Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / / Christopher J. Steffen, Shaye Yungster

• Autore: Steffen Christopher J.
• 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