02055oam 2200565 450 991071710880332120220222142033.0(CKB)5470000002529132(OCoLC)1158388801(EXLCZ)99547000000252913220200615d1940 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel investigation of fuselage stability in yaw with various arrangements of fins /by H. Page Hoggard, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1940.1 online resource (7 pages, 8 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;no. 785"November 1940."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 7).AirplanesFuselageTestingAirplanesControl surfacesStability of airplanesWind tunnel testingAirplanesControl surfacesfastAirplanesFuselageTestingfastStability of airplanesfastWind tunnel testingfastAirplanesFuselageTesting.AirplanesControl surfaces.Stability of airplanes.Wind tunnel testing.AirplanesControl surfaces.AirplanesFuselageTesting.Stability of airplanes.Wind tunnel testing.Hoggard H. Page1416725United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910717108803321Wind-tunnel investigation of fuselage stability in yaw with various arrangements of fins3522969UNINA