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317
2
1 Geometry
1 Mesh
0 Simulation setups
0 ResultsTo understand the airflow around a NACA 0012 airfoil and derive the lift and drag coefficients
by slilbaekslilbaek
akintheboy created this project
over 7 years ago
1 Geometry 1 Mesh 0 Simulation setups 0 ResultsTo understand the airflow around a NACA 0012 airfoil and derive the lift and drag coefficients
