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aircraft wing analysis


Our aim of this project is analysis the aircraft wing with our desired specifications. In this project first we design the aircraft wing by using deigning software is CATIA with specific limitations. After designing the aircraft wing we analyze the wing by using finite element method. This finite element method basically had three steps. These three steps are Preprocessor, Analysis and Postprocessor. Preprocessor is used to split the wing by elements and nodes. Then we are applying our desired loads to that aircraft wing. Postprocessor is used to give our analyzing results like tension load, compression and stress. These three steps of finite element method is done by two software’s like Hypermesh and NASTRAN.

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