Effect of Aeroelastic Tailoring Design on Wing Mode

Table 2

Lift coefficient and drag coefficient of HIRENASD wing under different grid numbers.

	Mesh 1	Mesh 2	Mesh 3	Mesh 4	Mesh 5
Element
Node
	0.324	0.350	0.3669	0.3559	0.3561
	0.049	0.038	0.0331	0.0342	0.0343