02175oam 2200625I 450 991071365030332120210104152957.0(CKB)5470000002503171(OCoLC)1100474465(EXLCZ)99547000000250317120190508d1932 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /by Fred E. Weick and Thomas A. HarrisWashington, [D.C.] :National Advisory Committee for Aeronautics,1932.1 online resource (7 pages, 11 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 422"May, 1932."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 6).Wind tunnel testingSplit flaps (Airplanes)AirplanesModelsWingsTrailing edge flapsTrailing edge flapsfastAirplanesModelsWingsfastSplit flaps (Airplanes)fastWind tunnel testingfastWind tunnel testing.Split flaps (Airplanes)AirplanesModelsWings.Trailing edge flaps.Trailing edge flaps.AirplanesModelsWings.Split flaps (Airplanes)Wind tunnel testing.Weick Fred E.1387817Harris Thomas A.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOMUBOCLGPOBOOK9910713650303321The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear3476038UNINA