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

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

By David M. McGowan

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Publish Date

1997

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

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