01842nam 2200505I 450 991070273080332120150327154009.0(CKB)5470000002430893(OCoLC)905724843(EXLCZ)99547000000243089320150327j201409 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierAFC-enabled simplified high-lift system integration study /Peter M. Hartwich [and seven others]Hampton, Virginia. :National Aeronautics and Space Administration, Langley Research Center,September 2014.1 online resource (v, 31 pages) color illustrations, mapsNASA/CR ;2014-218521Title from title screen (viewed March 27, 2015)."September 2014."Includes bibliographical references (page 14).Active Flow Control enabled simplified high lift system integration studyLift devicesnasatLeading edge slatsnasatAerodynamic characteristicsnasatNavier-Stokes equationnasatTrailing edge flapsnasatDrooped airfoilsnasatLift devices.Leading edge slats.Aerodynamic characteristics.Navier-Stokes equation.Trailing edge flaps.Drooped airfoils.Hartwich Peter M.1387208Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702730803321AFC-enabled simplified high-lift system integration study3451028UNINA