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CFD Final Wings - New
476
1
Statistics
11Â Geometries
11Â Meshes
5Â Simulation setups
7Â Results
11Â Geometries 11Â Meshes 5Â Simulation setups 7Â 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
