02004oam 2200565 450 991071335840332120200401074906.0(CKB)5470000002500059(OCoLC)1111633657(EXLCZ)99547000000250005920190806d1923 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /by Max M. Munk[Washington, D.C.] :National Advisory Committee for Aeronautics,1923.1 online resource (9 pages, 2 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 122"January, 1923."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 1).Lift (Aerodynamics)Angle of attack (Aerodynamics)AerofoilsCamber (Aerofoils)AerofoilsfastAngle of attack (Aerodynamics)fastCamber (Aerofoils)fastLift (Aerodynamics)fastLift (Aerodynamics)Angle of attack (Aerodynamics)Aerofoils.Camber (Aerofoils)Aerofoils.Angle of attack (Aerodynamics)Camber (Aerofoils)Lift (Aerodynamics)Munk Max M(Max Michael),1890-1386130United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCFOCLCOGPOBOOK9910713358403321The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals3526198UNINA