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

<div class="floats-full-page floats-full-page-other"><h2>Table 4</h2><div class="floats-full-page-caption">Lift of rotor in wind tunnel test.</div><div class="floats-full-page-content"><table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="10"><hr /></td></tr><tr><td class="align_left">Free stream velocity (m/s)</td><td class="align_center" colspan="3">0</td><td class="align_center" colspan="3">5</td><td class="align_center" colspan="3">10</td></tr><tr><td class="align_left">Collective pitch (°)</td><td class="align_center">8</td><td class="align_center">10</td><td class="align_center">12</td><td class="align_center">8</td><td class="align_center">10</td><td class="align_center">12</td><td class="align_center">8</td><td class="align_center">10</td><td class="align_center">12</td></tr><tr><td class="align_left">Rotor lift (kg)</td><td class="align_center">35</td><td class="align_center">45</td><td class="align_center">59</td><td class="align_center">37</td><td class="align_center">49</td><td class="align_center">62</td><td class="align_center">41</td><td class="align_center">53</td><td class="align_center">65</td></tr><tr class="table-tr"><td colspan="10"><hr class="tbody-hr" /></td></tr></table></td></tr></table></div></div>

Table 4 | Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology

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Table 4: Study on Helicopter Antitorque Device Based on Cross-Flow Fan Technology

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Table 4

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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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