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Aircraft wing design optimization - Copy
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Statistics
4Â Geometries
4Â Meshes
9Â Simulation setups
6Â Results
4Â Geometries 4Â Meshes 9Â Simulation setups 6Â 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. - Copy
