Hi have a big plated structures (support for a foundry ladle) and I have a big problems to mesh all the structures at the same time. Do I decided to mesh separately. Importing on Mecway the meshes I have two plates that have to been joined with bonded contact but I receive the attached message. I tried to move the parts (mesh) and to adjust the tolerance on bodend contact window with no succes. Any idea?
Thanks in advance
On the pictures only two parts of the structures...other parts must be joined with bonded contact
Comments
Or, if you use the non-TIE option, it allows unlimited distance as long as the slave nodes are in the direction of the master face normals. So for flat plates like this, it should connect with no problems.
I'll switch to *EQUATION but I will work on a simple model to understand if the problem is due to the type of elements.
Regards
I thought that it has no problems with 2D elements because CCX expands them to 3D elements but with shell not every nodes partecipates to *TIE, so the results is not acceptable.CCX manual about this section must be interpreted literally
Look to the solution when the master/slave nodes are placed on the same plane.
I tried to change tolerance but I never obtain the right solution.
Last chance is to try applying shell offset.
Other problem is how CCX expands shell elements. If the master/slave surface are not placed at the right distance you will obtain two different thickness
Regards
In the meantime I tried to apply offset to the shell and also these parameters has effect on the results
I see what you mean about reading the manual. It explicitly says shells aren't allowed so I've added an error message to Mecway if you try to use *TIE with shells or beams.
I did find that it seems to work OK as long as the shell T-joints aren't on the Master surface. But I wouldn't be confident that it's completely right.
I always preffer to make a mesh extrusion and work with solid elements, at least with small models.
I think that's no possible to assign a general rule for shell/tie combination
Agreement with classic theory (Saint Venant beams) is very good. I'm testing a frame modelled with two mesh block bonded with RBE (Mesh onto Salome and imported). The same frame is modelled with beam element with a FEA for steel structures (that I utilize to design steel frames) and in modal analysis the results are very close.
Obviously stress field is different because in shell model there are singularity not present on beam model. Some differences I found on reactions but the model weight is slightly different because of the presence of the plates on shell model