Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/4045164/figures/4045164.fig.002a.svgz" name="4045164.fig.002a" 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-preview.hindawi.com/articles/ijae/volume-2023/4045164/figures/4045164.fig.002b.svgz" name="4045164.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Drag coefficient</td></tr></table>

<div>Comparison of lift and drag coefficients versus angle of attack [<a href="/journals/ijae/2023/4045164/#B17">17</a>].</div>

International Journal of Aerospace Engineering

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Figure 2

Figure 2: Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration 