01831nam 2200481 450 991070612020332120170914100726.0(CKB)5470000002455228(OCoLC)1003643373(EXLCZ)99547000000245522820170914j199912 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSubsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /Bryan A. Campbell [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1999.1 online resource (103 pages) illustrationsNASA/TM ;1999-209701"December 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 102-103 ).Subsonic wind tunnelsnasatLeading edge flapsnasatVorticesnasatSupersonic transportsnasatAerodynamic configurationsnasatSeparated flownasatSubsonic wind tunnels.Leading edge flaps.Vortices.Supersonic transports.Aerodynamic configurations.Separated flow.Campbell Bryan A.1395236Langley Research Center,GPOGPOBOOK9910706120203321Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration3453410UNINA