|
[Sponsors] |
July 20, 2010, 23:49 |
Inviscid Flow Convergance issues
|
#1 |
New Member
James Merkel
Join Date: Jul 2010
Posts: 1
Rep Power: 0 |
HI,
I am currently doing a inviscid flow simulation over a body and appear to be having a convergance issue. My Residuals were for momentum and continuity were settling around .1 and .01 and not dropping any lower. however when i monitor lift and lift coefficient, they appear to be converging perfectly within .5% Is this acceptable? i have tried dropping the relaxation values for the segregated flow model but still no change.. Thanks! |
|
November 19, 2010, 15:18 |
Re:
|
#2 |
New Member
Tallness
Join Date: Nov 2010
Location: Upstate NY
Posts: 2
Rep Power: 0 |
Depends what software you are using. With most CFD software (STAR-CCM+) you can set up monitors for different convergence factors and monitor those as well. For example, if you are interested in the concentration of a species in a sensitive area, you could set up a volumetric average monitor for that specific species and watch the actual number converge. Residuals are necessary, but can be misleading. You might have a converged solution in front of you and not know it by only looking at the residuals. Another example would be if you were modeling a small server room and were interested in the temperatures in that space. Instead of watching the residual for energy, you could set up a monitor to watch the volumetric average temperature throughout the room. You will notice this monitor converge towards a single number whereas your residual might not show what is considered convergence. Hope this helps..
-yoyo |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Flow meter Design | CD adapco Group Marketing | Siemens | 3 | June 21, 2011 09:33 |
Inviscid flow in a Laval nozzle | Giorgio | FLUENT | 1 | August 3, 2007 06:46 |
time step for inviscid supersonic wedge flow. | yaseer | Main CFD Forum | 1 | March 8, 2007 10:40 |
Inviscid flow | Atit Koonsrisuk | CFX | 12 | January 2, 2003 13:40 |
Velocity Gradients at Inviscid Flow | Lada | FLUENT | 0 | January 15, 2001 08:20 |