02153oam 2200625 450 991071687400332120210921141936.0(CKB)5470000002525444(OCoLC)1159597665(EXLCZ)99547000000252544420200623d1938 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel tests of a Clark Y wing having split flaps with gaps /by Carl J. WenzingerWashington, [D.C.] :National Advisory Committee for Aeronautics,1938.1 online resource (4 pages, 3 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 650"May 1938."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 4).AirplanesModelsWingsSplit flaps (Airplanes)Lift (Aerodynamics)Drag (Aerodynamics)Wind tunnel testingAirplanesModelsWingsfastDrag (Aerodynamics)fastLift (Aerodynamics)fastSplit flaps (Airplanes)fastWind tunnel testingfastAirplanesModelsWings.Split flaps (Airplanes)Lift (Aerodynamics)Drag (Aerodynamics)Wind tunnel testing.AirplanesModelsWings.Drag (Aerodynamics)Lift (Aerodynamics)Split flaps (Airplanes)Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910716874003321Wind-tunnel tests of a Clark Y wing having split flaps with gaps3459727UNINA