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Forum: OpenFOAM Running, Solving & CFD

November 15, 2019, 10:53

Replies: 0

2D Airfoil do not converge - pressure residuals do not go below 1e-4

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Posted By rinaldialberto

2D Airfoil do not converge - pressure residuals do not go below 1e-4

Hi there,

I am running a 2D simulation on a MH32 airfoil.
I generated an O-Grid mesh using construct2D and then converted using plot3DToFoam. The mesh diameter is 30x the chord length, y+<1 and...

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