Propulsive Efficiency of Ridge/Inlet Configuration

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0029a.svgz" name="7462024.fig.0029a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Inlet without ridge</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0029b.svgz" name="7462024.fig.0029b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Ridge/inlet configuration</td></tr></table>

<div>Mach contours at different sections at <i>M<sub>∞</sub></i> = 0.8.</div>

International Journal of Aerospace Engineering

fig29

Figure 29

Figure 29: Propulsive Efficiency of Ridge/Inlet Configuration 