01803oam 2200517 450 991071602160332120210528122054.0(CKB)5470000002517892(OCoLC)1150919729(EXLCZ)99547000000251789220200416d1936 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffect of changes in tail arrangement upon the spinning of a low-wing monoplane model /by C.H. ZimmermanWashington, [D.C.] :National Advisory Committee for Aeronautics,1936.1 online resource (8 pages, 4 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 570"June 1936."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 8).AirplanesTail surfacesAir flowSpin (Aerodynamics)Air flowfastAirplanesTail surfacesfastSpin (Aerodynamics)fastAirplanesTail surfaces.Air flow.Spin (Aerodynamics)Air flow.AirplanesTail surfaces.Spin (Aerodynamics)Zimmerman Charles Horton1908-1996,1407431United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716021603321Effect of changes in tail arrangement upon the spinning of a low-wing monoplane model3488880UNINA