This document discusses the structural design analysis of a bypass casing for an aero engine. The goal is to reduce weight while meeting strength and buckling requirements. Five configurations are analyzed: the baseline ortho-grid design and modified designs using different ortho-grid and iso-grid patterns. Finite element analysis is used to evaluate stresses and buckling factors. The results show that Configuration 5, an iso-grid design, meets strength and buckling requirements while achieving a 15% weight reduction compared to the baseline. Therefore, the iso-grid configuration is selected as the final design.