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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
Paxson Daniel E.  
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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Development of an actuator for flow control utilizing detonation [[electronic resource] /] / Patrick J. Lonneman and Andrew D. Cutler
Development of an actuator for flow control utilizing detonation [[electronic resource] /] / Patrick J. Lonneman and Andrew D. Cutler
Autore Lonneman Patrick J
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2004]
Descrizione fisica 1 online resource (xvi, 156 pages) : illustrations (some color)
Altri autori (Persone) CutlerAndrew D
Collana NASA/CR
Soggetto topico Active control
Flow distribution
Separated flow
Detonation
Actuators
Flow regulators
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702039903321
Lonneman Patrick J  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2004]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines [[electronic resource] /] / Daniel E. Paxson, Thomas A. Kaemming
Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines [[electronic resource] /] / Daniel E. Paxson, Thomas A. Kaemming
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) KaemmingThomas A
Collana NASA/TM
Soggetto topico Gas turbines
Combustion chambers
Flow distribution
Pressure ratio
Thermodynamics
Extraction
Detonation
Combustion
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702122103321
Paxson Daniel E  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A simplified model for detonation based pressure-gain combustors [[electronic resource] /] / Daniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
A simplified model for detonation based pressure-gain combustors [[electronic resource] /] / Daniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
Autore Paxson Daniel E
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (13 pages) : illustrations, color
Collana NASA/TM
Soggetto topico Detonation
Gas turbines
Pulsed jet engines
Combustion chambers
Flow distribution
Reliability analysis
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910700371103321
Paxson Daniel E  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui