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Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others]

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Bibliographic Details
Online Access:	Online Access Online Access
Main Authors:	Myers, David E. (Engineer) (Author), Pineda, Evan J. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013-2014.
Series:	NASA technical memorandum ; 217822. NASA technical memorandum ; 2014-217822.
Subjects:	Fibrous composites. Finite element method. Honeycomb structures. Ares 5 cargo launch vehicle. Epoxy matrix composites. Fiber composites. Robustness (mathematics) Sandwich structures. Technical reports.

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Call Number:	NAS 1.15:2013-217822/PT.1-2
NAS 1.15:2013-217822/PT.1-2	Available