|
[Sponsors] |
May 6, 2013, 06:14 |
LES boundary layer
|
#1 |
Member
Ignacio
Join Date: Jan 2013
Posts: 33
Rep Power: 13 |
Hello,
I am going to run a LES case using the Spalding law to calculate the turbulent eddy viscosity at the boundary. OpenFOAM provides a patch called --> mutUSpaldingWallFunction My question is: How many grid lines should I set in the boundary layer? Where should I place the first grid point? (y+) Thanks a lot in advance |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[snappyHexMesh] No layers in a small gap | bobburnquist | OpenFOAM Meshing & Mesh Conversion | 6 | August 26, 2015 10:38 |
Error finding variable "THERMX" | sunilpatil | CFX | 8 | April 26, 2013 08:00 |
[Gmsh] Gmsh Boundary Layer - Wing | bcorr | OpenFOAM Meshing & Mesh Conversion | 0 | April 18, 2012 14:38 |
Boundary Layer roughness/ low reynolds wall treatment | Luigi_ | STAR-CCM+ | 1 | March 14, 2012 09:40 |
Grid Independence of Boundary layer | Luigi_ | Main CFD Forum | 0 | December 14, 2011 14:42 |