Combustion Characteristics in Rotating Detonation Engines

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/8839967/figures/8839967.fig.002a.svgz" name="8839967.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Global view</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/8839967/figures/8839967.fig.002b.svgz" name="8839967.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Close-up view</td></tr></table>

<div>Pressure traces obtained by S1 and S2 for the air mass flow rate 72 g/s.</div>

International Journal of Aerospace Engineering

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Figure 2

Figure 2: Combustion Characteristics in Rotating Detonation Engines 