01968oam 2200577I 450 991071364610332120200630130639.0(CKB)5470000002503213(OCoLC)1104148274(EXLCZ)99547000000250321320190610d1934 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic effects of a split flap on the spinning characteristics of a monoplane model /by M.J. BamberWashington, [D.C.] :National Advisory Committee for Aeronautics,1934.1 online resource (8 pages, 5 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 515"December 1934"No Federal Depository Library Program (FDLP) item numberIncludes bibliographical references (page 8)AerodynamicsSpin (Aerodynamics)Split flaps (Airplanes)Wind tunnel testingAerodynamicsfastSpin (Aerodynamics)fastSplit flaps (Airplanes)fastWind tunnel testingfastAerodynamics.Spin (Aerodynamics)Split flaps (Airplanes)Wind tunnel testing.Aerodynamics.Spin (Aerodynamics)Split flaps (Airplanes)Wind tunnel testing.Bamber M. J.1386953United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713646103321Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model3450762UNINA