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.0024a.svgz" name="6664968.fig.0024a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>3D-opt rotor</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.0024b.svgz" name="6664968.fig.0024b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Tip-forward+0.1</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.0024c.svgz" name="6664968.fig.0024c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Tip-forward+0.2</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.0024d.svgz" name="6664968.fig.0024d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Tip-forward+0.30</td></tr><tr class="fig-image" id="e"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/6664968/figures/6664968.fig.0024e.svgz" name="6664968.fig.0024e" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(e) </b>Tip-forward+0.40</td></tr></table>

<div>Mach number contours at 90% span of the five rotors at working point 1.</div>

International Journal of Aerospace Engineering

fig24

Figure 24

Figure 24: Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio 