Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.005a.svgz" name="5396876.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Curves of lateral force with rotation speed</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.005b.svgz" name="5396876.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Curves of power with rotation speed</td></tr></table>

<div>Influence of blade mounting angle.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology 