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Search: Posts Made By: mevoili
Forum: OpenFOAM Running, Solving & CFD July 10, 2012, 18:08
Replies: 20
Views: 13,660
Posted By mevoili
Because I've created my mesh such that it is wall...

Because I've created my mesh such that it is wall resolved (y+ ~ 1 ), in order to see all the detail of the boundary layer. Indeed, I want to study boundary layers, so using wall functions would be a...
Forum: OpenFOAM Running, Solving & CFD March 15, 2012, 09:00
Replies: 20
Views: 13,660
Posted By mevoili
I'll run a case on a finer mesh to compare...

I'll run a case on a finer mesh to compare results, but i used rather conventional values to generate my mesh so it should be ok...
Forum: OpenFOAM Running, Solving & CFD March 15, 2012, 08:19
Replies: 20
Views: 13,660
Posted By mevoili
Hi, I'm using openFOAM 2.0.1. What do you...

Hi,

I'm using openFOAM 2.0.1. What do you mean by "checking for grid independence", my omega BC at the wall depends on the first cell so I'm not sure to understand what you mean? My mesh is such...
Forum: OpenFOAM Running, Solving & CFD March 15, 2012, 05:45
Replies: 20
Views: 13,660
Posted By mevoili
Hella again, I followed your advices, and my...

Hella again,

I followed your advices, and my results are better than before, but I still don't get the right logarithmic slope in the log layer..

Do you have any ideas what could cause this ?
Forum: OpenFOAM Running, Solving & CFD March 13, 2012, 13:01
Replies: 20
Views: 13,660
Posted By mevoili
Thanks for your advices, Felix, I will try to do...

Thanks for your advices, Felix, I will try to do so as soon as I can, and I will comment my results here.
Forum: OpenFOAM Running, Solving & CFD March 13, 2012, 12:33
Replies: 20
Views: 13,660
Posted By mevoili
And here are my fvSolution & fvSchemes, but I...

And here are my fvSolution & fvSchemes, but I don't think the problem comes from there...
fvSolution
/*--------------------------------*- C++ -*----------------------------------*\
| ========= ...
Forum: OpenFOAM Running, Solving & CFD March 13, 2012, 12:27
Replies: 20
Views: 13,660
Posted By mevoili
Here are my boundary and initial conditions : ...

Here are my boundary and initial conditions :

inlet :
k = 1e-4;
omega = 1;
nut : calculated;
U = (1 0 0);
p : zeroGradient;

outlet :
Forum: OpenFOAM Running, Solving & CFD March 13, 2012, 07:51
Replies: 20
Views: 13,660
Posted By mevoili
k-omega SST for wall-resolved TBL, problem with log layer.

Hello Foamers,

I'm trying to compute a turbulent flow on a 2-D airfoil usin RANS. I've created my mesh such that the flow is wall resolved (y+ ~ 1 ). I would like to compare different models: the...
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