02299nam 2200517 450 991070657600332120171120092821.0(CKB)5470000002456685(OCoLC)1012398455(EXLCZ)99547000000245668520171120j200102 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierComputational analysis of the combustion process in an axisymmetric,RBCC flowpath /Christopher J. Steffen, Shaye YungsterCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,February 2001.1 online resource (15 pages) illustrationsNASA/TM ;2001-210679"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.Includes bibliographical references (page 15).Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpathComputational fluid dynamicsnasatNumerical analysisnasatCombustion physicsnasatThree dimensional modelsnasatSupersonic combustion ramjet enginesnasatSimulationnasatComputational fluid dynamics.Numerical analysis.Combustion physics.Three dimensional models.Supersonic combustion ramjet engines.Simulation.Steffen Christopher J.1386995Yungster ShayeNASA Glenn Research Center,GPOGPOBOOK9910706576003321Computational analysis of the combustion process in an axisymmetric,RBCC flowpath3436394UNINA