01725oam 2200469 450 991071538590332120210212090305.0(CKB)5470000002510172(OCoLC)1146215365(EXLCZ)99547000000251017220200326d1933 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing /by Carl J. WenzingerWashington [D.C.] :National Advisory Committee for Aeronautics,1933.1 online resource (5 pages, 4 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 472"September, 1933."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 4).AirplanesModelsWingsWind tunnel testingAirplanesModelsWingsfastWind tunnel testingfastAirplanesModelsWings.Wind tunnel testing.AirplanesModelsWings.Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715385903321The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing3541814UNINA