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

<div class="floats-full-page floats-full-page-figure"><h2>Figure 10</h2><div class="floats-full-page-caption"><div>Blade mounting angle is 10 degrees.</div></div><div class="floats-full-page-content"><table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-01.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.0010a.svgz" name="5396876.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Curves of side force with rotation speed</td></tr><tr class="fig-image" id="b"><td><object data="https://static-01.hindawi.com/articles/ijae/volume-2016/5396876/figures/5396876.fig.0010b.svgz" name="5396876.fig.0010b" 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></div>

Figure 10 | Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology

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Figure 10: Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology

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Figure 10

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<p><em>International Journal of Aerospace Engineering </em>serves the international aerospace engineering community through the dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles.</p>


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<p>Chief Editor, Professor Zhao, is based at the University of Canterbury and his research interests include applying theoretical, numerical and experimental approaches to study combustion instability, thermoacoustics and aerodynamics.</p>


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