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

near wall treatment for k-omega on finite difference grid

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 18, 2024, 13:12
Exclamation near wall treatment for k-omega on finite difference grid
  #1
Member
 
Tom Waits
Join Date: Aug 2018
Posts: 42
Rep Power: 7
TomWaits is on a distinguished road
I am coding up k-omega-SST on a finite difference grid (such that u,p,omega,k are defined at the grid points and not at the cell centers). The near wall boundary condition for omega is
\omega = \frac{6\nu}{\beta_i y^2}


However y=0 for a finite difference grid at the wall! And my solution is blowing up at the boundaries if I take y to be the distance from the wall to the nearest grid point in my grid and use that omega at the wall. What is the appropriate way to treat omega in the near wall case for grids which are not cell centered?


Additionally, should I expect \omega to be very large near the wall if my yplus is small? As y->0, omega->large. But in the log layer as y->0, k->0 so omega remains bounded.


Many thanks for any help,
Tom Waits



Many thanks for any help,
Tom Waits

Last edited by TomWaits; May 21, 2024 at 14:42.
TomWaits 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
SU2-7.0.1 on ubuntu 18.04 hyunko SU2 Installation 7 March 16, 2020 04:37
[Commercial meshers] Fluent3DMeshToFoam simvun OpenFOAM Meshing & Mesh Conversion 50 January 19, 2020 15:33
Enhanced wall treatment and Enhanced wall functions Alina FLUENT 2 January 3, 2012 18:48
Combustion Convergence problems Art Stretton Phoenics 5 April 2, 2002 05:59
Grid Independent Solution Chuck Leakeas Main CFD Forum 2 May 26, 2000 11:18


All times are GMT -4. The time now is 05:47.