02193nam 2200553I 450 991070762590332120161013131212.0(CKB)5470000002466282(OCoLC)960642505(EXLCZ)99547000000246628220161013j199703 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEvaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /Scott R. Thomas, H. Douglas Perkins, and Charles J. TrefnyCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,March 1997.1 online resource (10 pages) illustrationsNASA technical memorandum ;107422"March 1997"--Report documentation page."Prepared for the 89th Symposium sponsored by the Propulsion and Energetics Panel of the NATO Advisory Group for Aerospace Research and Development, Palaiseau, France, April 14-17, 1997.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (page 4).EjectorsnasatHydrocarbon fuelsnasatWind tunnel testsnasatSupersonic speednasatMach numbernasatEngine testsnasatPropulsion system performancenasatFlow distributionnasatEjectors.Hydrocarbon fuels.Wind tunnel tests.Supersonic speed.Mach number.Engine tests.Propulsion system performance.Flow distribution.Thomas Scott R.1413894Perkins H. DouglasTrefny Charles J.GPOGPOBOOK9910707625903321Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight3511516UNINA