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Application of CARS to scramjet combustion / / Richard R. Antcliff
| Application of CARS to scramjet combustion / / Richard R. Antcliff |
| Autore | Antcliff Richard R. |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987] |
| Descrizione fisica | 1 online resource (vi, 27 pages) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Diagnosis
Nondestructive tests Raman spectroscopy Supersonic combustion ramjet engines |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704491403321 |
Antcliff Richard R.
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1987] | ||
| 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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Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / / Christopher J. Steffen, Shaye Yungster
| Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / / Christopher J. Steffen, Shaye Yungster |
| Autore | Steffen Christopher J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Numerical analysis Combustion physics Three dimensional models Supersonic combustion ramjet engines Simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath |
| Record Nr. | UNINA-9910706576003321 |
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Steffen Christopher J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 | ||
| 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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Conceptual model of turbulent flameholding for scramjet combustors / / Paul W. Huber
| Conceptual model of turbulent flameholding for scramjet combustors / / Paul W. Huber |
| Autore | Huber Paul W (Paul William), <1920-> |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1980 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Flame holders
Flame propagation Fuel combustion Supersonic combustion ramjet engines Turbulence models Flame spread Internal combustion engines - Combustion Jet propulsion Supersonic planes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707490703321 |
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Huber Paul W (Paul William), <1920->
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1980 | ||
| 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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Dual-pump CARS development and application to supersonic combustion / / Gaetano Magnotti and Andrew D. Cutler
| Dual-pump CARS development and application to supersonic combustion / / Gaetano Magnotti and Andrew D. Cutler |
| Autore | Magnotti Gaetano |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (xxvi, 274 pages) : color illustrations |
| Collana | [NASA contractor report] |
| Soggetto topico |
Computational fluid dynamics
Hydrogen Nitrogen Oxygen Laser pumping Supersonic combustion ramjet engines Raman spectroscopy Supersonic combustion Mathematical models Temperature measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702296403321 |
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Magnotti Gaetano
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fuel injector design optimization for an annular scramjet geometry / / Christopher J. Steffen, Jr
| Fuel injector design optimization for an annular scramjet geometry / / Christopher J. Steffen, Jr |
| Autore | Steffen Christopher J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2003 |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Design optimization Fuel injection Injectors Rocket-based combined-cycle engines Supersonic combustion ramjet engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705619303321 |
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Steffen Christopher J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2003 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Further shock tunnel studies of scramjet phenomena [[electronic resource] /] / R. G. Morgan ... [and others]
| Further shock tunnel studies of scramjet phenomena [[electronic resource] /] / R. G. Morgan ... [and others] |
| Pubbl/distr/stampa | [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1986] |
| Descrizione fisica | 1 volume |
| Altri autori (Persone) | MorganR. G |
| Collana | NASA-CR |
| Soggetto topico |
Combustion physics
Film cooling Gas dynamics Heat transfer Shock tunnels Silanes Supersonic combustion ramjet engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910698845103321 |
| [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others]
| Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others] |
| Autore | Foster Lancert E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Engine inlets
Hypersonic flight Supersonic speed Air breathing engines Supersonic combustion ramjet engines Specific impulse Propulsion system configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704671703321 |
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Foster Lancert 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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