01993nam 2200505I 450 991070243090332120141203130447.0(CKB)5470000002427862(OCoLC)897378500(EXLCZ)99547000000242786220141203j201310 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierUnderstanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses /David J. FriedlanderCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,October 2013.1 online resource (xvi, 105 pages) color illustrationsNASA/TM ;2013-218081Title from title screen (viewed on Dec. 3, 2014)."October 2013."Includes bibliographical references (pages 58-63).Understanding the flow physics of shock boundary layer interactions using Computational Fluid Dynamics and numerical analysesComputational fluid dynamicsnasatShock wave interactionnasatBoundary layersnasatFlow distributionnasatParticle image velocimetrynasatLarge eddy simulationnasatComputational fluid dynamics.Shock wave interaction.Boundary layers.Flow distribution.Particle image velocimetry.Large eddy simulation.Friedlander David J.1398592NASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702430903321Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses3473449UNINA