01915nam 2200517I 450 991070529730332120140320153822.0(CKB)5470000002448389(OCoLC)873950466(EXLCZ)99547000000244838920140319d1983 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades /F. Sisto and A.T. ChangHoboken, N.J. :Department of Mechanical Engineering, Stevens Institute of Technology ;Cleveland, Ohio :Lewis Research Center, National Aeronautics and Space Administration,1983.1 online resource (95 pages, 19 unnumbered pages) illustrationsNASA-CR ;175444Title from title screen (viewed on Mar. 19, 2014)."December 1983.""Report no. ME-RT-82006."Includes bibliographical references (pages 94-95).Cantilever membersnasatDynamic structural analysisnasatFinite element methodnasatForced vibrationnasatPrecessionnasatTurbomachine bladesnasatCantilever members.Dynamic structural analysis.Finite element method.Forced vibration.Precession.Turbomachine blades.Sisto Fernando1401958Chang A. T.Stevens Institute of Technology,Lewis Research Center,GPOGPOBOOK9910705297303321The influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades3471452UNINA