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

Table 3

Equal thickness layup scheme.

Unbalanced coefficient	Layer	Thickness	Layer order
0.2	40	8.0 mm
0.3	40	8.0 mm
0.4	40	8.0 mm
0.5	40	8.0 mm
0.6	40	8.0 mm
0.7	40	8.0 mm
0.8	40	8.0 mm