02011oam 2200577 450 991071684970332120210930133732.0(CKB)5470000002525689(OCoLC)1159597685(EXLCZ)99547000000252568920200623d1938 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing /by R.O. HouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1938.1 online resource (6 pages, 7 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 663"September 1938."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 6).AirplanesModelsWingsFlaps (Airplanes)AileronsWind tunnel testingAileronsfastAirplanesModelsWingsfastFlaps (Airplanes)fastWind tunnel testingfastAirplanesModelsWings.Flaps (Airplanes)Ailerons.Wind tunnel testing.Ailerons.AirplanesModelsWings.Flaps (Airplanes)Wind tunnel testing.House R. O.1392490United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910716849703321The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing3547022UNINA