A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="252478.fig.0014a" src="https://static.hindawi.com/articles/jam/volume-2014/252478/figures/252478.fig.0014a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Drag coefficient</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="252478.fig.0014b" src="https://static.hindawi.com/articles/jam/volume-2014/252478/figures/252478.fig.0014b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Pressure drag coefficient</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="252478.fig.0014c" src="https://static.hindawi.com/articles/jam/volume-2014/252478/figures/252478.fig.0014c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Friction drag coefficient</td></tr></table></td></tr></table>

<table>Effect of mesh size on aerodynamic coefficients at Mach 1.2. The red lines are reference values.</table>

Journal of Applied Mathematics

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Figure 14

Figure 14: A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders 

Figure 14 | A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders 