Hey all,
I need some help with a composite simulation. I want to model a foam core, that's surrounded entirely by a composite laminate. I can think of multiple ways to model that, but I'm not shure, which is the right one.

This is what my sorta test geometry looks like.
The section view for that looks like this:

That is with the core being part of the laminate and it obviously overlaps itself, which doesn't seem like the right way of modeling the part.
The other way would be with the laminate and the core being part of separate components.
This is with the laminate extended inward:

And this is with the laminate extended outward from the core geometry:

Apart from wanting to know, what's the right way to do it and why, there're a few other questions I have:
Hyperworks takes the offset of the layers, which aren't lying directly on the shell geometry into account for its calculations, right?
Is a freeze contact actually the right way to model a contact between a composite and a foam or honeycomb core?
Would rounds be favorable for the laminate geometry (sort of like in the first picture)?
That's a rather long question, but I'd really apprectiate some help with this.