
maximum value, effeas appear which are not pre-
diaed by straight -forward modification of flat -top
shock data. These include the rapid decrease of the
average pressure on the front face to a value below
the free stream pressure and the persistence of
average pressure on the back above that corresponding
to free air pressure. (Author)
Research Labs, for the Engineering Sciences, U. of
Virginia, Charlottesville.
LABORATORY INVESTIGATION OF THE BASIC
NATURE OF LOW DENSITY GAS FLOW AT HIGH
SPEEDS, by John E. Scott, Jr. and James E May.
Annual progress rept. for 1 Jan- 31 Dec 60 on Contract
NOrd-18211. Jan 61, 58p. 15 refs. Rept. no.
AST-4435-109-61U; AD- 249 523.
Order from LC mi$3. 60, ph|9. 30 PB 154 158
TTie primary objective of the research in rarefied gas
dynamics is to establish the mechanism by which reo-
mentian and energy are exchanged during the collision
cf the neutral molecules of a rarefied gas with a solid
lurface. A quantitative description of this process
will enable a more accurate prediction of the aerody-
namic drag and heat transfer associated with high
speed flight at high altitudes. An aerodynamic mo-
lecular beam source is under development, the ob-
jective of which is to provide a nearly isoenergetic
beam of neutral molecules of large Intensity. This
molecular beam system has been used with a differ-
ential ionization gauge detection system to establish
the properties and characteristics of the molecular
beam source. A complementary phase cf the molecu-
l«r beam research is concerned with the actual de-
termination of aerodynamic drag under low density
conditions. This phase makes use of a concentric
cylinder apparatus in which a curved Couette flow is
produced in the annulus between the cylinders. Em-
I*«sl$ hi this phase was placed on the proper in-
fcrpreution of Couette flow experiments at high
n*eds and low gas density. (Author)
Space Sciences Lab. , General Electric Co. ,
Philadelphia, Pa.
AEROTHERMODYNAMIC FEASIBIUTY OF GRAPH-
ITE FOR HYPERSONIC GUDE VEHICLES, by
S. M. Scala and E.J. Nolan. Rept. on Contract
AF 04(647)269. 2 Aug 60, 53p. 36 refs. Technical
Information Series i^pt. R60SD425; AD- 248 259.
Order from LC mi$3.60, ph$9.30 PB 153 693
^"•lytiial studies of transient heat transfer and sur-
'•ce oxidation are presented for a range of typical
glide vehicle re-entry trajectories . In particular, a
typical value of lift to drag ratio of 2.0, a flight time
of approximately two hours , and a range of values of
the wing loading parameter between 25 and 100 lb per
square ft were selected . The instantaneous heat
transfer, surface and back face temperature, and
rate of surface recession are determined, by using
represenutive properties of both commercial and
pyrolytic graphke. The peak temperature and the
total shape change at the leading edge are normalized
and correlated so that many combinations of aerody-
namic, geometric and structural factors can be eval-
uated systematically. It is concluded that due to its
excellent high temperature properties . and its rela-
tively low oxidation (ablation) rate , graphite may be
used today in designing the leading edges of the aero-
dynamic control surfaces erf hypersonic lifting
vehicles. (Author)
Space Sciences Lab. , General Electric Co. .
Philadelphia, Pa.
STEADY FLOW OVER A MAGNETIZED BODY IN A
FLUID OF LOW ELECTRICAL CONDUCTIVITY.
PART I GENERAL THEORY, by S. I. Pai. Aug 60,
41p. 3 refs . Technical Information Series R60SD417;
AD- 248 449.
Order from LC mi$3.30. ph*7.80 PB 153 692.
The fundamental equations of the steady flow over a
magnetized body in a fluid of low electrical conductiv-
ity were analyzed . The resultant equations are
applied to two special cases: (1) a thin body in a com-
pressible flow, and (2) a bluff body in an incompress-
ible flow. Finally the general formulas for the forces
and moments acting on the magnetized body in an
electrically cpnducting fluid flow are given. (Author)
H)rdrod)<namics, H)rdraulics, and Hydrostatics
Brown U. (Div. of Applied Mathematics] Providence,
R. I
WAVE PROPAGATION IN ELASnC TUBES FILLED
WITH BREAMING UQUID. PART I, by G. W. Mor-
fan. Technical rept. no. 1 on Contract Nonr-562(07).
1955) 15p. 5 refs. Rept. 562(07)/l; AD-51 344.
Order from LC nrU$2.40, ph$3.30 PB 154 862
This report released for sale to the public 24 Mar -61.
A study of M(N-gan and Klely (J. Acoust. Soc. Am. ,
Vol. 26, no. 3, p. 323, 1954) of the propagation of
pressure waves through liquid filled flexible tubes is
extended to the case in which a steady stream flows
through the tube. The analysis assumes the liquid is
Inviscid and that R/A< < 1, where R is the tube radius
and 2vX is the wavelength of the disturbance. Wave
velocities are determined for the special cases of
negligible wall inertia and of negligible Poisson's ratio,
and an approximate solution is given for the general
case. The analysis shows that when the fluid is invis-
cid and wall inertia is neglected, the wave velocity
through a system at rest is simply superposed on the
velocity of the steady stream. For negligible Poisson's
ratio the wave velocity through a system at rest also
superposes on the average stream velocity. The
analysis of the general case shows that the combined
773
influence d *all (nertia and Poisson'a ratio on the
wave velocity is 0( greater importance than the effect
due to wall inertia alone so that one cannoc, in general
take account of will inertia without including Poisson's
r«io.
D»vid Taylor K^xlel Basin [Washington, D. C. ]
EVALUATION OF THE STATIC YAWING STA-
NLlTf OF THE AN/SQS-22 SONAR VEHICLE WITH
THREE DIFFERENT TAIL CONFIGURATIONS, by
Samuel M. Y. Liim and Reece Folb. Jan 61, 16p.
4 refs. Rept. 1488; AD- 249 820. ^ ,,. ,^^
Order from LC i*l$2. 40, ph$3. 30 PB 154 165
The static yawini stability of the AN/SQS-22 sonar
body with three different tail configurations was de-
termined. Basinjtests indicate that one of the three
proposed corflgUraiions is statically stable, one mar-
ginally stable, and one unstable. Theoretical approxi-
mations at the yawing stability ijnd to confirm the ex-
perimental data. (Author)
David Taylor Mxlel Basin, Washington, D. C.
PROPULSION CHARACTERISTICS OF A SUBa '
MERGED MODE - AS AFFECTED BY REYNOLDS
NUMBER, by Joh i L. Beveridge. Dec 60, I6p. 4 refs.
Rept. 1454; AI>i49 053.
Order from LC ttu$2.40, ph$3.30 PB 153 919
Tbe results of »n experimental investigation on the
effect of Reynold! number on model propulsion tests
of a submerged body are presented. A propeller was
characterized in lopen-water and behind a 15-foot
submerged body tjf revolution. The influence of test
Reynolds number* on propeller thrust and torque is
determined and tlie results obtained are discussed.
Conclusions: In agreement with previous Model Basin
criteria, a criiioal Reynolds number of approximately
5 X 106 is indicated and recommended for use in con-
ducting open-waOEr propeller tests. In view of die
experimental thrust deduction and wake factors ob-
tained in this study, it appears reasonable to con-
clude that model, propulsion tests on submerged
streamlined bodijes -of -revolution should not be con-
ducted at Reynolds numbers which are lower than
the critical valu4 recommended for open-water
propeller tests. (Author)
Digital Compuier Lab . . U . of Illinois , Urbana .
SINGULAR SHOCK INTERSECTIONS IN PLANE
FLOW, by C. William Gear. Doctoral thesis. Rept.
on National Sciance Foundation Grant G-9503.
17 May 60. 92p 13 refs. Rept. no. 100; AD-238 376.
Older from LC mi$5.40. ph$15.30 PB 148 394
Contents: ~ . .-
Non-viscous flow
Analytic supersonic flow behind a siiock
A singular transformation of subsonic flow
Non-analytic shock attached to a straight wedge
Non-analytic shock attached to a curved wedge
The Lin and Rubinov solution
Subsonic pseudo-stationary flow
A general form of the solution for stationary and
pseudo-stationary flow
Viscous flow
The shock region in one dimension
Two dimensional shock regions . The modified
Rankine-Hugoniot equations
The slip stream region. The nKXlified matching
conditions
The intersection region in regular and Mach reflec-
tion
The shock configuration in Mach rrflection
Modificatigns for regular reflection
Hydrodynamics Lab. , Calif. Inst, of Tech. ,
Pasadena .
EVALUATION OF THE INTEGRALS OCCURRING IN
THE CAVITY THEORY OF PLESSET AND
SHAFFER, by Byrne Perry. Rept. on Contracts N6(tar
24420 and N6onr- 24424. Dec 52, 30p. 11 refs. Rept.
no. 21-11: AD-7616.
Order from LC mi$2.70, ph$4.80 PB 154 871
This repon released for sale to the public 24 Mar 61.
Formulas are presented from which the pressure dis-
tribution and the drag in 2 and 3 dimensions can be
calculated. The original tabulations of Plesset and
Shaffer for these parameters are considered adequate
for most applications; only a few terms were added
for small values of a parameter related to the cavita-
tion number. Approximations are discussed for low
cavitation numbers which may be used to extend the
ubulated results with reasonable accuracy
Instl^te of Engineering Research, U. of CalifomU,
PROPAGATION OF WAVES OVER AN OBSTACLE
DM WATER OF FINITE DEPTH, by T. Francis
Ogilvie. Rept. on Contract Nonr- 222(30). May 60,
92p. 10 refs. Series no. 82, issue no 14; AD-242 865.
Order from LC mi$5. 40, ph$15. 30 PB 150 624
The following situation is discussed: Consider a
channel of infinite horizontal extent with a uniform
fluid depth except in a finite region. The contour of
the bottom is specified by some function, y » b(x).
If sinusoidal waves are incident from the left, then,
as t -> o», there will be a reflected wave moving to-
ward the left and a transmitted wave moving toward
the right. Under appropriate conditions on b(x),
several results are proved: (1) the velocity potential
can be expanded In an asymptotic series In powers of
wave number, k^, valid as k^O; (2) as | x|-»<».
the potentUi varies slnusoldally with x, and this
asymptotic solution (in x) also has alii asymptotic ex-
pension In powers of k^; (3) tf the complete coef-
ficients of k" are required to satisfy the usual
boundary conditions and to have the behavior at | x (
—MD specified by the asymptotic expansion, then the
coefficients are uniquely described; and (4) the re-
flection and transmission coefficients can be ex-
pressed In terms of asymptotic series of powers of
kj^ The case of a bottom which is completely flat for
illx. Interrupted by a vertical barrier of vanishing
thickness, is considered. Curves are given for the
reflection coefficient as a function of wave number,
with (barrier helght)/(undisturbed water depth) as a
ptrameter.
Institute of Mathematical Sciences, New York U
N. Y.
ANALYTICAL THEORY OF TURBULENT CHF-
FUSION, by P. H. Roberts. Rept. on Contract
Nonr-285(33). June 60. 68p. 15 refs. Research Rept.
no. HSN-2; AD- 243 924.
Onler from LC mi$3. 90, phJIO. 80 PB 152 117
l&mlchnan(J. Fluid Mech. 5:497-543, 1959) pro-
pounded a theory of homogeneous turbulence, based
on a perturbation method, that leads to closed equa-
tions for the velocity covarlance. This method is ap-
plied to the theory of turbulent diffusion, and closed
equations are derived for the probability distributions
of the positions of marked fluid elements released In
■ turbulent flow. Two topics are discussed: (I) the
probability distribution, at time t, of the displace-
ment of an element from its initial position: and
(2) the Joint probability distribution of the displace-
ments of two fluid elements. Attention Is focused iqxm
the probability distribution of relative displacement.
(Author)
Johns Hopkins U. School of Engineering, Baltimore,
Md.
A LAMINAR PLANETARY JET, by Robert R. Long.
Technical rept. no. 9 on Contraa Nonr-248(3l).
Mtr 60, 18p. 7 ref; AD- 233 795.
Order from LC mi$2. 40. ph$3. 30 PB 153 783
A theory is developed of a jet In a rotating, viscous
fluid. It is suggested that it may be related to a Jet
obeerved in an experiment with a rotating spherical
«hell of liquid and, in addition, may partly explain the
existence of the sub-surface equatorial current in the
P«clfic Ocean. The fundamental physical idea is that
oft balance of vortidty brought into the jet by advec-
tlon and diffused by friction. The necessary approxi-
mations are borrowed from boundary layer theory.
The linear case is solved completely and Inferences
•bo« the non- linear jet are obtained by dimensional
"Moolng. (Author)
Michigan U. Coll. of Engineering, Ann Arbor.
CONTRIBUTIONS TO THE THEORY OF HYDRO-
DYNAMIC STABILITY, by L V. Schensted. Doctoral
thesis. Rept. on Contract Nonr-I224(I5). June 60,
118p. 15 refs. UMRI ProJ. 03114; AD-240 144
Order from LC ml$6. 00, ph$I8. 30 PB 148 951
Expansions theorems are Investigated with relate to
the expansion of arbitrary functions in terms of the
elgenfunctlons of the plane p>arallel flow stability
problem and those of the stability problem for the flow
through a circular pipe. Such expansions are shown to
be valid for functions which satisfy certain boundary
conditions and regularity conditions. Applications is
made of these expansion theorems to the solution of
the initial value problem, to the solution of theforced
oscillation problem, and to the non- linear problem.
The approximate location is given of some of the eigen-
values of the parallel flow stability problem and of the
stability problem for the flow through a circular pipe.
Rensselaer Polytechnic Inst., Troy, N. Y
THE SFABIUTY OF VISCOUS FLOW BETWEEN
ROTATING CYLINDERS WITH AN AXIAL FLOW, by
R. C. DiPrima. Rept. on Contract Nonr-591(06).
23 June 60, 26p. U refs; RPI MathRep no. 35;
AD- 239 764.
Order from LC mi$2.70, ph$4. 80 PB 149 210
The stability of a viscous fluid between two concentric
rotating cylinders with an axial flow is investigated.
It is assumed that the cylinders are rotating in the
same direction and that the spacing between the cylin-
ders is small. The critical Taylor number is com-
puted for small Reynolds number associated with the
axial flow. It is found that the critical Taylor number
increases with increasing Reynolds number. (Author)
METALLURGY
Climax Molybdenum Co. of Michigan, Detrcrft.
EFFECT OF THERMAL-MECHANICAL VARIABLES
ON THE PROPERTIES OF MOLYBDENUM ALLOYS,
by M. Semchyshen, Robert Q. Barr, and Gordon D.
McArdle. Rept. for 30 June 60 on Metallic Materials,
Contract AF 33(616)5447. Nov 60. I12p. 4 refs.
WADD Technical rept. 60-451 .
Order from OTS$ 2. 50 PB 171 597
Unalloyed molybdenum and the alloys, Mo-0. 50% Ti,
Mo-0. 059% Zr, and Mo-0. 49% Ti-0. 057% Zr, have
been studied from the standpoint of effect of fahrica-
tlort variables on mechanical properties and structural
stability. Strain hardening was accomplished either
by rolling or by forging. Working temperatures were
2200 and 3000 F . Molybdenum and the above-men-
tioned alloys were capable of being strain hardened
775
774
even at low redujtions by rolling or forging at 3000 F.
For any given set of deformatian variables, the high-
est strength properties and greatest resistance to re-
crystallization were consistently demonstrated by the
ternary alloy, MoO. 49% Ti-0.057% Zr. The role (rf
externally applieid stresses in influencing the recrys-
ullizaiion behavior of the materials under investiga-
tion was found td be quite complex. At least part <rf
the complexity of the problem as approached here re-
sulted from the jarge number of fabrication variables
that were inherent in the test specimens. Four new
experimemal alJpy compositions are discussed.
(Author)
Defense MetaW Informatioo Center. Battelle
Memoriallnst. , Columbus. Ohio.
BRAZING FOR IflGH-TEMFERATURE SERVICE, by
H E. PatteeawiR M. Evans. Rep<. on Contract
AF 33(616)7747. 21 Feb 61. 32p. 118 refs. DMIC
Order from CTSJ $1 . 00 PB 151 108
This report sumlnarizes many d the important devel-
opments in brazing for service temperatures in excess
trf 600 F. Heating methods, filler metals, atmos-
pheres, fluxes, and deoxidizing agents are discussed
as rtjey affect th^ brazing at heat-resistant mewls and
alloys. Some attention is given to specific brazing
appUcatioDS. (A|Uthar)
Defense Metal* Information Center, Baaelle
Memorial Inst; , Columbus, Ohio.
REVIEW OF CURRENT DATA CM^ THE TENSILE
PROPERTIES Of METALS AT VERY LOW TEM-
PERATURES, br J. E. Campbell. Rept. on Contract
AF 33(616)7747 14 Feb 61, 79p. 29 refs. DtMC
ChirfromOTi$2.00 PB 151107
This report reviews current data on the tensile prop-
erties of selected metals at temperatures down to
-423 F, the temperature d liquid hydrogen. (Author)
This memorandum deals with several forgeable
nickel -base, iron- base, and cobalt- base alloys d»at
have useful service temperatures in the range c*
1200 F to 1800 F. It does not cover the more widely
used alloys, such as A-286 or Inco 901, but Is limited
to the newer alloys that have higher useful service-
temperature raises. The review Is Intended to pro-
vide useful data on sizes, shapes, and mechanical
properties at superalloy forgings.
Institute of Engineering Research. U. d California.
Berkeley.
A STUDY OF THEORIES OF FRACTURE UNDER
COMBINED STRESSES, by I. Cornet and R. C Grassi.
Final rept. on Contract DA 04-200-ORD-171, T.O.IO.
Feb 58, 47p. 30 refs. Series no. 78, issue no. 2;
OOR proj. 1182; NP-6712; AD- 162 607.
Order from LC ml$3. 30. ph$7. 80 PB 155 153
This report released for sale to the public 29 Mar 61.
Included in this report is Physical significance of in-
variants of stress used in the theory of plasticity, by
V. V. Novozhilov. trans, of Prikladnaya Matematlka 1
Mekhanika (USSR) 1952, v. 16 (no. 5) p. 617-[6I9).
Brittle fraaure was investigated in specimens ranging
from relatively duaile nodular iron to brittle high-Si
cast iron. Tubular cast iron specimens were subjected
to internal pressure and axial tension or compression.
Axial loading of the specimens was accomplished by a
200, 000- lb testing machine. The experimental data
were compared with various fracture theories. Essen-
tialiy, the stress system may be related to, or formu-
lated in terms of, an average shearing stress acting on
an infinitesimal volume in the body of a soUd. Struc-
tural factors may be combined in terms of a notch con-
centration factor which is based on hypothetical and
fictitious cavities within and at the surface of the
material. Failure under combined stresses of brittle
materials can be predicted adequately by applying a
notch modified distortion energy criterion of J. C
Fisher (ASTM Bui. No. 181, April 1952)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Ohio.
SUPERALLOY, FORCINGS, by »-„^^,*^.^ ^JSpIkM
Boulger. [Rept, on Contract AF 33(616)77471. 10 Feb 61
41p. 19 refs. ^MIC memo. 86. «... -,.
Order from OtS ^. 50 PB 161 236
Northwestern U. , Evanston, Dl.
AN EXPERIMENT ON THE INFLUENCE OF AL-
LOYING ELEMENTS ON THE INTERNAL FRIC-
TION OF COLD WORKED AND QUENCHED
MARTENSITIC IRON AND STEEL, by T. Mura. J. Q
Brinaln. and L Tamura (Osaka U. ). Rept. on Con-
tract AF 49(638)780. 12 Jan 61. 14p. 18 refs. AFO«
rept. no. 115. ~, ,-.• jc«
.S5er from LC ml$2. 40, ph$3. 30 PB 154 453
Plain carbon steel in the cold worked or Martenslrtc
conditions has an internal friction peak at about 250^
at a frequency of 1 cps. The Influence of substitutional
alloyli* elements on this peak was examined experl-
mentaUy. "Die alloys which were vacuum melted Co-.
776
Cr-, Mo-, Nl- and Si- Iron (about 3% alloying ele-
ments), and carburized Si- iron were used as speci-
mens for the determination of internal friction versus
toaperature as measured by torsional pendulum
nielbod. The cold worked alloys had a peak at about
JSfiC which was much lower in the height than thato*
plain C-lron and steel. Carburized Si -iron in the
quenched condition had a peak which occurred at a
slightly lower peak temperature than in quenched plain
C-steel, but the height d the peak was substantially
greater than that found for the same alloy in the cold
worked condition. The activation energy of this peak
for martensitlc Si- steel was about 35 kcal/mol.
(Author)
Office of Technical Services, Dept. of CcMnmerce,
Washington, D. C.
HEAT TREATMENT OF METALS. Feb 61, 19p.
210 refs. OTS Selective Bibliography SB -454.
Order from OTS $0. 10 OTS SB-454
Lists PB reports, AEC reports, and translations added
to the OTS collection during period 1950 to February
1961. Reports include heat treatment of high strength
steels, government research on titanium alloys,
uranium -molybdenum alloys, zirconium alloys, and
other metals.
(Xflce of Ttechnlcal Services, Dept. d Commerce,
Washington. D. C.
HIGH TEMPERATURE METALLURGY AND HEAT
RESISTANT ALLOY& Feb 61, 36p. 674 refs. OTS
Selective Bibliography SB- 452.
Order from OTS $0. 10 OTS SB- 452
includes PB reports, ABC reports and translations
added to the OTS collection during period 1950 to
February 1961. Covers reports on general research
in this field as well as high temperature Intermetallic
compounds, alloys by powder metallurgy, brazing for
high temperature service and some reports on high
temperature metal coatings.
Powder Metallurgy Lab. . Stevens Inst, of Tech. ,
Hoboken, N. J.
EFFECTS OF REFRACTORY COMPOUND ADDI-
TIONS ON X-40 ALLOY PROCESSED BY POWDER
METALLURGY, by Edmund B. Wilson, Donald P.
Ferriss. and Gregory J. Comstock. Final rept. on
Cootraa NObs 72100. June 57, 45p. 7 refs;
AD-219 061.
Order from LC mi$3. 30, ph$7. 80 PB 154 537
The effects d minor additiooa of refractory compounds
on X-40 alloy fabricated by hot coining were deter-
mined. Strengthening phenomena found in alloys con-
taining additions of metallic diborides were shown to
be essentially independent d the meul associated with
4e boride and construed due to the boron in the com-
pound. The strengthening effect observed, required
thit both boron and carbon be present in the alloy.
The strengthening effect was uniform over a boron,
range of 0. 25% to 1 . 0%. Some indications of strength-
ening X-40 alloy by the addition of molybdenum
Aslllclde were obtained. (Author)
TRIAS, Inc.. Baltimore, Md.]
SYNTHETIC ALLOYS. byH. R. Peiffer. Final rept.
on Contract NOas 58-150-C. 1 Apr 59. 38p. 9 refs;
AD- 225 507.
Order from LC mi$3. 00. ph$6. 30 PB 154 536
Hard particles consisting of finely divided alumina,
thorla, and stainless steel in various concentrations
and particle sizes were added to an Al matrix. Alu-
mina was added to Ag matrix in a 1/10 volume ratio
and in particle sizes of 240 mesh, 400 mesh, and
Linde B. Cylindrical billets were formed by pressing
at 20 to 25 ton/sq in. , sintered f or 4 hr close to the
melting point of the matrix, and enruded at 1000^
(Al matrix) and 1100°F (Ag matrix). Tensile strengths
were determined at various temperatures from 25° to
850OF. Ductility values were obtained from elongation
and reduction -in -area measurements. Density deter-
minations of the various alloys were made with both a
Jolly balance and a laboratory scale. Conclusions
based on the experimental results include: (1) the
particle size of the dispersed phase can influence the
mechanical properties d a dispersed -phase alloy; (2)
the elastic properties of the dispersed phase influence
the properties of dispersion -hardened alloys; (3) the
rate of change of tensile strength with temperature is
influenced by microstructural variables; (4) the coher-
ency of the dispersed phase and the matrix affect the
strengthening of the structure; and (5) for the
Al - AI2O3 system, there is a certain critical tem-
perature at which the strength is the same regardless
of dispersed particle size or quantity. Above the
critical temperature, strengths again vary with the
dispersion distribution.
Watertown Arsenal Labs. , Mass.
DESULFURIZATION BY CALCIUM INOCULATION
IMPROVES PROPERTIES OF CA^ STEEL, by David
A. Colling and Paul j . Ahearn. Jan 61, 2lp. 9 refs.
Technical rept. no. WAL TR 311/45.
Order from OTS y). 75 PB 171 384
Steels with sulfur content as low as 0.001/0.002% were
produced in basic induction furnaces by iiHx:ulation
with Ca-Mn-Si combined with high slag basicity. The
effects of initial sulfur content, alloy elements, and
calcium additions for the desulfurization process were
assessed. Mechanical properties for low sulfur 4325
and 4340 steels show improved ductility and toughness
o^^er normal sulfur steels at the same strength level.
(Author)
Watervliet Arsenal [N. Y. ]
APPUCATION OF HIGH STRENGTH ALUMINUM
CASTINGS, by M. L. Slawsky and F. A. Heiser.
Oct 59, 22p. 9 refs. Rept. no. WVT RI 5904;
AD-231 098.
Order from OTS $0. 75 PB 171 564
The mechanical properties of aluminum castings can
be improved through careful contrc" yf foundry varia-
bles, particularly iron contamination, process varia-
tions and specialized heat treatment. These princi-
ples have been applied to the casting of two specific
ordnance components, namely, the sight bracket and
the yoke of the 81 mm Mortar. The processes utilized
777
in this investigaQion are the permanent mold technique;
employing an an^zed aluminum mold, and chilled
shell molding, employing aluminum chills to effect
localized rapid solidification. With the former, ten-
sile properties (* 47, 000 pal TS, 32, 400 psi YS and
7% elongation hatre been realized for the sight bracket
whereas with th^ laner properties of 44, 000 pel
tensile: 37,000 psi yield: 10% elongation have been
olxained in the yoke. In addition, through variations
in heat treatmei^, properties in excess at 60,000 psi
TS and 50, 000 y6, but with negligible ductility have
been possible. (Kuthor)
ijerrous Metals
Aeronautical Materials Lab. . Naval Air Material
Center. Philadelphia, Pa.
INTVESriGATlON OF CRACK PRC»>AGATION IN
HYDROGEN EMBRITTLED STEEL, by E. J Jankowsky
and W Beck. Rtpt. on ProJ. TED NAM AE 4110,
pt. 14. 28 Aug 3ft, 2Sp. 13 refs. Rept. no
NAMC-AML-AE|1102; AD-227 511.
Order from LC |il$2. 70. ph$4. 80 PB 150 780
i
In order to replace the notch tensile specimen used in
delayed failure testing, which in general requires a
stress rupture r^chioe, a C-ring was desigpied with a
shallow, sharp V notch. This specimen is stressed by
tightening a holl<iw bolt equipped with one or two strain
gages. Owing tot crack propagation, the restraining
load on the stressed embrittled notched C-ring de-
creases and thia produces a corresponding reduction
in bolt strain which is recorded by an oscillograph.
Time to cracking and rate of stress relief in the bolt,
controlled by ra^ of crack propagation in the ring are
determined frqni the oscillographic records. Compu-
tations at the notninal stress at the root at the notch
were based on tlie standard formula for bending stress
in a beam, corrected for specimen curvature, and on
the applied load> Delayed failure curves were re-
corded for plated notched C- rings and tensile bars,
respectively. Agreement between the stea()y state
stresses for bot^ type of test specimens is very good,
although notche*^ C-rings reach Uils stress in a much
shcnrter time tha^ notched tensi Im pec i mens. Fluo-
borate cadmium plated notched dfrings require a high
stress and a lon^ "incubation period"' before cracking
takes place. No incubation period can be observed for
either cyanide cadmium or chromium plated speci-
mens aiK) critical stresses are much lower (Author)
Cleveland Pneutnatic Tool Co. , Ohio.
EVALUATION Of FORCINGS OF INCO AND TM-2
STEELS AT HI^H- STRENGTH LEVELS; by
F. A. Matter, P. J. RagJaod, Jr., and
G. N. Barrett, JT. Rept. on Metals and Metallic Ma-
terials, Contract AF 33(616)376. Dec 54, 49p. 2 refs.
WADC Technical rept. 54-587; AD-63 620.
Order from LC ^$3.30, ph$7.8e PB 154 870
This report reie|ised for sale to the public 24 Mar 61.
Two potential aifcraft structural steels known com-
mercially as Inc^ Steel and TM-2 Steel were evaluated
using specimenS|Cut from large forged sections.
While the test r^ults covers only one s.trength level
in each range, tie data indicate that Inco Steel in the
290.000 - 310,001) psi range and TM-2 in the 200,000-
220,000 psi and t20,000 - 240,000 psi ranges would
probably be adequate for aircraft structural com-
ponents. The Inco Steel in the 240,000 - 260,000 psi
range I9 too brittle for use as an aircraft structural
material. Good flash bun wddmeitts can be made with
Inco Steel. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Colunibus, Ohio.
THE FACTORS INFLUENQNG THE FRACTURE
CHARACTERISnCS OF HIGH-STRENGTH STEEL.
byC. W. Marschall. Rept. on Contract
AF 33(616)7747. 6 Feb 61, 4^. 30 refs. CMIC
rept. 147.
Order from OTS$ 1.25 PB 151 106
National Bureau of Standards, Washington, D. C
A STUDY OF EMBRITTLEMENT OF HIGH
STRENGTH STEELS BY THE HYDROGEN ISOTOPES,
by Gwendolyn B. Wood and Abner Brenner. Rept. for
July 58-July 60 on Contract AF 33(616)58-18. Dec 60.
55p. 4 refs. ARL Technical rept. 60-309; AD- 250 257
Order from OTS $1. 50 PB 171 253
Deuterium embrittled 4130 steel, but 10 a much
smaller extent than did hydrogen. On the other hand,
specimens embrittled in solutions made with heavy
water contained a larger volume of gas (deuterium)
than specimens similarly treated for the same length
of time in an ordinary water solution.
Naval Research Lab. , Washington, D. C.
PRELIMINARY OBSERVATICWS ON THE EFFEC-
TIVENESS OF HEAT TREATMENT FOR THE RE-
COVERY OF PROPERTIES OF IRRADIATED
STEELS, by J. R. Hawthorne and L. E. Steele. In-
terim rept. 16 Feb 61. I6p. 3 refs. NRLrept. 5582.
Order from OTS >0. 50 PB 171188
Investigations on the effects of neutron radiation on
steels used in nuclear -reactor construction have re-
vealed that under certain exposure conditions the
notch-duaility properties 0* these materials may be
severely deteriorated. In seeking a method for re-
storing the initial material properties by a means
within reactor operational capabilities, the possibility
of using postirradiation heat treatment is being ex-
amined. Prehminary investigations have been com-
pleted on the relationships of annealing time and tem-
perature to recovery and on the resultant effect of
other experimental variables, such as the total neutror
exposure and the material composition. Initial obser-
vations indicate that heat treatment is effective in re-
covery of notch-ductility properties of irradiated ma-
terials, the extent of recovery being strongly depend-
ent upon Irradiation temperature. (Author)
(North Carolina State Coll. , Raleigh].
AN INVESnGATION OF THE EFFECTS OF THE
TERNARY CARBIDE, FejAlC, ON THE MECHANI-
CAL PROPERTIES OF CERTAIN I RON- ALUMINUM-
CARBON ALLOYS, by Jerry M. Waller. Master's
thesis. [Rept. on Contract DA 36-034-ORD-2766]
[i960] 38p. 60 refs. Rept. 2215.14-Met. AD-239 436.
Order from LC ml$3.00, phJ6.30 PB 153 673
The following specific conclusions within the composi-
778 3
don range tested are enumerated: (1) increased ter-
nary carbide quantity tends to provide the alloy with
l)etter mechanical properties at elevated tempera-
ture; (2) the ordering in the iron-aluminum-carbon
ailoys with compositions near the ideal composition,
peSAl, promotes embrittlement in the alloy; (3) tem-
peratures above lOOOop (538°C) are excessive for re-
taining a reasonable ponion of the room temperature
tensile strength; and (4) ternary carbide quantity
within the two-phase region of the iron-aluminum-
carbon ternary system may be controlled by control-
lii^ the carbon content . (Author)
Light Metals
bttelle Memorial Inst. , Columbus, Ohio.
DEVELOPMENT OF IMPROVED METHODS FOR
OCyLD EXTRUSION OF TITANIUM, by A. M. Sabroff,
R. A. Sannicandro and others. Pinal engineering repc.
for 11 Sep 56-11 Sep 57 on Contract 33(600)33540.
11 Oct 57, 96p. 8 refs; AD- 156 541.
Onter from LC ml$5. 40, ph$15. 30 PB 155 150
This report released for sale to the public 29 Mar 61.
The applicability was investigated at the cold-ex-
trusion process for producing shapes of commercially
pure and alloyed TI that simulate parts used in engine
and aircraft construction. Studies at die design, sur-
face coatings, and lubricants, in which 1 1/2- in. -diam
billets at unalloyed Tl were forward-extnided with a
(0% reduction to bars 0. 95- In. in diameter, led to the
development at techniques for producing extruded
shapes with surface finished of 30 to 60 ^In. In
studies on cold extrusion at hollow shapes erf unalloyed
TI, reductions of up to 50% in backward extrusion
•ere successfully performed on solid billets 1 1/2- in. In
diameter to produce cups with wall thicknesses of
0. 338, 0. 275, and 0. 220 Inches. Reductions of up to
60%lnforward extrusion were accomplished on 1 l/2-ln.
-od by 7/8- In. -Id billets to produce cylinders with
0. I47-in. walls. By using a fluoride-phosphate chemi-
cal conversion coating In cxxijunction with a 10%
graphite-gun resin lubricant, typical working
pressures for grade AMS 4900 Tl were: (1) 46, 000 to
169, 000 psi for forward (solid) operations; (2) 60, 000
to 148, 000 psi for forward (hollow) operation; and (3)
338, 000 to 394, 000 psi for backward operation.
Oeformatlon efficiencies increased with increasing
reduction during cold extrusion. Evaluation of metal-
flow patterns and work hardening at the extruded
shapes indicated that parts with essentially uniform
structure and properties over the cross section can
be produced by the process. (Author)
Convair, San Diego, Calif.
EFFECTS OF SOMUM CHLORIC* ON STRESS
C»RROSION CRACKING OF TFTANIUM ALLOY
DURING STRESS REUEVING, by B. Faulkenberry and
I lannucct. Rept. on Contraa AF 33(600)34814.
19 May 59, i:^. Rept. no. MP 59-053.
Order from LC mi$2.40, ph$3.30 PB 153 295
This report released for sale to the public 27 Mar 61 .
Rinse water which contained as much as 400 ppm of
•odiini chloride produced evidence of stress corrosion
cracking. Stress corrosion cracking occurred during
the stress relieving operation.
Defense Meuls Information Center, Bane lie
Memorial Inst. , Columbus, Ohio.
CKSIGN INFORMATION ON TFTANIUM ALLOYS FC»
AIRCRAFT AND MISSILES, by W. P. Achbach and
R.J. Favor. Rept. on Contraa AF 33(616)7747.
10 Jan 61, 87p. DMIC rept. 145.
Order from GTS $2. 25 PB 151 104
Design allowables are summarized for die commer-
cially Important titanium alloys. Information on the
all-beu Ti-13V-llCr-3Al allay is not yet complete,
and linle design information is yet available on the
super alphas. (Author)
Defense Metals Information Center, Battelle
Memorial Inst. , Columbus, Chio^
MANUAL FOR BERYLLIUM PROSPECTORS, by
W. L. Smith. Rept. on Contract AF 33(616)7747.
18 Jan 61, 40p. 49 refs. DMIC rept. 146.
Order from OTS %l 00 PB 151 105
The Information In this manual, although no reve-
lation to geologists experienced in beryllium explo-
ration. Is selected to be of help to prospectors and to
the technically trained wfx) may commercially or
otherwise become Involved with the search for /or
applications of the rare metal. The manual Is de-
signed to avoid the technical aspects which are the
prcMnces erf the mineralogists, engineers and metal-
lurgists, as well as to avoid offensive generalization
or over -simplification.
Defense Meuls Information Center, Banelle
Memorial Inst. , Columbus, Ohio.
A STATISTICAL SUMMARY OF MECHANICAL-
PROPERTY DATA FOR TITANIUM ALLOYS, by
W. Stuart Lyman. fRept. on Contract AF 33(616)7747]
14 Feb 61, 25p. DMIC memo. 87.
Order from OTS |0. 50 PB 161 237
This m^noorandisn describes in a series of histograms
and chatts some mechanical properties of several ti-
tanium Alloys in various conditions and directions in
terms of average values and standard deviations. The
alloys described were produced and tested in the period
from 1957 into 1960. The usefulness of these de-
scriptions depends entirely on the Judgment of the user
in combining them with his own or any other similar
data showing the effects of changed titanium production,
as well as changes in processing or testing techniques,
on titanium -alloy strength properties and their
variability.
GnnunM Aircraft Eoglneering Oorp. [Bethpage.
N Y 1
EVALUATION OF TITANIUM SHEET ALLOYS Ap-
pendices C-E. Final engineering rept. on Contract
NO(a8)58-100C. 30 Oct 60, 234p; AD-248 265.
Order from LC mi$10. 20. ph$36. 30 PB 153 752
Contents:
Appendix C. Test specimens, equipment and pro-
cedures
Appendix Di Structural element test results
Appendix E. Effect of various heating rates to aging
temperature on the tensile properties of Tl-2 1/2A1-
16V sheet
(See also PB 153 751)
779
\
Grumman Airctaft Engineering Corp. , Bethpage,
N. Y.
EVALUATION OF TITANIUM SHEET ALLOYS.
PART I. QUAUTY ANALYSIS. PART 2. MANU-
FACTURING EVJ^LUATION, by Francis X. Drumm.
Final engineerin| repc. Pans I k II. Feb 58- July 60.
on Contract NO(^s) 58-lOOC. 30 Aug 60. I82p.
AD -248 263.
Order from LC itii$8.40. ph$28.80 PB 153 750
Quality Analysis iTests: Five out of 65 sheets of 4A1-
3Mo- IV alloy we^-e out of flat by nx>re than 5%, while
the majority of tie sheets were out of flat by 3% or
less . Five out of 31 sheets of 2.5 A1-16V alloy were
out of flat by mof e than 2% . but none exceeded 4% .
All of the sheets imeasured for thickness variation
were within specifications . The results of bend tests
were inconclusive. The 4Al-3Mo-lV alloy in the solu-
tion heat created condition exceeded the 10.5% target
minimum elongaiion, and in the aged condition, gen-
erally exceeded fhe 5.5% target minimum. The solu-
tion heat treated 12.5 A1-16V alloy was generally be-
low the urget maximum (105.000 psi) in tensile yield
strength. Manuficturing Evaluation: The work per-
formed in this p<irtion of the program concerned it-
self with developfnent of manufacturing parameters
for the two high Itrengih titanium sheet alloys under
evaluation . The kwo alloys were evaluated in relation
to several commpn forming operations such as ,
brake forming, joggling, dimpling, contour stretch
forming and rubber press stretch and shrink flange
forming . The program also included development of
production processes and techniques related to clean-
ing, application «>f organic finishes , adhesive bond-
ing, resistance ipot welding, and a limited amount of
fusion welding. Limited programs were also con-
ducted to evaluaOB warm forming and fixture aging as
fabrication techniques . The program provided an
opportunity to develop the techniques necessary to
fabricate the 3% horizomal tail stabilizer later in the
program.
Grumman Airc^ft Engineering Corp. , Bethpage,
N Y
EVALUATION Of TITANIUM SHEET ALLOYS.
PART 3. CTRUCTURAL ELEMENT TESTS. PART4.
COMPONENT DBSGN, MANUFACTURE AND TEST,
by Francis X. Difumm. Final engineering rept.
Parts III MV, Ffb 58-July 60. on Contract
NO(as)58-100C.i30Oct 60. 172p. AD-248 264.
Order from LC i|J$8. 10. ph$27. 30 PB 153 751
It is concluded that the 4Al-3Mo-lV alloy Is more
suitable for use iti airframe construction than the
2 I/2A1-16V alloy. At the outset of the material prop-
erty evaluation portion of this program, difficulties
were encountered in heat treating the 2 I/2A1-16V
alloy. The initial aged tensile values exceeded
210,000 psi . An additional aging treatment brought
the values in line with the vendor test data . The en-
tire test progran) was conducted on the double aged
specimens . Upon testing of notched fatigue specimens
it was determine* that the double aged material
was in a notch sensitive condition. Tlius , all com-
parisons made between the properties of each alloy,
2 1/2A1-16V and,4Al-3Mo-IV, should be interpreted
with the above fatt in mind. (Author) (See also
PB 153 750)
Pitman-Dunn Labe. Group, Frankfcrd Arsenal,
Philadelphia, Pa.
HARCWESS AND PREFERRED ORIENTATION IN
MAGNESIUM, byM. Schwartz, S. K. Nash, and
R. Zeman. Aug 59, 20p. 17 refs. Technical rept.
R-1528; AD-230 401.
Order from LC nU$2. 40. ph$3. 30 PB 153 924
Cold rolling of magnesium sheets which have been pre-
viously hot -rolled does not appreciably change the pre-
ferred orientation. With cold roUing, the scatter In
the basal planes was found to increase, more so in the
rolling direction; there is a tendency for the [lllo]
direction to be aligned in the rolling direction. The
empirical results of Knoop hardness number as a fimc-
lion of orientation in single crystals and rolled poly-
crystalline sheets of magnesium can be approximated
by cosinusoidal functions, the period of which is re-
lated to the symmetry of the crystallographic plane on
which the hardness data are taken. The single crysul
is aotiest., and the hot -rolled material is a little
harder due to the grain boundaries firesent. From an
examination of the results on both the longitudinal
plane and the rolling plane it can be concluded that a
cold reduction of more than about 9 per cent is neces-
sary to appreciably increase the hardness. No signlfl-
cant variation in hardness was found as a function at
depth below the rolling plane. The hypothesis c4
Daniels and Dunn [Trans. Am. Soc. Metals 41:419,
1949] successfully explains the hardness data in the
(ICflO) plane of a single crystal at magnesium and,
also, in the longitudinal plane which, because d the
preferred orientation, can be considered to approxi-
nuue the (lOFO) and (ll20) planes. TTiis approach is
not so successful for the basal plane in the single
crystal under the assumption of either tensile or
compressive forces. (Author)
Watertown Arsenal Lab. , Mass.
FEASBIUTY OF BRAZING HIGH -STRENGTH SHEET
TITANIUM, by Joseph L. Sliney. Nov 60, 47p.
11 refs. Technical rept. no. WAL TR 401.54/1;
AD- 247 685.
Order from LC ml$3. 30, ph$7. 80 PB 153 558
This report is concerned with the fluxless brazing at
commercially pure Titanium and the all-beta tiunium
alloy B-120VCA (Tl-l3V-llCr-3Al). -Lap Joints were
induction -brazed inside a bell Jar, using argon at re-
duced pressure for protection during the heating cycle.
Load-carrying ability of the Joints increases with the
length of overlap and with the strength of the base
metal. Aging after brazing increases the Joint strength
by increasing the strei^^th of the base meui. (Author)
Shuctural Metallurgy and Corrosion
Illinois U., Urbana.
SOME COMMENTS ON THE AUSTENITE- MARTEN -
SITE INTERFACE, byC. M. Wayman. Technical
note on Contract AF 49(638)420. Jan 61, 14p. 28 refs.
AFOSRno. 116.
Order from LCmi|2. 40. ph(3. 30 PB 154 553
780
Materials Research Lab. . U . of California ,
Berkeley .
DEFORMATION TWINNING AM) FRACTURE IN
MOLYBDENUM, by F. O. MueUer and E. R. Parker.
Technical rept. no. 21 on Contract Nonr-222(52).
June 60, 30p. 13 refs . Series no. 27, issue no. 21;
AD- 242 468.
Onler from LC mi$2.70, ph$4.80 PB 150 006
The purpose at these experiments was to investigate
the relationships between deformation and fracture in
neighboring grains of a polycrystalline metal. Large
friin. high purity molybdenum was available in ingot
form. Compression tests on specimens cut from this
ingot were made at room temperature and at -1%%.
Large grained molybdenum specimens are more sus-
ceptible to brinle fracture at low temperatures than
are single crystals . Both transgranular and inter-
gianular cracking occur in polycrystals strained at
low temperatures . Twin bands form when polycrys-
talline molybdenum fractures at low temperatures .
The traces of twin bands are parallel to {^H^ planes.
The twins are not planar, but consist of many irregu-
lar prisms having axes parallel to a ■^lj> direction;
the prismatic faces are not parallel to \Il^ planes ,
but they are often parallel to {llO} planes , or to
planes of irrational or higher indices . Twinning is
accompanied by localized slip in the region of the
(Win band . (Author)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
CORROSION INHIBITORS FOR LITHIUM CHLORIDE
SOLUTIONS, by C. V. BrouUlene. 27 Jan 58, 26p.
3 refs. Technical note N-328.
Order from LC mi$2J0, ph$4-80 PB 154 611
The 2-1/2 gallon copper fire extinguisher containing
sodium dichromate-oxallc acid inhibitor was pro-
tected to the greatest extent from the 24 percent
lithium chloride solution. The stainless steel fire
aoinguishers were attacked at the water line and at
welds. Intergranular and crevice corrosion was so
severe that leaks developed in areas adjacent to the
velds. (Auchor)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
DETERIORATION OF BITUMINOUS COATINGS AT
GUANTANAMO BAY, CUBA, byC. D. Carpenter.
26 Nov 51 . 9p. 6 refs . Technical note TN-065.
Order from LC mi$ 1.80. pli$ 1.80 PB 154 641
Several preliminary observations and recommenda-
tions may be summarized as follows: Examination of
the original enamel chipped from the {nling has indi-
cated that the premature deterioration was caused by
the improper application of the bituminous coating.
A resume of the conditions necessary for the success-
ful application of bituminous coatings to marine
structures in the tidal zone is necessary to serve as
a supplement to the existing specification.
Naval Civil Engineering Lab. , Port Hueneme, Calif.
USE OP VOLATILE CORROSION INHIBITORS FOR
PRESERVING THE INTERIOR SURFACE OF STEEL
PIPE, by C. V. Brouillette. Final rept. [1958]
Technical note N-333.
Order from LC mi$2.40, ph$3.30 PB 154 612
The deterioration of the interior surface of steel pipe
•luring periods of outdoor storage has long been a
serious corrosion problem. Work at the
NAVCERELAB and other laboratories has shown that
VCI will protect the steel surfaces d enclosed spaces.
These inside surfaces can b£ cleaned by light flushing
prior to use and in many cases need no cleaning. The
VCL cyclohexylamine carbamate, can be easily pre-
pared from the reaction between cyclohexylamine and
carbon dioxide (dry ice). Cyclohexylamine carbamate
prepared in situ is recommended for use in preventing
corrosion inside of steel pipe which is stored outdoors.
Metal closures are effective seals for the ends of the
steel pipe. (Author)
Pitman-EXinn Labs. Group, Frankford Arsenal,
Philadelphia, Pa.
DESIGN PROPERTIES OF ALUMINUM ALLOY 2011,
by B. J. Rogus. 31 Dec 59, 22p. Test rept. T60-8-1;
AD-231 772.
Order from LC mi$2. 70. ph$4. 80 PB 153 581
Accelerated corrosion tests were conducted on four
aluminum alloys. The program was intended to deter-
mine whether any restrictions as to suggested use
should be included in Federal Specification QQ-A-365
for 2011 material. Alloys evaluated included 2011 T-3i
2011 T-8, 2017 T-4, and 2024 T-4 rod. Two corro-
sive environments were employed. These were con-
tinuous salt spray mist and alternate immersion in a
solution of sodium chloride and hydrogen peroxide.
Resistance to corrosion was determined for the alloys
in both the unstressed and stressed conditions. Test
results indicate that alloy 2011 T-3 has poor resist-
ance to stress corrosion cracking and should not be
used for highly stressed components. Tlie same alloy
in the T-8 temper, however, exhibited good resist-
ance to stress corrosion and compared favorably with
alloys 2017 T-4 and 2024 T-4 which are commonly
used for engineering and structural applications.
Little difference was noted between alloys with re-
spect to resistance to corrosion in the unstressed
condition. Based upon obtained test results, it is
recommended that restrictions be included in Federal
Specification QQ-A-365 against the use of alloy
2011 T-3 for highly stressed or structural sections,
but these restrictions would not apply to the T-8
temper for such applications. (Author)
NUCLEAR PHYSICS AND
NUCLEAR CHEMISTRY
Armour Research Foundation, Chicago, 111.
A STUDY OF THE NATURE OF FREE RADICALS
IN IRRADIATED CHEMICAL SYSTEMS, by P. Y. Feng,
W. A. Glasson, and S. A. Marshall. Rept. for 1 Jan 59-
30 June 60 on The Chemistry and Physics of Materials,
Contract AF 33(616)6141. Nov 60, 65p. 43 refs.
WADD Technical rept. 60-344.
Order from OTS $1 . 75 PB 171 596
A Study has been made of the radiation chemistry of
various organic compounds. The compounds studied
were chosen in order to ascertain the effect a( struc-
ture and presence of functional groups within the basic
carbon skeleton on the radiation damaging of the vari-
ous substrates. Compounds studied were n-, sec-, and
tert- butyl iodides, tert-butyl amine, n-butanol.
781
n-butyric acid, anil ethyl acetate. The alkyl iodides
were stiidied in order to ascertain the effect at struc-
tural isomerism c«i a system whose primary dissocia-
tive step is known. I.e. carbon-iodine bond fission.
The other compoutds were studied in order to evaluate
the effect of changing the functional gproup (alcohol,
amine, acid, etc. ) and the over -all structure (ester)
in a four carbon organic system. The results indicate
that over-all yieltte of products Increase on changing
from a primary to a secondary to a tertiary bond to the
dissociable entity. Further, on changing the functional
group the character o* the products change as the bond
energy In question approaches that al the carbon-
hydrogen bond. (Author)
, Jnd
Dewey, G. C. . 4x1 Co. , Inc. , New York.
SELECTED NUCL^EAR DATA FROM MONTTE
CARLO CALCULATIONS, by J. R. Lamarsh,
A. I. Lieberman, and M. O. Vassell. Rept. on Con-
tract DA 30-069-5D1-ORD-2204. 1 Oct 58, 122p.
3« ref s . j
OrderfromLCmij6.30, phH9.80 PB 155 324
This report released for sale to the public 3 Apr 61 .
This report summerizes the neutron cross section
data currently used in connection with certain Monte
Carlo studies of neutron penetration. The present
document containsi dau from 0.025 ev to 14 mev for
hydrogen, boron, fcarbon, nitrogen, oxygen, alumi-
num, sulphur, iroki. barium, and lead, and from
0.025 ev to 10 met for the isotopes of uranium.
Naval Radiological Defense Lab. , San Francisco,
Calif. I
FRACTIONATION I. HIGH- YIELD SURFACE
BURST CORRELATIONS, by E. C. Freillng.
29 Oct 59, 38p. 5 refs . Research and development
technical rept. U^RDL-TR-385; AD- 232 085.
Order from LC n4$3.00. ph$6.30 PB 154 717
The phenomenon df fractionation is described and its
imponance to various radiological and nuclear chemi
cal problems is etplained. Fractionation data from
four high-yield sujiace bursts over sea water and
coral are then coifrelated. The correlations appear
to hold within a factor of 2 for even the worst cases ,
compared to observed fractionation factors as high
as 100. Possible Applications are discussed.
(Author)
[Nepa DIv. , Fai^child Engine and Airplane Corp. ,
Oak Ridge. Tenn. ]
HYI»OGENOUS SHIELDING MATERIALS, by A. J.
MUler. 10 Feb 4$, 3p. NEPA 398- SCM-j6.
Onter from LC nk^l. 80. pb$l. 80 PB 155 431
Nepa Dlv. . Fairlchlld Engine and Airplane Corp. ,
Oak Ridge. Tera).
RUBBER SHIELD, by Hans R. Stephan. 12 Feb 48, 4p.
1 ref. Memo. no. NEPA-406-EMM-12; rev. of Memo.
NEPA-388-EAM-S17.
BO.
Onler from LC nni$l. 80, ph$l. 80
PB 155 432
(Nepa Div. , Pairdilld Engine and Airplane Corp. ,
Oak Ridge, Tenn. ]
SPECULATIC»4S AS TO THE NEED FOR BORON IN
SHIELDS, byM. L. Lesser. 17 Dec 47, 4p.
NEPA-354-EAM-S15.
Order from LCmi$ 1.80. ph$ I. 80 PB 155 429
New Mexico U . [Albuquerque],
EXTENSIVE AIR SHOWERS OF THE gOSMlC
RADIATION, by John R. Green. Final rept. on
Contract AF 49(638)34. 16 Jan 61 , 66p. 19 refs .
AFOSR-243.
Order from LC mi$3.90, p*>$10.80 PB 154 704
A number of investigations have been carried out on
the structure, the propenies , and the interactions of
the components of the extensive air showers of the
cosmic radiation. To carry out this program, two
scintillators having an accepunce area of 7.3 m2
have been developed together with the circuits neces-
sary to analyze and record the data from the scintilla-
tors . An autonrtatic data reduction system with con-
siderable flexibility of function has been designed to
give the dau in the form of punched cards . Three
smaller scintillators with an area of 0.66 m2 were
also constructed. The size spectrum of extensive air
showers in the region of 10* to 10^ particles has been
investigated and found to be represented by a power
law. These results are of significance to theories
regarding the origin of the very energetic particles
that produce these showers . A mu-meson telescope
was constructed from the three smaller scintillators
with a toul of 8 in. of lead absorber and was put in
operation for a period of 55 days to obtain barometric
and temperature coefficients for the mu- mesons and
to observe variations in the flux of these particles .
A vertical telescope formed from the two larger
scintillators with variable amounts of absorber (lead
and water) between them was used to find the average
energy of the electronic component as a function of
distance from the shower core. A new transition
effect for the showers with water as an absorber has
been obtained .
Pennsylvania U. , RiiladelphU.
STUDIES IN PHOTONUCLEAR REACTIONS Annual
rept. [for 1960] on Contract AF 49<638>454. 19 Dec 60,
7p. 5 refs. AFOSR-135; AD-249 231.
Order from LC mi$l. 80. ph$l. 80 PB 153 862
(See also PB 149 006)
Elementary Particles
Johns Hopkins U . , Baltimore , Md .
BEAM OPTICS ANALYSIS USING THE !M^ 650, by
Peter E. Schlein. Technical rept. on Contract
AF 18(603)143. Nov 60, 28p. AFOSR-TN-60-1480:
AD- 250 102.
Order from LC mi$2.70. ph$4.80 PB 154 261
This repon describes an IBM 650 computer program
BOMMIT (Beam Optics Matrix Multiplication and Iter*
lion) which greatly faciliutes the design d precision
782
beam optics . A beam system consisting of an arbi-
trary ordering , type , and number of optical elements
up to a maximum of SO can be considered . The ma-
trix method is used.
Naval Radiological Defense Lab. . San Francisco,
Calif.
A METHOD OF CALCULATING THE DENSITY OF
THERMAL NEUTRONS IN A SLAB, by F. Forelli.
17 Mar 60, 26p. 2 refs. Research and Development
technical rept. USNRDL-TR-409; AD- 235 684.
Order from LC mi$2J0, ph$4.80 pg 153 891
Ibis rqxnt released for sale to the public 24 Mar 61.
A trial application at Grossjean's method at calculat-
ii^ multiple scattering of particles has been made
for the case at a plane isotropic source of thermal
neutrons in a slab o< finite thickness. The meithod
involves the expansion of the neutron distribution in
Legendre polynomials. Hand computations were
carried out to the fourth order widi results that indl
cate a much higher order is needed. The method is
suitable for use with an electronic computing
machine. (Author)
Instruments and Installations
Air Force Special Weapons Center, Kirtland APB,
N. Mex.
SULFUR AS A SENSITIVE TOTAL NEUTRON DO-
SIMETER, by John A. Blaylock, Eugene Omoda, and
Bllen M. Hippeli. Jan 60, 30p. 6 refs. AFSWC-TN-
59-36; AD- 235 304.
Order from LC mi$2. 70. ph$4 80 PB 155 254
This report released for sale to the public 31 Mar 61.
A Riethod is suggested for using sulfur as a total neu
iron dosimeter in connection with nuclear detonations.
The technique was studied using the Los Alamos
Godiva II assembly as a neutron source. Reliable
meMurements were obtained out to 367 yd. from this
relatively weak neutron source. After the technique
was developed and the appropriate calibration estab-
lished, sulfur was used as a neutron dosimeter in
Operation Hardtack II. Comparison of the results of
the sulfur technique with those of the more elaborate
foil techniques shows very good agreement. This com
pariaon also points out that the sulfur method makes
it possible to monitor dosage to about three times the
slant range presently covered by the foil method.
(Author)
Carnegie Inst, of Tech., Pittsburgh, Pa.
DESIGN OF CLOUD CHAMBER COILS, by Martyn H.
Foaa. Technical rept. no. 2 on Contra a N7onr-
303(01). [1950] 18p. M-4277; ATI-52 581.
Order from LC mi$2. 40, ph$3. 30 PB 154 863
TUs report released for sale to the public 24 Mar 61 .
Formulas are developed for the design of cloud cham-
ber coils. This development is based on the problem
of producing a uniform field of Helmholtz type coils.
Helmholtz coils have a cross-section small in com-
parison with their radius squared, and dius require
excessive power where a high field is required. It is
clear that any uniformity condition can be met by mak-
ing the coils sufficiently large. The problem of the
uniformity of the field is studied by making a power
series expansion in terms of the radium, (u), of the
field point in the mid-plane. This power series is
developed from the expression for the field of a loop
of wire.
Flight and Engineering Test Group, Wright Air
Development Div. , Wri^ -Patter son Air Force Base,
Ohio.
A GASEOUS XENON THERMAL NEUTRON DETEC-
TOR, by Raymond H.Kelley and Anthony N. Fasano.
Nov 60, I6p. 6 refs. WADD Technical note 60-281.
Order from OTS %0. 50 PB 171 616
A Stable gaseous xenon thermal neutron detector, con-
sisting of a thin U^*^ source sealed in a xetno scintil-
lation chamber and coupled to a photomultiplier tube,
has been 'constructed. Characteristics of the device
have not changed significantly over an 18 -month period
The compact deteaor (approx. 9 in. long and 2 in. in
diameter) is especially useful for accurately locating
thermal neutron beams because the detector's sensitive
volume is precisely defined, by the U^^ source. The
method of construction, performance charaaeri sties,
and potential application of this device are considered
in detail. (Author)
Nuclear Engineering and Power
Armour Research Foundation, Chicago, 111
POWER PLANT EFFIQENCY ENHANCEMENT, by
E. GyoryandC. C. Miesse. Final rept. for
10 June 58-10 Apr 59 on Contract AF 30(602)1911 .
June 59, 82p. 4 refs . ARF Proj. no. D165; RADC- -
TR-59-77' AD-217 407.
OrxlerfromLCmi$4.8b, ph$13.80 PB 150 908
Tlie results are presented of an investigation which
was c<MKlucted for the purpose of establishing the fea-
sibility of improving the performance of nuclear
power plants for Arctic installations . Various power
plant cycles which would take advantage of the low
temperature heat sink available in the Arctic region:
were analyzed . It is concluded that the addition of a
secondary cycle to the existing steam cycle of pres-
ent nuclear power plant cycles such as the Army Pack
age Power Reactor (SM- 1) and the Argonne Low
Power Reactor (SL-l) will result in Increasing the
thermal efficiency by a factor of approximately 1.4.
