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

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aperture, it is shown how to eliminate certain aberrations by accepting aberrations <strong>of</strong> o<strong>the</strong>r<br />

types which are <strong>of</strong> no harm in PIV. This point is <strong>of</strong> primary importance because higher order<br />

aberrations like distortion and curvature <strong>of</strong> <strong>the</strong> field just influence <strong>the</strong> position and <strong>for</strong>m <strong>of</strong><br />

<strong>the</strong> image but do not lower <strong>the</strong> resolution. <strong>The</strong>y can be completely eliminated numerically by<br />

using <strong>the</strong> methods examined in chapter 3. Primary aberrations, on <strong>the</strong> o<strong>the</strong>r hand, like spherical<br />

aberration, coma and especially astigmatism deteriorate <strong>the</strong> image and alter <strong>the</strong> shape in<br />

a characteristic way. This leads to an increased measurement error because <strong>the</strong> per<strong>for</strong>mance<br />

<strong>of</strong> <strong>the</strong> peak-fit routine <strong>for</strong> sub-pixel accuracy strongly decreases <strong>for</strong> particle image diameter<br />

not equal 2-3 pixel. For completeness it should be mentioned at this point that <strong>the</strong> multiplane<br />

stereo PIV technique is frequently applied in o<strong>the</strong>r laboratories by now, see [77, 32] <strong>for</strong><br />

example, and also commercially available.<br />

<strong>The</strong> second part <strong>of</strong> this <strong>the</strong>sis reveals <strong>the</strong> main fluid mechanical results measured with<br />

<strong>the</strong> Multiplane Stereo PIV techniques in <strong>the</strong> temperature-stabilised, closed circuit wind tunnel<br />

at <strong>the</strong> Laboratoire de Mécanique de Lille (LML). In chapter 5 <strong>the</strong> stream-wise wall-normal<br />

plane (ñŸ¹ -plane) <strong>of</strong> <strong>the</strong> <strong>turbulent</strong> boundary layer <strong>flow</strong> is examined at ª«§=@? í parameter and <strong>the</strong> ¸ ä í ½A=@? í ï B<br />

turbulence-level<br />

76 to 78. <strong>The</strong> shape, size and coherence <strong>of</strong> <strong>the</strong> <strong>turbulent</strong> <strong>flow</strong> <strong>structures</strong> and <strong>the</strong>ir dependence<br />

on <strong>the</strong> Reynolds number was estimated from <strong>the</strong> primary spatial ªS·· correlations ªSÔÔ , and<br />

<strong>of</strong> <strong>the</strong> velocity fluctuations and ªDC#EFC#E , see page 80 to 87. <strong>The</strong> similarity between <strong>the</strong><br />

ªSÙ&Ù<br />

size ªS·· <strong>of</strong> ªSÙ&Ù and in stream-wise direction and <strong>the</strong> elliptical shape around <strong>the</strong> maximum,<br />

accompanied with <strong>the</strong> general variation <strong>of</strong> <strong>the</strong> orientation with increasing wall distance <strong>of</strong><br />

<strong>the</strong> fixed point, implies a strong relation between both fluctuations over several hundred wall<br />

units. However, <strong>the</strong> crestfallen shape <strong>of</strong> ªSÙ&Ù <strong>the</strong> correlation indicates that <strong>the</strong> physical mechanism<br />

which connects ä <strong>the</strong> å and fluctuations depends on <strong>the</strong> wall distance. This can be<br />

explained by <strong>the</strong> different shape <strong>of</strong> <strong>the</strong> <strong>coherent</strong> <strong>flow</strong> <strong>structures</strong>. While <strong>the</strong> near-wall region<br />

¹¥»&% °<br />

below is dominated by well organised low-speed streaks, <strong>the</strong> log-law region above<br />

is dominated by shear-layers and large-scale eddy <strong>structures</strong>. It is shown that <strong>the</strong> pro-<br />

°<br />

¹&»G%<br />

duction <strong>of</strong> turbulence ¹ »<br />

¡ °<br />

at is frequently associated with span-wise vortices which are<br />

located on top <strong>of</strong> <strong>the</strong> shear-layers. <strong>The</strong>se vortices pump low-speed fluid from <strong>the</strong> shear-layer<br />

away from <strong>the</strong> wall. This process is associated with a relatively large velocity component in<br />

wall normal direction. However, <strong>the</strong> spatial extent <strong>of</strong> <strong>the</strong> region äŸã where is negative is quite<br />

small. Large areas äŸã Û with are frequently associated with relatively simple eddy <strong>structures</strong><br />

(no vortices) which transfer high momentum fluid towards <strong>the</strong> wall as assumed in <strong>the</strong> <strong>mixing</strong><br />

length <strong>the</strong>ory by Prandtl, see page 91 to 94. As <strong>the</strong> stream-wise momentum transported with<br />

this structure is quite large, <strong>the</strong>ir contribution to <strong>the</strong> production <strong>of</strong> turbulence is already significant<br />

when <strong>the</strong> negative wall-normal velocity component is relatively small. However, as <strong>the</strong><br />

probability density function <strong>of</strong> <strong>the</strong> wall-normal velocity component is symmetrically within<br />

<strong>the</strong> log-law region, this process is compensated on average by a motion <strong>of</strong> high-speed fluid<br />

away from <strong>the</strong> wall. This changes in <strong>the</strong> near-wall region examined in chapter 6. <strong>The</strong> analysis<br />

<strong>of</strong> <strong>the</strong> various double- and triple-correlations, which are associated with <strong>the</strong> production <strong>of</strong> tur-<br />

165

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