01918oam 2200553 450 991071716000332120220210084613.0(CKB)5470000002528615(OCoLC)1156323832(EXLCZ)99547000000252861520200602d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierPressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs /by William G. Street and Milton B. Ames, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (11 pages, 31 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 734"November 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).AerofoilsAerodynamic loadFlaps (Airplanes)Aerodynamic loadfastAerofoilsfastFlaps (Airplanes)fastAerofoils.Aerodynamic load.Flaps (Airplanes)Aerodynamic load.Aerofoils.Flaps (Airplanes)Street William G.1418271Ames Milton B.Jr.,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFXFFOCLCOGPOBOOK9910717160003321Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs3529204UNINA