Structural Analysis on Composite Laminate with Different Orientation

The aim of the project is to analyze the structural analysis on a composite plate with different orientation, with the same material properties. A composite material consists of two or several material. A composite laminate of cantilever beam was designed and fabricated using graphite epoxy for structural mechanics behavior. Two design cases {[0/90/0/90], [0/45/0/45]} of different orientations of composite laminate were considered for the better combinations, by using FEM program of ANSYS 16.0. The bending test on a composite laminate of cantilever beam was performed by applying load conditions