02053oam 2200517 450 991071691250332120211129142724.0(CKB)5470000002527075(OCoLC)1286629299(EXLCZ)99547000000252707520211129d1941 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel investigation of effect of yaw on lateral-stability characteristicsIIISymmetrically tapered wing at various positions on circular fuselage with and without a vertical tail /by Isidore G. Recant and Arthur R. WallaceWashington, [D.C.] :National Advisory Committee for Aeronautics,1941.1 online resource (12 pages, 12 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 825"September 1941."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 12).Symmetrically tapered wing at various positions on circular fuselage with and without a vertical tailAirplanesWingsTestingAirplanesFuselageStability of airplanesRolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testingAirplanesWingsTesting.AirplanesFuselage.Stability of airplanes.Rolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testing.Recant Isidore G.1386872Wallace Arthur R.United States.National Advisory Committee for Aeronautics,GPOGPOGPOBOOK9910716912503321Wind-tunnel investigation of effect of yaw on lateral-stability characteristics3523012UNINA