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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
| 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 | ||
| Materiale a stampa | ||
| 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
| 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 |
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Werner Roger A
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| 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 |
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Vinci Samuel J.
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| 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 |
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Jeracki Robert J
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
| Materiale a stampa | ||
| 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
| 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 |
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Kulkarni Sameer
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2013 | ||
| Materiale a stampa | ||
| 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
| 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 |
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Bartels Robert E.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
| Materiale a stampa | ||
| 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
| 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 |
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Castner Raymond S
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| 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
| 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 |
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Castner Raymond S
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| 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
| 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 |
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Paxson Daniel E
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| 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
| 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 |
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Ameri Ali A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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