01766oam 2200517 450 991071341150332120200505132647.0(CKB)5470000002501543(OCoLC)1121049812(EXLCZ)99547000000250154320190926d1924 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierOn the distribution of lift along the span of an airfoil with displaced ailerons /by Max M. Munk[Washington, D.C.] :National Advisory Committee for Aeronautics,1924.1 online resource (7 pages, 1 unnumbered page) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 195"June, 1924."No Federal Depository Library Program (FDLP) item number.Includes bibliographical reference (page 1).AileronsFlaps (Airplanes)Lift (Aerodynamics)Aerodynamic loadAerodynamic loadfastLift (Aerodynamics)fastAilerons.Flaps (Airplanes)Lift (Aerodynamics)Aerodynamic load.Aerodynamic load.Lift (Aerodynamics)Munk Max M(Max Michael),1890-1386130United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713411503321On the distribution of lift along the span of an airfoil with displaced ailerons3525994UNINA