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Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities [[electronic resource] /] / Richard P. Woodward and Christopher E. Hughes
Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities [[electronic resource] /] / Richard P. Woodward and Christopher E. Hughes
Autore Woodward Richard P
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (57 pages) : color illustrations
Altri autori (Persone) HughesChristopher E
Collana NASA/TM
Soggetto topico Acoustic measurement
Aeroacoustics
Low speed wind tunnels
Test facilities
Turbofans; wind tunnel tests
Aircraft models
Simulators
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702110203321
Woodward Richard P  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report / / Samuel J. Vinci
CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report / / Samuel J. Vinci
Autore Vinci Samuel J.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2012
Descrizione fisica 1 online resource (xiv, 113 pages) : color illustrations
Collana NASA/CR
Soggetto topico Computational fluid dynamics
Pressure ratio
Boundary layers
Finite volume method
Low speed wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil
Record Nr. UNINA-9910702453303321
Vinci Samuel J.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models [[electronic resource] /] / Robert J. Jeracki
Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models [[electronic resource] /] / Robert J. Jeracki
Autore Jeracki Robert J
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006]
Descrizione fisica 1 online resource (iii, 140 pages) : illustrations
Collana NASA/TM-
Soggetto topico Pressure ratio
Scale models
Simulators
Tip speed
Turbofan engines
Ducted fans
Low speed wind tunnels
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697168503321
Jeracki Robert J  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Contraction design for small low-speed wind tunnels [[electronic resource] /] / by James H. Bell and Rabindra D. Mehta
Contraction design for small low-speed wind tunnels [[electronic resource] /] / by James H. Bell and Rabindra D. Mehta
Autore Bell J. H
Pubbl/distr/stampa [Moffett Field, Calif.?] : , : National Aeronautics and Space Administration, Ames Research Center
Descrizione fisica 1 volume
Altri autori (Persone) MehtaR. D
Collana JIAA TR
NASA CR
Soggetto topico Contraction
Flow distribution
Iterative solution
Low speed wind tunnels
Pressure distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Contraction design for small low speed wind tunnels
Record Nr. UNINA-9910698899603321
Bell J. H  
[Moffett Field, Calif.?] : , : National Aeronautics and Space Administration, Ames Research Center
Materiale a stampa
Lo trovi qui: Univ. Federico II
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The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / / Christopher E. Hughes [and three others]
The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / / Christopher E. Hughes [and three others]
Autore Hughes Christopher E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Descrizione fisica 1 online resource (35 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Aeroacoustics
Aerodynamic characteristics
Aerodynamic noise
Aircraft noise
Fan blades
Far fields
Laser doppler velocimeters
Low speed wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702436703321
Hughes Christopher E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga
Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga
Autore Hughes Christopher E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013
Descrizione fisica 1 online resource (22 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aircraft performance
Bypass ratio
Fan blades
Fixed wings
Low speed wind tunnels
Noise reduction
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702436203321
Hughes Christopher E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel [[electronic resource] /] / David M. Elliott
Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel [[electronic resource] /] / David M. Elliott
Autore Elliott David M
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (22 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Wind tunnel tests
Rotor aerodynamics
Low speed wind tunnels
Rotor blades (turbomachinery)
Counter rotation
Scale models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701916803321
Elliott David M  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Modifications to the 4 x 7 meter tunnel for acoustic research [[electronic resource] ] : engineering feasibility study
Modifications to the 4 x 7 meter tunnel for acoustic research [[electronic resource] ] : engineering feasibility study
Pubbl/distr/stampa Orlando, Fla. : , : DSMA Engineering Corporation
Descrizione fisica 1 online resource (vii, 77 pages) : illustrations
Collana NASA contractor report
Soggetto topico Acoustic measurement
Aeroacoustics
Design analysis
Low speed wind tunnels
Wind tunnel drives
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Modifications to the 4 x 7 meter tunnel for acoustic research
Record Nr. UNINA-9910702107703321
Orlando, Fla. : , : DSMA Engineering Corporation
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Quiet High Speed Fan II (QHSF II) : final report / / Karen Kontos, Don Weir, and Dave Ross
Quiet High Speed Fan II (QHSF II) : final report / / Karen Kontos, Don Weir, and Dave Ross
Autore Kontos Karen
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012
Descrizione fisica 1 online resource (xiv, 183 pages) : illustrations (some color)
Collana NASA/CR
Soggetto topico Low speed wind tunnels
Acoustic properties
Aeroacoustics
Aeroelasticity
Guide vanes
Turbofans
Structural design
Tip speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Quiet High Speed Fan II
Record Nr. UNINA-9910702342303321
Kontos Karen  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Vapor generator wand [[electronic resource] /] / inventor, David B. Robelen
Vapor generator wand [[electronic resource] /] / inventor, David B. Robelen
Edizione [[Redacted ed.]]
Pubbl/distr/stampa [Washington, DC] : , : [National Aeronautics and Space Administration], , [1994]
Descrizione fisica 1 online resource : illustrations
Altri autori (Persone) RobolenDavid B
Collana NASA case
Soggetto topico Air flow
Heating
Low speed wind tunnels
Strain gages
Vaporizers
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697263803321
[Washington, DC] : , : [National Aeronautics and Space Administration], , [1994]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui