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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
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
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (16 pages) : color illustrations
Collana NASA/TM
Soggetto topico Exhaust nozzles
Nozzle flow
Plumes
Supersonic aircraft
Computational fluid dynamics
Nozzle geometry
Pressure ratio
Shock waves
Elastic waves
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701912103321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner
Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (16 pages) : color illustrations
Collana NASA/TM
Soggetto topico Exhaust nozzles
Sonic booms
Computational fluid dynamics
Elastic waves
Plumes
F-15 aircraft
Supersonic aircraft
Pressure ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701950003321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
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
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (10 pages) : illustrations
Collana NASA TM-
Soggetto topico Exhaust nozzles
Sonic booms
Wing slots
Aircraft control
Computational fluid dynamics
Exhaust gases
Supersonic speed
Mach number
High aspect ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699548503321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
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
Autore Castner Raymond S
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (10 pages) : illustrations
Collana NASA TM-
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
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699547103321
Castner Raymond S  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui