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256
0
1 Geometry
0 Meshes
0 Simulation setups
0 ResultsFEA analysis on an internal wing structure using a NACA 0015 airfoil.
by slilbaekslilbaek
hsturrock1 created this project
over 9 years ago
1 Geometry 0 Meshes 0 Simulation setups 0 ResultsFEA analysis on an internal wing structure using a NACA 0015 airfoil.
