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Aircraft wing design optimization
384
0
Statistics
3Â Geometries
3Â Meshes
1Â Simulation setup
0Â Results
3Â Geometries 3Â Meshes 1Â Simulation setup 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.
