02331oam 2200625 450 991070743860332120160825115306.0(CKB)5470000002465144(OCoLC)761200664(EXLCZ)99547000000246514420111115j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /Robert L. Stallings, Jr., and Milton Lamb[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (45 pages) illustrationsNASA technical paper ;1789Title from title screen (viewed on Aug. 23, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 17-18).Boundary layer flownasatBoundary layer stabilitynasatHeat transfernasatReynolds numbernasatWind tunnel testsnasatAerothermodynamicsfastBoundary layerfastSupersonic wind tunnelsfastBoundary layer flow.Boundary layer stability.Heat transfer.Reynolds number.Wind tunnel tests.Aerothermodynamics.Boundary layer.Supersonic wind tunnels.Stallings Robert L.1396665Lamb MiltonLangley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707438603321Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 33513904UNINA