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VDI Wing Optimization Exercise - Anna Testing
476
2
Statistics
3 Geometries
3 Meshes
3 Simulation setups
6 Results
3 Geometries 3 Meshes 3 Simulation setups 6 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
