notekit
Mechanical
- Sep 22, 2004
- 8
I am currently modeling the static deformation of an Airbus fuselage part. The part has three main components, shell, frames and stringers. They are connected with rivets.
At the moment, I model the rivet joints by merge all the nodes in the contact area together. This assumes that the whole contacting areas is moving together not just the rivet joints. Do anybody have a better idea on how to model this connections?
Thank you very much!
At the moment, I model the rivet joints by merge all the nodes in the contact area together. This assumes that the whole contacting areas is moving together not just the rivet joints. Do anybody have a better idea on how to model this connections?
Thank you very much!