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Airplane Wing Design Optimization – Stress Analysis
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3 Geometries
3 Meshes
5 Simulation setups
5 Results
3 Geometries 3 Meshes 5 Simulation setups 5 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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by kpettykpetty
Project History
ahmedhussain18 created this project
jourada copied this project