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Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet / / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee
| Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet / / Michael K. Ponton, Lawrence S. Ukeiley, Sang W. Lee |
| Autore | Ponton Michael K. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1999 |
| Descrizione fisica | 1 online resource (84 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aeroacoustics
Convergent nozzles Jet flow Subsonic flow High Reynolds number Pressure oscillations Flow characteristics Engine noise Exhaust nozzles Exhaust gases |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706169303321 |
Ponton Michael K.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A comparison of combustor-noise models / / Lennart S. Hultgren
| A comparison of combustor-noise models / / Lennart S. Hultgren |
| Autore | Hultgren Lennart S (Lennart Sven) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (27 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Noise generators
Turbofan engines Prediction analysis techniques Noise prediction Engine noise Combustion chambers Exhaust nozzles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702357403321 |
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Hultgren Lennart S (Lennart Sven)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Castner Raymond S
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Castner Raymond S
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model [[electronic resource] /] / Raymond Castner, Troy Lake
| Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model [[electronic resource] /] / Raymond Castner, Troy Lake |
| Autore | Castner Raymond |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (some color) |
| Altri autori (Persone) | LakeTroy |
| Collana | NASA/TM |
| Soggetto topico |
Exhaust gases
Exhaust nozzles Pressure distribution Sonic booms Body-wing configurations Plumes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702114003321 |
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Castner Raymond
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental investigation of an ejector-powered free-jet facility [[electronic resource] /] / Mary Jo Long
| Experimental investigation of an ejector-powered free-jet facility [[electronic resource] /] / Mary Jo Long |
| Autore | Long Mary Jo |
| Pubbl/distr/stampa | [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1992] |
| Descrizione fisica | 1 online resource (13 pages) : digital, PDF file |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aircraft noise
Ejectors Engine noise Exhaust nozzles Free jets Subsonic wind tunnels Test facilities |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699534103321 |
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Long Mary Jo
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| [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1992] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Jet noise reduction potential from emerging variable cycle technologies / / Brenda S. Henderson, James E. Bridges, and Mark P. Wernet
| Jet noise reduction potential from emerging variable cycle technologies / / Brenda S. Henderson, James E. Bridges, and Mark P. Wernet |
| Autore | Henderson Brenda S. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA/TM 2012-217744 |
| Soggetto topico |
Jet aircraft noise
Noise reduction Flow distribution Commercial aircraft Supersonic aircraft Aeroacoustics Nozzle flow Exhaust nozzles Computational fluid dynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704623703321 |
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Henderson Brenda S.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Noise from aft deck exhaust nozzles : differences in experimental embodiments / / James E. Bridges
| Noise from aft deck exhaust nozzles : differences in experimental embodiments / / James E. Bridges |
| Autore | Bridges James E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014 |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aeroacoustics
Jet aircraft noise Convergent nozzles Exhaust nozzles Green's functions Navier-Stokes equation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Noise from aft deck exhaust nozzles |
| Record Nr. | UNINA-9910702438603321 |
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Bridges James E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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
| 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 |
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Castner Raymond S
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter
| Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control / / Scott C. Asbury and Craig A. Hunter |
| Autore | Asbury Scott C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999 |
| Descrizione fisica | 1 online resource (134 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Exhaust nozzles
Porosity Hole geometry (mechanics) Cavities Thrust vector control |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706145403321 |
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Asbury Scott C.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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