Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/7561856/figures/7561856.fig.005a.svgz" name="7561856.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Geometry of a Fan-wing airfoil</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/7561856/figures/7561856.fig.005b.svgz" name="7561856.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Geometry of a cross-flow fan blade</td></tr></table>

<div>Fan-wing section dimension parameter.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust 