| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000cam a2200000Ia 4500 |
| 001 |
in00002761513 |
| 005 |
20211120165755.0 |
| 006 |
m d f |
| 007 |
cr cn||||||||| |
| 008 |
120515s2011 vaua obt f000 0 eng d |
| 035 |
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|a (OCoLC)ocn793644818
|
| 040 |
|
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|a GPO
|c GPO
|d MvI
|d UtOrBLW
|
| 049 |
|
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|a WWW
|
| 074 |
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|a 0830-D (online)
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| 086 |
0 |
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|a NAS 1.15:2011-217308
|
| 245 |
0 |
0 |
|a Design, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners /
|c David Havens [and others].
|
| 264 |
|
1 |
|a Hampton, Va. :
|b National Aeronautics and Space Administration, Langley Research Center,
|c [2011]
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| 300 |
|
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|a 1 online resource (43 pages) :
|b color illustrations
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| 336 |
|
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|a text
|b txt
|2 rdacontent
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| 337 |
|
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|a computer
|b c
|2 rdamedia
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| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
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|a NASA/TM ;
|v 2011-217308
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| 500 |
|
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|a Title from title screen (viewed on Mar. 15, 2012).
|
| 500 |
|
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|a "November 2011."
|
| 504 |
|
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|a Includes bibliographical references (page 28).
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| 536 |
|
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|d L-20097
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| 536 |
|
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|h 561581.02.08.07.15.15
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| 500 |
|
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|a Electronic resource.
|
| 650 |
|
7 |
|a Design optimization.
|2 nasat
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| 650 |
|
7 |
|a Load tests.
|2 nasat
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| 650 |
|
7 |
|a Tolerances (mechanics)
|2 nasat
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| 650 |
|
7 |
|a Panels.
|2 nasat
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| 650 |
|
7 |
|a Stiffening.
|2 nasat
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| 650 |
|
7 |
|a Curvature.
|2 nasat
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| 650 |
|
7 |
|a Loads (forces)
|2 nasat
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| 700 |
1 |
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|a Havens, David.
|
| 710 |
2 |
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|a Langley Research Center.
|
| 830 |
|
0 |
|a NASA technical memorandum ;
|v 217308.
|
| 856 |
4 |
0 |
|u https://purl.fdlp.gov/GPO/gpo22684
|t 0
|
| 999 |
|
|
|a MARS
|
| 999 |
f |
f |
|s 5bb3ad78-c600-36da-95c2-ca9ffb7b48da
|i ed45b493-669c-3c3a-8b78-aed94ea7dabc
|t 0
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|s www_evans
|d Available Online
|t 0
|e NAS 1.15:2011-217308
|h Superintendent of Documents classification
|
| 998 |
f |
f |
|a NAS 1.15:2011-217308
|t 0
|l Available Online
|