How to Analyze the ONERA M6 Wing
This video shows how Stallion 3D is used to analyze a transonic wing: Watch Video
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.
About
Dr. Patrick Hanley is the owner of Hanley Innovations. He received his Ph.D. degree in fluid dynamics for Massachusetts Institute of Technology (MIT) department of Aeronautics and Astronautics (Course XVI). Read more ..
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