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Pressure instabilities when running RANS on mixed grid type ( Case from DPW7) #2576
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fomistul-cfd
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Have you tried using Green-Gauss gradient instead of weighted least squares? |
8 replies
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Also happens with INC_NAVIER_STOKES, with rho,T,mu = constant |
2 replies
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3 replies
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Hi @fomistul-cfd , I think this is due to inaccurate flux computations on skewed meshes. Can you share the exact dpw7 grid (.su2 or cgns) and SU2 config file that you used that will reproduce the problem? I will try to see if there are existing solutions for this problem. |
6 replies
3 replies
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Hi,
My apologies, just now I've noticed that the mesh was already attached,
sorry.
Regards,
Yair
…On Sun, Oct 19, 2025 at 10:05 PM Nijso ***@***.***> wrote:
Here is the mesh, just replace the filename in your config file. It has
markers in,out,wall,sym.
https://drive.google.com/file/d/1t_ElCgt8mW_dCu3oCwFLzNnUWteZMsES/view?usp=sharing
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Hi, I've noticed that the PR addressing the alpha-damping scheme (by Nishikawa) is missing. Does this mean that this PR has been merged into the developed code? |
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Thanks, but I don’t find it in the PR list
בתאריך יום ג׳, 22 בספט׳ 2026 ב-16:36 מאת fomistul-cfd <
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… Hi @YairMO <https://github.com/YairMO> , no merge that address this
problem was done as far as I know.
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What does it means “CLOSED”
בתאריך יום ג׳, 22 בספט׳ 2026 ב-16:51 מאת fomistul-cfd <
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… here is the pull request that tried to address this problem #2584
<#2584>
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Thank you for clarifying this for me. No need to reopen.
…On Wed, Sep 23, 2026 at 2:00 AM Nijso ***@***.***> wrote:
closed means I closed it without merging into develop. The original author
@tbellosta <https://github.com/tbellosta> of the branch that I took this
from is still working on this and want to merge that into develop. I can
keep it open for now if it makes it is convenient?
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Hi all, I encounter a problem when running a case for grid convergence from dpw7

The case is :
When inspecting the solution on the surface section the contour plot is showing instabilities that are not influenced by convective scheme , MUSCL reconstruction or limiter.

This was run on a grid generated by me, so to see if it's a grid problem I run also a simulation with comitee grid from dpw7 workshop ( DLR grid with mixed elements)
https://dpw.larc.nasa.gov/DPW7/DLR_Grids.REV00/
When converged the plot showed the same instabilities but on the wing tip where I observed they are appearing on a specific grid topology.


The pressure instabilities:
The grid topology:
We can see that the instabilities appear when a topology of this type is appearing in the grid:
Here is a config file example.
config.txt
I also tried to inspect residuals and orthogonality of the mesh to see if it's a warping/quality problem but the output for quality show zero for all volume cells( it can be me doing something wrong, if someone could help me with that will be great). In term of residuals they were low -8 in logarithmic scale.
Is there something I can do to get rid of these instabilities or is it a bug/ numerical error related problem?
Thank you.
L. E. : In term of force coefficients the results are really good.
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