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Aircraft wing design optimization
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3 Geometries
1 Mesh
0 Simulation setups
0 Results
3 Geometries 1 Mesh 0 Simulation setups 0 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.
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Project History
ahmedhussain18 created this project
asoni copied this project