Propulsive Efficiency of Ridge/Inlet Configuration

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0032a.svgz" name="7462024.fig.0032a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Total pressure ratio variation with Mach number</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0032b.svgz" name="7462024.fig.0032b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Captured mass flow rate at the AIP</td></tr></table>

International Journal of Aerospace Engineering

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Figure 32

Figure 32: Propulsive Efficiency of Ridge/Inlet Configuration 