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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
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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 aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development / / Daniel L. Tweedt
| Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development / / Daniel L. Tweedt |
| Autore | Tweedt Daniel L (Daniel Lawrence) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (57 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Computational fluid dynamics
Mass flow rate Acoustic measurement Rotor blades (turbomachinery) Wind tunnel tests Boundary layer separation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703550203321 |
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Tweedt Daniel L (Daniel Lawrence)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima
| Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| 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 |
Computational fluid dynamics
Engine inlets Supersonic aircraft Supersonic inlets Inlet airframe configurations Overpressure Supersonic flow Sonic booms Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701537703321 |
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Chima Rodrick V
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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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Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009
| Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition [[electronic resource] /] / John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009 |
| Autore | Slater John W |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (27 pages) : illustrations |
| Altri autori (Persone) | SaundersJohn D |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics 241
Data simulation Hypersonics Static pressure Supersonic combustion ramjet engines Wind tunnel tests Aerodynamics Boundary layers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Computational fluid dynamics |
| Record Nr. | UNINA-9910699653003321 |
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Slater John W
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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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Cruise noise of the SR-2 propeller model in a wind tunnel [[electronic resource] /] / James H. Dittmar
| Cruise noise of the SR-2 propeller model in a wind tunnel [[electronic resource] /] / James H. Dittmar |
| Autore | Dittmar James H |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1989] |
| Descrizione fisica | 27 pages : digital, PDF file |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aerodynamic noise
Aircraft noise Propellers Turboprop aircraft Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910698094803321 |
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Dittmar James H
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design study of an entry probe spectro-reflectometer [[electronic resource] /] / by Godfrey T. Sill, Uwe Fink
| Design study of an entry probe spectro-reflectometer [[electronic resource] /] / by Godfrey T. Sill, Uwe Fink |
| Autore | Sill Godfrey T |
| Pubbl/distr/stampa | Tucson, AZ ; ; Lunar and Planetary Laboratory, University of Arizona ; [Washington, D.C. ; ] ; [National Aeronautics and Space Administration, : [publisher not identified], , [1986] |
| Descrizione fisica | 1 online resource (11 unnumbered pages) : illustrations |
| Altri autori (Persone) | FinkUwe |
| Collana | NASA-CR |
| Soggetto topico |
Cryogenics
Experiment design Frost Ice formation Jupiter atmosphere Test equipment Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701401803321 |
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Sill Godfrey T
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| Tucson, AZ ; ; Lunar and Planetary Laboratory, University of Arizona ; [Washington, D.C. ; ] ; [National Aeronautics and Space Administration, : [publisher not identified], , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Determination of HART I blade structural properties by laboratory testing / / Sung N. Jung, Benton H. Lau
| Determination of HART I blade structural properties by laboratory testing / / Sung N. Jung, Benton H. Lau |
| Autore | Jung Sung N. |
| Pubbl/distr/stampa | Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , 2012 |
| Descrizione fisica | 1 online resource (vi, 29 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Wind tunnel tests
Aeroacoustics Harmonics Rotor blades (turbomachinery) Mechanical properties Dynamic structural analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Determination of Higher Harmonic Control Aeroacoustic Rotor Test blade structural properties by laboratory testing |
| Record Nr. | UNINA-9910704439103321 |
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Jung Sung N.
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| Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Determination of turbine blade life from engine field data / / Erwin V. Zaretsky [and three others]
| Determination of turbine blade life from engine field data / / Erwin V. Zaretsky [and three others] |
| Autore | Zaretsky Erwin V. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2013 |
| Descrizione fisica | 1 online resource (23 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Air breathing engines
Propulsion system configurations Propulsion system performance Research and development Jet propulsion Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Seventy years of aeropropulsion research at NASA Glenn Research Center |
| Record Nr. | UNINA-9910704879103321 |
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Zaretsky Erwin V.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene
| Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene |
| Autore | Tornabene Robert |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] |
| Descrizione fisica | 1 online resource (15 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Air flow
Characterization Engine inlets Pulse detonation engines Supersonic wind tunnels Gas valves Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697023103321 |
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Tornabene Robert
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 / / Mark C. Davis [and five others]
| Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 / / Mark C. Davis [and five others] |
| Autore | Davis Mark C. |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , May 2000 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA TM |
| Soggetto topico |
Mach number
Research vehicles Supersonic combustion ramjet engines Wind tunnel tests Air data systems Design analysis Detection |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706263503321 |
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Davis Mark C.
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , May 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Wind tunnel tests
(154)
- Aerodynamic characteristics (20)
- Flow distribution (16)
- Ice formation (15)
- Computational fluid dynamics (13)