Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
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| Autore: |
Asbury Scott C.
|
| Titolo: |
Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
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| Pubblicazione: | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999 |
| Descrizione fisica: | 1 online resource (134 pages) : illustrations |
| Soggetto topico: | Exhaust nozzles |
| Porosity | |
| Hole geometry (mechanics) | |
| Cavities | |
| Thrust vector control | |
| Persona (resp. second.): | HunterCraig A (Craig Allen) |
| Note generali: | "August 1999." |
| "Performing organization: NASA Langley Research Center"--Report documentation page. | |
| Nota di bibliografia: | Includes bibliographical references (pages 19-20). |
| Titolo autorizzato: | Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910706145403321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |