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Rear Wing NACA 8412 Main Modified NACA 8416 Flap
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1 Geometry
1 Mesh
1 Simulation setup
2 Results
1 Geometry 1 Mesh 1 Simulation setup 2 ResultsAbout this project
First iteration of rear wing design with NACA 8412 main element and modified NACA 8416 flap (for better pressure recovery at high angle of attack)
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Project History
Appable created this project