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 | |
| Publication status | Published - 1991 Jan 1 |
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All Science Journal Classification (ASJC) codes
- Civil and Structural Engineering
- Ceramics and Composites
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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 journal › Article
TY - JOUR
T1 - Thermal buckling behaviour of composite laminated plates with a circular hole
AU - Chen, Wann Jane
AU - Lin, Psang-Dain
AU - Chen, Lien-Wen
PY - 1991/1/1
Y1 - 1991/1/1
N2 - 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.
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.
UR - http://www.scopus.com/inward/record.url?scp=0025757727&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0025757727&partnerID=8YFLogxK
U2 - 10.1016/0263-8223(91)90005-J
DO - 10.1016/0263-8223(91)90005-J
M3 - Article
VL - 18
SP - 379
EP - 397
JO - Composite Structures
JF - Composite Structures
SN - 0263-8223
IS - 4
ER -