02052oam 2200553 450 991070749090332120160810111609.0(CKB)5470000002464615(OCoLC)784798060(OCoLC)995470000002464615(EXLCZ)99547000000246461520120408j197904 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /Robert M. Hall[Washington, D.C.] National Aeronautics and Space Administration, Scientific and Technical Information OfficeApril 19791 online resource (69 pages) illustrationsNASA technical paper ;1385Title from title screen (viewed on Aug. 10, 2016)."April 1979.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 22-23).AirfoilsnasatCryogenic wind tunnelsnasatPressure distributionnasatStagnation temperaturenasatSupercoolingnasatAirfoils.Cryogenic wind tunnels.Pressure distribution.Stagnation temperature.Supercooling.Hall Robert M.157258Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Office,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707490903321Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel3488837UNINA