02181oam 2200577 450 991071538550332120210212100721.0(CKB)5470000002510176(OCoLC)1146215374(EXLCZ)99547000000251017620200326d1933 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance /by M.J. Bamber and C.H. ZimmermanWashington [D.C.] :National Advisory Committee for Aeronautics,1933.1 online resource (11 pages, 8 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 474"November, 1933."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).AirplanesControl surfacesAirplanesTail surfacesPitching (Aerodynamics)MeasurementYawing (Aerodynamics)MeasurementSpin (Aerodynamics)AirplanesControl surfacesfastAirplanesTail surfacesfastSpin (Aerodynamics)fastAirplanesControl surfaces.AirplanesTail surfaces.Pitching (Aerodynamics)Measurement.Yawing (Aerodynamics)Measurement.Spin (Aerodynamics)AirplanesControl surfaces.AirplanesTail surfaces.Spin (Aerodynamics)Bamber M. J.1386953Zimmerman C. H.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715385503321Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance3497115UNINA