 |
 |
 |
|
|
|
[Sponsors] | ||||
November 18, 2015, 11:41
|
Convergence issues in wind tunnel simulation
|
#1 |
|
New Member
Join Date: Nov 2015
Posts: 1
Rep Power: 0  |
Hi, I am currently investigating fluid flow over vehicles. I have successfully tested the ahmed body and have moved on to a more complex geometry. Using around 0.98 million nodes in the mesh, my solution has not converged infact quite the opposite. Using the k-epsilon model my residuals and drag/lift coeffs are as follows
   Any assistance or a point in the right direction would be much appreciated. Thank you all. |
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| [How to obtain supersonic flow inside a supersonic wind tunnel ?] | yx213 | Siemens | 1 | September 17, 2014 13:52 |
| Wind Tunnel Flow Simulation Mass Flow BC Issue | ledelman | SU2 | 4 | August 3, 2014 18:38 |
| Wind Tunnel Testing | Vinnende | Main CFD Forum | 4 | April 13, 2012 15:15 |
| convergence problem when use pisoFoam, LES for wind tunnel case | Forrest_Lei | OpenFOAM | 3 | July 19, 2011 06:00 |
| how to consider perforated wind tunnel wall in CFD simulation | littlelz | CFX | 4 | June 11, 2009 05:51 |
Linear Mode
