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.001a.svgz" name="5396876.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Principle of side force generation</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.001b.svgz" name="5396876.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>The installation position of the antitorque device</td></tr></table>

<div>Schematic diagram of CFF antitorque device.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology 