Abstract
Thermal buckling of laminated composite plates subjected to a temperature change is studied. The displacement equations of equilibrium are used and Galerkin's method is employed to determine the critical buckling temperature. Clamped and simply supported boundary conditions are both considered. The effects of various parameters on the thermal buckling are examined.
Original language | English |
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Pages (from-to) | 345-356 |
Number of pages | 12 |
Journal | Journal of Thermal Stresses |
Volume | 10 |
Issue number | 4 |
DOIs | |
Publication status | Published - 1987 Jan 1 |
All Science Journal Classification (ASJC) codes
- General Materials Science
- Condensed Matter Physics