Study on Dynamic Stall Control of Rotor Airfoil Based on Coflow Jet

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/8845924/figures/8845924.fig.004a.svgz" name="8845924.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift coefficient</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/8845924/figures/8845924.fig.004b.svgz" name="8845924.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Drag coefficient</td></tr></table>

<div>Variation of the lift and drag coefficients of the NACA6415 baseline and CFJ airfoils.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Study on Dynamic Stall Control of Rotor Airfoil Based on Coflow Jet 