A DES Procedure Applied to a Wall-Mounted Hump

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="149461.fig.0012a" src="https://static.hindawi.com/articles/ijae/volume-2012/149461/figures/149461.fig.0012a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>RANS</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="149461.fig.0012b" src="https://static.hindawi.com/articles/ijae/volume-2012/149461/figures/149461.fig.0012b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Instantaneous DES</td></tr></table></td></tr></table>

<table>Spanwise averaged vorticity magnitude contours.</table>

International Journal of Aerospace Engineering

fig12

Figure 12

Figure 12: A DES Procedure Applied to a Wall-Mounted Hump 