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NACA Wing
12
0
Statistics
2 Geometries
2 Meshes
1 Simulation setup
1 Result
2 Geometries 2 Meshes 1 Simulation setup 1 ResultAbout this project
Implementation of a test case for analyzing a 3D wing profile designed in Onshape using SimScale, based on NACA airfoil geometry for low Reynolds number analysis.
