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2 Geometries
2 Meshes
2 Simulation setups
4 ResultsThis is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15. - Copy
by simscalesimscale
2 Geometries 2 Meshes 2 Simulation setups 4 ResultsThis is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15. - Copy
UllWarg created this project
over 7 years ago
hmtksy383838 copied this project
5 months ago
