Moreover, you're using shell aspects. Shell elements are a great deal more at risk of convergence challenges that their equivalent stable aspects. This is due to The point that good components are way more stiffer compared to shell components due to the arithmetic driving them. You won't ever come upon a extreme thickness adjust trouble in the stab

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Excessive thickness adjust problem can (I think) interchangably be employed with excessive distortion difficulty. So I'd endorse switching towards the equal solid aspects, or merely enhance the thickness in the shell components so which they turn out to be significantly rigid and thus fewer liable to excessive thickness transform. If a bureaucra

Secondly, I do not know if you already know this or not, but in case you interept the solution (even if its managing on cluster), you should be capable to get the NR residuals for the last 3 (I ordinarily use three but you can enter a lot more) iterations. The answer will immediately stop immediately after finishing The existing iteration. In this

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