02562oam 2200733 450 991071673450332120210825104918.0(CKB)5470000002524832(OCoLC)1159597641(EXLCZ)99547000000252483220200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tailsIIMass distributed along the fuselage /by Oscar Seidman and A.I. NeihouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (11 pages, 17 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 630"December 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).Mass distributed along the fuselageSpin (Aerodynamics)AirplanesFuselageAirplanesTail surfacesAirplanesWingsMass (Physics)Wind tunnel testingAerodynamic loadAerodynamic loadfastAirplanesFuselagefastAirplanesTail surfacesfastAirplanesWingsfastMass (Physics)fastSpin (Aerodynamics)fastWind tunnel testingfastSpin (Aerodynamics)AirplanesFuselage.AirplanesTail surfaces.AirplanesWings.Mass (Physics)Wind tunnel testing.Aerodynamic load.Aerodynamic load.AirplanesFuselage.AirplanesTail surfaces.AirplanesWings.Mass (Physics)Spin (Aerodynamics)Wind tunnel testing.Seidman Oscar1405963Neihouse A. I.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716734503321Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails3483584UNINA