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VDI Wing Optimization Exercise - Anna Testing

VDI Wing Optimization Exercise - Anna Testing image
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geometries 3 Geometries
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simulations 3 Simulation setups
runs 6 Results

About 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