Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan-Wing Aerodynamic Characteristics

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.0022a.svgz" name="8941453.fig.0022a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>No winglet and single winglet</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.0022b.svgz" name="8941453.fig.0022b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>No winglet and double winglet</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.0022c.svgz" name="8941453.fig.0022c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>No winglet and triple winglet</td></tr></table>

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International Journal of Aerospace Engineering

fig22

Figure 22

Figure 22: Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan-Wing Aerodynamic Characteristics 