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Aircraft wing design optimization - Copy - Copy
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7
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3 Geometries
3 Meshes
6 Simulation setups
6 Results
3 Geometries 3 Meshes 6 Simulation setups 6 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 - Copy
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Project History
ajunifia created this project
ajunifia copied this project