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0 ResultsCFD simulation of a NACA 4412 airfoil at 13,89 angle of attack, RE 1.52 Mio and Ma 0.09.
mgeiermann created this project
almost 5 years ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsCFD simulation of a NACA 4412 airfoil at 13,89 angle of attack, RE 1.52 Mio and Ma 0.09.
by simscalesimscale
