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.hindawi.com/articles/ijae/volume-2015/252404/figures/252404.fig.003a.svgz" name="252404.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Results from the initial model</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/252404/figures/252404.fig.003b.svgz" name="252404.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Results from the modified model</td></tr></table>

<div>Results of one-dimensional combustion tube simulation obtained with some reaction models compared to initial and modified Evans-Schexnayder reaction model [<a href="/journals/ijae/2015/252404/#B9">12</a>].</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Numerical Simulation of Reactive Flows in Overexpanded Supersonic Nozzle with Film Cooling 