02030nam 2200505 450 991070561930332120170908152907.0(CKB)5470000002452207(OCoLC)988393722(EXLCZ)99547000000245220720170531j200301 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFuel injector design optimization for an annular scramjet geometry /Christopher J. Steffen, JrCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,January 2003.1 online resource (15 pages) illustrationsNASA/TM ;2003-212094"January 2003.""Prepared for the 41st Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-9, 2003.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field" Report documentation page."AIAA-2003-0651."Includes bibliographical references (page 7).Computational fluid dynamicsnasatDesign optimizationnasatFuel injectionnasatInjectorsnasatRocket-based combined-cycle enginesnasatSupersonic combustion ramjet enginesnasatComputational fluid dynamics.Design optimization.Fuel injection.Injectors.Rocket-based combined-cycle engines.Supersonic combustion ramjet engines.Steffen Christopher J.1386995NASA Glenn Research Center,GPOGPOBOOK9910705619303321Fuel injector design optimization for an annular scramjet geometry3479308UNINA