02122oam 2200541 450 991070746710332120160817101400.0(CKB)5470000002464856(OCoLC)761455916(EXLCZ)99547000000246485620111115j198011 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,November 1980.1 online resource (18 pages) illustrationsNASA technical paper ;1752Title from title screen (viewed on Aug. 17, 2016)."November 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 11).Mach numbernasatPressure measurementnasatReynolds numbernasatTransonic wind tunnelsnasatWind tunnel calibrationnasatMach number.Pressure measurement.Reynolds number.Transonic wind tunnels.Wind tunnel calibration.Lawing Pierce L.1408115Adcock Jerry B.Ladson Charles L.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCOGPOBOOK9910707467103321A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel3492835UNINA