Wing Cell lofting error with multiple sections over constant cross-section

[ewerthen]

Use-Case with 5 cpacs sections and 4 segments and a constant cross-section: analytical_example_circ_beam_loads_composite_CPACS.zip

Error message: File "C:\Anaconda3\envs\predocs\lib\site-packages\tigl3\configuration.py", line 19045, in get_loft return _configuration.CCPACSWingCell_get_loft(self) RuntimeError: OpenCASCADE Error: BSpline curve: at least 2 poles required