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356
2
0 Geometries
1 Mesh
2 Simulation setups
2 Resultssubsonic flow over a NACA 5012 airfoil at Reynolds number of 100 and 1000.
by simscalesimscale
mspink created this project
almost 6 years ago
0 Geometries 1 Mesh 2 Simulation setups 2 Resultssubsonic flow over a NACA 5012 airfoil at Reynolds number of 100 and 1000.
