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Abstracts - KTH Mechanics

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Combined Velocity and Temperature Measurement in a Buoyancy<br />

Induced Ring Vortex<br />

S.M.M. Salim a , J.G.C. Kunnen a , C.C.M. Rindt a and A.A. v. Steenhoven a<br />

A combined velocity and temperature measurement in a buoyancy induced<br />

vortex ring was conducted. The vortex ring was produced by a droplet of<br />

Rhodemine B solution falling into a small tank filled with a solution of equal<br />

concentration but higher temperature. The main target was to test the accuracy of a<br />

combined velocity and temperature measurement technique using a pulsed laser.<br />

Additionally, a dye-visualization was conducted to understand the formation process<br />

of the ring vortex.<br />

The experimental setup consists of a small tank filled with a Rhodamine B<br />

solution (1.0×10<br />

10<br />

1<br />

20<br />

-4 mol/m 3 ) seeded with hollow spherical 10µm particles. A 29 Hz<br />

single pulsed Nd:YAG laser (532nm wavelength) was used as a lightsource. A 1.0 mm<br />

thick light sheet was created. Two 10-bit CCD cameras were used to capture the PTV<br />

and LIF images. A high pass filter of 532nm was put in front of the camera which<br />

captures the LIF signal emitted by the Rhodamine B (wavelength around 575nm) in<br />

order to block the light intensity scattered by the particles.<br />

To obtain the temperature field an innovative correction method was developed<br />

to correct for the spatio-temporal variations of the Nd:YAG laser intensity. The<br />

correction is local and based on a correction line by line. The method requires<br />

knowledge of the temperature field in part of the image.<br />

The velocity field is measured to see if the flow field could be resolved in the<br />

vortex cores which have a maximum outer diameter of 20mm. Figure 1(a) and (b)<br />

show the vorticity field as derived from the measured velocity field and the vorticity<br />

distribution along a line through the vortex cores. It can be concluded that the flow<br />

field can be resolved with high accuracy. Figure:1(c) shows the temperature field as<br />

measured in a different realization using the correction method. The result clearly<br />

shows the low-temperature vortex cores (Note different scale). The present method<br />

will be used for investigation of the 3D wake behaviour behind a heated cylinder 1 .<br />

____________________________<br />

a<br />

Energy Technology Group, Mechanical Engineering Department, Technische Universiteit Eindhoven,<br />

The Netherlands<br />

1 Ren et al., Physics of Fluids 16 (8): 3103 – 3114 (2004)<br />

-10<br />

0<br />

-30<br />

-1<br />

0<br />

-15 2.5 20 -15 2.5 20 0 10 20<br />

Figure1: (a) vorticity field (b) one line vorticity (c) temperature distribution<br />

10<br />

69

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