Using FEM for the Modeling and Structural Analysis of Aircraft Wings made of Various Materials

Abstract

Aircraft Skin, ribs, and spar sections make up the wing structure. While on the ground, the spar supports the weight of the wings and flying loads. The spars are joined to other forming and structural components, including ribs, which have stressed skin. The most crucial component of the airplane that produces lift is the wings. The type of aircraft and its intended use might influence the wing design. Wing structure examination by experimentation is a more costly and time-consuming procedure. CATIA V5 R20 was used in this project to create a thorough design of the airplane wing structure. The stresses at the wing structure are then calculated using structural analysis of the wing structure.