02235oam 2200625 450 991071699050332120211026141217.0(CKB)5470000002526287(OCoLC)1154792930(EXLCZ)99547000000252628720200519d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distribution measurements on a tapered wing with a full-span split flap in curved flight /by Th. Troller and F. RokusWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (8 pages, 8 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 683"January 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 8).AirplanesWingsSplit flaps (Airplanes)Aerodynamic loadMeasurementRolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic loadMeasurementfastAirplanesWingsfastRolling (Aerodynamics)fastSplit flaps (Airplanes)fastYawing (Aerodynamics)fastAirplanesWings.Split flaps (Airplanes)Aerodynamic loadMeasurement.Rolling (Aerodynamics)Yawing (Aerodynamics)Aerodynamic loadMeasurement.AirplanesWings.Rolling (Aerodynamics)Split flaps (Airplanes)Yawing (Aerodynamics)Troller T.1414262Rokus Frank G.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716990503321Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight3512978UNINA