02161oam 2200613 450 991071715630332120220210084805.0(CKB)5470000002528653(OCoLC)1156324008(EXLCZ)99547000000252865320200602d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight /by Frank G. RokusWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (7 pages, 8 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 742"December 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 6).Aerodynamic loadFlaps (Airplanes)Split flaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic loadfastFlaps (Airplanes)fastRolling (Aerodynamics)fastSplit flaps (Airplanes)fastYawing (Aerodynamics)fastAerodynamic load.Flaps (Airplanes)Split flaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic load.Flaps (Airplanes)Rolling (Aerodynamics)Split flaps (Airplanes)Yawing (Aerodynamics)Rokus Frank G.1389134United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717156303321Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight3440303UNINA