01927oam 2200529I 450 991070745840332120160818163128.0(CKB)5470000002464944(OCoLC)760936051(EXLCZ)99547000000246494420111114j198011 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierIn-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 /Robert D. Quinn and Leslie Gong[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,November1980.1 online resource (49 pages) illustrationsNASA technical paper ;1764Title from title screen (viewed on Aug. 18, 2016)."November1980.""Performing Organization: NASA Dryden Flight Research Center"--Report documentation page.Includes bibliographical references (pages 18-19).Heat transfer coefficientsnasatMach numbernasatReynolds numbernasatShear flownasatHeat transfer coefficients.Mach number.Reynolds number.Shear flow.Quinn Robert D.142872Gong LeslieHugh L. Dryden Flight Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707458403321In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.03474760UNINA