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1 Geometry
1 Mesh
1 Simulation setup
0 ResultsCFD analysis of a NACA 2412 airfoil to evaluate aerodynamic performance at different angles of attack and determine the stall angle.
by slilbaekslilbaek
shivani_s_s created this project
about 1 month ago
1 Geometry 1 Mesh 1 Simulation setup 0 ResultsCFD analysis of a NACA 2412 airfoil to evaluate aerodynamic performance at different angles of attack and determine the stall angle.
