These are the steps to follow to solve the Onera M6 wing in Stallion 3D.
1. Import the wing geometry
2. Set the flow conditions
3. Setup the CFD solution (we use the RANS solver for this case)
4. Generate the grid and solve the flow
In this video, we show how to obtain the cp plots at various wing span stations. More information about Stallion 3D can be found at: [ Ссылка ]
Thanks for watching.
