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Aircraft wing design optimization
1131
10
Statistics
3Â Geometries
3Â Meshes
6Â Simulation setups
6Â Results
3Â Geometries 3Â Meshes 6Â 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.
