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

Table 2

UT700 material parameters.

Density ()	Elastic modulus (GPa)			Shear modulus (GPa)			Poisson’s ratio
	1800	115	6.43	6.43	6	6	6	0.28	0.34	0.28