01911oam 2200565 450 991071341640332120200504144444.0(CKB)5470000002501493(OCoLC)1121049808(EXLCZ)99547000000250149320190926d1924 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe induction factor used for computing the rolling moment due to the ailerons /by Max M. Munk[Washington, D.C.] :National Advisory Committee for Aeronautics,1924.1 online resource (4 pages, 1 unnumbered page) illustrationTechnical notes / National Advisory Committee for Aeronautics ;No. 187"April, 1924."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 1).AileronsRolling (Aerodynamics)Flaps (Airplanes)AerodynamicsMathematical modelsAerodynamicsfastMathematical modelsfastRolling (Aerodynamics)fastAilerons.Rolling (Aerodynamics)Flaps (Airplanes)Aerodynamics.Mathematical models.Aerodynamics.Mathematical models.Rolling (Aerodynamics)Munk Max M(Max Michael),1890-1386130United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713416403321The induction factor used for computing the rolling moment due to the ailerons3526001UNINA