Hello,
in my model I simulate a carbon fibre wing. I do get results for it's deformation but none for the composite stress and failure in all areas. Only for certain plies stress and failure are visible. I had this problem a few times with this model. After redoing the laminate the visible areas change, but I only get results for the entire wing when I use very simple plies. I wonder why that happens. Due to the lack of a meshing feature in the 2022 version of Hyperworks I am using the 2021.2 version.
Thanks for your advice!
