Numerical Simulation of Reactive Flows in Overexpanded Supersonic Nozzle with Film Cooling

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/252404/figures/252404.fig.007a.svgz" name="252404.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Calculated and measured wall pressure  (Case 1)</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/252404/figures/252404.fig.007b.svgz" name="252404.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Calculated and measured wall pressure (Case 2)</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/252404/figures/252404.fig.007c.svgz" name="252404.fig.007c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Comparison between calculated Cases 1 and 4</td></tr></table>

<div>Calculated and measured wall pressure in the zone downstream the injection slot.</div>

International Journal of Aerospace Engineering

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Figure 7

Figure 7: Numerical Simulation of Reactive Flows in Overexpanded Supersonic Nozzle with Film Cooling 