Postbuckling Analysis of an Aircraft Fuselage

Application ID: 133501


This model studies the structural deformation of an aircraft fuselage structure subjected to buckling loads. The structure is an assembly of panels and skin connected by rivets. The Fasteners feature sets up a large number of connections and computes the forces acting on each rivet.

この model の例は, 通常次の製品を使用して構築されるこのタイプのアプリケーションを示しています.