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CFD Final Wings - selig
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Statistics
8Â Geometries
7Â Meshes
5Â Simulation setups
5Â Results
8Â Geometries 7Â Meshes 5Â Simulation setups 5Â ResultsAbout this project
Simulate drag and efficiency of prototype wing. Incompressible subsonic flow at 8m/s 'x' axis. - fuselage. Updated to fit the launcher spec. - Copy - Copy - Copy
