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Airplane Wing Design Optimization with Stress Analysis
2002
134
Statistics
3Â Geometries
0Â Meshes
0Â Simulation setups
0Â Results
3Â Geometries 0Â Meshes 0Â Simulation setups 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.
