02010oam 2200589I 450 991070783570332120161223131258.0(CKB)5470000002468203(OCoLC)846317155(EXLCZ)99547000000246820320130602j199709 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions /Robert E. Bartels and John W. EdwardsHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,September 1997.1 online resource (13 pages) illustrationsNASA technical memorandum ;110272"September 1997.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 4).AirfoilsnasatCryogenicsnasatTransonic wind tunnelsnasatBuffetingnasatReynolds numbernasatHigh Reynolds numbernasatPressure measurementnasatAngle of attacknasatAirfoils.Cryogenics.Transonic wind tunnels.Buffeting.Reynolds number.High Reynolds number.Pressure measurement.Angle of attack.Bartels Robert E.106924Edwards John W.Langley Research Center,OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910707835703321Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions3488289UNINA