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.004a.svgz" name="8941453.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(a) Computational domain</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.004b.svgz" name="8941453.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(b) Mesh generation in ring region</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.004c.svgz" name="8941453.fig.004c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(c) Slip interface</td></tr><tr class="fig-image" id="d"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.004d.svgz" name="8941453.fig.004d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(d) Mesh at leading edge winglet</td></tr><tr class="fig-image" id="e"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8941453/figures/8941453.fig.004e.svgz" name="8941453.fig.004e" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(e) All flow grid</td></tr></table>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan-Wing Aerodynamic Characteristics 