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| Autore: |
Castner Raymond S
|
| Titolo: |
Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009
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| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica: | 1 online resource (10 pages) : illustrations |
| Soggetto topico: | Wind tunnel tests |
| Supersonic aircraft | |
| Aerodynamic configurations | |
| Low cost | |
| Supersonic wind tunnels | |
| Wind tunnel models | |
| Sonic booms | |
| Static pressure | |
| Pressure sensors | |
| Exhaust nozzles | |
| Note generali: | Title from title screen (viewed on Oct. 7, 2010). |
| "April 2010." | |
| "AIAA-2009-5369." | |
| Nota di bibliografia: | Includes bibliographical references (page 10) |
| Titolo autorizzato: | Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles ![]() |
| Formato: | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910699547103321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |