Abstract
The buckling behavior of generally layered composite plates subjected to a uniform temperature field is studied. Transverse shear flexibility is accounted for in the analysis using the thermoelastic version of the first order shear deformation theory. Numerical results are presented for thermal buckling problems using a nine noded isoparametric quadrilateral finite element. The influence of boundary conditions, ply orientation, and plate geometries on the critical buckling temperature is examined.
| Original language | American English |
|---|---|
| Pages (from-to) | 29-33 |
| Number of pages | 5 |
| Journal | American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP |
| Volume | 203 |
| State | Published - Jan 1 1990 |
| Event | Winter Annual Meeting of the American Society of Mechanical Engineers - Dallas, TX, USA Duration: Nov 25 1990 → Nov 30 1990 |
ASJC Scopus Subject Areas
- Mechanical Engineering
Keywords
- Mathematical Techniques-Finite Element Method
- Thermal Effects
Disciplines
- Aerospace Engineering
- Mechanical Engineering
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