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Forum: OpenFOAM Running, Solving & CFD

May 28, 2008, 04:25

Replies: 3

Is it possible to obtain wallY%23601 for an airfoil

Views: 1,433

Posted By madad2005

Hi Dino, Did you manage to

Hi Dino,

Did you manage to get this working? Sorry for taking so long to reply. I looked at your output and a couple of things caught my eye. Firstly, why is your AMG residuals appearing three...

Forum: OpenFOAM Running, Solving & CFD

May 26, 2008, 12:56

Replies: 3

Is it possible to obtain wallY%23601 for an airfoil

Views: 1,433

Posted By madad2005

Yes, it should be possible. Wh

Yes, it should be possible. What are you using for mesh generation? To assure you've resolved the boundary layer, you want your first cell distance to be between 10^-5 - 10^-6 of the aerofoil chord...

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