An edition of Compression response of a sandwich fuselage keel panel with and without damage (1997)

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

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Compression response of a sandwich fuselage k ...
David M. McGowan, David M. McG ...
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Last edited by WorkBot
January 20, 2010 | History
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An edition of Compression response of a sandwich fuselage keel panel with and without damage (1997)

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

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Publish Date
Publisher
National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
Language
English

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Subjects

Fuselages, Graphite-epoxy composites, Honeycomb cores, Sandwich structures, Impact damage, Composite structures, Finite element method

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Cover of: Compression response of a sandwich fuselage keel panel with and without damage
Compression response of a sandwich fuselage keel panel with and without damage
1997, National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
in English
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Cover of: Compression response of a sandwich fuselage keel panel with and without damage
Compression response of a sandwich fuselage keel panel with and without damage
1997, National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
Microform in English

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Book Details

Edition 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.

Published in
Hampton, Va, [Springfield, Va
Series
NASA technical memorandum -- 110302.

The Physical Object

Pagination
1 v.

ID Numbers

Open Library
OL17806199M
OCLC/WorldCat
37496094

Source records

Oregon Libraries MARC record

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January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page