Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/1477251/figures/1477251.fig.0024a.svgz" name="1477251.fig.0024a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Rotor37</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2023/1477251/figures/1477251.fig.0024b.svgz" name="1477251.fig.0024b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>RotorSD</td></tr></table>

<div>Pressure differences between the pressure and suction sides of the clearances along the chords at the four tip clearances.</div>

International Journal of Aerospace Engineering

fig24

Figure 24

Figure 24: Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors 