Experimental Study of the Effect of Radially Distorted Inflow on a Contrarotating Fan Stage

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="503579.fig.0014a" src="https://static.hindawi.com/articles/ijrm/volume-2014/503579/figures/503579.fig.0014a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Design mass flow rate</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="503579.fig.0014b" src="https://static.hindawi.com/articles/ijrm/volume-2014/503579/figures/503579.fig.0014b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Peak pressure mass flow rate</td></tr></table></td></tr></table>

<table>Spanwise variation of axial velocity ratio at the exit of rotor-2.</table>

International Journal of Rotating Machinery

fig14

Figure 14

Figure 14: Experimental Study of the Effect of Radially Distorted Inflow on a Contrarotating Fan Stage 