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Composites Modeling: Conventional/Continum shells

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Dillip30

Aerospace
Joined
Feb 17, 2010
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1
Location
CA
Hello,
I am trying to model a foam core/carbon epoxy skin sandwich specimen for static stress analysis (in three point bending) in ABAQUS 6.8-2/Standard.

In my model, I have the foam core as solid and skins as shells sitting right on top of the foam core (No gaps/offsets) in the assembly. The skin is tied to the core during analysis using geometric tie constraints.

I created a continuum shell section with the correct layup. When applying the section properties to the skin, what should I set the offset parameter to in this situation?

In general, can someone explain me what the offset parameter and reference surface mean for conventional shells and continuum shells?
Thanks
 
You would find a detailed description of reference surface and offset parameter in Abaqus analysis user's manual, Section 25.6.3 (Abaqus 6.9).
 
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