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February 16, 2016, 00:40 |
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#21 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
Rep Power: 66 |
You need at least 2 points across the structure you are trying to resolve (preferably 4 or more). Mesh independence is same as for any numerical computation. Look-up grid convergence index by Roache if you are totally lost.
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February 16, 2016, 11:10 |
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#22 |
Senior Member
Andrea
Join Date: Feb 2012
Location: Leeds, UK
Posts: 179
Rep Power: 16 |
There is no such a thing as mesh independence for a LES performed with an implicit filter (which is the most common approach when it comes to LES), since the size of the filter is directly related to the mesh size the more you refine your grid the more you tend towards DNS (for a well posed LES), so in this case is more correct to talk about grid convergence rather than grid independence.
It is possible to obtain a mesh independent LES by switching to explicit filtering, and thus eliminating the direct relationship between filtering and discretization, as explained here: https://web.stanford.edu/group/ctr/S...0/3_04_you.pdf |
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February 16, 2016, 12:36 |
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#23 |
New Member
farouk
Join Date: May 2013
Posts: 4
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hi, according to fluent a mesh corresponds to y+=1 (or less) is sufficient for LES turbulence model. to see the independance mesh simulation you could make several meshes correspond to different y+ values (ex: y+=1; 0.8; 0.6; 0.4; 0.2) and you could find the optimal mesh where there is no difference between two successive y+ values. good luck
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February 16, 2016, 14:53 |
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#24 |
New Member
Hitesh
Join Date: Sep 2015
Posts: 11
Rep Power: 10 |
Thank You Very Much all of you for reply.....
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February 16, 2016, 18:14 |
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#25 |
Senior Member
Andrea
Join Date: Feb 2012
Location: Leeds, UK
Posts: 179
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To complete my previous postI would suggest you to have a look at Celik et al, Index of resolution quality for Large Eddy Simulations, Journal of Fluids Engineering 127 (2005) 949-958
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February 16, 2016, 19:50 |
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#26 | |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
Rep Power: 66 |
For wall bounded flows (and wall-resolved LES) the y+ requirement near the walls is the most limiting factor and satisfying the y+ and some maximum cell aspect ratio (15,20,25 etc) usually dictates the largest cell size in the domain.
But if you wanted to, you could estimate the "turbulent length scale" of interest and use that as your base cell size, whether the length scale of interest is the geometric scale, integral scale, Taylor scale, or Kolmogorov scale is up to you. I also want to correct myself. Quote:
But depending on what variables it is you are trying to resolve, those can become mesh independent or mesh insensitive (but I still prefer to refer to this as grid convergence rather than grid independent). While detailed local variables such as (velocity, temperature) may be grid sensitive, you can still achieve grid insensitive results for bulk quantities like overall pressure drop, pumping power, overall heat flux, etc. |
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March 16, 2016, 13:31 |
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#27 |
New Member
Hitesh
Join Date: Sep 2015
Posts: 11
Rep Power: 10 |
Thank You very much.
one more query is there. How to determine time step size for LES(is it using CFL criteria) and is this CFL criteria is important for implicit LES formulation? |
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March 16, 2016, 13:49 |
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#28 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
Rep Power: 66 |
I think you meant implicit time-stepping and not implicit LES (implicit LES means LES with an implicit filter).
The CFL criteria is for determining stability which you generally do not have trouble with in implicit time-stepping schemes. But the Courant number does tell you a lot about temporal resolution. Stability also does not guarantee accuracy and you still need small enough time-steps to ensure accuracy. Hence, you should still target sufficiently small time-step (Courant number approximately 0-1) to ensure your results are accurate and ensure you are not temporally clipping the results. |
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