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FSAE 2017-Workshop-S1-FrontWing Analysis HM
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2 Geometries
2 Meshes
2 Simulation setups
2 Results
2 Geometries 2 Meshes 2 Simulation setups 2 ResultsAbout this project
Behavior of drag and lift and determination of the stall zone for two different front wing flap angles: 6 degrees (standard) and 18 degrees (high downforce) considering a constant inlet velocity of 20 m/s.
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svnnryd created this project