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.006a.svgz" name="8986217.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Coefficient of normal force</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/sv/volume-2017/8986217/figures/8986217.fig.006b.svgz" name="8986217.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Coefficient of pitching moment</td></tr></table>

<div>Coefficients of unsteady normal force and pitching moment during stall onset.</div>

Shock and Vibration

fig6

Figure 6

Figure 6: Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights 