WING STRUCTURAL ANALYSIS USING DIFFERENT FIBER REINFORCED COMPOSITES AND HYBRID COMPOSITES

Modeling the wing in ANSYS Mechanical APDL using working model parameters and applying the loads accordingly. The iIdealization of the wing and all its structural components to a single wing element. Obtaining the results and comparing them. In this project, we are considering different composite materials and their properties. The wing model is generated and meshed to produce required elements and nodes. The Loads are applied accordingly with reference to the working model. When the solution is done, the stress intensity and Von Mmises stress of the model for a concern composite is obtained and the same is done for different composites. After obtaining the results, we compare the properties. In this project, we are comparing only stress of the component. KEYWORDS: Stress Analysis, Wing Analysis & Ansys