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Divergence detected in AMG Solver:TEMPERATURE |
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November 19, 2016, 10:05 |
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#21 |
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abhijeet jaiswal
Join Date: Sep 2016
Posts: 7
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sorry bro....i am not understand your problem....so please define it clearly....
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November 19, 2016, 10:07 |
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#22 | |
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abhijeet jaiswal
Join Date: Sep 2016
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Quote:
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November 19, 2016, 10:15 |
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#23 | |
New Member
yes
Join Date: Oct 2016
Posts: 17
Rep Power: 10 |
Quote:
l work on the three dimensional computational fluidic dynamics modeling of PEM fuel cell I study the effect of the inlet pressure on the current density.and to draw the polarisation curve of fuel cell it should show the relation between the Vcell and current my work is normally it work very good but I have problem in Vcell=0,6 the current density deacrease a lot and after that it work normally I mean why the current density fall and deacrese a lot in V cell =0. is the work correct and it work normally or the is a mistake thank you |
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November 19, 2016, 10:21 |
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#24 | |
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abhijeet jaiswal
Join Date: Sep 2016
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Quote:
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November 19, 2016, 11:16 |
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#25 |
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yes
Join Date: Oct 2016
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November 22, 2016, 09:18 |
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#26 |
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abhijeet jaiswal
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March 11, 2017, 03:20 |
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#27 |
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Rajendra Singh
Join Date: Aug 2015
Posts: 16
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First, you should check your mesh. If the mesh is bad or ratio is too high, the solution will be divergent and you will get AMG error.
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March 11, 2017, 10:13 |
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#28 |
New Member
yes
Join Date: Oct 2016
Posts: 17
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the mesh is Good and all the parameters are perfect
Sent from my SM-J700H using CFD Online Forum mobile app |
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July 3, 2017, 23:56 |
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#29 |
New Member
Join Date: Jul 2017
Posts: 1
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Hey abir, how is it going?. I have had the same issue with amg solver: w-swirl. It does not matter how your mesh is but a little fine should be good enough. I have a question for you, how are you importing you geometry for analysis ?.
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January 20, 2018, 13:37 |
Under relaxation Factor in Fluent
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#30 |
Member
Hells Blade
Join Date: Nov 2017
Posts: 61
Rep Power: 9 |
On what basis does one decide to reduce the value of which URF in Fluent for eg when using k epsilon should i resude trubulence or the dissipation rate or another parameter or the value of the equation which is diverging in the residuals .
Also how does this affect my results |
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March 15, 2018, 02:37 |
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#31 |
Member
Vignesh Lakshmanan
Join Date: Nov 2016
Posts: 79
Rep Power: 10 |
Hi Everyone,
First of all sorry for restarting the thread. I am working with simulation of air flow through an airconditioning outdoor unit panel, with condenser coil. Fan I have modelled using MRF. My mesh size is 4,000,000 cells and 0.97 skewness. My aim is to estimate the airflow (CFM) delivered by the fan. The problem works fine. I got result matching within 5% wrt experiments. The problem is, while running, I initially ran the problem in Fluent -13 using standard initilaization and the case completed. But, if I run the same case in Fluent-17 , I get AMG solver divergence: Temperature in the first iteration itself. But if I run in Fluent -17 using Hybrid initialisation, the case runs. Could someone explain what is the problem with Fluent -17?? Thanks |
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April 22, 2018, 06:44 |
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#32 | |
New Member
Daniel
Join Date: Nov 2017
Location: Queensland Australia
Posts: 9
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Quote:
I am having a similar problem with the choice of the multigrid cycle. Please, why changing the multigrid cycle for pressure from "V" to "W" for the 3D ROTATING/ SWIRL flow inside the pipe? |
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April 25, 2018, 07:17 |
AMG Solver Divergence: Temperature
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#33 |
New Member
Rajan Bhandari
Join Date: Dec 2017
Posts: 14
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When I used inlet BC's as velocity-inlet and outlet BC's as pressure outlet, no error takes place. But when I changed outlet BC's to velocity-inlet, the divergence error occured. Why is that so?
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April 25, 2018, 07:52 |
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#34 |
Member
Vignesh Lakshmanan
Join Date: Nov 2016
Posts: 79
Rep Power: 10 |
Are you sure you changed the outlet boundary condition to velocity intlet??? If ya, then obviously it will diverge because you had given an inlet at the outlet.
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May 9, 2018, 02:58 |
About the convergence of VAWT residual.
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#35 |
New Member
Inderjeet Singh
Join Date: Feb 2018
Posts: 1
Rep Power: 0 |
Hello everyone, I am working vertical axis wind turbine. I have designed fine 2d model in SW and now trying analyse it's flow analysis. But I am facing convergence problem from many days. My solution residual is not going down to 10-3. My meshing skewness ratio 0.83, orthogonal quality 1., aspect ratio 93.
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