02154oam 2200517 450 991070701020332120160405141651.0(CKB)5470000002461390(OCoLC)703661229(EXLCZ)99547000000246139020110224j199706 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFlight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /Sheryll Goecke Powers and Lannie D. Webb[Washington, D.C.] National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information ProgramJune 19971 online resource (v, 850 pages) illustrationsNASA technical memorandum ;4789Title from title screen (viewed April 5, 2016)."June 1997.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (pages 849-850).Boundary layersnasatPressure distributionnasatSupercritical wingsnasatF-111 aircraftnasatWing cambernasatBoundary layers.Pressure distribution.Supercritical wings.F-111 aircraft.Wing camber.Powers Sheryll Goecke1418307Webb Lannie D.NASA Dryden Flight Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,United States.National Aeronautics and Space Administration,SSNSSNGPOBOOK9910707010203321Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing3529337UNINA