Research Article
Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method
Table 1
Geometric parameters of the wing and the piezoelectric patch.
| | Modulus of elasticity (Gpa) | Length (mm) | Width (mm) | Height (mm) |
| | Rigid part of the wing | — | 700 | — | — | | Elastic bending part of the wing | 200 | 300 | 36 | 1.5 | | Piezoelectric patch | 74 | 300 | 36 | 1 |
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