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

Table 3

Total aerodynamic lift.

	Airfoil without control surface	Morphing piezoelectric wing	Traditional wing with rigid trailing edge
Origin, traditional linearized VLM	3.5793	11.3167	9.9551
Origin, geometrically exact VLM	3.2547	10.8865	9.4613
Aeroelastic deformation, traditional linearized VLM	6.1865	8.5917	7.8819
Aeroelastic deformation, geometrically exact VLM	5.9250	8.9471	8.1935