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Attempt 2 at FSAE Rear Wing - Copy
42
0Statistics
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
adelmogmachado copied this project