In addition to diis binary cycle, a single cycle re-
placing the steam cycle indicates promise. A refrig-
erant such as Freon-I2 would be used as a woiicing
fluid . It is recommended that the binary cycle and
single cycle systems be subjected to a detailed design
study for purposes of obtaining a more definite basis
for comparison than was possible within the scope of
this project. (Author)
783
[Nepa Div. , Fair^ld Engine and Airplane Corp. ,
Oak Ridge, Tenn. )
DISCUSSION OF POSSIBLE FABRICATICW TECH-
NIQUES AND DENSITIES OBTAINABLE IN SUG-
CTSTED SHIELDING MATERIALS, by Robert W.
Coyle. 31 Oa 47, 5p. NEPA-303-EMM-6.
Order from LC mill . 80. ph$l 80 PB 155 428
Nuclear Structure
High Energy Physics Lab. , Stanford U. , Calif.
SCATTERING OF HIGH-ENERGY ELECTRONS
FROM Ca4'*0, ySl, Co59, lnH5, Sbl21.l23. AND
^209, by H. Cramisll, R. Helm and others . Rept. on
Contract N6oor-25il6. 1 June 60, 22p. 9 refs .
HEPL-206. I
Order from LC mli2.70. ph$4.80 PB 150 171
The absolute elastit electron-scatterirw cross sec-
tions of Ca^O, v51i Co59, inH5, Sbl2r,123, and
Bi209 have been, measured at a number of angles at a
primary electron etiergy of 183 Mev. The cross sec-
tions were obtained by comparison with scattering
from the proton. These data have been compared
with the previous relative angular distributions meas-
ured by Hahn, Rav^nhall, and Hofstadter. The pres-
ent data are In closer agreement with the charge dis-
tributions found fmm fitting a Fermi two-parameter
model to the older data than with those found from a
fit of the Ford and Hill charge distributions . The
absolute cross secfioos for bi209 show the least
agreement: they arte 35^6 larger than the predictions
of the Fermi nxxlel and about 70% larger than the
Ford and Hill mod^l . (Author)
Institute of Theoitetical Physics. Stanford U. , Calif.
PSEUD-CLUSTER EXPANSIW II. APPLICATION TO
SINGLE-PARTlCLt NUCLEAR MATRIX ELEMENT,
by Jun-Ichi Pujita. [Technical note no. 29 on Contract
AF 49(638)388. Aui; 6a 14p. 9 refs. APOSR-TN-
60-1135; AD- 246 6^6.
Order from LC ml42. 40. ph$3. 30 PB 153 187
Possible corrections due to the short range correla-
tions to a single -particle nuclear matrix element are
discussed from the viewpoint of the cluster expansion
method. The corraction for the diagonal matrix ele-
ment is usually 10^, at most, and the conventional cal-
culation in the configuration mixing method is justified
with good accuracyi The possible small effect can be
expressed as (1 +0) (O. M, O), where O is an asymp-
totic wave function in the model space and a super-
position of low-lyirig shell sutes, M is a single parti-
cle operator and D stands for the effect of wave func-
tion normalization. It is rfiown that D is a positive
q^ntity with the onder of magntldue of 10% if M
involves the radial coordinates of nucleons such as the
electric dipole or duadrupole moment. If M has no
radial coordinate mch as the magnetic moment or
beta -decay mainen{in the allowed transitions, a nega-
tive correction due to the possible increase of the heal
ing distance at the hudear surface is possible. The
relationship berwe^ the correlation functions and
higher energy pherbmena is also mentioned. (Author)
'"•^ • Radioactivity
California U- , Los Angeles.
CHEMICAL EFFECTS OF RADIATION, by W. P.
Libby. Technical rept. on Contract AF 49(638)901.
30 Sep 6a 65p. 62 refs. AFOSR TN -60- 1269;
AD- 247 702.
Order from OTS »L 75 PB 171 572
Contents: CHEMISTRY O)? POSITIVE ICWS- Part I,
General theory, TTieory of the chemistry of ions;
PART II, Radiation -Induced cross linkage of polymers.
THE CHEMISTRY OF NEUTRON MODBRATICWJ.
which is the problem of the chemical tectors in remov-
ing momentum for neutrons. SIZE EFFECTS AMONG
ISOTOPIC MOLECULES, by Hubert W Joy and W. F.
Libby. THE NOSE CONE PROBLEM: Optical trans-
parency and resistance to flash heating, by W. F.
Libby (to appear in Nov. 1960 issue of the journal of
Chemical Physics). THE URANIUM OXIDES. TRIT-
lUM GEOPHYSICS, with the Tritium Water List of
W. P. Libby, dated 15 Sep 1960. These data denrKXi-
strate that (1) the Mediterranean Sea does not mix at
150 meters, at least south of Sicily and in the*
Tyrrhenian Sea; (2) the Dead Sea does not mix at 45
meters and greater, or at least does not mix anywhere
completely In 10 years or so; and (3) hydrologlcal ap-
plications in California seem to be useful; it is possi-
ble to distinguish rainwater from old ground water and
to show that recharge operations lead to spotty and
patchy deposits.
Convair. Fort Worth. Tex.
SPEQFICATION OF NEUTRON FLUX IN THE CON-
VAIR RADIATION EFFECTS TECTING FAQUTY,
by W . E . Dungan . Rept . on Contract
AF 33(600)38946. 30 June 60. 114p. 13 refs. NARF-
60-23T; MR-N-270: AD- 240 860.
Order fromLCmi$6.00. ph$18.30 PB 155 322
This report released for sale to the public 3 Apr 61 .
The current s»te-of-the-art in the specification of
the neutron flux in the Convair Radiation Effects
Testing Facility is described as it relates to activa-
tion and radiation damage in material . The results
are adaptable to configurations in which a boral-
shieldlng material is used . These results indicate
that the neutron flux in the facility may be reasonably
specified by a series of integrals of an isotropically
attenuated, analytical spectrum. This spectrum is
normalized to experimental ihermal-and fast-neutron
measurements . Recommendations concerning fpil-cx
posure nnethods are presented. Specific data concern-
ing flux measurements and penurbations are in-
cluded. (Author)
Massachusetts Inst, of Tech. , Cambridge.
APPUCATION OF WEATHER RADAR TO FALLOUT
PREDICTION, by Pauline M. Austin. C^rterly tech-
nical rept. no. 11. 1 Sep- 30 Nov 60, on Weather
Radar Research, Contract DA 36 - 039- sc- 75030.
15 Dec 60 lip.
OrderfromLCmi$2.40. pH|3.30 PB 154 706
Since fair weather was prevalent during the quarter.
784
aod records of a number of hours' duration were ob-
ftiaei in only six storms . These included the rain-
itorm associated with Hurricane Donna on
September 12. Recent comparisons of simuluneous
measurements on the two radars indicate that the dis-
CTtfUtcy between their relative values is only 2-3 db.
Computations and measurements are being made to
(Jetermine the cause of the difference. The data
processing program is progressing satisfactorily.
most of the data for summertime storms having been
Qiiiscribed to the form of intensity contour maps .
Work is also continuing on the digitalization and
■imerical analysis of the squall line data. The com-
puter program for obtaining fallout and rainout pat-
wnis for a 10 iGT detonation has been completed and
HSted. For a selected wind field a distribution in the
abseoce of precipitation and two distributions with
now showers have been computed . (Author) (See
tlsoFB 152 661)
Naval Civil Engineering Lab. , Port Hueneme, Calif.
ANALYSIS OF THE CRITICAL SHIELDING VOL-
UME FOR UNDERGROUND SHELTERS, by J. C
Ledoux. [1960] 30p. 6 refs. Technical note N-381.
Orter from LC mi$2. 70, ph>4. 80 PB 154 697
This repori presents the results at an investigation to
determine which part of the earth covering a buried
shelter is the most important as a radiation shield.
The following equation: (IF) Ej (ujX sec 6 ) when
lolved for the critical angle, 6 , will define the vol-
■ne of earth which provides the fraction. F, of the
toal shielding to the shelter system. E^ is die ex-
ponential integral; u. is the effective linear absorp-
Uoa coefficient for tne shield material; x is the ef-
fective shield thickness. Computations have been
oompleced for slab and hemisphere geometry for frac-
dooa. P. of 0.99 and 0.999. For slab geometry x is equiv
tlent to tj^, the thickness of the slab shield. For
hemigpherlcal geometry x is equivalent to R^ which
is the sum at the radius at the hemisphere plus
(he minimum cbver over the arch. In ortler to pre-
serve the shielding Integrity of the shelter system,
dM shielding volume defined by ^ should not be vto-
Itted by openings of any son such as vents, ducts,
and entranceways . (Author)
Naval Civil Engineering Lab. . Pon Hueneme. Calif.
DETERMINATION OF PARAMETERS IN AN EMPIRI-
CAL FUNCTION FOR BUILD-UP FACTORS FOR
VARIOUS PHOTON ENERGIES, by Arthur B. Chilton.
Dennis Holoviak (Bureau of Yards and Docks) and
Lawrence K. Donovan t Interim rept. Aug 60, 13p.
3 refs. Technical note N-389; AD-249 195.
Order from LC mi^ 2.40, ph$ 3. 30 PB 153 908
In the computation of gamma- ray aaenuation. it is
desired to use a simple expression for build-up fac-
tors. A simple analytical expression was used for
dose build-up factors from a radioactive isotropic
point source. The parameters of the expression were
determined by the method of least squares to obtain
•n optimum fit to experimental data for build-up fac-
tors for aluminum at various photon energies .
(Author)
Naval Radiological Defense Lab. , San Francisco,
Calif.
A WIND-MEASURING SYSTEM FOR THE TACTI-
CAL PREDICnCW OF FALLOUT . by A . D . Ander-
son. 15 Oct 59. 37p. 22 refs . Research and Develop-
ment technical rept. USNRDL-TR-369; AD-231 332.
Order from LC ml$3. 00. ph$6. 30 PB 153 582
A system is discussed that is capable of obtaining
accurate wind measurements in the region of the
atmosphere where fallout is occurring. Such a sys-
tem must include (1) a vehicle to deliver wind-sound-
ing urgets rapidly to pertinent locations in the atmos-
phere, and (2) an adequate tracking system that
makes the wind data available immediately. Since
current meteorological sounding equipment cannot
meet these requirements . a new wind- measuring sys-
tem is proposed that uses radar to measure the drift
of telling passive targets delivered by rockets or gun
projectiles . It appears feasible to develop an opti-
mum system that can provide both accurate wind data
and the associated fallout-area prediction for a
region of interest within 10 min after a nuclear
burst. (Author)
Propulsion Lab. , Wright Air Development [Div. ]
Wright -Patterson AFB, Ohio.
COMPARISON OF MONTE CARLO CALCULATION
AND EXPERIMENTAL MEASUREMENTS FOR
GAMMA -RAY AIR SCATTERING, by David M.
Dawson. William L. Kirk and others. Aug 58, 26p.
2 refs. WADC Technical note 58-256; AD- 206 OSl.
Order from LC mi$2. 70, phJ4- 80 PB 155 257
This report released for sale to the public 31 Mar 61.
Convair has reported an experimental determination
of the angular distribution and energy spectrum of air
scattered gamma -rays from a cobalt -60 source.
Lynch. Johnson. Benolt and 25erby have reported the
results of a Monte Carlo study of gamma-ray air
scattering from a monoenergetic beam source which
was performed at WADC on the Remington Rand 1103
digital computer. This program has been modified to
perform similar calculations for a monoenergetic,
poiiit isotropic source. The code was further modified
to print separately photon currents due to first col-
lisions, to second collisions, to third collisions, and
to all higher order collisions. The angular distribu-
tion and energy spectra as reported by Convair are
compared with the results of Lynch, et. al. , and with
results obtained with the modified program. In gen-
eral, the agreement between theory and experiment is
within a factor of two. (Author)
PERSONNEL SUPPLIES AND
PERSONAL EQUIPMENT
Arctic Aeromedical Lab. . Ladd AFB. Alaska.
COLD WEATHER TEST OF INSULATED UNDER-
WEAR, by Joseph Mayer . Nov 60, Up. Technical
note AAL-TN-60-21: AD-249 802.
Order from LCmiJ 2.40, ph$3. 30 PB 154 169
Two types of insulated underwear were evaluated
under extreme cold , arctic field conditions . Type A
785
Ms an outer she i of 100% nylon with polyester fiber
fill and snap clotures on the jacket and trousers .
Type B is constructed of the same material as that of
Type A , but has a snap and zipper closure on the
jacket and snap closure on the trousers . Test results
shew that Type Q insulated underwear is superior to
that of Type A ii| the standing phase of the test and
equal to Type A In the exercising phase. In the stand-
ing position or any Immobile position a man is nx>re
vulnerable to co^ exposure; therefore, the garment
affording the mo^t protection in this position is con-
sidered superion. The insulated underwear has a
promising potential as an Air Force garment. By
wearing the insulated underwear, personnel can elimi
nate some of the heavy, bulky-, restrictive clothing
and still have adequate thernuil pro-
wom in the past
tection . (Author i
Arctic Aerome^ical Lab. , Ladd AFB, Alaska.
DRY COLD EVALUATION OF THE CRAWFORD
PAPER BLANKET, by Freeman E. White. Nov 60,
6p. Technical n^eAAL-TN-60- 19; AD- 249 800.
Order from Lciiijl. 80. ph$ 1.80 PB 154 167
Cold weather te^s were ccmducted to evaluate the
paper blanket fot use in cold climate as an emergency
substitute for regular blankets in case of mass evac-
uation or other emergencies . It was the general
opinion of all four test subjects that this type of
blanket would bei inadequate for climatic conditions
encountered this. far north during the winter. (Author)
r
YSICS
G«^enheim A^ooautlcal Lab. , CaUf. Inst, of
Tech. , Pasadeia
EFFUSION OF CHARGED PARTICLES FROM A
SHOCK HEATEp GAS, by Bradford Sturtevant. Rept.
on Contract Nont-220(21). June 60, I36p. 17 refs.
AD- 240 283.
Order from LC itii$6. 90, ph$21 .30 PB 149 540
An experimental! and theoretical investigation is made
d the application ot a molecular beam type sampling
device for studying low density shock tulie flows to the
case at slowly ionizing argon behind a reflected shock
wave. The flux of charged particles from a gas heated
to about 10,000OK and 20 mm. Hg. through a small
orifice in the sh^k t\ibe end wall is measured. The
processes detertiining this flux are the initial stages
of ionization in argon and the diffusion of charged par-
ticles to a cold itietallic wall. Providing the diffusion
process is undertstood, the measurements constitute a
direct observation of incipient ionization (o'>^ lO'^).
The transient charge diffusion mechanism is studied in
detail theoretically, avoiding the assumption of
ambipolar diffusion. It is concluded that the major
problem lies in 0ie understanding of the wall-gas
interactiaa as represented by boundary conditions at
the wall. An approximate relation for charge effusion
is derived. It is concluded from the experimental re-
sults that the initial ionization can not be due to a
single step, eleqtroo-atom collision process but must
result from a s^ies of several atom-atom collisions
resulting in the Ionization of argon atoms. (Author)
Laboratory of Statistical Research, U. of
Washington, Seattle.
MULTI -COMPONENT SYSTEMS AND STRUCTURES
AND THEIR REUABIUTY, by Z. W. Bimbaum,
J. D. Esary, and S. C. Saunders (Boeing Scientific
Research Labs.). Technical rept. no. 36 on Contract
Nonr-477(ll). 8 June 60, 42p. 4 refs . AD-239 376.
Order from LC mi$3. 30. pli>7. 80 PB 148 974
The combinatorial properties and reliability of study
deals with general classes of systems which contain
two-terminal- networks and most other kinds of sys-
tems are investigated. These classes consist, with
several variants . of systems such that the more com-
ponents jwrform the greater the probability that the
system performs . For such systems . if each com-
ponent has reliability p and the reliability of the sys-
tem is denoted by h(p). then under mild additional
assumptions h(p) is shown to be an S-shaped function.
Some of the consequences are these: (1) there exists
a critical value of p such that above that value the re-
liability of the system is greater than the reliability
of a single component and below that value it is
smaller; (2) for p small, the system has a reliability
comparable to that of a series system, and for p
large to that of a parallel system; and (3) by repeat-
edly iterating the system, i.e. by using replicas of
the system instead of single components , systems
with reliability arbitrarily close to 1 are obtained if
staned with component reliability above the critical
value, but with reliability arbitrarily close to 0 if
staned below that critical value. (Author)
Maryland U. , College Park.
AN OPTICAL ANALOG TO THE MOTION OF MAG-
NETICALLY TRAPPED PARTICLES, by D. Stem.
Rept on Contract AF 49(638)530. [1960] lip. 8 refi.
AFOSR-25; AD- 249 719.
Order from LC mi$2. 40, ph$3. 30 PB 154 243
It is shown that the motion of a beam of light confined
in a diamond -shaped mirror geometry has many
properties in common with the motion of magnetically
confined panicles. The significance and reason of this
are discussed; the long term behavior of the beam's
motion is also investigated, by means of a simplified
model. In this model it is shown that the solution's
behavior depends on a cenain numerical initial con-
dition and fluctuates according to the terms of Its con-
tinued fraction development. If this Is Infinite, the
fluctuations will go on indefinitely, on a small though
not Intrinsically limited scale; If on the other hand the
numerical value Is rational and Its expansion finite,
the fluctuations will exhibit a recurring pattern which
may not be superimposed on a monotono s drift. (Ai ithor)
Stanley-Thompson Labs. , Columbia U. , New York.
EFFECT OF ADSORBED FILMS ON THE SURFACE
POTENTIALS OF METALS BY A RADIOACTIVE
ELECTRODE TECHNIQUE, by Leonard Nanis.
Marianne Baruch, and Jack H. Schulman. Rept. on
Contract Nonr- 266(64). 1 June 60, 28p. 11 refs.
AD- 243 864.
Order from LC mi$2. 70. ph$4. 80 PB 150 864
Results for the Pt/Au contact potential in various gas
atmospheres indicate that gold flamed under oxidizing
786
conditions is suitable as a substrate for study of reac-
tions with organic over -layers. The Pt/Au potential is
changed by water vapor and oxygen adsorption, chiefly
oo Pt. For over -layer 8 of long chain organic com-
pounds dissolved in non -polar medium, potential
ctianges can be due to reaction at the metal -oil inter -
taoe or the oil-gas interface, especially where solu-
bility of water is possible. (Author)
Temple U . Philadelphia, Pa.
SFECTROPHOTOMETRIC DETERMINATION OF HIGH
TEMPERATURES, by J. Lloyd Bohn, Otto P. Fuchs and
Roben K. Morton. Scientific rept. #1 on Research
Directed Toward the Attainment and Utilization of High
Temperatures. Contraa AF 19(604)3076. 1 Nov 60.
33p. 1 ref. AFCRL-TN-60-823; AD-249 239.
Order from LC ml$3. 00. ph$6. 30 PB 154 161
An effort was made to discover some method which
would allow a direct measurement of the real tempera-
turea of extremely hot bodies, or. failing that, to de-
ftoe a new substitute temperature which wou Id be more
universally applicable than present types, and which
could be considered as a good approximation to real
temperatures. Assuming that a body whose tempera-
ture iB to be determined displays a continuous distri-
bMtloo of energy, two measuring procedures were
developed which appear fnromising. The development
of these two procedures resulted from a single objec-
dve: the radiometric measurement of the real (thermo-
dynamic) temperatures of substances energized to up-
wards of a few thousand degrees Kelvin. The principle
problem which had to be solved was how to minimize
the influence of the unknown spectral emissivity. Each
of the two measuring techniques which were derived
tnempts to solve this problem In a different way. The
double-ratio method utilizes, in a double-ratio, the
measured energy at three wavelengths in order to
derive a temperature. In some respects it resembles
the well-known method Involving the ratio of energies
u two wavelengths (single-ratio method). In the appli
cadon of the single-ratio method, however, common
praaice is simply to Ignore the existence of the un-
knoirn emissivity. (Author)
Acoustics
Acoustics Research Lab. , Harvard U- , Cambridge.
Mass.
PROPAGATION AND REFLECHON OF PLANE
SOUND WAVES OF FINITE AMPLITUDE IN GASES,
by David T. Blackstock. Technical memo. no. 43 oo
Cootraa Nonr -1866(24). June 60. 23Ip. 59 refs.
AD- 242 729.
Order from LC ml$6. 90, ph$21. 30 PB 150 198
Conteau:
HlRorlcal review
Propagation
Waves of arbitrary amplitude in nondissipative
fluids
Inflnltesinwl waves in ddssipatlve fluids
Reflection and refraction
Normal incidence
Oblique incidence
The equations of hydrodynamics for plane, one-dimen-
sional motion in a viscous, thermally conducting fluid
Propagation in a nondissipative gas
Eulerian coordinates
Lagrangian coordinates
Propagation in a viscous, thermally cooducting perfect
gas
Penurbation solution for the case of sinusoidal
piston motion
Propagation of a step-wave of small amplitude
A simplified theory for waves of moderately nnall
amplitude in dissipative gases
Reflection and transmission
The mechanics of reflection and transmission
Shock formation in the presence of a rigid wall
Research Lab. of Electronics. Mass. Inst, of Tech.,
Cambridge.
MEASUREMENTS OF SOUND ATTENUATION IN
THE ATMOSPHERE (PART I), PULSE DISTRIBU-
TION ANALYSIS OF SCATTERED SOUND (PART U)
by Uno Ingard, Stanley K. Oleson. and Michael D.
Mintz. Final rept. on Contract AF 19(604)2051.
4 Nov 60, 55p. 10 refs. AFCRL-TR-60-431;
AD- 248 636.
Order from LCmi$3. 60. ph$9. 30 PB 153 906
An attempt is made to measure acoustic scatter atten-
uation produced by atmospheric tuiixilence . Labora-
tory experiments on scattering cH sound by turbulence
are described; in particular, a new experimental
technique involving pulse-height analysis of scattered
sound. (Author)
Willow Run Labs. , U. of Michigan, Ann Arbor.
REVERBERATION-ROOM ANECHOIC CHAMBER
TRANSMISSION-MEASUREMENT TECHNIQUE, by
S. S. Kushner and N. E. Barnett. Rept. on Dynamic
Problems in FUght Vehicles, Cootraa AF 33(616)3435.
Apr 59, 53p. 8 refs. WADC Technical rept. 59-130;
AD-215 221.
Order from LC mi$3. 60, ph$9. 30 PB 155 382
This report released for sale to the public 12 Apr 61.
A preliminary investigation was undertaken to charac-
terize several parameters involved in a reverberant
source room-anechoic termination method for meas-
uring acoustic transmission. This method appears
potentially capable of evaluating the acoustic transmis-
sion in great deuil of samples possessing widely di-
vergent physical characteristics. Exploratory experi-
mentation included examination of reverberation-room
diffusion, termination diffraction and directionality,
effects of sample mass on transmission, and trans-
mission of various stiff -panel configiirations . <^"thnr)
Electricity ahd Magnetism
Carnegie Inst, of Tech., Pittsburgh, Pa.
HIGH MAGNETIC FIELDS, by Martyn H. Foes. Tech-
nical rept. no. 3 on Contract N7onr- 303(01). [1950]
22p. M-4278; ATI-52 532.
Order from LC mi$2. 70, ph$4. 80 PB 154 864
This report released for sale to the public 24 Mar 61.
Obtaining very high magnetic fields, several million
787
gauss, is physictlly possible. The limlution Is the
large power requirement. A good background for the
design at practiaal magnets is found in the study of an
"ideal" magnet ^hich has the optimum current density
dlstrlbiaion. tW) designs of coils are discussed. The
first comes clost to the optimum and the second makes
the region where the field is developed very
accessible. (Au^or)
[]iainond Ordnftnce Fuze Labs., Washington, D. C
THE ELECTRO^ATIC POTENTIAL DUE TO A
POINT CHARGE, IN THE PRESENCE OF A CON-
DUCTING SPHERE AND AN INFINITE GROUND
PLANE, by Clyde Morrison and Nick Karaylanis.
1 Feb 60, 27p. 3 rerfs. TR-804; AD- 238 626.
Order from LC |ni$2.70, ph$4.80 PB 148 958
jnil
The solution at i particular electrostatic potential
problem involving a conducting sphere and infinite
ground plane in the presence of a point charge is dis-
cussed. Use is made of the conventional imaging
method to obcaiq the solution in terms d Lambert
series. It is shown how some d the resultant series
may be combtne<l and expressed as contour integrals
in the complex plane, and how, by a suitable defor-
mation of die codtour, the series may be transformed
into an extremelv rapid convergent series. The con-
tour method is laed to obtain very simply an asymp-
totic expansion qf part at the solution for a limiting
case of the problem which was obtained very labori-
ously by Schldmllch. (Author)
illc
Digital Computer Lab. , U. d Dlinois, Urbana.
COMPUTATION OF ORIXR PARAMETERS IN AN
ISING LATTICH BY THE MONTE CARLO METTIOD.
by ;. R- Ehrmaa. L. Di Fosdick and Dl C Hands-
comb. Rept. onTContract Nonr- 1834(27). 15 Apr 60,
44p. 11 refs. Ke^i. no. 98; AD- 236 208.
Order from LC tni|3. 30. ph$7. 80 PB 154 103
The lof«-range »nd short-range order parameters are
computed for th* ising lattice using a Monte Carlo
sampling scheme. The square lattice, the simple
cubic lattice, arii the body-centered cviWc lattice are
considered. In the three dimensional calculations
both the anttferryxnagnetic and ferromagnetic cases
are considered Is well as the coupling to an external
magnetic field of various strengths. Agreement is
found where the results can be compared with the ex-
act two dimensional results, and in the three di-
mensional case the results agree with those obtained
from series approximations in the regions where the
series approxiniatlons are valid. The present method
appears to give good results for the short -range order
even very close to the critical temperatxire, but in
this neighborhood the long-range order estimate Is
crude. The coriputations were performed on the high-
speed computer, ILLIAC. (Author)
Douglas Aircrift Co. , Inc. , Santa Monica, Olif .
SOME NOTES ON THERMOELECTRIC EFFECTS.
MODEL. GENERAL, by L. L. ScWlb. 1 July 60.
40p. 8 refs. Rett. no. SM- 37637.
Order from LCjml$3. 00, ph$6. 30 PB 152 061
With the lncrea$ing interest in semi-conductor re-
search, thermoelectric equipment will be competitive
with other methods of cooling and power generation in
the near future. It seems , therefore, that a complete
understanding of thermoelectric phenomenon will be
important to the engineer. The basic thermodynamic
principles of these effects are developed and investi-
gated in this repon. Design philosophies are sug-
gested for both cooling and power generation . The
basic thermo- physical equations have been presented
for computer programming. A simple computer pro-
gram for thermoelectric cooling has been included.
This program will aid feasibility studies of vehicle
cooling. (Author)
Electrical Engineering Research Lab. , U. of Texaa,
Austin.
A SURVEY OF PAST AND PRESENT INVESTIGA-
TIONS OF THE NATURAL EARTH CURRENTS, by
George H. Hopkins, Jr. Rept. on Contract Nonr-
375(01). 1 Apr 6a 37p. 24 refs. Rept. no. 113;
AD- 235 463.
Order from LC mi$3. 00, ph$6. 30 PB 154 102
Earth current measuring systems are discussed, the
results of the investigations are summarized, and an
outline summary of the current theories is given.
Measurement programs in progress are concentrating
increasingly on the short -period activity, and on cor-
relating the geoffiagnetic and earth current fluctua-
tions. (Author)
Electro-Optical Systems, Inc. , Pasadena. Calif.
STUDY OF ELECTRICALLY EXPLOC«D WIRE
MATERIALS, by F. Webb. Quarterly progress rept.
no. 4. 1 Apr-3I July 59. on Contract DA 04-495-ORD-
1298. 25 Ai« 59. 35p. 13 refs. BOS rept. 210-QL-4;
AD- 228 063.
Order from LC nU$3. 00. ph$6. 30 PB 155 573
This report released for sale to the public 19 Apr 61.
High energfy densities were achieved of the order of
10 to 15 ev/atom under some conditions. Electrical
conduction in very dense gases above the critical poia
is inferred. A rapidly expanding luminous zone (pre-
shock wave) and its possible interaalon with a rare-
faaion wave was observed. Some of the causes of the
voltage and current wave forms as well as fast wire
exploding mechanisms are discussed. (Author)
Institute for Fluid Dynamics and Applied Mathe-
matics, U. of Maryland. College Park.
THE CONTAINMENT OF PINCHED DISCHARGE BY
AN AXIAL MAGNETIC FIELD, by R. K. Jaggi. Rept
on Contract AF 18(600)1315. Dec 60, I5p. 4 refs.
Technical note BN-221; AFOSR-47; AD- 249 477.
Order from LC ml$2. 40, ph$3. 30 PB 154 080
A calculation of the loss of deuterons from a pinched
current to the wall of the container given by G. Thom-
son (Phil. Mag. 32:886, 1958) Is extended so that ac-
count is taken of an axial magnetic field. Such aflekl
can materially reduce the particle loss. (Author)
Laboratorie de Ferromagnetlsme, Instltut de
Physique, Strasbourg (France).
PREPARATION OF IRC»I PHOSPHIDES, IRON
BORIDES, COBALT BORIDES, AND THE STUDY OP
THEIR DIFFERENT MAGNETIC PROPERTIES, by
788
it R. Forrer. Final technical rept. no. 2 for
1 hii-31 Dec 60 on Contract DA 91-591-EUC-1370.
fl961] I5p. 14 refs. AD-250 379.
OnJer from LC ml$2. 40, ph$3. 30 PB 154 364
Fe,P is a normal ferromagnetic compound with a
Curie point at 443°C, and an absolute saturation mo-
ment of 1, 84 Mb for one Iron atom of the compound.
Pe«P is only ferromagnetic at low temperatures below
ttsuirle point at -7°C. TWo Iron borides Fe2B and
PeB are ferromagnetic at room temperature. FeB
IMS an orthorhomblc unit cell. Its Curie point is at
309°C FejB has a quadratic unit cell with a Curie
point at 740°C and an anomaly temperature at 245°C,
CD2B has a Curie point at 155°C and an absolute satu-
ration moment of O 75 pt, for one atom of Cobalt.
C03B has a Curie point at 478°C ± 29C and CoB is not
ferromagnetic at room temperature.
Stanford Research Inst. , Menlo Park. Calif.
A STUDY OF CORONA DISCHARGE NOISE IN AIR-
CRAFT ANTENNAS, by A. Vassiliadis. Technical
rept. 70 on Contraa AF 19(604)3458. Aug 60, 117p.
21 refs. SRI ProJ. 2494; AFCRL-TN-60- 1107;
AD- 249 378.
Order from LC mi$6. 00, ph$l8. 30 PB 154 078
This study was conducted to investigate the character-
istics of radio noise interference which is caused by
ccrooa discharges on the aircraft. The discharge,
which consists of numerous high-energy pulses of
current, causes electromagnetic interference which
coi^les to an aircraft antenna. The character at the
oaiae pulses at the antenna depends not only on the
original characteristics of the corona but also on the
aircraft structure and aircraft resonances which In-
Queoce the frequency spectrum of the pulses. Tech-
niques developed at SRI made it possible to measure
Che pcwer spectrum of the noise source and the mag-
aitude erf the coupling function from the various
vulnerable spots on the aircraft to a particular an-
tenna location. Rational function approximations which
were obtained for the coupling functions, are inter-
preted as network transfer functions where the corona
pulse as determined from measurements is the input
while the output is the noise pulse at the antenna
terminals. The characteristics of the noise are cal-
culated for a particular aircraft and antenna, e.g. , a
Boeing 707 tail-cap antenna. It is shown that under
relatively heavy charging conditions the decoupled dis-
charge method assuming 50 db of decoupling is supe-
rior to a blanker operating under ideal conditions.
(Author)
Electronics
Army Signal Research and Development Lab. , Fort
Monmouth, N. J.
PROCEEDINGS OF THE ANNUAL SYMPOSRJM ON
PRBQUENCY CONTROL (NO. 14). 31 MAY.
1-2 JUNE 60, ATLANTIC CITY, N. J. 28 Sep 60,
«9p. 116 refs; AD- 246 500.
Order from LC mi$ll. 10, ph$68. 10 PB 153 716
Contents:
Acoustic behavior of modified synthetic quartz; Piezo-
electric properties of cadmium sulfide crystals; Study
of methods for improving the quality of synthetic
quartz; Influence of lattice parameters on the proper-
ties of crystal resmators; Measurements of the vibra-
tions of quartz plates; Coupled contour and thickness
shear vibrations; Pareillel field exciution of thickness
modes of quartz plates; Effects of initial stress on
quartz plates vibrating In thickness modes; The aging
of aluminum plated 16. 5 Mc. AT-cut quartz resona-
tors; Nuclear radiation effects in quartz crystals;
Development of precision crystal units for satellite
use; Design of low frequency AT-cut resonators; Sta-
bility of crystal oscillators; Quartz crystal units and
precision oscillators for operation in severe mechani-
cal environments; The micro-module program; Effects
of thermal noise on the freq^iency of a regenerative
oscillator; Is the fine structure constant invarient;
Work on atomic frequency standards at the National
Physical Laboratory during 1959-1960; Preliminary
results on project WOSAC; A superior atomic clock
for continuous long time operation; Results of GBR ex-
periment; Stabilization of VLF transmissions at NBA;
Timing potential of Loran-C; NBS atomic frequency
standards; Molecular beam devices with storage boxes;
Missile-borne atomlcron frequency standards; Effect
of molecular frequency spread on emission in cavities;
Frequency shifts of microwave resonance in a gas cell
using optical pumping; Design considerations for a
self-contained ammonia maser'oscillator; Description
of a long cesium beam frequency standard; VHF crys-
Ul filters; Development of quartz crystal synthesizers
Tuning forks as circuit elements; Frequency standards
for tnilitary applications; Frequency and phase con-
trol of local oscillators by transmitters of standard
frequency
Chalmers U. of Tech. (Sweden).
ELECTROMAGNETIC AND SPACE CHARGE WAVES
IN A SHEATH HEUX. by Sven Giving. Rept. no. 6
on Contract AF 61(052)159. 1960, 90p. 46 refs. Re-
search Lab. of Elearonics rept. no. 49; AFCRC-TN-
60-564; AD-242 188.
Order from LC mi$4. 80. ph$l3. 80 PB 150 414
The electromagnetic interaction between a sheath helix
and an electron beam is investigated theoretically.
The whole doubly infinite set of space charge waves is
included and approximate expressions for their propa-
gation constants are derived. The validity and pxrop-
erties of these expressions are analyzed. Only the 1
first order (i.e. dominant) slow space charge wave 'is
amplified in the system while higher order waves,
which propagate with constant amplitude, show certain
transformation properties. The analysis also shows
that previous theories fail near the low electron ve-
locity end of the amplification region. The velocity
bandwidth of traveling wave tubes is considerably
wider than these theories indicate. (Author)
Polytechnic Inst, of Brooklyn, N, Y.
Dl C. EFFECTS IN FERROMAGNETIC RESONANCE
OF THIN NICKEL FILMS, by Walter G. Egan
(Doctoral thesis) and Hellmut J. Juretschke. Technical
rept. no. 10 on Contract Nonr839(06). 1 June 60, 84p.
18 refs; AD- 238 472.
Order from LC mi$4. 80, ph$13. 80 PB 148 757
Ferromagnetic resonance has been observed in nickel
789
films thin compao-ed to their skin depth by the ap-
pearance of d. c. electric fields in the film plane.
These d. c. voltages have been attributed primarily to
the Hall effect interaction al the microwave electric and
magnetic fields >y virtue of the precession at the
magnetization, tills report deals with the design and
execution of a series d experiments to test fully a de-
tailed theory following this assumption proposed by
juretschke. Pulsed microwave energy at a frequency<rf
10 KMC and peat powers of 5. 6 KW impinges upon a
nickel film located transversely in a waveguide in front
of a short of adjustable spacing and the observed volt-
age in the film plane is measured as a function of film
location, Incldeiit microwave power, direction and
magnitude <rf a static magnetic field. With respect to
the latter, the voltage displays a pronounced peaking
near the condition for ferromagnetic resonance. As
predlrted by the theory, the signal is composed of two
contributions, o»e dhje to the Hall effect, the other due
to the ferromagrfetic magneto- resistive anlsotropy.
All detailed features <rf the theory have been verified,
in an experimental arrangement in which greatest care
was taken to subject the film to controlled and known
local elearoinagnetlc fields, since the microwave
boundary conditions at the film can critically influence
the observed effects. Four typical films Investigated
in detail by this tnethod give values of surface resis-
tivity and extraordinary Hall coefficient larger than at
d. c. , while the anisotropic resistivity remains
unchanged. (Autfior)
i
Naval Civil Bn|lneering Lab. , Port Hueneme, Calif.
AN ANALYSIS OF A SYSTEM FOR THE DETERMI-
NATION OF MICROWAVE REFLECTION COEF-
FICIENTS, by W. L. Surr, R. H Hitchcock and
others. 30 Apr $4, 21p. Technical memo. M-090.
Order from LC lnl$2. 70. phK 80 PB 154 631
tni
A system for determining microwave reflection coef-
ficients by multiple reflections is described and theory
presented. Thi» theory yields an expression giving
electric field Inoensity, E, as a funaion of distance,
_x. and reflection coefficient, r. In order to anain the
'dMired agreement between data and theory, attenu-
ation and floor reflection had to be considered.
Compuution of ♦le reflection coefficient of one ma-
terial is given as an example of the appllcatkxi of this
theory. (Author)
Ramo-Wooldriage Div. , Canoga Park, Calif.
TRANSIENT M€) STEADY STATE BEHAVIOR IN
CESIUM ION BSAMS, by J. M. Sellen and H. Shelton.
Rept. on Contract AF 49(638)886. [1960] 63p. 6 refs .
RW-RL-186; AFOSR TN-60-1395; AD-250 289.
Order fromLC|ni$3.90, ph$10.80 PB 154 460
A series of exparimens with broad cesium ion beams
is described. T|iese experiments relate to both the
transient behavior and the steady state behavior in
these high pervaance beams The techniques and the
experiments themselves are a continuation and an ex-
tension of a program of study in the problems of
charge neutrali^tion . From the results of the experi-
ments , an involved pattern of behavior in these ion
beams has been revealed. In some insunces , the re-
sults may be interpreted simply, while other pheno-
mena are only suggestive of the mechanisms which
produce them . Attempts are made to interpret the
behavior of the ieam and to construct models which
may hope to account for the observed results .
Molecular Physics and Spectroscopy
California U. , Berkeley.
h}i LCAO TREATMENT OF THE AaWTY OF HY-
DROCARBONS, by Andrew Sireitw4eser, Jr. Rept. on
Contract AF 49(638)105. 3 Mar 60, 23p. 9 refs.
AFOSR rept. no. TN-60-162; AD- 233 688.
Order from LC ml$2. 70, ph$4. 80 PB 153 655.
Determinations were made of thp extent to which the
simple molecular orbital theory quantiutlvely corre-
lates the pK values of McEwen (J. Am. Chem. Soc.
58: 1 124, 1936) and acidities of aome hydrocarbons.
The following assumptions were made: (1) the acidity
of hydrocarbon is proportional to the change in the
7r-bond energy resulting from the difference in config-
uration between the hydrocarbon and the corresponding
anion; (2) effects such as changes in a-bond energies
and solvation are relatively constant from one system
to another; and (3) and strain energy is the same in
both the hydrocarbon and anion. Correlation of acidi-
ties with simple molecular orbital calculations was
plotted. In the scatter of points a Kood straioht line
emerged through the compounds wnose anions were
expected to be completely coplanar. The anions of the
other compounds containing aryl groups were less
acidic than predicted by the correlation by about 4 pK
points per nonplanar phenyl group. In all of the pre-
dicted results the anion -stabilizing character of the
5-membered ring was evidenced.
Catfaolic (J. at America, Washington, Di C.
AN LCAO MO SCF ITTUDY OF THE ELECTRONIC
STATES OF SEVERAL LINEAR HYDROGEN COM-
PLEXE;^ by Anthony R. Ruffa and Virginia Griffing.
Rept. on Contraa AF 18(600)1537. [1960] 17p.
8 refs. AFOSR-TN-60-735; AD-248 888.
Order from LC mi$2.40, ph$3.30 PB 153 829
This study is an attempt to determine for what dis-
tance of approach the two diatomic molecules make a
transition into the four atom complex. At large sepa-
rations, the hydrogen noolecules may be considered
separately, with their interaction considered as a per-
turbation on the system. However, as the separation
of the molecules begins to approach the magnitude cf
their interatomic separation, this method becomes
highly inaccurate and hence ineffective. Therefore,
for small inter molecular separations, the calculatlco
must involve the four atom system as a whole.
Catholic U. of America, Washington, D. C.
A THEORETICAL INVESTIGATION OF THE
EXCITED STATES OF LINEAR H3, by Harry L.
Morrison and Virginia Griffing. Rept. on Contraa
AF 18(600)1537. [I960] 17p. 9 refs. AFOSR -TN-60-
734; AD-248 887.
Order from LC (nl$2.40, ph$3.30 PB 153 828
This study is coocerned with the explicit calculatloa
of electronic states that can be constructed from a
linear combination of Is atomic orbitals for the
doubly occupied orbital and linear combinations of 2s
and 2p atomic orbitals for several singly occupied
excited orbitals. The variation of the total energy (tf
790
Oj u a function of the intemuclear distance is studied
for three electronically excited states. The extent of
perturbation of the closed shell orbital by the excited
tii^y occupied orbital is estimated.
Colorado U. , Boulder.
WTBRRUPTION OF NUCLEAR SPIN DIFFUSION, by
0L A. Jennings and W. H. Tanttila. Technical note on
Contract AF 49(638)611. Oct 60. lip. 12 refs. AFOSR
TN-60-1184; AD- 246 515.
Older from LC mi$2. 40, ph$3. 30 PB 153 207
Biperimental results are shown in which the nuclear
■iplD diffusion responsible for nuclear relaxation at low
temperature, under certain circumstances, can be in-
cerrupced by introducing strains into crystals either by
the paramagnetic impurity Introduced into the crystal
or by surface strains made to be significant by grind-
ing the sample to a powder. Nuclei with large quadru-
pole moments, such as iodine, have their spin diffu-
lion strongly interrupted whereas nuclei with no quad-
nipole moment, such as fluorine, show no effect of
itiains on the spin diffusion. The interpretations are
made from measured values of the spin-lattice relaxa-
ilcn time at liquid helium temperature. (Author)
(general Atomic, San Diego, Calif.
(XM>BNSATION OF ATOMIC AND MOLECULAR
HYDROGEN AT LOW TEMPERATURES, by R. T
Brackmann and Wade L. Flte. Rept. on Contracts
AF 49(638)301 and AF 49(638)356. 30 Jan 61. 26p.
6r«f8. CJA-1683; AFOSR TN-60- 1246.
Older from LC ml$2. 70, ph$4. 80 PB 154 457
mth die use of reflected modulated atomic beam tech-
niques, the reflection of hydrogen atoms ana molecules
It cold surfaces has been examined. It was found that
at low temperatures (-'4°K) hydrogen atoms reflect aa
■tains with a very high probability. The reflection (rf
hydrogen molecules Is strongly dependent upon the
imount of water vapor condensed on the target pre-
Tkwaly to or simultaneously with the H2- The fact that
coodenaation of stable gases can be affected by simul-
taneous condensation of water vapor at temperatures
ooeedlng the gases' normal boiling points leads to an
i|i|lUcatlon in the form of an extraordinarily inexpen-
sive way to produce vacuums in the lO'S mm Hg range.
(Audior)
(lUggenhelm Jet Propulsion Center, Caltf. Inst, of
Itefa. , Pasadena.
E(3UILIBRIUM EMISSIVITV CALCULATIONS (FROM
SPECTROSCOPIC DATA) FOR COj AT 3000K AND AT
MO^ by M. Lapp and & & Fienner. Technical rept
00. 32 on Contract Nonr-220(03). June 60, 19p. 22 refs;
AD- 239 404.
Okder from LC ml$2. 40, ph$3. 30 PB 148 935
Bi^librlum emisslvltles were computed for carbon di-
oUe by using available low- temperature spectro-
(fioplc data. Satisfactory agreement with empirical re-
iultt at 6OOOK is obuined if the assumption is made
tliat the emissivlty is determined by the sutistical
•iVerposition of randomly distributed bands. (Author)
Iowa Engineering Experiment Station, Ames.
TEMPERATURE DEPENE«NCE OF SOUND DIS-
PERSION IN HALO-METHANE GASES, by Sam
Legvold, Robert C Amme. and Leonard M. Valley.
Rept. on Contract AP 18(600)1496. Mar 58, 69p.
43 refs. AFOSR TN-60- 1206; AD- 246 239.
Order from LC ml$3. 90, ph$10. 80 PB 153 082
The Interferometer used in the studies may be used as
an absolute Instrument in the determination of relax-
ation absorption. Inflection frequencies of the velocity
dispersion in the methane derivatives studied donot
change rapidly with temperature. Therefore, their
relaxation times are not strongly temperature de-
pendent. Series excitation which prevails at room
temperature persists as the temperature is increased
The energy excitation theory postulates the existence
of a minimum energy of approach which is propor-
tional to the energy of the lowest mode of vibration.
The temperature dependence of collision lifetime pre-
dicted by theory based on this hypothesis is in wide
disagreement with the results of this study. There-
fore, the assumption of such a threshold energy can-
not be correct. Contrary to the result of Arnold, et.
al. (Trans. Faraday Soc. 53:738. 1957). a distinct
preference of the Landau- Teller temperature de-
pendence over the exponential T to the - 1 power de-
pendence has been observed. However, the Landau-
Teller theory does not account for the peculiar linear
dependence of the logarithm of collision lifetimes
upon the lowest mode of molecular vibration. Reason-
able values for the range of intermolecular forces
are obuined from this study. (Author)
Malllnckrodt Chemical Lab. , Harvard U. ,
Cambridge, Mass.
MICROWAVE SPECTRUM, BARRIER TO INTERNAL
ROTATION AND QUADRUPOUE COUPLING OF
ACETYL BRCA4IDE, by Lawrence C. Krisher. Rept.
on Contraa Nonr- 1866(14). [19601 18p. 13 refs.
AD- 239 170.
Order from LC mi$2. 40. ph$3. 30 PB 148 563
The microwave spenra of the two acetyl bromide
species, CHaCOBr™ and CHaCOBr"^ have been in-
vestigated in the region 12, 000 to 33, 000 Mc. The
bromine nuclear quadrupole hyperfine splittings were
analyzed to give values for the quadrupole coupling
constants. The observed coupling constants indicate a
considerable deviation from cylindrical symmetry of
the elearic field gradient about the C-Br bond. Sev-
eral of the rotational transitions were further split
into doublets due to the hindered internal rotation of
the methyl group. The quadrupole hyperfine and in-
ternal rotation spUnings were found to be essentially
independent, and analysis of the latter gives a barrier
to internal rotation of 1305 « 30 cal/mole. (Author)
Massachusetts Inst, of Tech. , Cambridge.
SOLID-STATE AND MOLEC^JLAR THEORY GROUP.
Quarterly progress rept. no. 36 on Contract
Nonr- 1841(34). 15 Apr 60, 37p. 26 refs. AD- 235 577.
Order from LC mi$3. 00, ph$6. 30 PB 154 092
Contents:
Spinor waves in a crysul, by E. Ol Thompson
Neutral iron series atom Hartree-Pock solutions.
by
791
R. E. Watson
Computer programs for APW method, by J. H. Wood
Energy bands in semi-conductors, by F. W.
Quelle. Jr.
Automatic codir|g, symbol manipulation and related
topics, by M. IJ. Bailey, M. P. Bamen. E. J. a
Carter, D. E.! Ellis and a C. Plumb
Non-empirical Quantum chemical calculations, by
M. P. Bamert
Programs for evaluation at molecular integrals: four
center integrals, by Ol P. Merrtfield (See also
PB 1S2 863)
Michigan U. Coll. of Engineering, Ann Arbor.
THEORY OF ^WERICAL TOP MOLECULES. THE
VIBRATION- RCrrATTON ENERGIES OF TETRA-
HEDRAL XY4 MOLECULES. I. THE VIBRATION-
ROTATION ENERGIES OF TETRAHEDRAL XY4
MOLECULES. II. THE FUNDAMENTAL V 3 OF
CH4, by K. T. ftecht. Technical rept. on Contract
Nonr-l224(15).ljune 60. 80p. 5 refs. UMRI 03114;
AD- 241 160.
Order from LC|mi$4.50, ph$l2.30 PB 149 567
An outline of
rotation pertur
mation are cla
and it is shown
simplify the ca
ic theory is given. The vibraticn-
llon terms to third order of approxl-
ified according to their symmetry,
this classification can be used to
ulation of the energies. Explicit ex-
pressions are given for the pure vibrational energies
of the simpler Qands. Explicit numerical values are
also given for tjje matrix elements of the Hamiltonian
for the rotational sublevels at types Aj, A2. E, Fi,
and F2 from wjfch the rotational energies at the
vibrational gro«ind state and the infrared active funda-
mentals can be icomputed. (Author)
Optics
Army Signal I^esearch and Development Lab. , Port
Monmouth, NJ J.
INSTRUMENTAinON FOR RADIATICW TRANSFER
MEASUREMENTS OF VISIBLE LIGHT THROUGH
THE ATMOSPfteRE. by Israel Cantor. Oct 60, 50p.
8 refs. USASROL Technical rept. 2152; AD- 249 321.
Order from LQmi$3. 30, ph$7. 80 PB 154 530
The equipment oescribed was developed in support of
an internal research and development program to
measure the ratios of diffuse to direct light trans-
mission factor^ under different weather conditions for
various fields of view. Two main approaches, sup-
ported by a phonographic method, were uken for the
light source an4 receiver. One approach involved a
steady or contiguous light source with a highly sensi-
tive, wide-ran^ logarithmic -type receiver. The
other method included a light -flashing unit with a fil-
tered, pulse -s^sitive receiving set. (Author)
Laboratoire dflnfra Rouge Technique et Applique,
Gif-Sur-Yvette (France).
CONSTRUCTION OF AN INFRA RED SOURCE OF
HIGH LUMINAUCE. Final technical rept. for 1 June-
30 Sep 60 00 COitract DA 91 -591 -EUC- 1130,
01-1413-59. [1^] 37p. 8 refs.
Order from LClmi$3.00, ph$6.30 PB 153 467
Work was devoted to the spectroscopic study of cad-
mium sulphide, either pure or activated with silver or
indium, and mercury sulphide. Besides the red radia-
tion already known from ultra-violet irradiation ex-
periments, a green light of unknown origin was ob-
served, its wavelength being close to that character-
istic of the abosrption limit of cadmium sulphide. This
radiation has no appreciable inertia and is therefore of
interest for optical teleconununication. It apf)ears to
compete with the red or infra-red radiation in which
we are interested, and it probably plays a part in the
destruction of powders by bombardment. An investiga
tion of this phenomenon is therefore important,
especially since an effea at similar origin is observed
in the case of mercury sulphide. The first results of
this research are given, together with some theoreti-
cal observations aimed at its interpretation. (Author)
Naval Aviation Ordnance Test Station, Chlncoteague,
Va.
AIR TO GROUND INFRARED SURVEY STUDY, by
L. C. Parker. Final rept. 13 Mar 59. 80p. 16 refs.
NAOTS rept. no. 9-59; AD-212 087.
Order from LC mlK 50. ph$12. 30 PB 155 437
This report released for sale to^he public 18 Apr 61.
The infrared survey project was conducted to obuin
basic data on the spectral distribution and absolute
value of infrared radiation of militarily significant
ground targets, and to measure transmission losses
under various atmospheric conditions for comparison
and correlation with existing atmospheric attenuation
data. A Barnes Engineering Company radiometer,
model number R-802. was used as the data gathering
device. Seven flights were made in a P2V-6Malrcraft.
followed by five in an HUS- 1 helicopter. It was found
that the P2V-6M was unsatisfactory as a test vehicle,
particularly at low altitudes. (Author)
Naval Ordnance Lab. , Corona, Calif.
INFRARED SPECTRAL EMISSIVITY OF OPnCAL
MATERIALS, by Donald L. Sderwalt. 15 Jan 61, 35p.
55 refs. NAVWEPS rept. 7160; NOCL rept. 537;
AD-250 530.
Order from OTS$ 1.00 PB 171 254
The spearal emissivlty of several optical materials
was measured in the 2- to l5-micron region of the in-
frared spectrum, at temperatures of 40 to ISO'^C. The
emission from each sample was compared with that
from a black body, by means of a modified Beckman
IR-3 spectrophotometer. Spectral emissivlty curves
are presented for germanium, silicon, cadmium
sulfide, KRS'5, glass, and quartz. From these dau,
the atworption coefficient was calculated for ger-
manium and for cadmium sulfide. The results indicate
that this method is an excellent one for meaaurlng lew
values of the absorption coefficient. (Author)
Ultrasonics Lab. , Michigan State U. , East Lansing.
TECHNICAL REPORT NO. 1, by E. A. Hledemann.
Rept. en Cootraa Nonr-2S87(01). Feb 60. 48p.
56 refs. AD- 234 229.
Order from LC ml$3.30, ph$7. 80 PB IS3 120
(Contents:
The diffraction at light by progressive waves at finite
amplitude, by K. L. Zankel and E. A. Hledemann,
792
pub. in die Naturwis senschaften (West Germany)
1958, V. 45, no. 7, p. 157-158
Ibe effect of a progressive ultrasonic wave on a
light beam of finite width, by K. L. Zankel, pub. in
die Naturwis senschaften (West Germany) 1959,
T. 46, no. 3, p. 105-106
BSects of a progressive ultrasonic wave on a light
beam of arbitrary width, by L. E. Hargrove,
K. L. Zankel, and E. A. Hledemann, pub. in The
jnL of the Acoustical Society of America 31: 1366-
1371, Oct 59
A simple method for the harmonic analysis of an
ultrasonic wave, by Walter G. Mayer and
E. A. Hledemann
Diffraction of light by two ultrasonic waves of the
same frequency, by K. L. Zankel
Diffraction of a narrow beam of light by ultrasonic
waves, by IC L. Zankel and E. A. Hledemann
Wayne State U. , Detroit, Mich.
THEORETICAL INVESTIGATIONS ON THE LIGHT
SCATTERING OF COLLOIDAL SPHERES DC
LATERAL SCATTERING AT 90° FROM INCIE«NT
NATURAL AND LINEARLY POLARIZED LIGHT, by
William J. Paogonis, Wilfried Heller, and Nicolaos A.
Bconomou. Technical rept. no. 40 on Contract
Nonr-736(00). 1 June 60, 43p. 8 refs; AD- 239 691
Order from LC ml$3. 30, ph$7. 80 PB 149 097
The Mle-quantlfies l|| , Ij^and their sum are calculated
for nonabsorblng spheres for the parameters y * 90°,
m - 1. 05 (0. 05) 1. 30 and Q ' 0. 2(0. 2) 25. 6. The ex-
perimentally Important specific scattered Intensity
(lu/loC)o *s derived from (i,.-^ I ■ )/2. The periodicities
in the prominent (secondary) i(a)-osciIlations and in the
less pronounced primary and tertiary oscillations are
briefly discussed. (Author) (See also PB 146 351)
Wayne State U. , Detroit, Mich.
■mEORETlCAL INVESTIGATIONS ON THE LIGHT
SCATTERING OF COLLOIDAL SPHERES X. THE
"SCATTERING RATIO" AND DEPOLARIZATION OF
LIGHT SCATTERED AT AN ANGLE OF OBSER-
VATION OF 90°, by Wilfried Heller, William J
Pugonis, and Nicolaos A. Economou Technical rept.
na 39 on Contract Nonr- 736(00). 1 June 60, 27p.
16 refs; AD- 239 690
Order from LC mi$2. 70, phj4. 80 PB 149 096
The scattering ratio, (T , for non absorbing spheres
«nd for an angle of observation, y, at 90° is calcu-
lated from data given previously for m ■ 1.05(0.05)
1. 30 and a - 0. 2(0. 2) 25. 6. The scattering ratio
represents the ratio of the total intensities scattered
from a linearly polarized incident beam vibrating once
psrallel and, subsequently, perpendicular to the plane
of observation. In the present Instance of spheres, the
results are identical with the depolarization In Infi-
nitely dilute systems The experimentally attractive
features of 0* measurements are pointed out and the
precautions to be observed for useful application of
the theoretical data are enumerated. The periodic! -
ties in the ff'(ft')- curves due to the primary, second-
»ry and tertiary undulations in the basic i(Q:)- ^unctions
*re briefly discussed with particular emphasis upon
wleaing conditions of optimum sensitivity of the
nwthod for particle size determinations, character-
ised by an error of not more 1-3 A in particle diame-
ter in monodisperse systems. (Author) (See also
n 149 097)
Solid State Physics
Banelle Memorial Inst. , Columbus , Ohio.
STUDIES, RESEARCH, AND INVESTIGATIONS ON
COMPOUNDS FORMED FROM ELEMENTS OF
GROUPS II AND VI OF THE PERIOWC TABLE, by
C. M. Chapman, B Paris and others. Final rept.
for 1 Oct 58-30 Sep 59 on Contract DA 44-009-eng-
3698. 31 Oct 59, 37p. 3 refs; AD- 229 603.
Order from LC mi$3.00, ph$6.30 PB 153 923
The studies begun on HgSe during the previous con-
tract have been continued The Bridgman rnetind of
ingot preparation has been used almost exclusively.
The best materials prepared have carrier densities at
room temperature on the order of 10^7 cm"^. Anneal-
ing and doping with copper have not reduced carrier
density significantly. A sound ingot produced from
vapor deposition of HgSe is comparable in quality to
ingots prepared by the Bridgman method Optical
transmission measurements on HgSe reveal a depend-
ence of transmission edge on carrier density. As the
carrier density is reduced, the transmission edge
moves to longer wavelengths . An edge at approxi-
mately 12 microns at room temperature was ob-
served in a sample of 3.5 x 10^' cm" 3 carrier den-
sity Reflectivity and transmission data have per-
mitted a rough calculation of the effective mass of
carriers in HgSe. The ratio of effective mass to free-
electron mass was computed to be in the neighborhood
of 0.05. Studies on the HgTe-CdTe alloy system re-
veal that a material of nominal composition
9OHgTe-10CdTe has a transmission edge within the
8 to 14- micron -wavelength region The position of the
edge moves to longer wavelengths with decreasing
cadmium content. The shift of transmission edge with
temperature is on the order of lxl0"*ev/oc. Hall
measurements at low temperature show that the low-
cadmium-content alloys made thus far are p-type,
having a hole-io-electron mobility ratio from 0.035
to 0.01. (Author)
Brown U., Providence, R. 1.
INVESnCATIONS OF SURFACE PROPERTIES OF
SIUCON AND OTHER SEMICONDUCTORS, by
H. E. Famsworth, J. A. Dillon, Jr. and others .
Scientific rept. no. 4, 1 July- 30 Sep 60, on Contract
AF 19 (604)5986, Phases 1 and 2. Oct 60, 30p.
30 refs . AD- 248 540.
