The CAD file for the M6 wing is from NASA's Open Vehicle Sketchpad (OpenVSP). The analysis was performed in Stallion 3D version 4.0 using the following steps:
1. Import the STL file in Stallion 3D
2. Set the flow field conditions for the wing experiment
3. Setup the CFD. Select the RANS solver.
4. Automatic grid generation
5. Run the flow solver.
6. Perform aerodynamics analysis using Stallion 3D built-in tools.