Assessing Turbulence Models on the Simulation of Launch Vehicle Base Heating

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4240980/figures/4240980.fig.006a.svgz" name="4240980.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Pressure</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4240980/figures/4240980.fig.006b.svgz" name="4240980.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Axial velocity component</td></tr></table>

<div>Pressure and axial velocity component distribution along the rocket center axis from the bottom.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Assessing Turbulence Models on the Simulation of Launch Vehicle Base Heating 