22.10.2014 Views

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

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

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

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

: T<br />

ž<br />

ž<br />

<br />

<br />

ò<br />

<br />

5.3 Statistical properties <strong>of</strong> <strong>the</strong> <strong>flow</strong><br />

<strong>for</strong> <strong>the</strong> stream-wise velocity in [55] but here <strong>the</strong> velocity could be determined directly without<br />

a sophisticated calibration procedure as required in case <strong>of</strong> <strong>the</strong> hot-wire investigation to<br />

compensate <strong>the</strong> additional heat-loss induced by <strong>the</strong> solid wall. When <strong>the</strong> wall-normal velocity<br />

component is considered, <strong>the</strong> first measurement point obtained with <strong>the</strong> hot-wire technique is<br />

far<strong>the</strong>r away from <strong>the</strong> wall by one order <strong>of</strong> magnitude, compared with <strong>the</strong> present PIV investigation,<br />

due to <strong>the</strong> orientation and size <strong>of</strong> <strong>the</strong> sensor applied in [55]. <strong>The</strong> domain covered by<br />

<strong>the</strong> PIV investigation is nearly constant when considered in outer variables :‚à[Ü 4‘“’,” (<br />

)<br />

because <strong>of</strong> <strong>the</strong> weak dependence <strong>of</strong> <strong>the</strong> boundary-layer Ü thickness on <strong>the</strong> Reynolds number.<br />

However, when considered in inner variables on <strong>the</strong> o<strong>the</strong>r hand, it can be seen that <strong>the</strong> investigation<br />

at &~€ رοތz roughly covers <strong>the</strong> domain from •<br />

—–<br />

<strong>the</strong> •Œ : T Œ range , because <strong>the</strong> log-law region increases in thickness with increasing<br />

Reynolds number when considered in wall-units. This allows to examine <strong>the</strong> near-wall<br />

, Reynolds number effects within <strong>the</strong> logarithmic region between<br />

οÞzŒ<br />

š<br />

: T<br />

Œ and at &~€ ؘ’,”zŒŒ<br />

structure at Ø<br />

&~€ and large-scale <strong>flow</strong> <strong>structures</strong> at &~€ Ø›’,”zŒŒ . <strong>The</strong> size <strong>of</strong> <strong>the</strong> region, where<br />

Œ<br />

h–<br />

•Œ <br />

v rms<br />

/u τ w rms<br />

/u τ u rms<br />

/u τ<br />

3<br />

2<br />

1<br />

u +<br />

rms<br />

w +<br />

rms<br />

Re Θ<br />

=7800 (PIV)<br />

Re Θ<br />

=7140 (HWA)<br />

rms<br />

v rms<br />

/ u<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

Re θ<br />

=7800 (PIV)<br />

Re Θ<br />

=7140 (HWA)<br />

0<br />

0<br />

10œ<br />

10œ<br />

1<br />

Ÿ +<br />

vrms<br />

10<br />

2<br />

œ<br />

y +<br />

10œ<br />

3<br />

œ<br />

4<br />

10<br />

0.0<br />

10<br />

œ<br />

0<br />

10œ<br />

1<br />

10<br />

2<br />

œ<br />

y +<br />

œ<br />

3<br />

10<br />

œ<br />

4<br />

10<br />

3<br />

0.8<br />

v rms<br />

/u τ w rms<br />

/u τ u rms<br />

/u τ<br />

2<br />

1<br />

0<br />

0<br />

10œ<br />

10œ<br />

1<br />

Re Θ<br />

=15000 (PIV)<br />

Re Θ<br />

=16080 (HWA)<br />

10<br />

2<br />

œ<br />

y +<br />

10œ<br />

3<br />

œ<br />

4<br />

10<br />

rms<br />

v rms<br />

/ u<br />

0.6<br />

0.4<br />

0.2<br />

0.0<br />

10<br />

œ<br />

0<br />

10œ<br />

1<br />

Re θ<br />

=15000 (PIV)<br />

Re Θ<br />

=16080 (HWA)<br />

10<br />

2<br />

œ<br />

y +<br />

œ<br />

3<br />

10<br />

œ<br />

4<br />

10<br />

FIGURE 5.3: Left: Non-dimensional rms-pr<strong>of</strong>iles <strong>of</strong> <strong>the</strong> three velocity ¡N¢<br />

fluctuations<br />

€U£©¨<br />

<strong>for</strong><br />

¡N¢ (top) and<br />

wall coordinate in inner-law scaling <strong>for</strong> both Reynolds numbers.<br />

vs¥s¥s (bottom). Right: Dependence <strong>of</strong> <strong>the</strong> anisotropy parameter ª «Z¬®­ ¯4¬®°²±<br />

s¥s<br />

¬ on <strong>the</strong><br />

€¤£¦¥§<br />

77

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!