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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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Autore: Castner Raymond S Visualizza persona
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 Visualizza cluster
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  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910699547103321
Lo trovi qui: Univ. Federico II
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Serie: NASA technical memorandum ; ; 216259.