| Popis: |
In the present work, the stress behavior of laminated composite plate under compressive loading using a four-node element with six degrees of freedom at each node and translations in the x and y directions is done. In the present study, the modeling is done in Abaqus. Investigations were carried on plates starting with three layers of the top location of 0° angle-ply laminated composite plates at clamped boundary condition. Similarly, with three layers of top location, 0°, 30° and −45° angle ply are laminated. By changing the location of ply orientations the bending stress may be improved. The effect of changing the ply orientation is to increase or decrease the stresses. The composite plate has been analyzed for various orientations and their effects on stresses so as to find the optimized conditions. |
