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Wing Optimization Exercise - Student Version
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2 Geometries
3 Meshes
5 Simulation setups
4 Results
2 Geometries 3 Meshes 5 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
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Project History
AnnaFless createdthis project
about 8 years ago
walidabdelraouf copied this project
over 6 years ago