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Old   February 6, 2018, 08:05
Default Mesh problems
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Hi guys.

I have some problem with my simulations of an open-wheel car.
I am doing a 3D steady analysis, but I get these errors:

-Conjugate-Gradient solver did not converge !
A floating point exception has occurred: floating point exception [Divide by zero]. The specific cause cannot be identified. Please refer to the troubleshooting section of the User's Guide.
Context: star.segregatedflow.SegregatedFlowSolver

-WARNING: Ap = 0 on multigrid level 6, nRows = 4203, blockSize = 1
AMG coarsening halted.

I don't understand where and what are the problems
Can you explain me why I get these two errors?

Thanks.
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Old   February 6, 2018, 08:09
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Quote:
Originally Posted by DesmoR View Post
Hi guys.

I have some problem with my simulations of an open-wheel car.
I am doing a 3D steady analysis, but I get these errors:

-Conjugate-Gradient solver did not converge !
A floating point exception has occurred: floating point exception [Divide by zero]. The specific cause cannot be identified. Please refer to the troubleshooting section of the User's Guide.
Context: star.segregatedflow.SegregatedFlowSolver

-WARNING: Ap = 0 on multigrid level 6, nRows = 4203, blockSize = 1
AMG coarsening halted.

I don't understand where and what are the problems
Can you explain me why I get these two errors?

Thanks.
Check your set up first. You have to narrow down the possible problem. Like check your mesh quality and parameters. Check physics. Then try reducing urf of pressure velocity etc. What is your physics set up?
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Old   February 6, 2018, 08:16
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I am using K-omega SST with Segregated flow and second order convection. I left all the default values for the urf.
For example the problems appear if I just add a volumetric control for the wake.
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Old   February 7, 2018, 00:42
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Originally Posted by DesmoR View Post
I am using K-omega SST with Segregated flow and second order convection. I left all the default values for the urf.
For example the problems appear if I just add a volumetric control for the wake.
ok so the problem may be with the mesh right!! May be there is sudden change in element sizes. Instead of using volumetric refinement we can use wake refinement. But it is available only with Automated mesh. You can refer CCM user guide.
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Old   February 7, 2018, 19:49
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This error is a pretty common problem for wrapped cases, is it wrapped?
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Old   February 8, 2018, 04:25
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No, it's not wrapped. I import the geometry files from rhino using .step or .iges format and then I use directly the subtract operation.
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Old   February 8, 2018, 17:21
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If you try to split the region by non-contiguous, does it result in more than one volume?
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Old   February 9, 2018, 03:27
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If you try to split the region by non-contiguous, does it result in more than one volume?
Yes, it's 100% solution. Each closed area must be a separate region
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Old   February 9, 2018, 04:37
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If you try to split the region by non-contiguous, does it result in more than one volume?
I obtain only two more regions made of one cell each.
Should i get one more region for each part or just one?
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Old   February 9, 2018, 04:42
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I obtain only two more regions made of one cell each.
Should i get one more region for each part or just one?
There should be only one region. You should get message like no region would be created. If there are more then split them. You may decide if you want to keep them and then physics will be solved fro them otherwise delete them if they are unnecessary.
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Old   February 9, 2018, 04:47
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Ok thank you. I will try to delete them and run again the simulation.
I will let you know.
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Old   November 6, 2018, 08:50
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Originally Posted by ashokac7 View Post
There should be only one region. You should get message like no region would be created. If there are more then split them. You may decide if you want to keep them and then physics will be solved fro them otherwise delete them if they are unnecessary.
Worked for me. Thanks a lot
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Old   November 16, 2018, 09:56
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This error is a pretty common problem for wrapped cases, is it wrapped?
Are you saying that floating point errors are common when using the wrapper?
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Old   November 16, 2018, 10:10
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Originally Posted by SoAero View Post
Are you saying that floating point errors are common when using the wrapper?
Not when used correctly. Floating point errors are very rarely the actual error in the simulation, they're usually a symptom of some other error, which includes user error.

The error I was referring to is the message from the AMG algorithm.
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