Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009 / Mark W. Hilburger [and three others].
Saved in:
| Online Access: |
Online Access Online Access |
|---|---|
| Main Author: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Hampton, Virginia :
National Aeronautics and Space Administration, Langley Research Center,
March 2017.
|
| Series: | NASA technical publication ;
2017-219587. |
| Subjects: |
MARC
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| 245 | 1 | 0 | |a Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : |b test dates: 3-6 February 2009 / |c Mark W. Hilburger [and three others]. |
| 264 | 1 | |a Hampton, Virginia : |b National Aeronautics and Space Administration, Langley Research Center, |c March 2017. | |
| 300 | |a 1 online resource (x, 91 pages) : |b color illustrations. | ||
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| 504 | |a Includes bibliographical references (page 80) | ||
| 513 | |a Technical publication. | ||
| 588 | |a Description based on online resource; title from PDF title page (NASA, viewed July 11, 2017) | ||
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| 650 | 7 | |a Buckling. |2 nasat | |
| 650 | 7 | |a Compression loads. |2 nasat | |
| 650 | 7 | |a Cylindrical shells. |2 nasat | |
| 650 | 7 | |a Launch vehicles. |2 nasat | |
| 650 | 7 | |a Aluminum alloys. |2 nasat | |
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