An improved arc-length method for postbuckling analysis of composite cylindrical panels

DOI10.1016/0045-7949(94)90099-XzbMath0880.73067OpenAlexW2067813486MaRDI QIDQ3129659

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Publication date: 5 February 1998

Published in: Computers & Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7949(94)90099-x

zbMATH Keywords

axial compressionangle-ply laminatesupdated Lagrangian formulationcross-ply laminateeight-node degenerate shell elementquasi-isotropic laminates

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Membranes (74K15)

Related Items (3)

Nonlinear response of imperfect eccentrically stiffened FGM cylindrical panels on elastic foundation subjected to mechanical loads ⋮ Nonlinear buckling and post-buckling of imperfect FG porous sandwich cylindrical panels subjected to axial loading under various boundary conditions ⋮ Arc-length technique for nonlinear finite element analysis

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