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Indeed this problem is related to the resolution of the interpolated cross sections. Possible solution is to introduce a fixed high resolution. This was achieved with 200 points:
A more efficient solution could be scanning the points of the interpolated sections, although this would create a more complex code.
Just implemented the most simple solution. 250 intermediate nodes should be enough for most applications. If someone is troubled with this, the value can be made adjustable.
The connection to the fuselage is sometimes wrong. This might have something to do with the reduced number of nodes in the cross sections.
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