Order from LC mi$2.70. ph$4.80 PB 153 849
Contents:
Surface structures and propenies of diamond-
structure semiconductors
Structure of the clean (111) surface
Adsorption rates of oxygen and carbon dioxide
Structure of (100) surfaces
Structure of a cleaved (111) germanium surface
The influence of wet and dry ambients on fast
germanium surface states
Air-vacuum
Dry ambients
The effect of a constant electrical field on fast sur-
face states of germanium
Experimental results
Effects of heat treatment on the conductivity of sill-
con surfaces .
(See also PB 150 208)
793
CSiicago U. , III.
SUMMARY OF RESULTS OF PREVIOUS RESEARCH,
by George W. DeVore. Final rept. on Contract Nonr-
1547(00). (1960)5p. 9 refs.
Order from LC mi$l. 80. ph$l. 80 PB 148 781
A brief summary of the results of research concerned
with the chemidal behavior of elements in natural min-
eral systems a« measured by the fractionation and
distribution of najor and trace elements between the
coexisting minerals.
leG^(
Compagnie G^n^rale de T^l^raphie Sans Fil
(Prance).
PREPARATION i OF U-IV SEMI-CONDUCTOR COM-
POUND MIXTUIRES AM) MEASUREMENT OF THEIR
ELECTRICAL AND THERMAL PROPERTIES, by
H Guernxx. (Quarterly technical status rept. no. 5,
1 Apr-30 June^. on Contract AF 61(052)243. [1960]
13p. 3 refs. At)- 242 540.
Order from Lqmi$2. 40. ph$3. 30 PB 150 545
No change was imade in the preparation of the
Mg2Sn-Mg2Pb tnixture. The preparation of Mg2Ge
was difficult; single crystals of a size comparable to
those obtained with Mg2Sn were hard to obtain, and
the graphite boets were not suited for melting the conn-
pound which roacts with C and sticks to the boat.
Attempts are being made to find a better material for
the boats . The) same difficulties were met in the first
attempts to prepare Ba compounds. Alumina boats
were used successfully in the Ba2Sn co-fusion experi-
ments . Micro«raphic examinations on samples of the
Mg2SnxPbi-x type indicated that as soon as the Pb
proportion was not negligible (about 0.95) separation
into 2 phases (jccurred. Samples exhibiting segrega-
tions became tiomogenous after annealing at SOCPC.
Mg2SnxGei-x ^nixtures were also studied. Ingots
cor res ponding Itox* 0.95, 0.90, andO.lOall showed
segregations. Resistivity measurements confirmed
the order of n^gnitude of the energy gap given in a
previous repoft for Mg2SnxPbi-x mixtures (See also
PB 148 213)
Honeywell Raearch Center, Hopkins, Minn.
EFFECT OF $UP DISTRIBUTION OF THE FRAC-
TURE BEHAVDOR OF MAGNESIUM OXIDE SINGLE
CRYSTALS, bt R. J. Stokes, T. L. Johnson, and
C H . Li . Technical rept . no . 8 on Contract Nonr-
2456(00). Junefeo, 40p. 16 refs. HR-60-479;
AD- 243 103. I
Order from U^ mi$3.00, ph$6.30 PB 150 558
The tensile de^rmation <rf chemically polished mag-
nesium oxide drystals has been correlated with the
distribution of'slip at the onset of plastic flow It two
slip bands , generated on orthogonal f llO) planes ,
happen to intefsect to nucleate a crack before other
slip bands develop nearby, then the crack so formed
is unstable and the cryswl completely brittle. If,
however thereiis a higher density of slip sources
cracks can beqome stabilized by adjacent slip bands
•nd the crystals continue to deform. Sometimes slip
is confined to a single slip band which expands later-
ally to fill theientire gauge length, these crystals are
extremely ductile . The fracture behavior of a given
crystal depends critically upon the relative orienta-
tion, number, thickness, and spacing between slip
bands The density of slip may be increased artifi-
cially when dislocation sources are injected into the
crystal surface by sprinkling with carborundum be-
fore loading. Such crystals are always ductile in ten-
sion. A similar treatment for crystals to be bent
leads to a profound change in their fracture behavior.
(Author)
Laboratoire Central des Industries Electriques
(France).
RESEARCH ON THERMO^GNETOELECTRIC
EFFECTS IN SEMI-CONDUCTOR, by P. Aigrain.
Final rept. for 15 Sep 58-15 Sep 59 on Contraa
AF 61(052)138. [1960] 9p. 1 ref. AFCRC-TR-59-293;
AD- 243 488.
Order from LC mi$1.80, ph$1.80 PB 152 199
An attempt was made to determine whether a study of
thermomagnetoelectric effects, in combination with
magnetoconductance effects could be used to investi-
gate the band structure of semiconductors. Samples
of n- and p-type Mg2Sn were prepared by varying the
rate of crystal growth from the melt; n- and p-type
crystals were produced by growth rates of 75° and
l50°C/hr, respectively. The ingots were either single
crysuls or large -grain polycrystals. Single crystal-
oriented specimens were cut from these; the orienta-
tion was carried out with an X-ray diffractometer
Magnetoconduaance measurements on p-type Mg2Sn at
77<^ yielded values at 910'^ ohm/cm and 200 cc/coul
for oo and Pf^. respectively. These observations, to-
gether with thermoelectric power measurements indi-
cated that the top of the valence band is probably made
up at & single isotropic valley with an effective mass
of (0. 14 * 0.03)mo- The bipolar Nernst effect of
Mg2Sn was large enough to indicate that both Mg2Sn
and Mg2Sn-Mg2Pb have potential value as heat
detectors. . .;
Laboratory of Chemical and Solid-State Physics,
Mass. Inst, of Tech.. Cambridge.
ANNUAL RESEARCH REPORT. Rept. on Govern-
ment-sponsored research. 15 July 60, 63p. 116 refs
AD-243 048.
Order from LCml$3. 90, ph»10. 80 PB 150 642
Solid State and Molecular Theory: Calculations on
atoms, molecules, and solids; Non-empirical quan-
tum chemistry; and Automatic coding. Structure of
5olids by X-Ray and Neutron Diffraction: Order-dis-
order in alloys; Distortion in metals; Neutron diffrac
tion; Magnetic studies; Crystal structures of blo-or-
ganic compounds; Zeolites; and Inorganic compounds
Low Temperature and Thermal Properties of Matter
Statistical thernrKKlynamics; Cryogenic engineering;
Phase transitions and specific heat measurements;
Low temperature physics; and Elastic and thermal
properties of solids J4uclear Magnetic Resonance:
Structural and molecular nxjtion in solids; and High
resolution nuclear resonance spectra: Molecular
Spectroscopy: Far IR spectroscopy; and IR studies d
hydrogen bonding . Interatomic and Iniermolecular
Forces: Scattering of high velocity molecular beams;
and Gaseous diffusion measurements; -Jransition _
>4etal Comtxxinds: Electronic structure of p-diketooe
complexes of metal ions; Tetrahedral Ni(II), tetra-
hedral CoOD. "nd Isonitrile complexes; Thermody-
namics and preparation of B compounds; Sulfoxide
794
complexes; Vibrational spectra d X9SO molecules;
Sjjectral and magnetic properties of tne d" configura-
tion; and Meul carbonyls; Electrical and Optical
fygpertles of Thin Metal Detwsits . Physical Chemis-
gv of Macromolecules: Thermodynamics and statis-
tical mechanics of dilute polymer solutions; and Dy-
Mmics of chain configuration. |^yslcal Metallurgy.
|fe:hanicar Properties of Solids .
Lincoln Lab . , Mas s . Inst . of Tech . , Lexington .
AKnFERROMAGNETIC RESONANCE IN (Cr203)i-x
(Al203)x SINGLE CRYSTALS, byS. Foner. Rept. on
Co«ract AF 19(604)7400. 13 Jan 61, lOp. 16 refs.
JJG-0024; AD-249 573.
Onler from LC ml$ 1.80, ph$ 1.80 FB 154 062
lesults of pulsed field antiferromagnetlc resonance
(APMR) experiments are briefly sununarized for the
nixed crystal system (Cr203) 1-X. (Al203)x as a
function of temperature, and X, where X * 0.003,
0.006, 0.008, 0.06, 0.1, 0.2 and 0.9. The tempera -
aire dependence of the critical field, (2 AlC)l/2 for
pure Cr203 and X ■ 0. 1 are compared in deuil . The
iaciease of (2 AK)1/2 at 4.2 K from about 59 kilo-
puss for Cr203 to 79 kalogauss for X- 0.1 is attri-
bund to a reversal in sign and rapid increase in mag-
altiide of the effective crystalline field contribution to
Ifaeanisotropy energy as X Is increased. AFMR line
widths from 800 to 2000 gauss were observed, but for
X10.2 the line width was almost independent of tem-
pamure for each composition. The decrease at Neel
temperature with increase of X is also summarized.
(Author)
Liaooln Lab. , Mass. Inst, at Tbch. , Lexington.
SOLID STATE RESEARCR Quarterly progress rept.
for 15 Oct 60 on Contract AF 19(604)7400. 21 Dec 60,
lOOp. ill refs. AFCCDD TN-60-1021; AD-249058.
Order from OTS $2. 25 PB 171 573
Contents:
Samiconductor device design
Qiemittry
liuerlals research
tad structure at solids
Microwave and magnetic properties at solids
M^netic materials
M^netlc films
San {conductor components
Display techniques
hyiaterials] Research Lab. , U. at Galtfomia,
leiteley.
THE GROWTH OF PRISMATIC CWSLOCA'nON
LOOPS DURING ANNEALING, by C A. Johnson and
B. R. Parker. Technical rept. no. 20 on Contract
Nanr-222(52). May 60, 22p. 9 refs. Series no. 27,
Umh no. 20; AD- 239 242.
(kder from LC mi$2. 70, phK 80 PB 148 516
Recent observations at the growth of quenched -in
dlskwatloa loops during annealing are discussed. A
nwcfaanlsm for the coalescence at loops is proposed.
Ibe mechanism depends on short-circuit diffusion
iround the periphery at prismatic dislocation loops.
lUs mechanism is contrasted with the theory at loap
cualescence by vacancy diffusion through the matrix.
It is shown that the experimental observations are in
better accord with the short-circuit diffusion theory.
Interpretation of the experlmenul observations on the
basis at the short-circuit diffusion mechanism leads
to a value for the activation energy for diffusion alotig
a dislocation line. For aluminum this value is calcu-
lated to be 0. 7eV. (Author)
[New Jersey] Ceramic Research [Station] Rutgers
State U. , New Brunswick.
AGING OF FERROELECTRICS (PART I). SYMME-
TRY OF THE LOW TEMPERATURE PHASE OF
BA'^JUtA TFTANATE (PART 2) by E. Sawaguchi and
M^PKiners. Technical rept. no. 1, parts 1-2 on
Contraa AF 30(602)1882. 1 July 59. 121p. 21 refs
RADC-TR-59-128; AD-227 737.
Order from LC ml$6. 30, ph$19. 30 PB 150 915
Aging of ferroelectrlcs: The mechanism of aging in
solid solution types of ferroelectrics received major
attention because the rapid aging phenomena is most
convenient for experimental study. The theory previ-
ously developed, which attributes the aging to the
growth and stabilization at a polar anlsotropy, was sub-
stantiated for the case where the polar anlsotropy is
due to composition differences within the ceramic solid
solution, PbxCai-xTi03. Dielectric dau. X-ray analy-
sis, and double hysteresis loop observations were the
{)rlncipal methods used. Barium titanate must derive
its polar anlsotropy from a different mechanism. The
present studies showed that the surface of BaTi03
ceramics has a preferred domain orientation, which is
quite stable. This is most likely a major factor for the
growth and stabilization at a polar anlsotropy. A third
mechanism is suggested by the growth of a polar
anlsotropy caused by gamma of neutron irradiation.
Symmetry of the l6w- temperature phase of BaTlOa: In
order to find the crystal symmetry of BaTlOs below
-80%, the domain patterns and optical properties
were examined using thin (111) plates. Four kinds at
domains were differentiated, these domains are opti-
cally uniaxial. The crystal symmetry proved to be
.rhombohedral. (Author)
Naval Ordnance Lab. , White Oak, Md.
PERMEABIUTY AND PERMTTTIVrrY MEASURE-
MENT OF GARNET AND FERRITE MATERIALS, by
George E.McDuffie, Jr. and J. Richard Cunningham, Jr.
15 July 60, 58p. 11 refs. NAVORD rept. 6742;
AD-245 562.
Order from LC mi$3. 60, ph$9. 30 PB 155 386
This report released for sale to the public 12 Apr 61.
The measurement techniques used in the determination
at the complex permittivity and complex permeability
of toroidal samples of garnet and ferrite materials are
presented. Techniques for permittivity measurementa
are described for the frequency range IKc/s to 20
Mc/s. Permeability measurenients are divided into
two regions: (1) a low frequency range (1 Kc/s to 20
Mc/s) in which windings are used on the toroidal
sample and (2) a high frequency range (20 Mc/s to 4
KMc/s) in which the toroid is measured using a thin
sample method. The instruments and the sample
holders used in the various frequency ranges are dis-
cussed. Equations relating the measured quantities to
the complex material constants are derived in d/OAil
and errors discussed. (Author)
795
Naval Ordnaijce
POLYCRYSTA
Elmer E. Andferson
others. 17 Nair
AD-231 919.
Order from LC
„w^ Lab. . White Oak, Md.
.UNE FERRIMAGNETIC GARNETS, by
•son..]. Richard Cunningham, Jr. and
59. 60p. 36ref8. NAVORD rept. 6741;
mi$3.60. ph$9.30 PB 155 385
This report released for sale to the pubUc 12 Apr 61.
PolycrystalUni samples have been prepared of yttrium
iron garnet (YtC) and a number of rare earth garnets.
The effect of ^onic substitutions on such properties as
lattice constaiits, magnetic moments, dc conductivity,
permittivity apd permeability are discussed. The
magnetic prooerties of garnets can be explained by the
Nefel theory t^ing a 2- or 3-sublanice model. The
permeabiUty ipectrum shows two absorpcion regions,
one due to domain wall processes in the RF region and
the other due to spin resonance in the microwave re-
gion. Electri«:al losses are thought to be due to oxygen
defects and tit reduction of the ferric ion. (Author)
New York U
PHENOMENA
no.
Aug 60, 45p
N. Y.
RESEARCH CN SOLID STATE RADIATION -INDUCED
by Hartmut Kallmann. Quarterly rept.
1. Feb-Abr [60] on Contract DA 36-039-8C-85126
12 refs; AD- 244 598
Order from LiC mi$3. 30. ph$7. 80
PB 153 936
Three aspect* of the conductivity problem are dis-
cussed theordtically: (1) Static phenomena, in which an
equilibrium ataie is reached where no electric current
is flowing; (2) conductivity phenomena, where the re-
lationship beclween current and external voltage and
other parameters is discussed; (3) current multiplica-
tion by high fields. Examples and experimental results
are presented. Dark as well as photoconductivity are
both attributed to an emission of positive charges
(holes from t^ electrode). A theoretical analysis of
this phenomeijon is given. Apparatus was built and
calibrated fot the measurement of the fluorescence of
or^aic solutions at varying temperature. Preliminary
dau are presented. It was found necessary to modify
the apparatus to avoid caviution at elevated tempera-
tures. (Author)
North Caroiina U. , Chapel Hill.
ELECTRIC InD MAGNETIC PROPERTIES OF VERY
THIN FILM$ WITH SPECIAL EMPHASIS ON SUPER-
CONDUCTIVITY, byRolfeE Glover. III. Annual
summary re«. for 1 June 59-31 May 60 on Contract
Nonr-855(08. [1960] I2p. 10 refs. AD- 244 745^
Order from Xmi$2.40, ph$3.30 , PB 152 220
Contents:
Changes in Superconducting critical temperature pro-
duced by electrostatic charging
Effect of strtin on the superconducting transition tem-
perature
Harmonic g^eration
Persistent currents in thin films
146 846)
(See also PB
I^imsylvaria State U. , University Park.
FIELD ION MICROSCOPY OF IRON WHISKERS, by
Erwin W. N/^ller. Rept. on Research on Chemical
Synthesis, Contract AF 33(616)6397. Oct 60, 26p.
10 refs. WADD Technical rept. 60-534; AD-249 773.
Order from OTS $0. 75 ^ 17 1 598
The design, construction and operation of a complete
field ion microscope unit is described. The restric-
tions due to the high rate of field evaporation of iron
are considered. Tliis microscope is used for the study
of the atomic structure of iron whiskers. Indications of
crystal defects such as screw dislocations and Inter-
stitials are found, although the whiskers did usually
not have sufficient strength to withstand the extremely
high field forces. (Author)
Polytechnic Inst, of Brooklyn, N. Y.
GALVANOMAGNETIC AND MAGNETIC PROPERTIES
OF THIN NICKEL- IRON FILMS, by H. J. Juretschke.
Technical rept. no. 8 on Contract Nonr- 839(06).
1 Jan 60, lip. 4 refs; AD-236 220.
Order from OTS $0. 50 PB 171 569
An Investigation was made of the role of magneto-
resistance effects in gal vanomagnetic measurements
on Ni-Fe films of various compositions. Assuming i
reasonable behavior for the magnetization the follow-
ing expression was derived to account for the ex-
perimenul results for the case of a film in the x-y
plane, with current flowing along x: fey/J^=A ^ m^
my -»- HjM m^ whereby "ferromagnetic effect.
J_ = current density,/* -resistivity, M - satu-
Mtion magnetization, m =■ the direction of M, and
R, = the extraordinary Hall constant. With this In-
terpretation, experimenul results indicated that the
behavior of the magnetization In a truly normal field
is unstable with respect to small deviations from the
normal; instead of simply lifting out of the film plane,
the magnetization also spirals through a large angle.
It was thought that galvanomagnetic effects caused by
this rotation could persist to very high fields and
easily distort the Hall slope far above the knee of the
usual Hall curve. The Interpretation of the results
led to the conclusion that since the method is so
sensitive to the actual behavior of the film. It Is
more suitable for an investigation of the fines truaure
of magnetic behavior once the overall properties haw
been established bv some other means.
Purdue U . , Lafayette , Ind .
EXCESS CARRIER UFETIME IN INDIUM ANTI-
MONIDE, by Robert Allan Laff. Technical rept. on
Contract Nonr- 1100(04). 1 June 60. I23p. 20 refs.
AD- 237 970. « , .o «•*
Order from LC mi$6.30. ph$19.80 PB 148 014
Investigation was made using photoconductivity and
photoelectromagnetic effect, of the temperature de-
pendence of lifetimes of excess majority and minority
carriers in n- and p-type indium antimonide samples
of various carrier concentrations . Analysis of the
results leads to a nwdel for the recombination, con-
sisting of a donor center having 2 energy levels wltWi
the forbidden energy gap, at 0.055 and 0.12 ev abow
the valence band. The recombination rates for elec-
tron and hole capture for both levels were obtained.
Dau on p-type samples in the majority carrier
freezeout range indicates that excess holes n«y
796
freeze out onto acceptor centers . Under steady state
without optical excitation between valence band and
acceptors , the holes on the acceptors must'be in
statistical equilibrium with the free holes . An in-
crease in free hole concentration is accompanied by
(D increase of trapped holes in the acceptors . Addi-
tiooal centers of the same type present in crystals as
grown were introduced into p-type material by bom-
bardment with 4.5mev electrons. This result indi-
cates that the centers originate from structural im-
perfections in the crystal lattice rather than from
chemical impurities (Author)
Raytheon Co. , Waltham, Mass .
INVESTIGATION OF THE MICROWAVE PROPER-
TIBS OF FERROELECTRICS, by Georg RuK)recht,
B. D. Silverman, and R.J. Bell. Final rept. for
16 June 58-15 Oct 61 on Contract AF 19(604)4085.
[I960) 109p. 23 refs. S-210; AFCRL-TR-60-37I;
AD-249 871.
Order from LC mi$5.70. ph$l6.80 PB 154 077
The complex dielectric constant of single crystal
strontium titanate and polycrystalline barium-stron-
tium-tiunate has been measured over a temperature
lai^e extending from 90 degrees K to 230 decrees K
and a frequency range from 2.30 to 6.50 kmc . The
real part of the dielectric constant consists of a large
field-independent contribution which obeys a Curie-
Weiss law over the entire range of measurement plus
• smaller anisotropic field-dependent contribution.
The results are shown to be in qualitative agreement
with the theory of ferroelectricity in perovskite
structures as proposed by Slater. The observe^ loss
taiyent consists of a contributioRyWhich is quadratic
in an applied biasing field plus a smaller field-inde-
pendent contribution. The field -independent loss
tai^ent goes through a minimum at about 170 degrees
K with a much steeper rise on the low temperature
side of the minimum than on the high temperature
side. A theory for the temperature dependence of the
field- independent loss tangent is proposed which
agrees with the data to within the experimental accu-
racy. The theory also predicts a contribution to the
loss ungent which is proportional to an applied bias-
ing field; however, the rapid decrease with increas-
ing temperature is not understood. (Author) (See
alsoPB 149 905)
Space Technology Labs. , Inc. , Los Angeles, Calif.
SUPERCONDUCTIVE PROPERTIES OF THIN TIN
FILMS, by Eugene C. Crittenden, Jr. , John N. Cooper
(Naval Post Graduate School) and Frederick W.
Scfcmidlin. 2 Nov 60, 37p. 2 refs. STL/TR-60-0000-
NR356; AD-249 519.
Order from LC mi$3. Oft ph$6. 30 PB 154 232
The niperconductive properties of a carefully pre-
pared family of 8 thin tin films with thicknesses vary-
ing from 0. 03 to 1 . 04 microns were studied in the
temperature range between 1. 5 and 3. 9 deg K. The
films were prepared by vacuum evaporation upon pol-
ished glass substrates cooled to -20 deg C. Film
tUdmesses were measured by Fabry- Peroc interfer-
ometry and were also calculated both from mass
evaporated and frtjm resistance measurements. Criti-
cal temperatures, panicularly for the thinner films,
were substantially above that for bulk tin. presumably
because of tensile stresses. The dc critical currents
as a function of thickness t can be well approximated
by an expression or me form A(l - f(x))/ (I + f (x)),
where A is a constant determined by the temperature
and X is essentially independent of temperature.
(Author)
Stanford U . , Calif .
COMPARISON OF RANGES OF APPLICAWUTY OF
PREDICTIONS OF CREEP BUCKUNG TIME , by
B. M. Lempriere. Technical rept. no. 1 on Contract
Nonr- 225(47). June 60. 30p. 11 refs. SUDAER no. 97;
AD- 240 788
Order from LC mi$2.70. ph$4.80 PB 150 053
The most rigorous theory of the creep buckling of ini-
tially imperfect columns is examined for possible
simplifications . It is found that the influence of plas-
ticity on the life of a column can be ignored under cer
tain conditions characterized by the proportional limit
stress . a creep parameter, the applied stress , and
the initial curvature. These conditions are conven-
iently presented in the form of graphs for steady
creep as represented by the power and the exponential
laws The simplification possible in the regions so
defined permits the application of early theories . For
steady creep these lead to simple formulae which con-
sist of the life determined according to Gerard's
0 Aeronaut. Sci. 23, no. 9:879, Sept. 1956) sugges-
tion multiplied by a correction factor . Some pub-
lished data are examined in terms of the present
ideas and give encouraging agreement with the theo-
retical results , for values of the correction factor
ranging from 0.0074 to 1 .25. (Author)
Stockholm U. (Sweden).
STUDIES ON THE CRYSTAL CHEMISTRY OF TI-
TANIUM, VANADIUM AND MOLYBDENUM OXIDES
AND OF ALKAU WOLFRAM BRONZES AT ELE-
VATED TEMPERATURES, by Ame Magneli , Sven
Westman and others . Final Techincal rept. no. 1 ,
15 Nov 59-14 Nov 60, on Contract DA 91-591-EUC-
1319. Dec 60, 185p. 98 refs. AD-248 112.
Order from LC mi$8.40. ph$28.80 PB 153 721
The mechanism of dissolution of oxygen in hexagonal
close-packed titanium was compared with results ob-
tained for the zirconium-oxygen and hafnium -oxygen
systems. Phase analysis studies on mixed titanium-
/.ranadium oxides in the monoxide region demon-
strated the existence of a probably ordered phase erf
the approxiniate composition Ti9VOi2 in samples
which have been heat-treated at 8000C. Extensive
studies of the ordered phase VO^ _27 ^^® ^^ ^° ^*
proposal of a pair of homometric structures . The ti-
tanium and vanadium sesquioxides have been found to
form a continuous series of solid solutions . The
crystal structure of Ti509 has been refined. Ex-
pressions for the ideal structural properties of the
homologous series Tijj02u- 1 - VjjOja- 1 and
TiQ.2Cr202ix-l have been derived and compared with
observed x-ray daw. The structure of an intermedi-
ary phase in the titanium dioxide-vanadium dioxide
system has been determined, as has also the struc-
ture of VO2 above 7(PC. The crystal structures of
Mo40ii(mon) and M017O47 were refined. The sub-
structure of M010O28 **s derived. The thermal ex-
pansion coefficients have been measured for the hexa-
;r
797
gonal wolfram bronzes of potassium, rubidium and
cesium and for the tetragonal potassium wolfram
bronze. The hex^onal jxxassium bronze shows a
ptwse transition ^t 5450C similar to those exhibited
by the cubic soditim wolfram bronze and WO3.
(Author)
I to.,
Synthetic Mica to. , Caldwell, N. J.
SYNTHETIC MIGA CRYSTAL GROWTH PROGRAM,
by John G . Froeii»el , Edgar C . Worden and others .
Interim technical engineering rcpt. no. 2. 16 Aug-
16 Nov 58. on Co»itract AF 33(600)36853. [1953] lllp.
AD-207 856. «,rr.c.
OnlerfromLCrfl$6.00. ph$18.30 PB 155 154
1
This report released for sale to the public 30 Mar 61 .
This report describes the installation and testing of a
laboratory crystal grower designed specifically for
synthetic mica wprk. Studies of the growth of mica
from high -temperature solutions are included along
with solubility and melting data. A series of plant-
scale experimennal melts is described including the
use of the central heat -sink, controlled cooling sched
ules and precise batch control . The second "pro-
gressive" melt ii described in which large rectangu-
lar electrodes afe utilized for thermal gradient con-
trol. (Author) (^ also PB 154 515)
Synthetic Mica Co. . Caldwell, N. J.
SYNTHETIC MICA CRY^AL GROWTH PROGRAM,
by James G. Frc^mel. Edgar C. Worden and others.
Interim technical rept. no. 3. 17 Nov 58-16 Feb 59. on
Contraa AF 33(400)36853. (1959) 75p. AD-214 354.
Order from LC fiiM- 50, ph$l2. 30 PB 155 155
Thia report released for sale to the public 29 Mar 61.
Methods are beiig developed for growth of Urge
(4" X 6") synthetic mica crystals en a commercial
scale. Special fijrnacing techniques are being evalu-
ated 00 an in-pUnt basis including progressive (step)
melting, controied cooling schedules, seeding meth-
ods and melt super -heating. In the laboratory, special
crystal growing techniques such as zone melting, crys-
tal pulling and thermal gradient crystallization are
under study on lioth mica melts and solutions. This re
port describes isembly and testing of a laboratory
zone -melting apbaratus for synthetic mica crystalliza-
tion. Experiments with a crystal pulling furnace are
also described iHilizing lead borate as a solvent for the
fluor-phlogopitesmica. Pilot-plant scale melts are also
discussed in wh(ch thermal gradients within the melt
are controlled ly the use of a water-cooled heat sink.
Size of crystal growth is correlated to rate d heat
withdrawal. Experiments are also described in which
electrodes are withdrawn from the melt prior to crys-
ullization to eliminate seeding. (See also PB 155 154)
Synthetic MlcJ Co. . Caldwell, N. J.
SYNTHETIC MlCA CRYSTAL GROWTH PROGRAM,
by John G. Froefnel, Edgar C Worden and others.
Interim technical engineering rept. no. 4, 17 Feb-
16 May 59, on^ontraa AF 33(600)36853. [1959] 65p.
AD- 219 020. i „ .,^
OrderfromLC|mi$3.90. ph$10.80 PB 155 156
This report released for sale to the public 29 Mar 6l .
The feasibility was investigated of growing mica crys-
tals from solution by utilizing zone melting equipment.
Crystals about 1/2 x 1/2 In. were grown in a 3-in.
id. x6-in. hi^. Wxon sand crucible which was filled
with a mix of 40% Synihamica 202 synthetic niica and 605^
lead borate. Seeding experiments were made with a
frit of the same composition and with 30 to 60% mica.
Zone melting experiments were performed to deter-
mine the feasibility of using a carbon tube suscepjor;
the material used was K^g6A 12516020^4 The re-
sults are sununarized: a solid mica bar of 3-in.
dlam x 25-in. long was obtained; (2) large single crys-
tals were not present; and (3) long neeedle-like crys-
tals were present, all oriented in the vertical direc-
tion. The need for controlled thermal gradients in 2
directions is cited. Crystals 1/2 in. wide by 2 to 3 in.
long were grown with a zone travel speed of 6 l/2ln./ht
Excellent results were alao obtained with a zone travel
rate of 1/2 in. /hr. but extraction of the crystals from
the ingot was difficult. Pilot-plant scale melts included
(I) a variation Of the controlled thermal gradient, (2)«
refinement of the electrode removal technique, (3) a
progressive melt yielding about 7000 lb of mica flake,
and (4) three controlled seeding melts. (See also
PB 155 155)
Synthetic Mica Co. , Caldwell, N. J.
SYNTHETIC MICA CRYSTAL GROWTH PROGRAM,
by John G. Froemel, Edgar C. Worden, and Philip S.
Hesslnger. Interim technical engineering rept. no. 5,
17 May- 15 Dec 59. on Contraa AF 33(600)36853.
[1959] 77p. AD-230 769.
Order from LCmi$4. 50, ph$l2. 30 PB 155 157
This report released for sale to the public 29 Mar 61.
A series of zone melting experiments indicated that dw
optimum temperature for growing mica crystals is
from 13650 to 1390°C. Progressive melting resulted
in higher yields of 2- to 4-in. crystals than were ob-
tained with 2 elearodes. The mica books produced in
various progressive and zone melting experiments
were delaminated by 4 general techniques including (1)
thermal and pressure, (2) chemical. (3) shock tube,
and (4) ultrasonic. The use of an autoclave and super-
heated steam produced very little delamination after
3 hrs of treatment. An ultrasonic whistle of the
Boucher type operated at a power output of over
10 w/sq cm at a frequency of 9 kc produced some
delamination of the larger pieces. Conclusions in-
clude that (I) horizontal zone melting produced the
most promising results in growing large (12 in. long)
oriented synthetic mica crystals, (2) the use o# a
wedge type seed eliminator was most successful in
eliminating extraneous seeds. (3) melts of synthetic
mica had less carbon contamination than melts from
batch material. (4) larger volume melts produce mica
crystals with less carbon contamination, and (5)
delamination can be accompUshed by ultrasonK; whistle
techniques. (See also PB 155 156)
798
Theoretical Physics
Center for Radlophysics and Space Research.
Cornell U. , Ithaca, N. Y.
BLBCTRON DENSITY FLUCRJATIONS IN A
fU»*A. by E. E. Salpeter. Scientific rept. no. Son
Cbotract AF 19(604)6158 and ARPA order no. 106-60.
I Aia 60, 41p. 16 refs. Research rept. RS 18;
APCRL-TN-60-979 , „,,.*,,
Onler from LC ml$3. 30. ph^. 80 PB 154 272
The spatial Fourier transform ?^^ Is considered for
lave vector ^of the charge distribution of the elec-
tnns In a plasma with particle density n. electron
god lor temperatures T and T,. and Debye length D.
Ttie absence erf a magnetic field, neglect collisions,
and nD^-^** 1 are assumed. The stttlstical average
o' IPu I . is calculated as a function erf 0= 1/kD
MMnlng complete thermodynamic equilibrium; that
component at | P^el ^. wblch keeps In phase with the
ion charge density fluctuations is also calculated. The
frequency spectrum of the time- varying function P^^
It obtained at thermal equilibrium and simplified,
usvinlng the ions mass to be much larger than the
electioa mass, for general values of • and T/Tj.
For small o the main component of the spectrum has
the characteristic Doppler broadening shape corre-
ipooding to the elearon's thermal velocity. For
large a there Is a component with narrow width
corresponding roughly to the ion- velocity Doppler
ipread and v^ry narrow side bands at plus and minus
the frequency d electrostatic plasma oscillations.
(Author) •
General Atomic, San Diego. Calif.
RECOMBINATION AND ATTACHMENT IN IONIZED
GASES, by V. A. J. van Lint. Rept. on Contract
AF 29(601)1225 Aug 59, 67p. 25 refs. GA-1168;
AFSWC TR-59-43; AD- 232 161
Qnler from LC ml$3. 90, ph$10. 80 PB 153 584
An experimental program is described which measures
recombination and attachment of electrons in ionized
gases, with emphasis on oxygen and mixtures contain-
iif oxygen. The experiment was performed by pro-
ducing some ionization in the gas sample and observing
die rate of decrease of the electron density subsequent
to the ionizing event. The ionization was performed by.
the traversal through the gas of a short pulse (2 ^sec)
of 20 mev electrons from an electron linear accelera- .
tor. The electron density was measured by observing
the attenuation and phase shift of an X-band microwave
puaed through the ionized gas. The rate of decrease
cf the electron density was interpreted in terms of
ttuchment, recombination and diffusion of the elec-
trons. (Author)
Maryland U . , College Park .
SURFACE PLASMA OSQLLATIONS OF A DEGEN-
ERATE ELECTRON GAS, by E. A. Stem and
R. A. FerreU. Rept. on Contracts DA 49-170-8C-
1837 and Nonr- 1797(00). Dec 59. 27p. 12 refs. Dept.
of Physics Technical rept 162; AD- 235 929.
Order from LC mi|2.70, ph$4.80 PB 152 180
Following Ritchie (Phys . Rev. 106:874, 1957) the
anomalous characteristic energy losses of energy
lower than the plasmon energy, exhibited by some
metals , are attributed to quantized surface waves of
the degenerate electron gas . The present analysis
studies the dependence on thickness of the oxide
coating, and it is found that a surprisingly thin coat-
ing of only 20 A thick can produce a significant effect.
It is established that a measurement of the dispersion
of the energy loss versus angle of scattering in the
transmission experiment would yield a measurement
of the oxide filni thickness . A further check on the
theory is suggested by a measurement of the angular
dependence of the intensity ot the low-lying charac-
teristic ener^ loss . A special effect is predicted
for non-normaUy incident fast electrons . It should
be found that the intensity panem should fUre away
from the-plane of incidence. Besides these special
angular effects it is predicted that because of the
sensitivity of the surface plasma oscillations to any
surface coating the value of the surface characteris-
tic energy loss can be varied between wide limits by
choosing the appropriate coating. In particular ,
making double films of two different metals should
produce surface characteristic energy losses in be-
tween the bulk characteristic energy losses of the
two separate metals (Author)
New Mexico Sute U. , University Park.
THE STATISTICS OF THE ELECTRICAL MICRO-
FIELD IN AN IONIZED GAS AND ITS RELATION
TO TRANSPORT COEFFICIENTS, by OttoM. Theimer^
Final rept. 00 Contract N9onr-953(06). 31 May 60. 5p.
AD- 242 408. __
Order from LC ml$l. 80. ph$l. 80 PB 149 911
Norfheastem U. . Boston, Mass.
NORMAL -MODE TREATMENT OF PINCH INSTA-
BILFriES, by John Sullivan. Rept. on Contract
AF 49(638)555. May 60. 80p. 25 refs. AFOSR TN-
60-1146; AD- 250 065. ^ ^^
Order from LC ml$4. 50. ph$l2. 30 PB 154 455
The basis of the pinch effect arises from the principle
of magnetic induction and the tendency of parallel cur-
rent conductors to exert a mutual attraction when
carrying current in the same direction. By a consider
ation of particle motion and the hydron^gnetic theory
of the plasma, a relation was established between the
current, linear density of particles and the tempera-
ture in the plasma plnch.j These theoretical results
were compared with experimental results from the
ZETA apparatus and the agreement was reasonably
good. An elementary discussion of the two most prom
inent pinch instabilities was given. In the absence of
an internal axUl magnetic field and exterior conduct-
ing surface the pinch was proved to be m-0 and m-1
unstable for real values of the penuroation wave-
number, |k|. The inclusion of an internal axial mag-
netic field is seen to have an important effect upon the
stability of the pinched plasma.
799
Ohio State U. Research Foundation, Columbus.
THE BASC PRlfliaPLES OF MAGNETOGASDYNA-
MICS, by S. L. |»etrie. Rept. on Contract
AF 33(616)5593. Mar 60, 2iOp. 25 refs . RF proj. 818;
Rept. no. TN(AU)SU)l60-4: ARL-TN-60-121;
AD- 242 346.
Order from LC Aii$2.70. ph$4.80 PB 155 323
This report released for sale to the public 3 Apr 61 .
The basic principles of magnetogasdynamics are col-
lected from the tterature and are examined from an
aerodynamic vie^vpoint . The electromagnetic field
equations are prfesented and explained The thermo-
dynamics , macroscopic equations of nwtion, and the
governing "Boltzmann" equation for an electrically
conducting gas it an electromagnetic field are given
and comparisonsjwlth the nonconducting, field-free
system are madf. The non-dimensional parameters
arisingfrom a dimensional analysis of the system are
discussed and th4 types of solutions possible with their
various relative magnitudes are indicated. (Author)
Riysical ReseaJ-ch Lab. , Space "ftch. Labs. . Inc. .
Los Angeles. <^lif.
NONLINEAR PLASMA OSOLLATIONS, by R W.
Wyld. Jr. 12 Sed 60, 52p. 7 refs. STL/TR-60-0000-
GR303 1
Order from LC Li$3. 60, ph|9. 30 PB 154 154
A study is made a€ nonlinear plasma oscillations in
one dimension Irt a low, but finite, temperature two-
compooent plasT«a. htonlinearities arising from ther-
mal effects and tonlinearities due to finite ion mass
are considered separately. Thermal nonlinearities
are shown to glv^ rise to a nonlinear dispersion re-
lation for a mon|>chromatic wave and to spectral de-
cay, i. e. the migration erf energy in wave number
space. Spectral decay arising from nonlinearities due
to finite ion masis is discussed. A statistical equation
for nonlinear pWsma oscillations, or theory d turbu-
lence d plasma bsclllatlons, is briefly considered.
It is shown that In a two stream plasma a growing
wave generates Iria the nonlinear terms an effective
field which opposes the drift causing
The significance of these effects
for the problem \d collective resistivity Is discussed.
(Author)
uniform electric
the growing wavi ;
Space Tech. Libs. , Inc. , Los Angeles, Calif.
ON THE DETECTION OF ION OSCILLATIONS IN A
MERCURY DISCHARGE, by Burton D Fried and Roy
W. Gould. 9 Ded 60, 15p. 6 refs. STL/TR-60-0000-
GR413.
Order from LC ^i%2. 40. ph$3. 30 PB 154 371
t'
The possibility df using a low pressure mercury dis-
charge to detect ion plasma oscillations is examined.
It is found that (\) collisions will not interfere with the
phenomenon; (2) the current which maintains the dis-
charge will cause the waves to grow (through the rwo-
stream instabilicy) in a time comparable with or less
than the oscillation period. Aside from complications
caused by the fa^t that the maximum growth occurs at
rather short wavielengths (A'SO. 5 mm), detection of
these waves appears quite feasible. (Author)
Space Tech. Labs. . Inc. , Los Angeles, Calif.
THE STABILITY OF PLASMAS IN THE PRESENCE
OF CONDUCTING WALLS, by Carl Iddings. Rept. on
Contract AP 04(647)594. 9 Sep 60, 23p. 6 refs.
STL/TR - 60-0000-9431 6.
Order from LC mi$2. 70. phM 80 PB 154 372
It has been suggested that the presence of conducting
walls can prevent the growth of "flute" instabilities in
magnetically confined plasmas. It is the purpose of
this note to investigate this possibility in two highly
idealized situations. First, the gravitational (Taylor)
instability is considered for a fluid which is confined
between conducting walls. The magnetic field is taken
normal to the conductors. The second problem is the
confinement of a plasma column in the angular section
between two conducting walls. In this case there is no
graviutional field present, the magnetic field inside
the plasma is zero, and outside the plasma the field is
in the <J> direction.
Stanford Electronics Labs. , Stanford U. , Calif.
THE GAS LAW AND THE CONDUCTIVITY OF A
COLLISION-FREE PLASMA, by O Buneman. Rept.
on Contract AF 19(604)5480. 12 Dec 60, 32p. 13 refs.
Technical rept. no. 104-5; AFCRL 103.
Order from LC mi$3. 00, ph$6. 30 PB 154 370
The moment method is used to derive a form of two-
component magneto-gas dynamics for a collision -free
plasma. Closure of the moment equations is achieved
by ignoring variations of fourth moments of the pecul-
iar velocities for each component. This provides a
"fully adiabatic gas law" which represents a generali-
zation of the sir^le or double adiabatic laws in that it
predicts the gyrations of the pressure tensor, as well
as the principal pressures. The currents are calcu-
lated which small perturbing electric fields cause to
flow in each species, in accordance with its own adi-
abatic gas dynamics. A conductivity tensor is thus
deduced. This tensor is compared with that resulting
from rigorous kinetic theory (without closure), for
the case of a uniform plasma. It is found to be identi-
cal with the "warm plasma approximation" which takes
into account temperature to first order. Hence, a
two-component fully adiabatic theory describes super-
sonic phenomena adequately but misses (altogether)
the phenomenon of Landau damping. It could serve to
provide pessimistic stability, tests for nonuniform
(confined) plasmas. (Author)
Thermod)rnamics
Army Rocket and Guided Missile Agency. Redstone
Arsenal, Ala.
ONE- DIMENSIONAL COMPRESSIBLE FLOW TABLES
FOR A PERFECT GAS IN MACH NUMBER INCRE-
MENTS OF 0. 001 (k - 1. 22) ISENTROPIC PROCESS,
by C Hoeblch. Dec 59. 90p. ARGMA TNlHlN-7;
AD- 232 079.
Order from LC mi$4. 80. ph$l3. 80 PB 154 208
Functions are tabulated of Mach numbers for com-
pressible perfect gas. Tlie rado dt specific heats kli
1. 22. The increment used in these tables is suffi-
ciently small (0. 001 Mach number) to eliminate time-
consuming interpolation. These ubles are for sug-
nation temperature change without friction. (Author)
no
kY>wn U. Dtv. of Applied Mathematics, Providence,
R. L
TRANSIENT THERMAL STRESSES IN A CIRCULAR
CYLINDER, by Carl K. Youngdahl and Eli Sternberg.
Ibcfanical rept. no. 8 on Contract Nonr- 562(25).
May 60. 42p. 14 refs. 562(25)/8; AD- 238 040.
Order from LC mi$3. 30. ph$7. 80 PB 148 348
Work is concerned with the transient temperature
jUtrlbution, as well as with the accompanying time-
dependent thermal deformations and stresses, which
arise in an Infinitely long elastic circular shaft If its
surface temperature undergoes a sudden uniform
change over a finite band between two cross -sections,
asl is steadily malnMlned thereafter. The cylinder,
which is supposed to be initially undisturbed and
permanently free from loading, is assumed to be
bORiogeneous and isotropic with respect to both its
Itermal and mechanical response. All material
ptoperties are considered to be Independent of the
temperature. The solution is exact within the frame-
■ork of the linear theories of heat -conduction and
elasticity, provided Inertia effects and the influence
of diermoelastlc coupling are disregarded. The heat-
conduction problem is attacked on the basis of a com-
bined Fourier and Laplace-transform technique,
whereas the associated thermoelastic problem Is ap-
proached with the aid of the Boussinesq-Papkovich
stress functions. Numerical results are presented
(or the case in which the width of the heated (or
cooled) surface band is equal to the diameter of the
iteft. (Author)
Brown U. Div. of Engineering , Providence. R. I.
ON TRANSIENT THERMAL STRESSES IN VISCO-
BLASTIC MATERIALS WITH TEMPERATURE-
DEPENDENT PROPERTIES, by Rokuro Muki and Eli
Sternberg. Technical rept. no. 18 on Contracts
Nonr- 562(20) and Nonr -562(25). June 60. 66p. 23 refs
Noor- 562(20)/ 18; AD- 239 400.
Order from LC mi$3.90. ph$10.80 PB 148 970
A quasi-static analysis of transient thermal stresses
in the linear theory of homogeneous and isotropic
vitcoelastic solids with temperature -dependent physi-
cal characteristics is presented. Exact solutions are
deduced to two specific problems . The first concerns
the transient thermal stresses in a slab of infinite
extent , generated by a temperature field that depends
•rbltrarily on the thickness coordinate and on the
tlnje. The second application aims at the stresses in
a sphere, produced by an arbitrary time -dependent
radially symmetric temperature distribution. The re
suits are particularized for solids of the Maxwell and
Kehrln type, and are compared with the analogous re-
sults for an ideally elastic solid. Numerical
examples are given for the case in which the stress-
inducing temperature distribution Is a solution of the
(uncoupled) equation of heat conduction and corre-
sponds to an instantaneous uniform change ii^''the sur-
face temperature of the solids . These examples in-
clude a quantitative study based on actual test data
for a polymethyl methacrylaie. (Author)
California U. . Berkeley.
EXPERIMENTAL STUDY OF THE DEVELOPMENT
OF DETONATION, by A. J. Laderman and A. K.
Oppenheim. Technical note DR 9 on Contract
AF 49(638)166. Nov 60, 206p. 38 refs. AFOSR TN-
60-1303; AD-250 661.
Order frtxii LC mi$9. 3a ph$31. 80 PB 154 458
The initial bhase of flame acceleration during the de-
velopment'« detonation in stoichiometric hydrogen -
oxygen mixtures, with particular emphasis on the gen-
eration of pressure waves at the flame front, was in-
vestigated. This was accomplished by means of streak
self-light, streak schlieren, and flash schlieren photo-
graphs, together with simultaneous pressure meas-
urement at several locations in the induction regime.
Experimental records revealed considerable detail of
the pressure wave ahead of the flame. They yield also
evidence of the structure of the reaction zone, as well
as information on the transition from a wrinkled lami-
nar to a turbulent flame. Marked influence of the type
of ignition, spark discharge, pilot flame, and glow
coil, has been demonstrated. The flame acceleration
and pressure history computed in this manner were in
satisfactory agreement with experimenul observation.
(Author)
Carnegie Inst, of Tech., Pittsburgh, Pa.
HEAT CONDUCTION IN ALLOYS AND SEMI-CON-
DUCTORS AT LOW TEMPERATURES, byl. Ester -
mannandj. E. Zimmerman. Technical rept. no. 6
on Contraa N6ori-47. T. O. 3. 30 June 51. 60p.
22 refs. ATI -207 933.
Order from LC mi$3. 60, ph$9. 30 PB 154 868
This report released for sale to the public 24 Mar 61 .
With a view to studying the mechanism of heat con-
duction in low -conductivity alloys and semi-conduc-
tors, a method has been devised by which thermal
conductivity of relatively small samples (1/8 to 1/4
inch diameter. 1 to 2 inches long) of various mate-
rials can be measured in the temperature regions
obtainable with liquid nitrogen, liquid hydrogen, and
liquid helium. Preliminary measurements on several
commercial alloys (monel, inconel, and stainless
steel) gave Wiedemann- Franz ratios several times
greater than the theoretical value of 2.45 x 10'^ watt-
ohm/deg2, the deviation being greater for annealed
than for cold-worked spjecimens. Samples of an alloy
of 90j?, copper 10% nickel were prepared with varying
amounts of cold work and with different grain sizes.
Results with these samples were similar to those
obtained with monel and inconel and confirm the
hypothesis of lattice conduction and give a qualitative
indication of the effectiveness of cold work in linuting
lattice conduction. (Author)
Cryogenic Engineering Lab. , National Bureau of
Standards, Boulder. Colo.
A COMPENDIUM OF THE PROPERTIES OF MATE-
RIALS AT LOW TEMPERATURE (PHASE I). PART I.
PROPERTIES OF FLUIDS, ed. by Viaor J. Johnson.
Rept. for Jan 58 -Mar 59 on Thermophysical Properties
of Cryogenic Materials, Contraa AF 33(616)58-4.
Oct 60, 446p. 741 refs. WADD Technical rept. 60-56,
Part I; AD- 249 644.
Order from GTS $6.00 PB 171 618
801
This volume of t je Compendium covers ren properties
of ten fluids. D^nisty, expansivity, thermal conduc-
tivity, specific Heat and enthalpy, transition heats,
phase equilibria, dielectric constants, adsorption, sur
face tension and; viscosity for the solid Liquid and gas
phases of heilunl. hydrogen, tjeoo, nitrogen, oxygen,
air, carbon moiiaxlde, fluorine, argon and methane are
given wherever adequate data could be collected. Data
sheets, j«-imarijy in graphic form, are presented from
best values of d4ta colleaed. 'T'>— <«rnTrr** of the mate-
rial used, other! references and tables of selected
values with appropriate comments are furnished with
each data sheet to document the data presented. Con-
version tables at>d other helpful information are also
included. (Authdr)
. Cryogenic Engineering Lab. , National Bureau of
Standards, Boulder, Colo.
A COMPENDIUM OF THE PROPERTIES OF MATE-
RIALS AT LOW TEMPERATURE (PHASE 1) PART
II. PROPERTIES OF SOUDS, ed. by Viaor J.
Johnson. Repi. for Jan 58-Mar 59 on Thermc^ysical
Properties of Cryogenic Materials, Contract
AF 33(616)58-4 Oct 60, 294p. 323refs. WADD Tech-
nical rept. 60-56, Part II; AD- 249 786.
Order from OT$$4.00 PB 171 619
j
This volume of llhe Compendium covers three proper-
ties of solids. Thermal expansion, thermal conduc-
tivity and specific heat and enthalpy are given for a
number of solid* of interest in cryogenic engineering.
Data sheets, primarily in graphic form, are presented
from best value$ of data collected. The source of the
material used, other references and tables of selected
values with appnopriate comments are furnished with
each data sheet to document the dau presented. Con-
version tables a|Kl other helpful information are also
included. (Authir) (See also PB 171 618) '
th«r)
Cryogenic Engineering Lab. , National Bureau of
Standards, BoUlder, Colo.
A COMPENDIUW OF THE PROPERTIES OF MA-
TERIALS AT LOW TEMPERATURE (PHASE I).
PART III BIBLIOGRAPHY OF REFERENCES
(CROSS- iNDEXED), ed. by Victor J. Johnson. Rept.
for Jan 58-Mar ^ on Thermophyslcal Properties of
Cryogenic Materials, Contract A F 33(616)58-4.
Oct 60, 166p. 1,402 refs. WADD Technical rept.
60-56. Part III; AD- 249 777.
Order from OT$ $3. GO PB 171 620
This volume of the Compendium covers an extensive
bibliography of preferences, (see also PB 171 618,
PB 171 619)
Diamond Ordnance Fuze Labs , Washington, D C.
PELTIER HEAT PUMPS- -APPLICATION PARAME-
TERS AND DEVICE POSSIBILITIES, by Harold F
Gibson. 7Jan6i, lOp. TR-902.
Order from OT$ $0. 50 PB 171 559
The Peltier effect is that property of a material which
causes one end of a rod tp absorb heat and the other to
liberate heat when a d-c current is passed along its
length. The effect is reversed by reversing the direc-
tion of current t^cm, thereby providing a basis for the
design of temperature control devices Materials
developments now make possible the construction of
practical reversible Peltier heal pumps and simple
refrigerators for a variety of military applications.
This report examines both the simple design theory
and the possible applications oi such heat pumps with
particular emphasis on their use in ordnance
elearonics. (Author)
■erv'
Douglas Aircraft Co. , Inc. , Santa Monica, Calif.
TEMPERATURE DISTRIBUTION IN A CONDUCTOR
ADJACENT TO A PLATE OF INFINITE CONDUC-
TIVITY MODEL GENERAL, by R. A. PapetU.
Aug 6a 31p. 3 refs. Rept. no. SM-37766.
Order from LC mi$3. 00. ph$6. 30 PB 150 243
An exact expression which relates the temperature at
the interface of two infinite slabs to time and the mate-
rial properties of the two slabs is obtained for a two-
zone system which Is perfectly insulated on one exter-
nal surface and experiences a constant heat input on
the remaining surface. Two analytical models are dis-
cussed. The principal model considered has infinite
thermal conductivity assigned to one zone. The more
accurate representation considers the effect of finite
conductivities in each zone. A comparison between
the solutions for the two models is made for an alumi-
num-quartz system. The results of the comparison
show close agreement between solutions for the two
models. A Laplace transformation of the time variable
in the thermal conduction equations is employed to ob-
tain the exaa temperature -time relationships. The
analytical results for the principal model are plotted
along with the computer solutions of the same problem
The computer solutions are based on the one-dimen-
sional Runge-Kutta analysis of thermal conduction,
time-variant problems. Qose agreement between
computer and anal^cal results is obtained. This
agreement supports the use of the Runge-Kutta tech-
nique in more complex systems where exact solutions
are not presently available. (Author)
Institute of Science and Tech. , U. of Michigan, Ann
Arbor.
USE OF A LARGE THERMOCOUPLE JUNCTION TO
LOCATE TEMPERATURE DISTURBANCES, by Philip
L. Jackson. Rept. on Project Michigan, Contract
DA 36-039-SC-78801. Jan 61. 19p. Rept. 2900-218-R.
Order from LC mi$2. 40. ph$3. 20 PB 154 508
A temperature disturbance within a large thermo-
couple junction produces a voltage which decreases
with distance from the disturbance. With proper Junc-
tion geometry, resulting voltage residues may be com-
pared at two or more points on the junction. Positions
and magnitudes of temperature disturbances are there
by determined. Useful measurement applications
result. (Author)
Massachusetts Inst, of Tech., Cambridge.
CLOSED FORM EVALUATION OF THE THERMO-
DYNAMIC PROPERTIES OF STEAM IN THE SUB-
CRITICAL REGION, by Jorge C. Boehringer.
Master's thesis. Technical rept. no. 2 on Contract
Nonr- 1841(60). June 60. 73p. 17 refs. AD-238 169
OrderfronlLCmi$4.50. ph»12.30 - PB 148 353
KB
Anempu were made to extend a formulation of the
lliennodynamic propenies of steam to temperatures
bdow the critical temperature in a form suitable for
use in computers . A reasonable degree of accuracy
«as obtained in the region from 10 to about 5cc/gand
lubcrilical temperatures . The shortcomings of this
type of application of Tchebichef polynomials were
illuminated . The IBM programs for determining
coefficients and the thernwdynamic properties from
the polynomial equation were written in such form
ikat they can be easily Interpreted and, with simple
ctenges , can be used with other primitive equations
(j»er other regions for steam or any other substance
The original equation by Keyes , which was used to
leneralize data at very specific points that permit •,
determination of coefficients for the Tchebichef poly*
■omials; was corrected with the help of Program j
M830-669-Boehringer- 3 .
Massachusetts Inst, of Tech. , Cambridge.
HEMISPHERIC TEMPERATURE CONDITIONS DUR-
ING THE YEAR 1950, by Jose P Peixoco. Scientific
rapt. no. 4 on Planetary Circulations Project. Con-
tract AF 19(604)6108. Nov 60. 215p. 10 refs. AFCRL
TO-60-818.
Older from LC mi$9. 6a ph$33. 30 PB 154 449
The method followed In computing the different quanti-
ties which characterize the distribution and the trans-
port of enthalpy and some of the limitations that are
inherent in the approach are discussed. The serologi-
cal results reported here are in good agreement with
results obtained from other independent considerations
such as radiation measurements. In spite of some un-
certainties in analysing the maps over regions of the
hemisphere lacking sufficient observations, it is rea-
sonable to assume that the major features of the en-
thalpy distribution and flow are well represented.
Michigan U. , Ann Arbor.
OH THE STRUCTURE OF PLANE DETONATION
WAVES, by T. C Adamson. Jr. Rept. on Project
Squid. Contract Nonr- 1858(25). June 60. 45p. 13 refs.
Technical rept. MICH-6-P; AD-242 454.
Order from LC mi$3. 30. ph$7. 80 PB 150 534
A perturbation solution is a relatively simple and
accurate solution for the concentration and tempera-
ture profiles, for B « 1. However, Its use Is re-
stricted to Mach number ranges which do not include
the classical Chapman Jougiiet case for reversible re-
actions, if the final Mach number is based on the
equilibrium speed of sound. In view of the physical
Interpretation of the perturbation parameter B, it
seems clear that within the given final Mach number
range, a perturbation solution should hold for most
reactions. Thus, detonations traveling through most
nsctlve mixtures should have relatively small cou-
Jrting between the shock and reactive zones. The first
order reaction rate mechanism is difficult to justify
mechanistically. The explanation accepted by most
baetlcists is that initially a relatively fast second
outer reaction produces active reactant particles
which then decompose slowly at a rate which is first
order. Thus, the overall rate controlling reaction Is
first order. Generally, the pre -decomposition re-
actions are not takep into account in simplified com-
bustion or detonation wave treatments so that with a
given set of parameters. It Is possible to calculate
reaction zones of the order of a mean free path In
thickness, wlihB>l. However, postulating such a
, rate would seem to give results of doubtful practical
value, since in such a case, there would be no way of
producing the necessary supply of active particles
such that the decomposition was still the slowest rate
controlling part erf the reaction. <Author)
Naval Ei^lneerlng Experiment Station, AnnapoUf,
Md.
CONDENSING HEAT TRANSFER RATES OF TUBES
OP VARIOUS MATERIALS, by R. M. Jackson. Jr.
12 July 56, 23p. 1 ref. Evaluation rept. 030038,
AD-115 343.
Order from LC mi$2. 7a ph$4. 80 PB 155 081
TTils report released for sale to the public 28 Mar 61.
Tests on'^seven^Bliafcnser tubes of various materials
were conducted to determine the condensing steam-
to- water heat transfer rates. Comparative tests
under Identical conditions were made on all tubes for
water velocities up to 25 ft/sec. Next to Admiralty
brass, the highest heat transfer rates were obtained
with the titanium and the 90-10 copper-nickel tubes.
(Author)
Naval Ordnance Lab. , White Oak. Md.
FEASIBIUTY STUDY OF THE SPECTROSCOPIC
DETERMINATION OF TEMPERATURE OF AN
ADIABATLCALLY COMPRESSED GAS, by
G. T. Lalos and M. Wolk. Feb 60. 4lp. 4 refs .
NAVORD REPT. 6727; AD-232 696.
Order from LCmi$3. 30. ph$7. 80 PB 154 720
An experimenul study is reported of the feasibility
of measuring spectroscopically the temperature of a
rapidly compressed gas . Ar was adiabatically com-
pressed and the resulting radiation (2100-7000 A)
photographically recorded. In general, the maximum
pressure was 16,000 psi . It was found upon analysis
of the tinr»e- Integrated shot spectrum that the emis-
sion resulted mainly from elements from which the
compressor is made. I.e., Fe, Cu, Cr, Mn, and
Nl. OH bands were also present and were attributed
to thermal dissociation of water vapor existing as an
impurity. Ar lihes were not detected. He was also
used as the test gas and gave the same shot spectrum
as that obtained with Ar. Time- resolved records
taken with a rxxating drum camera could not be used
for temperature determination because of poor dis-
persion. Design and construction of a hi^er-speed
electrical -mechanical shutter ftfr use in conjunction
with a higer dispersion spectrograph made possible
recording the radiation during the top part of the
pressure-time curve. By this means , effective time
resolution was achieved. Emission spectra thus re-
corded demonstrated the feasibility of spectroscopi-
cally measuring the temperature of an adiabatically
compressed gas . (Author)
803
h4aval Ordnance Test Station, China Lake, Calif.
THERMAL- RATE STUMES ON A DOUBLE- BASE
PROPELLANT U$ING A DERIVATIVE DIFFER-
ENTIAL THERN4AL- ANALYSIS TECHNIQUE, by
jackM. P&kuiakJjr. 17 |an 61, lOp. NOTS TP 2610;
NAVWEPS rept. '7612.
Order from LC rtiijl. 80, ph$l. 80
PB 154 440
In derivative dlfflerential thermal analysis (DDTA),
the application c4 a single probe, using an RC network,
makes it possible to yse a less complicated apparatus
to study the thermal changes in a propellant. Because
no reference staidard is necessary, any size sample
may be analyzed! without regard to differences in heat
capacities, probe centering or location 'in the block—
common considerations for sample and reference ma-
terial in differential thermal analysis. The resulting
kinetic studies t|at were performed on a double- base
propellant as a Standard for further propellant studies
show that the first exotherm peak varied with the heat-
ing rate. A negative straight- line relationship was
utilized for heat^g rates from 0. 2 to 5. 55°C/min.
The order of reaction, shape index activation energy,
and frequency fattor were considered. (Author)
hijic
Office of Techi^ical Services, Dept. of Commerce.
Washington, Dl C
HIGH TEMPERATURE RESEARCH (CERAMICS.
GASES. LUBRIOANTS, PLASTICS, ELECTRICAL
AND ELECTRONIC EQUIPMENT. ETC.). Feb 61.
36p. 473 refs. diTS Selective Bibliography SB- 453.
Order from OT$$0. 10 OTS SB-453
A bibliography oif refibrts listed in the two OTS monthly
abstraa journalt: U. S. Government Research Reports
and Technical Translations. Reports bated in this
bibliography wef e added to the OTS colleaion during
the period 1950 jo February 1961. Categories are
arranged as follpws: Ceramics and Refractories;
Gases; Lubricai*8 and Hydraulic Fluids; Plastics.
Paints and Textiles; Electrical and Electronic Equip-
ment; General Research; Translations; and AEC
Reports.
Plastics Lab
THERMCM3YNA
METALS AT
Pohl. Rept. on
AT(07-2)-l. 1
AD- 239 832.
Order from CfT
Princeton U , N J
..C SERL\L ORDER OF THE
[GH TEMPERATURE, by Herbert A.
iiraas DA 36-039-8C-78105 and
60, 14p. Technical rept. no. 58C;
$0.50
PB 171 567
To help evaluate more exactly Just which metal can be
expected to replace which, convenient tables d '
thermodynamic data for important metaUic salts are
assembled. Th*ir use is discussed especially in
regard to effects of low concentration. (Author)
Space Science^ Lab. , General Electric Co. .
Philadelphia, fa.
A NOTE ON T«E THERMAL DIFFUSiCW RATIO
IN DISSOCIATE AIR, by S. M. Scala. Rept. on
Contract AF 49<638)931 . Nov 60, 26p. II refs .
Technical Inforiuttion Series R60SD487; AFOSR
Document no. i; AD-250 672.
Order from LC mi$2.70, ph$4.80 PB 154 510
Great interest has been focus sed recently on viscous
effects at high altitude including non-equilibrium vis-
cous flow within shock waves , boundary layers and
wakes . A realistic treatment of this type of chemi-
cally reacting flow requires a detailed consideration
of the two competing rate processes , diffusion and
chemical kinetics . The mechanism of thermal dif-
fusion is reviewed, and, in particular, a number of
approximations to the thermal diffusion ratio in bi-
nary mixture dissociated air are presented
Wave Propagation
Electrical Engineering Research Lab. , U. of
Illinois, Urbana.
REFRACTIVE INDEX FOR PLANE WAVE PROPA-
GATION IN a' LOSSLESS MAGNETO -lOhJlC MEDIUM,
by G. A. Deschamps. Scientific rept. ho. 2 on Con-
tract AF 19(604)5565. 15 July 60. 25p. 5 refs. AFCRL
TN-60-809.
Order from LC mi$2. 70. ph$4. 80 PB 154 448
The present report deals with the case where the
losses are negligible but where the angle 8 between
the direction of propagation and the magnetic field is
arbitrary.
Electrical Engineering Research Lab. , U . of Texas
Austin.
RADIO WAVE ABSORPTION OF SEVERAL GASES
IN-THE 100-117 KMC FREQUENCY RANGE, by
C. O. Brltt, C. W. Tolbert. and A. W. Straiton.
Rept. on Contract Nonr- 375(01). 10 May 60. 19p.
6 refs. Rept. no. 114; AD- 237 109.
Order from LCmi$2. 40. ph»3. 30 PB 147 840
A technique is described for the measurement of the
absorption characteristics of millimeter radio waves
over a wide pressure range. The results of measure-
ments made with this technique are given for four
gases in the frequency band from 100 to 117 kmcps .
The four gases investigated in near pure state were
carbon monoxide, nitrous oxide, sulphur dioxide, and
nitrogen dioxide . (Author)
Lightning and Transients Research Inst. ,
Minneapolis, Minn.
ARTIFICIAL ATMOSPHERICS PROPAGATION. I. by
J. R. Stahmann. Final rept. for Apr 59-Sep 60 on Cos
tract AF 19(604)5545. Sep 60. 92p. 15 refs. UiT
rept. 373; AFCRL-TR-60-376; AD-249 921.
Order from LCml$5.40, ph$15.30 PB 154 273
The use of a schooner borne high peak power pulse
generator and a 10, 000 foot high altitude wire antenna
permits basic propagation studies at VLF frequencies
over long distances. Peak powers of the cMrder of 30
megawatts have been radiated using this technique.
The first portion of the received waveform is not af-
fected by ionospheric reflections so that a pure grovad
wave may be studied. Similar time standards at the
generator and mobile vanette receiver permit synchro-
nous triggered sweep oecillographlc received pulse re-
cording at various distances from the generator .
Theoretical studies of the waveshape of the radiated
pulse show that antenna shape and orientation affect the
aoi
waveshape radiated in a given direction. Earth curva-
ture effects are also considered theoretically. Pulses
were received at 10. 1(X), and 180 miles from the
generator using the vanette receiver and at 350 and
360 miles by the AFCRL "Inverse loran" network.
Similar pulses were also generated and received by
USASRDL. Waveshape studies reveal some character-
istics which could have been caused by antenna shape
and orientation and also by ionospheric reflections.
However, such reflections are difficult to positively
Identify and more data is required to study effects of
such parameters as terrain, geomagnetic location and
direaion using the. established measurement -
techniques. (Author)
National Bureau of Standards, Boulder, Colo.
PROLONGED SPACE- WAVE FADECXJTS IN TROPO-
a^ERIC PROPAGATION, by A. P. Barsls and Mary
Ellen Johnson. 8 Feb 61, 75p. 10 refs. Technical note
DO. 88.
Order from OTS $2. 00 PB 161 589
This paper contains the results at studies performed
during the last several years on the short-term vari-
ability of tropospheric signals received over within-
tbe-horizon paths. Signal variations of this type have
been termed "prolonged space -wave fadeouts, " as they
are mainly characterized by reductions in signal level
to many decibels below presumably constant values de-
termined from geometrical optics methods. The data
described here were obtained from measurements over
propagadon paths in the Pacific Coast region at South-
ern California, and the continental region of Eastern
Colprado. Fadeouts are analyzed as a function of
carrier frequency, path characteristics, andmeteoro-
kjgical parameters. The study also '"'''•••^^s an evalu-
ation of fadeouts observea over a path using a mountain
peak as a diffracting knife-edge like obstacle between
transminer and receiver. (Author)
National Bureau of Standards, Boulder, Colo.
QUARTERLY RADIO NOISE DATA, SEPTEMBER,
OCTOBER, NOVEMBER 1960, by W. Q. Crichlow.
RT. Disney, and M. A. Jenkins. 31 Jan 61, 65p.
11 refs. Technical note no. 18-8.
Order from OTS $1 . 75 PB 151 377-8
See also PB 151 377-7
RESEARCH METHODS. TECHNIQUES
AND EQUIPMENT
Anderson-Nichols and Co. , Boston, Mass.
MACHINE LANGUAGE TRANSLATION DEVICES
SYSTEM, by John F. McCarthy and James F.
McKenna, Jr. Quarterly progress rept. no. 4. 1 Apr-
30 June 59, on Contract DA 36-039-sc-78123.
21 July 59, 53p. AD- 226 522.
Order from LC ml$3. 60. ph$9. 30 PB 155 030
This report released for sale to the public 27 Mar 61.
A complete coverage of the 3Cope of the development
program for the Machine Language Translation De-
vices System is contained in this report. The cover-
age includes a complete phase breakdown of each of
the tasks of the overall development program including
the development engineering for the Militarized High
Speed Page Printing System, the Code Conversion Sys-
tem, the Keyboard Input Units, and the results of the
investigations for the Integration of the Magnetic Tape
Units, the High Speed Photoelectric Paper Tape
Reader, and the Militarized Digital Communications
Kineplex System. (Author)
Columbia U. , New York.
THE TRANSIENT BEHAVIOUR 6f A SINGLE
SERVER QUEUEING ^ROCESS WITH POlSSONL\N
INPUT, by Lajos Takacs. Rept. on Contract Nonr-
266(33). 8 June 60, 58p. 29 refs. CU-42-60-Nonr-
266(33)MS; AD- 238 288.
Order from LC mi$3.60, ph$9.30 PB 148 401
The following queueing model is ccMisldered: Cus-
tomers arrive at a counter at the instants
Tj, 1 > 1, . . . ,j. The customers are served by m serv-
ers in the order of their arrival. Let Xj denote the
service time of the j-th customer and VJ denote the
interarrival time between the j-th customer and the
(i-l)-th customer. Suppose that the interarrival times
iVj3 and the service times {X;] are independent se-
quences of identically distributed positive random
variables with respective distribution functions
F(x) . p[Vj < xj and H(x) - P[Xj S x}. This queiieing
model is described by the triplet [F(x), H(x), m] . A
modification of the process [F(x), H(x), 1 1 is consid-
ered, supposing that each customer, arriving at a
time when the server is not available, leaves the
queue without tteing served with probability q. The
particular case is ccmsidered when F(x) « l-e'*,
n s -y\xandx 2 0, i.e. , when the input process is a
Poisson process.
Indiana U . , Bloomington .
THE AUTOMATION OF GENERAL SEMANTICS, by
F. W. Householder. Jr. and J. Lyons. Quanerly
rept . no . 3 , 1 Sep- 30 Nov 60 , on Contract
AF 30(602)2184. 16 Dec 60. lip. 2 refs
Order from LC mi$2.40, ph$3.30 PB 153 805
The subject of the research is the syntactic and se-
mantic analysis of scientific English with the aid of
an electronic computer. The primary aim is the de-
velopment of general mechanical routines for the re-
duction of complex sentences to their constituent sim
pie sentences without loss of information-content.
Work so far has been directed to: (1) the collection of
a representative corpus of scientific writing in Eng-
lish; (2) key- punching and soning the preliminary
more limited corpus; (3) the elaboration of dictionary
look-up and suffix-splitting routines for English; (4)
the mechanical determination of the syntactic func-
tion of words and of the boundaries of phrases and
clauses. Progress in these several directions is de-
scribed.
805
Institute for the Study of Metals, U. d Chicago, lU.
HIGH PRESSURE RESEARCH. Annual repc. ncK 9,
July 5S-July 56. ooContraa N6ari-02020. 11956J
nop. 224 refs. AI>-121 182.
Order from LC mi|5 70, ph$l6. 80 PB 154 865
This report releasid for sale to the pubUc 24 Mar 61.
Contents: |
Solid sute studies under high pressure
Studies of high pressure polymorphism to 24,000 bars
by X-ray diffraction
Plastic deformation at single crystals tn tension under
hydrootatlc pressure
Pressure dependenjce and temperature dependence of
the rate at water exchange between Co(NH3)5H20*
and solvent
Improvements in the apparatus for measuring the
thermal conductivity of water as a funaicn of pres-
sure and temper tture
Self diffusion of bromine in AgBr
The internal frictipn at cold worked copper as a func-
tion of temperature and frequency
The elastcresistaUce constants al InSb
Ferromagnetic anlsocropy energy of gadoUnium
A zone refining apparatus
Electrical properties of thin single crystals oC
bismuth
Ultrasonic attenuation in metals
Temperature variptlon of the elastic constants of
AgBr
(See also PB 149 85)
Michigan U. Co|l. of Literature. Science, and the
Arts, Ann Arbo*. ^._.„
REGULAR CAN0^41CAL SYSTEMS AND- FINITE
AUTOMATA, by I- Richard Buchi. Technical rept. on
Contracts Nonr-1 224(21) and DA 3*-03?-8c-780Sr
Dec 59, 28p. lOjefs. 03106; 2794-7-T. AD- 230 541
and AD- 233 478 « .c, ,«
Order from LC it i$2. 70, ph$4. 80 PB 152 135
Regular canonical systems, whose rules of production
are of the form. M-*bx, are discussed. Repilar sys-
tems are interesting because they produce «"> recur-
sive sets of wordB, but not all recursive sets of words
(diagonal argumetit). The main result states that only
a very simple klt*d of set of words is generable by
regular systems.! namely, the regular sets or behav-
iors of finite automata. To a finite automaton with
binary output, a nystem ^ of regular productions can
be adjoined with pn axiom U in such a way that an
input word X is detected by the output of the auto;naton
just in case x is ^-deduciWe from U, i. e. , the set of
words generated by p from U is the behavior of the
finite automaton with binary output. The following
converse is assarted: the set of words generated by
any regular system from a finite set of axioms is the
behavior of somf finite automaton with binary output.
(Author)
Michigan U. Cm. at Literature, Science, and the
Arts, Ann Arbor. „^~r^
WEAK SECOND'ORDER ARITHMETIC AND FINITE
AUTXytAATK, by J. Richard Biichi. Technical rept. on
Nff Grant G-4790, Contracts. Nonr- 1224(21),
D^ a0-0l8-ORDt 16971. and DA 36-039-8C-78067.
Sen 59. 47p. 15 refs. OOR rept. 1863. 3-M; UMRI
^. ^os. 03105; 2722: 2755; 2794-6-T; AD-M8 5Jt
CWer from LC ml$3.30. ph57.80 PB 150 726
A conventional formalism, a weak second-order arith-
metic is derived to replace the formaUsm of regular
expressions as Introduced by Kleene. Theorems
which are equivalent to Kleen's synthesis and analysis
theorems are presented. This result is d interest
for die automaw theory because formulas of weak
seccnd-order arithmetic seem to be more conveniea
than regular expressions for formalizing conditions
on the behavior c< automata. (Author)
Naval Ordnance Lab. , Corona, Calif.
FOUNDATIONAL RESEARCH PROJECTS. Quanerly
rept July-Sep 60. 15 Dec 60, 80p. 31 refs . NAVWEPS
rept". 7157; NOLC rept. 533; AD-249 659.
Order from LCmi$4. 50. ph$12. 30 PB 154 071
Contents:
Communication stochastlcs
High temperature polymer program
Infrared atomic spectra
Magnetization reversal
Semiconductor physics
Small antennas and microwave solid state devices .
(See also PB 152 035)
Stanford Electronics Labs. , Sanford U. , Calif.
ADAPTIVE SWITCHING QRCUITS. by i Wldrowand
M. E Hoff. Rept. on Contract Nonr-225(24).
30 June 60. jtOp. 18 refs. Technical rept. no. 1553-1;
SSeVliSi'LC ml». 00, ph|6. 30 PB 150 227
An adaptive pattern classification machine (called
"Adaline'. for adaptive linear) has been devised to
illustrate adaptive behavior and artificial learning.
During a training phase, crude geometric patterns are
fed to the machine by setting the toggle switches in a
4x4 input array. Setting another toggle switch tells
the machine whether the desired output for the par-
ticular Input pattern is -hi or -1. All input patterns
are classified into two categories. The system learns
a little from each pattern and accordingly experiences
a design change. After training, the machine can be
used to classify the original panerns and noisy (dis-
torted) versions of these patterns. At present the
purely mechanical adaption process is accomplished
by manual potentiometer -setting. A means of auto-
mating this is being developed which makes use of
multi-aperture ferromagnetic devices. Solid-state
adapcivelogical elements will result that should ulti-
mately be suitable to be microminiaturized. Net-
works of such elements would be very effective in
pattern recognition systems, Information storage
and retrieval -by-class If icatlon systems, and self-
repalrii^ logical and computing systems. (Author;
^
806
Communication Theoiy
Dynamic Analysis and Control Lab. , Mass . Inst, of
Tech . , Cambridge .
CHARACTER RECOGNITION AND PHOTOMEMORY
STORAGE DEVICES FEASIBIUTY STUDY, by
D. M. Baumann, F. T. Brown and others. Second
summary rept. RM-7692-3 on Contract Nonr-
1841(41). [1960] 78p. 2 refs. AD- 237 108.
Order from LC mi$4.50, ph$12.30 PB 147 787
A study was conducted to determine the feasibility of
high speed photoelectric scanning of printed material
The desired goal is to develop a system that will scan
and encode printed matter In a fashion suitable for
digital computer input. Photoelectric character recog-
nition, related optics , and photomemory development
•re discussed. A theory of weighted area scanning is
presented which yields an analog voluge by means of
a photocell. (See also AD- 203 709)
Electronic Research Lab. , U. of California,
IPBerkeley.
ERROR BOUNDS FOR CONTINUOUS CHANNELS, by
A. J. Thomasian. Rept. on Contract Nonr -222(53)
28 Apr 60, 27p. 9 refs. Series no. 60, Issue no. 278.
Order from LC mi$2. 70, ph$4. 80 PB 148 502
A general inequality Is obuined for bounding the error
probability of a channel when the signal and noise may
be continuous but time Is discrete. The inequality
permits a constraint on the channel inputs. Application
is made to the band- limited channel with white
(jauBsian noise and an input average power constraint.
(Author)
SOCIAL SCIENCES
Applied Mathematics and Sutlstlcs Labs. , Stanford U.
Ciltf
EDGEWORTHS BARTER PROCESS AND WALRAS'
TATONNEMENT PROCESS, by Hlrofuml Uzawa.
Technical rept. no. 83 on Contract Nonr-225(50)
10 May 60, 28p. 16 refs, AD-237 459.
Onler from LC ml$2. 70. phH 80 PB 147 843
A formulation of Edgeworth's barter process (the two-
good case) is given for a general nnodel of exchange.
Ilie stability problem of the process is discussed in
relation to that of Walras' tatonnement process (Ele-
cs of Pure Economics. 1954X (Author)
Applied Mathematics and Statistics Labs. . Stanford
U.. Calif.
A NOTE ON THE CLASSIFICATION OF TECHNI-
CAL INVENTIONS, by Hlrofuml Uzawa andTsunehiko
Watanabe. Technical rept. no. 85 on Contract
NoBr-225(50). 30 June 60. 13p. 2 refs; AD-240 160.
Order from LC mi$2. 40, ph$3. 30 PB 149 523
Hides' classification of technical inventions is gener-
alized to the case in which there are more than two
factors of production. The economic unit is assumed
to produce an output using certain factors of pro-
duction. The production functlon(|> (vj %''^^
specifies the maximum quantity of the output that can
be produced by using the factors at production by
quantities Vj, . . . , v at the 8Ute*of technology T
The assumption Is made that T may be represented
by a real number, and the production function satis-
fies all the neoclassical conditions. The production
factors are assumed to exhaust all -the productive fac-
tors that are limltational to the economic unit.
Applied Mathematics and Statistics Labs. . Stanford
U. . Calif.
A THEOREM ON NON- TATONNEMENT STABILITy,
by F. H. Hahn and Takashi Negishl. Technical rept.
no. 82 on Contract Ncmr- 225(50). 4 May 60, lOp.
6 refs; AD-237 454.
Order from LC mi$l. 80. ph$l. 80 PB 147 842
Under certain assumptions concerning the progress of
exchange out of equilibrium, the stability of the com-
petitive equilibrium system Is shown to be quasi -
stable.
California U. . Los Angeles.
BARGAINING EXPERIMENTS: AN EXPLORATORY
STUDY, by David H. Stem. Doctoral thesis. Rept.
on Management Sciences Research ProJ. [Contract
Nonr -233(02)] June 60. 290p. 120 refs. Research
rept. na 66; AD- 242 538.
Order from LC ml^lLia ph$44.10 PB 152 114
A variety of hypotheses about bargaining behavior are
tested by means of laboratory experiments with
human subjects. It is the methods and techniques of
experimentation, rather than the results, which are
of primary interest. These methods and techniques
fall into several categories: (1) formulating a bargain-
ing model; (2) realizing the abstract model in a fash-
ion which enaibles hypotheses to be conveniently tested
(3) controlling the laboratory environment so that
only the variables included in the model will affect
behavior; (4) measuring die variables; (5) suting
hypotheses; and (6) designing the experiments so that
one may use in jcood conscience the techniques of
statistical analysis one wishes to use. It is urged that
the experiment results be viewed as illustrations of
how modem statistical methods can be used In con-
Junction with laboratory eacperlments to study eco-
nomic behavior, rather than taken of face value as
conclusions about how people bargain. (Author)
Documentation
Armed Services Technical Information Agency,
Arlington, Va.
GUIDELINES FOR USING ASFIA DESCRIPTORS.
Feb 61. I7p.
Order from OTS JO. 50 PB 171 519
807
Drastic changes ai the philosophy of subject Indexing
were undertaken when the Armed Services Technical
InfcrnMtion Agency (ASTIA) recently automated its
information retrieval functions. A Thesaurus ol ASTIA
Descriptors was tleveloped to take the place of the
Ai>'riA^>u5ject Hqadings. The concepts behind the
arrangement of tlje Thesaurus, the development of its
vocabulary, and ttte use of the terminology, for both
input and output operations are discussed. The use of
"open-ended tern|s" such as trade names, nomen-
clature, project titles, and the like is also explained
as supplementing the descriptors for retrieval
purpxDses. (Auth<^)
ZatorCo. , Canibridge, Mass.
THE APPLICATION OF SIMPLE PATTERN INCLU-
SION SELECTION TO LARGE-SCALE INFORMA
TION RETRIEVAL SYSTEMS, by Calvin N.Mooers.
Rept. or Contract AF 30(602)1900. Apr 59, 26p.
7 refs. ZTB 131;JRADC-TN-59-157; AD-215 434.
Order from LC nk%2.70, pb^dO PB 155 068
This report releajsed for sale to the public 24 Mar 61.
Simple panem inclusion selecticMi coding for informa-
tion retrieval can| speed up the serial scanning rate ci
some present retrieval machines 4 to 25 times. It
may also make possible machines with simpler hard-
ware or selective circuits. One present device has a
potential retrieval scanning rate al 36 million items
per hour with pattern inclusion selection. Set against
the advantages c€ this method at coding are certain
peculiarities or limitations: (1) retrieval prescriptions
can be formed by conjoint descriptors only (combined
only by AND), anfl (2) the coding method produces a
small fraction of extra noise selections. For many
retrieval applicadons, particularly with some very
large collections, these peculiarities are at less
importance than tjie gain in scanning speed- The
conditions under Which simple pattern inclusion
selection can be advantageously used are stated, and
the code system 4esign rules are given. (Author)
MISCELLANEOUS
Naval Research Lab. , Washington, D. C
REPORT OF NRL PROGRESS. May 61.
Order from OTS %i. 25, $10 00/year PB 171 318
Contents:
Articles:
Accurately Oriented A DP Crystal Plates and Lenses for
Electro-Optic Shutters, by S. I. Slawson and
J. W. Davisson
Radiation Behavior of Electrical Materials and Com-
ponents for Space Vehicles, by J. W. Kallander and
J. F. Weller
Scientific program:
Electricity: Method of establishing the best voltage
levels for future naval aircraft
Mechanics: Navy high -impact shock machines for
lightweight and medlumweight equipment
Metallurgy and Ceramics: Gas analysis system cali-
bration check. Slow growth and rapid propagation of
cracks. Procedure for the evaluation of fracture
toughness of pressure -vessel materials. Effect of
environment on the fatigue properties of Type 316
stainless steel and Iconel X at ISOO'^F. Density of
liquid bismuth and of dilute solutions of copper in
bismuth. Mechanical properties of refractory alloys.
Effect at phosphate on the corrosion o< steel in aque-
ous media at 316oc
Nuclear and Atomic Physics: Lithium, beryllium, and
boron in the primary cosmic radiation. Monte Carlo
calculation of gamma -ray slab penetration
Radio: Distribution of reflecting cross sections of sat-
ellites. Selection of an atmospheric refractivity
model for radar range -height -angle charts. Cathode
research (thermocouple errors)
Solid Sute Physics: Optical masers. Compressibility
at a luminescent center
SouKt Effect of hydrostatic pressure on a variety of
illuminating devices, miniature and subminlature
electron tubes, and glass tubing
ATOMIC ENERGY COMMISSION REPORTS
Reports may be purchased in accordance with instructions on the inside front cover of die U S
GOVERNMENT RESEARCH REPORTS. As PB numbers are not indicated, order by series andliUJ^r.
Tbeae reports may also be consulted at any ABC Depository Ubrary. A list of these libraries may be
obtained from the U. S. Department of Copunerce, Office of Technical Services, Washington 25, D. C.
Reproduction in whole or part of any report listed herein is encouraged by the U. S. Atomic Energy
Commission, subject to the approval of authors or originating sites. General inquiries from the indus-
trial press about AEC-developed information should be directed to the Industrial Information Branch
Atomic Energy Commission, Washington 25, D. C.
General, Miscellaneous, and Progress
Reports
Chemical processing technology.
ress report for July througn Septembe
by
Quarterly prog
„ft :;>eptember 1960,
J, R. Huffman and others. Phillips Petroleum
Company, Atomic Energy Division, Idaho Falls,
kkbo. Feb 61. Contract AT(10-l)-205. 69p.
Order from OTS. $1.50. IDO-14540
Ground motion studied at hi
— ByW
incident overpreasure.
It high incioent oyerpr
R. PerretandJ. W. Wistor. Sandia
Corporation. Albuquerque, N. Mex. Oct 57.
Decl. August 31, 1960. 42p. Order from LC.
Mi $3. 00, ph$6.30. ITR-1405
Applications of ultrasonic energy. Progress report
no. 16 covering period from June 1, "l959 throu^
July 31, 1959. Aeroprojects. Inc.. West Chester,
Pa.. Aug 59. Contract AT(30-1)- 1836. 44p.
Order from LC. Mi $3. 30, ph $7. 80 .
NYO-2570
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending September 10, 1954,
by A. W. Savolainen. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. Oct 54. Decl. with
deletions December 2, 1959. Contract W-7405-
eng-26. 152p. Order from LC. Mi $7. 50,
ph$24.30. ORNL- 1771 (Del.)
808
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending June 10, 1955, by
A. W. Savolainen. Oak Ridge National Labora tor y,
Oak Ridge, Tenn. July 55.
November 13, 1959. 179p.
Mi $8.70. ph$30.30.
Decl. with deletions
Order from LC.
ORNL- 1 896 (Del.)
Aircraft nuclear propulsion project quarterly prog-
ress report for period ending June 10, 1956, by
A. W. Savolainen. Oak Ridge National Labora-
tory. Oak Ridge, Tenn. Sep 56. Decl. with
deletions Ctecember 2, 1959. Contract W-7405-
eng-26. 257p. Order from LC. Mi $11. 10,
pii$39.60. ORNL-2l06(Pts. l-5KDel.)
Concealment of underground explosions, by A. L.
Latter. RAND Corporation, Santa Monica, Calif.
Mar 60. Contract AT(1 1-1)- 135. 7p. Order
from LC. Mi $1 .80, ph $1 , 80.
RM-2562-AEC
Seniiannual progress report for the period ending
Jtitie 30, 1960. University of California, Schwl
df Medicine, Los Angeles, Calif. 1960. Contract
AT-04-1-GEN-12. 73p. Order from LC.
Mi $4. 50, ph $12. 30. UCLA-460
Seismic decoupling for explosions in spherical
cavities, by W. M. Adams and D. S. Carder.
University of California, Lawrence Radiation
Laboratory, Livermore, Calif. Sep 60. Con-
tract W-7405-eng-48. 27p. Order from LC.
Mi $2.70, ph $4.80. UCRL-5843
Shear and compressional velocity measurements, by
R. J. Swain and others. United Electro Dynamica
Inc. , Pasadena, Calif, and University of Califor-
nia, Lawrence Radiation Laboratory, Livermore,
Calif. Apr 60. Contract W-7405-eng 48. 64p.
Order from LC. Mi $3.90, ph $10.80.
UCRL-5993
Use of large cavities to reduce seismic waves from
underground explosions. Final report, by R. F
Herbst and others. University of California,
Lawrence Radiation Laboratory, Livermore,
Calif. Sep 60. Contract W-7405-eng-48. 60p.
Order from LC. Mi $3. 60, ph $9. 30.
UCRL-6165
Biology and Medicine
Research in radiobiology Semi-annual report of
work in progress on the chronic toxicity program,
by T. F. Dougherty. University of Utah, College
of Medicine, Salt Lake City, Utah. Sep 60.
Contract AT(11-1)- 119. 143p. Order from LC.
Mi $7.20, ph $22.80. COO- 222
809
Investigatioo (rf ipe epizootic and potentially epizoot-
ic diseases of mioe. Final report for June 15,
I95?^=^ptember 14, 1958. by K. B. Murphy and
W, C. Moag Roscoe B. Jackson Memorial Lab-
oratory, Bar Harbor. Me. Oct 60. Contract
AT(30-1)-153&. 18p. Order from LC. Mi $2.40,
ph$3.30. NYO-7147
Strontiuni and a Icium metabolism in man. Final
— report, byA. R. Schulert. Columbia University,
Lamont Geological Observatory, Palisades, N. Y.
July 60. Contract AT(30-i)- 21 16. 36p. Order
from LC. Ml $3. 00. oh $6. 30. NYO-9131
Ml $3.00, ph$6.
Biology divlBion semiannual progr'
— period ending August 15. 1966. Oak
al Laboratory. Oak Ridge,
tract W-7405-eng-26. 208p
Mi $9. 30, ph. $31. 80.
ess report for
idge Nation -
enn. Oct 60. Con-
Order from LC.
ORNL-2997
Final scientific report on therapeutic uses of r><^o-
— active coiloitjs, by P. F. . Hahn. Meharry Medi-
cal College, Cancer Research Laboratories,
Nashville, Ttnn. July 60. Contract AT(40-1)-
269. 41p. Order from LC. Mi $3.30, ph $7.80.
^ ORO-311
To investigate and evaluate radioisotopes for tele -
therapy Final report for September 1. ^954—
TOi^ilstTl. 1^5^, ByH. 5. Weens. Emory Uni-
versity, 5ch«»ol of Medicine, Atlanta, Ga. 1959.
Contract AT(40-1)- 1759. 70p. Order from LC.
Ml $3. 90, p»|$10.80. ORO-312
Study of the heailing at corneal wounds with radio-
active isotoaesrwith special reference to the
plastic artificial cornea, by W. Stone. Jr.
Harvard University, Massachuaeus Eye and Ear
Infirmary, Qoeton, Mass. 1960. Contract AT
(30--l>-1909. 13p. Order from LC. Mi $2.40,
ih$3.30. ■ TID-5823
Sonae effects
females.
OCX
X rays on longevity in l||fa;g|Myc<Mi
M. Clark. University of Deta-
ware, "Newark, Dela. and Oak Ridge National
Laboratory, Oak Ridge, Tenn. [19581. Contract
AT(30-1)-1752. 21p. Order from LC. Mi $2.70,
ph$4.80. , TID-6053
External localigation of brain-tumors employing
aitron-enjitting isotopes. Progress report for
xwitron-eniitting isotopes. Progress report l
uly 1. 195^uly i. i9bb. General Hospital,
MaM- ai» Ceoeral Hospital. Physics Re-
Johns Hopkins University. School of Hygiene and
Pul^lic Health, Baltimore, Md. (nd). Contract
AT(30-1)-2481. 7p. Order from LC. Mi $1.80,
ph$1.80. TID-6590
Technical progress report for February 1. 1906—
— January 31, 1961. byA. B. Burdick. Purdue
Research Foundation. Lafayette, Ind. Oct 60.
Contract AT(ll-l)-856. 4p. Order from LC.
Ml $1.80, ph$1.80. TID-6833
Quality of Sr^ analyses on hyman bone- Interim
technical report, by J. Laurence Kulp. Columbia
University, Lamont Geological Observatory,
Geochemical Laboratory, Palisades, N. Y. May
60. 29p. Order from LC. Mi $2.70, ph $4.80.
TID-6841
I ton.
Con-
search Laboratory, Boston. Mass. July 60.
tract AT(30t-l)-1242. 33p. Order from LC.
Mi $3.00, i^ $6.30. TID-6220
The effects of onizing radiations on helminth para -
sites. Annual prepress report, by E. L. Schiller.
Studies on chemical protection against radiation-
induced intestinal injury. Period covered June 1,
l»5»_|uly 1. 1^, byE. E. Schwara and
B. Shapiro, Albert Einstein Medical Center.
Philadelphia. Pa. Oct 60. Contract AT(30-1)-
2406. 22p. Order from LC. Mi $2.70,
ph$4.80 TID-6868
Irradiation effects on the central nervous system.
Progress report covering period January 1. 1960
to date, by V. Nair and others. University of
Chicago. Chicago, 111. Sep 60. Contract AT
(ll-l)-847. 8p. Order from LC. Mi $1.80,
ph$1.80. TID-6874
Cancer research program of die division of biology
and medicine, by L. O. Jacobson and others.
Division of Biology and Medicine. U. S. Atomic
Energy Commission. Washington, D. C. Nov 60.
94p. Order from OTS. $2.25. TID-11132
Studies of the graft host interaction in die mouse.
— Tliesis, by I. McRae. University of California,
Lawrence Radiation Laboratory. Berkeley, Calif.
Oct 60. Contract W-7405-eng- 48. 82p. Order
from OTS. $2.00. UCRL-9448
Distribution and excretion of niobium-95 '" '^a"
following daily adminiBtraiion in the food and
drinking water, by R.G. Thomas and others.
University of Rochester, Atomic Energy Project,
Rochester, N. Y. Dec 60. Contract W -7401-
eng-49. 21p. Order from OTS. 50 cents.
* UR-584
Biomedical and aerosol studies associated with a
field release of plutonium, by R. H. Wilson and
otfiers. University of Rochester, Atomic Energy
Project. Rochester. N. Y. Nov 60. 70p. Order
from OTS. $1.75. WT-1511
810
Chemical Separations Processes for
Plutonium and Uranium
Efficiency of a three inch Higgins column, by V. C.
Vaugheaand others. Massachusetts Institute of
Technology, Engineering Practice School. Oak
Ridge, Tenn. Dec 56. Decl. with deletions
Gaober 2, 1957. 2lp. Order from LC.
Mi $2.70, ph$4.80. AECD-4294
Eyilibrlum extraction characteristics at alkyl
amines and nuclear fuela metals in nitrate sys-
tems. Quarterly progress report no. v for tSe
Quarterly progress repor
July I -September 30, 19!
period July I -September 30, 1959, by E.A .
Mason and V. C. Vaughen. Massachusetts Insti-
nite at Technology, Cambridge, Mass. Dec 59.
22p. Order from LC. Mi $2.70, ph $4.80.
AECU-4631
Solvent extraction: pulse wave studies and pulse
generator developtnent. Quarterly report for
period August lOJ 1951 to November 10, 1951,
perioa August
by J. E. Conai
J. E. Conaway and A. C. Jealous. Oak Ridge
National Laboratory, Oak Ridge, Tenn. Dec 51.
Decl. March 23, 1960. 17p. Order from LC.
Mi $2. 40. ph$3.30. CF-51-12-32
Chemical technology division unit operatioos section
monthly progress report. May 1958. by J. C.
Bresee and others. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. Sep 58. Contract W-
7405-eng-26. 67p. Order from LC. Mi $3.90,
ph$10.80. CF-58-5-50
Power reactor fuel reprocessln]
byB. B. Klima.
nuechanical phase,
«k Ridge Rational LaboratoryT
Oak Ridge. Tenn. Sep 59. Contract W -7405-
eng-26. 36p. Order from LC. Mi $3. 60,
ph$9.30. CF-59-8-88 (Suppl. I)
Operadon of TNX evajporator, by G. S. Nichols and
E. S. Occhipinti. Du Pont de Nemours (E. I. ) k
Company, Explosives Department, Wilmington,
Del. Oct 54. Decl. April 21, 1960. Contract
AT(07-2)-l. 27p. Order from LC. Mi $2.70,
ph$4.80. DP-82
Pi-2-amyl 2-butylpho8phonate as an extractant for
the recovery of uranium and plutonium. by T. H.
Siddall, III. E.I. du Pont de Viemours & Company.
Savannah River Laboratory. Aiken, S. C. Feb
61. Contract AT(07- 2)- 1. 16p. Order from
OTS. "50 cents. DP-548
Oxidation of uranium (IV) by oxygen and nitrous acid,
by A. L. Slade. E. I. du Pont de Nemours &
Company. Savannah River Laboratory. Aiken,
S.C. Feb 61. Contract AT(07 -2)- 1. 12p. Order
from OTS. 50 cents, DP-554
The In-line estimation of the sulfamate loo coocen-
tration In the Purex IBP stream, by F. A. Scott.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Aug 57.
DecL March 28. 1960. Contract W-31-109-
Eng-52. lOp. Order from LC. Ml $2. 40,
ph $3 30. HW-51673
Technology for the reprocessing o< nonproduction
reactor fu^s; budgst activity Z790. 'Quarterly
report, by V. R. Cooper. General Bectric
Conpany, Hanford Atomic Products Operation,
Richland, Wash. Mar 58. Decl. June 25, 1959.
Contract W-3l-109-Eng-52. 9p. Order from
LC. Mi $1. 80. ph $1. 80. HW-55419
Trough-tray dlssolver, by R. W. McKee. General
Electric Company, Hanford Atomic Products
Operation, Richland, Wash. June 59. Contract
AT(45-1)-1350. I8p. Order from LC.
Ml $2. 40, ph $3. 30. HW-60823
Technology of non -production reactor fuels repro-
ces sing budget activity 2790. Quarterly report.
ig budge
R. Coo
by V. R. Cooper. General Electric Company.
Hanford, Atomic Products Operation. Richland,
Wash. Aug 60. Contract AT(45-1) -1350. 12p.
Order from LC. Ml $2. 40, p*i $3. 30.
HW-66191
The interaction .trf bare systems at containers.
fert n, by L. Geller. Carbide and Carbon
Chemicals Company, K-25 Plant, Oak Ridge,
Tenn. Dec 52. Decl. March 7, 1960. 26p.
Order from LC. Ml $2. 70, ph $4. 80.
iCS-347
McCabe-Thlele graphical solution of uranlum-
thorium partitioning from 30^^ TBF-AMSCO"soi-
yent, byA. D. Ryon. Oak Ridge National
Laboratory, Oak Ridge. Tenn. [ndj. Contract
W-7405-eng-26. 13p. Order from GTS.
50 cent*. ORNL-3045
Plutonium extraction from nitrate and sulfate solu-
tions by amines and organophosphorus compounds,
by D. E. Homer and C. F. Coleman. Cak
Ridge National Laboratory, Oak Ridge, Tenn.
Mar 61. Contract W-7405-eng-26. 62p. Order
from OTS. $1.50. ORNL.-3051
Chemistry
Diffusion-controlled dissolution of zirconium in
molten uranium with monotonlcally increasing
temperature, by G. H. Golden. Jan 61. Coifrtract
W-31-109-eng-38. 43^). Order from OTS.
$1-00. ANL-6294
811
Preliminary economic evaluation of the fluoroxpro-
cess for manijacturlng UF4 and UFfe, by J. E.
ring uf 4
Oak rtldge National Laboratory, Oak
Sep 55. Ded. April 28, 1960.
Moore.
Ridge, Tenn.
Contract W-74p5-eng-26.
LC. Mi $2, 4C . ph %3. 30.
I6p. Order from
CF-55-9-51
Determination of oxygen in oxide films by neutron
activation anatysis, by J. W. Winchester and
others. Oak Ridge National Laboratory, Oak
Ridge, Tenn. |July 59. Contract W-7405-eng-26.
60. Order frdm LC. Mi $1. 80, ph $1. 80.
CF- 59-7 -128
Chemical technology division monthly progress re-
port for chemical development section B, Febru-
ary 1960, byl. E. Blanco. Oak Ridge National
Cateratary, Cpk Ridge, Tenn. May 60. 37p.
Order from Lt- Mi $3. 00, ph $6. 30.
CF-60-3-84
Comment on caldulatlons by Lietzke and Stouriiion
on concentratijons of species in aqueous UQ2SO4
solutions as a'function of temperature, by R. S.
Greeley. Oak; Ridge National Laboratory, Oak
Ridge, Tenn. Mar 60. 3lp. Order from LC.
Ml $2. 40, ph $3. 30. CF-60-3-139
ment sec
ojogy
Chemical technology division, chemical develc
3 re.
Oak Ridge l^ational Lab-
VfST
tion t progress report for Tune - "I'^y
K- Bi Brown. Oak Ridge National La
oratory. Oak Ridge. Tenn. Sep 60. 60p. Order
from LC. Mi, $3. 30, ph $7. 80. CF- 60-7 -108
The transport an^ thermodynanuc properties of
saturated and 'compressed heavy water, by A. A.
Bishop. Westinghouse Electric Corporation,
Atomic Power
60. 58p. Order from LC.
Department, Pittsburgh, Pa. July
Summa ry technical report for the .
'n, 1953, by J. S. Brei ten stein
Ml $3. 60. ph$9.30.
CVNA-54
riod April 1,
1953 to June ;
National Leat^ Company of Ohio. Cincinnati,
Ohio. July 5;
AT(30-1)-11
Mi $6.90. ph 521.30.
Decl.
134p.
March 7, 1960. Contract
Order from LC.
FMPC-255
Chemistry of urinium- -oxygen systems. First
quarterly rep )rt for the^ period January i,~79«)-
March3J, 1^30, by J. T. Porter. General
Atomic Division, General Dynamics Corporation,
San Diego, Cilif. Apr 60. Contract AT(04- 3)-
167 7p. OrlerfromLC. Mi $1. 80. ph $1. 80.
GA-1385
rimer for bi:
prinv
Good
A study of the effectiveness of using a zinc chromate
:umastic paint, by F. A. Koehler.
year Atomic Corporation, Portsmouth, Ohio.
Apr 60. Contract AT(33-2)-l. 5p. Order
from LC. Mi %l. 80, ph %l. 80. GAT-T-797
X-ray diffraction data for nine new salts containing
hexafluoro-uranate(V), -molybdate (V) , or -tung-
state (V) ions, by K. Ralston and F. J. MusiL
Goodyear Atomic Corporation, Portsmouth, Ohio.
Oct 60. Contract AT(33-2)-l. 22p. Order from
LC. Mi $2. 70. ph $4. 80. GAT-T-839
The identification and determination of trace
amounts of rare earths in graphite By
activation, by A, M, Ross" Hanford
neutron
Works.
Richland, Wash. Sep 49. Decl. January 29,
1960. Contract W-31-109-Eng-52. 28p. Order
from LC. Mi $2. 70. ph $4. 80. HW- 14337
Analytical technical manual, by R. A. Schneider
and K. M. Harmon. Hanford Atomic Products
Operation, Richland, Wash. Feb 61. Contract
AT(45-1)-1350. 278p. Order from OTS. $3.50.
HW-53368
Coalescence in pulse columns, by W. R. Hamilton.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. June 59.
DecL February 4, 1960. Contract W-31- 109-
Eng-52. 70p. Order from LC. Mi $4. 50,
ph$l2.30. HW-56281
osg
gen removal with hydrazine. Interim report,
jyT. F. Demmitt. General Electric Company,
Hanford Atomic Products Operation. Richland,
Wash. Jan 60. Contract AT(45-1)- 1350. 9p.
Order from LC. Mi $1. 80, ph $1. 80.
HW-63534
Preparation of stoichiometric U308' by G. S. PeUt
and C. A, Kienberger. Oak Ridge Gaseous
Diffusion Plant, Oak Ridge. Tenn. N v 60.
Contract W-7405-eng-26. i5p. Order from LC
Mi $2.40, ph$3.30. K-1424
Tabulated values of thermal diffusion column shape
factors for the Lennard-Jones (12-6) potential,
niiis report supersedes LAMS-2413), by B. B.
Mclnteer and M. J. Reisfeld. Feb 61. Contract
W-7405-ENG-36. 56p. Order from OTS. $ I. 25.
LAMS-2517
Process development quarterly report. Part I. by
A.E. Ruehle and J. U. Shepardson. Mallinckrodt
Chemical Works, St. Louis, Mo. Apr 55. Decl.
June 10, 1960. Contract W- 14- i08-eng-8. 116p.
Order firom LC. Mi $6. 00, ph $18. 30.
MCW-1373
812
Analytical procedure manual for a radium recovery
process, by R. W. Moehier. Monsanto Research
Corporation, Mound Laboratory, Miamisburg,
Ohio. Sep 52. Contract AT-33-1-GEN-53. 37p.
Order from OTS, 75 cents. MLM-591
Final safety evaluation of plutonium processing to be
performed ip the heavy element processing
facility, by J. Watcher. Martin CompanyT Nu-
clear Division, Baltimore, Md. Sep 60. Contract
AT(30-3)-217. 56p. Order from 0T5. $1.50.
MND-P-2396
Vaporization of zirconium oxide, by M. M. Nakata
and others. Atomics International. A Division
of North American Aviation, he. , Canoga Park,
Calif. Apr 61. Contract ATXll-l)-GEN-8. 14p.
Order from OTS. 50 cents. NAA-SR-6095
The radiochemistry of the rare earths, scandium,
yttrium and actinium, by P. C. Stevenson and
W. E. Nervik. University of California, Law-
rence Radiation Laboratory, Livermore, Calif.
Feb 61. 282p. Order from OTS. $3.00.
NAS-NS-3020
The radiochemistry of technetium, by E. Anders.
Enrico Fermi Institute and Department of
Chemistry, Univerai ty of Chicago, Chicago, 111.
Nov 60. 50 p. Order from OTS. 50 cents.
NAS-NS-3021
The radiochemistry of the rare gases, by F. F. 1
Momyer, Jr. University of California, Law-
rence Radiation Laboratory, Livermore, Calif.
Oct 60. 55p. Order from OTS. 75 cents.
NAS-NS-3025
Self-diffusion of chromium in nickel-base alloys,
by R. B. Evans, III and others. Oak Ridge
National Laboratory, Oak Ridge, Tenn. [ndj.
Contract W-7405-eng-26. 38p. Order from OTS.
$1.00 ORNL-2982
Kinetics of the catalyzed oxidation of hydrogen, car-
bon monoxide, and methane by oxygen in a flowTng
stream of helium, by C. D. Scott Oak Ridge
Niational Laboratory, Oak Ridge, Tenn. [ndj.
Contract W-7405-eng-26. 2Ip. Order from ?
OTS. 50 cents. ORNL-3043i
Experiment on continuous release of fission gas dur-
ing irradiation. An interim report, by rTm.
Carroll and C. D. Baumann. Oak Ridge National
Laboratory, Oak Ridge, Tenn. [nd. ], 25p. Or-
der from OTS. 75 cents. ORNL-3050
Analytical chemistry division annual progress
Analytical chemistry division annual progress re-
port for period ending December 31, i960, by
M. T. Kelley and C. D. Susano. Oak Ridge Na-
tional Laboratory, Oak Ridge, Tenn. 1960.
Contract W-7405-eng-26. 121 p. Order from
OTS. $2.50. ORNL-3060
Superposition of forced and diffusive flow in a large-
gjre graphite, by R. B. Evans III and others,
ak Ridge National Laboratory, Oak Ridge, Tenn.
[nd]. Contract W-7405-eng-26. 61p. Order
from OTS. $1.75. ORNL-3067
The effect of structure on the reactivity of polyfl
organic compounds. Final report, by J. Hine
uoro
and others. Georgia Institute of Technology,
Engineering Experiment Sution, Atlanta, Ga.
Mar 60. Contract AT(40-1)-2084. 4^. Order
from LC. Mi $3.30. ph $7,80. ORO-265
A study of the extraction of the rare earths by
acetylacetone. Thesis, by W. B. Brown. Uni-
versity of Kentucky, Lexington, Ky. 1959. Con-
tract AT(40-I)-2124. 71p. Order from LC.
Mi $4. 50, ph$ 12. 30. ORO-271
The inipurity analysis of americium solutions, by
A. J. Johnson and E. Vejvoda. Dow Chemical
Company, Rocky Flats Plant, Denver, Colo.
Apr 60. Changed from OFFICIAL USE ONLY
May 19, 1960. Contract AT(29-1)- 1106. 26p.
Order from LC. Mi $2.70, ph $4.80.
RFP-194
Quarterly report for July 1, 1960- -September 30.
1960. Mellon Institute, Radiation Research
Laboratories, Pittsburgh, Pa. Oct 60. Contract
AT(30-1)-2310. lOp. Order from LC. Mi $1.80.
ph$1.80. RRL-45(Q-13)(NYO-9164)
Vacuum ultraviolet spectroscopy. Bibliography, by
M.Comstock. Brookhaven National Laboi^itory,
Upton, N. Y. Aug 60
Mi $2. 40, ph$3.30.
23p. Order from LC.
TID-3905
Trends in the stabilities of.some rare earth chelates.
Thesis, by A. S. Tompa. Fordham University,
New York, N. Y. 1960. Contract AT(30-l)-906.
81p. Order from LC. Mi $4.50, ph $12.30.
TID-5761
Resonance in radiation effects. Technical report no.
1, by H. J. Gomberg and others. University of
WTchigan, Michigan Memorial -Phoenix Project,
Ann Arbor, Mich. Feb 60. Contract AT(1 1-1)-
684. 42p. Order from LC. Mi $3.30, ph $7.80.
TID-5797
813
Resonance radUtipo effecta of low e«^rgy mooo-
cfaronmtic x-raya on cacalase. Thesis, byA.H.
Emmons. Uoiveraity at Michigan, Ann Arbor,
Mich. 1959. Contract AT(ll-l)-684). 122p.
Order from UJ.
Mi $6.00. ph$18.30.
TID-5798
Synthetic resins f0r liquid- liquid extractor constnic-
tlon. Report 234 period covered August 31, 1958
to February 9, 1959, by P. A. Lincoln. Michi-
gan Chemical Corporation, St. Louis, Mich. Apr
.V». 8p. Order from LC. Ml $1.80, ph $1.80
TID-6416
Polyngrlzatloo of|vinyl compounds in the crystalline
BUte, by H. Morawetz. Polytechnic Institute,
Polymer Research Institute, Brooklyn, N. Y.
1959 Cootradi AT(30-1)-1715. 21p. Order
from LC. Ml 12.70. ph $4.80. TID-6457
An immunogeoetiC study of the mechanisms of prc-
tection against' radiation death by treatment with
haemopoietic tisaues. Annual progress report
for December 1, 1959 to Aui
newal proposal: December
30. 1961, by G. Hoecker7~
t 31, i960. Re-
1960 to November
Universidad Chile,
Santiago. Chil« Aug 60. Contract AT( 30-1)-
2488. 18p. Order from LC. Mi $2.40, ph$3.30
TID-6531
Thermodynamics and conductance of simple electro-
lytes in polar organic solvents. Progress report
no. 4 for peripaFebnary 1, 1960- -September"
30, 1960 and pproposal for renew 1 of ContracTT
Oct 66. Contract AT(30-1)-1999. Up. Order
from LC. Mi 12.40, ph $3- 30. TID-6652
E3iploeive8--A bibliography, by C. J. Wensrich.
university of Cabfornla, Lawrence Radiation
Laboratory, Uvermore, Calif. July 60. Con-
tract W-7405-eng-48. 21p. Order from LC.
Mi $2. 70. Dh |4. 80. UCRL-6055
ict W-7405-en
$2.70. phi4
Studies on the cafboxydismutase system and related
nMterials. by^J. 6. Pon. University of Califor-
nia, Lawrence) Radiation Laboratory, Berkeley,
Calif. Aug 60. Contract W-7405-eng-48. 195p.
Order from OTS. $2.75. UCRL-9373
Dp. $2.
The spectrochem|CTl determination of impurities in
zirconium and'Zircaloy usingthe silver chloride
carrier technique, by R. F. Farrell and others.
Westlnghouse Electric Corporation. Benis Plant,
Pittsburgh, Pa, June 59. 9p. Order from LC.
Ml $1.80, phSl.80.
WAPD-CTA(GLA)-l62-l(Rev. 3)
A compilation of the basic physical properties erf
light water, by B.N. Nelson. Westlnghouse Elec-
trlc Corporation, Bettis nant, Pittsburgh. Pa.
Aug 56. 44p. Order from LC. Ml $3. 30,
ph$7.80. WAPD-T-401
Evaluation of crud deposits on PWR blanket bundles,
by R. D. Oldenkamp and others. Westinghouse
Electric Corporation, Bettis Atomic Power
Laboratory, Bittsburgh, Pa. Jan 61. Contract
AT-ll-l-GEN-14. 31p. Order from OTS.
75 cents. WAPD- 1X1-261
Controlled Thermonuclear Processes
Astron thermonculear reactor, by N. C Chrlstofiloe.
University of California. Lawrence Radiation
Laboratory. Uvernwre. Calif. 1958. Contract
W-7405-eng-48. 29p. Order from LC. Mi $2.70.
ph$4.80. UCRL-5032
Criticality Studies
Practical methods for calculating reactivity of
homogeneous uranium compounds, by J. L. Feuer-
bacher. Goodyear Atomic Corporation. Ports-
mouth. Ohio. Oct 59. Contract AT(33-2)-l.
22p. Order from LC. Mi $2.70, ph $4.80.
GAT-T-692
Proposed method for treating hydrogen displacement
effects in critical ntess measurements, by P. F.
Cast. Hanford Works, Richland, Wash. May 52.
Etecl. February 24. 1960. 12p. Order from
LC. Mi $2. 40, ph $3. 30. HW-24454
t Engineering and Equipment
An empirical modification of nucleation theory and
its application to boiling heat transfer, by Y. P.
Chang. Argonne National Laboratory, Argonne,
III Feb 61. Contract W-31-109-eng-38. 34p.
Order from OTS. 75 cents. ANL-6304
A temperature distribution analysis along a diermal
ramating fin of nonuniform thickness, by M. J.
Janlcke and L. C Just. Argonne National Labora-
tory, Argonne, 111. Feb 61. Contract W- 31 -109-
eng-38. lOp. Order from OTS. 50 cents.
ANL-6308
Scale 'Up or down" analysis for prototype test. Alco
ProuOcts, Inc. , Sdjenecudy, N. Y. May 60.
814
Contract AT(ll-l)-666. 74p. Order from LC.
Ml $4. 50, ph$12.30. APAE-66
Aerosol generator design.
:kKai
Letter report, by J.
Roeinskiand ]. Stoclcham. Illinois Institute of
Technology, Armour Research Foundation,
Chicago, 111. Oct 60. Contract AT(1 1-1)- 626.
3p. Order from LC. Mi $1.80. ph $1.80.
ARF-3127-15'
In-line gamma monitoring, by T. S. Mackey. Oak
Ridge Nadonal Laboratory, Oak Ridge, Tenn.
.^ug59. 16p. Order from LC. Mi $2. 40,
ph$3.30. CF-59-8-101
Thermal characteristics of fluid flow in pipes, by
D. B. Hinton. Oak Ridge National Laboratory.
Oak Ridge, Tenn. Sep 60. 22p. Order from LC.
Mi $2.70, ph$4.80. CF-60-9-116
The effect of gas film resistance in diffusion from a
porous septum into a fluid stream, by A.T^
Saunders. Oak Ridge National Laboratory, Oak
Oct 60. lOp. Order from LC.
CF-60-10-40
Ridge, Tenn.
Mi $2.40, ph$3.30.
Hanford controlled potential coulometer. by R. E.
Connally and F. A. Scott. Hanford Atomic
Products Operation, Richland, Wash. July 60.
Contract AT(45-1)- 1350. 26p. Order from OTS.
75 cents. HW -65919
A finger ring ionization chamber for the measure-
ment of production plutoniom hand doses, by
L. G. Faust. General Electric Company, Han-
ford Atomic Products Operation. Richland, Wash.
July 60. Contract AT(45-1)-1350. 13p. Order
from LC. Mi $2.40. ph $3.30. HW-66088
A new power revenue metering concept, by R, J.
Thomas. Union Carbide Nuclear Company,
Paducah Plant, Ky. June 59. Contract W-7405-
eng-26. 20p. Order from LC. Mi $2.70.
ph$4.80. KY-296
Operational history of the Paducah plant power load
anticipator from July 1958 throu^ August 1959,
byE. M. Jones and R. J. Thomas. Union Car-
bide Nuclear Company, Paducah Plant, Paducah
Ky, Mar 60. Contract W-7405-eng- 26. 26p.
Order from LC. Mi $2. 70, ph $4. 80.
KY-322
Table of coolant properties, by W. S. Scheib, Jr.
California Research and Development Company,
Uvermore, Calif. Jan 53. Decl. November 24,
1959. 6p. Order from LC. Mi $1.80, ph $1.80.
LWS- 24654
Pressure drop throurfi the reactor pressure vessel,
J. E. Gingrich. Atomics International. A Divi-
sion of North American Aviation, Inc. , Canoga
Park. Calif. Oct 57. 9p. Order from LC.
Mi $1.80, ph $1.80. NAA-SR-Memo-2I79
Sintered metal filters for sodium coolant systems,
by J. S. McDonald. Atomics International. A
Ciivislon of North American Aviation, Inc. ,
Canoga Park, Calif. June 58. lOp. Order from
LC. Mi $2. 40, ph $3. 30. NAA-SR-MenK>-2830
Calculated burnout heat fluxes for santowax-R, by
E. Baumeister. Atomics International. Division
of North American Aviation, Inc. , Canoga Park,
Calif. May 59. 8p. Order from LC. Mi $1.80,
ph$1.80 NAA-SR -Memo- 3860
NaK free convection cooled shaft freeze seal for
SRE pumps, by F. Perez. Atomics Intematioaal.
Division of Nordt American Aviation, Inc. ,
Canoga Park, Calif. June 59. 22p. Order frtMn
LC. Mi $2.70, ph$4.80. NAA-SR -Memo- 3984
Use of teflon in ultrahigh vacuum systerns, by W.J.
Lange and H. Riemersma. Westinghouse Elec-
tric Corporation, Research Laboratories, Pitts-
burgh, Pa. Jan 59. Contract AT(30-1)-2176.
7p. Order from LC. Ml $1.80, ph $1.80.
NYO-8704
Development of hi^ speed electron accelerator
structures. InKrim report no. 1 1 for February
1, 1960- April 30. 1960. by J. A. Baicker and
others. Etevld Sarnoff Research Center, Prince-
ton. N.J. 1960. Contract AT(30-1)- 1958.
24p. Order from LC. Mi $2.70, ph $4.80.
RIB-44
Adding a seventh dial to the L^eds and Northrup G-2
Mueller Bridge, by J. L. Hartley. Sandla Corpor-
ation, Albuquerque, N. Mex. Aug 60. lip.
Order from LC. Ml $1, 80, ph $1.80.
