Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/8091927/figures/8091927.fig.0017a.svgz" name="8091927.fig.0017a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Temperature distribution on line 1</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2022/8091927/figures/8091927.fig.0017b.svgz" name="8091927.fig.0017b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Temperature distribution on line 2</td></tr></table>

<div>Temperature distribution on two marking lines. Line 1 is on the high temperature wall, while line 2 is on the low one.</div>

International Journal of Aerospace Engineering

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Figure 17

Figure 17: Effects of the Air Inlet Angle on the Combustion and Ablation Environment of a Hybrid Powder-Solid Ramjet 