Investigation of the Normal Blowing Approach to Controlling Wingtip Vortex Using LES

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6688569/figures/6688569.fig.002a.svgz" name="6688569.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Leading edge</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6688569/figures/6688569.fig.002b.svgz" name="6688569.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Near maximum thickness</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6688569/figures/6688569.fig.002c.svgz" name="6688569.fig.002c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Trailing edge</td></tr></table>

<div>The spatial distribution of mesh at the wingtip.</div>

International Journal of Aerospace Engineering

fig2

Figure 2

Figure 2: Investigation of the Normal Blowing Approach to Controlling Wingtip Vortex Using LES 