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.0011a.svgz" name="7462024.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Perspective view of diffuser duct</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.0011b.svgz" name="7462024.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Outlet mesh (AIP)</td></tr></table>

<div>Diffuser duct mesh structure. The plane of symmetry is omitted in this picture.</div>

International Journal of Aerospace Engineering

fig11

Figure 11

Figure 11: Propulsive Efficiency of Ridge/Inlet Configuration 