02019nam 2200529 450 991070588910332120170815101723.0(CKB)5470000002453522(OCoLC)994007818(EXLCZ)99547000000245352220170718j200210 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierMultiple-cycle simulation of a pulse detonation engine ejector /S. Yungster, H.D. PerkinsCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,October 2002.1 online resource (10 pages) illustrationNASA/TM ;2002-211888"October 2002.""Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page."ICOMP-2002-05.""AIAA-2002-3630."Includes bibliographical references (pages 4-5).Detonable gas mixturesnasatEjectorsnasatImpulsesnasatMass flow ratenasatPulse detonation enginesnasatShock wavesnasatDetonable gas mixtures.Ejectors.Impulses.Mass flow rate.Pulse detonation engines.Shock waves.Yungster Shaye1401113Perkins Hugh DouglasNASA Glenn Research Center.Institute for Computational Mechanics in Propulsion,GPOGPOBOOK9910705889103321Multiple-cycle simulation of a pulse detonation engine ejector3469337UNINA