Figure 14.

Numerical prediction of delamination damage at the top surface of (a) ${\left[0\right]}_{32}$ (b) ${\left[+45/-45\right]}_{16s }$ (c) ${\left[0/90/90/0\right]}_{8s},$ and (d) ${\left[0/90/+45/-45\right]}_{8s}$ composite laminate.