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Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 : test dates: 19-21 November 2008 / / Mark W. Hilburger, W. Allen Waters, Jr., Waddy T. Haynie
| Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 : test dates: 19-21 November 2008 / / Mark W. Hilburger, W. Allen Waters, Jr., Waddy T. Haynie |
| Autore | Hilburger Mark W (Mark William) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 |
| Descrizione fisica | 1 online resource (viii, 61 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Buckling
Axial strain Critical loading Performance tests Structural analysis |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 |
| Record Nr. | UNINA-9910704016403321 |
Hilburger Mark W (Mark William)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Finite element analysis and test results comparison for the hybrid wing body center section test article / / Adam Przekop [and three others]
| Finite element analysis and test results comparison for the hybrid wing body center section test article / / Adam Przekop [and three others] |
| Autore | Przekop Adam |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 |
| Descrizione fisica | 1 online resource (viii, 106 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Critical loading
Finite element method Strain measurement Structural stability Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706249303321 |
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Przekop Adam
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Soggetto topico
-
Critical loading
(2)
- Axial strain (1)
- Buckling (1)
- Finite element method (1)
- Performance tests (1)