Investigation on the Optimal Design and Flow Mechanism of High Pressure Ratio Impeller with Machine Learning Method

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8855314/figures/8855314.fig.006a.svgz" name="8855314.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Meridional curves</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8855314/figures/8855314.fig.006b.svgz" name="8855314.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Camber line</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/8855314/figures/8855314.fig.006c.svgz" name="8855314.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Thickness (suction side)</td></tr></table>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Investigation on the Optimal Design and Flow Mechanism of High Pressure Ratio Impeller with Machine Learning Method 