01932oam 2200565 450 991071672110332120210831134942.0(CKB)5470000002524968(OCoLC)1159597638(EXLCZ)99547000000252496820200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure distribution over a Clark Y-H airfoil section with a split flap /by Carl J. WenzingerWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (5 pages, 6 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 627"December 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).AerofoilsSplit flaps (Airplanes)Aerodynamic loadWind tunnel testingAerodynamic loadfastAerofoilsfastSplit flaps (Airplanes)fastWind tunnel testingfastAerofoils.Split flaps (Airplanes)Aerodynamic load.Wind tunnel testing.Aerodynamic load.Aerofoils.Split flaps (Airplanes)Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716721103321Pressure distribution over a Clark Y-H airfoil section with a split flap3459782UNINA