I'll try the CRODS on all sides, the model runs with CQUADS though. I have a point load (in-plane shear force) at one of the nodes. A colleague mentioned I needed to apply the load on all nodes in the line of action of the shear force (i.e. on one edge of the model where load is applied). There...
Hello all,
I have a two cell wing box cell structure that has been idealized as concentrated areas for the flanges and stiffeners. The spar flanges and stiffeners are assumed to carry only axial loads and the skin and spar webs are assumed to take only the shear loads. My question is how would I...
Hello all,
I have a two cell wing box cell structure that has been idealized as concentrated areas for the flanges and stiffeners. The spar flanges and stiffeners are assumed to carry only axial loads and the skin and spar webs are assumed to take only the shear loads. My question is how would...
