New Findings by High-Order DNS for Late Flow Transition in a Boundary Layer

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="721487.fig.0024a" src="https://static.hindawi.com/articles/mse/volume-2011/721487/figures/721487.fig.0024a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b><i>x = </i>465. 10 contour levels −0.456~0.718</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="721487.fig.0024b" src="https://static.hindawi.com/articles/mse/volume-2011/721487/figures/721487.fig.0024b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b><i>x = </i>464. 10 contour levels  −0.698~1.202</td></tr></table></td></tr></table>

<table>Contours of spanwise component of the vorticity disturbance in the (<i>y, z</i>)-plane at <i>t = </i>6.6<i>T.</i> Light shades of gray correspond to high values.</table>

Modelling and Simulation in Engineering

fig24

Figure 24

Figure 24: New Findings by High-Order DNS for Late Flow Transition in a Boundary Layer 