Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel /

Bibliographic Details

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.
Subjects:	Fibrous composites. Finite element method. Honeycomb structures. Ares 5 cargo launch vehicle. Epoxy matrix composites. Fiber composites. Robustness (mathematics) Sandwich structures. Technical reports.
Online Access:	https://purl.fdlp.gov/GPO/gpo51535 http://purl.fdlp.gov/GPO/gpo51535