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Inverted Naca 4412
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1 Geometry
1 Mesh
1 Simulation setup
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1 Geometry 1 Mesh 1 Simulation setup 0 ResultsAbout this project
This setup is for: NACA 4412 rear wing smooth + tubercled comparison AoA = 8°–18° yaw angle β = 6° V∞ = 50 m/s SST k–ω turbulence model
