Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/5583681/figures/5583681.fig.0013a.svgz" name="5583681.fig.0013a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Mass flow-total pressure ratio</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/5583681/figures/5583681.fig.0013b.svgz" name="5583681.fig.0013b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Mass flow-efficiency</td></tr></table>

<div>Comparison of the performance between the optimized blade and original blade in the second phase.</div>

International Journal of Aerospace Engineering

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Figure 13

Figure 13: Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy 