Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack
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| Autore: |
Mack Robert J.
|
| Titolo: |
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack
|
| Pubblicazione: | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 |
| Descrizione fisica: | 1 online resource (15 pages) : illustrations |
| Soggetto topico: | Aerodynamic characteristics |
| Body-wing configurations | |
| Nacelles | |
| Sonic booms | |
| Wings | |
| Aerodynamic configurations | |
| Supersonic flight | |
| Aerodynamic noise | |
| Noise reduction | |
| Wind tunnel tests | |
| Note generali: | "December 1999." |
| "Performing organization: NASA Langley Research Center"--Report documentation page. | |
| Nota di bibliografia: | Includes bibliographical references (pages 13-15). |
| Titolo autorizzato: | Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910706143703321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |