nIs this the correct setup for this type of part? I made a 5 ply composite plate with a hole that would have a bolt going through so it behaves like a tab. A force would be applied on the top face. For the solid geometry exported from ACP, I selected the node at each ply, so there were a few going across and then around the circle. I didn't try the shell geometry yet. For the nodal displacement, I fixed it in the x and z direction of the cylindrical support to imitate tangential and axial constraints. However, it was not able to solve. nnn