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

Table 4

Variable thickness layout scheme.

Unbalanced coefficient	Area	Layer	Thickness	Layer order
0.2	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.3	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.4	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.5	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.6	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.7	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm
0.8	I	40	8.0 mm
	II	36	7.2 mm
	III	32	6.4 mm