Compression response of a sandwich fuselage keel panel with and without damage /

Bibliographic Details

Main Authors:	McGowan, David M. (Author), Ambur, Damodar R. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
Series:	NASA technical memorandum ; 110302.
Subjects:	Composite structures. Finite element method. Fuselages. Graphite-epoxy composites. Honeycomb cores. Impact damage. Sandwich structures.
Online Access:	https://purl.fdlp.gov/GPO/LPS72357