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Record Nr. |
UNINA9910707910803321 |
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Autore |
McGowan David M. |
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Titolo |
Compression response of a sandwich fuselage keel panel with and without damage / / David M. McGowan and Damodar R. Ambur |
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Pubbl/distr/stampa |
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Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997 |
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Descrizione fisica |
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1 online resource (33 pages) : illustrations |
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Collana |
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NASA technical memorandum ; ; 110302 |
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Soggetti |
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Composite structures |
Finite element method |
Fuselages |
Graphite-epoxy composites |
Honeycomb cores |
Impact damage |
Sandwich structures |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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"February 1997." |
"Performing organization: NASA Langley Research Center" Report documentation page. |
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Nota di bibliografia |
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Includes bibliographical references (pages 13-14). |
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