02286oam 2200649 450 991071715970332120220210084950.0(CKB)5470000002528618(OCoLC)1156323833(EXLCZ)99547000000252861820200602d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight /by Th. Troller and F. RokusWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (6 pages, 6 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 735"November 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).Aerodynamic loadAirplanesWingsTestingFlaps (Airplanes)Split flaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic loadfastAirplanesWingsTestingfastFlaps (Airplanes)fastRolling (Aerodynamics)fastSplit flaps (Airplanes)fastAerodynamic load.AirplanesWingsTesting.Flaps (Airplanes)Split flaps (Airplanes)Rolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic load.AirplanesWingsTesting.Flaps (Airplanes)Rolling (Aerodynamics)Split flaps (Airplanes)Troller T.1414262Rokus Frank G.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717159703321Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight3529203UNINA