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Front wing Design
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240
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2 Geometries
2 Meshes
2 Simulation setups
2 Results
2 Geometries 2 Meshes 2 Simulation setups 2 ResultsAbout this project
To investigate the behavior of drag and lift and determine 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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Project History
Sunish created this project