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Wing Optimization Exercise - Student Version
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Statistics
4Â Geometries
3Â Meshes
3Â Simulation setups
3Â Results
4Â Geometries 3Â Meshes 3Â Simulation setups 3Â ResultsAbout 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
