Abstract
Material properties that can be done to show a smooth and constant change
starting with one surface then onto the next, along these lines taking out interface issues
and alleviating concentrations of thermal stress. In the present work, a polymeric
composite with functionally graded mode and their deflection behavior were studied using
analysis through Finite element analysis via ANSYS 16.1 and visual basics 6.0 language
depending on Mori Tanka formula and classical laminated theory in order to decide the
stiffer material under flexural load. The proposed tests were essentially using the square
plates under static uniform stress. The two kinds of composites were involved in a paired
of materials with constant volume fraction. The outcomes revealed that stiffness of FGM
less than laminate composite.
Key words: FGM, Laminate, ANSYS, Visual basic, Flexural.