Analysis of Simply Supported Laminated Plate Using CLT and FSDT

Abstract

Composite is the special kind of engineered materials. The mechanics of the composite are a little bit complicated. In the present work, the classical laminate theory (CLT) and first-order shear deformation theory (FSDT) is used for the finding the deformation/deflection in the simply supported composite plate loaded with the uniformly distributed load. The Navier solution applied to find the desired result.