02267oam 2200649I 450 991071375610332120200730145637.0(CKB)5470000002504122(OCoLC)1104148275(EXLCZ)99547000000250412220190610d1950 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel /by Ralph W. Stone, Jr., Sanger M. Burk, Jr., and William Bihrle, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1950.1 online resource (59 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2181"September 1950."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 25-26).AerodynamicsAirplanesModelsTestingFighter planesSpin (Aerodynamics)Wind tunnel testingAerodynamicsfastAirplanesModelsTestingfastFighter planesfastSpin (Aerodynamics)fastWind tunnel testingfastAerodynamics.AirplanesModelsTesting.Fighter planes.Spin (Aerodynamics)Wind tunnel testing.Aerodynamics.AirplanesModelsTesting.Fighter planes.Spin (Aerodynamics)Wind tunnel testing.Stone Ralph W.1399791Bihrle WilliamBurk Sanger M.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713756103321The aerodynamic forces and moments on a 13465692UNINA