CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > CFX

SST Convergence

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 30, 2005, 10:34
Default SST Convergence
  #1
new@cfx
Guest
 
Posts: n/a
Hi,

I am facing problems in getting good convergence with an SST model. whereas for the same geometry the K-E model converges easily. The expert parameter section in the documentation mentions a parameter tef numerics option which limits the flux in regions of high omega gradient. Could someone kindly clarify what this option does exactly?

Regards,

  Reply With Quote

Old   September 30, 2005, 10:57
Default Re: SST Convergence
  #2
Robin
Guest
 
Posts: n/a
Are you sure your convergence problem is numerical? Quite often, using the SST model will capture boundary layer separation that the k-e model does not. A separated boundary layer results in a detached shear layer, which can be very unstable.

Before looking for an expert parameter, write a sequence of backup files and look for fluctuating flows downstream of separation points. YOu can also try increasing/decreasing the timestep by factors of 10. In some cases a larger timestep will be enough to get rid of the disturbance.

Regards, Robin
  Reply With Quote

Old   October 1, 2005, 02:29
Default Re: SST Convergence
  #3
Vikram
Guest
 
Posts: n/a
Hi Robin, Thanks a lot for that incisive reply. I will be trying that out and I will keep you posted. Regards, Vikram
  Reply With Quote

Old   October 1, 2005, 06:28
Default Re: SST Convergence
  #4
Vikram
Guest
 
Posts: n/a
Hi, The original question was about the tef numerics option. The documentation says that "the k-omega and SST turbulence models give convergence difficulties in areas of high gradients in "omega" , for example at a blunt trailing edge or sudden rearward facing step, in conjunction with a highly refined boundary layer grid ( generally resolved into the viscous sub-layer). In such situations a flux limiting numerics implementation can be used for the omega equation, activated by setting this parameter to 1."

So what does this flux limiting implementation do exactly? Can someone kindly enlighten me on this ? Robin?

Thanks in advance, Vikram
  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
Convergence Centurion2011 FLUENT 48 June 14, 2022 23:29
Force can not converge colopolo CFX 13 October 4, 2011 22:03
convergence problem of the SST and RNG k-e model for mixing tank ziyan7 FLUENT 0 March 8, 2011 06:13
Convergence of CFX field in FSI analysis nasdak CFX 2 June 29, 2009 01:17
Convergence issue in SST for Porous model Raj CFX 0 May 2, 2008 02:43


All times are GMT -4. The time now is 18:44.