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Feature Request/Query: Modeling fully solid cross-sections (Foam Core filling 100% of internal volume) #44

@stage-be-sketch

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@stage-be-sketch

Hi SONATA team,

I am currently working on a wing project and I would like to model a cross-section that is entirely filled with a core material (e.g., foam or solid reinforcement) inside an outer skin.

I have tried using the fixed: core attribute in the YAML configuration. However, when I define a layer that covers most of the arc (from 0.01 to 0.99), I frequently encounter the following issues:

UnboundLocalError: local variable 'U' referenced before assignment in find_BSplineLst_coordinate.

ValueError: data must be of shape (n, m) in fuse_rows (cKDTree initialization).

My questions are:

Is SONATA natively designed to handle a 100% solid core filling?

What is the "best practice" YAML structure to achieve a full-core section without triggering B-spline offset errors at the leading or trailing edges?

Should I use a specific cutoff_style or a virtual web to stabilize the topology for solid sections?

Thank you for your help and for this great tool!

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