01820nam 2200481 450 991070726790332120160608090639.0(CKB)5470000002462827(OCoLC)951418247(EXLCZ)99547000000246282720160608j201604 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierImpact of an exhaust throat on semi-idealized rotating detonation engine performance /Daniel E. PaxsonCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,April 2016.1 online resource (12 pages) color illustrationsNASA/TM ;2016-219076Title from title screen (viewed on June 8, 2016)."April 2016.""Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016.""AIAA-2016-11647."Includes bibliographical references (pages 11-12).Computational fluid dynamicsnasatExhaust flow simulationnasatFuel flownasatInviscid flownasatPropulsion system performancenasatComputational fluid dynamics.Exhaust flow simulation.Fuel flow.Inviscid flow.Propulsion system performance.Paxson Daniel E.1386438NASA Glenn Research Center,GPOGPOBOOK9910707267903321Impact of an exhaust throat on semi-idealized rotating detonation engine performance3539463UNINA