Buckling analyses of fiber-composite laminate plates with material nonlinearity

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12 Citations (Scopus)


A nonlinear material constitutive model, including a nonlinear in-plane shear formulation and a failure criterion, for fiber-composite laminate materials is employed to carry out finite element buckling analyses for composite plates under uniaxial compressive loads. It has been shown that the nonlinear in-plane shear together with the failure criterion have significant influence on the buckling behavior of composite laminate plates.

Original languageEnglish
Pages (from-to)169-179
Number of pages11
JournalFinite Elements in Analysis and Design
Issue number3
Publication statusPublished - 1995 Apr

All Science Journal Classification (ASJC) codes

  • Analysis
  • Engineering(all)
  • Computer Graphics and Computer-Aided Design
  • Applied Mathematics


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