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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
Opac: Controlla la disponibilità qui
Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeronautics and Astronautics Kissimmee, Florida, January 8-12, 2018 / / Daniel E. Paxson
Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics : prepared for 2018 SciTech Forum spnsored by the American Institute of Aeronautics and Astronautics Kissimmee, Florida, January 8-12, 2018 / / Daniel E. Paxson
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2018
Descrizione fisica 1 online resource (17 pages) : color illustrations
Collana NASA/TM
Soggetto topico Turbulence
Detonation waves
Computational fluid dynamics
Heat transfer
Two dimensional models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Examination of wave speed in rotating detonation engines using simplified computational fluid dynamics
Record Nr. UNINA-9910709898803321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson
Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016
Descrizione fisica 1 online resource (12 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Exhaust flow simulation
Fuel flow
Inviscid flow
Propulsion system performance
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707267903321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
An incidence loss model for wave rotors with axially aligned passages / / Daniel E. Paxson
An incidence loss model for wave rotors with axially aligned passages / / Daniel E. Paxson
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1998
Descrizione fisica 1 online resource (approximately 12 pages) : illustrations
Collana NASA/TM
Soggetto topico Aerodynamics
Wave rotors
Computational fluid dynamics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910717116603321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The influence of unsteadiness on the analysis of pressure gain combustion devices / / Daniel E. Paxson, Tom Kaemming
The influence of unsteadiness on the analysis of pressure gain combustion devices / / Daniel E. Paxson, Tom Kaemming
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2013
Descrizione fisica 1 online resource (16 pages) : color illustrations
Collana NASA/TM
Soggetto topico Thermodynamic efficiency
Combustion
Performance prediction
Thermodynamic cycles
Steady flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704910903321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , January 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Numerical assessment of four-port through-flow wave rotor cycles with passage height variation / / D.E. Paxson and Jules W. Lindau
Numerical assessment of four-port through-flow wave rotor cycles with passage height variation / / D.E. Paxson and Jules W. Lindau
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997
Descrizione fisica 1 online resource (12 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Computational fluid dynamics
Flow distribution
Fuel consumption
Gas turbine engines
Pressure ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705782403321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , June 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors / / Daniel E. Paxson
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors / / Daniel E. Paxson
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999
Descrizione fisica 1 online resource (12 pages) : illustrations
Collana NASA TM
Soggetto topico Computational fluid dynamics
Equations of motion
Combustion chambers
Combustion stability
Thermal instability
Premixed flames
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706280003321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Using the NASA GRC sectored-one-dimensional combustor simulation / / Daniel E. Paxson and Vishal R. Mehta
Using the NASA GRC sectored-one-dimensional combustor simulation / / Daniel E. Paxson and Vishal R. Mehta
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014
Descrizione fisica 1 online resource (20 pages) : color illustrations
Collana NASA/TM
Soggetto topico Combustion chambers
Mathematical models
Manuals
Educational resources
FORTRAN
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Using the NASA Glenn Research Center sectored one dimensional combustor simulation
Record Nr. UNINA-9910703626203321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Wave augmented diffusers for centrifugal compressors / / Daniel E. Paxson, Gary J. Skoch
Wave augmented diffusers for centrifugal compressors / / Daniel E. Paxson, Gary J. Skoch
Autore Paxson Daniel E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Descrizione fisica 1 online resource (6 pages) : illustrations
Collana NASA/TM
Soggetto topico Centrifugal compressors
Centrifugal force
Compression waves
Elastic waves
Computational fluid dynamics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705843303321
Paxson Daniel E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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