01705oam 2200481 450 991070618680332120170821080814.0(CKB)5470000002454556(OCoLC)703664195(EXLCZ)99547000000245455620110224j199910 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEstimated benefits of variable-geometry wing camber control for transport aircraft /Alexander Bolonkin, Glenn B. GilyardEdwards, California :National Aeronautics and Space Administration, Dryden Flight Research Center,October 1999.1 online resource (v, 40 pages) illustrationsNASA/TM ;1999-206586"October 1999.""Performing organization: NASA Dryden Flight Research Center"--Report documentation page.Includes bibliographical references (pages 18-19).Wing cambernasatWind tunnel testsnasatTransport aircraftnasatAdaptive controlnasatCambered wingsnasatWing camber.Wind tunnel tests.Transport aircraft.Adaptive control.Cambered wings.Bolonkin Alexander1148258Gilyard Glenn B.Dryden Flight Research Facility,SSNSSNGPOBOOK9910706186803321Estimated benefits of variable-geometry wing camber control for transport aircraft3446818UNINA