|
[Sponsors] | |||||
|
|
|
#1 |
|
New Member
Eric
Join Date: Mar 2013
Posts: 22
Rep Power: 2 ![]() |
Hi,
I have previuosly posted here related to a nozzle mesh problem which has been solved with a fine mesh, good schemes as well as suitable turbulence model. However, I am now extending my model to the complete geometrical entity which is a 1.2 meter long lance with varying radius(minimum radius 1mm, max radius 4mm). My goal is to calculate the flow rate of water (velocity, density=constant) of the complete lance using known pressures at inlet and outlet, 50 mbarg and 0 barg, respectively. Reynolds number is approximatley 200 (from experimental resutls) so I use laminar flow settings. At the moment while using simpleFoam, my convergence is very slow and approaches constant residual higher than my required tolerance. Using relaxation factors for U, p around 0.01 - 0.1 leads to a continuing minimisation of the residual, however, very slow. Looking at late intermediate iterations in paraView, it appears that the velocity profile isn't correct as the flow has not a shape of a parabola (maybe explained by the fact that the mesh has a lot of cells in the center of the tube). It is becoming clearer and clearer that my mesh is most likely not good enough, however, what that exactly means in my case, I am not sure of. My current mesh is based on the geometry seen in the attached file, consisting of about 100 000 hex cells. My question is maybe too general but what should my mesh look like to improve convergence and a good result that compares to the experimental data? Thanks for your input |
|
|
|
|
|
|
|
|
#2 | |
|
Member
Andreas Wendy
Join Date: Aug 2012
Posts: 63
Rep Power: 2 ![]() |
Quote:
100.000 cells are not much. when your mesh is base on blockMesh and SHM just douple the cell numbers in the blockMeshDict and try to compute. best wishes Andreas |
||
|
|
|
||
|
|
|
#3 |
|
Senior Member
HECKMANN Frédéric
Join Date: Jul 2010
Posts: 121
Rep Power: 4 ![]() |
Just to confirm, your mesh is 3D ?
The best thing to find if you mesh is good is to look at your data with paraview or any other software. Try to find the high gradient regions and check if you have enough cells in the gradient direction. To build a good mesh from the first time, you need to have a good guess of the flow structure and you also need to use all your previous simulation experiences. |
|
|
|
|
|
![]() |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Waves2Foam Related Topics | ngj | OpenFOAM Running, Solving & CFD | 299 | May 9, 2013 09:16 |
| compiling firefoam | Farshad_Noravesh | OpenFOAM | 27 | December 24, 2012 04:21 |
| meshing F1 front wing | Steve | FLUENT | 0 | April 17, 2003 12:37 |
| Ignore cells on partition boundary | Karl | FLUENT | 7 | May 11, 2002 22:12 |
| Looping over cells | Karl | FLUENT | 4 | March 26, 2002 21:18 |