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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.  
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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Cause and cure: deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids / / Sin-Chung Chang, Chau-Lyan Chang, Balaji Shankar Venkatachari
Cause and cure: deterioration in accuracy of CFD simulations with use of high-aspect-ratio triangular/tetrahedral grids / / Sin-Chung Chang, Chau-Lyan Chang, Balaji Shankar Venkatachari
Autore Chang Sin-Chung
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Descrizione fisica 1 online resource (39 pages) : illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
High aspect ratio
High Reynolds number
Navier-Stokes equation
Space-time CE/SE method
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Cause and cure
Record Nr. UNINA-9910706177203321
Chang Sin-Chung  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions / / Robert E. Bartels and John W. Edwards
Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions / / Robert E. Bartels and John W. Edwards
Autore Bartels Robert E.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1997
Descrizione fisica 1 online resource (13 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Airfoils
Cryogenics
Transonic wind tunnels
Buffeting
Reynolds number
High Reynolds number
Pressure measurement
Angle of attack
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707835703321
Bartels Robert E.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Flow and noise control in high speed and high Reynolds number jets using plasma actuators [[electronic resource] /] / M. Samimy ... [and others] ; prepared for the Third Flow Control Conference sponsored by the American Institute of Aeronautics and Astronautics, San Francisco, California, June 5-8, 2006
Flow and noise control in high speed and high Reynolds number jets using plasma actuators [[electronic resource] /] / M. Samimy ... [and others] ; prepared for the Third Flow Control Conference sponsored by the American Institute of Aeronautics and Astronautics, San Francisco, California, June 5-8, 2006
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006]
Descrizione fisica 1 online resource (22 pages) : illustrations
Altri autori (Persone) SamimyM
Collana NASA TM-
Soggetto topico Actuators
High Reynolds number
Plasma generators
Aeroacoustics
Flow regulators
High speed
Gas dynamics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699312603321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Optimization of an advanced design three-element airfoil at high Reynolds numbers / / J.C. Lin, C.J. Dominik
Optimization of an advanced design three-element airfoil at high Reynolds numbers / / J.C. Lin, C.J. Dominik
Autore Lin J.-C (Jiun-Chuan)
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1995]
Descrizione fisica 1 online resource (11 pages) : illustrations
Collana NASA-TM
Soggetto topico Airfoils
Computational fluid dynamics
High Reynolds number
Leading edges
Prediction analysis techniques
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705749003321
Lin J.-C (Jiun-Chuan)  
[Washington, D.C.] : , : National Aeronautics and Space Administration, , [1995]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section / / Raymond E. Mineck
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section / / Raymond E. Mineck
Autore Mineck Raymond E.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , December 1987
Descrizione fisica 1 online resource (96 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Airfoil profiles
Cryogenic wind tunnels
High Reynolds number
Wall flow
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707804203321
Mineck Raymond E.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , December 1987
Materiale a stampa
Lo trovi qui: Univ. Federico II
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