01812oam 2200505Ka 450 991069899310332120100323102926.0(CKB)5470000002397940(OCoLC)387723198(EXLCZ)99547000000239794020090611d1989 ua 0engtxtrdacontentcrdamediacrrdacarrierAn integrating matrix formulation for buckling of rotating beams including the effects of concentrated masses[electronic resource] /William D. Lakin, Raymond G. KvaternikHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[1989]1 volumeICASE report ;no. 89-39NASA contractor report ;181862Title from title screen (viewed June 10, 2009)"Institute for Computer Applications in Science and Engineering."Beams (supports)nasatBucklingnasatFlexible bodiesnasatMassnasatRotating bodiesnasatStructural stabilitynasatBeams (supports)Buckling.Flexible bodies.Mass.Rotating bodies.Structural stability.Lakin William D726167Kvaternik Raymond G1393658Institute for Computer Applications in Science and Engineering.Langley Research Center.GPOGPOGPOBOOK9910698993103321An integrating matrix formulation for buckling of rotating beams including the effects of concentrated masses3530392UNINA