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.001a.svgz" name="7462024.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>General Atomics, Avenger [<a href="/journals/ijae/2018/7462024/#B6">6</a>]</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.001b.svgz" name="7462024.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Northrop Grumman, Global Hawk [<a href="/journals/ijae/2018/7462024/#B7">7</a>]</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.001c.svgz" name="7462024.fig.001c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Boeing, X-47 [<a href="/journals/ijae/2018/7462024/#B8">8</a>]</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7462024/figures/7462024.fig.001d.svgz" name="7462024.fig.001d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>EADS, Barracuda [<a href="/journals/ijae/2018/7462024/#B9">9</a>]</td></tr></table>

<div>Top-mounted inlets on different UAVs.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Propulsive Efficiency of Ridge/Inlet Configuration 