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Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima
Analysis of buzz in a supersonic inlet [[electronic resource] /] / Rodrick V. Chima
Autore Chima Rodrick V
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (36 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Supersonic wind tunnels
Acoustic resonance
Frequency response
High frequencies
Mach number
Inlet pressure
Supersonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702114103321
Chima Rodrick V  
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
Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry [[electronic resource] /] / Gregory C. Herring and James F. Meyers
Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry [[electronic resource] /] / Gregory C. Herring and James F. Meyers
Autore Herring Gregory C
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Descrizione fisica 1 online resource (29 pages) : illustrations (some color)
Altri autori (Persone) MeyersJames F
Collana NASA/TM
Soggetto topico Velocity measurement
Sonic booms
Flow characteristics
Supersonic speed
Oblique shock waves
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Conical shock strength determination on low sonic boom aircraft model by doppler global velocimetry
Record Nr. UNINA-9910700812003321
Herring Gregory C  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Design and analysis tool for external-compression supersonic inlets [[electronic resource] /] / John W. Slater
Design and analysis tool for external-compression supersonic inlets [[electronic resource] /] / John W. Slater
Autore Slater John W
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (23 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Supersonic inlets
Flow distribution
Aerodynamic characteristics
Drag
Flow velocity
Supersonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702353503321
Slater John W  
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
The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine [[electronic resource] /] / Theresa L. Benyo ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010
The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine [[electronic resource] /] / Theresa L. Benyo ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010
Autore Benyo Theresa L
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (13 pages) : illustrations (chiefly color)
Collana NASA/TM
Soggetto topico Magnetohydrodynamics
Thermodynamic cycles
Turbojet engines
Thermal conductivity
Supersonic speed
Specific impulse
Enthalpy
Hypersonic flight
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Effect of magnetohydrodynamic
Record Nr. UNINA-9910700383203321
Benyo Theresa L  
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
Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods [[electronic resource] /] / Gary E. Erickson
Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods [[electronic resource] /] / Gary E. Erickson
Autore Erickson Gary E
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010]
Descrizione fisica 1 online resource (v, 36 pages) : illustrations
Collana NASA/TM-
Soggetto topico Aerodynamic characteristics
Control surfaces
Launch vehicles
Shock wave interaction
Supersonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697041703321
Erickson Gary E  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / / Harry W. Carlson and Robert J. Mack
Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / / Harry W. Carlson and Robert J. Mack
Autore Carlson Harry W.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1980
Descrizione fisica 1 online resource (81 pages) : illustrations
Collana NASA technical paper
Soggetto topico Aerodynamic characteristics
Computer programs
Leading edge thrust
Nonlinearity
Supersonic speed
Aerodynamics, Supersonic
Airplanes - Wings
Supersonic planes
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707472303321
Carlson Harry W.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny
Autore Thomas Scott R.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997
Descrizione fisica 1 online resource (10 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Ejectors
Hydrocarbon fuels
Wind tunnel tests
Supersonic speed
Mach number
Engine tests
Propulsion system performance
Flow distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707625903321
Thomas Scott R.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental effects of wing location on wing-body pressures at supersonic speeds / / Jerry M. Allen and Carolyn B. Watson
Experimental effects of wing location on wing-body pressures at supersonic speeds / / Jerry M. Allen and Carolyn B. Watson
Autore Allen Jerry M.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1993
Descrizione fisica 1 online resource (195 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Angle of attack
Body-wing configurations
Flow coefficients
Pressure distribution
Supersonic flight
Supersonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707953503321
Allen Jerry M.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, , April 1993
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / / Floyd J. Wilcox, Jr. [and five others]
Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / / Floyd J. Wilcox, Jr. [and five others]
Autore Wilcox Floyd J (Floyd Jay)
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Descrizione fisica 1 online resource (130 pages) : illustrations
Collana [NASA technical memorandum]
Soggetto topico Sonic booms
Wind tunnel tests
Supersonic speed
Angle of attack
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702349803321
Wilcox Floyd J (Floyd Jay)  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Focused and steady-state characteristics of shaped sonic boom signatures [[electronic resource] ] : prediction and analysis / / Domenic J. Maglieri ... [and others]
Focused and steady-state characteristics of shaped sonic boom signatures [[electronic resource] ] : prediction and analysis / / Domenic J. Maglieri ... [and others]
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Descrizione fisica 1 online resource (143 unnumbered pages) : illustrations (some color)
Altri autori (Persone) MaglieriDomenic J
Collana NASA/CR
Soggetto topico Sonic booms
Waveforms
Supersonic aircraft
Supersonic speed
Transition flight
Amplification
Transonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Focused and steady-state characteristics of shaped sonic boom signatures
Record Nr. UNINA-9910701159203321
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione