01803nam 2200481I 450 991070719630332120160426150632.0(CKB)5470000002461530(OCoLC)947887365(EXLCZ)99547000000246153020160426j201512 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierSecondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone /Fei Li [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 2015.1 online resource (24 pages) color illustrationsNASA/TM ;2015-218997Title from title screen (viewed April 26, 2016)."December 2015.""Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.Includes bibliographical references (pages 20-24).Boundary layer flownasatCircular conesnasatCross flownasatHypersonic boundary layernasatVorticesnasatBoundary layer flow.Circular cones.Cross flow.Hypersonic boundary layer.Vortices.Li Fei1406930Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707196303321Secondary instability of stationary crossflow vortices in Mach 6 boundary layer over a circular cone3487092UNINA