02165oam 2200601 450 991071712510332120220211120250.0(CKB)5470000002528968(OCoLC)1156324027(EXLCZ)99547000000252896820200602d1940 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distributioin investigation of an N.A.C.A. 0009 airfoil with an 80-percent-chord plain flap and three tabs /by Milton B. Ames, Jr., and Richard I. SearsWashington, [D.C.] :National Advisory Committee for Aeronautics,1940.1 online resource (11 pages, 23 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 761"May 1940."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).AirplanesWingsTestingFlaps (Airplanes)AirplanesControl surfacesAerodynamic loadAerodynamic loadfastAirplanesControl surfacesfastAirplanesWingsTestingfastFlaps (Airplanes)fastAirplanesWingsTesting.Flaps (Airplanes)AirplanesControl surfaces.Aerodynamic load.Aerodynamic load.AirplanesControl surfaces.AirplanesWingsTesting.Flaps (Airplanes)Ames Milton B.Jr.,1401876Sears Richard I.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFXFFOCLCOGPOBOOK9910717125103321Pressure-distributioin investigation of an N.A.C.A. 0009 airfoil with an 80-percent-chord plain flap and three tabs3495043UNINA