Computational Investigation of Flow Control Methods in the Impeller Rear Cavity

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/2187975/figures/2187975.fig.001a.svgz" name="2187975.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>The impeller rear cavity with baffle</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/2187975/figures/2187975.fig.001b.svgz" name="2187975.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>The impeller rear cavity with swirl-controlled orifice</td></tr></table>

<div>Impeller rear cavity with control method.</div>

International Journal of Aerospace Engineering

fig1

Figure 1

Figure 1: Computational Investigation of Flow Control Methods in the Impeller Rear Cavity 