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!