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Forum: FLUENT

July 21, 2022, 18:19

Replies: 2

Airfoil Convergence Problem at High Angle of Attack

Views: 516

Posted By ArashDi

To some extent done

Hi, Thank you, Indra
It was a meshing problem and I tried to refine the mesh and finally, It was Solved, It was a steady state modeling, Therefore, I was unable to use a pseudo time step, I did it...

Forum: FLUENT

July 20, 2022, 09:26

Replies: 2

Airfoil Convergence Problem at High Angle of Attack

Views: 516

Posted By ArashDi

Airfoil Convergence Problem at High Angle of Attack

Hi
I'm simulating an airfoil in range of 0-18 (deg) angle of attack, And I have convergence problem at 16...18 degree.
flow is incompressible,
Geometry is fixed and flow has direction,
K-Omega...

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