Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing

Table 6

Variable thickness and angle layup scheme example.

Unbalanced coefficient	Area	Layer	Thickness	Layer order
0.2	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.2	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.2	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm