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

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4.8 Feasibility study<br />

experiments in <strong>turbulent</strong> boundary layers <strong>for</strong> instance, requires that ei<strong>the</strong>r no aberrations are<br />

present or <strong>the</strong> major axis <strong>of</strong> <strong>the</strong> aberration coincides with <strong>the</strong> respective axis <strong>of</strong> <strong>the</strong> cylindrical<br />

lens. O<strong>the</strong>rwise <strong>the</strong> per<strong>for</strong>mance <strong>of</strong> <strong>the</strong> light-sheet is biased by <strong>the</strong> aberration.<br />

4.8 Feasibility study<br />

To study <strong>the</strong> accuracy <strong>of</strong> <strong>the</strong> light separation and <strong>the</strong> reliability <strong>of</strong> <strong>the</strong> multiplane stereo system<br />

described in <strong>the</strong> previous sections, <strong>the</strong> acoustic receptivity <strong>of</strong> a laminar boundary layer along<br />

a flat plate with zero pressure gradient was examined. <strong>The</strong> measurement was per<strong>for</strong>med in<br />

<strong>the</strong> open circuit low turbulence wind tunnel at DLR, which possesses a contraction ratio <strong>of</strong><br />

15:1 and a cross section <strong>of</strong> ¾ÁÃÂÅÄÇÆÁÉÈ mÊ , see figure 4.13. To obtain reproducible conditions<br />

6<br />

1.5<br />

18.65<br />

2.3<br />

6.25<br />

1<br />

2<br />

3 4<br />

5.0<br />

5<br />

0.3<br />

Units in m<br />

FIGURE 4.13: Low turbulence wind-tunnel at DLR Göttingen (TUG). Top: Side view. Bottom: Top<br />

view. 1 engine, 2 fan, 3 honeycomb and screens, 4 settling chamber, 5 side window, 6 seeding generator,<br />

7 recording system.<br />

<strong>for</strong> <strong>the</strong> generation and development <strong>of</strong> small disturbances, an acoustic excitation device was<br />

applied in <strong>the</strong> <strong>for</strong>m <strong>of</strong> a span-wise slot pair, Ë0¾¾ mm in length and ¾¥ÁÌ mm in width, which was<br />

connected to an amplifier loudspeaker system in such a way that span-wise and oblique waves<br />

could be generated simultaneously, <strong>for</strong> details see [107]. By changing <strong>the</strong> amplitude <strong>of</strong> <strong>the</strong><br />

disturbance, different stages <strong>of</strong> Í -vortices could be generated <strong>for</strong> a given free-stream velocity<br />

(12 m/s) and frequency <strong>of</strong> <strong>the</strong> acoustic excitation (150 Hz), see figure 4.14. <strong>The</strong> slot pair was<br />

located 200 mm behind <strong>the</strong> elliptically shaped leading edge <strong>of</strong> <strong>the</strong> smooth plate and embedded<br />

with high accuracy to minimise uncontrollable disturbances <strong>of</strong> <strong>the</strong> <strong>flow</strong>. <strong>The</strong> dimension <strong>of</strong> <strong>the</strong><br />

plate in stream-wise and span-wise direction are ÆÆÏÎÈ mm ÄÐÆÈ¿¾¾ mm to avoid side effects<br />

introduced by <strong>the</strong> walls <strong>of</strong> <strong>the</strong> wind tunnel test-section.<br />

To generate a homogeneous seeding and to avoid artificial <strong>flow</strong> disturbances due to <strong>the</strong><br />

injection <strong>of</strong> <strong>the</strong> tracer particles, <strong>the</strong> whole laboratory was seeded be<strong>for</strong>e starting <strong>the</strong> experi-<br />

65

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