02158oam 2200601 450 991071673410332120210825112211.0(CKB)5470000002524836(OCoLC)1159597686(EXLCZ)99547000000252483620200623d1938 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tailsIIIMass distributed along the wings /by Oscar Seidman and A.I. NeihouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1938.1 online resource (12 pages, 17 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 664"September 1938."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 12).Mass distributed along the wingsAirplanesWingsAirplanesTail surfacesSpin (Aerodynamics)Wind tunnel testingAirplanesTail surfacesfastAirplanesWingsfastSpin (Aerodynamics)fastWind tunnel testingfastAirplanesWings.AirplanesTail surfaces.Spin (Aerodynamics)Wind tunnel testing.AirplanesTail surfaces.AirplanesWings.Spin (Aerodynamics)Wind tunnel testing.Seidman Oscar1405963Neihouse A. I.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910716734103321Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails3483584UNINA