Thermal buckling behaviour of composite laminated plates with a circular hole

Wann Jane Chen; Psang Dain Lin; Lien Wen Chen

doi:10.1016/0263-8223(91)90005-J

Thermal buckling behaviour of composite laminated plates with a circular hole

Wann Jane Chen, Psang Dain Lin, Lien Wen Chen

Department of Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

14 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 language	English
Pages (from-to)	379-397
Number of pages	19
Journal	Composite Structures
Volume	18
Issue number	4
DOIs	https://doi.org/10.1016/0263-8223(91)90005-J
Publication status	Published - 1991

All Science Journal Classification (ASJC) codes

Ceramics and Composites
Civil and Structural Engineering

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10.1016/0263-8223(91)90005-J

Cite this

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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.",

author = "Chen, {Wann Jane} and Lin, {Psang Dain} and Chen, {Lien Wen}",

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AB - 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.

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Thermal buckling behaviour of composite laminated plates with a circular hole

Abstract

All Science Journal Classification (ASJC) codes

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