01787nam 2200457 450 991070570530332120170711083616.0(CKB)5470000002453359(OCoLC)993434099(EXLCZ)99547000000245335920170711j201705 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierExperimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 /Brian R. HollisHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,May 2017.1 online resource (viii, 168 pages) color illustrationsNASA/TM ;2017-219613"May 2017.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 15-16).Boundary layer transitionnasatHypersonic wind tunnelsnasatSurface roughnessnasatSurface roughness effectsnasatThermographynasatBoundary layer transition.Hypersonic wind tunnels.Surface roughness.Surface roughness effects.Thermography.Hollis Brian R(Brian Ray),1406209Langley Research Center,GPOGPOBOOK9910705705303321Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 103496045UNINA