Message 1 of 11
Issue with lofting airfoil profiles
Not applicable
06-24-2016
12:44 PM
- Mark as New
- Bookmark
- Subscribe
- Mute
- Subscribe to RSS Feed
- Permalink
- Report
Hello, I'm having some trouble lofting a few simple airfoil shapes. I've imported two NACA 0005 airfoils with chords of 3 and 2 in an attempt to loft a wing shape that tapers. I was able to do this just the other day, but now I get an error saying that
"Error: Loft1 Reference Failures. The loft could not be created. Try changing the inputs, swapping profiles for rails or a centerline, or adjusting the continuity conditions."
Before it was saying it could not create a meaningful geometry change, or something along those lines. I'm not really sure what to do for this, as it seems to be a very simple lofting operation.