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Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [[electronic resource] /] / Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010



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Autore: Castner Raymond S Visualizza persona
Titolo: Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [[electronic resource] /] / Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010 Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica: 1 online resource (10 pages) : illustrations
Soggetto topico: Exhaust nozzles
Sonic booms
Wing slots
Aircraft control
Computational fluid dynamics
Exhaust gases
Supersonic speed
Mach number
High aspect ratio
Note generali: Title from title screen (viewed on Oct. 7, 2010).
"March 2010."
"AIAA-2010-1386."
Nota di bibliografia: Includes bibliographical references (page 10)
Titolo autorizzato: Slot nozzle effects for reduced sonic boom on a generic supersonic wing section  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910699548503321
Lo trovi qui: Univ. Federico II
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Serie: NASA technical memorandum ; ; 216258.