Aerodynamic Load Reduction on a Supercritical Airfoil Using Tilted Microjets

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/7843757/figures/7843757.fig.003a.svgz" name="7843757.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Generated grid</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/7843757/figures/7843757.fig.003b.svgz" name="7843757.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Surface jet boundary</td></tr></table>

<div>The computational grid around RAE2822 airfoil with a normal jet on the suction surface (every 4 points).</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Aerodynamic Load Reduction on a Supercritical Airfoil Using Tilted Microjets 