SCTM-277 -60(27)
Production of relay under controlled conditions,
by K. V. Newton. Bendix Aviation Corporation,
Kansas City. Mo. 1959? Contract AT(29-1)-613.
27p. Order from LC. Mi $1.80, ph $1.80.
TID-6259
Hydrodynarnic aspects of nucleate pool boilitig
Part I. The region of isolated bubbles, by N.
Zuber. Ramo^ooldridge. Division at Thomp-
son Ramo Wooldridge Inc. . Canoga Park. Calif.
Jan 60. 60p. Order from LC. Mi $3. 60,
ph $9. 30 , TID-6338
815
N. Mex.
ph$1.80.
High powered »P^^ cap switches, by E. L. Kemp.
Los Alamos Scientific Laboratory, Loe Alamos.
I960. lOp. Order from LC. Mi $1.80,
TID-6670
Standardiz.ation in the design and constriiption of
' all
electronic inslrumentation and cuotrot systems,
by J. G. Nish. University of California, Law-
rence Radiatldn Laboratory, Livermore, Calif.
I960. Contract W-7405-eng-48. 37p. Order
from LC. Mil$3.00, ph$6.30. UCRL-5964-T
A 3
r i)r
»pectronr>eter Ibr study of neutron activitation of
beryllium-7 at a function of energy, by W. T.
Boyer, Jr. Uifiversity of California, Lawrence
Radiation Labfcratory, Livermore, Calif. May
60. Contract W-7405-eng-48. 38p. Order
from LC. Mi $3.00. ph $6. 30. UCRL-6005
Optimization of molecular flow conductance, by L.
L. Levenson 4nd others. University of California,
Lawrence Radiation Laboratory, Livermore,
Calif. Aug 60. Contract W-7405-eng-48. 25p.
Order from Lp. Mi $2. 70, ph $4. 80.
UCRL-6014
Measuring reactor neutron spectra with threshold
detectors. R. J. Grader. University of Califor-
nia, Lawrenct Radiation, Livermore, Calif.
Sep 60. Contract W-7405-eng-48. 17p. Order
fromLC. Mi $2.40, ph $3. 30. UCRL-6089
Isoetatic pressirc at Lawrence Radiation Laboratory,
by P. J. Crunte. University of California. Law-
rence Radiatiin Laboratory, Livermore. Calif.
1958?. ContitctW-7405-eng-48. Up. Order
fromLC. Mii$2.40. ph $3. 30. UCRL-6149-T
Axial variation cjf transient temperatures in an in-
finite hollow (^ylinder. Thesis. 'by R. J.
Scavuz.<;o, Jr. University of Pittsburgh, Pitts
burgh. Pa. 1 >59. 48p
Mi $3. 30. ph
$7.80.
Order from LC.
WAPD-T-934
Geolc)gy and Mineralogy
Atmospheric mo sture data for thermal attenuation
«
aphe
aolei
roblems, by
Ibuquerque,
from LC. Mi
B. N. Charles. Sandia Corporation,
N. Mex Dec 59. 12p. Order
$2.40. ph$3.30.
SCTM- 394- 59(15)
Health and Safety
Atmospheric tritium analysis. Technical prom-esa
report no. 2, by E. W. Barrett and L. Hueoner
University of Chicago, Chicago, III. Feb 60.
Contract AT(ll-l)-636. 33p. Order from LC
Mi $3.00, ph$6.30. AECU-4739
Scavenging of particulate matter in connection with
nuclear-powered ships. Scientific report no ."1.
Theoretical dissertation on diffusion and deposi-
tion of radioactive particulate matter in connec-~
tion with nuclear -powered ships. Appendix tf:
Graphs of shape variables ancl area as a function
of diffusion parameters and velocity of depositioTi
Illinois Institute of Technology. Armour Research
Foundation. Chicago, 111. Jan 58. Contract AT
(ll-l)-586. 69p. Order fromLC. Mi $3.90,
ph$10.80. AECU-4138(App. B)
Safety, health physics, and operating procedures
for chemical technology division teryllium fa^l-
ity byK. S. Warren and L. M. Ferris. Oak
TfiHge National Laboratory. Oak Ridge. Tenn.
June 60. 13p. Order from LC. Mi $2.40,
ph$3.30. .CF-60-6-64
Fallout program quarterly summary report for
December 1. 1960 through March I 1961.~by
E.P.Hardy. Jr and others. United States Atomic
Energy Conimission, New York Operations Office,
Health and Safety Laboratory, New York. N.Y.
Apr 61. 212p. Order from OTS. $3.00.
HASL-Ul
Radioactive decontamination of the 60 ton overhead
crane in a separations facility, by G.C. Loud
and A. J. Low. General Electric Company,
Hanford Atomic Products Operation, Richalnd,
Wash. Aug 57. 12p. Order from LC. Mi $2. 40,
ph$3.30. HW -52734
Atmospheric organic concentration in the OMR criti-
cal facility assembly room, by L. A. Mountford.
Atomics International. Division of North Ameri-
can Aviation, Inc., Canoga Park, Calif. July 59.
3p. Order fromLC. Mi $1.80, ph $1.80.
NAA-SR-Memo-4131
Rainout containment, by G. L. Wegmann. Atomics
International. Division of North American Avia-
tion. Inc. , Canoga Park, Calif. Jan 60. 26p.
Order from LC. Mi $2.70, ph $4.80.
NAA-SR -Memo- 4801
816
Plutonium release incident of November 20, 1959,
by L. J. King and W. T, McCarley. Oak Ridge
National Laboratory, Oak Ridge, Tenn. (ndj
Contract W-7405-eng-26. 77p. Order from
OTS. $2.00. ORNL-2989
Applied health physics annual report for 1959, by
J. C. Hart and others. Oak Ridge National
Laboratory, Oak Ridge, Tenn. [ndj. Contract
W-7405-eng-26. 37p. Order from OTS. $1.00.
ORNL-3073
Evaluation of filter flammability and filter bank fire
detection systems, by P. D. Erickson and others.
The Dow Chemical Company. Rocky Flats Plant,
Denver, Colo. Feb 61. Contract AT(29-1)- '"
1106. 85p. Order from OTS. $2.00. t
KEP-222
Environmentpl beta -gamma radioactivity in air
Sandia Laboratory fourth quarter 196), by R
at
. ITE.
Womelsduff and j! E. Baker. Sandia Corpora -
tlon. Albuquerque. N. Mex. Feb 61. 9p. Order
from OTS. 50 cents. SC-4498(RR)
Shipping, handling and storage of radioactive mate-
rials. A literature search, by T. F. Davis.
Oak Ridge National Laboratory, Oak Ridge,
Tenn. Jan 61. 45p. Order from OTS. $1.00.
TID-3552(Rev.)
Sampling the upper atmosj;^re for particulate
n^atter. Second and third quarterly progress
" ' "' 1959 to March fs. 1
repons. September 25. 1959 to March
^60,
by M. Markels. Jr. and H. E. Bishop. Atlantic
Research Corporation. Alexandria, Va. Apr 60.
Contract AT(30-l)-2404. 39p. Order from LC.
Mi $3.00, ph$6.30. TlD-5794
Chemical dosimetry of prompt and residual radia-
tions from nuclear detonations, by G. V. Taplin
and others. University of Califorfiia, Los
Angeles, Calif. July 60. 34p. Order from OTS.
75 cents. • WT-1493
Instruments
An improved nuclear tneasuring principle. Period
covered from June 5. 1959 to June 5, 1960. by
S. V. White. Illinois Institute of Technology,
Armour Research Foundation, Chicago, 111.
Aug 60. Contract AT(ll-l)-745. 41p. Order
from OTS. $1.50. ARF-1152-12
Aerial radiological monitoring system. I. Theo-
retical analysis, design, and operation of a
revised system, by R. F. Merian arid others.
Edgerton, Germeshausen & Grier, Inc., Santa
Barbara. Calif, and Civil Effects Test Operations.
Division of Biology and Medicine. U. S. Atomic
Energy Conmiission. July 60. 54p. Order
fromOTC. $1.25. CEX-59.4
Inductively coupled scanning switch, by F. P. Caiatl.
E. I. du Pont de Nemours k Company, Savannah
River Laboratory, Aiken, S.C. Aug 59. Con-
tract AT(07-2)-l. 1^. Order from OTS.
50 cents. " DP- 401
Gammascan operating details and servicing instruc-
tions. General Electric Company, Hanford
Atomic Products Operation. Richland. Wash.
1956. Decl. May 4. 1960. Contract W-31 -109-
Eng-52. 16p. Order fromLC. Mi $2. 40.
ph$3.30. HW -44842
Transistorized line-operated radiation detection
instrumentation, by W. G. Spear. Hanford
Atomic Products Operation, Richland. Wash.
Jan 61. Contract AT(45-1)-1350. 39p. Order
from OTS. $1.00. HW-65553
Fuel core tester - UT-2. by C. L. Frederick and
G. L. Waldkoetter. Ranford Atomic Products
Operation, Richland, Wash. July 60. Contract
AT(45-1)-1350. 37p. Order from OTS. $1.00.
HW -65701
MRU driver and detector circuit for precision
sodium level probe, by J. Campbell. Atomics
International. Division of Nordi American
Aviation. Inc., Canoga Park, Calif. July 59.
8p. Order fromLC. Mi $1.80. ph $1.80. '
NAA-SR-Memo-4144
Instrumentation and controls division annual prog-
ress report for period ending July 1, 1960' by
C. J. Borkowski and C. S. Harrill. Oak Rid^
National Laboratory. Oak Ridge. Tenn. 1960.
Contract W-7405-eng-26. lUp. Order frMii
OTS. $2.50. ORNL-3001
Interfacial area measurement in^liuqid- liquid sys-
tems by radioisotopes. II. The use of a liquid
scintillator, by C. V. Chester and J. S. New-
man. Oak Ridge National Laboratory. Oak
Ridge. Tenn. [nd). Contract W-7405-eng-26.
24p. Order from OTS. 50 cents. ORNL-3018
Design and construction of a unit for measuring
metal skin temperatures. Sandia Corporation,
Albuquerque, N. Mex. Feb 61. 52p. Order
from OTS. $1.50. SC-4464(RR)
817
A time-based ar^alysia of GMD-1 data for electronic
computera. by R. L. Levesque. Sandia Corpora-
^ ■• *' Feb 61. 7p. Order
SC1M-35-6l(72)
tion, Albuqiiep-que, N. Mex.
from OTS. A) cents.
Sandia Corpori
Oct 54. lOp
ph$1.80.
A wind velocity ^ge model 11, by H. G. Laursen.
ration, Albuquerque, N. Mex.
Order from LC. Mi $1. 80.
501^1-234-54(52)
Radiation Applications Inc. , Long Island City.
N. Y. Jan 61. Contract AT(30-1)-2186. 105p.
Order from OTS. $2.50 NYO-2503
Radiation preservation of selected fruits and vege-
tables. An analysis of R &D programing and
market factors, by O. F. Poland and others.
Stanford Research Institute, Menlo Park, Calif.
Jan 61. Contract AT(04-3)-115. 228p. Order
from OTS. $3.00. SRIA-30
Mechanical desitai analysis for whip- type antennae,
AU^ Sandia Corporation, Albuquerque,
by I. W.
N. Mex.
50 cents
Mar 61. 16p.
Order from OTS.
SCTM-381 -60(14)
The unbalanced line directional coupler, by L. J.
Allen. Sandila Corporation, Albuquerque, N.Mex.
Feb 61. I6p4 Order from OTS. 50 cents.
SCTM-428-60(14)
«
N. Mex.
50 cents
Initial peak surie current detection circuits, by
Conrjd. Sandia Corporation, Albuquerque,
Fe}6l. ISp.
Order from OTS.
SCTM- 431 -60(24)
Determination of induced gamma -ray activity in beef
sterilized by cobalt-60-irradiation, by F. F.
Rieke and J. E. Brugger. University of Chicago,
Chicago Midway Laboratories, Chicago. 111.
Aug 59. Contract AT(11-1)-712. 9p. Order from
LC. Mi $2.40. ph $3.30. TID-6550
A literature survey on the effects of ionizing radia-
tions on sea foods with respect to wholesomeiiess
aspects, by S. A. Miller and others. Department
of Nutrition, Food Science and Technology.
Massachusetts Institute of Technology, Cambridge,
Mass. [nd]. Contract AT(30-1)- 2580. 35p.
Order from OTS. 75 cents. TlD-11610
Instrumentation of French underground shelters.
?>roject 30. Q), by J. ]. Meszaros and J. G. Schmidt.
erminal Ballistics Laboratory. Ballistic Re-
search Laboratories, Aberdeen Proving Ground,
Md. Jan 61. 126p. Ortter from OTS. $2.50.
WT-1535
Isotopes
-Industrial Technology
Intrinsic -radiotracer process control, by J. L.
McFarling a id others. Battelle Memorial Insti-
tute, ColumJ^s, Ohio. Feb 61. Contract W -7405-
eng-92. 44f
Order from OTS.
$1.00.
BMl-1499
Programmers t|ianual for the oracle compiler, by
M. E. La Verne and others. Oak Ridge National
Laboratory, i Oak Ridge, Tenn. Aug 57. Revised
June 15, 195b. 39p. Order from LC. Mi $3.00.
ph$6.30. T CF-57-8-92
The development of principles and methods of high
dilution on- ^tream isotopic tracers (uxsjm
tracer project). Annual report by O. M. Bi^zell.
and others. William H. Johnston Laboratories,
Inc., Baltimore, Md. May 60. Contract AT(1 1-1)-
650 - Sec. i I37p. Order from OTS. $2.50.
JLl-650-6-3
The technology and applications of large fission
Isotope Seporation
Separation of the isotopes of uranium, by J. W.
Beams. University of Virginia, Charlottesville.
Va. Feb 42. Decl. February 1, 1960. 37p.
Order from LC. Mi $3. 00, ph $6. 30.
A-42
Mathematics and Computers
I
Numerical solution of reactor stress problems, by
R. F. Redmond and others. Battelle Memorial
Institute. Columbus, Ohio. Feb 61. Contract
W-7405-eng-92. 53p. Order from OTS. $1.50.
BMl-1503
IBM*
704 p
rograms for unfolding complex gamma -ray
I, by W. B. Strickfaden and R. V. Kloepper
e technology, and applications oi large iission
products feia sources, by J. Silverman and others.
spectra, by W. B. btricklaoen ana r. n . Nloepper
he University of California, Los Alamos Scienti-
fic Laboratory, Los Alamos, N. Mex. Sep 60.
Contract W-7405-ENG-36. I26p. Order from
OTS. $2.50. LA-2461
Tables of solutions of Bessel's differential eqi^tion
for use in one -group reactor calculations, by CT
Goertzel and r" Sullivan. Nuclear Development
Corporation of America, White Plains, N. Y.
Sep 60. Contract AT(30-1)-2303(IX). 27p. Order
from LC. Mi $3.00. ph $6.30. NDA-2131-22
818
BiKnvalue routine, by J. R. Matdiews. University
at California, Lawrence Radition Laboratory,
Llvermore, Calif. June 60. Contract W-7405-
eng-48. 19p. Order from LC. Mi $2.40,
ph$3.30. . UCRL-6023
Stability for inhomogeneoua difference schemes, by
T. Seidman. University of California, Lawrence
Radiation Laboratory, Llvermore, Calif. July
60. Contract W-7405-eng- 48. 9p. Order from
LC. Mi $1.80, ph$1.80. UCRL-6042
MUFT-5-A fast neutron s;
ictrum program for the
Philco-2000, byH. Bohl. Jr. and A. P. Hemphill.
Westinghouse Electric Corporation, Bettis Atomic
Power Laboratory. Pittsburgh. Pa. Feb 61. Con-
tract AT-ll-l-GEN-14. 94p. Order from OTS.'
$2.00. WAPD-'IW-218
Nuclear reactor depletion programs for the Philco-
2000 computer, by O. ]. Marlowe and others.
Westinghouse Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburgh, Pa. Jan 61. Con-
tract AT-ll-l-GEN-14. 118p. Order from OTS.
$2.50. WAPD-TM-221
RANCH-an IBM -704 program used to solve the one-
dimensional, single energy neutron transpoTT
equation with anisotropic scattering, by L. A.
Hageman and J. T. Mandel. Westinghouse Elec-
tric Corporation, Bettis Atomic Power Laboratory.
Pittsburgh, Pa. Feb 61. Contract AT-ll-l-GEN-
14. 25p. Order from OTS. 75 cents.
WAPD-TM-268
PRESTO— A pressurizer transient program for the
IBM -704, by J. P. Cunningham and H. R, Meyer.
Westinghouse Electric Corporation. Atomic
Power Department, Pittsburgh, Pa, Aug 60.
Contract AT(30-3)-222, Subcontract No. 1.
146p. Order from LC. Mi $7.20, ph $22.80.
YAEC-141
Metals, Ceramics, and Materials
Evaluation of nickel
andG.
based alloys, by J. S. Bruhhouse
ioys,
W. Titus. Aerojet-General Nucleonics,
San Ramon, Calif. Jan 61. 56p. Order from
OTS. $1.50 AGNTM-361
Effects of irradiation on the EBWR fuel alloy frani-
uni-5 w/o zirconium- 1 . 5 w/o niobium, by J. H.
kittel. Argonne National Laboratory, Argonne,
111. July 60. Contract W-31-109-eng- 38. 43p.
Order from OTS. $1.00. ANL-5639
Examination of an irradiated prototype fuel element
for the Elk River reactor, by L. A. Neimark.
Argonne National Laboratory, Argonne. 111.
Jan 61. Contract W-31-109-eng-38. 19p. Order
from OTS. 50 cents. ANL-6160
Welded tratisition joint between 2-1/4% Cr 1% Mo
steel and type 316 stainless steel. Sodium cctii-
ponents desj^gn project research and develcymeot
i
Final re
rogram. hinal report. Alco Products, Inc.
esearch and I>evelc^ment Department, Schenec-
tady, N. Y. Aug 60. Contract AT(ll-l)-666.
59p. Order from OTS. $1.75. APAE-72
Welding 2-1/4% Cr
Cr - 1% Mo stee
> dei
■ 1% Mo steel tubes to 2-1/4%
tubesheets. Sodium compo^
tients design project research and development
S rogram. Final report. Alco Products, Inc. ,'
esearch aad Development Department. Schenec-
tady, N. Y. Aug 60. Contract AT(ll-l)-666.
41p. Order from OTS. $1.25. APAE-73
Ptiage diagram studies. Final report for January 9 -
CteoenJier 31, 1958, by R. F. Domagala. Gener-
al Electric Company, Aircraft Nuclear Propulsion
Department, Cincinnati, Ohio. Mar 61. Con-
tracts AT(ll-l)-171.and AF 33(600) -38062. 56p.
Order from 015. $1.25. APEX-583
ified -graphite technology. Quarterly report no.
, by S. w. Bradstreet. Illinois Institute of Tech -
Modified
nology. Armour Research Foundation, Chicago,
111. Jan 60. Contract AT(33-3)-4. 58p. Order
from LC. Mi $3. 60, ph $9. 30. ARF-6038-8
Development of container materials for LAMPRE
lopi
ipnl
applications, by D. C. E)rennen and others.
Battelle Memorial Institute, Columbus, Ohio.
Feb 61. Contract W-7405-eng-92. 46p. Order
from OTS. $1.25. BMI-1500
Thermal diffusion in a solid solution of h
ydrogen
Battelle
in beta zirconium, by J. W. Droege.
Memorial Institute, Columbus, Ohio. Feb 61.
Contract W-7405-eng-52. 39p. Order from
OTS. 75 cents. BMI-1502
The development and testing of homogeneous ceram-
ics fuels. Progress report for period June 1-
August 31, 19o0. Combustion Engineering, Inc..
Nuclear Division, Windsor, Conn. 1960. Con-
tract AT(30-1)- 2379. 31p. Order from LC.
Mi $3.00. ph $6.30. . CEND-9d
Metallographic examination of P&W capsules 1-10
and 1 -II, by M. J. Feldman and others. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Dec 54. Decl. June 13, 1960. 41p. Order
from LC. Ml $3. 30. ph$7.80. CF-54-12-212
819
A meul CO graphite joint for a molten salt system,
by J. L Crowley and W. 6. McDonald. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
Aug 60. 15p. Order from LC. Mi $2. 40,
ph$3.30. CF-60-8-32
Corroaion reseai ch — the sealin
aluminum surfaces, by J. E.
of cracks in
^ ^ raley and G,C.
English. Unii ersity of Chicago, Meullurgical
Laboratory, qhicago, III. Oct 44. D3cl. Janu-
ary 23, 1960.1 Contract W-7401-eng-37. 9p.
Order from Lp. Mi %l.iO, ph Jl. JO.
CT-3057
Thermal conduct vity of aluminum- — lithium alloys
^~- ■- ' P. Costas.
conwInInFuplo]8^3i^i^r^y~CT
Pont de Nernours (E. L ) k Co.
River Labora
August 4. 19
Order from
Savannah Riv
>ry. Aiken, S. C. Apr 60. Decl.
Contract AT(07 -2)- 1. 6p.
Mi $1.80, ph$1.80.
DP- 463
Maritime gas -coaled ractor program. Reactor
materials corjpatibility with impurities in helium,
by J. C. Bokr^ and H. E. Shoemaker. General
Dynamics, General Atomic Division, San Diego,
Calif. Jan6l] Contract AT(04- 3)- 187 73p.
Order from OTS. $2.00. GA-1508
Maritime gas-ccjoled reactor program. Thermal
and mechanical properties of teryllia ceramics
Final report
Atomic a
Calif. Aug
Order from
^
nd EJecgric B
ug 6d. Contr
amCTS. $1.
Recent developntents in graphite, by W. L. Kosiba.
DTvision, General Dynamics
San Diego, Calif. July 59. 21p.
Mi $2.70. ph$4.80.
GAMB-873
General A
Corporation
Order from
tomic
lie.
End seals for "c jred
eral Electric
Operation. R
May 18. 1960.
Order from
slugs by E. A. Smith. Gen-
Company" Hanford Atomic Products
chland. Wash. Mar 55. Decl.
Contract W -31- 109-Eng-52. lOp.
, Mi $2. 40, ph$3.30.
HW- 35511
IC
Lobsinger am
Company
Richland, W
Mi $1.80, ph
The stability of
S helium--ca
„.B7
pany, Hanfor 1
neral Dynamics, General
Boat Divisions, San Diego,
Contract AT(04-3)-187. 34p.
00. GA-1906
Corroaion of ali^ninum in high purity water, by R.J
General Electric
^rr
M. Atwood.
Htiiford Atomic Products Operation,
h. Feb 57. lOp. Order from LC.
$1.80. HW-48413
as
hree base metal thermocouples in
dioxide, carbon dioxide and air
rfcon
H. Sako. General Electric Com-
Atomic Products Operation,
Richland, Wash. Apr 59. Contract AT(45-1)-
1350. lOp. Order from LC. Mi $1.80.
ph$1.80. HW-59371(Rev.)
Development of ribbed jacket tubing for PRTR, by
R. C. Aungst. General Electric Company,
Hanford Atomic Products Operation, Richland,
Wash. Sep 59. Contract AT(45- 1)- 1350. 15p.
Order from LC. Mi $2. 40, ph $3. 30.
HW-61797
Fabrication of aluminum-plutonium alloy fuel
elements by coextrusion, by W. J. Bailey and
others. General Electric Company, Hanford
Atomic Products Operation, Richland, Wash.
Dec 59. Contract AT(45-1)- 1350. 32p. Order
from OTS. 75 cents. HW-63151
Fabrication of 10 weight per cent plutonium-
aluminum monitoring foils and pin, by R. E.
Sharp and L. C. Lemon. General Electric Com-
pany, Hanford Atomic I*roducts Operation,
Richland, Wash. Jan 60. Contract AT(45-1)-
1350. 20p. Order from OTS. 50 cents.
HW- 63558
Thermal redistribution of h;
)rocess tubes, by R. E.
&ral
estermaiT General
lectric Company, Hanford Atomic Products
Operation, Richland, Wash. Aug 60. Contract
AT(45-1)-1350. I9p. Order from LC. Mi $2. 40,
ph$3.30. HW-66196
Evaluation of welded and seamless zirconium and
2ircaloy-2 tubing Final report, byS.H. Bush.
General Electric Company, Hanford Atomic
Products Operation, Richland, Wash. Aug 60.
Contract AT(45-1)- 1350. 31p. Order from OTS.
75 cents. HW -66575
Army gas -cooled reactor systems program
mary report on materials for the GCRE-
R. Carpenter and A. Del Groeso. Aerojet
Sum-
RE-ll. by
General Nucleonics. The Engineering Division,
San Ramon. Calif. Dec 60. Contract AT(10-I)-
880. I31p. Order from OTS. $2.50.
IDO- 28564
Proton recoil as a source of hydrogen in reactor
materials, by A. H. Willis. General Electric
Company, Knolls Atomic Power Laboratory,
Schenectady, N.Y. Mar 60. Contract Vv- 31 -109-
Eng-52. 8p. Order from OTS. SOcents.
KAPL-2078
Mechanical properties of Zircaloy-2, by R. L.
Mehan and F. W. Wiesinger. General Electric
Company, Knolls Atomic Power Laboratory.
Schenectady, N. Y. Feb 6L Contract W-31 -109-
Eng-52. 47p. Order from OTS. $1.5Q KAPL-2U0
820
preparation and fabricatiopofplutonium fuel alloy
for Los Alamos molten plutonium reactor experi-
ment no. 1, J. W. Anderson ind others. Los
Alamos Scientific Laboratory, Los Alanxse,
N.Mex. Apr 60. Contract W-7405-eng-36.
28p. Order from LC. Mi $2.70, ph $4.80.
LA -2439
Pinal safety analysis report SNAP III therinoelec-
trie generator, by W. Hagis. Nuclear Diviaion.
Martin Company, Baltimore, Md. June 60.
Contract AT(30-3)-217. 63p. Order from OTS,
$1.75. MND-P-2364
Permeability of cladding niaterials to inert gases
Progress report no. 15 for period March 15,
i'rogre
-^
1960 to April 15, i960, by G. T. Murray and
XT. Pincus. Materials Research Corporation,
Yonkers, N. Y. Apr 60. Contract AT(30-1)-
2286. 6p. Order from LC. Mi $1.80, ph $1.80.
MRC-R156
Bi-nnetal bond inspection by ultrasonics, byD. E.
Lord. California Research and Development
Company, Livermore Research Laboratory,
^ Livermore, Calif. Sep 52. Decl. February 4,
1960. Contract AT(ll-l)-74. I6p. Order fron
LC. Mi $2. 40, ph $3. 30. MTA-l
Oxidation rates of U-10 wt. % Mo in air, by J.
Close ffi. Atomics International. DTvision of
North American Aviation, Inc., Canoga Park,
Calif. Jan 60. 12p. Order from LC. Mi $2.40.
Iih$3.30. NAA-SR -Memo- 4845
The permeation of hydrogen through haste Hoy B, by
D. W. Rudd and others. Atomics International.
A division of North American Aviation, Inc.
Canoga Park. Calif. Feb 61. Contract AT(ll-l)-
GEN-8. 16p. Order from OTS. 75 cents.
NAA-SR-4898 (Rev.)
Urattium rod coextruded with zircoaium alloy clad,
by H. F. Sawyer. Nuclear Metals, Inc., Con-
cord, Mass. Mar 59. 5p. Order from LC.
Ml $1.80, ph$1.80 NMI-4918
Deplet
letedvs natural uranium in Pu reactors, by K. H.
chl. Nuclear Materials and Equipment Corp. ,
Apollo, Penna. May 60. 4p. Order from LC.
Mi $1.80, ph$1.80. NUMEC-TM-P-ll
Fuel element development program for the pebble
bed reactor. Phase I: progress report tor Mayl,
1959 to October 31. 1959. Sanderson & Porter,
New York. N. Y. Nov 59. Contract AT(30-1)-
2378. I32p. Order from OTS. $2.50.
NYO-2706
Aircraft nuclear propulsion project quarterly prog-
ress report_for period ertding September 30,
1957. Oak Ridge National Laboratory, Oak R idge ,
tenn. Feb 58. Decl. with deletions October 28,
1959. Contract W-7405-eng-26. 281p. Order
from LC. Mi $11. 10, ph $45.00. ,
ORNL-2387(Pl8. l-5KDel.)
The mechanical properties of INOR-8, by R. W.
Swinderman. Oak Ridge National Laboratory,
Oak Ridge, Tenn. (ndj. Contract W-7405-eng-
26. 73p. Order from OTS. $1.75. ORNL-2780
Metallurgy of Zircaloy-2. Part II: The effects of
fabrication variables on the preferred orientation
and anisotropy of strain behavior, by P. L.
Rittenhouse and M. L. Picklesimer. Oak Ridge
National Laboratory, Oak Ridge, Tenn. [nd].
Contract W-7405-eng-26. 2l6p. Order from
OTS. $3.00. ORNL-2948
Preparation of high -density oxides and vibratory
compaction in fuel tubes, by S. D. Clinton and
others. Oak Ridge National Laboratory, Oak
Ridge. Tenn. [ad]. Contract W-7405-eng-26.
19p. Order frcMii OTS. 50 cents. ORNL-2965
Fuel-bearing fiberglac in aluminum base fuel ele-
ments. Quarterly rejport no. 5 for May 1, 1960
to July 31? 1960, by R. H. Baskey. Clevite
Corporation, Mechanical Research Division,
Cleveland, Ohio. Sep 60. Contract AT(40-1)-
2557. 30p. Order frcMU LC. Mi $2.70,
ph$4.80. . ORO-316
Synthesis and fabrication of refractory uranium
compounds. Monthly progress report no. 9 for
August 1, 1960 throurii August 31, 1960, by K. M.
Taylor and C. H. McMurtry. Carborundum Com-
pany, Research and Development E>ivision,
Niagara Falls, N, Y. Sep 60. Contrcct AT
(40-l)-2558). 4p. Order from LC. Mi $1.80,
ph$1.80. ORO-319
letter for August
by R. L. Robinson.
Fuel cycle development pro'jram. Monthly news-
" " august 1960,
National Carbon Company, Fostoria, Ohio. Sep
60. Contract AT(04-l)-2560. 8p. Order from
LC. Mi $1.80, ph $1.80. ORO-326
Fuel bearing fiberglas in aluminum base fuel ele-
ionthly progress letter no. 16 for
ments.
period September I. 1960 to September 30, I960.
by R. H. baskey. Clevite Corporation, Mechani-
cal Research Division, Cleveland, Ohio. Oct 60.
Contract AT(40-l)-2557. 3p. Order from LC.
Mi $1.80. ph$1.80. ORO-330
821
Anodization of Bteel in a fluoride batfa. by H. F.
Priest and M. Leviu. Columbia University, New
York. N. y. Feb 43. Decl. November 23. 19S9.
2p. Order from LC. Mi $1.80, ph $1.80.
1 TID-5090
Measurement of the equilibrium concentration of
lattice vacancies in silver near the melting point,
by R. O. Simmons and R. W. Balluffi. Univer-
sity of IllinO.s. Urbane. 111. Feb 60. Contract
AT(ll-l)-l|B2. 28p. Order frcOTi LC. Mi $2.70.
Sanderson and Porter, New York. N. Y. 1960.
Decl. September 23, 1960. Contract AT(30-l)-
2378. 18p. Order from LC. Mi $2.40,
ph$3.30. TID-6810
Fission gas release in PWR core 1 blanket fuel rods
>n conclusion of seed 1 life, by B. Rubin.
ph$4.80.
TID-5655
The determination of the equilibrium phase diagram.
Zirconium -'-niobium. Period covered March ij
1960 to April 1, 1960, by C. E. Lundin. Univer-
sity d Denver, Denver Research Institute, Den-
ver. Colo. I Apr 60. Contract AT(ll-l)-752. 6p.
/estinghouse Electric Corporation, Bettis Atomic
Power Laboratory, Pittsburg, Pa. Feb 61.
Contract AT-ll-l-GEN-14. 20p. Order from
OTS. 50 cents. WAPD-TM-263
Examination of PWR core 1 blanket fuel rods for
and burst
microstructure, h
lydrogen"
ubin. We
Order froR
iphi
al&
LC. Mi $1.80, ph$1.80.
TlD-5768
Metallographii : preparation c< selected ceramic
materiale^ by C. H. Brady and others. Battelle
Memorial (bstltute, Columbus, Ohio. May 60.
Contract WV-7405-eng-92. 13p. Order from LC.
Mi $2. 40, ^ $3. 30. TID-S912
j*$3.
Slip casting of nuclear fuel elements. Progress
letter no. 14 for July 1. 1960 through July 31,
1960, by G« J. Comatock. Stevens Institute of
fechnologt, Powder Metallurgy Laboratory,
Hoboken. h. J. Aug 60. Contract AT( 30-1)-
2258. 7p. Order from LC. Mi $2.40. ph $3.30.
TID-6492
Mechanism of_high energy radiation effects in poly-
ethylene, technical report no. 5 covering period
repot
%e^
March 1. 1^59 to Marcfil 1960. by M. uoie.
Northwestern University. Evanston. 111. Mar 60.
Contract Attll-l)-89. 6p. Order from LC.
M $1.80, k$1.80. TII>-6S18
Development df flat plate ceramic fuel elements
Tecnnical progress letter no. 14 for summary
./Qgx
of work dofie rrom January 1. 1959 to February
28, 1960, by J. J. Fargo. Gladding, McBean
and Compaty, Los Angeles, Calif. Mar 60.
Contract AT(04-3)-249. I6p. Order from LC.
Mi $2. 40, eh $3. 30. TlD-6569
Study of factors influencing ductility of iron--alumin-
urn alloys. ' Monthly letrer report no. 5, by G. P.
Rauscher, )r. and others. University of Denver,
Denver Restorch institute, Denver, Colo. Oct
60. Contract AT(ll-l)-742. lOp. Order from
IX. Mi $1.80. ph $1.80. TID-6752
Fuel element ^velopment program for the pet)ble
i960.
bed reactoi
Prc^ess report for July
^ pickup,
strength, by B. Rubin. Westinghouse Electric
Corporation. Bettis Atomic Power Laboratory,
Pittsburgh, Pa. Feb 61. Contract AT-ll-l-GEN-
14. 35p. Order from OTS. $1.00.
WAPD-TM-264
Thermoelectric nuclear fuel element quarterly
progress report for July through Septemberi960,
by u. R. Kilp and others. Westinghouse Electric
Corporation, Pittsburgh, Pa. Oct 60. Contract
AT(30-3)-500. 50p. Order from OTS. $1.25.
WCAP-1647
Nuclear Explosions — Peaceful Applications
Seismic measurements by the U. S. Geological
survey during the pregnome hidi-explosives testg
near Carlsbad, New Mexico. Final report, by
P. E. Byerly and others. U. S. Department of
Interior, Geological Survey, Washington, D. C.
Apr 60. 40p. Order from OTS. $1.00.
TEl-761
Cavity definition, radiation and temperature distri-
butlons resulting from the Logan event, by W.P.
Bennen and others. University of California,
Lawrence Radiation Laix>ratory. Mercury, Nev.
Dec 60. Contract W-7405-eng-48. 54p. Order
from OTS. $1.25. UCRL-6240
Final report on the Pinot experiment, by F. L.
Adelman and others. University of California,
Lawrence Radiation Lalxiratory. Livermore,
Calif. Dec 60. Contract W-7405-eng-48. 2ip.
Order from OTS. 50 cents. UCRL-6274
822
Particle Accelerators and High-Voltage
Machines
Corrections to betatron frequencies in the Brook-
haven alternating-gradient synchrotron, by X.
Smith. Brookhaven National Laboratory, Upton.
N. Y. May 56. 16p. Order from LC.
Mi $2. 40, ph$3.30. BNL-4637
Alternating gradient synchrotron; suinmary founda-
tion report, by J. H. Lancaster. Brookhaven
National Laboratory, Upton. N.Y. July 56.
I6p. Order from LC. Mi $2.40, pfa #3.30.
BNL-4638
Some saturation characteriestics of altemating-
radient magnet models, by M. H. Blewett.
rookhaven National Laboratory, Upton, N. Y.
Oct 56. Up. Order from LC. Mi $2.40,
ph $3. 30. BNL-4640
A parallel-transistor cascaded amplifier for con-
trolling very large currents, by R. H. RhBauine.
Brookhaven National Laboratory, Upton, N. Y.
Mar 59. 7p.
ph$1.80.
Order from LC.
Mi $1.80,
BNL-4651
Relativistlc charged particle tralectories in crossed
electric and magnetic fields, by R. A. Beth.
Brookhaven National Laboratory. Upton, N. Y.
Mav59. 6p. Order from LC. Mi $1.80,
ph$1.80. BNL-4656
A radiofrequency beam separator for complete
separation of hi^ energy particle beanis, by
J. P. Bleweet and J, D. Kiesling. Brookhaven
National Laboratory, Upton. N. Y. Aug 59.
17p. Order from LC. Mi $2.40, ph $3.30.
BNL-4658
Saturating inductor for controlling the magnetic
field of the alternating gradient synchrotron, by
E. J. Rutan. Brookhaven National Laboratory,
Upton, N. Y. Oct 59.
Mi $3. 00, ph$6.30.
35p. Order from LC,
BNL-4659
Computational studies of coupling resonances in
Bpirally-ridged accelerators, by C. A. Lasset-
tre. Midwestern Universities Research Associa-
tion, Madison, Wis. Jan 61. Contract AT(1 1-1)-
384. 25p. Order from OTS. 50 cents.
MURA-595
Theoretical remarks concerning the 3<r-, ^- 2^ =
2^r resonance in spiral sector accelerators. By
'^.
Sessler. Midwestern Universities Re-
search Association, Madison, Wis. Jan 61.
'Contract AT(11-1)- 384. 8p. Order from OTS.
iiO cents. MURA-596
The effect of nearby buckets on bucket area in RP
acceleration, by J. B. Boilen. Midwestern
Universities Research Association, Madison,
Wis. Feb 61. Cono-act AT(ll-l)-384. 4p.
Order from OTS. 50 cents. MURA-606
Research studies with a 1-Mev Van cte Graaff ma-
chine. Annual report, by F. L. Hereford. Uni-
versity of Virginia. Charlottesville, Va. June 60.
Contracts AT(40-1)-1754 and DA-36-034-ORD-
2046. 16p. Order from LC. Mi $2. 40.
ph $3. 30. ORO-302
Minutes of ttie MURA general conference, Madison,
Wisconsin, January 8-9, 1960. Midwestern
Universities Research Association, Madison,
Wis. 1960. 21p. Order fran LC. Mi $2.70,
ph $4. 80. TID-6176
Ph)fsics
Determination of lattice parameters with tiie aid of
a computer, by M. H. Mueller and L. Heaton.
Argonne National Laboratory, Argonne, HI.
Jan 61. Contract W-31-109-eng-38. 29p.
Order from OTS. 75 cents. ANL-6176
Physics division sumnary report. September, Octo-
ber I960. Argonne National Laboratory, Ar-
gonne, 111. 1960. Contract W-31-109-eng-38.
27p. Order from LC. Ml $2.70, ph $4.80.
AN L- 621 4
Buildup (rf Cf^^^ and intermediate isotopes from
Cmj44 in a hi^ flux, by S. E. Vandenbosch and
P. R. Fields. Argonne National Laboratory,
Argonne, 111. Feb 61. Contract W- 31 -109 -eng-
38. 9p. Order from OTS. 50 cents. .
> AN L- 6252
Fractional parentage coefficients in Intermediate
L byD.
atory, Aigonne, 111. Mar 61
parentage
coupling, by D. Kurath. Argonne National Labor-
Ai
109-eng-38. 18p.
Contract W-31-
Order from OTS. 50 cents.
ANL-6312
Electron diffusion paranwters, by J. R. Beeler and
M. R. Smith. General Electric Company, Air-
craft Nuclear Propulsion Department, Cincinnati,
Ohio. Dec 58. Contracts AF 33(600)- 38062 and
AT(11-1)-171. 20p. Order from OTS.
50 cents. APEX-582
823
Minutes of ineetKg of accelerator development
department. Brookhaven flanonal Lab. , U^o".
N. y. Ma9 69. 3p. Order from LC. Mi>l;»J-
ph $1. 80. BNL-48UH
Heat transfer In fteptafoil geometries by mass -trans -
— fer measurenletitB. by J. L. WanUand and R. L.
Miller. Oak Ridge National Lab. . Oak Ridgp.
Tenn. June 59- Contract W-7405-cng-26.
29p. Order ffom LC. Mi $2. 70. ph $4. ^•_^
Instructions for the operation of an oracle code for a
Mnnte Carlo solution ot the transport problem for
- gamma ravs incident upon a slab, by S. AiTsIender
and D. K. Trubey. Oak Ridgp National Lab. .
Oak Ridge, T^nn. Oct «). 39p. Order fJomLC.
Ml $3.00. ph|$6,30. CF-60-IO-37
Progress report. for October. November. December
1^59 (^alunjbia University. t4ew York, ^egram
SGHear Physics Labs. Contract AT-30- 1 -GEN-
72, 39p. 0*ierfromLC. ^1 $3.^.^6. ».
Samarium Tabljs. by J. C. English and T C.
— Gorrell. E. 'L du Pont de Nemours k Co. .
Savannah Riv(er Laboratory. Aiken. South
CaroUna. Feb 61. Contract AT907 -2)- 1. 34p.
Order from CTS. 75 cents. DP-557
A machine code for computliy
jtups, by U. B. MacMilia
icn"oirs" Atomic Power Lab. , Schenectady. N. Y.
Sourceless BUrtup ..
irw«/-Bource reactor startups, by D. B. Mai
an.
I CTS.
o^ low
M«>aHurement o{ low enerf^y neutron spectra, by
— I R, Beyster and others. General Atomic Div. .
General Dyn»mic8 Corp. . San Diego. Calif.
Nov 59. Contract AT(04-3)-l67. 15p. Order
fromLC. fli $2. 40, ph $3. 30. GA-1088
Manual of procedures for g«^y«.^°""°\,P^|P. .
materiX bJB. S, Lewis and cxhers.HuUips
Petroleum 60. Atomic Energy Div. . Idabo Falls,
iSS ^ b6. Contract AT(10-1)-2D5. 63p.
'^^rirZ^C. Mi$3.40. phJ10.80 IDO- 14384
An ion source tor mnlecular effusion smdies by
DM. Jacklon and t>. \L Hudson. AuieB Lab-
Satory. aLs. Iowa. May 59. Contract W-
7405-eng-8j. 82p. Order from OTS. ^^-JW ^^^^
Numerical ..^il-H^n nf the diffusion equation n
tH^ntn.lar and hexagonal geometries, by J. P.
Tewen General Slgctnc Co. . knolls Atomic
Power'LabSratory. Schenectady, htew York.
Sept 60. ^ntract W-3l-109-eng-52 31p.
Order frorlorrS. $1.00. KAPL-2085
Pressure and utcmt^x^v^-^-
to a sphered, by L. Deagle
thermal stresses at a pipe attachment
General Electric
to a spnerq, uy i^. i^—e> — c^u«.«
Co. , knol$ Atomic Power Laboratory. Schen-
ectady. NeU York. Sept 59. Contract W-31
ICAPL-2109
109-eng-5;. 30p.
lune 60. Contract W-31- 108-eng-52. ep. Order
}^ Lb, Mi $1. 80. ph $1.80. KAPL-M-DBM-1^
rh.rcr^ particle cross sections. Neon to chromium.
edJ by Darryl B. Smith. Los Alamos Scientific
Laboratory, University of California. Los Ala-
mos. New Mexico. June «). Contract W-7405-
ENG. 36. I37p. Order from GTS. *2.50^^^^
kinematics of Xh- relatlvlstic two-bodv problem, by
Leroy Blumberg and Stweart I- ScWe8»"g"-
LOS Alamos Scientific Lab N Mex. Aug 55.
85p. order fromLC. ^ ^■^- ^'^ll^[,,,
Pinal safety analy^^^ report-SNAP lA radioisotope
fueled thermoelectric generator, by George P.
Dix Martin Co. Nuclear Lhv. , Baltimore.
^; 60^ Contract AT(30-3)-217. aOOpL Orc^r
from LC. Mi $9. 60. ph $33. 30. MND-P-2352
Preliminary operational safety ^eport for the "sk
■ ■; A rh.rmr!^ectric generator, by Uamel gni^ton.
Nuclear Division, Martin Co. , Baltiniore, Md.
r '^irs^i's *'''^-'"'- tSiD-TSi9
from OTS. $i. *3.
^^,^p pr^rams. Quarterly progress report no l._
»i.T S and 6^for Uct^-r 2M>ecember 31.
-^^ia^SFDHnil^irM^^
5s:rs.%3.r^^^^^'^"-'"^"--^
■SNAP program^ f>.arterly P^ogjess report no 4
— f^r luiy 1 rhrouyrh Septemnpr 30, 19«). TasKs
gd^i:73^p.'and^. byF.J.'uck Isjuclear
Divisioii. Martin Co.. Baltimore. Md. Dec 60.
Contract AT(30-3)-217. 53p. OrderfromLC
Mi $3. 30. ph $7. 80 MND-P-3012 I
Mesh size in transport codes, by E. U. Vaughan.
Atomics International Div. . North American
Aviation, Inc.. Canoga Park. CaliL Mar 59.
5p. OrderfromLC. Mi $1. 80, ph $1. 80
^ NAA-SR-K4emo-3672
Recent ^^Tvriences with Candle 1, by R. A. Blaine.
AtomicTlntemational Div. . Nbrth American
Aviation. Inc. , Canoga Park Calif June59.
lOp. OrderfromLC Mi $1. 80, ph $1. 80^
*^ NAA-SR-Memo-4033
•24
Status of the neutron cross section program, as
presented at the January, 1955 meeting of the
AEC nuclear cross section advisory group, by
H. Goldstein. Nuclear Development Associates,
Inc. , White Plains, N. Y. Feb 55. Contract
AT(30-l)-862. 23p. OrderfromLC. Mi $2. 70,
ph $4. 80. NDA-Memo-15C-66
On a method of searching for neutral bosons or
boson-system resonances in the mass re^on
d several M^r. by W. Selove. Pennsylvania
Univ. . Philadelphia. June 60. Contract AT
(30-l)-2171. 5p. Order from LC. Mi $1. 80,
ph$1.80. NYO-2812
Measurement of the Wolfenstein parameter R at
210 MEV, by W. A. Gibson and others.
Rochester Univ. . Rochester. N. Y. Aug 60.
128p. Order from LC. Mi $6. 30. ph $19. 80.
NYO-9264
The single -scattering approximation to the gamma -
ray air-scattering problem, by D. K. Trubey.
Oak Ridge National Laboratory, Oak Ridge,
Tennessee, [n. d. ]. Contract W-7405-eng- 26.
20p. Order from OTS. 50 cents. ORNL-2998
Self- supported cyclotron targets of boron and mag-
nesium, by G. R. Hoke and E. Newman. Oak
Ridge National Laboratory, Oak Ridge, Tenn.
(n.d.J. Contract W-7405-eng-26. 6(3. Order
from OTS. 50 cents. ORNL-3021
The structure of an ALGOL translator, by A. A.
Grau. Oak Ridge National Laboratory. Oak
Ridge. Tenn. fn. d.). Contract W-7405-eng-26,
S7p. Order from OTS. $1.50. ORNL-3054
Electronuclear research division annual progress
report for period ending March
nnualpr
1. 1960.
Oak
Ridge National Laboratory. Oak Ridge. Tenn.
[n.d. ). Contract W-7402-eng-26. 87p. Order
from OTS. $2.00. ORNL-3047
Plutonium Plexiglas assemblies. Part II. by G. H.
Bidinger and others. Dow Chemical Co. . Rocky
Plats Plant. Denver. Colorado. Apr 60. Con-
tract AT(29-1)- 1106. 20p. OrderfromLC.
Ml $2. 40. ph $3. 30. RFP- 190
Mathematical problems in seismology, by W. J.
Byatt and G. P. DeVault. Sandia Corporation.
Jan 61. 81 p. Order from OTS. $2.25.
SC-4542(RR)
Theories and applications of very low temperatures,
by Nicholas Kurti. Sandia Corporation. Jan 61.
20p. Order from OTS. 50 cents. SCR -263
Maximum temperature patterns in hot climates, by
C R. McAllister. Sandia Corp. . Albuquerque,
N. Mex. June 54. 9p. Order from LC. Mi
$1. 80, ph $1.80. SCTM-80-54-51
The electrical behavior of exploding wires: a survey
of various materials, by T. J. Tucker. Sandia
Corp., Albuquerque, N. Mex. Dec 59. lUp.
Order from OTS. $2. 50. SCTM 334-59-51
Total gamma absorption in C
12 ^14 0I6
and Al
27
at 2D MEV. Technical report no. 5, by Edward
E. Carrol. Jr. Pennsylvania University, Phila-
delphia. Sept 59. Contract N-onr-55l(17). 13Q).
Order from LC. Ml $6. 90, ph $21. 30. TII>5695
Annual progress report for period December 1958
through November 1959. Minnesota University,
Linear Accelerator Lab. . Minneapolis. June 60.
Contract AT(1 1-1) -50. 130p. OrderfromLC.
Mi $6. 90, ph $21. 30. TID-5767
Effects of dissolved gas evolution at the surfaces of
heated vertical cylinders (thesis), by Jerry R.
Peterson. Engineering Research Laboratories,
Columbia University, New York. Sept 60. Con-
tract AT(»- 3) -187. 45p. Order from OTS.
$1.25. TID-6611
Nuclear -energy power sources, presented at the
jal c
14th aiuiual power sources conference, May 17-
19. 1960, Atlantic City, New Jersey, by Maj.
George H. Ogbum. Jr. , USAF. Feb 61. I2p.
Order from OTS. 50 cents. TID-6612
Fifth Nuclear Congress. Rome. Italy, June 20-26,
1960. U. S. Papers. 96p. Order from OTS.
$2725! TID-7601
Photodisintegration cross section of beryllium near
thresholdi^ by J. M. ProsserandW. John. Jr. '
University of California. Lawrence Radiation
Laboratory, Livermore, Calif. May 60. Con-
tract W-7405-eng-48. 34p. Order from LC.
Mi $3.00. ph $6. 30. UCRL-5996
The nuclide Hf^^^, by W. Hutchin and H. Lindner.
University of California. Lawrence Radiation
Laboratory, Livermore, Calif. Sep 60. Con-
tract W-7405-eng-48. 5p. Order from LC.
Mi $1.80. ph $1.80. UCRL-6094-T
Vibrational states of the HrT*" and HT^ ions, by S.
Cohen and others. University of California,
Lawrence Radiation Laboratory. Berkeley. Calif.
Sep 60. Contract W-7405-eng-48. 5p. Order
fromLC. Mi $1.80. ph $1.80. UCRL-9414
Physics division semiannual report, May -October
1960. Lawrence Radiation Laboratory. Unlver-
sity of California, Berkeley. California. Dec 60.
Contract W-7405-eng-48. 76p. Order from
OTS. $1.75. UCRL-9479
Atomic beam research on the spins, hyperfine struc^
43 91) 141)
tures, and moments of K , Y . La , and
Lu , by F. R. Petersen. Lawrence Radiation
Laboratory, University of California, Berkeley,
California. Nov 60. Contract W-7405-eng-48.
160p. Order from OTS. $2.75. UCRL-9480
Calibration at an 8"X8" sodium isodide (Tl) crystal,
by W. L. Weiss. General Electric Co. . Air-
craft Nuclear Propulsion Dept. , Clnncinnati,
Ohio. Mar 60. 28p. Order from LC. Mi $2.70,
ph$4. 80. XDC-60-3-212
&2S
Radiation Effects on Materials
Compatibility c|f magnet wires in pccting (
"^ under gamma irradiation, by S. F. He
and 1. w. K.i-uetzkamp. Aircraft Nucl
King compounds
lemmenway
J. W. K.J-uetzkamp. Aircraft Nuclear Pro-
pulsion Department, General Electric, Cincinnati,
Ohio. Mar 61. Contract AT(ll-l)- 171. 50p. Or-
der from ofs. $1.2S APEX-584
Healing o< fasfneutron-induced changes in graphite.
n. The effect dL heating during exposure. Interir
report on prcfclem 323 MCL 2301. by 1. J.Neubert
and others. Metalli
sity. July4|l. Up.
ph )3. 30.
rconium moqerator (
an<l others. Metallursdcal Lab
Order from LC
Chicago Univer-
Ik $2.40,
CC-1669
Zirconiu
cladding irradiated in the
sodium reaotor experiment, by J. J. Gill.
Atomics Lnternatlon, North American Aviation,
Inc. . Canogp Park, California Dec 60. Con-
tract AT(lltl)-gen-8. 35p. Order from OTS.
75cenu. NAA-SR-5970
Cyclotron Irr
elevatedle
North Ame
Nov 52.
Order fromlLC
.atlon of fused fluorldea in Inconel at
^,ratures. by Walter V. Goeddel.
. jcan Aviation, Inc. , Downey, Calif,
Contract AT-40-1-GEN-1064. 69p.
Mi $3. 90, ph $10. 80.
•NAA-SR-208
Solid -state and irradiation physics miarterlv progress
report for October -pecember 1952. ed. by E. C.
Crittenden. Jr. , and F. E. Paris. North Ameri-
can Aviatioil, Inc. , Downey, Calif. July 53. Con-
tract AT- lL-1 -GEN- 8. [n.p. > Order from IX.
Ml $7. 50, I h $24. 30. NAA-SR-229
Reactor Technology
mers
Pathfinder atoitiic power plant technical prope
report, lanaary- March 1960. Allis-Chalmf
Mfg. Co. , Atomic Energy Div. , Milwaukee
Jum60. Ctmtract AT(11-1)-589. 209p. Order
from LC. pi $9. 90, ph $34. 80. ACNP-6006
Pathfinder atoitiic power plant technical progress
report, ApT'il-June L^^U. Aliis Chalmers Mrg.
C6., Afomfc Energy Uiv. , Milwaukee. Oct 60.
Contract AT(1 1-1)1589. 189p. Order from LC.
Mi $8. 40, ^ $28. 80. ACNP-6007
Safety radiatioi level survey
— Bfirtorman*. — I6sr rtaaiti tjl-s
Light Co. . bhi
Order froni
m^
Fourth
TXRpgsne
■One 59. 7p.
Mi $1. 80, ph $L8a AECU-4258
ingport.
Section II.
T57:
Kenna.
Operating manual for the Argonaut reactor Argon
National Lab. . Argonne, Ul. Aug bV. L-ontract
W-31-l09-«ng-38. 39p. Order from LC.
Mi $3. 00, Ml $6. 30.
Gas -cooled relctors in the U. S. A. A survey and
ANL-6036
iai
recommendation, by K. M. Arnr^trong. Argonne
National L*oratory, Argonne, Qlinois. Nov 60.
Contract W' 31 -109- eng- 38. 53p. Order from
OTS. $1.2^. ANL-6255
Idaho division summary report for July, August,
— September ViiM, by Meyer Novick and 1-. W.
Illinois, [n.d.j. Contract W-31-l09-eng- 38.
146p. Order from GTS. $2.50. ANL-6301
EBWR Core 1 A physics analysis, by R. Avery and
others. Reactor Engineering Division, Argonne
National Laboratory. Argonne, Ullnois. Feb 61,
Contract W- 31 -109- eng- 38. 76p. Order from
OTS. $1.75. ANL-6305
Reactor developn^nt proyg-aro tn-ogress reixnt.
February 1961. coordinated by R. M. Adams.
Argonne National Laboratory, Argonne, 111.
Mar 61. Contract W- 31 "109- eng- 38. 8(to.
Order from OTS. $2.00. ANL-6328
Specifications and fabrication procedures for PM-2A
" Core II control rod fuel elements. AlcoTroducta.
Inc. , Schenectady, N. Y. May 60. Contract
AT(30-3)-326. 94p. Order from LC. Ml $4. 80,
ph $13. 80. APAE-Memo-260
Fast reactor core design parameter study. Atomic
Po*er Development Associates, Inc. , Detroit,
Michigan. Mar 60. Contract AT(ll-l)-800.
321p. Order from OTS. $4.00. APDA-133
Economics of nuclear and conventional tankers, by
— Tack J. Uordon and Keith E. bucic. Amerlcan-
Standard, Atomic Energy Dlv. , Mountain View,
California. Oct 58. Contract AT(04-3)-l09.
71p. Order from LC. Ml $4. 50, ph $12. 30.
*^ ASAE-S-13
Control blade worth by partial water height and sd-
uble boron metnooa, by Ariand L. MacRinney
and Russell M. Ball. Babcock and WUcox Co. ,
Critical Experiment Lab. , Lvnchburg, Va.
July 60. Contract AT(30-3)-274. 19p. Order
from LC. Mi $2. 40, ph $3. 30. BAW- 307
Nuclear merchant ship reactor project: survey (<
the reactor and control drive system research
and development program, comp. by Uon M.
Bylund. Babcock and W tlcox Co. , Atomic Energy
Div., Lynchburg, Va. Aug 59. Contract AT
(30-5)-274. 287p. Order from LC. Ml $11.10,
ph$46.80. BAW-1153-l
Critical experiments with General Electric Com-
— pnny fuel tor the N.b. Savannah, by K. m. Ball
and others. BabCocic and wiicox Co. Atomic
Energy Dlv. , Lynchburg, Va. luly 59. Con-
tract AT(30-1)-2340. 79p. Order from LC.
Mi $4. 80, ph $13. 80. BAW-1158
Atomic Energy Division, Lynchburg^ Va.
[ad.j. Contract AT(30- 1)2602. 66p. Order
Co
from OTS. $2.25,
BAW-1218
Newsletter
Argonne Neutron cross section evaluation group, News!
ntract — no. 3. February 19bi, by Kudolph bner ana
Sophie Moore. Brookliaven National Laboratory,
Upton, Long Island, N.Y. Feb 61. 6p. Order
from OTS. 50 cents. BNL ^3 (N-3)
Evaluation of experiment off-gas system for the
ECXJK-Ll'lK capsule experiment, by K. fc..
Adams and W. b. Browning, uak Ridge Na-
tional Lab, , Oak Ridge, Tenn. Sept 60. I2p.
Order from LC. MI $2. 40, ph $3. 30.
CF-60-9-8
Thalgott.
j^t^^N^iS^alTaSat'^yV A"rgonne. Dry mainten«x:e facility for the HRT, by P.P.Holx.
826
Oak Ridge National Lab. , Oak Ridge, Tenn.
Oct 60. 8p. Order from LC. Mi $1.80,
ph$l.80, CF-60-10-85
^gHPgl'"*y ^^. ^^1 neutron heat deposition in the
EGCR core, by E. A. Nephew. Oak RiHge Na-
tional Lab, , Oak Ridge, Tenn. Oct 60. 27p,
Order from LC. Ml $2, 70, ph $4. 80.
CF-60-10-122
Reactor plant containpr Jnrpgriry t^^y
L.KA
, . Core I,
seed 2. Section 1. Test resultB CUiAX7\X\.
IXjquesne Light Co. , Shippingport, Penna.
June 60. I3p. Order from 1^. Ml $2. 40,
ph $3. 30. DLCS- 35701 01
Mechanical Propeniea of irradiated welds in
stainless steel, by J. W. Joseph, Jr. Atomic
Energy Division , E. I. duPont deNemours &
Co. IJec 60. Contract AT(07-2)-l. 12p.
Order from OTS, 50 cents. DP-534
Stainless steel failures in Savannah River plant
reactor areas, by R. H. NfcKane and others.
E. I. du Pont de Nemours i^Co. . Savannah
River Laboratory, Aiken, Sguth Carolina.
