Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20
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| Autore: |
Castner Raymond S
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| Titolo: |
Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20
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| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica: | 1 online resource (16 pages) : color illustrations |
| Soggetto topico: | Exhaust nozzles |
| Nozzle flow | |
| Plumes | |
| Supersonic aircraft | |
| Computational fluid dynamics | |
| Nozzle geometry | |
| Pressure ratio | |
| Shock waves | |
| Elastic waves | |
| Note generali: | Title from title screen (viewed on Aug. 30, 2012). |
| "December 2011." | |
| "AIAA-2010-4936." | |
| Nota di bibliografia: | Includes bibliographical references (page 16). |
| Titolo autorizzato: | Exhaust nozzle plume effects on sonic boom test results for isolated nozzles |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910701912103321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |