Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method

Table 2

Properties of different airfoils.

	(/c)	(/c)	(N·m/rad)	(Pa)	(deg)	(deg)
Airfoil without control surface	—	0.33	10	200	5	—
Morphing piezoelectric wing	0.3	0.33	10	200	5	10
Traditional wing with rigid trailing edge	0.3	0.33	10	200	5	10