02805oam 2200841 450 991070971280332120180828111904.0(CKB)5470000002473122(OCoLC)761308948(OCoLC)995470000002473122(EXLCZ)99547000000247312220111115j198605 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierR4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /Renaldo V. JenkinsWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,May 1986.1 online resource (111 pages) illustrationsNASA/TP ;2565Prepared at Langley Research Center."May 1986."Includes bibliographical references (pages 9-10).AirfoilsnasatReynolds numbernasatTransonic wind tunnelsnasatMach numbernasatBoundary layersnasatAerofoilsTestingStatisticsReynolds numberTransonic wind tunnelsWall pressure (Aerodynamics)Boundary layerAerofoilsTestingfastBoundary layerfastReynolds numberfastTransonic wind tunnelsfastWall pressure (Aerodynamics)fastStatistics.fastStatistics.lcgftAirfoils.Reynolds number.Transonic wind tunnels.Mach number.Boundary layers.AerofoilsTestingReynolds number.Transonic wind tunnels.Wall pressure (Aerodynamics)Boundary layer.AerofoilsTesting.Boundary layer.Reynolds number.Transonic wind tunnels.Wall pressure (Aerodynamics)Jenkins Renaldo V.1409222United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOMERUCGPOBOOK9910709712803321R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel3495076UNINA