01882oam 2200529I 450 991071397650332120201001141700.0(CKB)5470000002505895(OCoLC)1136490294(EXLCZ)99547000000250589520200116d1930 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe effect of wing tip floating ailerons on the autorotation of a monoplane wing model /by Montgomery Knight and Carl J. WenzingerWashington, [D.C.] :National Advisory Committee for Aeronautics,1930.1 online resource (19 pages, 6 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 336"March, 1930."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 13).AileronsFlaps (Airplanes)Rolling (Aerodynamics)Wind tunnel testingRolling (Aerodynamics)fastWind tunnel testingfastAilerons.Flaps (Airplanes)Rolling (Aerodynamics)Wind tunnel testing.Rolling (Aerodynamics)Wind tunnel testing.Knight Montgomery1390967Wenzinger Carl J(Carl Joseph),1903-1988,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713976503321The effect of wing tip floating ailerons on the autorotation of a monoplane wing model3446722UNINA