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Aircraft wing design optimization
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0
Statistics
3Â Geometries
1Â Mesh
0Â Simulation setups
0Â Results
3Â Geometries 1Â Mesh 0Â Simulation setups 0Â 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.
