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Aircraft wing design optimization
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Statistics
3Â Geometries
3Â Meshes
2Â Simulation setups
2Â Results
3Â Geometries 3Â Meshes 2Â Simulation setups 2Â ResultsAbout this project
This project involves the simulation of stress analysis of an aircraft wing. There are total 6 comparison configurations with 3 different models and two different load definition.
