01872nam 2200481I 450 991070427760332120160202162800.0(CKB)5470000002438896(OCoLC)936387373(EXLCZ)99547000000243889620160202j201509 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierCFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /David O. DavisCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,September 2015.1 online resource (13 pages) color illustrationsNASA/TM ;2015-218841Title from title screen (viewed on Feb. 2, 2016)."September 2015.""Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015Includes bibliographical references (page 13).Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interactionBoundary layersnasatComputational fluid dynamicsnasatShock wave interactionnasatFlow measurementnasatTurbulent flownasatBoundary layers.Computational fluid dynamics.Shock wave interaction.Flow measurement.Turbulent flow.Davis David O.1402770NASA Glenn Research Center,GPOGPOBOOK9910704277603321CFD validation experiment of a Mach 2.5 axisymmetric shock-wave3500659UNINA