Effect of Partial Span Aspiration on the Performance of a Transonic Axial Compressor Rotor: A Numerical Study

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijrm/volume-2015/761918/figures/761918.fig.009a.svgz" name="761918.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Inlet to rotor</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijrm/volume-2015/761918/figures/761918.fig.009b.svgz" name="761918.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Exit to rotor</td></tr></table>

<div>Radial variation of relative Mach number at inlet and exit to the baseline rotor at 100% design rotational speed and comparison with experimental data of [<a href="/journals/ijrm/2015/761918/#B12">12</a>].</div>

International Journal of Rotating Machinery

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Figure 9

Figure 9: Effect of Partial Span Aspiration on the Performance of a Transonic Axial Compressor Rotor: A Numerical Study 