Marcos Tejeda
unread,Mar 9, 2026, 8:51:16 AM (5 days ago) Mar 9Sign in to reply to author
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Hello everyone! I'm contacting you to ask about a fuselage that's giving me a hard time... I developed the complete model and was able to solve it using VLM, but I've never been able to solve it using the panel method. I've attached the VSP3 file. I honestly don't remember which version I created it in, but it must have been around V3.35.
The problem is that when I run CompGeom, it returns a positive theoretical area (which is correct), a zero wetted area (this is the strangest thing of all...), a negative theoretical volume (which could indicate that there are intersecting surfaces), and a -NaN volume (Wow...). Therefore, it doesn't generate a mesh.
The attached model is essentially made up of superellipses (except for the nose, which is a point). The nose doesn't have a flap (because it's a point), but the tail does. What have I tried?:
* Removing almost all the skinning requirements.
* Replace some of the superellipses with rectangles with rounded corners.
* Replace all the superellipses and rounded rectangles with ellipses.
* Delete the sections one by one, from the tail to the bow, until only the initial and final sections remain (to identify the problematic section).
* Export only the fuselage to a new file in version 3.48.2 and try running CompGeom.
None of these actions has helped me obtain a valid mesh.
Sorry for the length of the message, but I wanted to share everything I've tried without success. I'm probably making some rookie mistake that I'm not noticing. Thanks in advance!
Best regards.