Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/sv/volume-2017/8986217/figures/8986217.fig.008a.svgz" name="8986217.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Modal shape of flap</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/sv/volume-2017/8986217/figures/8986217.fig.008b.svgz" name="8986217.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Modal shape of twist</td></tr></table>

<div>The modal shapes of flaps and twists.</div>

Shock and Vibration

fig8

Figure 8

Figure 8: Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights 