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VDI Wing Optimization Exercise - Student Version
118
1
Statistics
3 Geometries
4 Meshes
2 Simulation setups
2 Results
3 Geometries 4 Meshes 2 Simulation setups 2 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
