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.006a.svgz" name="7462024.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Highly integrated inlet</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.006b.svgz" name="7462024.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Highly integrated inlet with ridge concept</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.006c.svgz" name="7462024.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Sectioned view of ridge/inlet integration</td></tr></table>

<div>Highly integrated inlet with and without ridge on a flat surface, used in CFD simulations.</div>

International Journal of Aerospace Engineering

Propulsive Efficiency of Ridge/Inlet Configuration

Figure 6