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|a NAS 1.15:2016-218973
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|a Online Government Document
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1 |
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|a Przekop, Adam,
|e author.
|
| 245 |
1 |
0 |
|a Finite element analysis and test results comparison for the hybrid wing body center section test article /
|c Adam Przekop [and three others].
|
| 264 |
|
1 |
|a Hampton, Virginia :
|b National Aeronautics and Space Administration, Langley Research Center,
|c April 2016.
|
| 300 |
|
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|a 1 online resource (viii, 106 pages) :
|b color illustrations.
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|a text
|b txt
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|a computer
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|a online resource
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|a NASA/TM ;
|v 2016-218973
|
| 500 |
|
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|a "April 2016."
|
| 500 |
|
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|a "Performing organization: NASA Langley Research Center"--Report documentation page.
|
| 504 |
|
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|a Includes bibliographical references (pages 104-105).
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| 513 |
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|a Technical memorandum.
|
| 536 |
|
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|a Sponsored by the National Aeronautics and Space Administration
|h 338881.02.22.07.01.01
|
| 536 |
|
|
|d L-20629
|
| 588 |
|
|
|a Description based on online resource; title from PDF title page (NASA, viewed Oct. 18, 2017).
|
| 650 |
|
7 |
|a Critical loading.
|2 nasat
|
| 650 |
|
7 |
|a Finite element method.
|2 nasat
|
| 650 |
|
7 |
|a Strain measurement.
|2 nasat
|
| 650 |
|
7 |
|a Structural stability.
|2 nasat
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| 650 |
|
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|a Wings.
|2 nasat
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| 710 |
2 |
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|a Langley Research Center,
|e issuing body.
|
| 830 |
|
0 |
|a NASA technical memorandum ;
|v 2016-218973.
|
| 856 |
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0 |
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|c 03-20-18
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|a Middle Tennessee State University
|b Main
|c James E. Walker Library
|d Electronic Resources
|t 0
|e NAS 1.15:2016-218973
|h Library of Congress classification
|
| 856 |
4 |
0 |
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|u https://purl.fdlp.gov/GPO/gpo85619
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|
