Compression response of a sandwich fuselage keel panel with and without damage
By: David M. McGowan and Damodar R. Ambur.
Contributors: Ambur, Damodar R.; Langley Research Center.
Series: NASA technical memorandum -- 110302.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Subjects: Sandwich structures; Graphite-epoxy composites; Composite structures; Finite element method; Fuselages; Honeycomb cores; Impact damage
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 97-0681-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.