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Autore: |
Steffen Christopher J.
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Titolo: |
Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / / Christopher J. Steffen, Shaye Yungster
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Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
Descrizione fisica: | 1 online resource (15 pages) : illustrations |
Soggetto topico: | Computational fluid dynamics |
Numerical analysis | |
Combustion physics | |
Three dimensional models | |
Supersonic combustion ramjet engines | |
Simulation | |
Persona (resp. second.): | YungsterShaye |
Note generali: | "February 2001." |
"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." | |
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. | |
Nota di bibliografia: | Includes bibliographical references (page 15). |
Altri titoli varianti: | Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath |
Titolo autorizzato: | Computational analysis of the combustion process in an axisymmetric,RBCC flowpath ![]() |
Formato: | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910706576003321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |