02151oam 2200625I 450 991071364670332120200630125227.0(CKB)5470000002503207(OCoLC)1104148288(EXLCZ)99547000000250320720190610d1934 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /by Millard J. BamberWashington, [D.C.] :National Advisory Committee for Aeronautics,1934.1 online resource (8 pages, 3 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 493"March 1934"No Federal Depository Library Program (FDLP) item numberIncludes bibliographical references (page 8)AileronsAirplanesWingsRolling (Aerodynamics)Wind tunnel testingYawing (Aerodynamics)AileronsfastAirplanesWingsfastRolling (Aerodynamics)fastWind tunnel testingfastYawing (Aerodynamics)fastAilerons.AirplanesWings.Rolling (Aerodynamics)Wind tunnel testing.Yawing (Aerodynamics)Ailerons.AirplanesWings.Rolling (Aerodynamics)Wind tunnel testing.Yawing (Aerodynamics)Bamber M. J.1386953United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713646703321Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance3526012UNINA