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Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel / / by Leo L. Beranek, Samuel Labate, and Uno Ingard
Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel / / by Leo L. Beranek, Samuel Labate, and Uno Ingard
Autore Beranek Leo L (Leo Leroy), <1914-2016, >
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955
Descrizione fisica 1 online resource (86 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Supersonic wind tunnels
Noise - Measurement
Noise control
Charts, diagrams, etc
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Acoustical treatment for the National Advisory Committee for Aeronautics eight- by six-foot supersonic propulsion wind tunnel
Record Nr. UNINA-9910713883803321
Beranek Leo L (Leo Leroy), <1914-2016, >  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955
Materiale a stampa
Lo trovi qui: Univ. Federico II
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The Ames 10- by 14-inch supersonic wind tunnel / / by A.J. Eggers, Jr. and George J. Nothwang
The Ames 10- by 14-inch supersonic wind tunnel / / by A.J. Eggers, Jr. and George J. Nothwang
Autore Eggers A. J.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954
Descrizione fisica 1 online resource (43 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Supersonic wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Ames ten- by fourteen-inch supersonic wind tunnel
Record Nr. UNINA-9910713888703321
Eggers A. J.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954
Materiale a stampa
Lo trovi qui: Univ. Federico II
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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
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Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / / Raymond Castner [and three others]
Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / / Raymond Castner [and three others]
Autore Castner Raymond S.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2013
Descrizione fisica 1 online resource (12 pages) : color illustrations
Collana NASA/TM
Soggetto topico Pressure distribution
Sonic booms
Spatial distribution
Supersonic wind tunnels
Wind pressure
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705291903321
Castner Raymond S.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) [[electronic resource] /] / E. Allen Arrington
Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) [[electronic resource] /] / E. Allen Arrington
Autore Arrington E. Allen
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (113 pages) : color illustrations
Collana NASA/CR
Soggetto topico Supersonic wind tunnels
Wind tunnel tests
Calibrating
Honeycomb structures
Flow distribution
Vortex generators
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel
Record Nr. UNINA-9910702042503321
Arrington E. Allen  
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
Calibration of the NASA Glenn Research Center 16 in. mass-flow plug / / David O. Davis [and four others]
Calibration of the NASA Glenn Research Center 16 in. mass-flow plug / / David O. Davis [and four others]
Autore Davis David O.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014
Descrizione fisica 1 online resource (15 pages) : color illustrations
Collana NASA-TM
Soggetto topico Supersonic wind tunnels
Mass flow
Discharge coefficient
Compressible flow
Nozzle flow
Flow measurement
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702743403321
Davis David O.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Check calibration of the NASA Glenn 10- by 10-foot supersonic wind tunnel (2014 test entry) / / Aaron Johnson, Christine Pastor-Barsi and E. Allen Arrington
Check calibration of the NASA Glenn 10- by 10-foot supersonic wind tunnel (2014 test entry) / / Aaron Johnson, Christine Pastor-Barsi and E. Allen Arrington
Autore Johnson Aaron
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2016
Descrizione fisica 1 online resource (15 pages) : color illustrations
Collana NASA/CR
Soggetto topico Calibrating
Data acquisition
Pressure measurement
Supersonic wind tunnels
Systems integration
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Check calibration of the NASA Glenn 10- by 10-foot supersonic wind tunnel
Record Nr. UNINA-9910707674203321
Johnson Aaron  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / / Randy Thomas and Thomas J. Stueber
Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / / Randy Thomas and Thomas J. Stueber
Autore Thomas Randy
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Descrizione fisica 1 online resource (24 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Actuators
Control equipment
Data acquisition
Engine inlets
Feedback control
Hardware-in-the-loop simulation
Pressure sensors
Supersonic wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Combined cycle engine large-scale inlet for mode transition experiments
Record Nr. UNINA-9910705296403321
Thomas Randy  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene
Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene
Autore Tornabene Robert
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Descrizione fisica 1 online resource (15 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Air flow
Characterization
Engine inlets
Pulse detonation engines
Supersonic wind tunnels
Gas valves
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697023103321
Tornabene Robert  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Experimental and computational sonic boom assessment of Boeing N+2 low boom models / / Donald A. Durston [and five others]
Experimental and computational sonic boom assessment of Boeing N+2 low boom models / / Donald A. Durston [and five others]
Autore Durston D. A.
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 2015
Descrizione fisica 1 online resource (xi, 146 pages) : color illustrations
Collana NASA/TP
Soggetto topico Computational fluid dynamics
Pressure measurement
Sonic booms
Supersonic test apparatus
Supersonic wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703627803321
Durston D. A.  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
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