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Last edited by callison59
September 14, 2019 | History
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David M. McGowan

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

    First published in 1997 — 2 editions
    Not in Library

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Subjects

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

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ID Numbers

  • OLID: OL4883477A

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History

Download catalog record: RDF / JSON
September 14, 2019 Edited by callison59 Edited without comment.
September 20, 2008 Created by ImportBot Imported from Oregon Libraries MARC record