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VDI Wing Optimization Exercise - Student Version TE
104
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Statistics
4 Geometries
4 Meshes
4 Simulation setups
4 Results
4 Geometries 4 Meshes 4 Simulation setups 4 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
