02094oam 2200613I 450 991070790530332120170228101331.0(CKB)5470000002469520(OCoLC)844684497(EXLCZ)99547000000246952020130526j199703 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierWind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /Brenda E. Gile Laflin, Zachary T. Applin, and Kenneth M. JonesHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,March 1997.1 online resource (127 pages) illustrationsNASA technical memorandum ;110304"March 1997.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (page 9).Angle of attacknasatMach numbernasatPressure distributionnasatReynolds numbernasatSideslipnasatSubsonic speednasatWingsnasatAerodynamic characteristicsnasatWind tunnel testsnasatAngle of attack.Mach number.Pressure distribution.Reynolds number.Sideslip.Subsonic speed.Wings.Aerodynamic characteristics.Wind tunnel tests.Laflin Brenda E. Gile1410731Applin Zachary T.Jones Kenneth M.Langley Research Center,OCLCEOCLCEOCLCOOCLCQGPOBOOK9910707905303321Wind tunnel results of the aerodynamic performance of a 13500059UNINA