Reynolds Stress Tensor
Hello Foamers
I am quite new to CFD and OpenFoam, and I was wondering if someone can help me with this: How can be calculated / displayed the Reynolds Stress Tensor, in order to, say, calculate the stresses at a given point of the domain. Please also note that I am using a LES turbulence model Thanks in advance for your help |
In the controlDict, the last part you can choose to add functions:
Code:
functions This function will give a symmetric tensor field with 6 components for the times you choose. |
Hi David, thanks for your answer. I will try it.
On the other hand, checking commands, I found stressComponents and typed it. The thing, is that it created at each time step a sigmaxx, sigma xy.... sigmazz files. However when I opened any of those files the units I found are [0 2 -2 0 0 0 0], while I was expecting [1 -1 -2 0 0 0 0]. Do you, or any other foamer have something to say about this? Thanks |
In its source code, stressComponents is defined as:
laminarTransport.nu()*2*dev(symm(fvc::grad(U))) so I guess its the deviatoric stress tensor divided by the density, hence the units [0 2 -2 ...] These stress components are different than the Reynolds stresses: Re Stresses: velocity fluctuation. Dev. Stresses: deformation. |
Gracias David
The tech support folks from OpenFoam, have said the following about this issue stressComponents was written for incompressible laminar flow. For LES you need to accumulate the Reynolds stress by averaging during the run.It looks as if it is time for this newbie to dig into the programming aspects of OpenFoam (auch!!!) |
It finally makes some sense:
Tau= mu*dV/dy stressComponents uses nu [m2 s-1] instead of mu [kg m-1 s-1], and that is the reason why the stress tensor yields [m2 s-2] However I still need to know how to calculate the stress tensor components |
If you need to calculate the Re stress tensor use the info in my first post, at the end of control dict add the fieldaveraging function, UPrime2mean gives the Re stress tensor.
I'm also a newbie at foam and programing, but I have digged several times into the source codes. Have fun :) |
Hi David,
I saw you post about the Reynolds stress tensor. I also found that UPrime2mean yielded six columns which should be stress tensor. I was just wondering how I can get the RMS value from the UPrime2mean file. Hope you can give me some hints. Thank you very much. Kind regards, Tony |
Hey David,
This is quite an old post but maybe I'm lucky and get a reply. I want to plot the Reynolds stress versus the normal wall direction at a specific point. To do so, I used the post process utilities of OpenFOAM (simpleFoam -postProcess -func R -latestTime) but I cannot sample this tensor along a line. (see my post here https://www.cfd-online.com/Forums/op...rmal-wall.html) I thought I can use your option which is to write the UPrime2Mean using your proposed function above. However, comparing the Reynold stress that I got from the post process utility and UPrime2Mean, there is quite a difference. Any idea why? Cheers, Dimitri |
Hi All
I wish you guys could help me with my problem. I use following code in controlDict to calculate reynolds stress tensors. But these values are not shown in paraFoam, though they are calculated and reported in relevant file. Can anybody help me?? Code:
functions |
Quote:
Thanks for ur excellent post about UPrime2Mean and Reynolds Stress, In your previous post, I noticed you said UPrime2Mean (including 6 components: xx xy xz yy zz yz) is exactly the Reynolds Stress. Are u sure about that? Do you have reference about this? I, sorry because I know it's really an old thread. Best regards, Gang Wang |
Quote:
Hopefully my (no longer very recent) thread will answer your question. In a LES simulation for example, 'Uprime2Mean' provides the Reynolds Stress Tensor of the resolved flow, while 'R' provides the sub-grid (modelled) tensor. |
Quote:
I suppose you are right. So in LES, if we would like to compute the percentage of the resolved part of reynolds stress, it should be tr(UPrime2Mean) / (tr(UPrime2Mean)+tr(R) ). Am I right about this? Best, Gang |
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