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MaxCo for airfoil simulation

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Old   November 26, 2019, 07:00
Default MaxCo for airfoil simulation
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Goodmorning to everyone,

I am doing a simulation of an airfoil in 2D with a Re = 30000 and I have some problems regarding the maxCo because Initially I have set this value around 20 but when I have reduced this value to 10 I have noticed that the solution is very different. I am using a pimpleFoam solver.

Is there a general rule to impose the maxCo value?
thanks
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Old   November 28, 2019, 16:46
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rans, des or les?
please consider to read the forum's guidelines for questions, so that the community can try to help you.
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Old   November 29, 2019, 00:09
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I assume you are talking about the Courant number. Yes, you might need a Courant number of < 1. This way a the fluid does not travel further than your cells within one time step. That is explained in most text books. This is also called the CFL (Courant-Friedrichs-Lewy) condition.
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