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

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6 Investigation <strong>of</strong> <strong>the</strong> xz-plane<br />

300<br />

250<br />

200<br />

Q4<br />

z<br />

+<br />

150<br />

Q4<br />

secondary <strong>flow</strong><br />

100<br />

50<br />

300<br />

0<br />

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

250<br />

??]<br />

x [???]<br />

z<br />

+<br />

200<br />

150<br />

Q2<br />

Q4<br />

Q2<br />

100<br />

Q2<br />

50<br />

0<br />

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

FIGURE 6.24: Same as figure 6.23 but measured at Ó ® Ú¥Ø<br />

(red: CG Ø<br />

; blue: C_! Ø<br />

).<br />

x<br />

+<br />

??]<br />

x [???]<br />

less elongated and broader than <strong>the</strong> low-speed regions because <strong>the</strong>se <strong>flow</strong> <strong>structures</strong> originate<br />

statistically from <strong>flow</strong> regions which are fur<strong>the</strong>r away from <strong>the</strong> wall, see section 5.4. This can<br />

be estimated from <strong>the</strong> sign <strong>of</strong> <strong>the</strong> wall-normal velocity component which is represented by <strong>the</strong><br />

contours in figure 6.22. At ® Ê ª¥À <strong>the</strong>se high momentum <strong>structures</strong> look sometimes similar<br />

to <strong>the</strong> streaks with regard to size and shape according to figure 6.21 but more frequently <strong>the</strong>y<br />

resemble small elliptically shaped islands, approximately 200 wall units in length and roughly<br />

­<br />

50 to 100 wall-units in width according to figure 6.23. It can be seen from <strong>the</strong> out-<strong>of</strong>-plane velocity<br />

component, displayed in figure 6.24, that <strong>the</strong>se <strong>structures</strong>, which are labelled as sweeps,<br />

transfer momentum towards <strong>the</strong> wall. Thus, <strong>the</strong>se <strong>structures</strong> are statistically represented by<br />

126

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