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.006a.svgz" name="8839967.fig.006a" 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.006b.svgz" name="8839967.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Transient phase</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2021/8839967/figures/8839967.fig.006c.svgz" name="8839967.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Steady phase, LPD</td></tr></table>

<div>Pressure traces obtained by S1 and S2 for the air mass flow rate 573 g/s.</div>

International Journal of Aerospace Engineering

fig6

Figure 6

Figure 6: Combustion Characteristics in Rotating Detonation Engines 