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February 22, 2011, 08:03
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Plot of the turbulent viscosity
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New Member
Girolamo
Join Date: Oct 2010
Location: Napoli
Posts: 14
Rep Power: 16  |
Hi,
i would like to plot with parafoam the turbolent viscosity on my Omera M6 wing. I made a case with the Spalart-Allmaras turbolent model and i can obtain the plot of the nut easily. now i'm trying to use the k-omega model, but in parafoam i have nut=0 so i don't have any plot. which parameter should I choose to view the turbolent viscosity on my wing??? thanks very much p.s. i have also u=0 in the paraview menu!!! |
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February 26, 2011, 06:17
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#2 |
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Senior Member
Claus Meister
Join Date: Aug 2009
Location: Wiesbaden, Germany
Posts: 241
Rep Power: 18 |
On the Wing (Wall) itself are these values zero: nut - because of the boundary layer and U by definition.
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February 26, 2011, 16:00
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#3 |
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New Member
Girolamo
Join Date: Oct 2010
Location: Napoli
Posts: 14
Rep Power: 16 |
ok, thanks
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