Effect of Aeroelastic Tailoring Design on Wing Mode

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/1711088/figures/1711088.fig.0013a.svgz" name="1711088.fig.0013a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Area 1 chordal deformation</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/1711088/figures/1711088.fig.0013b.svgz" name="1711088.fig.0013b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Area 2 chordal deformation</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/1711088/figures/1711088.fig.0013c.svgz" name="1711088.fig.0013c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Area 3 chordal deformation</td></tr></table>

<div>Relationship between the unbalanced coefficient and the chordal deformation of the wing.</div>

International Journal of Aerospace Engineering

fig13

Figure 13

Figure 13: Effect of Aeroelastic Tailoring Design on Wing Mode 