Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9589415/figures/9589415.fig.002a.svgz" name="9589415.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Crossover angle = 0°</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9589415/figures/9589415.fig.002b.svgz" name="9589415.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Crossover angle = 90°</td></tr></table>

<div>Definition of the crossover angle.</div>

International Journal of Aerospace Engineering

fig2

Figure 2

Figure 2: Vibration and Performance Analyses Using Individual Blade Pitch Controls for Lift-Offset Rotors 