Numerical Simulations of Vertical Discrete Gusts Driven by Trailing Edge Blowing

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/5520443/figures/5520443.fig.006a.svgz" name="5520443.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>CC020-010EJ circulation control airfoil profile [<a href="/journals/ijae/2023/5520443/#B28">28</a>]</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/5520443/figures/5520443.fig.006b.svgz" name="5520443.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Details of the 3D mesh</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/5520443/figures/5520443.fig.006c.svgz" name="5520443.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>The pressure coefficient distribution data</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/5520443/figures/5520443.fig.006d.svgz" name="5520443.fig.006d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>The lift coefficient data</td></tr></table>

<div>The airfoil profile, mesh, and results of numerical method validation.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Numerical Simulations of Vertical Discrete Gusts Driven by Trailing Edge Blowing 