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Advanced noise control fan aerodynamic performance [[electronic resource] /] / Richard F. Bozak, Jr
Advanced noise control fan aerodynamic performance [[electronic resource] /] / Richard F. Bozak, Jr
Autore Bozak Richard F., Jr.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
Descrizione fisica 1 online resource (19 pages) : illustrations
Collana NASA TM-
Soggetto topico Noise reduction
Aerodynamic characteristics
Inlet pressure
Static pressure
Flow measurement
Flow distribution
Mass flow
Acoustics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910696921303321
Bozak Richard F., Jr.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009]
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
Opac: Controlla la disponibilità qui
Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility [[electronic resource] /] / Roger A. Werner and John D. Wolter
Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility [[electronic resource] /] / Roger A. Werner and John D. Wolter
Autore Werner Roger A
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (49 pages) : illustrations, color
Altri autori (Persone) WolterJohn D
Collana NASA/TM
Soggetto topico Nozzle thrust coefficients
Discharge coefficient
Nozzle flow
Calibrating
Choked flow
Thrust measurement
Test facilities
Pressure ratio
Inlet pressure
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700371003321
Werner Roger A  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet / / Colin S. Bidwell
Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet / / Colin S. Bidwell
Autore Bidwell Colin S.
Pubbl/distr/stampa Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , February 1997
Descrizione fisica 1 online resource (26 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Boeing 737 aircraft
Ice formation
Prediction analysis techniques
Engine inlets
Inlet pressure
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707328303321
Bidwell Colin S.  
Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , February 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Dynamic simulation of a wave rotor topped turboshaft engine / / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri
Dynamic simulation of a wave rotor topped turboshaft engine / / R.B. Greendyke, D.E. Paxson, M.T. Schobeiri
Autore Greendyke Robert B.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1997
Descrizione fisica 1 online resource (9 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Turboshafts
Inlet pressure
Dynamic characteristics
Flow velocity
Fuel flow
Transient response
Computerized simulation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707633903321
Greendyke Robert B.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / / Zhuohui J. He [and four others]
Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / / Zhuohui J. He [and four others]
Autore He Zhuohui J.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014
Descrizione fisica 1 online resource (7 pages) : color illustrations
Collana NASA/TM
Soggetto topico Combustion chambers
Inlet pressure
Inlet temperature
Fuel injection
Combustion temperature
Nitrogen oxides
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702438303321
He Zhuohui J.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The high stability engine control (HISTEC) program : flight demonstration phase / / John C. DeLaat [and three others]
The high stability engine control (HISTEC) program : flight demonstration phase / / John C. DeLaat [and three others]
Autore DeLaat John C.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Descrizione fisica 1 online resource (11 pages) : color illustrations
Collana NASA/TM
Soggetto topico Engine control
Gas turbine engines
Flight tests
F-15 aircraft
Flow distortion
Real time operation
On-line systems
Control systems design
Inlet pressure
Stability augmentation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti High stability engine control
Record Nr. UNINA-9910705842703321
DeLaat John C.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
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NASA numerical and experimental evaluation of UTRC low emissions injector / / Yolanda R. Hicks [and five others]
NASA numerical and experimental evaluation of UTRC low emissions injector / / Yolanda R. Hicks [and five others]
Autore Hicks Yolanda R (Yolanda Royce)
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2014
Descrizione fisica 1 online resource (19 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Fuel injection
Inlet pressure
Laser induced fluorescence
Flow velocity
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti NASA numerical and experimental evaluation of United Technologies Research Center low emissions injector
Record Nr. UNINA-9910703638603321
Hicks Yolanda R (Yolanda Royce)  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet / / René Fernandez [and three others]
Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet / / René Fernandez [and three others]
Autore Fernandez René
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2001
Descrizione fisica 1 online resource (15 pages) : illustrations
Collana NASA/TM
Soggetto topico Scale models
Inlet pressure
Performance tests
Wind tunnel tests
Rocket-based combined-cycle engines
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706600403321
Fernandez René  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
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V/STOL model fan rig, design report [[electronic resource] /] / [ J. G. Cheatham, T. L. Creason]
V/STOL model fan rig, design report [[electronic resource] /] / [ J. G. Cheatham, T. L. Creason]
Autore Cheatham J. G
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1983]
Descrizione fisica 1 online resource (x, 249 pages) : digital, PDF file
Altri autori (Persone) CreasonT. L
Collana NASA CR
Soggetto topico Fan blades
Guide vanes
Inlet flow
Inlet pressure
V/STOL aircraft
Variability
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699719803321
Cheatham J. G  
[Washington, D.C.] : , : National Aeronautics and Space Administration, , [1983]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui