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| LEADER |
00950nam a2200265 a 4500 |
| 001 |
c000118861 |
| 003 |
CARM |
| 005 |
20010731110336.0 |
| 008 |
921029s1952 nyu 000 0 eng d |
| 019 |
1 |
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|a 9651648
|5 LACONCORD2021
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| 035 |
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|a (OCoLC)2083130
|5 LACONCORD2021
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| 040 |
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|a TU
|b eng
|c TU
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| 082 |
0 |
4 |
|a 629.1341
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| 082 |
0 |
4 |
|a 629.141*
|
| 100 |
1 |
|
|a Shanley, Francis Reynolds,
|d 1904-
|
| 245 |
1 |
0 |
|a Weight-strength analysis of aircraft structures :
|b The Rand Corporation.
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| 250 |
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|a 1st ed.
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| 260 |
|
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|a New York, McGraw-Hill, 1952,
|c 1952.
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| 300 |
|
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|a xi, 394 p. diagrs. 24 cm.
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| 440 |
|
4 |
|a The Rand series
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| 500 |
|
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|a Includes bibliographies.
|
| 650 |
|
0 |
|a Airplanes
|x Design and construction.
|
| 852 |
8 |
|
|b CARM
|h A2:AL09E0
|i C05001
|p 0201984
|f BK
|
| 999 |
f |
f |
|i d4399b38-da66-5ab2-bfc6-582e4d4884e4
|s c975d057-c5d5-5c01-9f4a-fb28a7a2c28a
|
| 952 |
f |
f |
|p Can circulate
|a CAVAL
|b CAVAL
|c CAVAL
|d CARM 1 Store
|e C05001
|f A2:AL09E0
|h Other scheme
|i book
|m 0201984
|