Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.008a.svgz" name="6664968.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Mass flow rate vs. total pressure ratio</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.008b.svgz" name="6664968.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Mass flow rate vs. efficiency</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.008c.svgz" name="6664968.fig.008c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Total pressure ratio vs. efficiency</td></tr></table>

<div>Performance curves for the three rotors.</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio 