Modifying the "Transonic Flow over an Airfoil" tutorial for supersonic flow?
I am taking a CFD course in school and we used this tutorial to learn how to setup STAR CCM for analyzing an airfoil in 2D for transonic speeds. I was wondering how I would setup STAR CCM for supersonic flow now. I tried changing the initial velocity and mach number to those appropriate for a mach number of 2. But when I run the solution it gives me a diverging error in the AMG solver.
Any tips or advice would be appreciated. Thanks.
Can you please send me a tutorial on airfoil simulation on Star CCM+. Now I am working on 3D airfoil simulation.
My mail address: firstname.lastname@example.org
Thank you in advance.
I am looking to produce a similar model. Did you have any luck previously with this?
Thanks in advance,
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