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449
6
2 Geometries
2 Meshes
2 Simulation setups
3 ResultsThis is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15.
by slilbaekslilbaek
UllWarg created this project
over 7 years ago
2 Geometries 2 Meshes 2 Simulation setups 3 ResultsThis is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15.
