Thermal Buckling of Rectangular Laminated Plates with a Hole
| Autor: | Ahmet Avcı, Behcet Dağhan, Sami Kaya |
|---|---|
| Rok vydání: | 2005 |
| Předmět: |
Materials science
Polymers and Plastics Computer simulation Antisymmetric relation Mechanical Engineering Isotropy Glass fiber 02 engineering and technology 021001 nanoscience & nanotechnology Finite element method 020303 mechanical engineering & transports 0203 mechanical engineering Buckling Mechanics of Materials Materials Chemistry Ceramics and Composites Boundary value problem Composite material 0210 nano-technology Boron fiber |
| Zdroj: | Journal of Reinforced Plastics and Composites. 24:259-272 |
| ISSN: | 1530-7964 0731-6844 |
| DOI: | 10.1177/1731684405043554 |
| Popis: | Thermal buckling analysis of symmetric and antisymmetric laminated composite plates with clamped and simply supported edges, and containing a hole is presented in this paper. The first-order shear deformation theory in conjunction with the variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used to find thermal buckling temperatures of isotropic, glass-epoxy and boron-epoxy laminates. The effects of hole size, angle of ply orientation, lay-up sequences, and boundary conditions on thermal buckling temperatures are investigated. The result is shown in graphical forms for various boundary conditions. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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