A Grid Fusion Lifting Surface and Its Flow Control Mechanism at High Angles of Attack

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/7788011/figures/7788011.fig.004a.svgz" name="7788011.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Surface grid distribution</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/7788011/figures/7788011.fig.004b.svgz" name="7788011.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Grid distribution of flow field in typical sections</td></tr></table>

<div>Computational domain grid of grid fusion lifting surface with the diversion angle of 20° and grid number of 2.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: A Grid Fusion Lifting Surface and Its Flow Control Mechanism at High Angles of Attack 