Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/sv/volume-2017/2564314/figures/2564314.fig.008a.svgz" name="2564314.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Wing weight</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/sv/volume-2017/2564314/figures/2564314.fig.008b.svgz" name="2564314.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Wingtip displacement</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/sv/volume-2017/2564314/figures/2564314.fig.008c.svgz" name="2564314.fig.008c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Flutter speed</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/sv/volume-2017/2564314/figures/2564314.fig.008d.svgz" name="2564314.fig.008d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Torsion angle</td></tr></table>

<div>Nonlinear optimization process.</div>

Shock and Vibration

fig8

Figure 8

Figure 8: Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation 