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Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber
| Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber |
| Autore | Csank Jeffrey T. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Inlet flow
Controllers Feedback control Computerized simulation Turbine engines Engine inlets |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704816803321 |
Csank Jeffrey T.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch
| Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch |
| Autore | McVetta Ashlie B. |
| Edizione | [Revised copy.] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 |
| Descrizione fisica | 1 online resource (23 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic turbines
Turbine blades Aerodynamic heat transfer Computational fluid dynamics Reynolds number Pressure distribution Inlet flow Angles (geometry) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702656103321 |
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McVetta Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch
| Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch |
| Autore | McVetta Ashlie B. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic heat transfer
Computational fluid dynamics Flow measurement Inlet flow Supersonic turbines Turbine blades |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702431803321 |
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McVetta Ashlie B.
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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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Aeromechanics analysis of a boundary layer ingesting fan / / Milind A. Bakhle [and four others]
| Aeromechanics analysis of a boundary layer ingesting fan / / Milind A. Bakhle [and four others] |
| Autore | Bakhle Milind A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (15 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Dynamic loads Propulsion system configurations Inlet flow Propulsion system performance Reynolds averaging |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704911103321 |
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Bakhle Milind A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick
| Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick |
| Autore | Herrick Gregory Paul <1972-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014 |
| Descrizione fisica | 1 online resource (17 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Turbomachinery
Flutter analysis Inlet flow Computational fluid dynamics Aeroelasticity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703769103321 |
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Herrick Gregory Paul <1972->
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / / Daniel E. Paxson [and three others]
| Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / / Daniel E. Paxson [and three others] |
| Autore | Paxson Daniel E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2015 |
| Descrizione fisica | 1 online resource (10 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Detonation
Computational fluid dynamics Inlet flow Convergent-divergent nozzles Potential flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704025303321 |
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Paxson Daniel E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational analyses of the LIMX TBCC inlet high-speed flowpath [[electronic resource] /] / Vance F. Dippold, III
| Computational analyses of the LIMX TBCC inlet high-speed flowpath [[electronic resource] /] / Vance F. Dippold, III |
| Autore | Dippold Vance |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (26 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Turbine engines
Cycles Inlet flow Supersonic combustion ramjet engines Combustion chambers High speed Mass flow rate Reynolds averaging Free flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701830003321 |
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Dippold Vance
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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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Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall
| Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall |
| Autore | Hughes Donald L (Donald Lee), <1926-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static pressure
Aircraft engines Inlet flow Flight tests Pressure measurement Static pressure probes - Testing Airplanes - Turbojet engines - Air intakes Eagle (Jet fighter plane) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709611203321 |
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Hughes Donald L (Donald Lee), <1926->
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
| Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan [[electronic resource] /] / Gregory P. Herrick ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010 |
| Autore | Herrick Gregory Paul <1972-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aeroelasticity
Turbomachinery Turbofans Computational fluid dynamics Inlet flow Aerodynamic characteristics High speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700302303321 |
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Herrick Gregory Paul <1972->
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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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An experimental device for generating high frequency perturbations in supersonic wind tunnels / / Kevin J. Melcher and Mounir B. Ibrahim
| An experimental device for generating high frequency perturbations in supersonic wind tunnels / / Kevin J. Melcher and Mounir B. Ibrahim |
| Autore | Melcher Kevin J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Supersonic wind tunnels
Gusts Inlet flow Wind tunnel apparatus Surges Pressure pulses |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707307003321 |
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Melcher Kevin J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Inlet flow
(21)
- Computational fluid dynamics (12)
- Engine inlets (3)
- High speed (3)
- Reynolds averaging (3)