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

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4.8 Feasibility study<br />

10 20 30 40 50 60 70 80 10 20 30 40 50 60 70 80<br />

Streamwise direction [mm]<br />

Streamwise direction [mm]<br />

FIGURE 4.15: Instantaneous velocity vector field (left) and vorticity (right) with Ñ -vortices recorded<br />

simultaneously in two planes parallel to <strong>the</strong> wall but at different heights (lower field closer to wall).<br />

<strong>The</strong> <strong>flow</strong> direction is from left to right.<br />

an output frequency between 0.01 Hz and 1 MHz was used. <strong>The</strong> width <strong>of</strong> each pulse is freely<br />

adjustable according to <strong>the</strong> specifications <strong>of</strong> <strong>the</strong> equipment used. <strong>The</strong> delay <strong>of</strong> all output<br />

trigger pulses with respect to <strong>the</strong> input trigger can be selected in <strong>the</strong> range from 50 ns up to<br />

140 s with a resolution <strong>of</strong> 50 ns (jitter 12.5 ns).<br />

<strong>The</strong> mean displacement <strong>of</strong> corresponding particle-images was 8 pixel <strong>for</strong> ³æå”Ø©Þ¿¾çÕ s and<br />

<strong>the</strong> height <strong>of</strong> <strong>the</strong> correlation coefficient was 0.6 <strong>for</strong> ÂÛ)ÄèÂ0Û pixelÊ interrogation windows. <strong>The</strong><br />

evaluation technique <strong>of</strong> <strong>the</strong> stereoscopic images is based on <strong>the</strong> second order warping to ensure<br />

that <strong>the</strong> interrogation spots from each <strong>of</strong> a pair <strong>of</strong> stereoscopic images correspond to <strong>the</strong> same<br />

region <strong>of</strong> <strong>flow</strong> and <strong>the</strong> magnification is constant <strong>for</strong> all image positions [108]. For <strong>the</strong> evaluation<br />

<strong>of</strong> <strong>the</strong> data <strong>the</strong> FFT-based free shape cross-correlation was employed, which combines<br />

<strong>the</strong> advantages <strong>of</strong> <strong>the</strong> direct correlation (free-sized and free-shaped windows, high accuracy)<br />

and <strong>the</strong> simple FFT-based correlation (high speed evaluation), see section 2.4 <strong>for</strong> details. For<br />

sub-pixel accuracy <strong>the</strong> two dimensional Gaussian fit using <strong>the</strong> Levenberg-Marquardt method<br />

has been applied to find <strong>the</strong> position <strong>of</strong> <strong>the</strong> correlation peak and <strong>the</strong> Fisher trans<strong>for</strong>mation<br />

to determine <strong>the</strong> weight <strong>for</strong> each value, see section 2.4.2 <strong>for</strong> details. Figure 4.15 shows <strong>the</strong><br />

in-plane velocity (left) and out-<strong>of</strong>-plane vorticity distribution (right) <strong>for</strong> two distances from<br />

<strong>the</strong> wall measured simultaneously. <strong>The</strong> <strong>flow</strong> direction is from left to right and a constant<br />

convection velocity <strong>of</strong> ÈOÁÉÎÈ m/s has been subtracted from both vector fields in order to show<br />

<strong>the</strong> distribution <strong>of</strong> <strong>the</strong> velocity <strong>structures</strong> more clearly. <strong>The</strong> observation area started 265 mm<br />

67

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