Nov 60, Contract AT(07-2)-l 59p, Order
from OTS, $1.50. DP-539
Economic potential for D^O power reactors, by
L. IsakoCf. E. I. du Pont de Nemours k Co. ,
Atomic Energy Division, Wilmington, Delaware.
Feb 61. Contract AT(07-2)-l. 76p. Order
from OTS. $1.75. DP-570
Prcyess report of some recent HTGR nuclear
ocsign studies, by I. Bornstein and others.
General Atomic Div. , General Dynamics Corp. ,
San Diego, Calif. Feb 60. Contract AT(04-3)-
314. I27p. Order from LC. Mi $6. 30,
ph$$19. 80. GAMD-1248
Past oxide breeder-reactoi- physics. Part I. Para-
metric study of 300(e) MW reactor cOTe. by P.
Greebler and others. Atomic Power Equipment
Dept, , General Electric Co. , San Jose, Calif.
Nov 59. Contract AT(04-3)-l 89 PA-#10. 55p.
Order from OTS. $1.50. • GEAP-3287
Fuel ryrlp program. a hnning <vflr».r r«.a/-tm- r«.-
■parrh ant\ rjoyplnpmpnf prf>gram— Firar quar-
terly report. August -September 1960. by W. H.
Cook. Atomic Power Equipment Dept. . General
Electric Co. , San Jose, Calif. Oct 60. Contract
AT(04-3)-189, PA »11. 50p, Order from OTS.
$1.50. GEAP-3558
A report on dissolved O2 in the primary coolant d
the Ker loops, by L. M. Eikum. Hanford Atom-
ic Products Operation, General Electric Co. ,
Hanford, Wash, ^r 59. Contract W-31- 109"
Eng-52. 30p. Order from LC. Mi $2. 70,
Ph$4, 80. HW-60991
COFir-'A 709 program fcH" determining extrapo-
tatlai lenyth from horizontal traverse data, bv
). D. Matsumoto. Hanford Atonic Products
Operation. General Electric Co. . Hanford.
Wash. Aug 59. Contract AT(45-1)- 1350. 15p.
Order from LC. Mi $2. 40, ph $3. 30. HW-61204
Semiconductor switching for nuclear reactor control
ilheais). by J. H. Greer. Atomic Products Oper-
ation, General Electric Co, , Richland, Wash.
1960, Contract AT(45- 1)1 1350, 49p, Order
fromLC, Mi $3, 30, ph $7. 80. HW-SA-1830
MTR-ETR Technical branches Quarterly report
April 1-hine 30. i960. Phillips Petroleum Co, ,
Atomic Energy Division, Idaho Falls, Idaho.
Jan 61, Contract AT(lO-l)- 205. 72p, Order
from OTS. $2.00. IDO-16648
ABWR Quarterly pro^gress report for lulv 1 to Sep-
tember 30, 1959. Volume I. SL-1 operation and
evaluation. Volume U. SL-1 health physics and
gafetv. Volume III. ABWR design and deveI^iP~
ipent. Combustion Engineering, Inc. Nuclear
Dlv, , Idaho Falls, Idaho. Oct 59. Contracts
AT(10-l)-967andDA-44-l92-eng-ll. Vol. I.
64p. , Vol. II, 25p, , Vol, III , 143p. Order from
LC. Vol. I, mi $5. 40, ph$15.3o. Vol. II,
mi $2. 70, ph $4. 80, Vol , III, mi $7. 50, ph
$24,30, Volumes issued separately, but
cataloged as a unit. IDO- 19005
Army gas-cooled reactcr Bystenis
my gas-cooled reactcr systems program
progress report for August 190U. Aero<<
era] Nucleonics, San Kamon. Calif. Sep
ram monthly
srojet Gen-
., Sept 60.
?."V"'*^^'^<^0'1>"8*^- 95p. Order fromLC.
Mi $4. 80. ph $13. 80, IDO- 28562
Transient hydrodynamic operation of EGCR
coolant system, by D. W. Burton. Union
Nuclear Company. Oak Ridge Gaseous Di:
lyin
, . Carbide
ompany. Oak Ridge Gaseous Diffusion
Plant, Oak Ridge, Tenn. Mir 61. Contract
W7405 eng 26. 29p, Order from OTS. 75 cents.
K-1468 Part I
Turret pglrrtnar y nuclear calculations, by B. M.
uarmichael and others. Los Alamos Scientific
Laboratory of the University erf California, Los
Alamos, New Mexico. Mar 61. Contract W-
7405-ENG,36. 47p. Order from OTS, $1.00.
LAMS- 2482
A study of multipurpose plants as an f^proach to
competitive nuclear power. CaHfornla Hpfl«»arn>i
and Development Co. Livermore Research Lab. ,
Livermore, CaUf. Dec 53. Contract AT(ll-l)-
74. 71p. Order from LC. Mi $4. 50, ph $12, 30,
LRL-79(DeL)
Operation and analysis of a 3000KW liquid metal
moael steam generator, ed. by L. f. Wt>h«fPr
Atomics International, North American Aviation,
Inc. , Canoga Park, Calif. Feb 61 , Contract
AT(ll-l)-gen-8. 211p, Order from OTS. $3.00
NAA-SR-4884
827
Ejq)erlmeatal evaluation of a aodium-to-sodium
heli^low hejt exchanger at temperaturcB up to
1200" F, by J. i>. McDonald. Atomics Internation-
al, A Division at North American Aviation. Inc. ,
Canoga Pari, Calif. Feb 61. Contract AT(1 1-1)-
GEN-8. 4lp. Order from OTS. $1.00.
^ NAA-SR-5661
ProceedingB o the organic cooled reactor forum
— October 6-y. 1960° by R. H.J. Gerclce and others.
Atomics International, A Division of North Ameri-
can Aviation, Inc. , Canoga Park. Calif. 1960.
306p. Ord^r from OTS. M-OO. NAA-SR-5688
OtAR steam c^cle study, by G. S. Budney. Atomics
Internatioipl, Division of North American Avia-
tion. Inc., Canoga Park. Calif. July 57. 9p.
Order frot<i LC. Mi Jl.80. ph $1.80.
NAA-SR-Memo-66-
Stainless ste^l clad fuel for the OMR, byW. Leggett.
Atomics Itjternational, A Division of North Ameri-
can Aviati^Ki, Inc., Canoga Park, Calif. Oct 57.
16p. OrdirfromLC. Mi $2.40. ph $3.30.
NAA-SR-Memo-2217
OCR fuel and' clad survey, by H. I, Raiklen.
Atomics Ititernational, Division of North Ameri-
can A viatitn, Inc., Canoga Park, Calif. Jan 59.
20p. OrAtr from LC. Mi $2.70. ph $4.80.
NAA-SR-Memo-3330
Nuclear calculations for xylene moderated OMRE
core, by 8. Moakowiu. Atomics International,
A Divisioq of North American Aviation, Inc.,
Canoga PWk. Calif. Feb 59. 6p. Order from
LC. Mi $(1.80. ph$1.80.
NAA-SR-Memo-3538
OCR steam aenerator by-pass organic flow control,
by R. F. Audette. Atomics International, A
Division df. North American Aviation, Inc. ,
Canoga Pairk. Calif. Apr 59. 8p. Order from
LC. Mi $1.80. ph$1.80.
NAA-SR -Memo- 3787
Additional safe
core of the '
aics fci
rds evaluation for the U- Mo fueled
lear power facility, by
Division of Nortn Ame
Ham nucl
Atomics kite r national. Division of North Ameri-
can Aviation, Inc. , Canoga Park, Calif. July 59.
60p. Orir from LC. Mi $3. 90. ph $10.80.
NAA-SR -Memo-4067
Burnup studies for the U-10 w/o moly reference
design ^1 elements loading of the HNPF core
using the mark a control rod scheme by R. H.
Davidson. Atomics International. Division of
North Anaerican A/iation, Inc.. Canoga Park,
Calif. Ji*y59. 29p. Order from LC. Mi $2. 70.
Status report for sodium graphite reactors. Atom-
ics International. Division of North Anjerican
Aviation. Inc. . Canoga Park. Calif. July 59.
llOp. Order from LC. Mi $6.90. ph $21.30.
NAA-SR-Memo-4156
Power diatributions and control rod analysis, by J.
Hume and M. P. .\ronchick. Atomics Iniernatioo-
al. Division of North An>erican Aviation, Inc. ,
Canoga Park, Calif. Oct 59. 29p. Order from
LC. Mi $3.00, ph$6.30.
NAA-SR-Memo-4426
Origin and removal of asymmetries in Sy>j approxi-
mations the Bolumann equation, byR. A. Axford.
Atomics International. Division of North Ameri-
can Aviation. Inc. , Canoga Park. Calif. Mar 60.
Up. Order from LC. Mi $2.70. ph $4.80.
NAA-SR -Memo- 5103
Reactivity worth of control rods in the PIOUA OMR
critical assembly, by K. Einfeld. K. Einfeld. '
Atomics International. Division of North Ameri-
can Aviation. Inc.. Canoga Park, Calif. May 60.
lOp. Order from LC. Mi $2. 40. ph $3. 30.
NAA-SR-Memo-5270
Resonance absorption in D^O lattice reactors, by
— W. L. Brooks and H. tJoodak. Nuclear lievelop-
roent Corporation, of America, White Plains, N.Y.
Sep 60. Contract AT(30-l)-2303. 35p. Order
fromLC. Mi $2.70, ph $4.80. NDA-2131-19
Design report on the aircraft reactor test, by A. P.
FrassandA. W. Savolainen. Uak Ridge i'latiooal
Laboratory, Oak Ridge, Tenn. May 56. Decl.
with deletions October 19, 1959. I63p. Order
fromLC. Mi $7.50. ph $24.30.
ORNL- 2095 (Del.)
Investigation of fluid flow in the art and other
reflector -mode rated reactor cores, by C L.
Muller and others. Oak Ridge National Labora-
tory, Oak Ridge, Tenn. Apr 58. Decl. Novem-
ber 24, 1959. Contract W-7405-eng-26. 148p.
Order from LC. Mi $7. 20, ph $22. 80.
ORNL-2199
Gas-cooled reactor project. Quarterly progress
report for the periocl ending December 31,"T960,
by 5u^ o^ Oak Ridge National Laboratory, Oak
Ridge. Tenn. (nd). Contract W-7405-eng-26.
341p. Order from OTS. $4.50. ORNL-3049
Effect at heat flux on the corrosion of aluminum by
water. Part II. Influence of water temperaturg,
velocity, and pH on cortoe ion -product formatioo.
by J. C. Griess and others. Oak Ridge National
Laboratory, Oak Ridge. Tenn. [nd). Contract
ph $4. 80
NAA-SR -Memo-41 39
828
W-7405-eng-26. 38p. 6rder from OTS. $1.00.
ORNL-3056
Monthly technical report for March 1960. Power
Reactor Development Company, Detroit, Mich.
1960. Contract AT(ll-l)-476. 30p. Order
fromLC. Mi $2.70. ph $4.80. PRDC-TR-33
Itoithly technical report for April 1960. ^svfr
Reactor Developinent Company, Detroit Mich.
1960. Contract AT(ll-l)-476. 22p. drd^
fromLC. Mi $2.70, ph $4.80. PRDC-TR-34
Heavy water power reactor program monthly prog-
report, June 1960. St '
tions Onice, Atomic Energy Commission.
res 8 report, June 1960. Savannah River Opera-
Aiken, S. C. 1960. 19p.
Mi $2. 40. ph$3. 30.
Order from LC.
SRO-34
Heavy water power reactor prograin. Monthly
progress report for September 1960. Savannah
River Operations Office, Atomic Energy Com-
mission, Aiken. S.C. 1960. 21p. Order from
LC. Mi $2.40. ph$3.30. SRO-37
Nuclear training reactor for the AEC reactor tour.
Preliminary report and hazards analysis. Lock-
heed Nuclear Products, Marietta, Ga. Feb 60.
Contract AT( 49 -9)- 1777. 72p. Order from LC.
Mi $4. 50. ph $12. 30. TID-5906
Monthly operating report for June I960. Duquense
Light Company, Snippingport, Pa. r960. Con-
tract AT(ll-l)-292. 42p. Order from LC.
Mi $3. 30. ph $7 . 80. TID-6378
A study of wet steam as a reactor coolant. Progress
report for the month of September 1960. Nuclear
Development Corporation of America, While
Rains, N. Y. Oct 60. Contract AT(30-1)-2303.
26p. Order from LC. Mi $2.70, ph $4.80.
TID-6893
Study of conventinnal steam power P|*"t8. Capital
and energy costs 44 000 and 12.650 KW (gross).
Kaiser tngineers, Division of Henry J. Kaiser
Company, Oakland, Calif. Aug 60. Contract
AT(04-3)-334. 82p. Order from OTS. $2.00.
TlD-8532
Study of nuclear power plants capiul and power
neration costs 44 and 12. 65 MWE (grows).
iser Engineers, Division of Henry J. Kaiser
Company, Oakland, Calif. Oct 60. Contract
AT(04-3)-334. 185p. Order from OTS. $2.75.
TID-a533
Study at conventional process steam plants capital
and steam production costs — 125, OOO pounds
per hour (^MWT). Kaiser Engineers Division
of Henry J. Kaiser Company, Oakland, CaUf.
Oct 60. Contract AT(04-3)-334 suppl. 36p.
Order from OTS. $1.00. TID-8534
The Livermore pool type reactor (LPTR), by J. B.
Radcliffe, Jr. and E. E. Hill. Lawrence Radia-
tion Laboratory, University of California.
Livermore. Calif. Nov 60. Contract W-7405-
eng-48. 56p. Order from GTS. $1.25.
UCRL-4919 Rev.
Tory II- A reactor control system developments,
by R. E. Finnigan. Lawrence Radiation Labor-
atory. University of California. Livermore,
Calif. May 60. Contract W-7405-eng-48. 45p.
Order from LC. Mi $3. 30, ph $7. 80.
UCRL-5465
Transient thermal stress In tubular reactor ele-
ments, by LaMar I. Deverall. Lawrence
Radiation Laboratory, University of California,
Livermore, Calif. Sept 60. Contract W-7405-
eng-48. 21p. Order from LC. Mi $2.70.
ph $4. 80. UCRL-5887
Pulsed neutron measurement of control rod worths,
by O. C. Kolar and F. A. Kloverstrom. Law-
rence Radiation Laboratory. University of Cal-
ifornia, Livermore, Calif. Aug 60. Contract
W-7405-eng-48. 24p. Order from LC. Mi
$2.70. ph $4. 80. UCRL-6070
PressuVlzed water reactor (PWR) project: technical
progress report for the period December 24.
1960 to February 23, 1961. Bettis Atomic
Power Laboratory, Westinghouse Electric Corp.,
Pittsburgh, Penna. fci.d.]. Contract AT-U-l -
gen -14. 104p. Order from OTS. $2.25.
WAPD-MRP-90
Transfer functions for boiling reactor stability
calculation, by S. G. Margolis and S. Kaplan.
Bettis Atomic Power Laboratory. Westinghouse
Electric Corp. , Pittsbur^i, Penna. Apr 60.
Contract AT-1 1-1 -gen- 14. 48p. Order from
LC. Mi $3. 30, ph $7. 80. WAPD-T-1158
Over -all evaluation of blanket fuel removed from
fWR core 1 during the first refueling of the
seed, by F. Schwoerer. Bettis Atomic Power
Laboratory. Westinghouse Electric Corp..
Pittsburgh, Penna. Feb 61. Contraa AT- Il-
l-gen-14. 20p. Order from OTS. 50 cents.
WAPD-TM-266
829
.-J
TJ V. ,
, -. ^
■ i) ,
ItV it« ».i
SOUTCT
RasMrch Late. ,
HvrardU.. Otmbrldfe,
P^
7i7
A^Blnl Corp . ducafo. III. 711
Aaro-Sfiace LMb. , Honb
Aawrlcan Aviation. Inc.
Calif.
AaraalMtlc and Structure R«-
nardi Lab. . Maaa. Inai. al
TWi. . Cambrtdgr
iUrotat-Cenaral Corp. ,
Calif.
AaroBaullcal Engine Lab. ,
Hani Air Material Center,
Mladelptaa. Pa.
736
708
747
735
AaroMUdcal Inairumeni L«b. ,
Naval Air Devclopcneni Ccniar,
JdHavUle, ■>* 709
AaroMuttcal Materula Lab. ,
Naval Air Maieriala Ceatm-.
Ikiladelphla. Pa. 77S
Aaroaautlcal Reaearch Lab. .
Wrt^'Air Ovelopmeni Dlv.
•rIgil-Patteraon AFB. Ohio
769
Air Force BalllaUc kllaalle Dlv..
Air Reaearch and Devekipnieat
Command, Loa Ar^lea. Calif. 736
Air Force Cambridge Reaearch
Late., Bedford, Maaa. 704
Air Force Command and CoMrol
Oavelopmenl Dlv. . Bedford,
Air Force Plight Teat Center,
BdMrda APB. Calff.
6S2
6*4
755
Air Force Inat. of Tech. .
Wrll^-Paiteraon APB, Ohio 711
Air Force Mlaaile DevelofMneni
Canter. Hollocnan AFB,
N. Mex.
Air Force Special Weapona
tr, Klrtland AFB.
737
154 535
ISO 710
1SS144
171 247
171 248
171 249
171 250
155 089
154 303
154 063
154 064
154 716
171 609
153 731
N. Mex.
783
155 2S4
Air Proving Ground Center.
BgllaAFB. FU.
709
133 861
Alrboroe laetnimeaia Lab. .
Mthrtllc. N. Y.
718
190 901
Alrteme Inatrumeala Lab. .
MlaeoU. N. Y.
709
718
154 743
1SS258
All American Engineering Co.
«llmli«laa. Del.
709
161 914
161 915
Allied Reaeardi Aaaoclatea,
lilica. Maaa.
737
148 216
AateraiCotl.. MaM.
6W
154 872
154 873
154 874
Aaertcan Electronic Lataa. ,
hK.. Ruiadelphla, Pa.
719
153 594
Aamon Inat. for Reaearch,
noaburgh. Pa.
682
154 S22
SOURCE INDEX
FB Number
Source
fr
n Number
Amphanol Electronica Corp. ,
Chlca«D, III.
719
150 849
150 198
Andaraoa-Nlcbola aod Co, ,
154 241
Boetoo. Maaa.
SOS
155 030
Applied Mathematlca and
Sutlatlc* Laba.
Stanford
133 870
U., Calif.
r '
...
684
148 756
149 521
149 522
-
7a
148 099
155 090
,
758
147 844
"
.-
799
148 420
148 782
154 434
'-'■ '
149 334
14* 398
149 750
"'
807
147 842
171 257
K-
147 843
149 323
Applied n>ratC8 Lab. , Jc
HopklM U. . Silver Sprlog.
tU 699
Applied Paychoioglcal Servicea.
Wayw. Pa.
Arctic Aeromedlcal
LaddAFB, Alaaka
Arctic Inat. of North America,
Waahli«too, D. ^ 707
Armed Service* TecAalcal
InformatKai Agency,
Arlli«tan. Va. 681
8C7
Armour Reaearch Poindatlon.
Chlcafo. III. 691
719
781
783
Army Balliatlc Miaalle Agency,
Radauae Araenal, Ala. 737
733
Army Chemical Reaearch and
Development Labs.. Army
Chemical Center, Md. 691
732
Army Reaearch Office,
Waahlngion. D. C.
Army Rocket and Guided
Miaalle Agency, Redatone
Araeoal, AU.
Army Signal Reeearch and
Development Lab. , Fort
Monmouth, N. ].
699
699
SCO
70S
Army Tranaporutloo Rea
Command, Port Euatla,
752
789
792
sarch
Va. 709
Source
P>a» WNuaifcer
AraoM Ei^ineerli^ Develop-
ment Center, Tullahoma.
Tens.
1-1
790
769
7J7
Automatic Mfg. Dlv. , General
laatruroaat Corp. , Newart,
N. J. 719
Avtabon Medical Acceleration
Lab. , Naval Air Development
Oeaier, Jchaavllle. Pa. 689
710
748
Bartol Reaearch Pouodatlaa,
Praaklla Inat. , Swarthmore,
Pa. 719
Batielle MemorUI Inat.
Columbua, Cklo
754
779
793
134 538
Behavioral Scienoea Lab. ,
Wright Air Development Dlv. ,
Wright -Patteraon AFB. Ohio 682
769
Bell Aircraft Corp. ,
BufUlo. N. Y.
683
732
148 774
133 900
Benaoo- Lehoer Corp. ,
Suva Motdca, Caltf .
688
785
786
154 168
154 169
154 167
BioKchnology Lab. . U. of
California. Loa Anpelea
154 551
171 689
171 519
171*08
153 777
171 996
130 901
153 947
155 231
133 232
135 0*5
153 841
133 843
133 843
134 438
171 M2
171 133
133 619
134 208
134 331
154 332
134 333
134 329
133 716
134 330
134 sn
171 614
171 613
133 533
153 648
153 846
Birmingliam U. (Ct. Brtt.)
Boeing Scientific Reaearch
Laba., Seattle, Waah.
Borden Chemical Co. ,
Philadelphia. Pa.
Boaton U. School of MadiLiw,
6*2
690
786
753
MO
Brltiah Cotton loduatry Re-
aearch Aaaociation
BromU., Pi u» Mate. R.L
751
793
Brown U. Dlv. of Applied
Mathematlca, Providence, R. L 760
768
773
BOl
BrovB U. Div. of Engineerian
Providence. R. I.
Bureau of Miaea. Barttaevllle.
Ohio
Bureau of Mlaee,
Pittaburgh, Pa.
Buraeu of Naval Kraonnel.
Waahington, D. C.
Bureau of Naval Weapoaa,
Waahlngnm, D. C.
Bureau of Shipa,
Waahington, D. C.
Bureau of Yarda and Docka,
Waahington, D. C.
Burke Reeearch Co. ,
tanpano Beech, Fla.
Burke Reaearch Co. ,
Warren, Mich.
CalMoniaU., Berkeley
768
SOI
694
738
683
740
744
744
783
757
7S7
790
133 199
154 468
153 695
153 694
153 907
171 617
153 190
133 923
171 601
171611
171*00
134 213-1
154 213-2
764 190 909
149 444
133 714
148 974
171 S«S
171602
644 171 374
132 00*
133 849
149 16S
148 813
154 1)0
134 121
134 862
148 S4B
150 739
148 970
19903*
192 022
133 74*
133 29*
155 413
171 231
193 Mi
171 57*
171 579
133*33
Source
CaUtoraia U., Bertc^Ccoo.) SOI
CaUtoniaU.. Loa
A laelea
705
712
719
720
764
7S4
M7
Caatorra U. Coll. (A uatralu) 761
Caroefle loat. of T«^
Plttaburgh. Pa.
Carnefie loat. of Te^
Graduate Sdiool at
Admifiisirailan. PltlatMrgh
Ca*oiicU. of Anterfa,
Waahiagioo. D. C.
CB5 Electronics Div
Columbia Broadcasdnf Syatem,
lac., Dunara, Iiia4a
Cancer for Radiophyatca and
Space Reaeardi. Qtrnell U.
Ithaca. N. Y.
OaHiiieraU. cf T«
783
7r7
SOI
nduatrial
Pk.M3
74S
749
Ckeaapeake Bay Inat.
lohM'
Ho|*lnaU.. AnuixilM, Md.
Chlcafo U.. III.
Clark U. . Woroestei
Clavcland nieumaiic
OMo
Maaa.
Tool Co. .
CUmax Molybdenum y>. cf
Mldugan, Detroit
Coaaial Studlea loat. ,
Stan U. . Baton Rou p
Lab.
Coaling and dteinlca
Aberdeen Proving G round. Md. 7SB
Colorado Scbool of M|nea.
Golden
Colorado U.. BoukJci
Columbia U. . New W rlc
' / / /
Compagaic Ceoerale le TeW-
grafAie. Sana Fil(1 'ranee)
Lousiaoa
710
720
799
7B9
692
794
707
778
775
704
Coavair, Fort Worib,
Coorair. San Diego. ZtMl.
Cook Rescarcb Laba. ,
Morton Grove. Ill
CoraeD Aartjoautlcal
faK.. BuOalo. N. Y
Cornell U., Idiaca. • .Y.
CrTOgaolc Englneerli | Lab.
Nailoaal Bureau at ^aadarda,
ar. Colo.
Curtiaa- Wright Corp
Pa.
Tex.
73S
791
760
805
720
794
7S4
770
779
720
Lab.
WWiMnber
154 458
' 154 447
154 245
149 816
149 137
149 138
171 572
1S2 114
154 088
154 123
154 863
154 B64
154 868
148 313
148 7S7
149 088
154 869
153 82B
153 829
150 912
154 Z72
150 414
150 654
14B781
150 489
154 870
171 597
149 2U
171 330
171 256
153 207
154 098
148 401
153 719
150 545
155 322
150 866
153 295
1SS147
710
154 744
760
147 559
770
149^28
I49S9S
Soaroa Pag
Curtiat-Wrlgbt Corp. ,
Santa Barbara. Cillf. 770
David Sarnon Reaearcb
Center. Princeton. N. J. 721
David Taylor Model Baaln.
Waatainglon. D. C.
Davidaon Lab.. Sievena Inat.
of Tech. , Hoboken. N. ].
Dayton U., Ohio
Defenae Meula InformaUon
Center, Battel:: Memorial
Inat., Columbua. Ohio
Dkpartmenl a< the Navy.
Waahlagton, D. C.
De Paul U. . Cluca«a, III.
Development Engineering
Corp., Washington, D. C.
Dewey. G. C. , and Co. ,
Inc. , New York
721
735
744
745
765
774
750
756
740
776
778
779
752
695
721
782
Diamond Ortkiance Pu<e Laba,
Waahington. D. C. 722
788
802
Digital Computer Lab. , Maaa.
iaat. of Tech.. Cainbr.d«e 765
DIgtuI Computer Lab. . U. of
IlUnota, Urbaaa
I
,Dlrectorate at Advanced Sys -
I tains Tech. . Wright Air
Development Div. . Wright-
htterson APB, Ohio
Douglas Aircraft Co. . Inc. ,
Santa Monica, Calif.
774
788
765
788
802
Dunlap and Aaaociatea. Inc. .
Stamford, Conn.
722
Dynamic Analyaia and Contol
Lab.. Mass. Inat. of Tech..
Cambridge 807
Dynamic Simulationa Lab. ,
Ordnance Taok-Aulamuclve
Command. Center Line.
Mich 738
Educatlanal Teating Service.
Piinceton. N. ].
Electrical Englaeering Re-
6B5
1-2
171 604
154 523
154 525
154 526
155 577
154 307
155 064
155 253
149 745
153 706
153 707
155 578
153 919
154 165
153 713
155 oa3
161 239
151 107
n\ 108
161 236
151 106
151 104
151 105
161 237
155 3B1
154 269
155 025
155 324
15S61S
171 582
148 958
171 559
155 376
148 394
154 103
171 258
152 061
150 243
Di^fway Proving Ground. Utah 760 148 212
150 910
ISO 911
147 787
153 866
150 433
801
171 618
search Lab., U. of Illinois.
802
171 619
171 620
Urbana
Electrical Engineering Re-
search Lab. . U. al Texaa.
804
154 448
720
149 847
Auatln
788
804
154 102
147 840
Source
Paa
Electro-Optical Syatema, Iik..
Paaadena. Calif. 788
Electron Biyslcs Lab. .
U. of Michlgin. Ann Arbor 722
mNintor
155 573
154 501
154 S02
Electron Tube and Microwave ,
Lab.. Calif. Iaat. of Tech.,
Paaadena 723
Electron Tube Reaearch Lab. .
U. of MInneaou. Minneapolis 723
Electronic Defense Lab. ,
Sylvanu Electric Producu,
Inc. . MountaiB View, Calif.
Electronica Reaearch Lab. ,
U. of CalifomU, Berkelfy
723
724
760
-^ .. »07
Erie Reaiator Corp. . State
Collefe, Pa. 724
Pairdiild Aircraft and MlssUe
Div.. Hageratown, Md. 710
Feltman Reaearch Laba..
Picatinny Araenal. Dover, N.j.
695
738
Flight and Engineerli^ Teal
Group. Wright Air Develop-
ment Div.. Wright- htterson
AFB. Ohio
Flight Control Lab. . Wright
Air Development Div.. Wright
Patieraon AFB. Ohic.
770
783
710
770
Florkte State U. , Tallateaaee 695
Florida U. Coll. of Agriculture.
Gainesville 687
Florida U. Engineering and
Industrial Experiment Sution,
Gainesville. Fls.
Ford Instrument Co. , Long
Uland City. N. V.
Foreat Products Lab. .
Madiaon, Wia.
FrefaaiACo..
Clendale. Caltf.
Prick Chemical Lab.,
Princeton. N. J.
General AtonUc. San Diego.
Calif.
Ceoaral Broiu« Corp. ,
Garden aiy. N. Y.
General Electric Co. ,
Evendale. Ohio
General Electric Co. ,
Syracuse, N. Y.
General Electric Reaearch
Lab.. Schenectady, N.Y.
General Electronic Laba.,
Inc.. Cambridge, Maaa.
General MIIU. Inc..
Minneapolia, Miw.
148 323
154 450
723 154 213
150 109
148 098
150 792
153 704
153 706
153 211
148 502
153 723
155 146
ISO 730
153 022
171 604
171 616
J55 255
171 593
148 937
148 938
148 966
696
154 251
724
150 900
710
154 955
739
154 289-3
699
149 083
17157$
791
799
154 457
153 584
725
153 S64
770
154 572
725
155 073
754
171 595
725
150 847
706
154 163
154 376
Source
Caograpbiachea Inatitut der
UatveraitJIt Zbrich
(Iwitierland)
OaiMgi Waahingtoa U. ,
WaahlogtoB. a C.
Cuanis loet. o' Tech. Bagi-
narlng Experiment Siatkai,
Atlanta
Ciaanlni Controla Corp. ,
Duarte, Calll.
I Aircraft Engiaecr-
H^Corp. , Beihpi^, N. Y.
f!E
7S3
7S0
72S
736
779
780
Gaggenteim Aeronautical Lab.
Calif. Inat. of Tech.,
haadena
Cuggeaheim Jet Propulsion
CMtar, Calif. Iaat. erf Tech.
I bKkiatriea, lie. ,
Macuchen. N. J.
Harvard Coll. Obaervalory,
Cambridge. Maaa.
Harvard U.. Cambridge.
Hawaii Inat. of Geoph> ic*.
HoMitalu
Hawker Siddeley Nuclear Power
Co., Ltd. (Ct. Brit.)
Naraaa Etactroaica Co. ,
Cambrtdge, Maaa.
Hi^ Altitude Observatory,
loulder. Colo.
High Energy Phyaica Lab. ,
ScaafordU., Calif.
Hlller Helicopter Corp. ,
ffeloAIco, 0|1U.
Honeywell Reaearch Center.
Hopklna, Minn.
Howard induatiiea, Inc.,
Racine, Wla.
Laba., Columbia U..
New York
Hugh Aircraft Co. , Malibu,
Calif.
786
791
726
696
706
7S1
765
706
784
7U
794
72*
707
726
NlHaB Reaources Reaearch
OBoe, George Washington U.,
Waahiiwton. D.C. 683
Hydrodynamica Lab. , Calif. ,
laac. of Tech. , Paaadena 774
n Number
Source Pa^e
FB Number
155 438
Inaucutc for Fluid Dynamica
arid Applied Matbematica, U.,
of MaryUnd, College Park 700
761
788
154 509
147 904
154 OBO
153 756
154 166
155 568-1
155 568-2
155 568-3
1S5 569-1
153 752
153 750
153 751
149 540
148 935
1SSS67
154 585
171 571
154 566
153 914
154 087
154 275
150 171
1S3 642
150 558
ISO 846
153 781
154 595
154 596
153 865
154 871
DItoato Iaat. of Tech. , Cklcago
748
768
148 095
153 124
UlaataU., Urbaaa
727
7M
780
154 114
154 958
154 553
Ulnoto U. Coll. of Medlcuie,
CMcafD
746
155 566
hritaaa U. , Bloomington
805
153 SOS
liduatnal Teat Lab. .
Ihiladalphis Naval Shipyard.
Pa.
742
155 250
hpwaoll KaUmazw) Div. .
iaig-Wamer Caep. , MM*.
749
IS3 917
Inadtute for the Study of
MetaU, U. of Chicago. III.
Ifacltute for die Study of Rate
Proceaaes. U. of Utah. Salt
iQty
806
700
Inatltute of Engineering Re- '
search. U. of California,
Berkeley
Inatltute of Flight Structurea,
Columbia U. , New York
Inatltute of Mathematical
Sciences. New York U. N.Y.
Inaatuie of Rubber Research,
U. of Akron. Ohio
Inatltute of Science and Tech.
U. of Michigan, Aon Arbor
laatituia of Siatiatica, U. of
North CarollM. Owpel Hill
774
776
761
761
775
757
758
707
802
761
762
Inatltute of Tech. . U. of
Mlnneaota, Minneapolia 762
Inaucuie of Theoreucal
Phyaica, Stanford U. . Calif. 784
loaututo de Quimica Fisics
(Spain) 696
700
International Buauieas
Machines Corp. . Yorktown
Haighta, N. Y. 765
766
Iowa Engineering Experiment
Statioa, Amea 791
)et Propulsion Center. Purdue
U., Lsfayette, Ind. 747
Johsnnes Guienberg-UniversitUt
Mainz (West Germsny) 681
Joboa Hapkioa U. , Balamore,
727
7B2
Johns Hopkins U. School of
Engineering, Bsltiinore, Md. 775
ICellett Aircraft Cwp. ,
Willow Grove, FO.
Laboralolce Central des
Industries Electriques
(France)
Laboratoire d'lnfrs I
Technique ei Applique,
Clf-sur-Yvette (Frsnce)
711
794
792
LaboraBMre de Ferromag-
netiame, Inatitut de niyaique '
Straabourg (France) 789
Laboratory of Chemical and
Solid -State niysics,
Maaa. Iaat. af Tech.,
Cambridge 794
»-3
154 865
154 709
150 624
155 153
ISO 994
148 906
148 907
152 117
ISO 844
ISO 845
153 915
154 508
154 088
154 123
154 094
154 124
154 452
153 187
154 465
1S3 911
150 086-1
150 086-2
150 086-3
ISO 086-4
IS0 086-S
IS0QB6-6
153 082
155 149
153 718
152 965
154 261
153 783
153 851
152 199
153 467
154 364
150 642
SoMTca
Laboratory of Climatology,
Centerton, N. J.
Laboratory of Statiatical Re-
aearch, U. of Waahington,
Seanle
Land Locomotian Lab. , Ord-
I Tank-Automotive Com-
Center Line, Mich.
Life Support Syatema Lab. ,
Wright Air Development Div.
Wright Patterson APB, Ohio
Lightning and Tranaients Re-
sesrcfalnat. , Minneapolu,
Minn.
Faae PB Number
706 154 527
Lincoln Lab. , Maaa.
Tech., Lexington
Inat. of
Lisbon U. (Partial)
Little, Arthur D., Inc.,
Cambridge, Maaa.
Lockheed Aircraft Corp. ,
Sunnyvale, C^alif.
LoodonU. (Gt. Brit.)
< Louiaiana Sute U. ,
Baton Rouge
762
786
750
751
711
804
727
739
762
763
7b7
795
803
756
756
763
762
665
700
Lowey-Hydropreas Dtv. ,
Balwin- Lima-Hamilton Corp. .
New York 749
Malluickrodt Chemical Lab. ,
Harvard U.. Cambridge,
696
696
791
Marine niyaical Lab. , Sciippa
Inatitution of Oceanography.
San Diego, Calif. 707
Mar(|uardt Corp. , Van Nuya,
Calif. 747
Material Lab., New York Naval
Shipyard. Brooklyn. N. Y. 727
Material Labs., Pugei Sound
Naval Shliqrard, Bremerton,
7SB
147 847
148 974
152 004
1S2 006
152 006
152 007
152 OOB
152 009
171 599
154 273
154 061
154 589
154 588
152 957
153 486
153 905
154 SB7
154 062
171 573
154 449
155 256
171 252
154 349
154 094
154 124
147 902
147 903
150 967
171 568-1
171 568-2
154 262
155 453
148 563
153 781
155 383
MaryUodU., College Park
786
154 243
799
152 180
Massachuaetu Inat
of Tech..
Cambridge,
689
148 214
700
150 031
771
149 778
784
154 706
791
154 092
803
148 353
803
154 449
Maaaadiuaettt Mental Health
Center, Boston
685
171 610
Massachuaetu U. .
Amherat
701
154 518
155 320
154 281
Ummriaia Hwarcfc Lik.
U. ofCaUfomla. Be teiey
Milka iMi. . noatwrt IP*. 696
MldUgaa Sun U. . B4KLaMU«762
lU. , AoB Ar
U. Coil.af llifl-
Aao Arbor
781
795
809
775
792
MlcklCMU. Coil. a( L teranire .
Sdaaca, •ad the Ar^,
Am Arbor
lU. M
Aaa Axtaar
MicrotKh
Ulcrovaiw Reaaarch I
totytachiuc Inst, al ^ooklyn,
N.Y. 728
nrd loat.
rck ( b. .
727
748
Ml— nwi U. , Mlnna^lH
Ml—lim U. School
Mlaaiaaippt StM* U.
ScaaCoUafi
MouM WaaUoctoal
Gottan. N. H.
National Buraau of !
Boulder. Cote.
Otaenrsmry.
Staidardi.
NaOoaal Buraau of Sia^rda.
B. O. C.
Va.
NaiMoal Reaearch
Ooawa (Canada)
Naval A
Suttoa.
NiMl ATlonica Pacill^'.
IWanapotti. lad.
Naval am Enflaearli
PonHMeaama. Callt
796
711
693
7U
771
766
76»
808
778
711
729
735
792
728
701
712
713
714
715
71«
717
WWimtiar
150 006
148 516
171 570
147 847
190 534
148 951
149 567
150 726
152 135
150 902
1S3 847
150 906
154 804
155 160
171 569
171 594
153 784
148 918
148 317
ISO 848
161 S77
151 3n-8
161 SB9
171 253
154 549
154 590
154 725
155 437
154 487
154 «S»
154 615
154 679
154 (
1541
IS4<
154 613
154 614
154 619
154 623
154 62S
154 629
154 672
154 678
154 621
154 653
154 663
154 666
154 669
154 870
154 671
154 673
154 647
154 648
154 665
154 667
154 6«*
154 682
154183
154 469
1 W/T
ii
Sourca
Naval Civil Ei^oearliig Lab.,
Port Huenema, CaUf. (coa)
Naval Baflaaerlag Experiment
Stadoa, Annapoli*. Md.
Naval Medical Re
Md.
■rdi laat.,
Naval Miaalle and Aatronauilca
Caetar. l\>«mMii(u. Calif.
Naval Ordaancc Lab..
Coroaa. Calif.
Navel
WUKOak
Md.
Naval Ordnaaca Teat Stailaa.
OUW Lake. CaUf.
Naval hMtgraduaia Scbool,
MoBvrey. CaUf.
f*i?
n Number
Source
Neval Radldoflcal Oeleaae
»^
PBNianbar
717
154 617
Lab. . Sao Fraaclaco. Calif.
154 630
(COB.)
783
153 891
154 633
785
153 582
t
154 645
154 654
Naval Reaearcfa Lab .
154 700
Waflbli«tan. D. C.
713
171479
718
154 644
730
171691
154 652
• ■•^- '
769
151 9SI
7M
154 618
778
171 188
154 624
808
171 318
154 643
154 651
Naval School of AvUtlon
154 t«0
Medicloe, Penaacola. FU.
763
155 087
154 681
730
154 639
Naval WeapoiM Lab..
154 656
Dahltren. Va.
740
155 296
735
154 634
769
153 904
736
154 626
742
154 622
154 642
Navy Medical Neuropeydilatrlc
Reeearch Unit. San Diefo,
743
154 627
154 655
154 657
154 675
Calif.
Nepa Div. . Palrdilld Engine
and Airplane Corp. . Oak
687
154 593
154 677
Ridfc. Tena .
782
155 439
154 689
155 431
744
154 674
155 433
745
154 616
154 640
154 664
Netberlamte Ship Model Baaln.
784
155 438
746
154 649
154 660
154 662
154 676
Wafrainfen
New Jcracy Ceramic Reaearcb
Station. Ruiyira Suie U..
746
153 729
747
154 635
154 646
New Brunewick
795
150 913
748
154 637
Na* Mexico Suie U. ,
751
154 658
Univeralry Park
799
149 911
753
154 620
154 636
New Mexico U. . AUuquerque
782
154 704
798
154 650
154 661
New Mexico U. Enctneertaf
781
154 611
Experiment SuUoa.
154 612
Albuquerque
730
155 079
154 641
785
153 908
New York State Coll. of
154 697
Ceramlca. Alfred U.
754
132 980
790
154 631
New York U. . N. Y.
796
153 936
713
155 565
New York U. Coll. of Ea0-
t03
155 081
neerl^ N.Y.
North American Aviatlaa, lot. .
706
154 570
692
155 r4
155 rs
Dowaay. CaUf.
North Carolina Sale Cod. .
740
159 148
1
Ralei^
778
153 679
669
153 844
Nordi Carolina U. . Chapil Hill
763
796
155 088
152 230
730
171 690
792
171 254
Nordi Carollia U. Scltnnl of
806
154 071
Medictae. Chapel Hill
Northeaaiarn U., Boaioa.
688
171 607
730
154 814
Maaa.
799
154 459
739
154 578
.
171686
776
154 453
793
171 688
756
154 721
Noyaa Chemical Lab. . U. at
757
154 719
171 665
llllnota. Urbane
701
ISO 133
763
171 687
Office of Defenae Reeearch and
768
171 664
Bi^neeruit. Waahli^laa. D. C. 740
155 149
771
154 815
772
154 816
Omca of Ordnance Reaearch.
795
155 386
Durham. N. C.
740
155 145
796
155 385
809
154 720
Office of Scientific Reaearch
and Devek)|iaieai. Dlv. 9.
713
154 875
694
154 210
Office of Technical Servloea.
739
153 647
Waahli«taa. O.C.
681
OTSS8 -442
153 730
744
OTSS8-448
7«
153 930
753
OTSS8-491
804
154 440
777
OlS 88-483
79? 154 232
Naval Radlolofical I
Lab. . San Frandaco. CaUf. 783 154 717
804
Ohio Stan U. Reaearch Fouada-
tloa, Cd'jmbua 701
800
OTSSS-454
OTSS8-499
154 19*
154 99*
155 333
Source
Par
PB Number
Source
Page
FB Number
OUa Maihleaon Chemical Corp.
Ne* Haven. Coon.
'70a
171255
Paycbometrlc Lab. . U. of
Nonfa Carolina. ChapL-IHIll
686
154 459
154 463
Onfloo Suie Coll. , Corvallla
703
148 079
PubUc Healdi Service,
Onka U. a*P*n)
776
154 453
Waahlngton, D. C.
692
121 784-R
161 371-11
f^ Communlcabooa Engi-
Mera. Uic., Waahlngton, D. C
.731
150 914
Purdue U. . Lafayette, Ind.
693
796
161 371-12
148 016
nana I It Chemlt^ali Corp. .
Wyndmoor, Pa.
694
697
153 163
147 841
RadUtlon Lab. , johna Hopkioa
U.. Baltimore. Md. 763
154 961
764
154 960
rieaMylvanU Stan U. ,
Ualveralty Park
697
702
796
154 564
148 932
171 598
Radio Corp. at America.
Somervllle, N. ].
732
154 479
ylvanli State U. Mineral
tries Experiment Station.
Udversity Park
lyhraala U. . Philadelphia
ftouylvanU U. School of
Medicine
Mko Corp. , PhlladelphU, Pa.
MUpa Laba.. Inc..
Irvlagton-oa-Hudaan. N.Y.
(hyilcal Reaearcb Lab. . Space
Tecfa. Laba.. Inc..
Loa Angelea, Calif.
Fhyalcal Reaearch Laba.
lU. "
fbyalca. Engineering and
Chemiatry Corp. . Boulder,
Goto.
PMaU. duly)
Plmaa-Duna Laba. Croup,
Prankford Arsenal,
fhiladelphu. Pa.
naamadyne Corp. . Sanu
Am. CaUf.
Plaatlca Lab. . Princeton, N.J.
Polytechnic Inat. . of Brooklyn,
N.Y.
Mytechnic Reaearch and
Dtvclopmeni Co. . lac. .
Brooklyn. N. Y.
ar Meullurgy Lab.
I Inai. of Tech..
Hobokra, Ne j.
707
687
668
782
746
731
754
755
800
683
780
781
748
697
804
702
772
789
796
731
732
777
154 562
148 219
171 606
153 862
155 414
171 566
155 239
155 240
155 241
155 242
154 154
150 916
171 600
150 338
153 924
153 581
159 345-1
171 563
171 567
148 473
153 848
148 757
171 569
154 956
154 957
155 259
154 537
PrtacetonU.. N. J.
702
763
772
148 747
148 748
149 214
154 582
154 583
155 080
Prapulalon Lab. . W
right Air
Dsvelopmeni Div. ,
V>
right-
Faaerson AFB. Ohio
756
155 083
785
155 257
Nfcteloglcal Lab.,
U,
of
Iaa*am California.
^oa
Aaplaa
686
148 005
RadloMologlcal Lab. , U, at
Texaa, Auailn
Ramo-Wooldrldge Dlv. ,
Canoga Park. Calif.
Raytheon Co. . Waltham,
RCA Service Co. . Camden.
N.J.
REP M^. Corp. . Mlneola.
N. Y.
Reneaelaer Polytechnic Inet. .
Troy. N. Y.
666
(86
693
790
797
732
740
775
Reaearch Lab. of Electronlca,
Maaa. Inat. at Tech..
Cambrld(e 733
Reaearch Labs, (or the Engi-
neering Sciences. U. of
VlrglBla. Charlotteaville
RIAS. Uic.. Bcltlmore. Md.
RocheaierU.. N. Y.
7«7
773
777
693
702
Rock Uland Araenal Lab. , III. 756
Rockeidyne, Canogs Park.
Calif.
Royal Hoaplial for Sick
Children. Edinburgh (Scot . )
Rutgers Sute U. . New
Bninawlck. N. j.
Rutgers Sute U. School of
Chinnlatry. New Brunawick.
N. J.
Sanu Barbara Dlv. . Curtlaa-
Wright Corp. , CaUf.
School at Aviation Medicine.
Brooke AFB. Tex.
736
740
741
690
764
703
711
669
690
693
694
Small Groi^ia Reaearch Ceniec
Waahlog^on U.. St. Louia.
Mo. 666
Southweat Reaearch Inat. ,
San Antonio. Tex.
752
Space Sclencea Lab. . General
Electric Co. , Riiladelphu.
P». 773
M
155 575
154 594
155 576
154 460
154 077
155 151
155 152
171 60S
149 210
150 913
154 19S
154 199
153 906
^54 158
154 536
153 903
154 374
155 082
1 S3 870
154 290-1
154 290-2
153 720
148 561
148 400
153 859
155 486
154 263
154 427
155 S74
154 992
195 576
154 264
149 904
153 703
153 692
153 693
Source
Pag^ fBWianber
Space Scienoea Lab. , General
Eleclrlc Co. , Ruladelphia.
Pa. (coo.) 804
Space Technology Laba. Inc.
Loa Angelea, Calif.
Sundard Preaaed Steel Co.
Jenkiatown. Pa.
Sunford Electronlca Laba.
SunfordU.. Calif.
Sunford Reaearch Inat.
Menio Park. Calif.
SunfordU.. CaUf.
Sunford U. School at
Medicine. CaUf.
Stanley -Thocnpeon Laba.,
Columbia U. . New York
Stockhobn U. (Sweden)
Stoddart Aircraft Radio Co.
be., Hollywood. CaUf.
Systems Development, Inc. ,
Binghamton, N. Y.
Tecbnlache Hochschule,
Karlsruhe (Weal Germany)
Techniache Hochachule,
Vienna (Auatria)
Temple U.. rhiladelphu. Pa.
Texaa A. andM. Research
Foundation, College Suuon
Texas U. Medical Branch,
Galveeton
Ultraaonlca Lab., Michigan
Sate U. , Eaat Lanalng
Unlveratty of Southern Califor-
nia, Loa Angelea
U. (Auatrta)
736
7*7
800
733
734
767
800
806
708
767
789
762
797
786
797
734
Synthetic Mica Co. , Caldwell,
N. J. 798
735
697
697
787
707
691
792
703
708
Virpnia Agriculture Experlmeni
Sution, Bladsburg 764
VirglBia U. , Ourkxtesville 686
703
Vitro Ei^neerU^ 0>. .
Waahli^ton, D. C. 741
Waahlngton U. . St. Louia.
Mo. 687
WaahinponU.. St. Louia, Mo.
School of Medicine 687
691
154 510
171 347
171348
171 349
171 3S0
154 333
154 371
154 373
712 155 086
148 332
149 235
148 398
149 236
155 360
153 785
154 371
150
^
154 556
148 231
154 078
147 847
190 053
689 155 297
190 864
153 731
154 413-1
154 412-2
155 154
159 155
159 196
155 1S7
150 903
153 717
154 157
154 161
154 528
148 415
153 120
148 075
148 076
148 077
154 199
148 535
147 530
150 535
153 890
149 334
154 993
149 336
u..
WaierUOTn Araenal L te.
WaBnrllM Aracnal. I I. Y,
P«ai WNanber
R^i nNunbtr
MS
7C4
741
742
757
777
710
74J
749
777
IM 118
148 233
1S5 099
1S5 061
1SS062
1»0U
1^5 060
155 572
171 384
153 558
154 207
171 112
171 564
Wayne State U. ,
Mich.
OMTOtt.
Weather Bureau,
Waahington, D.C.
Weiznaon Inat. c< Sci«ac«
(Urael)
Weai Virginia U. ,
Margaaraon
703
704
764
793
707
148 406
148 407
154 456
171 580
149 096
149 097
153 715
704 149 775
704 153 662
Source
WeatlaifKaiae Electric Corp.
Youngwood, Pa.
Weaioa Inairumeata,
N.J.
Whltiaker Coetrola, La*
AnfBlea, Calif.
Willoii Run Laba., U. of
Miciiigan. Ann Arbor
Wtlaoa, Nuttall. Raunood
Eaglaiecra, tac.
Zator Co. .
Cambridge. Maaa.
*i»
n Number
735
155 321
735
155 384
712
153 611
787
I5S382
750
1S3 713
soe
155 061
^^■
(r 5i»^,^» . '<f ■
1-6
AMauon ntiatertala
Accelerauon
-Matheniatical analyata
- -Meaauremeni
Acceteratlon tolerance
--TesHag equipment
Aceuli
-DKompoaltlan
Acetooe.
-Detenninatioa
Acetyl bramide
■Microvive apectra
Acoaatlc iinpedance
--Meaaurement
AcoBtic propertlea
Taat iiiadMXla
Acrylatea
-Sywheaia
Adayttve awiiching circuit
Aerial cameraa
•-Afpllcationa
Aerial pbotographa
■-AnalyaM
■-froceaaing
Aerial photography
- - Applicatiooa
Aerial targeta
--Drag
Aerodynamic heating
- ' Couaierineaaurea
--Theory
anuca
--Mathematical aiulyaia
-Siady and teaching
Air
-MbUography
--mrificaticn
■-RaMoaaivlty
Air caadltioning equipment
(Airborne)
--Dbatpi
Air haake filtera
-Ttat reault*
Aircraft
- -De (action
--Heat tranai^r
--Landing
--Maintenance
-MaicrUla
--CaaArlch coaatmctkia
--Sircaaaa
-VtatMlity
Aircraft cabina
-Coolii^
Aircraft a^ipment
--Blkcta o( radiation
AlrcBaft finiahea
--BIbctiveneaa
AUMla
-Ull
-■Madwmatical analyaia
Aiiframea
-MaicrtaU
Airpliae landinga
--Meteorological factora
Aiiytaae panels
--Vlferatian
AltrlhaUdea
— Soand tranamlaaion
Akyl radical*
-Ckamical reacdoM
-ror^ag
•-Heat rranafer
alhjrgical
-CrfMal atructara
■ion
'Mmi traatmeot
Faa»
757
710
726
710
748
700
694
791
687
787
695
806
806
707
683
752
707
709
711
773
769
740
800
771
774
736
744
«92
693
735
744
710
752
769
709
709
779
710
708
752
735
709
732
710
773
779
780
709
711
791
697
776
801
776
739
795
7H
WWtartier
154 719
153 695
155 567
153 695
153 694
153 911
154 210
148 563
140 219
155 382
150 730
150 227
ISO 227
153 915
150 916
155 438
153 815
153 861
153 658
153 693
154 215-1
154 215-2
155 296
155 323
149 778
OTSSS-448
154 626
OTSSa-448
161 371-11
161 371-12
171 257
154 674
154 744
153 900
154 215-1
154 215-2
161 914
161 915
171 614
151 104
154 955
155 090
153 900
171 257
154 535
153 900
135 146
153 692
153 752
153 750
153 751
154 743
171 594
153 082
154 564
161 236
154 868
154 453
148 H6
171 666
148 516
154 936
SUBJECT INDEX
Subject
Aluminum alloya
--Corroaion
'--Extrualoa
Aluminum-carboo-iron alloya
anical propertiea
I caatinga
--Mechanical properties
Aluminum oxidea
- -Magemic properties
Amiaea
--Chemical reactiona
--Toxic effecta
AmphUMoua operations
-B^iipmeot
Ptge PB Number
Amplitude modulation
- -Meaaurement
AN/APD-4
AN/FPS-3
AN/QPX
AN/GPX-20
ana;iic-27
ANA5SQ-16(XW-1)
ANAnUl«-37
Analytic functiona
Anchora
--Teat reaults
Anechoic chambera
- -Acouatic propertiea
Anonhoatte
Antenna tnaais
- -Oevelofiineni
Antennn radiatioo patterna
- -Aaalyala
aia
-Cootrol syatema
-Oeol|^
-^tovelopmenf
781
7*9
778
777
795
697
691
714
717
745
746
727
764
732
732
732
732
765
766
729
7«0
746
787
753
729
725
726
719
720
725
718
789
795
Antilerromagneilam
Antiorgan aerum
- -Biochemical effecu 691
Applied mathemaUca
--Theory 761
Approach Ughta
-Viaibillty 709
Apprasimaae compuution 761
ApUtuda tests
--Scadatical analyata 686
Aquatic aaimala
- -Biochemiatry 703
Arresting hook 709
Artificial denturea
-Analyals 690
Aniflclal lightning wavelorjn 804
Artlfir'al limbs
- -CoMTol syatema 682
Astla deacriptors 807
Atmosphere
layer 707
■I aoalyaia 708
: properties MS
708
792
706
688
706
787
706
804
- -Haat traaater
- - Ufi* traoamlaalon
-Motion
- -AyaMogical affects
--Tanparature factors
- Turbulence
AuiAiaphi re mn^la
Aiaaoapheric electricity
Atomic bomb exptoMoaa
- -Rtyaical efiects
Atomic clocka
Atomic po»er plants
- -Arctic regiona
4(oatB apanii
708
789
7>3
153 581
171 568-1
171 568-2
153 673
171 564
154 062
154 157
153 845
154 614
154 633
154 616
154 649
154 589
150 909
155 151
155 152
155 151
155 152
155 151
155 152
150 086-1
150 086-2
150 086-3
150 086-4
ISO 086-5
1S0 086'«
154 660
148 212
154 662
155 382
154 636
154 681
153 864
154 595
154 596
154 071
153 594
153 719
153 864
ISO 901
154 078
154 062
148 415
150 994
154 743
147 904
148 005
148 079
161 915
154 263
154 273
149 444
171 519
154 562
154 155
161 589
154 556
156 530
154 275
171 600
154 275
153 906
154 275
154 273
1SS090
153 716
150 908
154 071
Sid>|ea
Atomic structure
Attenualiaa
- -Measurement
Attitudes
--Meaaurement
- -Psychological factora
Audit
Auditory perception
--Sutistical analyaia
Auatei.ite
- - Deforma tion
Autofrettage
Automata
Automation 4
Aviatloa accidaaH
- -Countermeaaurea -
Aviation personnel
-Teat medxxls
Axially symmetric flov
--Madiemaacal analyaia
Azidaa
- -Chemical reactloaa
-Syalheata
Azo compounda
-SyMtieaia
B-70
Bacteria
- rkyaioiogy
Balaacea
-Dealgn
Balllatica
Bartaiaing
Barium oxides
-Magnetic properties
693
787
683
686
748
684
780
742
806
80S
710
688
769
772
695
697
695
697
711
687
694
740
807
754
755
755
Barium tiunate cryaula
- -Dielectric properties 795
Batteriea
--Comainera 730
Deaign 772
Beaches
-Geology 704
-Stabill^tion 713
Beama
- Dirformatioo 797
- -Streasea 753
Bebnke teat 689
Beiuoic acida
- - Thermodynamic propertiea 696
Beryllium
. Handboolts ' 779
-Mechanical propertiea 712
iibllography
-Air 744
- -Air pollution 744
--Armed Services Technical
lnfc>rmation Agency,
ArUagioB, Vm. 681
-China 681
-Electric baneriaa 731
--Fluorine compo—da
<OH>mk) ^ 756
- -Povaat Pradactv Lab. ,
Madlaoa. Wia. 710
- - Heat reaiataat alloya 777
--High temperature meal-
lurgy 777
- High temperature research 8M
--Low temperature raaearcA 753
802
--Matariata 7S2
--Meullurgy 777
-Nitroan fluorldba 756
- - Poarer auppliea 681
--Sandwich conatruction 710
- - Sedimeautloa 704
-Trailers 752
Biological warfare
• -Safcty measurea 743
Biological warfare sgi aiii
- -Countermeaaurea 742
744
mantca 7t»
f» Number
153 903
155 382
148 774
149 904
154 499
148 787
154 063
154 553
154 207
150 726
152 135
153 805
154 744
171600
155 144
153 848
148 938
147 841
148 937
154 157
171 599
148 966
1S316S
155 296
152 114
155 240
155 241
155 242
150 915
154 639
171 562
149 216
154 632
150 068
154 600
19S4M
154 466
151 106
155 06(
aTCSB-448
OTS 56-448
171 689
CnSSB-442
OlS SB-447
171 252
154 995
aTSS»-4S2
OTS 91-452
OTSSI-453
OTSSB-451
171 630
171612
OTS SB-452
OT5SS-454
171 2S2
171 <a9
154 955
149 216
153 703
154 627
154 622
154 674
171231
1-7
•trafrtofmce
Kl— fnin c«atln|
--OMertoratkia
--MMMlals
-BIlKta at radtaita
701
7tl
7M
vn
711
I ct mrotutioa
- -Hydradyaamic ctefactar-
laUcs
--tlrperkoalc diancterlaclca
--Pr— ur» dunibuqoo
Body temperature
--CUmatic tacnra
-Coacroi
Bolu
--Screaaea
-Radtafrapiilc aaal; aia
-Prxjpartiea
Boroa cartMdea
-Appiicaiioaa
--Onaliy
Boroa coavounda
■-Moiacular acr
--SoivaM |>iupartl«a
(Ortanic)
Botadary layar ooacrc I
--Partamausa
Brala
- Etactrtcal profier^
■raxlag
-MMartaU
Bromine
ntoiolyaii
BuHdoaiac reautaocc
Buraa
-Thara^
Cabiaa
-•Equipmeai
Calcian
- -Mctallurgtcat (
Cama
--Oaal«B
CarMdea
--Matalkirflcal aOrina
- -Ckaoiical reactlo4a
Carboa duaude
--Hwat atudlea
-apacuographic ai^lyala
CaavBvaMclaa
"CoMroi ajMMdia
lUiy
Oarrtar rockai
Caai aval
--Mackaaical propafiiea
Caalyata
--Appllcatlona I
Caramarana
1 laai raauitt
ivacer
CariHda ray wka aciiaaa
774
711
7W
712
7«3
7t2
7M
AM
m
-AppUcatloaa
Cadxidea <Elcctraa I
--Matariala
CavMaUoa
--Thaory
CallB #toiecy)
--BlKsrtcal
Cellutoaa
--Ckemlcal
W5
700
Ml
701
7S4
711
6M
776
«99
751
MO
702
W7
751
777
73B
77t
701
70B
791
7S0
730
730
7SB
737
777
735
745
742
727
745
719
723
774
M7
«91
171 610
154 511
154 641
154 167
171 60S
153 6S«
153 919
153 6S«
155 144
171 M*
155 297
155 086
154 SM
155 429
155 429
155 428
153 784
155 154
155 155
155 156
155 157
148 937
154 709
153 843
154 959
152 9S0
148 MS
150 338
151 108
149 085
152 009
153 720
154 374
154 564
154 668
171 384
153 866
153 673
154 959
154 155
148 935
153 713
152 006
152 004
171 330
153 731
171 384
154 725
153 706
154 642
155 320
154 640
153 907
154 450
154 871
148 219
148 415
171 574
Caatrtfugal punpa
[■aaa PBNianber
Paia WNun^at
CaacrUufaa
- -Equipment
• -Jolata
Caranuc capacitora
- -Davelofitneiit
Ceramic caaunfa
--Tem|ieratura bciora
Caraaaic raaicrtaU
--Dlatectrlc propertiea
- -Magnanc propertiea
,aranirc factora
Cerabrai cortex
- -Bxcltatlon
CealuD
- ' lool^acion
Cealum loaa
•-Motloaa
Chemical elamenia
- -Maallurglcal cffecia
Chemical a<)ullil>rium
-MeaauTemeiit
-Theory
Chemical iaader
Chemical milllnf
Chemical react loaa
--Aaalyala
--Temperature factors
Ot"-"''--' warfare apaau
aaurea
-ToKlc eflecia
Chemlacry
CheraMrd thermota lance
China
- •iMtosraphy
Chloral amidea
- -Decoetamlnatlnf effecta
Chloriae iafueer
Chioropreaea
- -Flqiatcal propertiea
Chraalum ioaa
--Chealcal raacUona
- -Propertiea
Chromium oacidaa
- -Magnetic propertiea
Clrcuiamry ayatema
- -Dietary factors
Claaaiflcation problem
Claya
--Mechanical propertiea
Climate
--Greenland
Cloeed loop control
Claude
--Abaorptlve propertiea
Cobalt borides
- -Mapiatic propertiee
Cabell compounda
--Moiacular structure
Coila
- -Appllcaiiane
--Oavetapmem
Colloida
-- Coagulation
--Optical efiecta
- -ScabtUxation
ComMaatorlal aaalyaia
Combuation
-AiHlyaia
- - nncographic aaalyaia
Communication theory
Compact charge loni^tlon
Complex Gompouada
--Decompoeltion
--Propartiea
-SoMUty
l-B
747
710
748
724
771
795
754
755
754
«S7
720
790
794
701
767
699
712
749
700
701
712
713
742
691
M3
694
Complex loaa
- -AMlyaU
713
712
757
758
703
701
795
688
763
751
707
733
681
789
703
717
783
787
703
793
703
704
786
699
767
801
807
720
695
794
694
702
703
70«
70S
154 6SS
153 695
153 694
153 723
154 815
130 915
155 239
155 240
155 241
155 242
171 593
154 5#3
149 847
154 460
148 781
130 133
153 930
171 575
154 615
171 112
154 709
154 959
154 679
154 875
154 622
153 841
153 843
154 438
153 903
153 163
681 (nSSB-442
154 875
154 615
130 844
150 845
148 076
150 133
154 062
154 168
154 349
152 005
153 715
130 913
153 718
154 364
148 075
154 700
154 863
154 864
148 406
149 096
149 097
148 406
148 407
148 974
153 619
171 155
153 930
154 4S8
148 302
149 847
148 938
130 642
153 163
148 932
148 075
153 662
148 075
Compiax iooaCcoa.)
