02622oam 2200697 450 991071691280332120211129134148.0(CKB)5470000002527072(OCoLC)1156323998(EXLCZ)99547000000252707220200602d1939 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel investigation of effect of yaw on lateral-stability characteristicsIIRectangular N.A.C.A. 23012 wing with a circular fuselage and a fin /by M.J. Bamber and R.O. HouseWashington, [D.C.] :National Advisory Committee for Aeronautics,1939.1 online resource (9 pages, 11 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 730"September 1939."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 9).Rectangular N.A.C.A. 23012 wing with a circular fuselage and a finRectangular National Advisory Committee for Aeronautics 23012 wing with a circular fuselage and a finAirplanesWingsTestingAirplanesFuselageStability of airplanesRolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testingAirplanesFuselagefastAirplanesWingsTestingfastRolling (Aerodynamics)fastStability of airplanesfastWind tunnel testingfastYawing (Aerodynamics)fastAirplanesWingsTesting.AirplanesFuselage.Stability of airplanes.Rolling (Aerodynamics)Yawing (Aerodynamics)Wind tunnel testing.AirplanesFuselage.AirplanesWingsTesting.Rolling (Aerodynamics)Stability of airplanes.Wind tunnel testing.Yawing (Aerodynamics)Bamber M. J.1386953House R. O.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716912803321Wind-tunnel investigation of effect of yaw on lateral-stability characteristics3436290UNINA