FINITE ELEMENT METHOD ANALYSIS OF THICKNESS OF PLATES

The advance in the improvement of using structural components for the aerospace structure is essential and their importance in the fields of engineering especially in the construction of bridges, floor panels and in the field of the aeronautical domain in the design of the wings and sheet panels. The main objective here is to find the optimum design thickness of the plates. Initially, the optimized selection of the material is chosen and then thickness analysis is carried using the numerical analysis. The results obtained are validated with optimized Computational results. Finally coming out with the improvised live load carrying capacity of the material.