-Analysis (coo.)
--Stability
Complex variablee
Comprcasible flow
- -Thermodynamics
propertiea
Compraaaioa shock
--Raductton
Compuaars
-Deaign
Concrete
--AppUcailona
-Mater la la
- -Streaaes
Conical bodiea
--Aerodynamic character-
iatlca
--Hyperaonic character -
latlca
Conaactora (Electric)
-Deaign
Construction
-Equipmenu
Coaiaiaera
--Deaign
Contlnuoua media
Cooirol aurfacsa
-Materia la
Coatroi ayatema
--Equipment
--Mattaemailcal aaalyaia
--^rformance
- -Siabillcauon
--Statistical aaalyaia
Convection
--Northern hemlaphere
Conveyors
-Equipment
Cool electrons
Copper
--Chemical reacttona
Coroaa (Electricity)
- -Electromagnetic eflecu
Correlation functiona
--Determination
-Theory
Corroaion inhibtiurs
- -Applicaaoaa
--Teat reaulta
Corroaion reaisiaai alloya
-Teat results
Coamic radution
--Analyaia
Couette flow
Craoaon
--Chemical aaalyaia
Croeaed field davicea
Ci yuganlca
Cryoaar memory
Crysul rectifiers
--Development
Cryaul structure
--Mathematical analyaia
Cryaula
- -Croadi
Cyaao radicala
-Chemical raactioae
Cyberaatica
703
703
760
800
744
758
753
753
770
772
719
715
716
730
749
768
773
737
723
720
728
734
803
751
731
704
789
763
761
781
781
781
782
773
758
722
739
794
801
802
767
735
7U
798
703
765
806
Cyclic compounda
- -Chemical reactxMia
- Molecular structure
Cylladara
--Aerodynamic character -
latica
--Haat tranafcr
- Hydrodynaroic character
lanca 775
- -Streaaes 768
- -Turbulent boundary layer 772
Cyuchanlatry 891
697
790
770
801
148 076
148 077
148 212
154 208
155 253
154 462
154 650
154 636
154 630
171 «0«
154 583
150 849
154 669
154 673
154 683
154 639
171 568-1
171 548-2
154 120
- 153 693
155 251
ISO 101
149 137
154 804
149 236
154 449
154 638
154 523
153 66]
154 071
155 087
154 088
154 612
154 611
153 581
154 70«
154 138
154 661
154 301
154 502
154 289-)
150 642
171 618
171 619
171 620
153 905
155 321
154 103
155 154
155 155
155 136
155 157
148 075
171 238
150 227
154 157
153 6SS
171 604
148 348
149 210
171 684
154 81*
1«41S
JMtject
OMtag
— nactiveoea
DM
--Prooaaalog
Page PB Number
I card medioda
systems
■OMelopmeat
DMi traaamiaaion systems
■-Codlag
• Error
Omd spsoe
Oacalerstlaa
- Ikyelologlcal eflecia
ObOBBpreea ion
• BlAnlnglcal effecta
Dawiaiiilnstioa equipment
-•Daaakpment
- -BflKtiveoeaa
7U
718
765
766
808
808
765
766
I of radtauoo
Daaial surgery
DMargnta
- Optical properties
DMcaatlon waves
•■Maibaiiiatlcal analysis
"Propagation
•-Theory
Olsaal aagines
-CaoUi«
OUkraaHal aquaOona
- Theory
DMaaioa
-Theory
Digital recording eyscems
- -AppUcsuons
-■AfptI est lone
- Teat resulta
OMpiay ayatema
■Pavel i|MHl
I eaglaaering
Ikaft ladlcatora
-Tat resulta
Drape
-Caabuation
Olasd bodiea
' Preasurc dtstributicn
bopoiy situatioa
OlBiald
BA-1814
Bat*
Praaaare
:conditlaaa
Mlity
Bhstlc shells
-Hast trsnafcr
Elastic iry
' -Wsdieinsucal aaalyaia
- -Ihvalopaeni
Blacirtc taatterlea
-■MMtagrapby
• Blilliiiaium
UKtric cablea
■-Cbrroaion
807
733
807
688
711
690
712
743
743
715
693
690
739
801
803
716
763
764
775
724
739
718
>S1
795
682
684
765
766
807
745
747
769
684
757
691
714
807
801
768
757
731
699
729
171 S94
171 609
150 096-1
155 376
150 086-2
130 086-3
130 086-4
150 086-5
ISO 0B6-6
155 068
155 068
150 086 1
150 086 2
130 086-3
130 086-4
ISO 086-5
150 086-6
147 787
149 235
148 502
171 607
171 599
155 574
154 615
154 677
154 675
154 669
155 576
154 437
149 895
154 578
154 458
154 534
154 883
154 961
154 960
152 117
150 900
153 647
155 258
171 566
171 573
154 303
154 063
154 064
150 086-1
130 086 2
150 086 3
130 086-4
150 086-5
130 086-6
171 519
154 664
154 454
155 144
149 521
155 572
153 841
154 623
147 842
147 843
148 348
148 813
171 684
171 578
171 579
crresB-447
171 155
154 624
Ssbta« fbe
Electric currenu
--Applications 788
- Eleciricsl eftacu 722
- Meaaurement 788
Electric detonatora
-Maiertala 738
Electric diacfaarfea
- -Magnetic (actors 788
Electric fields
- Mathematical analyaia 727
- SutlaUcal analyaia 799
Electric moiora
--Control systems 724
Electric motors (D. C. )
-Control systems 737
Electric poieniisl
- Meaaurement 700
-Theory 786
788
Electric propulaloa 731
- Devetopmeoi 748
Electric aervomechaniama
' Development 730
Electric wire
--PuBguaproa(ii« 728
--laaulstioo 730
Electricsl double layer
-Theory 700
Sublact
-Thermodynamic propertiea 698
Electrical e<|uipment
- -Arctic regiooa
-Deaign
-Salvage
Electrical oeiwortca
- -Aaalyaia
■ tlcal aaalyaia
--Theory
E lectrochemiairy
Electrodea
- -Electrical properties
E lectroencephs lography
ApplicsDons
Electrolyiea
--Apptlcattons
--Physical efiecta
Electroraapaetic flelda
- Mathematical analyaia
Electromagnetic theory
Electromagnetic wavea
- -Meaaurement
--Propagation
Electroa baama
- -Acouatic properties
- Aaalyaia
- Mathematical analysis
■-Propagation
Electron gsa
- Energy
Electron tubes
- Cooling
--Development
- -Military requlrementa
Ek-ctroolc circulu
- Mathematical analyaia
- Synthesis
Electroalc equipment
-Coding
--Devalopmem
-ReltaMllty
-■Salva«e
Electronic acanners
■ -AppUcailona
- -Control ayatema
Electronica
Electroae
-Daneiiy
- -Scattering
E lectrophoreaia
- - laatrbmentatton
730
721
713
721
786
724
728
728
699
722
731
700
688
687
703
703
760
800
789
792
804
734
722
723
789
799
721
733
727
723
733
733
734
733
713
730
734
733
733
799
784
799
701
155 573
155 618
154 102
153 022
154 080
ISO 902
149 911
150 792
155 251
ISO 967
130 864
148 958
OTSSB-447
155 345-1
155 147
154 487
154 656
150 967
154 872
154 873
154 874
154 656
155 577
171 479
155 577
148 974
153 704
153 705
ISO 906
155 160
171 155
171 582
OTSSi-477
150 967
130 338
154 593
148 406
148 400
14B213
155 323
148 757
171 354
1S4 373
154 448
148 398
154 SOI
154 503
148 323
150 414
153 180
154 523 .
148 332
155 330
154 213
149 235
130 910
150 911
1«0M
159 151
1SS153
171479
190 913
190 900
190 913
154 198
154 199
153 S84
154 372
ISO 171
152 180
154 659
EadnreaaaaM
Ensymae
- -Effecta of radiation 691
Epinephrine
- Determination 694
Epoxides
- - niys iologics I effects 691
--Thermal propertlaa 756
Equations of state
-ApplicaUona 799
Errors
--Detection 764
Eaters
■Propertiea 756
Eihaaolaminea
--Chemical reacttona 704
Evaporators
--Corroaion prevention 713
Exploding wire 738
Explosive chargea
-Detonation 738
Exploaives
■ -Chromatographic analyaia 694
--Detooatian 799
Page reNumber
730
- -Thermal propertiea
Expoaure
--Biochemical effecta
Extrualon proceaa
Pacalmllc recordli^ ayaieiiM
■Deal^
Factor analyaia
-Applicartaae
Paradaic rectlfteaOoa
Perrtiea
- -Magnetic propertlaa
Ferroelectric cryaula
--Temperature factora
Ferroelectric materials
■ ■Dielectric properties
Perrxxnsgnetic films
--Mapietic propertiea
Ferromagnetic materiala
--Magnetic propertiea
Perromagnetism
- -Mathematical analyaia
Fibrin
- niysiologlcal effiecu
Field Ion microscopy
Ptfdi wheel
FUlera
Film raadera
-Deaign
. Fire control compumra
- - Equipment
Fire extlnguiahera
-■Corroaion prevention
FIrea
■ ■Couniermeaaurea
Flame velocitiea
--Measurement
Plight simulators
--Appticationa
Floating crane
Floating docka
■ -Corroaion preveodoa
--Equipment
Floats
-■DevelopmeiK
-■E^iulpment
738
6U
749
724
686
686
700
795
796
795
797
!r96
789
789
-■Launching
■■Test reaulta
Floora
■-Arctic raglana
-■Maioienanoe
Fluid flow
■ -Magnetic factora
--Mathematical analyaia
-StaMUty
--Turbulence
Fluid machanica
690
796
7S0
757
764
738
781
7-2
700
710
746
t45
745
714
717
745
746
716
714
717
798
773
772
773
774
775
771
775
772
774
775
153 719
171608
154 264
149 396
154 721
153 790
150 90*
155 082
153 662
155 565
153 022
152 022
154 210
153 730
154 578
171 686
171 256
171606
171 5681
171 5M-2
150 900
154 459
148 OOS
150 967
155 386
155 385
150 915
154 077
171 569
148 7S7
154 964
788 154 109
154 427
171 598
171 619
171 579
150 909
153 866
154 611
155 290
150 031
154 744
154 660
154 640
154 664
154 614
154 633
154 616
154 649
154 660
154 682
154 672
154 700
171390
153 693
154 582
154 862
148 994
154 871
148 951
149 310
148 317
153 117
153 848
150 634
152 117
1-9
S>*fa
Fluids
■ -Temperature f«ct
PlHoreibylene potym^r*
-Heat transfer
Flttonoc conpouodB ^gaiuc)
- -hbltograpiiy
■ -Cheinlcsl properties
Fluorocarbona
-Synilwsis
FUnroediyleoes
- -Spectra
Flyioc plaiforiiM
--Tmi results
FlywtweU
- -Appilca liana
Food
- -Effects o< radtats^
-■Haatiin
PoraMidaivde
--AppUcatkna
--Decanuminauiig ^fbcta
--Toiuc effects
Prac jet implngemen
Frac radicals
- -Effacta ol radut^n
Freijufairy
--Control
Frequency modulatla i
- ' Applications
From ends
Fuel cells
Fual fillers
-Teat meilKida
Fuel lajeclion
niyatcal
FikU
- • Toxic eflecta
Fuactlaaa
-AppUcatooa
-TaMn
--Tteocy
Puagua eater
Camea theory
- AppUcjiijns
Canuna functioaa
-Tables
Gamma radiatioa
-Altaauatioa
- -Scanering
Caraets
--Cryaiai siructurt
Caa dMfusioa
- -Tni^ieraturc Tacfors
Gas tkm
--Daaaiiy
- -Electroaiacnetic
- -llaiWiHril analysis
Gas loaizatkxi
-Aaaljrsia
Majaiitlr factors
- -Measurement ,
Gss»oua rocket prof cllaMS
Isciors
Abaorptive prop irties
-Acoustic propert es
-Ckranangraphk analyaaa
- Molecular atruci ore
--fkyslcal factors
•-Sound transmissllDn
- -Specific teat
- -SpectrafrapMc a^lyais
Caafeeis
-Maieriala
Oeodaaics
- Afpttcattona
cure
GoUvirc
- -Applications
G— rtnln (Aero
- -AppUcatiooB
Gratna (MeulkuVt
<a)
GraiMw
-Afirilati.
aoi
757
756
69o
w%
M6
WD
711
737
746
746
740
743
743
742
711
7S1
7*9
730
725
M9
731
756
756
691
760
762
763
764
762
6S6
782
785
788
763
785
785
795
,796
699
773
800
773
T99
799
786
747
804
787
•94
742
739
8*1
703
70*
791
SOU
803
7S1
73*
71*
7»
710
7tl
773
nhuaber
171 618
155 572
171 252
155 453
154 118
154 251
154 262
153 859
155 251
155 414
155 566
171 60S
154 655
154 657
154 642
153 642
171 596
153 716
154 814
150 847
171 155
OR SB 447
155 256
155 2S6
153 845
154 098
152 957
154 961
154 960
154 452
154 462
155 324
155 257
154 103
171 687
153 908
155 257
155 386
155 385
154 538
154 158
155 323
153 692
153 584
149 911
149 540
155149
147 840
150 198
154 210
155 230
153 730
154 458
ISO 535
154 309
153 082
154 208
154 720
171 «M
171 248
1S4 647
153 033
153 895
150 006
153 693
Swblect
Graphite (coo. )
- - Impregnatlaa
Gravimetric analysia
--Instrumentation
Grossjean's method
Ground impact
Crcav dynamics
- -Psyclx>Io(ical (actors
- -Sociolo|tcal (actors
--Theory
Gun barrels
--Prooeaalng
--Teal meihcda
Gyro stabilizers
- -IVrforiiiance
HaiK] generators
- -Design
Hard top
Hardneas
-Measurement
Harvard test
Heart
--Psikology
Heal eachangers
Page fB Number
Heat I
Heat resisunt alloys
- Btbliograpby
-Brszing
--Coadnfa
- -Development
Hesi resisiani alloys
--De%clcFTT>ent
- -Machining
Heat resistant polymers
-Applications
Heat sink
Heat tranafer
- -MaAematical analyaia
- Meaauremeni
-Velocity
Heaiera
- -Operation
Helicopters
- -Control systema
Helium
- -Hsndling
HelmiMiiz colls
Hickory
High frequency commonicstK
systems
- Equipment
High pressure research
--BtbUography
- - Instrumentation
Hubert space
Hoists
Test resulu
Homotopy theory
Hot shot tunnel
Human engiaeeriag
- HanSnoks
Humidity
Control systems
Hydrsted ions
Hydraulic power systema
- -D^velapmaat
Hydraulic servomectMniaa
Development
Hyitoaziiis
Determlnaiioa
Hyihrides
'Api^icstlaae
Hydrocarb
- -Molecular structure
Nydraelaailciry
Hydrogen
- -GandraaatKMi
- -Hyperflita siriKture
--Molecular structirc
753
694
783
711
687
685
686
685
686
742
741
742
737
726
714
780
689
690
736
802
777
T76
754
775
775
749
753
771
802
726
803
735
711
740
741
783
758
721
806
770
7*7
804
804
787
760
709
764
7*9
«82
713
701
735
710
755
782
»«?
790
745
791
790
790
Hyikogra peroxide
- -Caiemcal reaciuva
153 914
153 163
153 891
171 599
149 324
147 902
149 904
147 903
147 530
154 207
155 059
155 061
155 062
155 CSS
155 060
155 252
150 846
154 619
153 924
155 486
171 602
154 626
171 559
OTSSa-452
151 108
171 617
171 597
171 597
171 112
171 565
154 815
ISO 243
155 567
155 081
154 725
153 851
154 290-1
154 290 2
154 863
154 281
155 025
154 865
154 572
153 721
171 567
anS8-4S3
154 161
154 098
171 614
154 456
153 553
154 522
154 638
154 6S9
150 903
155 147
154 716
155 431
153 717
153 635
148 745
154 457
153 Ul
153 839
T78
TOO isoaai
150 780
171 JSS
Subject
Hyperflnr structure
- Determinsiion
Hypersonic flow
-■Boundsry layer
- Laminar boundsry Isyer
-Mstbema Ileal analyaia
- -Measurement
-Theory
Hypersonic wind tunnels
-Equipment
Hyperveloctty guns
- -Aerodynamics character-
istics
Equipment
Hypervelocity projectiles
-Ionizing effects
Hypervelocity vehicles
- -Control surfsces
Hypothermia
- - Pathological effecta
Hysteresis
- -Temperature (actors
Ignition systems
-Interference
Impact shock
-Physiological effecu
Indexes
- Handbooks
Indium antimonides
--Electrical properties
Indoles
- - Applicstioos
Industrial production
- Control systenw
--Quality control
- -Scheduling
Inertial guidance systema
Information theory
Infrared detectors
-Matenals
Infrsred Ismpa
- Design
Infrsred spectra
- -Analysia
- - Measurement
Infrsred wsves
--Attenustion
Insulation
- -Heat tranafer
Inagral equationa
-Applicationa
Integral functiona
Integral tranaforma
Intelligence tesu
- Development
Intermetallic compounds
-Properties
Inventions
- Classificstion
Inverter circuits
- -Magnetic edacta
loo beams
--Oacillation
loooaphere
--ReftecTlve eflecta
loaa
-Chemical properties
- Chemical reactions
- Oscillaiiun
- -Physiological efiects
- -Sources
Iroa
— Internal frictioa
Iron biandrs
- -Mayiatlc propertlea
Iroa crystals
- -Microatructure
Iron-aidtel alloys
--Magnetic properties
Iron oxides
--Ma^atlc propertlea
Iron phoaphides
- Maprtic propertiaa
Wag laRlce
Pape PB Number
790 153 828
711
804
772
737
769
770
7J7
737
727
773
690
701
748
711
807
796
694
748
748
749
737
684
808
793
792
696
792
694
792
802
760
763
774
763
774
760
761
686
793
807
724
790
731
784
699
800
688
710
776
789
796
796
754
755
789
788
153 658
154 SIO
154 583
153 846
153 55J
149 328
769 153 553
153 641
153 846
154 589
153 693
171 6QZ
150 133
154 637
171 599
171 519
148 016
154 264
148 787
148 095
149 088
154 869
155 252
154 064
155 0«8
153 923
153 467
154 262
149 567
171 254
153 036
155 437
150 243
154 098
171 687
ISO 624
153 486
154 871
153 211
150 994
148 005
153 923
149 523
150 792
154 440
150 914
171 572
149 085
154 371
171 too
149 847
154 453
154)64
171588
171589
155 239
155 240
155 241
laut
154 364
154 103
1-80
Sablect
Jet sagine fuela
- -Fbysical propertlas
Jatcaginea *
--Teat reaulu
Jai aiaiog flow
--T^irlMlence
jMpmpa
— Ibaory
)M
--Acoustic osdllatlan
--Theory
)o6aaalysM
--Appllcstiooa
I distribution
Laborstory animals
Lactic acid
--Effects of radiation
Laminar boundary layer
--Heat tranafer
--Madwmatiai analysis
- Ifcyalcal properties
"lliannal propertlea
laaillnrm maps
-That results
Ltadlaggear
--Teat reaulta
■Codli«
LCAO treatmeoi
--Corrosion
Laad-magnesium alloys
- Properties
Laadarahlp
--BOacti*
--hycbologlcal factors
-Sociological factora
Laarning
"Matfaemailcal analysis
o
--Ikfsloiagical factors
••Nycfcaloglcal (actors
- Theory
Least squarea
-Applicadoos
-DUtractlcn
■ Msssurement
--Inflection
--Scanering
U#)iaing
--Electrical eflecta
Umli theorem
• Theory
Uquid rocket propellanu
- Teal results
-Ananizatioa
-Wave transmissioo
LidUum chloride
■•Corrosive eflecta
Uytr
--Bazymes
- IkfBlokigy
L^ Impersture slloys
-IVnalle propertlea
Low •mpersture resesrch
--■iMiogrsphy
--■lactrlcal propertlea
UArtcaoag oila
-Storaae
M-4277
M-4Z78
Mi<*laa ahop practice
>*"*las tranaladooa
Pmr n Number
7<7 161 577
756 155 083
747 ISS 383
Sut>ect
ftige F» Number
Suhje
Page PB Number
Machine tranalations (con. ) 766
770
711
747
775
683
717
692
693
711
804
770
758
757
707
709
709
805
806
790
729
794
885
686
685
687
t«4
687
685
684
785
792
727
792
799
793
70S
Ml
761
755
747
773
781
746
689
776
767
791
801
802
753
747
715
783
787
744
765
76«
150 866
148 395
155 149
153 783
148 313
154 654
155 374
155 375
155 576
153 658
154 510
149 328
154 281
154 719
150 489
161 914
161 915
161 915
153 805
152 135
153 655
153 829
154 624
150 545
147 902
149 904
147 903
149 324
14B7S6
149 521
154 593
150 433
149 522
153 908
153 120
155 320
154 530
171 686
149 096
149 097
154 532
154 123
147 904
155 085
154 454
154 862
154 611
155 414
154 468
151 107
153 905
154 457
171 618
171 619
cms»-45i
171 630
154 646
154 671
154 863
154 864
171 251
150 086-1
150 086 2
Development
- ■ Instrumentation
Ms chines
- • Interference
Magnaflux inspecuon
Magnesium
- -Hardening
-Metabolism
Magnesium oxide crystals
- Deformation
Magneaium-tin alloys
-Properliea
Msgnetic fie Wis
- -Control
-Electricsl effects
- -Measurement
--Simulation
--Theory
MagneDc materials
- -Mapetic properties
--Properties
Magnetic recording systems
--Applicstlons
-Design
-Equipment
Magnetic resonance
-Absorption
- -Measurement
-Temperature (actors
Mapietogasdynamics
Magneto-hydrodynamic wavea
-Theory
Mapietaatriciion transducers
--Daaign
Mapati
- Deaip
- -Materia U
Magnus effect
MainlBoancc
-SchaduUiv
Management engineering
Mapa
- Preparation
Marine biology
Marine borera
-Control
- -Couotei meaaures
Marine meteorology
--Pacific Ocean
Markiw proceaa
Martenalle
- - Deformaiioo
- Internal frictlOB
MaaUcatlaa
--Analyaia
Mate rU la
-Bibliography
--Deformation
--Fracture
--Miliury requiremeata
- -<>ialiiy control
--Refractive propertlea
- -Streaaes
- -Temperature factora
Mathematical computer dau
-Codi^
-Proceaa ing
Matkematical computers
-AppllcaUona
-ClrculU
-Design
-Development
-Equipment
806
805
805
747
748
780
689
794
794
787
788
727
786
799
754
755
767
795
739
730
722
727
795
701
800
300
719
787
754
755
770
750
748
749
707
692
703
758
716
758
706
684
780
776
690
752
768
776
752
764
701
776
740
753
767
767
710
728
735
765
767
767
764
765
805
765
150 086-
150 086-
150 086-
150 086-
152 135
153 805
155 030
154 646
153 694
153 924
155 297
150 558
150 545
154 864
154 080
154 114
154 243
154 455
155 239
155 240
155 241
155 242
148 231
171 573
154 588
154 814
155 618
154 114
154 062
150 133
155 323
155 323
153 777
154 864
155 239
155 240
155 241
155 242
171 604
153 756
148 787
149 0B8
150 489
150 654
148 079
154 661
154 668
154 650
154 566
148 756
154 553
154 453
154 263
171 612 .
148 813
155 IS3
155 381
148 535
154 518
155 153
155 148
OTSSB-451
161 577
154 587
1SS2S5
150 906
154 507
155 578
153 930
153 906
149 138
171 258
153 806
150 086-1
Mathematical con^^uiera (con. )
- -Equipment (con. ) 766
-Opera tloo
-ReliaUlity
-Scheduling ">
-Theory
Mathematical logic
--Applications
Mathieu functkna
Matrix algebra
--Theory
Maxinution
MC-3
Measure theory
Measurement
- - Instrumentation
Mechanlca
-Theory
Membranea
-Vibration
Memory
-Phyaiological factors
Merchant veaaela
ScheduUi^
^telabolism
--Climstic (actors
--Effects of radiation
--Padiology
Metal carbonyla
- -Chemical propertlea
Metal chlor^les
-ThermodynsiBic properties
Metal fllma
--Adb<npcian
--Optical properties
-Thickness
Meul ions
-Chemical reactions
Metal-plastic adbeaives
-Development
Meul plates
--Vibrstion
Meullurgy
-Bibliography
767
807
765
765
738
763
782
806
806
762
767
763
764
763
758
709
760
727
768
759
687
750
688
693
690
696
W8
786
794
799
689
753
711
777
Meulorganic CKxnpounds
--Chemicsl properties
- -Spectrs
-Synthesis
Metals
--Frscture
- -Hest treatment
--Separstion
-Stresses
- -Surface propertlea
- -Tenaile pr^ertlea
-ThermodyBamlc prope
Meteorological hallooaa
--MaterUls
Meteorological dau
- -Greenland
- -North America
Meteorological inatnnnenu
696
696
696
776
777
749
768
786
776
rnes 804
- -DeveHpment
Meteorological
- -Applicationa
Mediyl hydrazlnea
Deierimnaiion
Michigan
MicroBk. teorology
- - Inatrumenutlon
Microacnpy
- Applications
Microwave ampliflera
- -Oevelopment
-Equipment
757
758
707
708
707
70S
150 086 2
150 0B6 3
150 086-4
1S0 086-S
150 086-6
153 785
147 787
155 376
154 087
153 866
155 087
154 261
150 726
150 726
152 135
152 957
148 231
154 961
154 960
155 088
147 844
153 861
149 165
154 114
153 124
148 420
154 593
153 756
171 606
154 592
153 720
155 453
154 872
150 864
150 642
152 180
153 844
171 565
171 594
OTS S8-452
OTSSB-454
155 453
154 262
171 571
155153
OTSSB-454
171 112
154 938
150 864
151 107
171 567
150 844
150 845
153 715
154 163
154 376
154 528
154 532
784 154 706
755
707
802
704
796
718
722
723
154 71*
153 915
154 501
14B233
171 99B
155 2Sa
154 501
154 aot
148 SIS
Ml
lAcrovave equtpoMM
- AppUcaaoo*
Mlcrovave oKiltonn
--De<elin»iniit
iitcfo»«w
kilttcuy
--(fazard*
Mlltury belli
•TVaWag
Mlttary craiatnf
-StaMlu^di
MtBc
-lUdicactlvUjr
Miaerala
- Chemical aoal^la
Miniature electronic efjulpniefii
AjipUcatnaa
•aglaania^
Mtrron
--ReOactlve eflacta
Mlaallc aoaes
- Coadnci
Mlaatle trackiof lyaKfna
Miaaike irtttaortm
--DwamilMtHM
- Matfaemaclcal aMl^ta
Mlaaliea
"CoMTOi ayMMM
•Pwl l^iectiai
•ChMmo* ayatema
•tti^oifmauc cta^cwr-
tsUca
MaKrIala
' Parlofina nee
- Rocket profwlatca ,
- Te temrter ayanaa
-TImc iHstfiodi I
MoMlebotota
' -Teal reaulta
Modulator tutiea
-Daatfa
-Ctroiiia
-Dȴekipn>ca>
MatacMiar roaooa
--Itaory
MotaOilar apectroaco^
Molaoalar atrucnire
--MiAiMatlcal aanl^ia
Theory
-Vltarauaa
ttloa
- Fatigue
MolytaleMai alkiya
■1 prope^tlea
-CriMal atractma
7X7
732
7»
7»
«9t
736
«U
««S
692
«93
7M
690
719
7M
«U
7M
7S7
771
739
737
736
736
736
71J
736
739
740
741
756
736
737
S02
779
736
736
730
741
740
746
7»
7M
723
703
7S6
791
791
792
791
794
693
790
791
699
702
773
791
792
7B1
7S4
77$
797
134 389
154 SOI
154 S03
154 19«
'154 199
154 631
153 S43
154 626
153 S6S
153 »6S
161 371-11
161 371-12
146 7(1
154 263
1S0M9
171 566
154 522
154 243
146 216
154 S15
153 647
153 731
171 24S
171 249
171 247
171 246
171 249
171 230
153 611
153 rro
154 2S9-3
154 290 1
155 141
154 290-2
153 256
171 2S0
146 216
150 243
151 104
171 247
171 249
171 «f90
153 190
155 145
154 466
154 660
154 213
154 213
ISO 109
ISO 535
149 540
154 4S7
148 S63
149 S67
148 935
154 092
150 642
153 903
153 655
153 829
154 092
154 538
148 473
154 158
153 082
149 367
150 006
171 617
171 S97
153 721
Moon
- -Riyalcal etiecia
Motion meter
Naval admimatraUoa
Naval e<)uipfnent
-Effectiveneaa
Naval logiatlca
Naval peraoonel
-Selection
-Teal mettioda
Naval procurement
Naval reaaarch
Naval
eatabliahmenta
--Water aupply
Naval aupfiliea
--Quality control
Navler-Stokea equatloaa
NeopUama
--Production
Nervoua ayaieina
- Riyaiology
Neuriator
Neutron croaa aectlona
-Tabiaa
NeiKroB dateciora
--Deaip
-MaierlaU
Neutron diSractlon aaalyata
Neuuua fluaea
--Spectra
Neutron metera
- Develoianeat
Neutrtna
-Energy
--nnietniiaa
Nickel
-Chemical reactiona
Nickel alloyB
--ApplicatKina
Nickel filma
-Reaonance
Nitratea
- -Chroinatocrapiuc aaalyala
-Phyatolosical eflecta
Nitrogen fluoridea
- -Slbllograpiiy
--Chemical raactlana
Notae
--Mathematical analyala
--Reduction
Notae (Radar)
Notae (Radio)
- Meaaureneni
-Raducuon
Non-deatrucuve leatiag
- ' Equptnenf
Norepinephrine
--Determination
Nuclear reacnona
--Aaalyaia
Nuclear aptna
-Energy
- -Meaauremeni
Nuclear itructure
- Detemunaaon
- -MaihefnaUcal analyala
Nucleatldea
- -Chemical reactiaia
Numbera
-Theory
Nylon
- -Elfccta of radiation
Ocean currenta
-Pacific Oceaa
Oceanography
■ Arctic Ocean
- Inatrumeniailoa
oncer peraoiaal
- -Selection
Oil-alidi rerooaal
Oil I
737
746
752
716
750
«63
683
7S0
806
808
781
742
752
7S»
746
767
782
783
783
794
784
783
782
782
704
723
789
694
687
756
WO
762
744
727
727
80S
734
741
742
694
I
791
I
Olla
-AtoorpOaa
784
784
«89
760
764
752
775
707
«83
716
715
716
n Number
153 947
154 676
155 381
154 648
153 756
153 746
148 774
153 756
154 071
171 318
154 641
154 642
155 361
149 534
155 566
155 297
153 785
155 324
171 616
155 254
150 642
155 322
153 254
153 862
155 324
133 662
154 490
148 7S7
154 210
148 966
171 252
1^291
152 957
155 253
152 965
152 965
151 377 §
148 398
159 099
155 061
155 062
155 098
159 060
154 264
153 862
153 828
153 829
153 207
190171
153 187
153 844
149 165
148 961
149 138
154 529
153 783
154 591
153 781
153 746
154 648
194 671
154 648
Si*iact
Oparadoo
rch
Operacora (Mathematica)
-Theory
Optical inatrumenia
--Daaign
--Devalopment
Optical materiala
--Radiation
Orbiul worker
Onlnance aieel
--Heat treatment
Organic compounda
- -Conduct! vliy
-Eflecta of radutlon
- -Spectra
Organic materiala
--Blacirlcal propertlea
Organic aolventa
--Solvent propertlea
Oamotlc preaaure
--Applicationa
Oilde cadiodea
--Coailnga
Oalmea
--Tcnlc eflecta
Oiygeo (Liquid)
--Cheimcal reaciiona
- -Eaulpmant
Ozygea conaumpiloa
- -Meajuremam
Oxygen laotopea
--Applicationa
Oxygen maaka
--nqralological eflecu
Czooe
- -Chemical eflecta
Packagl^i
-Miliary raquiremenu
Paper
--Applicationa
Paper capacltora
--Eflecu of radiation
Paramagnetic cryatala
- -Maipctlc propertlea
Paramaptttic looa
-Propertlea
Partial dlflerentlal equatlona
--Theory
Particle accelerator^
-•Development
Particle beama
--Optical aaalyaia
Partlclea
--Olffualan
-Moaoo
Partlclea (Airborne)
--Radioactivity
- -Jotata
Peltier eflect
Pentaerythrltol latranltrala
- - Applicationa
- Lumineaceoce
Peptidea
- SyMheala
Permafroat
Melting
Peroxldea
--Cbamical reactiona
--Corabuation
l^rturfaation theory
--AppUcatlana
Phaae detectora
--Applicationa
- -Qrcuica
niaaa modulation
- -Meaaurement
Wwaphinea
--Chemical reactiona
nuapliorua compounda
Prguilc)
--Chamiral reactiona
nioapborylation
-Analyala
Fhotoalactnc traoaducera
- -AppU cat tana
734
SOS
760
792
737
792
682
742
796
781
694
687
702
742
723
6W
740
712
668
703
688
757
743
786
718
791
701
759
703
782
786
786
784
785
714
802
738
702
689
717
782
703
737
790
702
775
792
727
733
727
695
695
697
689
807
WNua^ar
155 260
148 401
153 211
154 S30
153 846
171 254
171 611
154 207
153 936
171 596
153 036
148 219
148 473
154 207
154 490
I
153 841
161 239
153 611
171 606
148 076
171607
171 378
154 657
154 167
154 241
153 207
ISO 133
149 534
150 535
154 261
149 540
154 249
151706
153 S82
154 678
171 539
153 022
154 374
148 214
154 700
171 239
148 075
153 947
153 828
148 473
152 117
149 567
154 989
150 913
154 S69
148 938
1M938
147 841
154 468
147 787
1-13
fkongrapliic emulalons
- PlKXactiemical reactions
HMOgraphic intelligence
Batrgy
If
Tbat maihnrta
nara
-Coaaa^
niaa
--ftaaaure
-Taat reaulta
t
--Corroalon prevention
-Heat transfer
--Hydrodynamic characwr-
iaUca
-MaterUU
Plaaaa 0%yaica)
-AaalyaU
-•liMUty
llHaa oaclllationa
"AoHyaU
"Dawctton
Plaaiicflo*
--Ckyaical effecu
naaitcity
--Maiticinktical aaalyaia
-Theory
--AppUcadona
--DaeoBpoaluon
"Oavalopment
--ikai tranafer
NMaaaUc valvea
■Teat reaulta
taaia of dlmenaiun
Mymcr aolutiona
■-Optical propertlea
--Surface propertlea
MyaarUadon
--Aaalyaia
(ion
aliion
-Ocvelopmeni
-Olelacirlc propertlea
-Matacuar structure
ala
-Tamperaiure (actora
Kaiacn siruciuraa
Kirtable roadmy
■ralkiya
--MMhaaical propertlea
-■frooaaaing
tawrplama
--Bjiitumnt
hivar aupphes
-BtMioipaphy
haOfliadan
--Radar aaalyaia
Pradpiutlan static
-laduction
IVtlibricated bulldinga
--Coaatnictton
--Ihai raaulta
-Meaauremeni
-fhyalcal eflacta
idtTtcea
Pinaiui regulaiora
--that raaulta
752
663
789
689
716
735
715
799
781
803
773
742
803
770
789
799
800
799
804
800
799
800
800
794
768
768
730
757
752
757
736
763
694
703
o9o
699
704
757
752
697
696
644
696
806
716
715
716
777
777
7«
681
766
784
789
714
718
713
714
715
714
726
754
735
714
740
741
FflNiniber
155 438
150 916
153 908
155 486
154 668
154 634
154 673
154 455
154 612
155 081
154 862
155 250
155 081
154 572
150 414
153 584
154 455
154 370
154 272
154 448
154 372
152 180
154 194
♦154 371
ISO 558
ISO 739
153 124
154 120
171 i64
154 121
154 699
171 685
171 612
159 972
153 870
153 486
149 89S
148 400
171 570
171 575
148 407
171 685
171 612
171 563
171 570
171 574
171 570
171 571
154 071
154 682
154 663
154 665
154 667
154 537
154 536
193 847
171 689
150 848
154 706
194 078
154 625
154 652
154 628
154 613
154 666
154 623
155 567
171 595
154 634
1M6Z3
154 290-1
154 290-2
Si*>act
Preaaure awlKhaa
OevelopoMK
Preaaure veaaala
-Daaip
Preatreaaed concrete
Preatreaaed timber
Primatea
-Aging
Primed circuits
-MaterUla
Privation
-Psychological eflecta
Probability (SutiaUca)
- -Applicatkna
Propellaata
-Detonation
- -Thermal propertlea
Propellers (AerUl)
- Model lesi reaulta
Propellera (Marine)
- -Hydrodynamic characvr-
iatlca
Protecdve coveringa
-Teat reaulu
Protective aheltera
--Arctic regiona
- -Conumlnailon
-Praaaure diatribution
- -Safety measures
--Teat reaulu
--VenUlatlon
739
749
753
715
716
668
729
665
759
760
761
80S
807
738
804
711
746
744
786
715
743
742
742
714
717
715
743
744
690
746
Procona
-Applicationa 727
Proximity vamlng InformaUon 710
Pseud cluster expanaion 784
Paychology
Theory 666
Psycfaometrics 686
Public healdi
•Preaervailoo 692
Protelna
- -Macaboilam
Pulae modutkdaa
-AppUcaUona
Pulac tranamlitera
Development
Pyridine derivativea
- - Stability
- Toxic eflecta
Pyrogena
- Hiyalological eflecu
Quality control '
- Statistical analyala
• Theory
Quantum mechanlca
C^ieueing proceaa
Radar antennaa
-' Equipment
Radar equipment
Applicationa
Radar receivers
- -Mathematical analyaU
Radar rcflectiona
Radar signals
-Detection
Radar tracking
Radiation
Biochemical effecu
' Chemical effecu
- -Pathological effecta
- Physiological effecu
Radiaaon damage
- Meaauremeni
-Teat facilliiea
Radio antijamming
- - laatrumentatioo
Radio interferenca
■Maaaurengnt
l-U
693
723
723
702
691
689
759
764
748
693
806
739
730
734
730
727
739
693
784
796
746
691
784
784
718
729
794
HNMitor
1S4 2H-3
153 917
154 620
154 663
154 665
154 667
154 594
154 166
171 610
149 558
149 165
148 906
148 907
148 401
148 502
152 022
154 440
154 549
153 725
153 919
154 167
154 621
154 653
154 627
154 622
154 622
154 629
154 617
154 653
154 669
154 674
153 714
155 414
154 114
154 744
153 187
154 462
148 005
121 784-R
161 371-11
161 371-12
ISO 109
154 213
.148 932
193 841
155 297
148 782
148 535
148 787
153 903
148 401
190 903
199 079
159 260
155 079
152 965
153 647
154 592
171 572
153 936
155 566
171608
171 572
155 322
190 901
194 «M
194 412-1
194 412-2
Radio interference (cm. )
- - Reduction
-Sourcea
Radio interference ana ly^era
--Performance
Radio raceivera
--Scnaitivlty
Radio slgnsls
--Detection
Radio traaamlttera
--Applicatloaa
Radio iravea
--Abaorptioo
- -Attenuation
- -Scattering
Radioactive waaie
-riani metaboliam
Radioactivity
- -Recording devices
- -SutUtical aoalyaU
Radiobiology
Pamt P> Number
729
729
747
748
789
734
794
727
•90
804
805
731
692
785
782
686
693
692
781
-Handbooka
Radiocfaemlatry
Radiofrequency tranaformera
- Deaign 719
Radiol aotopea
- - Fractionadon 782
Radiological conumination
-Countermeaaurea 692
693
743
Radloraetera
- -Applicationa 792
- ■ Pe rformance 727
Raman specirs 702
Rare earth compounda
- -Stability 702
Rare eanha
- -Thenrodynamic propertlea 701
Rare gaaea
--Applicationa 690
Reaction (Psychology)
-Test medioda 664
--Teadng equlpoieni
Reactora
- -Shlekling
Reading machinea
-Oe^kipmeni
Reaaoaiag
- -Psychological factors
Recombioaticn reactiona
Re-entry aerodynaraica
Refractometera
•-Deaign
Refractory coatiacs
- -Temperature tactora
--Teal reaulta
Refractory materiala
--Riaae atudiea
--Phyaical effecu
Refrigeration syaiems
--Development
Regression theory
Rein/urced ctxicrete
- -Applicationa
Relaxation time
Reliability
--Mathematical analyala
--Sutladcal analyala
Remote underwater
manipulator
Reaiatora
--Temperature tactora
Reapiratiaa
--Maaaara— at
tRhaolnp
RncwB woototy
Roaife
- -Conatructioa
--MaierUla
--Teat reaulu
Rohota
-ManriaU
686
784
807
80S
685
699
736
771
701
771
754
754
777
802
763
716
701
786
764
707
725
7«i
688
713
715
716
717
686
749
154 651
154 643
154 646
154 637
154 078
154 412-1
154 412-2
154 412-1
154 412-2
152 9^
154 263
147 840
161 969
190 914
150 654
153 982
194 717
159 579
154 593
121 784-R
171 596
155 199
154 717
121 784-1
161 371-11
161 371-U
154 675
155 437
154 061
148 747
148 932
154 1S*
155 574
148 756
149 521
155 575
195 322
147 787
155 030
147 903'
149 085
171 248
154 819
154 918
154 815
171 617
152 9*0
154 537
171 999
148 741
194 666
150 133
148 974
171 9M)
193 7tl
194 166
171 607
154 120
154 594
154 632
154 669
194 665
154 667
154 645
154 462
153 917
urn
■I aiui)yata| 7»
Socket mcKori
^rformance 747
Rocket ooudizers
-Chemical reacilo^ 740
Maierxli 702
Rocket pr(velUnia
-CcmtiiMtKn 747
-Mawriala 756
Rocket propuUton 736
-tlieorT 747
RoudDg aurror ceinc raa
-AppDcauoas 739
Rotaaog structures
-Acoustic pToperti^* 747
eala
-ItalOmience 7S3
Rvddera (Marine)
-Hytirodynenuc dimeter -
ladca
Ruofi-Kutu analysia
Rimwy barrier syaie na
Ruovaya
- -AppUcatlOM
-Arcnc rvftoa
- Load dlatrlbut ton
-Visibility
Safety vaivea
- - Oeve hJiaiMUt
SampUng (Sianatlcs)
-Applications
Sand
-Mechanical propef^tie
SaiKturldi panela
-Aoalysia
Satellite vehicle trajfctoriea
--Analysis
--niyslcsl (actors
Sauclason antenna
Scheduling
Mslhetnatical analysia
-Tlieory
Science
• diina
S^ieocUlc reporta
- -Sutaject has dings
Scientific research
Scintitlatioa couMera
■AppllcatMas
Sea bne^
- -Meaaurement
Sea water
--Elcctroiyala
--OnsUaatioa
--BiMia(raptay
Seiamlc wavea
- -Pnyaflstion
--PFopwtles
Selavam (Liquid)
- -ftilyineruaiiaD
Semantics
Semiconductors,
-Blacarical propsi tlea
iaMory pBTcepUoii
-MMMtloa
SeqMoilal analysis
-AppHcailans
Sksfts
- Imerference
Sheets
--Hypers
salcal I
745
802
7aB
742
714
714
709
712
6B4
759
751
768
739
737
720
6«3
749
7*3
758
fl Number
154 716
155 149
161 239
171 255
154 454
171 2S2
171 249
154 454
171 W6
154 646
171 6*8
149 745
150 243
161 914
154 642
154 619
154 678
154 743
153 611
148 756
14«782
152 005
154 121
154 588
153 947
153 719
148 313
154 869
153 486
147 144
8i*i>ect
Shielding (con. )
- -Materials
Page n
tei cm sa-422
807
M8
806
808
782
706
712
712
704
704
793
699
806
806
718
79i
796
liropertles 794
801
793
794
T93
cter icicristlca
proptrtics
685
761
764
735
747
770
779
780
708
7«S
171 519
150 338
154 071
171 318
154 704
154 570
154 679
IS4 245
149 216
149 775
153 923
171 575
153805
154 071
155 258
171 573
148 016
152 199
154 868
153 849
150 545
153 849
171 610
148 906
148 907
148 535
150 903
154 646
149 328
153 7«
153 750
153 751
155 0*0
1S«««7
Ship hulls
- -Model test results
--Vibration
Ships
-Equipment
-Plreproofipg
--Mai mesa ace
Materia la
-Mooring
--Spectra
Shock avoidance apparatua
Shock waves
-•Analysis
--Difiraction
--loaizlngenecta
--Physical eflects
--Pressure
- - Reflection
Shrouded propellers
--EHeciiveness
--PBrformaoos
-Thruei
Silicon
- Applicaaooa *
- -Diffuaion
Silicon crystals
- -Surface pro^iertlea
Silicone reains
•-Apptications
Silicone rubber ^
Sllloooea
--Piopertlea
Silver
- -Cooducuvlty
Single crystsis
--Deformation
-Magnetic propertlea
--Polymorphism
Slip damping
Skiw neutrooa
-Oenaity
Snow
- Radiation
-Shear stresaea
-Trafncability
Snow cryaiala
- -Temperature (actors
Snow plaaBs
Snow roads
- - Constniction
Snow vehicles
-Applicstions
Soap solutiona
- -Surface properties
Social sciences
--Theory
Sodium chloride
- -Meullurgical eflecta
Sodtam hypochlorite
- -Decontaminating eftecta
SodiufB-tiMigaien alloys
Crystsl structure
Soil truss
Soils
-Erosion
- -Mechaaioal properties
-TralBcsbility
Solar batteries
- -DevelopmeM
Solar energy
--Ataaorptioa
-Applications
Solar flares
-Claaaificatlon
SoienoidB
- -Apptlcatwas
Solid delay lines
-Osaivi
Solids
- - Oelormatian
--Mapietic propertlea
•-Properties
--Tsaapersture fsctors
782
784
745
745
744
742
744
756
746
769
686
700
772
699
739
772
786
746
711
746
732
753
793
753
782
782
787
794
795
794
711
783
704
718
714
718
766
717
717
717
703
807
77»
712
797
718
711
751
716
717
721
Ml
740
681
736
729
739
795
794
801
802
155 439
155 431
155 432
159 322
199 428
159 706
149 745
155 253
155 250
171 251
154 281
154 676
151 932
155 575
154 509
155 ORO
149 085
171 666
199 080
149 540
153 725
153 642
153 725
154 479
153 914
153 849
171 688
195 432
155 432
154 864
150 558
194 062
148 781
171 594
153 891
148 233
194 644
194 619
154 644
150 848
154 463
194 463
154 463
148 400
152 114
153 295
154 679
153 721
194 644
193 642
192 006
152 009
154 667
154 630
154 525
154 526
193 718
171 605
194 SR5
199 870
IS9 073
171 686
171 573
190 642
148 970
171 619
St*i»ct
Solutions
-Luminescence
--HiyBical propertlea
Sonar equipment
- -Hydrodynamic character-
iatica
Sorting '3
Sound
--Absorptlan
--AttenunikMi
- - Propngation
Sound tranamisaioa
-niyalcal factors
Space charpaa
• -Electromagnetic eflecta
- -Madieniatlcal analysis
Spsce flight
--Physical eflects
- -Simulation
Space medicine
Spaceahipa
-Control syatema
--Ei^pment
--Propulsion
Spectrographic data
Specirophotocneters
-•Applicationa
Sptierea
•-Cooducuvlty
- -Scrssses
Spiral warp method
Spray tanka
••Dealgn
Sprays
••Prcductioa
Springs
-MsierUU
Sprue
• - Pathology
Squsre root iiielhod
Squid
Sisr trackers
-•Deslpi
Survstion
••Physiological effects
Sudatical anslyala
- - Applicatloos
--Theory
Statistical Inference
Paae PRNumhsf
796
702
774
765
791
787
787
787
723
789
727
682
710
MO
737
740
748
791
787
788
768
749
743
743
740
690
763
703
803
718
668
748
807
759
760
762
763
761
Statlaiica 763
-Theory 761
Steam
• •Thermodynamic propertlea 802
Sieel
••Applicatioaa 713
714
715
718
778
778
778
776
778
-Bflscts of radtation
-Fracture
-Heat ircatmem
-Internal friction
•Mechanical propertlea
- -Sireases
Steel tubing
- •Corrosioa prevention
Stereochemistry
Stereoregular polymers
Stersospeciflcity
Storsge bstteries
• - Tempe rature toctors
SnragB laaka
Storma
• -Detect ioo
Streas analysia
••Appticatiuns
--Equipment
••Theory
7M
781
697
696
697
729
715
705
749
768
718
776
797
153 936
148 747
154 165
155 376
153 062
153 906
ISO 198
150 198
148 323
150 414
150 908
171 601
171 611
153 695
155 574
155 251
155 252
171 60S
155 345-1
148 939
154 161
148 958
171 684
153 917
154 655
154 65S
155 148
153 714
155 088
150 53S
150 534
171 609
154 168
148 095
152 114
149 790
154 098
147 847
154 OM
154 124
148 748
154 349
148 906
148 907
155 088
194 121
148 353
154 628
154 613
154 646
154 652
171 188
151 106
171 188
154 453
150 780
154 870
171 253
154 958
154 612
154 564
171 570
171 563
154 598
154 671
154 532
171 548-1
171 684
154 644
155 153
ISO OSS
1-14
Sob'e'-t
ftr
PB Number
Sutaiect
fsm^
PB Number
Si*tecl
f^r
FB Number
liraniium asides
Test seta
Tranaducera (con. )
-Magnetic propertlea
754
155 239
-Performance
729
194 ABO
-Theory
726
155 567
Strootium titanate crysuls
Thermal radiation
155 568-1
-Dieleciric properties
797
154 077
- -Analyais
708
154 556
155 568-2
Structural metals
768.
154 958
Thermal stresaea
155 5683
Structural shells
- -Matheim tical analysis
801
148 348
155 569-1
•Stresses
7<a
155 090
148 970
Tranaformaiioaa (Mathemaacs)
Structures |
Thermionic emission
719
153 907
•Theory
760
153 211
•-Deformation
7M
148 813
^
723
194 450
Tranaiators
190 739
Thermlsiora
--Applications
724
150 792
-Design
7M
151932
-Applicationa
804
154 440
••Dealgn
719
149 816
•-Optical (sctors
.716
154 647
The rmoba lance
694
153 163
• -Developtnent
735
155 321
Submarine bulla
Thermochemiatry
700
154 709
•Materials
732
154 479
f-tlaat eflecu
796
153 904
Thermcouples
••Test results
731
171 566
-Materials
745
153 707
- -Applicationa
802
154 508
Tranamlssion lines
^
--Vibration
744
155 413
Thertnodynamlca
767
153 930
-•Radiadai
729
154 618
Svbnarine noise
- Tablea
804
171 567
Tranamltier tecelvera
- - Reduction
744
155 413
--Theory
733
154 196
•Equipment
726
150 846
Sutasonic (low
^
154 199
Tranaport coefficienu
799
149 911
-Turbulence
770
150 866
Thermoelectricity
730
171 691
Traveling saleaman problem
763
153 486
SuUonaiaa
788
152 061
Traveling wave tubes
-•Applications
- -Syntheaia
««•
154 118
794
152 199
727
154 061
Sulfur
. 802
171 559
•- Development
734
148 398
-Applications
7U
155 254
Thiazoles
-Maiheinatical analysis
723
148 323
-Separation
777
171 384
- -Properties
695
154 269
727
150 902
Sulfur oxides
Thin fllma
--Chemical reactions
698
154 118
- -Conductivity
797
154 232
Triangular trings
Stanable (unctlooa
762
154 452^
^^y^lectrlcal factors
789
148 757
--Aerodynamic diarscter-
Sua
s
l^^^pictrlcal properties
796
152 220
istics
772
149 214
--Riysicsl effects
737
153 947 ^
U^Hhoietic properties
796
152 220
Triazolea
-Radiation
681
153 718
^^11 '
171 569
--Syndieais
695
154 269
Si^raerodynamica
773
154 158
T^SftHfion
731
171 566
Tigger circuita
Saperalloys
776
161 236
Thorium
-Development
731
171 566
Sn^rconductivity
-Properties
719
153 907
Tngooottietry
--Meaaurepient
796
152 220
Thorium oxides
•Applicationa
726
154 595
797
154 232
- - Phase studies
754
152 980
Trinitrotoluene
Si^relevatlao
738
153 866
Throcnbin
• Thermal properties
738
171 256
StfsroKldlaera
702
ri 255
- -Physiological effects
690
154 427
Tropical deterioration
Si^rsoalc fkw
Thunderclouda
-Teat methoda
728
154 487
--Mathematical analysis
T70
171 593
-Electrical properties
705
154 532
Tropical regions
773
154 158
Tie rod yoke
746
154 649
-Meteorology
706
154 566-s
Supplies
Tilt-wing
710
155 255
Tungsten
N
-Scheduling
749
154 869
Time series
•Propertlea
719
153 907
759
149 558
- -Theory
759
149 750
Tungsten carbides
■X
Surface-active agents
762
154 094
•Applicationa
782
155 429
- -Effectiveness
713
171 479
154 124
- -Density
784
155 428
Surfsce urgeta
Tin
Turbulence
-Radution
792
155 437
- -Conductivity
797
194 232
- •Acoustic effects
787
153 906
Switching circuita
Tin compounds (Orginic)
Turbulent boundary layer
767
148 231
- -Chemical reactions
696
171 571
- -Analysis
772
154 816
806
150 227
Tirea
••Seat transfer
711
153 658
--Tempersture (actors
735
155 321
- Teat reaulta
750
152 006
••Mathematical anslyala
771
148 317
--Theory
719
149 816
757
171 578
UDeta
775
155 085
Syndietic alloya
777
154 536
Titanium
Ultra high (requency
■ Brazing
780
153 558
receivers
■Development
752
171 612
--Chemical reactlom
740
161 239
•Design
725
150 847
Syaihetic lubrlcaiita
-Diffuaion
753
153 914
Ultraaonic radiation
-Developtnent
756
155 082
- -Extrualon
779
155 150
-Reflective effects
792
153 120
Synthetic mica
Titanium alloya
Underground structures
--CrysuMlutlon
798
155 154
•ApplicaOons
749
153 917
• Shielding
785
154 697
155 155
- -Brazing
780
153 558
Underwater equipment
155 156 -
--Fracture
779
153 295
•Deaign
707
153 781
Y
155 157
-Mechanical propertlea
745
153 707
Underwear
Sysiema engineering I
734
155 260
779
151 104
-Thermal inaulaUon
785
154 169
Tiduaioacopes J
153 752
Urea
- -Apptications 1
684
154 063
161 237
•-Chemical reactions
644
171 574
TaiAa I
780
153 750
Urine
--Plre control systeira
738
153 866
193 751
- Analysis
694
154 264
Taran recognition ^
--Study and teaching \
Titanium oxldea
Valvea
683
150 916
■Cryaul structure
797
153 721
--Equipment
740
155 148
• -Visual (actors \
684
154 063
Topology
760
^ 148 212
VanadluniMxidea
• -Crystarstruaure
Targets \
t
• Theory
760
147 559
797
153 721
--Configuration
\6«4
154 063
764
154 456
Variable resistors
--DetecUon
\m
154 064
Tory ll-A
747
155 383
•Development
735
155 384
Taylor -MaccoU equation
772
154 563
Towed bodies (Aerial)
Vehicle wheels
TDU^/B. TDU-lOB
709
153 861
Drag
709
153 861
- - Teat reaulta
750
171 613
Ttlsmeiar systems
Towing cablea
Vahicles
--Design
730
171690
- -Teat reaulta
709
153 861
• -Electrical ayatema
729
154 643
--Development
737
153 648
Tracked vehiclea
-Maneuverability
717
154 630'
741
153 890
- Design
707
153 781
Verbal behavior
686
147 530
Telephone cables
-Motion
751
152 007
-Teat method.
