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Hello,
I generally use hex elements wherever possible. However, I have a project right now where I have an assembly of 35 or 40 parts, many of which are complex. Simplifying the CAD solids and then slicing them up in Femap is taking far more time and money than my Client has. So, I would like to drop back to CTETRAs on some of the parts, which don't need the slicing and usually mesh pretty easily.
Not having much recent experience with CTETRAs, here are my questions:
1. Years ago, many formulations of tet elements with midside nodes had problems when used on contact surfaces. Is this still a problem with the current 10 node CTETRA? I see that Ansys and some others no longer have this problem, but can't find the info on the Nei element.
2. 4 node tet elements used to be far too stiff and severely underpredicted both deflection and stress. As such, they were a good thing to avoid. Is the current formulation of the 4 node CTETRA still problemmatic? Are there any studies of mesh density v. accuracy for the Nei element compared to theoretical?
3. Is the Nei formulation of the tet a constant stress element? I note that Ansys quite a while ago went to a formulation for the tet element that is essentially a degenerate brick, and offers improved performance.
4. Can anyone offer any Nei-specific CTETRA guidance regarding the tradeoff between higher density of 4 node CTETRAs v. 10 node formulation? The node count gets out of hand quickly with a tet mesh.
Test cases can answer the above, but that would be a project in itself. I'm hoping for some guidance to save time.
Thanks!
Andrew
Solved! Go to Solution.
