02426oam 2200637 450 991070735560332120160719143723.0(CKB)5470000002463962(OCoLC)844670629(EXLCZ)99547000000246396220130526j199606 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierRocket-based combined cycle engine technology development inlet CFD validation and application /J.R. DeBonis and S. YungsterCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,June 1996.1 online resource (18 pages) illustrationsNASA technical memorandum ;107274Title from title screen (viewed July 19, 2016)."June 1996"--Report documentation page."Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page."ICOMP-96-6.""AIAA-96-3145."Includes bibliographical references (pages 7-8).Rocket-based combined cycle engine technology development Rocket engine designnasatRocket enginesnasatEngine inletsnasatNavier-Stokes equationnasatComputational fluid dynamicsnasatJet enginesAir intakesfastRocket enginesfastRocket engine design.Rocket engines.Engine inlets.Navier-Stokes equation.Computational fluid dynamics.Jet enginesAir intakes.Rocket engines.DeBonis James R.1387413Yungster ShayeLewis Research Center,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910707355603321Rocket-based combined cycle engine technology development3546766UNINA