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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 />

pare [111]. This is shown in <strong>the</strong> lower right graph. It is not surprising that <strong>the</strong> maxima do<br />

not coincide as <strong>the</strong> high momentum <strong>flow</strong> structure originates statistically from ÄHÅ locations<br />

where » ÅFEHGJI Ä4Å while low-momentum <strong>flow</strong> <strong>structures</strong> have <strong>the</strong>ir origin in <strong>the</strong> near-wall<br />

region on average, where » Å E Ä Å holds (see upper right figure). However, <strong>the</strong> reason<br />

that <strong>the</strong> maximum <strong>of</strong> K 6 ' , with 6 Æ , is fur<strong>the</strong>r away from <strong>the</strong> wall with respect to K 6 ' ,<br />

with 6 £ , is not evident. To examine <strong>the</strong> physical process associated with this experimental<br />

result, <strong>the</strong> statistical properties <strong>of</strong> a fully developed <strong>turbulent</strong> boundary layer <strong>flow</strong> along<br />

a flat plate is investigated in stream-wise span-wise planes located at Ä Å ;<br />

by using <strong>the</strong> multiplane stereo PIV technique described in chapter 4. First <strong>of</strong> all, <strong>the</strong> joint<br />

probability density function <strong>of</strong> <strong>the</strong> velocity fluctuations is analysed to determine <strong>the</strong> basic statistical<br />

properties <strong>of</strong> <strong>the</strong> <strong>coherent</strong> velocity <strong>structures</strong> like <strong>the</strong>ir occurrence, intensity and main<br />

<strong>flow</strong> direction relative to <strong>the</strong> wall. <strong>The</strong>reafter various spatial correlation, cross-correlation and<br />

conditional-correlation functions are presented in order to compare <strong>the</strong> mean size and shape<br />

<strong>of</strong> <strong>the</strong> dominant <strong>flow</strong> <strong>structures</strong> being present in <strong>the</strong> near-wall region <strong>of</strong> <strong>the</strong> <strong>flow</strong>. <strong>The</strong> dynamic<br />

<strong>of</strong> <strong>the</strong> dominant <strong>structures</strong> is investigated by means <strong>of</strong> spatio-temporal correlation and<br />

cross-correlation functions measured in spatially separated planes. Finally, characteristic <strong>flow</strong><br />

fields are considered to illuminate <strong>the</strong> relation between <strong>the</strong> instantaneous <strong>flow</strong> <strong>structures</strong> with<br />

respect to <strong>the</strong> averaged ones and to estimate <strong>the</strong> contribution <strong>of</strong> <strong>the</strong> identified <strong>coherent</strong> <strong>flow</strong><br />

<strong>structures</strong> to <strong>the</strong> production <strong>of</strong> turbulence and transport <strong>of</strong> Reynolds stresses.<br />

6.1 Experimental set-up<br />

þ¡ <br />

Ó and ,<br />

<strong>The</strong> experimental investigation was per<strong>for</strong>med 18 m behind <strong>the</strong> leading edge <strong>of</strong> <strong>the</strong> flat plate<br />

in <strong>the</strong> temperature stabilised closed-circuit wind-tunnel shown in figure 1.4 on page 8. <strong>The</strong><br />

multiplane stereo PIV-equipment applied <strong>for</strong> <strong>the</strong> investigation consists <strong>of</strong> <strong>the</strong> same BMI four<br />

pulsed Nd:YAG laser system as outlined in section 5.2, but in contrast to <strong>the</strong> configuration<br />

described on page 72, here <strong>the</strong> system was arranged in such a way that <strong>the</strong> differently polarised<br />

light pulses leave <strong>the</strong> laser housing at different output ports. This allows to cover a wider<br />

range <strong>of</strong> light-sheet spacings (up to a few cm) and an independent positioning <strong>of</strong> both beampairs,<br />

as pointed out in section 4.2. Behind each port one optical bench was installed with<br />

three appropriate lenses and a L98ŒÓ -retardation plate which allows to rotate <strong>the</strong> direction <strong>of</strong> <strong>the</strong><br />

polarisation vector continuously. By using long focal length lenses, <strong>the</strong> laser beams could be<br />

<strong>for</strong>med into sheets <strong>of</strong> about * Á mm thickness at <strong>the</strong> measurement position, corresponding to<br />

. It should be noted that <strong>the</strong> main problem associated with <strong>the</strong> generation <strong>of</strong> a light-<br />

ÅN; Ä<br />

sheet running parallel to a flat surface is <strong>the</strong> loss <strong>of</strong> energy with decreasing wall distance, due to<br />

<strong>the</strong> darkening <strong>of</strong> <strong>the</strong> light-sheet by <strong>the</strong> wall. This difficulty can be solved ei<strong>the</strong>r by using more<br />

optical elements, as described in section 4.8, or by using long focal length lenses (in <strong>the</strong> meter<br />

range) as applied here. <strong>The</strong> positions <strong>of</strong> <strong>the</strong> light-sheets could be smoothly adjusted in vertical<br />

direction by moving properly coated mirrors, mounted on a micrometer translation stage. <strong>The</strong><br />

determination <strong>of</strong> <strong>the</strong> distance <strong>of</strong> <strong>the</strong> light-sheets from <strong>the</strong> wall was achieved by illuminating<br />

a square metal block, placed on <strong>the</strong> flat plate and covered with light-sensitive paper. <strong>The</strong><br />

recording system utilised <strong>for</strong> this investigation is similar to <strong>the</strong> unit described in section 5.2<br />

apart from <strong>the</strong> lenses, which where replaced by mm Carl Zeiss lenses because <strong>of</strong> <strong>the</strong> short<br />

observation distance þ¡ (see table 6.1), and <strong>the</strong> required polarising beam splitter-cubes and<br />

OP<br />

mirrors in front <strong>of</strong> <strong>the</strong> lenses according to section 4.1. <strong>The</strong> arrangement was installed below<br />

<strong>the</strong> wind-tunnel, as shown in figure 6.2, at positions summarised in table 6.1. <strong>The</strong> positions <strong>of</strong><br />

98

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