02117oam 2200589 450 991071673490332120210825101626.0(CKB)5470000002524828(OCoLC)1159597612(EXLCZ)99547000000252482820200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tailsIBasic loading condition /by Oscar Seidman and A.I. NeihouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (13 pages, 17 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 608"August 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 12-13).Basic loading conditionSpin (Aerodynamics)AirplanesWingsAirplanesTail surfacesWind tunnel testingAirplanesTail surfacesfastAirplanesWingsfastSpin (Aerodynamics)fastWind tunnel testingfastSpin (Aerodynamics)AirplanesWings.AirplanesTail surfaces.Wind tunnel testing.AirplanesTail surfaces.AirplanesWings.Spin (Aerodynamics)Wind tunnel testing.Seidman Oscar1405963Neihouse A. I.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716734903321Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails3483584UNINA