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.0012a.svgz" name="8839967.fig.0012a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Continuous high speed images</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/8839967/figures/8839967.fig.0012b.svgz" name="8839967.fig.0012b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Frequency domain analysis of the pressure trace</td></tr></table>

<div>Continuous high-speed images and frequency domain analysis for LPD, 20000 fps, air flow 677 g/s, and equivalence ratio 0.62 [<a href="/journals/ijae/2021/8839967/#B31">31</a>].</div>

International Journal of Aerospace Engineering

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Figure 12

Figure 12: Combustion Characteristics in Rotating Detonation Engines 