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.009a.svgz" name="5396876.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Calculation domain definition</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.009b.svgz" name="5396876.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Interface definition</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.009c.svgz" name="5396876.fig.009c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Mesh generation complete</td></tr></table>

<div>Computational grid generation.</div>

International Journal of Aerospace Engineering

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Figure 9

Figure 9: Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology 