01994oam 2200529 450 991071387990332120200825134918.0(CKB)5470000002504892(OCoLC)1104148324(EXLCZ)99547000000250489220190610d1956 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAnalysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel /by Stanley H. ScherWashington, [D.C.] :National Advisory Committee for Aeronautics,1956.1 online resource (54 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3611"April 1956."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 22).AirplanesTestingSpin (Aerodynamics)Wind tunnel testingAirplanesTestingfastSpin (Aerodynamics)fastWind tunnel testingfastAirplanesTesting.Spin (Aerodynamics)Wind tunnel testing.AirplanesTesting.Spin (Aerodynamics)Wind tunnel testing.Scher Stanley H.1416899United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713879903321Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel3523777UNINA