CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

TKE budget equation in LES

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 11, 2014, 23:58
Default TKE budget equation in LES
  #1
New Member
 
SSSSS
Join Date: Jun 2011
Posts: 28
Rep Power: 14
doctorWho is on a distinguished road
Hi,

I am calculating TKE budget equation by using solutions from LES simulation.
From filtered momentum equation of incompressible flow,(Please note than variables are filtered/resolved value and filter symbol is omitted)
\frac{\partial u_i }{\partial t} + \frac{\partial}{\partial x_j} (u_i u_j) = -\frac{1}{\rho} \frac{\partial p}{\partial x_i} + \nu \frac{\partial}{\partial x_j}(\frac{\partial u_i}{\partial x_j} + \frac{\partial u_j}{\partial x_i}) - \frac{\partial \tau_{ij}}{\partial x_j}
By using linear eddy-viscosity model, \tau_{ij} = -2 \nu_t S_{ij}, the above equation reduces to
\frac{\partial u_i }{\partial t} + \frac{\partial}{\partial x_j} (u_i  u_j) = -\frac{1}{\rho} \frac{\partial p}{\partial x_i} + (\nu  +  \nu_t)\frac{\partial}{\partial x_j}(\frac{\partial u_i}{\partial x_j} +   \frac{\partial u_j}{\partial x_i})

I could get tke budget equation using the above equation with time averaging like RANS
\frac{\partial k }{\partial t} + \bar{u_j}\frac{\partial k}{\partial x_j} = -\bar{u_i' u_j'} \frac{\partial \bar{u_i}}{\partial x_j} - \frac{1}{\rho} \frac{\partial   \bar{u_i' p'}}{\partial x_j} -   \frac{1}{2} \frac{\partial \bar{u_i' u_i'  u_j'}}{\partial x_j} + (\nu+\nu_t)   \frac{\partial^2 k}{\partial x_j^2}  - (\nu+\nu_t) \bar{\frac{\partial   u_i'}{\partial x_j}\frac{\partial  u_i'}{\partial x_j}}
where bar means time mean and tke k=0.5(u_i'u_i') and resolved fluctuation u_i'=u_i-\bar{u}_i.

this equation is basically identical to the counterpart from RANS except for \nu+\nu_t instead of \nu

When I applied this equation to the results of flow around a circular cylinder, I found there is imbalance around shear layer otherwise balance is made.

I have checked my discretizing each term and it looks good. When I compared resolved turbulent stress (u'v', u'w' and v'w') to subgrid stress (\tau_{ij}), resolved stress is more than 99%, that means I have resolved most of turbulent field. How can I explain this imbalance around shear layer?

Thanks in advance.

Last edited by doctorWho; March 12, 2014 at 10:04.
doctorWho is offline   Reply With Quote

Old   March 12, 2014, 03:49
Default
  #2
Senior Member
 
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71
FMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura about
According to the book of Sagaut, the equations 3.30 to 3.33 are in the form you should use. Now, is your solution statistically steady? What about production and dissipation budget?
FMDenaro is offline   Reply With Quote

Old   March 12, 2014, 10:02
Default
  #3
New Member
 
SSSSS
Join Date: Jun 2011
Posts: 28
Rep Power: 14
doctorWho is on a distinguished road
FMDenaro

Yes, the solution is statistically steady. As I understand, equation 3.30 of Sagaut is equation for instantaneous resolved kinetic energy not resolved turbulent kinetic energy. Also equation 3.33 is equation for unresolved kinetic energy but mine is equation for resolved turbulent kinetic energy which is following the time averaging of RANS.
Do you mean that I cannot use tke equation in LES?

As I check production and dissipation around shear layer, production is about 10 times larger than dissipation.
doctorWho is offline   Reply With Quote

Old   March 12, 2014, 11:27
Default
  #4
Senior Member
 
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,764
Rep Power: 71
FMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura aboutFMDenaro has a spectacular aura about
To be more clear, when you compute a LES solution your velocity field is

ULES = G*u = u -u'LES

then you can compute the satistical average

<ULES> = <u> -<u'LES>

Therefore, being <u> = URANS = u -u'RANS

<ULES> = URANS -<u'LES>

You can see the difference ...
FMDenaro is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Some problem of "Qcriterion.mcr& yuyuxuan Tecplot 9 February 12, 2016 03:27
Budget terms in LES shahzeb irfan FLUENT 0 August 10, 2011 00:00
Budget terms in LES shahzeb irfan Main CFD Forum 0 August 7, 2011 23:57
Derivation of Momentum Equation in Integral Form Demonwolf Main CFD Forum 2 October 29, 2009 19:53
Diffusion Equation izardy amiruddin Main CFD Forum 2 July 4, 2002 08:14


All times are GMT -4. The time now is 17:33.