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Author:
McGowan David M.
Title:
Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.
Format:
[microform] /
Publisher:
National Aeronautics and Space AdministrationLangley Research Center ;
Copyright Date:
1997
Description:
1 v.
Reproduction Info:
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Subject:
Sandwich structures.
Graphite-epoxy composites .
Composite structures.
Finite element method
Fuselages.
Honeycomb cores.
Impact damage.
Other Authors:
Ambur, Damodar R.
Langley Research Center
Notes:
Distributed to depository libraries in microfiche. Shipping list no.: 97-0681-M.
Series:
NASA technical memorandum 110302
OCLC:
(OCoLC)37496094
Locations:
USUX851 -- Iowa State University - Parks Library (Ames)

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