Aerodynamic Interaction Characteristics Study of the Ducted Coaxial Propeller for a Novel eVTOL in Hovering

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/8098307/figures/8098307.fig.007a.svgz" name="8098307.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift breakdown on each part under different rotation speed</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/8098307/figures/8098307.fig.007b.svgz" name="8098307.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Torque breakdown on each part under different rotation speeds</td></tr></table>

<div>Lift and torque breakdown on each parts of DCP and FCP.</div>

International Journal of Aerospace Engineering

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Figure 7

Figure 7: Aerodynamic Interaction Characteristics Study of the Ducted Coaxial Propeller for a Novel eVTOL in Hovering 