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Front Wing Design Study
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2 Geometries
2 Meshes
1 Simulation setup
1 Result
2 Geometries 2 Meshes 1 Simulation setup 1 ResultAbout this project
It is an investigation of the behavior of drag and lift and determination of the stall zone for two different front wing flap angles: 6 degrees and 18 degrees considering a constant inlet velocity of 20 m/s.
