Geometry Design of Coaxial Rigid Rotor in High-Speed Forward Flight

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/6650375/figures/6650375.fig.0030a.svgz" name="6650375.fig.0030a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Baseline rotor blade</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/6650375/figures/6650375.fig.0030b.svgz" name="6650375.fig.0030b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Optimized rotor blade</td></tr></table>

<div>Blade surface pressure contour distribution of baseline rotor and optimized rotor.</div>

International Journal of Aerospace Engineering

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Figure 30

Figure 30: Geometry Design of Coaxial Rigid Rotor in High-Speed Forward Flight 