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Aerofoil - Error Divergence Detected

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Old   October 21, 2015, 15:15
Default Aerofoil - Error Divergence Detected
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Hello there,

I am completing a college assignment on a NACA0012 aerofoil with the following details: Angle of Attack - 2degrees, Velocity Onset -2m/s and Chord length - 1m.

The assignment requires 200 iterations

I got the following Error: Divergence detected in AMG solver: pressure correction

I tried changing to flexible cycle under Multigrid settings. Same error.

I tried reducing the number of iterations.

New Error: Divergence detected in AMG solver: x-momentum

Please help me!!
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ansys, divergence amg solver, error, pressure correction, x-momentum

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