01852nam 2200481 450 991070402530332120151113160621.0(CKB)5470000002437404(OCoLC)929073430(EXLCZ)99547000000243740420151113j201508 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of numerically simulated and experimentally measured performance of a rotating detonation engine /Daniel E. Paxson [and three others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,August 2015.1 online resource (10 pages) color illustrationsNASA/TM ;2015-218835Title from title screen (viewed on Nov. 13, 2015)."August 2015.""Prepared for SciTech 2015 sponsored by the American Institute of Aeronautics and Astronautics, Kissimmee, Florida, January 5-9, 2015.""AIAA-2015-1101."Includes bibliographical references (page 10).DetonationnasatComputational fluid dynamicsnasatInlet flownasatConvergent-divergent nozzlesnasatPotential flownasatDetonation.Computational fluid dynamics.Inlet flow.Convergent-divergent nozzles.Potential flow.Paxson Daniel E.1386438NASA Glenn Research Center,GPOGPOBOOK9910704025303321Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine3520147UNINA