Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio

Table 5

Mechanical properties of the skins with different thicknesses.

Thickness (mm)	Maximum deformation (mm)	Maximum stress of the upper wing (MPa)	Maximum stress of the lower wing (MPa)	Maximum Inverse Reserve Factor of the upper wing	Maximum Inverse Reserve Factor of the lower wing
4	1031.5	713.55	734.76	3.9932	4.0353
6	873.67	605.94	604.69	2.6546	3.154
8	698.17	516.69	513.87	2.313	1.943
10	599.12	453.43	471.95	0.89972	0.95074
12	420.56	365.37	363.24	0.60421	0.61564
14	322.25	320.02	321.23	0.54848	0.49358