01947oam 2200565 450 991071534430332120210226134523.0(CKB)5470000002510592(OCoLC)1145759610(EXLCZ)99547000000251059220200323d1934 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel measurements of air loads on split flaps /by Carl J. WenzingerWashington, [D.C.] :National Advisory Committee for Aeronautics,1934.1 online resource (8 pages, 7 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 498"May 1934."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 7).AirplanesModelsWingsSplit flaps (Airplanes)Aerodynamic loadWind tunnel testingAerodynamic loadfastAirplanesModelsWingsfastSplit flaps (Airplanes)fastWind tunnel testingfastAirplanesModelsWings.Split flaps (Airplanes)Aerodynamic load.Wind tunnel testing.Aerodynamic load.AirplanesModelsWings.Split flaps (Airplanes)Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715344303321Wind-tunnel measurements of air loads on split flaps3472559UNINA