I have meshed an entire wing in Ansys. It was fairly complex with differing materials on the sides of each volume. The problem comes when I apply the load and run the solution, Ansys does not give any errors, however the solution is no good. It does not yield any stresses, nor does it yield any deformation etc.

Could it be because I applied the loads to key points created after meshing? if this is the case how would I go about meshing keypoints located on the top of the skin at certain locations since I meshed the skin from an area shell99 element...