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Wing Optimization Exercise - Student Version
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3 Geometries
1 Mesh
1 Simulation setup
1 Result
3 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
Weight is one of the most critical parameters in aircraft design. In this exercise, you will be provided with a baseline design of an aluminum aircraft wing. Your objective is to reduce the weight of the wing without exceeding the yield stress and maximum allowable deflection
