01984oam 2200553 450 991071712570332120220211111642.0(CKB)5470000002528962(OCoLC)1156324025(EXLCZ)99547000000252896220200602d1940 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 30-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 (14 pages, 29 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 759"May 1940."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 14).AirplanesModelsWingsFlaps (Airplanes)Wind tunnel testingAirplanesModelsWingsfastFlaps (Airplanes)fastWind tunnel testingfastAirplanesModelsWings.Flaps (Airplanes)Wind tunnel testing.AirplanesModelsWings.Flaps (Airplanes)Wind tunnel testing.Ames Milton B.Jr.,1401876Sears Richard I.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFXFFOCLCOGPOBOOK9910717125703321Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 30-percent-chord plain flap and three tabs3471200UNINA