Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/7604279/figures/7604279.fig.004a.svgz" name="7604279.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Static pressure contour</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/7604279/figures/7604279.fig.004b.svgz" name="7604279.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Mach number contour and streamlines</td></tr></table>

<div>Detailed flow field for Case  1.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor 