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.007a.svgz" name="2564314.fig.007a" 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.007b.svgz" name="2564314.fig.007b" 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.007c.svgz" name="2564314.fig.007c" 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.007d.svgz" name="2564314.fig.007d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Torsion angle</td></tr></table>

<div>The linear optimization process.</div>

Shock and Vibration

fig7

Figure 7

Figure 7: Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation 