Thermal buckling behaviour of composite laminated plates with a circular hole

Wann Jane Chen, Psang-Dain Lin, Lien-Wen Chen

Research output: Contribution to journalArticle

11 Citations (Scopus)

Abstract

Thermal buckling of antisymmetric cross-ply laminates having central circular holes subjected to uniform or non-uniform temperature distribution are analysed by the finite element method. To account for the transverse shear deformation, the thermo-elastic Mindlin plate theory is used. Numerical results show that significant reduction of the critical buckling temperature occurs for laminates having a central hole.

Original languageEnglish
Pages (from-to)379-397
Number of pages19
JournalComposite Structures
Volume18
Issue number4
DOIs
Publication statusPublished - 1991 Jan 1

Fingerprint

Laminated composites
Laminates
Buckling
Mindlin plates
Shear deformation
Temperature distribution
Finite element method
Temperature
Hot Temperature

All Science Journal Classification (ASJC) codes

  • Civil and Structural Engineering
  • Ceramics and Composites

Cite this

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Thermal buckling behaviour of composite laminated plates with a circular hole. / Chen, Wann Jane; Lin, Psang-Dain; Chen, Lien-Wen.

In: Composite Structures, Vol. 18, No. 4, 01.01.1991, p. 379-397.

Research output: Contribution to journalArticle

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