807
152 114
-Cor roe too
729
154 624
152 008
Vertical guai recorders
Telapboae communicauona
Tracking
--Design
706
154 527
systems
- Test reaulta
682
149 444
Vertlcsl indlcatora
: -Equipment
730
154 639
Trailers
-Errors
718
171 609
Tallurldes
Bibliography
752
153 703
Vertical take-off planea
--Properties
793
153 923
- -Maneuverability
752
153 703
- -Equipment
711
154 549
Taaperaiure
Training
- "Ilg^- test resulu
709
154 580
--Dstanm nation
803
154 720
- -Psychological (actors
685
147 903
-Landing
711
153 642
802
. 154 508
Training devicea
- Dealgn ^
- -Simulation
710
155 255
--Northern hemiaphere
803
154449 '
771
149 778
Very high (requency con-
Tcasloa controllers
751
154*58
Transducers
municaiKKi syanma
Ttareatrial msgneiism
- -Effects of rsdUtion
726
155 568-3
-Test (acilitiea
731
150 914
--Msssurement
788
154 102
-MaterUte
tlb
155 568 1
1-15
Very U^ frin— cy n^tven
--DnIfB
VIbratton
-PreqMBDcy measur^neM
--Madmnatlcal tnalytia
rtNumter
Mfwt
Hm ttHim^btT
Vlfendaa laoUton
-AfpUcattOM
' -MaAMMdcal aBaly^ia
VtaylMMM
- -n>iyiB*rUailan
VtoyI potymrrs
--AppUcaHoM
- - Wm^m daaenarad^
Viaual perception
- - MeaaureineiW
-nryatcal
-Teat meihoda
Viaual direahotda
Voltage ragulMara
- -BlactTooiafwtlc i
Vortloea
- -Mutemaacal aoal
VZ-7AP
Walraa' ta tonne met
Waidcaa
lyila
Warytnf tuB
WadMag mactunea
- -BlacmniafDetlc eC vcta
Wa»r
Wind (con. )
72S
1S0S47
-nuiflcackia
743
154 675
-CBltforala
704
155 089
154 677
- -Caophyalcal factora
705
154 447
735
154 507
-Spectra
702
141747
- -Meaauremeni
709
154 531
759
14 420
- - Vapor preaaure
74*
153 S47
706
154 527
735
155 M4
Water level
745
154 664
785
153 582
711
171 594
Water auppllea
- -New York
706
154 570
692
161 37111
- -North America
705
154 163
744
155 2S3
693
161 371-12
154 376
735
155 0*4
-Sourcea
742
154 642
--PacUlc Ocean
706
154 M6
735
154 307
Water tanka
- -Shaar atreaaea
704
155 089
--Arctic reflona
715
194 670
705
154 531
696
171 570
Water rapor
707
154 562
-Heat tranater
7«
154 S96
- -SlmuUtlon
. 705
154 533
757
171 578
- -Thermodynamic
--Tein|»rature factora
705
154 447
171 579
propertlea
74*
153 B47
-Turbuleaca
707
154 562
7M
154 4S7
Water wavea
-Velocity
704
155 089
--Fbyaical effiecu
746
154 676
Wlodtunoela
M2
171 601
- -Surface propertlea
774
150 624
-Daalgn
770
154 572
MS
130 916
Wavepitdea
Wli^ahxa
«*S
171 610
- -Oevelopmem ^1
731
154 956
- -Model teat reaulu
710
155 146
7U
1M647
154 957
Wlaga
iM
IS4 064
732
155 299
- -Superaonlc charactertatlca 770
171 593
Weaiker atationa
WinterlMtlon klu
7sa
153 900
- -OrfanUation
Weight leaaneaa
707
154 52S
--Arctic reglcna
Wire
715
154 669
7»
154 643
--Phyaical effecu
662
171 611
--Detonation
7a«
155 573
-niyalological effects
682
171 601
Wood
772
149 214
WekM joUiu
- -ApplicaUooa
715
154 663
153 84*
--Analyala
74a
153 694
716
154 665
711
153159
Wekla
154 667
■07
147 M3
- -Mactianlcal propertlea
796
153 904
--Jotaia
717
154 654
715
154 621
Weat Ford
739
154 SM
--Preacrvatlon
716
154 668
Wetting afenta
.-
7St
154 6S0
713
154 63t
-Phyaical effecu
703
148 400
171 330
745
154 616
WlUakera
796
171 596
X-2
715
154 663
Wlmi
X-3
716
154 665
7»
154 651
- -■ouodary layer
705
154 533
X-4
X-radUtlon
- -Doaafe determination
--Riyalologlcal effecu
716
692
692
154 667
155 374
155 375
NUMBER INDEX
1-16
I 91*
20l6
Wwaber ftai Number
AALTN-eO-19 786 AD-227 820
AALTN-60-20 688 AO- 227 821
AALTN-60-21 785 AD-228 063
Aa4A-IK-IN-4-59 737 AD-228 181
AB4A-DC-TN-59-59 ^737 AO-228 399
UHA D6P-TR-5-59 ^37 AD-228 558
ik»(A RP-TR-2-60 755 AO-228 594
*D-7616 774 AD-228 707
AD-24 718 698 AD-229 041
AD-5S 462 765 AD-229 236
AD-Sl 344 773 AO-229 434
AD-63 620 778 AD-229 435
AO-11S343 103 AO-220S02
AD- 121 182 106 AO-229 603
AD-121716 763 AD-230 401
AD-129 932 791 AD-230 412
AO-130 967 7(9 AD-230 528
AD-135 602 «•» AD-230 541
AD-136 863 716 AD-230 716
AD- 142 102 710 AO-2X769
AD-147gll 740 AO-230 993
AD-148 627 732 AD -231 098
AD-148 801 732 AD-231113
AD-153 917 72t AO- 231 332
AD-155 353 764 AD-231 372
AO-156 541 779 AD-231 772
AD-158 023 744 AO- 231 855
AD-158 529 726 AD-231
AD-161 563 747 AD-2321
AD-162 607 776 AD -232 079
ikD-200 088 72S AD-232 085
AD-200 649 731 AD- 232 098
AD-3D0 690 832 AD-232 161
AD-70O7O6 719 AD-232 180,
AD- 201 159 737 AD-232 445
AD-201 225 740 AD-232 446
AD-201 524 764 AD-232 486
AO-203 696 742 AD-232 696
AD-20S151 719 AD-232 942
AD-206047 718 AD -233 167
AD-306 051 785 AD-233 478
AD-207 217 721 AD-233 688
AD-2D7 400 752 AD-233 781
AD-2D7 856 798 AD-233 795
AD- 307 896 734 AD-233 959
AO-208 292 735 AO-234 057
AD-309 045 710 AD-234 229
AD-X>9 620 740 AD-234 445
AD-210II2 728 AD-234 483
AO-210 240 768 .AO-234 541
AO-210 287 725 AO-234 560
AO-210 804 701 AD-234 837
AO-211 267 690 AO-235 077
AO- 21 1303 763 AD-235 042
ilD-211435 724 AD- 235 043
AD-211733 720 AO-235 059
AO-2I2 087 792 AD -235 304
AD-212 748 735 AO- 235 445
AO-212g89 758 AD-23S 463
AD-214 354 798 AO-235 539
AD-214 596 725 AO-235 577
AD-2tS221 787 AO-235 684
A0-21S 434 808 AD-^5 929
AD-215 454 766 AD- 235 940
AD-216 434 728 ' AD- 235 942
AD-217 407 783 AO-236 208
AD-218 570 746 AO-236 220
AD-218 886 749 AD -236 453
AD-219 020 798 AD-236 735
AD-219 061 777 AO-236 758
AD-22D 201 765 AD-236 973
AD-230 202 266 AD-237 108
AD-220 203 766 AO-237 109
AO-220 204 766 AO-237 151
AD-220 205 766 AD-237 435
AD-220 206 766 AO-237 438
AD-230 920 751 AD-237 439
AD- 225 120 683 AD-237 454
AD-225 306 662 AD-237 455
AO-225 507 777 AO-237 459
AD-225 874 772 AD-237 631
AD-2» 974 733 AD-237 643
AO-226 006 7r AD-237 753
AD-226 522 805 AD-237 832
AD-227 460 764 AD-237 925
AD-227 511 778 AD-237 967
AD-227 641 771 AD-237 970
AD-237 699 , 699 AO-238 000
AD-2r 737 795 AO-238 034
/•
•uppl.
723
722
7M
781
720
721
(06
7SS
7M
7S2
7»
7W
721
793
7ID
721
7«2
■M
7<r
7M
777
73B
7H
739
731
«»4
7W
786
no
782
741
799
736
757
787
788
»8
<94
698
106
790
698
778
7«r
792
710
«9«
788
790
7M
733
707
738
«33
733
7W
791
738
799
<99
727
733
796
735
73ft
728
721
307
»4
397
761
«3S
MS
337
783
307
787
7«2
«3«
748
799
339
79*
7«
703
Number
AD- 238 035
AD-238 036
AD-238 040
AO-238 068
AD- 238 109
AO-238 142
AD-238 153
AD-238 169
AD-238 177
AO-238 255
AD-238 288
AD-238 294
AD-238 376
AO-238 423
AD-238 472
AO-238 481
AO-238 529
AO-238 626
AD-238 786
AO-238 823
AD-238 922
AO-238 991
AD-239 007
AO-239 043
AO-239 044
AD- 239 063
AD-239 064
AD- 239 108
AD-239 170
AO-239 242
AD-239 262
AD-239 361
AD-239 376
AD-239 400
AO-239 404
AD-239 436
AD-239 453
AO-239 476
AO-239 548
AO-239 652
AD-239 653
AD-239 690
AD-239 691
AD-239 764
AO-239 776
AD-239 777
AO-239 830
AO-239 832
AO-239 896
AD-239 919
AD-239 975
AO-240011
AO-240 024
AD-240 025
AD-240 036
AD-240 087
AO-240 134
AD-240 144
AD-240 159
AD-240 160
AO-240 177
AO-240 178
AO-240 179
AD-240 180
AD-240 283
AD-240 379
AO-240 389
AO-240 400
AD-240 514
AD-240 520
AO-240 631
AO-240 656
AD-240 709
AD-240 721
AD-240 788
AD-240 860
AD-241 139
AO-241 160
AD-241 238
AO-241 278
AD-241 421
AO-241 531
AO-242 188
AO-242 270
AO-242 346
AD-242 408
AD-242 445
AO-242 454
AO-242 468
1-17
703
703
801
771
734
723
663
■02
687
703
■05
711
774
704
789
703
764
788
763
664
756
683
768
695
695
761
761
702
791
795
702
691
786
801
791 '^
778
704
687
702
764
720
793
793
775
734
733
772
■04
704
687
690
760
632
770
<99
799
749
775
799
■07
736
736
736
736
786
745
684
719
722
799
«»4
771
730
«»1
797
734
«3*
792
TOO
728
701
306
300
799
708
791
he
AD-242 538
807
AO-242 540
794
AD-242 729
787
AD-242 865
774
AD-242 962
740
AO-242 963
721
AO-242 974
768
AD-242 997
770
AO-243 021
724
AO-243 048
794
AD-243 103
794
AD-243 251
796
AD-243 487
TOO
AD-243 488
794
AD-243 566
789
AO-243 746
697
AO-243 792
749
AD-243 793
749
AO-243 864
786
AD-243 924
775
AO-243 974
692
AD-244 034
737
AD-244 094
751
AD-244 095
791
AD-244 096
790
AO-244 097
790
AD-244 098
781
AD-244 099
781
AD-244 598
796
AO-244 745
796
AO-244 798
761
AO-244 937
790
AD-245 021
759
AD-245 359
,706
AD- 245 466
754
AO-24S 523
689
AO-24S 562
795
AD- 245 804
762
AD- 245 887
7r
AD-246 047
756
AO- 246 090
694
AD-246 1S3
752
AO-246 155
691
AD-246 239
791
AD-246 364
708
AD-246 395
684
AD-246 500
789
AD-246 515
791
AO-246 530
710
AO-246 636
784
AD-246 766
760
AD-246 771 superseded
718
AD-246 785
722
AO-247 248
770
AO-247 525
712
AD- 247 539
792
AD-247 564
769
AD-247 667
763
AO-247 685
730
AD-247 702
784
AO-247 721
722
AD-247 838
697
AD-247 839
681
AD-247 892
724
AD-248 019
7r
AD-248 040
790
AO-248 063
733
AO- 248 071
739
AD-248 112
797
AO-248 148
749
AD-248 151
724
AD-248 203
707
AD- 348 216
710
AD-248 227
688
AD-248 232
610
AO-248 233
711
AD-248 235
7»
AD-248 259
778
AO-248 263
730
AD-248 264
730
AD-248 265
779
AO-248 268
711
AD- 148 356
711
AD-248 367
799
AD-248 373
772
AO-248 393
748
AD-248 445
782
AO-248 449
778
AI>-a4S540
798
I!
Number
AD-M8 54S
7M
AD-3MSM
738
AO-aMS72
7S7
AD-MS 590
725
AD-3M623
699
AO-MS6M
6S3
AD- MS 636
787
AD-MS 647
753
AD- MS 651
761
AD-MS 652
762
AD-MS663
761
AD-MS 7M
709
AD- MS 716
711
AD-aM744
701
AD- MS 801
693
AD-MS 86*
752
AD-MS 887
790
AO-MSSSS
790
AD- MS 947
719
AD-M9 0S3
774
AD-M9 0S7
767
AD- 3*9 058
795
AD-M9 079
736
AD- 349 080
796
AD-M9 100
681
AD-M9 107
705
AO-M9 108
709
AD- 349 109
705
AD-M9 116
«f»l
AD-M9 167
700
AD- 349 189
70f7
AD-M9 192
746
AD-M9 195
7S9
AD- 349 196
7S7
AD-M9 224
701
AD-249 231
782
AD- 249 235
694
AD- 249 239
787
AD-249 269
718
AO-M9 321
792
AD-249 T78
789
AD-249 422
684
AD-249 423
684
AO-249 444
696
AD-249 452
705
AD-249 477
788
AD-249 519
T9I
AD-249 523
773
AD-249 571
753
AD-249 572
TV
AD-249 573
796
AD-249 588
vn
AD-249 644
801
AD-249 659
806
AD-249 715
708
AD-249 719
786
AD-249 770
7S4
\D 249 773
■nt,
AD 249 777
803
AO-249 786
802
AD-249 788
AU
AD-249 800
786
AD-249 801
6M
AD-249 802
785
AD-249 817
706
AD-249 820
774
AD-249 S26
725
AD-249 871
794
AD-249 921
8»4
\D-249 9r
730
AD-2S0 065
7»
AD-290 102
7*2
AD-2S0 104
•96
AD-250 199
762
AD- 250 202
758
AD-250 257
778
AD-2S0 289
790
AD-2S0 379
789
AD-2S0S0I
749
AD-2S0 530
792
AD-2S0 661
801
AD-2S0 665
73S
AD-2S0 672
804
AD- 230 675
700
AD-230 732
764
AD-2S0 782
770
AD- 230 799
IV
AD-2S0 896
«n
AD- 290 918
702
AD- 250 924
709
AD-250 937
726
AD-2S0 938
736
AD-2S0 9SS
739
AD-2S0 9S9
7«
AD- 230 980
772
!te
WurabcT
AEDC-TN-60-214
AEDC-TN-60-227
ABDC-TN-60-230
ABL-57033-F
AF-Tll-6682
AFIMD-9- 10372
APWID-60-968-5
AFaira>-eo-6i86. v
AFaMD-60-6187, v
AFBA) A60-5488
AFaMDTR-S9-18.
AFBMD-TR-eO-74.
AFBMD TR-60-74. ».
AFBMD-TR -60-85. v.
AFn4DTR-60-303
APCCDOTN-ftO-ftO
afcx;dotn-«)-io2i
afccdo-tr 60-40
afccdd-tr 60-41
afcrc-tr-s9-293
AFCRL-103
AFCRL-201
AFCRL-2X
AFCRL TN-60-360
AFCRL-TN-60-411
AFCRL-TN-60-417
AFCRL TN- 60 -564
AFCRL -TN-ftO-805
AFCRL TN-60-809
AFCRL TN-60-818
AFCRL-TN-60-823
AFCRL-TN-60-832
AFCRL -TN- 60 -835
AFCRL TN-60-836
AFCRL -TN-60-979
AFCRL -TN 60-1107
AFCRL-TN-60-U42
AFCRL TN-eO- 1154
AFCRL-TN-60-U68
AFCRL-TN-60-1178
AFCRL -TR 60-165
AFCRL -TR -60-371
AFCRL TR-60-372
APCRL-TR-60-376
AFCRL -TR-60-422
AFCRL -TR -60-431
AFCRL TR- 60 438
AFFTC-TN-59-38
AFIT GGC-60- 1 1 »upe
AFVOC-TR-60-13
AFMDC TR-60-18
AFOSR-7
AF06R-21
AF06R-25
AFCBR-47
AFOSR-60
AFCSR-78
AF06R-U4
AF06R-115
AF06R-116
AFOSR 135
AF06R 139
AFCBR-228
AFCBR-243
AFOSR -256
AFOSR -TN-60- 162
AFt»R-TN-60-498
AFOSR TN-60 -550
AF06R-TN-«)-734
AFOSR TN-eO-735
AFOSR-TN-60-894
AFOSR-TN-60-1135
AFOSRTN-60-1146
AFOSR-TN-60-1184
AFOSRTN-60-1206
AFOSR TN-eO-1214
AFOSR TN-eO-1221
AFOSR TN-60-1223
AFOSR TN-60-1246
AFOSR TN-60-1269
AFOSR TN-60- 1303
AFOSR TN-60-1308
AFOSR TN-60- 1381
AFOSR -TN-60- 1392
AFOSR TN-60-1395
AFOSR TN-60- 1412
AFOSR -TN-60- 1480
AFOSR -TN-60- 1485
_ OSR-TN-60-1486
AFOSR -TR 60-163
AFOSR -TR- 60- 177
AFSAM-55-25
AFSAM-58-76
APSAM-5S-152
AFSAM-60-I7
Bm Humb»r
737 AFSAM-60-71
769 AFSAM-60-75
737 AFSAM-61-11
719 AFSAM-61-12
tW AFSAM-14S. R-1
712 APSAM-410. R-1
739 AFSWCTN 59-36
741 AFSWC-TR-59-34
740 AFSWC TR- 59-43
739 AOC -0290-01-2
736 AIL-4589-M-1
740 AIL-5341-TN-4
741 AIL-5791-4
739 AINA-5
736 AIR-261-59-FR-202
682 AL-2606
795 ALOSU-ieO-4
6S4 AMC TR -60-7 -257, v.l
684 AMC TR-60-7-2S7, y.2
794 AMC -TR- 60 -7 -807
SOO APGC-TR-60-65
706 APL/JHU CM-958
705 ARA-823
727 ARF-1 149-3
704 ARF D165
707 ARCaiA TN-lHlN-7
789 ARL-TN-60-17
681 ARL-TN-60-121
g04 ARL TR-60-309
803 ARC- 2
787 ARPA order 5-98
706 ARPA order -6-58. Tart 8
708 ARPA Order-26-59
705 ARPA Order 40-59. T«»k 3
799 ARTEMIS-6
789 ASRDL-2149
719 ASROL-2152
723 ASRDL-2155
726 ASIlDL-2158
726 ASRDL-2159
725 ATI -52 532
797 ATI-52 581
725 ATl-86 039
804 ATI-86 858
707 ATI- 163 038
787 ATl-207 933
705 Bell -7006- 3352 -001. v.l
755 BeU-7006-3352-001. v. 2
r»eded71S »4-3734
737 BM RI-5658
702 BN-2U
762 BM-221
804 BN-225
7M BuMed MR005. 15-0002.7,
7M R 13
897 ■iA4cd-MR005. 15-0005. 6.
701 R-6
TOO BuMed- MROOS. 15-0005. 6.
776 R-7
7n BuPeri TB-60-9
7ta BuShlpa 375-N-29
TOO CAL AF-1285-A-2
747 CAL JA-1266-S-9
782 OB Ref-60-3
686 CaiTR-21
790 CCL-99
688 CIT-21-H
761 Cooralr MP-59-053
790 CRDL SP-2-34
790 CRDLSP-4-22
772 CRDLR-3026
784 CRDLR-3033
799 CRDLR 30S0
791 CSICon-60-2
791 CU-I6-60
772 aJ-16-60
694 CU -42-60
764 CUT(RLE)-49
791 CWR-700-10
784 DAC SM-37637
gOl DACSM-37766
686 OASA-140
702 DCL-R-232
693 OMIC M-86
790 OMIC M-87
770 DMICM-89
782 DMIC-145
696 OMIC- 146
696 D»iIIC-147
695 DMIC-148
701 DMIC-149
686 DOFL TR-804
093 DOFL TR-848
090 DOFL TR-883
693 DOFL TR-902
694
690
689
690
783
738
799
747
718
718
709
707
682
740
800
749
749
712
709
699
7S7
719
783
800
772
800
778
699
7»
747
708
696
707
752
792
705
705
705
787
783
698
698
772
801
769
769
738
694
761
788
700
6S9
748
710
683
744
770
710
692
692
758
774
779
691
752
691
691
091
704
760
761
805
789
7»
788
802
T72
765
776
779
740
779
779
77t
776
776
788
722
722
802
DOftimT-l-lO 768
DrCR-240, pc 2 760
D6R-7692-3 807
DmwB-SSO 744
DrrMB-1272 721
CrrMB-1295 765
000-1404 739
Dma-1431 745
Drnira-1454 774
DTlb«-1478 745
arMB-1480 735
Drn«-1482 . y 745
I7rMB-1488 774
EDL-M226 723
EKRL-113 788
EERI.-114 804
EES-010 058M 713
EES-030 038 803
EOS-210-QL-4 788
ERPRM-16 763
BTT-801 7S0
CTT N-600 750
FA-R-1530 780
FA-T60-8-1 781
FAMD-R246A-002 710
FDRG-60-2 771
FHLTR-15 695
GA-1168 799
GA-1683 791
GCC ER -00000-56. t. I,
book 1. pt. A 726
GCC ER -00000-56. v.l.
book 2. pc. B 726
GCC ER-00000-S6. ». 1.
book 3, pc. C 726
GCC ER-00000-56, v. 2,
pu. AC 726
GBL(Electronic)E-131-F 725
(a«-2145 705
CMl-2154 705
Cram AF AFOSR-61-28.
TR-1 701
CRD RN-35 704
GWU-Tl 11/60 7S0
HEI M-828 765
HBFL-2D6 784
HH-60-84 711
HR-60-479 794
HSN-2 775
HSNP-32/ 1960 753
HiimRRO-67 683
IER-27-20 795
lER-27-21 781
IER-60-28 7M
lER-60-278 807
IER-60-286 724
IER-60-290 723
IER-60-316 724
IER-60 317 724
IER-60-321 IfC
IER-78-2 776
lER-82-14 774
ILU DCL-98 788
ILUDCL-100 774
IMM-NYU-267 761
lMM-NYU-269 761
tSMS-244 762
ISMS- 247 761
ISMS-249 762
ISMS-290 761
IST-2900-218-R 802
IST-290O-23O-R 707
ITL-A2115 742
jPC 1-58-1 747
ICAC-159A-90-1 711
L4T-373 804
LL-21C-0003, rev. 2 767
LL-21C-0024 739
LL 22G-0035 762
LL -470-0011 828
LL-53C-0051 767
LL-55C-0030 763
LL-83C-0024 795
LL-312C-0002 727
LMSD-703 005 756
LMSD-703 006 763
Marq MR-60-109 747
Microtech- 172 748
MLNYNS-5032-B-15. 40 IT
MR -N- 270 784
MSRPRR-66 807
MUPTR-162 799
NAA-MD 60-98 736
NADC-AI-5957 709
NADC-MA-6026 689
Nwnber
Page
Number
HADC-MA-6027
748
MADC-MA-6034
710
NAFI-MR-54
728
NAMC-ACEL-444
752
MAMC-AEL-1675
735
NAMT AML AE-1102
778
HA0TSTR-9-59.fr
792
HARF-60-23T
784
NAVEXOS P-1034.app. A
752
MAVORD-5904
740
NAVORD 6244
7S7
NAVORD 6611
767
NAVORD -6633
730
NAVORD-6675
756
KAVORD-6727
803
HAVORD-6741
796
NAVORD-6742
795
NAVORD-7014
694
NAVORD-7157
806
J(AVQRD-7284
753
NAVWEPS-6026
799
NAVWEFS 6182
772
NAVWEPS-6298
771
NAVWEPS-6774
757
NAVWEPS-6786
766
NAVWEPS 6848
739
HAVWEPS-7160
792
NAVWBfS-7161
730
HAVWBPS-7292
763
NAVWEPS-7565
739
NAVWEPS 7612
804
J«S-TN-lg-8
805
WS-TN-76
767
nS-TN-88
805
NCELM-030
753
HCBL M-033
715
MCBL M-035
742
NCBLM-036
714
NCELM-042
729
NCELM-04S
714
NCELM-093
736
)CBLM-074
743
NCELM-080
713
NTRI M-081
714
MCEL M-084
717
yrm u-wo
790
NCELM-096, rer.
713
NCELM-102, rer.
717
NCELM-104
714
NCELM-106
714
NCB.M-110, aufipl.
716
ICELM-113
712
NCELM-122
716
NCELM-123
745
NCELN-OOS
735
NCELN-012
747
NCELN-OIS
753
NCEL N-019
748
ICELN-021
713
NCELN-029
730
NCBLN-060
745
NCBLN-06S
781
MCELN-OTO
742
MCELN-071
729
MCELN-075
718
MCBL N-081
717
MCELN-085
747
MCELN-086
716
ICELN-106
716
NCB. N- 109
746
NCBLN-lll
758
NCBLN-I28
739
NCSLN-139
718
NCBLN-145
715
NCEL N- 149
717
NCEL N- 157
743
MCBLN-158
730
NCBLN-160
743
NCBLN-16e
751
NCa.N-171
701
HCBL N- 175
746
NCEL N-176
758
NCEL N- 195
746
NCELN-202
715
NCBLN-212
745
NCBLN-216
716
MCBL N-232
715
NCELN-240
716
NCBLN-241
716
NCELN-244
715
NCELN-249
715
NCELN-2S5
715
NCHLN-267
714
MUa,N-r6
715
IC8LN-277
744
NCEL N-281
743
NCEL N-292
746
NCBLN-297
743
NCELN-299
714
NCEL N- 300
712
NCEL N-302
729
NCEL N-319
729
NCEL N-328
781
NCEL N-333
781
NCEL N-337
716
NCELN-354
743
NCELN-3gl
785
NCELN-389
789
NCBL N-392
717
NCBLR-002
717
NCEL R-C03
729
NCEL R-007
714
NCEL R-1 10
717
NEPA-303-EMM-6
784
NEPA-354-EAM-S15
782
NEPA-368-EAM-S17,
rex 782
NEPA 39g-SCM-6
782
NEPA-406-EMM-12
782
NMOOI 058.25.02
763
NM006 01Z04.43
692
NM 006 01 2. 04. 44
692
NMC-TM-eO-63
669
NOLBRR-9
772
NOLBRR-18
768
NOU:-533
806
NOLC-537
792
NOLC-538
730
NOTS TP-2338
730
NOTTS TP-2354
767
NOrrSTP-2371
094
NOTS TF-2535
739
NOTS TP- 2567
739
NOTSTP-2610
804
NP-6712
776
NRCCLR-291
711
NRCC MD-45
729
NROC MD-46
735
NRL-5386
769
NRL-5582
778
NRL-5606
713
NRLMR-U27
730
NWL-1599
740
NWL-1726
796
OMCC-9038-OIR-2
702
OORR-1182: . . .
776
OORR-1597-. . .
763
OORR-1604:12-C
704
OORR 1863. 3-M
806
C»RR-2215. 14-M
778
OSRD-6111
713
OSURF-653, PR
701
nSllRF-691-1
701
aSURF-818
BOO
or AC LL- 59
790
OTACLL-60
790
OTACLL-61
791
arACLL-64
751
OTAC LL-65
751
OTAC LL-66
751
OTAC RR-5
790
OTAC RR-14
751
OTAC RR-17
730
OTAC RR-19
751
OTAC RR-20
751
OTAC RR 22
751
OTAC RR-31
738
Urili SB-442
681
OTS S8-447
731
errs SB 448
744
ai-S Sfl-451
753
OTS Sfl-452
777
UnS SB-453
804
OTSSB-454
777
PA TR -2658
738
n 121 784-R
692
PB147 530
686
PB 1*7 559
760
PB 147 787
807
PB 147 840
804
PB 147 841
697
PB 147 842
807
FB 147 843
807
PB 147 844
758
PB 147 847
762
PB 147 902
685
PB 147 903
665
PB 147 904
761
PB 148 005
686
FB 148 016
796
n 148 075
703
Number
PB 148 076
PB 148 077
PB 148 079
PB 148 095
PB 148 098
FB 148 212
PB 148 214
n 148 216
PB 148 219
PB 148 231
n 148 233
FB 148 313
PB 148 317
n 148 323
FB 148 332
FB 148 348
PB 148 353
n 148 394
PB 148 ■WS
PB 148 398
PB 148 400
PB 148 401
PB 148 406
FB 148 407
PB 148 415
PB 148 420
PB 148 473
FB 148 502
PB 148 516
PB 148 535
PB 148 561
FB 148 563
FB 148 747
PB 148 748
FB 148 756
PB 148 757
re 148 774
re 148 781
re 148 782
re 148 787
re 148 813
re 148 906
re 148 907
re 148 932
re 148 935
re 148 937
re 148 938
re 148 951
re 146 958
re 148 966
re 148 970
re 148 974
re 149 085
re 149 088
re 149 096
re 149 097
re 149 137
re 149 138
re 149 165
re 149 210
re 149 214
re 149 216
re 149 235
re 149 236
re 149 324
re 149 328
re 149 336
re 149 444
re 149 521
re 149 522
re 149 523
re 149 534
re 149 540
re 149 558
re 149 567
re 149 745
re 149 750
re 149 775
re 149 778
re 149 816
re 149 847
re 149 895
re 149 904
re 149 911
re ISO 006
re ISO 031
re 190 053
re 130 086-1
re 190 086-2
re 190 086-3
re 190 086-4
n 190 066-9
re 190 0S6-6
re 190 109
n 190 133
703
70S
TOO
74S
7M
737
CC7
•fW
70*
MS
771
723
7S3
m
«a
774
771
7S4
703
ns
103
70*
Ml
789
702
07
7H
76*
764
7»1
708
7*3
«•*
709
«03
7M
799
740
7M
761
761
702
791
•95
•IS
775
7M
tm
■M
716
«•»
7*9
793
793
720
76*
710
775
772
70*
733
734
M7
770
691
tt2
m
799
7M
799
T92
769
799
704
771
719
729
69*
606
799
731
TOO
797
TflS
766
7«6
76*
766
7<6
723
701
n 190 171
re ISO 198
rei90 227
re ISO 243
re 150 338
re 130 414
re 150 433
re 130 489
re 190 534
re 190 535
re ISO 545
re ISO 558
re 130 624
re 130 642
re 130 654
re 130 726
re 130 730
re 130 739
re 130 780
re ISO 792
re ISO 844
re 150 845
re 190 846
re 190 847
re ISO 848
re ISO 849
re 190 864
re ISO 866
re 150 900
re 150 901
re 150 902
re 150 903
re 150 906
re 130 908
m 130 909
re 190 910
re ISO 911
re ISO 912
re ISO 913
re 150 914
re ISO 915
re 130 916
re 150 967
re ISO 994
re 151 104
re 151 105
re 151 106
re isi 107
n 151 108
re 151 377-8
m ISI 932
re 152 004
re 152 005
re 152 006
re 152 007
re 152 008
re 152 009
re 152 022
re 151 061
re 152 114
re 152 117
re 152 135
re 152 180
re 152 199
re 152 220
re 152 957
m 152 965
re 152 980
re 153 022
re 153 036
re 153 082
re 153 120
re 153 124
re 153 163
re 153 187
re 153 207
re 153 211
re 153 295
re 153 467
re 153 486
re 153 553
re 153 558
re 153 581
re 153 582
re 153 584
re 153 594
re 153 611
re 153 619
m 153 642
re 153 647
re 153 648
re 153 655
re 153 658
re 153 662
re 153 673
784
787
806
802
688
789
685
707
803
703
794
794
774
794
692
806
695
768
778
724
757
758
726
725
706
719
786
770
724
~-718
727
735
728
783
764
722
722
720
733
731
795
683
700
761
779
779
778
776
776
805
769
750
751
790
751
751
791
738
788
807
775
•06
799
794
796
762
727
754
738
694
791
792
768
694
794
791
760
779
792
763
769
780
781
785
799
719
712
699
711
739
737
790
771
704
778
1-18
1-19
n 1S3 W3
n tsseiM
nisseM
mSS703
n 153 70S
mS3 70«
niS3 707
n IS3 713
n 1S3 714
mS3 71S
n 193 71*
It 193 717
n 193 71S
FB 193 719
n 193 730
n 193 721
n 193 7U
n 193 729
n 193 730
n 193 731
ni93 74«
n 193 790
1*193 791
ft 193 792
II 193 79*
» 193 777
n 193 781
n 193 783
n 193 784
n 193 789
FB 193 809
n 193 828
n 193 839
n 193 841
n 193 843
n 193 844
n 193 849
n 193 846
ni»3M7
nusMs
f»l93«4«
n 193 851
FB 193 899
FB 193 861
FB 133 862
FB 193M4
FBISIMS
FB193BM
FB 193 870
n 193 890
FB 193*91
IB 193 900
IB 193 903
IB 193 904
IB 193 909
IB 193 90*
IB 193 907
FB 193 90*
FB 193 911
FB 193 914
FB 193 919
FB 193 917
FB 193 919
FB 193 923
IB 193 924
IB 193 930
IB 193 936
FB 193 947
FB 194 061
IB 194 062
FB 194 063
IB 154 064
IB 194 071
IB 194 on
IB 194 078
IB194 0BO
IB 194 0*7
IB 194 0*8
IB 194 092
IB 194 094
IB 194 098
IB IM 102
IB 194 103
IB 194 114
IB 194 118
IB 194 120
IB 194 121
FB 194 123
FB 194 124
FB 194 194
IB 194 199
IB 194 196
IB 194 1S7
773
IB 194 198
773
773
FB 194 161
TV
74*
FB 194 163
TM
710
FB 194 169
774
733
FB 194 166
735
7a«
IB IM 167
T06
7M
FB 194 16*
MB
749
IB 194 169
TW
749
FB 194 198
TM
730
FB 194 199
TM
«I0
IB 194Xr7
742
707
FB 194 208
no
7W
FB 194 210
M«
W7
FB 194 213
7»
*•!
rB194 219-1
7M
730
IB 154 219-2
TM
MO
IB 194 232
TB7
7*7
IB 194 241
TU
794
IB 194 243
TM
7**
IB 194 249
713
71*
FB 194 291
«B*
737
FB 194 261
▼M
IB3
FB 194 262
«B*
7n
IB 194 263
4M
7a>
IB 194 264
«»4
77B
FB 194 269
t*5
730
FB 194 272
7»*
719
FB 194 273
M4
717
FB194 rs
70*
ITS
FB 194 281
7M
m
FB 194 289-3
7M
TV
FB 194 290-1
TM
■6
FB 194 290-2
T41
710
FB 194 303
M3
710
FB 194 349
7M
Ml
FB 194 364
25/
Ml
IB 194 370
an/
FB 194 371
ttl
IB 194 372
8M
TV
m 154 374
1B2
%
FB 154 376
IM
IB 194 412-1
TM
703
IB 194 412-2
TU
711
IB 194 427
MP
711
IB 194 438
Ml
TBV
FB 154 4«0
aa*
*n>
P« 154 447
TM
7S
IB 194 448
BM
MS
FB 194 449
BM
TIB
FB 194 4S0
TV
73*
IB 194 492
' TM
741
IB 194 493
TH
703
IB 154 494
747
732
FB 194 495
7M
«n
IB 194 496
7M
74*
IB 194 457
.; '•'
707
IB 194 ♦9*
•^ Ml
737
FB 154 469
*M
71*
IB 154 460
7«
735
IB 194 463
MB
700
IB 194 463
7n
733
IB 194 469
M«
707
IB 154 46*
tw
7«»
IB 154 479
732
774
n 194 487
7M
m
FB 154 501
732
MB
FB 154 502
722
im
IB 154 507
7M
7M
FB 154 508
aB2
737
FB 1^509
700
727
FB 154 510
M«
7BS
FB 154 518
701
M«
FB 194 523
«a2
«•«
FB 154 523
7X1
SB*
FB 154 525
721
707
FB 154 526
711
7a*
FB 194 527
70*
7M
IB 154 528
707
7*5
FB 154 529
732
7*1
IB 154 530
7B2
7*1
IB 154 531
706
7*2
n 154 532
709
7«
FB 154 533
705
7M
FB 194 935
709
7M
IB 194 536
777
737
FB 194 537
777
•N
FB 154 538
«B9
7M
FB 154 549
711
7«
FB 154 550
729
7*1
FB 154 551
707
7*2
IB 154 993
780
MO
PB 194 556
708
FB 154 562
707
TBI
FB 154 564
«•?
107
FB 154 566
706
Number
FB 194 570
FB 194 572
FB 194 578
FB 194 580
FB 194 982
FB 194 983
FB 194 989
IB 194 987
FB 194 588
FB 194 989
re 194 592
re 154 593
n 154 595
n 194 596
n 194 611
re 194 612
re 154 613
re 154 614
n 154 615
n 194 616
n 194 617
re 154 618
re 154 619
re 154 630
re 194 621
re 154 623
n 194 633
re 194 634
re 194 635
re 154 636
rei54 627
n 154 638
n 154 639
n 154 630
n 194 631
rei94 633
re 194 633
re 154 634
re 154 635
re 194 636
n 194 637
n 194 698
re 194 639
n 154 640
re 154 641
re 154 642
ni54 643
n 194 644
re 194 649
re 194 646
re 194 647
re 194 648
n 194 649
rei94 630
re 194 651
re 194 652
re 194 693
rei94 694
re 194 695
re 194 656
re 154 657
re 154 658
ni54 6S9
re 154 660
re 154 661
re 154 662
n 194 663
n 194 664
n 194 666
n 154 666
ni54 667
n 194 666
FB 194 669
FB 194 670
FB 194 671
n 194 672
FB 194 673
FB 194 674
13 194 679
FB194 676
re 154 677
re 194 678
re 154 679
re 154 680
re 154 6*1
re 154 682
re 154 683
rei54 6«9
re 194 697
rei54 700
re 154 704
re 154 706
re 154 709
n 194 716
fm
Nianter
70*
IB 154 717
770
re 154 719
7M
re 154 7»
MB
re 154 721
772
re 154 729
772
IB 154 743
Ml
IB 154 744
7M
n 194 804
739
n 194 814
TV
re 194 819
«93
re 194 816
6*7
re 194 862
6**
re 194 863
736
re 154 864
726
re 194 865
7*1
re 154 868
7*1
re 154 869
714
re 194 870
714
re 154 871
713
re 154 872
749
re 154 873
717
re 154 874
739
re 154 875
714
re 154 955
793
re 154 956
719
n 194 997
743
re 194 998
714
re 194 959
739
re 154 960
714
re 154 961
736
re 155 029
743
re 155 030
713
rei55 058
714
IB 199 099
717
re 199 060
790
n 199 061
719
FB 195 062
717
n 195 068
739
FB 199 073
747
re 195 079
793
rei99 080
74*
m 199 061
713
re 199 082
730
re 199 083
749
n 195 084
781
re 159 085
743
n 199 086
739
n 199 087
718
re 199 0*8
717
IB 195 0*9
747
n 155 690
716
ni55 144
716
FB 199 149
746
n 199 146
79*
n 199 147
729
n 199 148
718
n 195 149
719
n 199 150
717
n 193 191
743
n 195 192
790
re 199 193
743
re 199 194
791
n 199 199
701
re 195 156
74*
re 159 157
75*
re 199 159
746
re 159 160
715
re 155 239
74S
re 155 240
716
re 155 241
719
re 155 242
716
re 199 250
716
re 199 251
715
n 195 292
715
re 195 253
715
re 155 254
714
re 155 255
715
re 155 256
744
re 155 257
743
re 155 258
746
re 155 259
743
re 155 260
714
re 155 296
712
re 155 297
729
re 155 330
729
re 155 321
716
re 195 322
716
re 195 323
743
n 199 324
7*5
re 195 349-
717
FB 159 374
783
re 195 375
784
re 155 376
700
re 155 381
755
n 199 382
7*2
757
803
75*
735
709
710
728
730
771
772
773
7*3
717
106
101
749
771
774
M*
713
710
731
731
76*
701
764
763
721
809
743
741
743
741
741
KM
729
730
772
803
75*
756
735
795
712
763
763
704
70*
7*9
740
710
7X)
740
747
779
733
732
776
7*8
7**
79*
79*
719
728
794
794
799
795
742
7J7
737
744
783
710
796
719
718
732
734
740
«*9
7r
739
784
100
782
748
m
ttn
765
792
7r
1-20
Wanbw
IB 195 3*3
1*193 384
11195 385
IB 195 386
11195 413
IB 199 414
IB 195 428
IB 199 429
Fl 155 431
11199 432
IB 155 437
IB 195 438
IB 195 493
(B 199 486
IB 195 565
11155 566
n 155 567
H 155 566-1
IB 155 568-2
1*155 568-3
11155 569-1
H 155 572
n 155 573
Ft 155 574
II 155 575
ni5SS76
11155 577
n 155 578
IB 155 618
11161 236
IB 161 237
IB 161 239
IB 161 371-1
ni*i 37i-i:
11161 577
IB 161 5*9
IB 161 914
IB 161 915
H 171 112
H 171 195
IB 171 188
ni71 247
IB 171 248
(1 171 249
ni71 290
II 171 251
n 171 252
ni71 253
11171 294
nni 295
IB 171 296
nni 257
IB 171 258
IB 171 318
11171 330
IB 171 384
IB 171 479
IB 171 919
IB 171 999
IB 171 563
IB 171 564
nni 565
nni 966
n 171 567
nt71 568-1
n 171 568-2
nni 569
ni71 570
ni71 S7I
747
735
796
799
744
74*
784
782
782
783
792
793
696
689
713
746
736
726
736
736
736
757
788
690
6*6
693
731
769
732
776
779
740
692
693
767
805
709
709
749
699
778
736
736
736
736
744
756
778
792
702
738
735
765
808
758
777
713
ao7
802
*97
777
753
731
•04
74*
74*
7»6
Wo
wo
Ntxniier
n 171 572
7*4
re 171 573
799
re 171 574
694
re 171 575
699
re 171 578
797
re 171 579
757
re 171 580
764
re 171 582
732
re 171 593
770
re 171 594
711
n 171 595
794
re 171 396
781
re 171 997
779
re 171 598
796
re 171 599
711
re 171 600
688
n 171 601
682
n 171 602
690
re 171 604
770
re 171 605
740
n 171 606
688
re 171 607
688
re 171 608
691
n 171 609
718
re 171 610
685
ni7i 611
682
re 171 612
753
re 171 613 .
re 171 614 •
750
709
re 171 616
783
re 171 618
801
re 171 619
802
n 171 630
802
re 171 664
768
re 171 685
757
re 171 686
739
n 171 667
763
re 171 688
793
re 171 689
681
re 171 690
730
re 171 691
730
PCE-R-6901A
731
IMlco 22t8-F
731
RB-564
728
PIB-629
728
PIB-647
728
PIBAL-628
772
PIBMRI-636-57
738
FIBMRI R-701-58
728
PIBMRI R-719-59
728
PUnna P-IFR039-5709
748
PLPR-58C
804
PLPR-59A
697
FOLyRDC-9.04
732
Pro). 9R38-01-015
709
PSNS-ML-E-412-8.fr
798
TV AEL-510
772
RJ AKL-523
772
FU ABL-93*
772
R60SD4I7
773
R60SD439
773
R60SD487
804
RADC-TN-58-70
732
RADC-TN-58-183
732
RADC-TN-58-353
718
RAOC-TN-99-33
728
RADC-TN-59-83
724
RADC-TN-59-157
808
RAnr-TN-59-183
728
Number
RADC-TN-99-294
718
RADC-TR-99-3
739
RADC-TR -59-27
6*3
RADC-TR -59-62
729
RADC-TR-99-77
783
RADC-TR-99-llO.v.
1
763
RADC-TR -59-1 10, V.
2
766
RADC-TR-99-110,».
3
766
RADC-TR-99-110,».
4
766
RADC-TR -99-1 10. ».
5
766
RADC-TR -59- 110.*.
6
766
RADC-TR -59- 124
727
RADC-TR-99-128
799
RADC-TR-59-142
764
RADC-TR-59-144
733
RADC-TR -59- 159
722
RADC-TR-59-160
722
RADC-TR -59- 170
730
RADC-TR -59- 179
731
Ray S-210
797
RCASC-R-1-98
732
RCASC-R-9-57
7tt
RIAL 53-3762
736
RL/JHU/AF-53
764
RL/IHU/AF-57
763
RLESAST-4435-109-61U
773
RLT-29B
699
Rocket R- 1962-1
741
Rocket R -2396, v. 1
740
Rocket R -2396. ▼. 2
741
RPI MachRe(>-39
779
RS-18
799
RW-RL-186
7«
SaDTR-60-37
.711
SELTR- 104-9
1 BM
SELTR-361-1
73*
SELTR-401-2
734
SBLTR-1506-1
7M
SELTR-1953-1
M*
SBL TR-2002-1
7M
SELTR -2103-1
734
SIORef -60-11
707
Squid M1CH-6-P
■a
S<Jiil<1UVA-l-P
TD3
SRI-2494
7M
SRI-2697
787
SRI-2994
708
STL/rR-«)-<XK)0-94316
800
STL/TR-60-00n0-CR303
800
STL/TR-60-O000-GR413
800
STL/TR -60-(KXX»-NR396
797
SUDAER-97
797
SwRI EE-384
752
TA*4C Ref-60-19T
707
TED ADC AE-70001
709
TED NAM AE 4110, pc 14
778
TED NAM AE -42222.
PL3
793
TREC-60-43
711
TRBC-60-99
711
T»BC-eO-67
7U
TRBC-60-6e
TM
TRBC-61-2
7M
TRBC-61-3
TM
TRBC-61-7
7M
UCLA DE-99-34
712
UCLA DE -60-39
7»
UCLA DE-60-37
71*
UCLA DB-60-50
IM
UCLA DB-60-52
7M
Number
UMRI-r23
n*
UMRI-2790-9-T
727
UMRI-2755
806
UMRI-3794-6-T
806
UMRI-r94-7-T
806
UMRI-2830-5-P
722
UMRI-3894-8-P
722
UMRI-03105
n6
UMRI -09114
775
UMRI-03114
792
USNRn.-TR-3«9
785
USNRDL-TR-385
783
USNROL-TR-409
783
Vitro- 233 1-2-99
741
WADC-TN-S7-287
769
WADC-TN-58-256
785
WADC TR-52-184,
•iVpl. 5
710
WADC TR-54-587
778
WAnr-TR-59-29, pt. 6
730
WADC-TR-98-669
770
WADC-TR-59-130
787
WADC -TR- 59- 189(1)
748
WADC -TR -59-742
726
WADD-TN-59-344
710
WADD-TN-60-76
770
WADD-TN-60-281
788
WADD-TR-99-743. ». 1,
honk 1
726
WAOn-TR -99-743. v. 1,
hnnk 2
72*
WADD-TR-99-745, ». 1.
book 3
726
WADD-TR -59-743. ». 2.
pu. A-C
WAPO-TR -60-96. pt. 1
726
801
WADD-TR -60-56. pt. 2
802
WADD-TR-60-56. pt. 3
802
WADD-TR -60-57
756
WADD-TR-60-161. pc 1
711
WADD-TR -60- 260
740
WADD-TR -60- 263
756
WADO-TR-60-304
754
WADD-TR-60-344
781
WADD-TR-60-427
754
WADD-TR -60-433
708
WADO-TR-60-451
775
WADD-TR -60-534
796
WADD-TR-60-590
711
WADD-TR-60-598
6B*
WADD-TR-eO-600
765
WADO-TR-60-eOl
682
WADO-TR-60-617
690
WAr)O-TR-60-633
688
WADO-TR -60-660
6*8
WADD-TR -60-662
691
WADD-TR -60-674
711
WAnO-TR-60-745
6*5
WADO-TR-60-748
6*2
WAL-311/45
777
WAL-397/lO
757
WAL-401. 94/1
7M
WAL -732/114-1
742
WAL-733/114-3
741
WAL-733/114-9
742
WAL -733/ 11 4-7
741
WAL -732/ 133
741
WC-2D00-11
712
WC D-133309-(l-«
712
WVT RI-9904
777
WVT-RI-«101-1
7M
ZTB-131
MB
1-21
'>!'
U. S. DEPARTMENT OF COMMERCE FIELD OFFICES
SERVE THE BUSINESS COMMUNITY
The Department of Commerce maintains Field Offices to enable the business community to
avail itself l(Kally of Government facilities designed to promote commerce. Working closely with
various units in the Department and, when necessary, with other Government agencies, the Field Offices
provide business services to manufacturers, wholesalers, retailers, trade publications, trade associa-
tions, advertising agencies, research groups, financial institutions, and exporters and importers.
Experienced personnel will gladly assist in the solution of specific problem.s, explain the scope
and meaning of regulations administered by the Department, and provide practical assistance in the
broad field of domestic and foreign commerce. Field offices act as official sales agents of the Super-
intendent of Doruments. and maintain an extensive business reference library containing periodicals,
directories, publications and reports from official as well as private sources.
Amonq the many ser\-ices which businessmen have found of value arc:
PRODUCTION
• Modernization of plant processes and other tech-
nological aids
• Development of new products
• Government-owned patents for free license
• Commodity standards
FOREIGN TRADE AND INVESTMENT
• lariff and exchange regulations
• Import and export quotas, liceruing regulations
• Statistics on imports and exix>rts
• Investment and trade opportunities abroad
• Economic conditions in foreign countries
GENERAL
• .Manai<ement and business aids
• Establishing a new business
lASiC ECONOMIC DATA
• Census data, with national and often State and
regional breakdowns, on manufacturing, wholesal-
ing, retaiiint;. service industries, employment and
unemployment, population, housing, agri<ulture
• Basic records of national income and product,
regional trends, balance of payments, foreign aid
MARKETING AND DISTRIiUTION
• Development and maintenance of markets
• Distribution channels, facilities and services
• Marketing and distribution statistics
COOPERATIVE OFFICES
I o make the services of the Department of Commerce more widely available, agreements
have been entered into with more than 750 Chambers of Commerce. Manufacturers Associatioas,
and similar busines.s groups under which these organizations have become official Cooperative Offices
of the Department. If specific information is not on hand in the Cooperative Office, your problem will
be referred to the nearest Departmental field office.
Department Field Offices
AUHMUMrqiM, N. M«l., U. a OoufthouM. Phooc: CHatwl
7-0311.
Atluta S. Oa.. «H Voliiialw> Side.. M LuckU m.. N«.
JAckson >4121.
BcHrton 10. Mua.. Room 230. M Pedanl tt. CApltol
VM12.
Bunslo 3. N. v., MM Pwicral Bldt., 117 Elllcoa M.
TL H21*.
Charlciton 4, 8.C., Area 2. S«i»ant J*sp« Bldg.. West
End Bfoad S. Phoiw: RAjraoad >Tni.
ChtiMuw. Myo.. 307 Ma)«stic Bldi., igth 81. and Capltot
A»«. Phone: 634-2731.
Chicaco «. 111.. RooB 1302, 2M W, Jackaon Bl*d.
ANdom >3a00.
Clnrlnnall 2.OM0. S09 Plfth TMrd Bank Bide.. 3« East
Pooth 8t>«««. DUnbai 1-2300. Eit. 344.
Clcralaad 1, OMo. Pedmal Rasatve Bank Bide.. E. Sth
m. aid Mpwlor Av*.. CH«it7 1-7000.
Dallaa l.Tai., Room 3-104 MMCltandUe Mart. Rlwaidc
•-S611.
DaaTO 2. Colo., 142Nr«CuatoRihouae. KE]rBtonc4-41Sl.
I>««rott M. Mich.. 43t Paderal Bid*. WOodwafd 9-9330.
to, H. C, 407 U. S, Poat omcc Bld«. Phone:
dwaj 3-1234.
)2.Tei.,eiOScanlanBldf.. 403 Main S. CApltol
>7301.
JackaoovUla 1. PU.. 425 Padaral Bid*.. KL*la4-Tlll.
Kanaaa Cltjr •. Mo.. Hooa XI 1. Oil Watoirt K. BAU-
aiore 1-7000.
Loa Aatetea IS,CaU(.. Rooa 4M. 1031 S. Bnmimms.
RIclMoad 0-4711.
Maaphla 3, Tena,, 212 Tails Bld(. JAckaoo 0-S4at.
Mtaai 32, Pla.. 40* Alnalay Bid*.. 14 N,C. Pint Ava.
PRaakila 7-2M1.
MInoeapulla I. Minn., 304 Pederal Bld(„ 110 80. Fourth
a. PEMetal >3211.
Ne« Otlaaaa 13, La., 333 a. Charles Ave. 520-3411.
New York l,N.Y.,EivlieaateBkl(. LOn«actc 3-3377.
Philadelphia 7- Pa., Jafleraoo Bld«.. 1015 Chaatnut a.
WAlBUl 9-2400.
Phocnli, Aflz., 137 N. Oacond Atc. ALplna 0-6051.
PIttabiBfh 22. Pa., 107 Hith a. ORant 1-S370.
Portland 4. Oiec., 217 Old U.S. Cotjrthouas*P.aBld(.
CApltol 0-33« .
Rano. NeT.. 147> Valla Ave. Phoaa: ytltt.
Rlchmofld 10. Vs.. 300 Parcel Poat Bldi. MTltoa 4-0471.
a. Louis 1. Mo., 910 New Psdetal Bld(. MAId \-SI00.
Salt Lake cut, l.Utafc, 222SW, TeaipIeaT. EMpUe4-2SS2.
Ban Praoclaeo ll,Callf..RaoB 419Cuatoaihouae. YUkoa
•-311I.
Savannah. Oa.. 236 U. 8. Courthouaa aBd<P. O. Bide
ADama >4755.
Baattle 4, Wsati.. 809 Padaral Odlce Bldf., OOOPVat
*6. Minual >3300,
For local trlpph^ne listinic, coniuh ^rrticn devoted to U, S..Cfiyrrnincnt
I..
jNiTED States
Government Printing Office
division of public documents
w4sHINGTON 25, O. C.
PCNALTT rOH PHIVATl U*C TO ««
rATMCNT or M>*T*o<. taoe
t
ICIAL BUSINESS
, -^^
V-
OTS Announces . • ♦
NEW LITERATURE SEARCHING SERVICE
FOR SCIENCE AND INDUSTRY
In response to public requests for "toilof mode" bibliographies of technical in-
formation suited to the doy-to^oy a, well as l«>ng-range r*<^}j^^r..nU of scien-
tists engineers, ond technical administrators, the Office of Techn cal Services,
!n cVp^IJotion ;ith tfie Science ond Technology Division of the Library of Con-
gress, has established a fast, inexpensive program of **V''^*''9.!r?:"°lZa^jTr
?ific and technical literature sources. A fee of $8 per hour will be charged for
searches.
"TAILOR-MADE SEARCHES"
According to the desires of the requestor, searches -* « ' l** -«J» '^/j^^; ^^,^^
the Office of Technical Services collection and the Librory of Congress collec
tion to the extent specified. Two types of searches are offered:
• C^irt Awf-.. Bibllogr-phy 5*'^«<«--'^»'* P"''^"/Vn U'!7di?ba*sil*'
keep the subscriber obreost of new literature m his field on a P«"0«'.'f *;»•'* '
Ue subscriber outlines the generic and specific sub.ect fields in "^^ich h. ^
interested, and at intervals prescribed by him (1 month. 3 months etc.) he r^
cervT. r^f^rence. to pertinent reports, periodical articles, technical papers, and
other moteriols accumulated during the period.
• Retrospective Bibllogrophy Servlce.-The requestor is furnished a bibliog-
raphT^f^atlHol avo^kible at the time of the r^uest and in accordance w.jj,
literoture dates and other limitations OSS igned by him.
THE COLLECTIONS
• OHice of Teck-lcal Servlce....-OTS has a collection of some 200,«)0 ♦•chni-
cal documents which is growing constantly and contain. '•»><''♦• ^r**^;"^^^^
search by or for the Army. h4avy. Air Force, Atomic Energy Commi.«.on and
oSer agencies of the Federal Government; translations of ^•',?" ♦•/j"""' ''*■
eroture; and U. S. Government-owned potents available for license.
• Scie.ee end TecKnele,y DItI.I-, Lib«iry •♦ Cengf ..—The «ci«n" "!••'=-
tion. of the Library of Congress, which ore preeminent in many <nsciplines,
c^^ broodly the Jorld out^t of literature in all major fiefds of science ond
technology.
For ^itional information ^J searcl. request forms writt, to OTS. U. S. Depart-
.Tienr of CoTmerce, Waaliington 25, D. C.
'ni-
RESOLUTION CHART
100MILLIMITIIS
INSTRUCTIONS Resolution is expressed in terms of the lines per millimeter recorded by a particular
film under specified conditions. Numerals in chaVt indicate the number of lines per millimeter in adjacent
"T-shaped" groupings. « \ \ t , t v ■ v
In microfilming, it is neccMary to determine the reduction ratio and multiply the number ot Imes m the
chart by this value to find the number of lines recorded by the film. As an aid in detenmimng the reduction
ratio, the line above is 100 millimeters in length. Measuring this line in the film image and dividmg the lejigth
into 100 gives the redyction ratio. Example: the line is 20 mm. long in the film image, and 100/20 _ i.
Examine "T-shaped" line groupings in the film with microscope, and note the number adjacent to finest
lines recorded sharply and distinctly. Multiply this number by the reduction factor to obtain resolving power
in lines per millimeter. Example: 7.9 group of lines is clearly recorded wWle lines m the 10.0 group are
not distinctly separated. Reduction ratio is 5. and 7.9 x 5 = 39.5 lines per millinrieter recorded satisfacto-
rily. 10.0 X S = 50 lines per millimeter which are not recorded satisfactorily. Under the particular condi-
tions, maximum resolution is between 39.5 and 50 lines per millimeter.
Resolution, as measured on the film, is a test of the entire photographic system, including lens, exposure,
processing, and other factors. These rarely utilize maximum resolution of the film. y>t>"t.ons during
exposure, lack of critical focus, and exposures yielding very dense negatives arc to be avoided.
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