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Airplane Wing Design Optimization – Stress Analysis
209 1
Statistics
3 Geometries 3 Meshes 5 Simulation setups 5 Results
About 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
jourada copied this project