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173
0
2 Geometries
1 Mesh
1 Simulation setup
1 Resultcfd simulation of a NACA 0012 airfoil with span 0.1m and chord 0.1m
by slilbaekslilbaek
SayanS created this project
over 4 years ago
2 Geometries 1 Mesh 1 Simulation setup 1 Resultcfd simulation of a NACA 0012 airfoil with span 0.1m and chord 0.1m
