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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 |
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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Ejector enhanced pulsejet based pressure gain combustors [[electronic resource] ] : an old idea with a new twist / / Daniel E. Paxson, Kevin T. Dougherty
| Ejector enhanced pulsejet based pressure gain combustors [[electronic resource] ] : an old idea with a new twist / / Daniel E. Paxson, Kevin T. Dougherty |
| Autore | Paxson Daniel E |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] |
| Descrizione fisica | 1 online resource (15 pages) : illustrations (some color) |
| Altri autori (Persone) | DoughertyKevin T |
| Collana | NASA/TM |
| Soggetto topico |
Combustion chambers
Ejectors Pressure oscillations Pulsejet engines Pulse detonation engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Ejector enhanced pulsejet based pressure gain combustors |
| Record Nr. | UNINA-9910701249703321 |
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Paxson Daniel E
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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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Multiple-cycle simulation of a pulse detonation engine ejector / / S. Yungster, H.D. Perkins
| Multiple-cycle simulation of a pulse detonation engine ejector / / S. Yungster, H.D. Perkins |
| Autore | Yungster Shaye |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (10 pages) : illustration |
| Collana | NASA/TM |
| Soggetto topico |
Detonable gas mixtures
Ejectors Impulses Mass flow rate Pulse detonation engines Shock waves |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705889103321 |
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Yungster Shaye
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Numerical analysis of a rotating detonation engine in the relative reference frame / / Daniel E. Paxson
| Numerical analysis of a rotating detonation engine in the relative reference frame / / Daniel E. Paxson |
| Autore | Paxson Daniel E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014 |
| Descrizione fisica | 1 online resource (16 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Pulse detonation engines Runge-Kutta method Propellant combustion Rotary engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703625903321 |
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Paxson Daniel E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Performance impact of deflagration to detonation transition enhancing obstacles [[electronic resource] /] / Daniel E. Paxson, Frederick Schauer and David Hopper
| Performance impact of deflagration to detonation transition enhancing obstacles [[electronic resource] /] / Daniel E. Paxson, Frederick Schauer and David Hopper |
| 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) |
SchauerFrederick F
HopperDavid H <1927-> (David Henry) |
| Collana | NASA/TM |
| Soggetto topico |
Pulse detonation engines
Computational fluid dynamics Deflagration Heat transfer Aerodynamic drag |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702216203321 |
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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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Pulse detonation engines for high speed flight / / Louis A. Povinelli
| Pulse detonation engines for high speed flight / / Louis A. Povinelli |
| Autore | Povinelli Louis A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Pulse detonation engines
Air breathing engines Propulsion High speed |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Solar electric propulsion vehicle design study for cargo transfer to Earth-Moon libration point |
| Record Nr. | UNINA-9910705649103321 |
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Povinelli Louis A.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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