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
Format: Microform
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.