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Wing Optimization Exercise - Student Version
253
1
Statistics
4Â Geometries
6Â Meshes
5Â Simulation setups
5Â Results
4Â Geometries 6Â Meshes 5Â Simulation setups 5Â 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
