|November 18, 2014, 16:47||
Solution will not converge?
Join Date: Nov 2014
Posts: 21Rep Power: 2
I'm trying to simulate a wind tunnel test. The Fluent model has a fluid domain of 460 x 460 x 1220 mm, & at the center is a wing 'projected span' = 200mm, 'center chord' = 81.82mm.
The educational version I'm using is limited to 512,000 cells. I've tried to use a fine mesh with 'inflation' layer on the wing. Slightly bigger mesh in a 'sphere of influence' around wing. Again a slightly bigger mesh for the rest of the 'fluid domain'.
I'm using a coupled 'Pressure/Velocity', 1st order model, but can not get convergence. What should I do to try and get it to converge?
Just incase, I've attached the files below:
|convergence problems, fluent|
|Thread||Thread Starter||Forum||Replies||Last Post|
|Naca 0012 (compressible and inviscid) flow convergence problem||bipulsaha||FLUENT||1||July 6, 2011 07:51|
|simple algorithm, converge of solution||bbasal||Main CFD Forum||0||February 13, 2010 03:58|
|Solution Does Not Converge||Rif||Main CFD Forum||3||March 7, 2008 06:33|
|My Solution wont Converge!!!||Chris||FLUENT||6||April 16, 2005 18:57|
|what to do when solution doesn't converge?||Jenny||CFX||5||January 28, 2004 05:00|