|
[Sponsors] |
July 27, 2014, 19:47 |
Verifying LES assumption in OpenFOAM
|
#1 |
New Member
David H.
Join Date: Oct 2013
Posts: 25
Rep Power: 13 |
Hi all, I'm wondering - is there an "easy" way in OpenFOAM / ParaView to validate your LES model?
That is, the assumption that 80% of your field is resolved, and 20% of the turbulence is being modeled. I'm trying to construct the total residual stress tensor from the resolved, and SGS components. But I don't think I have enough inputs to calculate the SGS contribution to the residual stress tensor. While working with the data, and going through different derivations and investigating models - I came across an idea. Since nuSgs is provided, and this is calculated by the turbulence model, is it reasonable to say the average nuEff = nuSgs + nu should provide this desired ratio? That is, nuSgs / nuEff ~= 20%? In my cases, this is not true. However it was more around 75% but I can't imagine with the cell refinement that this is true. Perhaps I'm making a poor assumption, however my idea is based on this, from the Smagorinsky documentation; Code:
B = 2/3*k*I - 2*nuSgs*dev(D) Beff = 2/3*k*I - 2*nuEff*dev(D) where D = symm(grad(U)); k = (2*ck/ce)*delta^2*||D||^2 nuSgs = ck*sqrt(k)*delta nuEff = nuSgs + nu |
|
July 28, 2014, 05:28 |
|
#2 |
Member
|
You should actually compare directly resolved turbulent kinetic energy with subgrid modelled kinetic energy.
You can compute the latter from the subgrid Reynolds stress tensor available from turbulenceModel class through the method B and the former time averaging instantaneous velocity field activating the functionObject fieldAverage with option prime2Mean on. Hope this helped, Cosimo
__________________
Cosimo Bianchini Ergon Research s.r.l. Via Panciatichi, 92 50127 Florence - ITALY Tel: +39 055 0763716 Mob: +39 320 9460153 e-mail: cosimo.bianchini@ergonresearch.it URL: www.ergonresearch.it |
|
July 28, 2014, 07:39 |
|
#3 |
New Member
David H.
Join Date: Oct 2013
Posts: 25
Rep Power: 13 |
After posting this, I did some more work on this subject, and it appears that UPrime2Mean calculates the resolved portion of this.
This is also supported by my results. I modified the solver to output UU as sqr(U), and also use the functionObject to time-average this at runtime (UUMean). From this, I have the time averaged <U><U> field, as well as the time averaged <U> and <U'><U'> (via UPrime2Mean). Plotting (time averaged) <filtered>: (<U><U>) - (<U>)*(<U>) This construction appears close to UPrime2Mean, but I believe it is just a matter of statistical convergence, since this should be equivalent to UPrime2Mean as t->(sufficiently long) Last edited by djh2; August 1, 2014 at 09:55. Reason: corrections |
|
May 25, 2020, 11:19 |
|
#4 |
Member
Sereff
Join Date: Jan 2019
Posts: 49
Rep Power: 7 |
Hi Cosimo,
Sorry I restart the thread. I have a simliar issue where I ran the channel flow tutorial case and found that UMean2Prime results do NOT match DNS validations (attachment: without_Rsgs.png). I also tried with including turbulenceProperties:R, which is from line "#includeFunc R;" in controlDict. But result is still off (attachment: with_Rsgs.png). > Is turbulenceProperties:R the same with what you meantioned in you previous post " turbulenceModel class through the method B"? > Since turbulenceProperties:R provides only instantaneous fields whereas UMean2Prime is a time averaged field, do you know any way to find a time averaged turbulenceProperties:R? kind regards, |
|
May 25, 2020, 14:05 |
V vs V
|
#5 | |
Senior Member
Santiago Lopez Castano
Join Date: Nov 2012
Posts: 354
Rep Power: 16 |
Quote:
The validation of a turbulence model starts at the consistency of the formulation (i.e. filters, coefficients, invariants). If the implementation is consistent with the theoretical aspects of the model, then you can move to verifying that for a particular scenario a solution obtained with your code (including said model) is reasonable. Classic trap in most OpenFOAM papers: to "validate" their turbulence model using a channel flow at re_tau=180. Yes, is turbulent, but the scales in a resolved simulation are almost always of a dissipative nature, and little backscattering is present. Part of this you can see it by plotting the spectrum: the inertial range is almost absent at those scales, and the integral scale is constant (unless the channel length is long enough). Anyway, this means that with a channel flow ANY DISSIPATION (under certain limits, of course) can be valid, be it numerical or otherwise. Catching errors there is unlikely. Even an under-resolved DNS performs well at those scales. So, yeah, you are up to a high road... |
||
May 25, 2020, 16:52 |
|
#6 |
New Member
David H.
Join Date: Oct 2013
Posts: 25
Rep Power: 13 |
I realize the title text said verify but the body said validate. Your response will be helpful for those who do not understand the difference.
My thesis was accepted 6 years ago, unfortunately I have not been using OpenFOAM since. I hope Sereff can find some help. |
|
May 25, 2020, 19:23 |
|
#7 |
Senior Member
Santiago Lopez Castano
Join Date: Nov 2012
Posts: 354
Rep Power: 16 |
Sorry for the late response, I guess
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Superlinear speedup in OpenFOAM 13 | msrinath80 | OpenFOAM Running, Solving & CFD | 18 | March 3, 2015 06:36 |
LES with OpenFOAM | samiam1000 | OpenFOAM | 1 | March 4, 2011 11:19 |
LES --> Fluent OR OpenFOAM | maysmech | OpenFOAM | 0 | February 2, 2011 06:20 |
64bitrhel5 OF installation instructions | mirko | OpenFOAM Installation | 2 | August 12, 2008 19:07 |
OpenFOAM Training and Workshop Zagreb 2628Jan2006 | hjasak | OpenFOAM | 1 | February 2, 2006 22:07 |