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. 2021 Nov 28;13(23):4159. doi: 10.3390/polym13234159

Figure 20.

Figure 20

Failure chart of CFRP composite cylindrical shells as a function of the shape factor (wall slenderness = radius/thickness) and stacking sequence (0°: axial fibre layup, 90°: transverse fibre layup, QI: quasi-isotropic layup, and optimal: [55/55/06]S) [160].