The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley |
Autore | Bozak Richard F. |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 |
Descrizione fisica | 1 online resource (8 pages) : illustrations (some color) |
Collana | NASA/TM |
Soggetto topico |
Acoustic properties
Aerodynamic noise Blade tips Oscillating flow Pressure ratio Turbofans Rotors |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910705296503321 |
Bozak Richard F.
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 | ||
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Lo trovi qui: Univ. Federico II | ||
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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
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
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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 |
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.
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2012 | ||
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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 |
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
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
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Lo trovi qui: Univ. Federico II | ||
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Computational study of the CC3 impeller and vaneless diffuser experiment / / Sameer Kulkarni, Timothy A. Beach, Gary J. Skoch |
Autore | Kulkarni Sameer |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013 |
Descrizione fisica | 1 online resource (14 pages) : color illustrations |
Collana | NASA-TM |
Soggetto topico |
Centrifugal compressors
Computational fluid dynamics Turbofan engines Centrifugal force Pressure ratio Vaneless diffusers Turboshafts |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702742603321 |
Kulkarni Sameer
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013 | ||
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Lo trovi qui: Univ. Federico II | ||
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Development, verification and use of gust modeling in the NASA computational fluid dynamics code FUN3D / / Robert E. Bartels |
Autore | Bartels Robert E. |
Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 |
Descrizione fisica | 1 online resource (32 pages) : illustrations (some color) |
Collana | NASA/TM |
Soggetto topico |
Aeroelasticity
Autoregressive moving average Computational fluid dynamics Dynamic response Pressure ratio Airfoils |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702454303321 |
Bartels Robert E.
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Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
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Lo trovi qui: Univ. Federico II | ||
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Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20 |
Autore | Castner Raymond S |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
Descrizione fisica | 1 online resource (16 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Exhaust nozzles
Nozzle flow Plumes Supersonic aircraft Computational fluid dynamics Nozzle geometry Pressure ratio Shock waves Elastic waves |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910701912103321 |
Castner Raymond S
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
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Lo trovi qui: Univ. Federico II | ||
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Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner |
Autore | Castner Raymond S |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
Descrizione fisica | 1 online resource (16 pages) : color illustrations |
Collana | NASA/TM |
Soggetto topico |
Exhaust nozzles
Sonic booms Computational fluid dynamics Elastic waves Plumes F-15 aircraft Supersonic aircraft Pressure ratio |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910701950003321 |
Castner Raymond S
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
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Lo trovi qui: Univ. Federico II | ||
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Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines [[electronic resource] /] / Daniel E. Paxson, Thomas A. Kaemming |
Autore | Paxson Daniel E |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
Descrizione fisica | 1 online resource (12 pages) : color illustrations |
Altri autori (Persone) | KaemmingThomas A |
Collana | NASA/TM |
Soggetto topico |
Gas turbines
Combustion chambers Flow distribution Pressure ratio Thermodynamics Extraction Detonation Combustion |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702122103321 |
Paxson Daniel E
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
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Lo trovi qui: Univ. Federico II | ||
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Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / / Ali A. Ameri |
Autore | Ameri Ali A. |
Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
Descrizione fisica | 1 online resource (25 pages) : illustrations |
Collana | [NASA contractor report] |
Soggetto topico |
Computational fluid dynamics
Turbulent boundary layer Turbine blades Heat transfer Losses Low Reynolds number Pressure ratio Three dimensional flow Laminar flow |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910702113803321 |
Ameri Ali A.
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
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Lo trovi qui: Univ. Federico II | ||
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