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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 |
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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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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Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers / / C.J. Steffen, Jr. and J.R. DeBonis
| Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers / / C.J. Steffen, Jr. and J.R. DeBonis |
| Autore | Steffen Christopher J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (9 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Flow distribution
Numerical analysis Engine inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706122403321 |
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Steffen Christopher J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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