Structural and Fatigue Analysis of Naca4412 Wing Using Ansys work bench

Analysis of Structure and its mechanical properties gives us the strength as well as Capability of the material. Structural Analysis over a Body gives us about various properties like its load baring capacity as well asDeformation to the load. Wings plays a crucial role in an aircraft, so it is important to analyze parameter such as Weight, load and deformation to load in order to increase its efficiency and for high performance. Wing is made of AluminumMaterial.in this paper certain analysis was carried out over the NACA 4412 airfoil wing structure and gone through structural analysis of the wing using ANSYS. Static structural analysis was done, and results of various stresses are obtained.