Plot of the turbulent viscosity
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!!!
On the Wing (Wall) itself are these values zero: nut - because of the boundary layer and U by definition.
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