01787nam 2200493 450 991070273500332120150227082241.0(CKB)5470000002430851(OCoLC)904125145(EXLCZ)99547000000243085120150227j201403 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBuckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory /Michael P. NemethHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,March 2014.1 online resource (408 pages) color illustrationsNASA/TM ;2014-218176Title from title screen (viewed Feb. 27, 2015)."March 2014."Includes bibliographical references (pages 131-138).Nonlinear equationsnasatRayleigh-Ritz methodnasatShell theorynasatShell stabilitynasatAnisotropic shellsnasatDonnell equationsnasatNonlinear equations.Rayleigh-Ritz method.Shell theory.Shell stability.Anisotropic shells.Donnell equations.Nemeth Michael P.1391721Langley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702735003321Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory3481438UNINA