Mesh Convergence Issue In Ansys

In summary, you are trying to make a model of a sector of a compressor disk with the blade attached to it. You are running into problems with mesh convergence. You mention that you are trying to solve this issue in a very short time. Are these 4-node or 8-node elements?
  • #1
cemadenver
4
0
Hi Guys,

I 'm currently trying to make a 2D model of a sector of a compressor disk with the blade attached to it by means of a frictional contact (as shown in the attached pic). The contact between the blade and disk is frictional (coeff=0.25), augmented lagrange formulation, and adjust to touch interface treatment. I subjected all bodies to rotational velocity of 1000rpm and the boundary conditions are friction-less supports at the bottom of the disk and at its two sides (which would represent the symmetry condition during operation of the full disc). I need to determine the equivalent von-mieses stress on the disk, just below the contact point of the blade and the disc. Now, my problem is that when I tried to do a mesh convergence test, von-mieses stress value at the point of interest does not reach a stable value as I refine the mesh. The error percentage from the previous mesh refinement run doesn't keep reducing. I'd be really grateful if anyone could help me around this.
 

Attachments

  • dovetail pic.png
    dovetail pic.png
    30.7 KB · Views: 1,063
Physics news on Phys.org
  • #2
I just have one more request, I need to solve this issue in a very short time and it's quite urgent for me. Will be extremely grateful if someone can help me resolve this soon.
 
  • #3
Are these 4-node or 8-node elements? it's hard to tell from a small-scale plot. 8-node elements will probably behave better for the curved contact faces you have, if Ansys has an 8 node element with the analysis capabilities you want (I don't know, I'm not an Ansys user!)

I suspect the "random errors" are partly caused by the distorted element shapes around the small radii. Having all the elements about the same size in a model like this is fairly wasteful. You probably have 10 times more elements than you need over most of the disk sector, and 10 times too few where the stress field changes rapidly. Make sure the element shapes in the critical regions are as close to rectangles as possible.

This is a a more complcated geometry, but look at the mesh in Fig 3 and compare with yours. http://www.sciencedirect.com/science/article/pii/S0168874X99000724

Or Fig 4 here: http://www.sciencedirect.com/science/article/pii/S0142112312000400
 
Last edited:
  • #4
Hi AlephZero,

Thanks for the quick response. I tried what you told me, mainly refining the mesh locally with quad elements (most are quad, though some sparse elements had to be triangular to satisfy continuity in some regions). However, I still don't think that mesh refinement is converging for me. I've posted a graph plotting iterations vs quantity. The iterations are in steps of 0.2 mm except the last three which are in steps of 0.03mm. I used the edge sizing method of workbench for the local mesh. The last mesh size I used was 0.11mm and I think it still didn't converge (as you can see in the graph). At this point I stopped because any further refinement in mesh wasn't helping, infact all quadilaterals couldn't be maintained at that size and the mesher had to replace many by the more robust filling but less accurate triangles. I've read some papers on fe analysis of dovetail regions of turbine discs of a similar geometry and I don't think any of the papers had to go anywhere near 0.11mm for convergence. There is one thing I forgot to mention in my previous post, I have two error messages: "one or more contact regions contains a friction value greater than 0.2mm and an unsymmetric solver had to be used" and "one or more bodies may be under constrained and experiencing rigid body motion, weak spring have ben added...". I feel though the second message however is not abnormal since, I'm dealing with friciotnal contact and naturally there has to be some sliding. I've also attached the total deformation behaviour of the model just in case you want to have a look at that also. Thanks.
 

Attachments

  • 2D mesh refinement result.png
    2D mesh refinement result.png
    11.6 KB · Views: 1,805
  • total deformation.png
    total deformation.png
    30.5 KB · Views: 967
  • #5
If your displacement plot shows the actual movements (not scaled in some strange way) there is something unrealistic going on. The "blade" shouldn't be pulled a quarter of the way out of the slot. It's hard to see what has deformed wrongly from just one screen shot though.

Try a run where the blade is fixed into the disk (no sliding interfaces, just equate the matching nodes on the blade and the disk) to check you get sensible looking displacements and stresses.

Then, presumably, you can make a similar model with a very large coefficient of friction and get similar results. Then reduce the friction to the value you want.

"one or more bodies may be under constrained and experiencing rigid body motion, weak spring have ben added...". I feel though the second message however is not abnormal since, I'm dealing with friciotnal contact and naturally there has to be some sliding.
You said you had a frictionless constraint on the "bottom of the disk". If the bottom of the disk is a circle, that means it will be free to rotate about its axis, so the program will have to fix that up somehow to make the stiffness matrix nonsingular.

It might be better to fix it yourself, by constrainng one node to have zero circumferential displacement, rather than letting the program try to fix it aotomatically.

Depending how Ansys works, you may also need to fix the blade to the disk just for the first iteration, if something nonsensical happens at the start because there are no loads on the sliding boundaries.
 
  • #6
Hi AlephZero,

Thanks for the response. Just had a quick question, how will the disc rotate with a fixed support at its base? Thanks.
 

1. What is mesh convergence issue in Ansys?

Mesh convergence issue in Ansys refers to the problem of obtaining inconsistent or unreliable results when the mesh used in a simulation is not fine enough. This can result in inaccurate results and a lack of convergence in the solution.

2. What causes mesh convergence issue in Ansys?

There can be several causes of mesh convergence issue in Ansys, such as an insufficient number of elements in the mesh, poor element quality, or improper boundary conditions. It can also be caused by a complex geometry or a highly non-linear problem.

3. How can I check for mesh convergence in Ansys?

To check for mesh convergence in Ansys, you can perform a grid refinement study by successively increasing the number of elements in the mesh and comparing the results. You can also use the convergence criteria provided by Ansys, such as the residual error or solution tolerance, to determine if the solution is converging.

4. How can I improve mesh convergence in Ansys?

To improve mesh convergence in Ansys, you can try refining the mesh by increasing the number of elements in areas where the solution is not converging. You can also try using a different element type or adjusting the element size to improve element quality. Additionally, ensuring that the boundary conditions are properly defined can also help in improving mesh convergence.

5. What can I do if I cannot achieve mesh convergence in Ansys?

If you are unable to achieve mesh convergence in Ansys, it may be helpful to consult with an expert or seek guidance from the Ansys support team. They can help identify the cause of the issue and provide suggestions for improving the mesh and achieving convergence. In some cases, it may also be necessary to simplify the model or use a different simulation approach to obtain accurate results.

Similar threads

  • Mechanical Engineering
Replies
1
Views
2K
  • General Engineering
Replies
1
Views
3K
Replies
4
Views
4K
Replies
2
Views
4K
  • General Engineering
Replies
5
Views
23K
  • Mechanical Engineering
Replies
1
Views
4K
  • Mechanical Engineering
Replies
23
Views
36K
Back
Top