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October 1, 2005, 13:25 
Divergence detected in AMG Solver:TEMPERATURE

#1 
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Hello all,
I am working on 3D, ROTATING/ SWIRL flow inside the pipe problem. Flow is compressible and turbulent. I started with Segregated and Implicit solver with underrelaxation factor for energy equation equal to 1. I am using RSM as a turbulence model. But after some iteration I have got the "Divergence detected in AMG Solver:TEMPERATURE" and then the iteration stop. Please help. Thanks in advance, best wishes, Sachin Nimbalkar 

October 2, 2005, 08:12 
Re: Divergence detected in AMG Solver:TEMPERATURE

#2 
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Chech the boundary conditions . If it is ok so , you may reduce the URF. Wael


October 3, 2005, 08:49 
Re: Divergence detected in AMG Solver:TEMPERATURE

#3 
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You should set your limits (Solve>Controls>Limits) pretty carefully when using high URF values and the segregated solver. This will help keep your model from getting too far out of the bounds of reality. You still need some margin so that the model can adjust as it approaches a converged solution, but the default values are rediculously broad.
Hope this helps, and good luck, Jason 

October 3, 2005, 12:28 
Re: Divergence detected in AMG Solver:TEMPERATURE

#4 
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Thank you Wael and Jason.
I am still working on the problem. As soon as I figure out the solution I will let you guys know. Appreciate! 

October 4, 2005, 10:17 
Re: Divergence detected in AMG Solver:TEMPERATURE

#5 
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Don't solve Energy Equation for the first 50 iterations, then turn it back on.
If it still fails, you have other issues. 

October 5, 2005, 22:49 
Re: Divergence detected in AMG Solver:TEMPERATURE

#6 
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i solved this problem by "decreasing the relax factor to a low number"


October 16, 2005, 02:10 
Re: Divergence detected in AMG Solver:TEMPERATURE

#7 
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Hi,
Try to change the multigrid cycle for pressure from "V" to "W". 

October 8, 2010, 04:08 

#8 
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sunqiang
Join Date: Nov 2009
Posts: 23
Rep Power: 8 
I had the same problem, i used mass flow rate as intlet , after fews iterations,the error occured ,but if i changed the inlet BC to velocity inlet and maintained other BCs ,the problem was gone.


October 8, 2010, 04:14 

#9 
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sunqiang
Join Date: Nov 2009
Posts: 23
Rep Power: 8 
I had the same problem, i used mass flow rate as intlet , after fews iterations,the error occured ,but if i changed the inlet BC to velocity inlet and maintained other BCs ,the problem was gone.


February 8, 2011, 08:58 
divergence detected in AMG solver: temperature

#10 
New Member
Amit Chauhan
Join Date: May 2010
Location: Chennai, India
Posts: 12
Rep Power: 8 
I too encountered the same problem.. and I tried to solve it by above methods. but sorry to say in my case it didnt work...
but I changed my time step size and it worked... what does it physically signifies??????? 

September 7, 2012, 07:11 
Re: Divergence detected in AMG Solver:TEMPERATURE

#11 
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Orkun Temel
Join Date: Feb 2012
Posts: 13
Rep Power: 6 
Hi chauhanji,
As far as i know, there are many reasons causing the referred problem. I don't know your case, but as i understand from your solution, your problem seemed to be stability problem. Assuming that you're using explicit approach, you just need to provide that your time step size is under the limitation due to CFL condition. Probably, when you changed your delta_t, you provided this. And this is how your finite equations became stable and consistent. Physically, it is also wise to keep delta_t under the characteristic convective and diffusive time scale, so that you can obtain a numerical solution including the whole transport process. 

January 4, 2013, 06:21 

#12 
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peyman
Join Date: Mar 2012
Posts: 8
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I had a same problem and I changed the relaxation factor of energy from 1 to 0.9 and it didn't error anymore


January 5, 2013, 04:19 

#13 
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SSL
Join Date: Oct 2012
Posts: 227
Rep Power: 6 
Are you using Coupled solver? else correct your mesh. You should use a finer mesh.


March 4, 2013, 12:02 

#14 
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Fan He
Join Date: Jan 2013
Location: Virginia
Posts: 11
Rep Power: 5 
Hi all,
1 I also select this probelm by reducing UnderRelaxation Factors from Turbulent Kinetic Energy from 0.8 to 0.1. 2 I guess this problem may be caused by using a high inlet velocity (i.e. large Reynolds #), because when I use some much lower inlet velocities to run the model, I can get good results though the URF is 0.8. 3 This problem is solved, but my results in this high inlet velocity case still are not convergent (energy equation is convergent, while continuety equation and momentm equations are not convergent). I will work on this problem for some more time. Thank you for your suggestion here. 

March 4, 2013, 19:53 

#15 
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sp
Join Date: Jul 2011
Posts: 23
Rep Power: 7 
In addition to what others have said, at your pressure/mass flow inlet boundary condition, you need to set the initial/supersonic pressure to a value close to your expected upstream pressure. If you initialize with default values, it will use 0 as the pressure at the inlet.
If you are using a pressure inlet and a pressure outlet, another thing that helps is to start with a lower pressure differential between your inlet and outlet, and then gradually decrease your exit pressure to the point that you need. Good luck. 

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