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front flap design 6 degrees
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2Â Geometries
2Â Meshes
2Â Simulation setups
2Â Results
2Â Geometries 2Â Meshes 2Â Simulation setups 2Â ResultsAbout this project
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 down force) considering a constant inlet velocity of 20 m/s.
