02196oam 2200613 450 991071716680332120220210082104.0(CKB)5470000002528547(OCoLC)1154792557(EXLCZ)99547000000252854720200519d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing /by Rufus O. HouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (5 pages, 5 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 719"July 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).AirplanesModelsWingsSlotted flaps (Airplanes)Flaps (Airplanes)AerodynamicsWind tunnel testingAerodynamicsfastAirplanesModelsWingsfastFlaps (Airplanes)fastSlotted flaps (Airplanes)fastWind tunnel testingfastAirplanesModelsWings.Slotted flaps (Airplanes)Flaps (Airplanes)Aerodynamics.Wind tunnel testing.Aerodynamics.AirplanesModelsWings.Flaps (Airplanes)Slotted flaps (Airplanes)Wind tunnel testing.House R. O.1392490United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717166803321The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing3529206UNINA