Design and Simulation of Flexural Stresses of PM Composite Beam

In the present work the stress behavior of laminated composite plates 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. The composite beam is designed analytically and the modeling is done in ABAQUS. In this study simulation is carried on plate starting with three layers of top location of 00angle ply laminated composite plates at clamped boundary condition. The ABAQUS results showed, on the stresses, have also been validated with comparison of numerical results.