Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/1208492/figures/1208492.fig.0017a.svgz" name="1208492.fig.0017a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Inlet flow angle of the aft stator</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/1208492/figures/1208492.fig.0017b.svgz" name="1208492.fig.0017b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Inlet axial velocity of the aft stator</td></tr></table>

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International Journal of Aerospace Engineering

fig17

Figure 17

Figure 17: Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number 