Analysis of Simply Supported Laminated Plate Using CLT and FSDT
Pages : 418-427, DOI: https://doi.org/10.14741/ijmcr/v.10.5.3Download PDF
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.
Keywords: Composite, Lamina, Laminate, Stacking Sequence