Finite element analysis of wing design

Abstract

The present analysis is based upon evaluation and optimization of the structural behavior of wings used in airplanes, as given by advanced material and transport aircraft structure. The main goal is to reduce mass and volume cum the stress and deformation in the plane geometry. The main focus of the analysis is on the factor of safety or level of safety, which is optimized to remain constant for both standard and new model. The analysis of the wing is kept organized only as far as structural and stress analysis is concerned. The aerodynamics analysis can be done for this geometry.