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The significance of coherent flow structures for the turbulent mixing ...

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6.4 Properties <strong>of</strong> <strong>coherent</strong> velocity <strong>structures</strong><br />

300<br />

250<br />

Q2<br />

Q4<br />

z<br />

+<br />

200<br />

150<br />

Q2<br />

Q2<br />

Q4<br />

Q4<br />

secondary<br />

secondary<br />

Q4<br />

100<br />

50<br />

Streak<br />

Q2<br />

0<br />

0 50 100 150 200 250 300 350 400 450 500 550<br />

300<br />

??]<br />

250<br />

Q2<br />

Q4<br />

x [???]<br />

200<br />

Q4<br />

z<br />

+<br />

150<br />

100<br />

Q2<br />

Q4<br />

Sweep<br />

secondary motion<br />

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50<br />

Q2<br />

0<br />

0 50 100 150 200 250 300 350 400 450 500 550<br />

x<br />

+<br />

y [???]<br />

x [???]<br />

FIGURE 6.25: Velocity fluctuations measured at Ó ® Ú¥Ø<br />

(top) and Reynolds stress component &C<br />

(bottom).<br />

<strong>the</strong> correlations shown in figure 6.8. If such a structure moves towards a low-speed streak, as<br />

visible in figure 6.24 <strong>for</strong> example, an interaction takes place and parts <strong>of</strong> <strong>the</strong> streaks, which<br />

are directly affected by <strong>the</strong> sweeps, are <strong>for</strong>ced to move away from <strong>the</strong> wall due to continuity<br />

(see blue region in ellipse). On average, this process is represented by <strong>the</strong> spatial correlation<br />

functions shown in figure 6.10 to 6.12. However, it can be seen from <strong>the</strong> samples shown in figure<br />

6.24 that <strong>the</strong> effect on <strong>the</strong> streaks is quite small in <strong>the</strong> present case. This can be explained<br />

by <strong>the</strong> fact that <strong>the</strong> momentum is insufficient to create a strong lifting <strong>of</strong> <strong>the</strong> streak. Figure 6.25<br />

shows <strong>the</strong> same interaction but <strong>the</strong> momentum transferred by <strong>the</strong> sweeps is much larger. In<br />

127

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