Buckling of moderately thick rectangular composite plates subjected to partial edge compression

DOI10.1016/S0020-7403(98)00009-5zbMath0957.74016OpenAlexW2040787184MaRDI QIDQ1960931

P. Sundaresan, G. Venkateswara Rao, Gajbir Singh

Publication date: 25 March 2001

Published in: International Journal of Mechanical Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0020-7403(98)00009-5

zbMATH Keywords

stability analysiscritical loadseight-node isoparametric plate elementmid-line symmetry conditionsmoderately thick laminated platespartial edge compressionpre-buckling stress analysis

Mathematics Subject Classification ID

Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60)

Related Items (2)

VIBRATION AND DYNAMIC INSTABILITY OF STIFFENED PLATES SUBJECTED TO IN-PLANE HARMONIC EDGE LOADING ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements – an addendum – A bibliography (1996‐1999)

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