Convergence Solution

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  • Last Post 30 March 2020
HCR_student posted this 17 March 2020

Hello everyone, I am facing a problem with the convergence graph. 

Before, I ran 300 iterations for my solution and I was unable to reach convergence. This is the graph I have achieved.

After that, I ran 850 iterations and reached convergence. The graph is as shown below.

I observed that there is a big spike at around 400~500 iterations. I am not so sure about convergence as I am still a beginner at ANSYS Fluent. I am not sure if there is a problem with this graph and if my convergence is correct or wrong. 

Please help!

 

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kkanade posted this 30 March 2020

i suggest you use tri mesh with prisms. 

please go through meshing methods 

Regards,

Keyur

 

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HCR_student posted this 27 March 2020

Hi, I have created a section view of a window frame by referencing to a picture model and there were chamfered edges hence I chamfered those corners. 

I am doing a CFD and FEA thermal model of this window frame. In the model above, the window frame has air "solids" to study the effect of the inclusion of air in thermal transfer. 

Just to clarify some more, for CFD, you have mentioned that hex dominant should never be used for CFD and so I used Multizone method and selected the prism setting instead.

For FEA, even though the analysis is the same as CFD and it is going through a "fluid" (air "solids"), is it wrong to use multizone method with hexa setting? The reason I am choosing hexa setting is because it gives a better mesh compared to the prism setting. 

Thank you so much for your help!

kkanade posted this 27 March 2020

Please see help documentation to get more information about meshing methods. 

Regards,

Keyur

 

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rwoolhou posted this 26 March 2020

Hex dominant method gives a very good layer of cells next to the surface and fills the rest up with rubbish quality.  Multizone with hex uses a pave/map mesh as required and will usually give a very good mesh. 

Hex & tet are both good in their own way. I'll leave you to read up on the various reasons.  In your case if the domain is extruded then sweep to give prisms is fine. However, the cells quality in the corners of some of the zones is awful: why have you chamfered those corners? 

What are you actually trying to solve? Once you get a mesh?

 

HCR_student posted this 26 March 2020

Alright thank you. However may I know if there is a difference between using Hex-dominant method and using multizone method (hexa)? 

Since I am not able to use the Hex-dominant method for CFD, will multizone method (prism) or tetrahedrons be better? 

When comparing the mesh quality metrics between the multizone method (prism) or tetrahedrons, the quality of multizone method (prism) is better. However I understand that prism is considered a 'wedge', so in this case, I am unsure of what to use for the mesh setting for CFD. 

I am solving this in the 3D Computational Grid. 

kkanade posted this 26 March 2020

to get more no. of elements across gap, please use edge sizing. 

please check more on edge sizing in help doc. you can also find many threads on this community. 

Regards,

Keyur

 

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HCR_student posted this 25 March 2020

Thank you for your reply!!

I am able to get this mesh after changing the mapped mesh type to prism under multizone method. The Orthogonal Quality value is 0.11. However, my mesh quality metrics were better with the previous hexa shape. 

How do I make sure that I am getting at least 3 elements across any gaps? 

I am running this simulation with FEA and CFD. For the FEA, does it matter more for my quality metrics to be optimal or tri element (PRISM setting)? 

Please help!

kkanade posted this 24 March 2020

use tri elements. make sure you have atleast 3 elements across any gap. use edge or face sizing. 

Regards,

Keyur

 

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HCR_student posted this 23 March 2020

Thank you for your response! That is what I am trying to model. It is a solid window cross section with fluid addition for the air. For the mesh settings, I used Multizone method while leaving the default 'mapped mesh type' to hexa. For this case, do I change it to prism? 

rwoolhou posted this 23 March 2020

The jumps in cell size aren't going to help, and resolution isn't enough assuming you have fluid regions. What are you trying to model, as I'd expect some temperature variation over a fluid zone.  Also, if you used "hex dominant" method, don't it's only for Mechanical and should never be used for CFD. 

HCR_student posted this 23 March 2020

Thank you for your help, this is the mesh that I achieved. All my mesh quality fits into the acceptable range. 

kkanade posted this 23 March 2020

can you please post image of your mesh cross section. 

please try to change your inputs so that you can solve it on student license. 

reduce your problem size by using symmetry if possible. 

Regards,

Keyur

 

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HCR_student posted this 22 March 2020

It is above 0.1. However I am not able to further reduce the element size due to my student license.

kkanade posted this 20 March 2020

yes. 

please check min orthogonal quality. it should be above 0.1. 

Regards,

Keyur

 

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HCR_student posted this 19 March 2020

This is the best mesh I can achieve with the Student License. Did the lack of mesh quality result in that huge spike?  

kkanade posted this 19 March 2020

please check mesh density. you may need to refine the mesh. also check orthogonal quality of the mesh. 

please search quality and refinement on this community. you would find many posts. 

Regards,

Keyur

 

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HCR_student posted this 19 March 2020

Thank you for your reply! I ran 3500 iterations to check and this is the result that I have:

I have checked my results and there is no difference from the previous simulation shown in the first post with 850 iterations. 

Temperature graph for 3500 iterations

(temperature graph for 3500 iterations)

VERSUS

(temperature graph for 850 iterations(or less due to convergence))

Since this is the case, would it be correct for me to state that it reached convergence correctly and that I am able to use 850 iterations for all my simulations? 

rwoolhou posted this 17 March 2020

Look at your flow field. Residuals are a function of the numerical error in the model, but aren't the only convergence check: do the tutorials and you'll be shown monitor points too. Chances are the flow has a number of stable solutions, and it took a while for the bulk flow to establish and then settle down. 

To add, I'd be wary of those results and run on for another few hundred iterations. Turn off convergence checking on the Residuals panel. 

 

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