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

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/5847627/figures/5847627.fig.004a.svgz" name="5847627.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Aerodynamic lift coefficient</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/5847627/figures/5847627.fig.004b.svgz" name="5847627.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Aerodynamic moment coefficient</td></tr></table>

<div>Effect of angle of attack and driving voltages on aerodynamic coefficient.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method 