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Attempt 2 at FSAE Rear Wing - Copy
2
1Statistics
2 Geometries
1 Mesh
1 Simulation setup
1 Result
2 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
This model has a cut on the trailing edge of all wing elements. The aim of this study was to produce reasonable values for the forces and coefficients while learning how to adequately use the softwrae. - Copy
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craigcahill2 created this project
4CEZ2122 copied this project