Abacus - constraining a wing box
Abacus - constraining a wing box
(OP)
Hello.
I'm new to Abacus, but I really like it.
I'm trying to model the stresses in the wing box imported from CATIA V5 (http://imgur.com/WJptbul), but I fail to properly constrain the system so I end up with something like this: http://imgur.com/V6KdOiz
What am i missing?
In the actual setup the wing box is clamped at the root and loaded at the tip with a tip clamp. In the model few stringers are missing, those will be added later.
Thanks for your help
I'm new to Abacus, but I really like it.
I'm trying to model the stresses in the wing box imported from CATIA V5 (http://imgur.com/WJptbul), but I fail to properly constrain the system so I end up with something like this: http://imgur.com/V6KdOiz
What am i missing?
In the actual setup the wing box is clamped at the root and loaded at the tip with a tip clamp. In the model few stringers are missing, those will be added later.
Thanks for your help




