Compression response of a sandwich fuselage keel panel with and without damage / / David M. McGowan and Damodar R. Ambur
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| Autore: |
McGowan David M.
|
| Titolo: |
Compression response of a sandwich fuselage keel panel with and without damage / / David M. McGowan and Damodar R. Ambur
|
| Pubblicazione: | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 1997 |
| Descrizione fisica: | 1 online resource (33 pages) : illustrations |
| Soggetto topico: | Composite structures |
| Finite element method | |
| Fuselages | |
| Graphite-epoxy composites | |
| Honeycomb cores | |
| Impact damage | |
| Sandwich structures | |
| Persona (resp. second.): | AmburDamodar R. |
| Note generali: | "February 1997." |
| "Performing organization: NASA Langley Research Center" Report documentation page. | |
| Nota di bibliografia: | Includes bibliographical references (pages 13-14). |
| Titolo autorizzato: | Compression response of a sandwich fuselage keel panel with and without damage |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910707910803321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |