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airfoil lift and drag simulation
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Statistics
1 Geometry
1 Mesh
1 Simulation setup
0 Results
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsAbout this project
i need a naca 2412 airfoil with a chord length 1m and 7 dimple and width id 20mm depth 5mmdistance between the dimple 60 mm give me lift coefficient drag coefficient cl/cd ratio pressure contuor velocity contour
