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Assessment of a wavelet based coherent structure eduction<br />
technique in turbulent wall flows.<br />
R. Camussi a, W. Da Riz a<br />
The aim of the work is to present an assessment of a wavelet based method for<br />
identifying coherent structures (CS) from 2D PIV data in turbulent wall flows.<br />
The database used is provided by Adrian and co-workers<br />
(http://ltcf.tam.uiuc.edu/) and previously used in Adrian et al. 1 for high and low<br />
Reynolds number flows (Re = 1015/7705, = 8.84/10.35 mm).<br />
The algorithm is based on wavelet analysis of 2D PIV velocity field (Camussi 2) and<br />
validated against a method based on the swirling strength (Zhou et al. 3). An algorithm<br />
for the computation of the velocity gradient tensor at each point of the 2D PIV<br />
velocity field has been implemented: the CS has been identified as to be the area<br />
where the velocity gradient tensor has a pair of conjugate complex eigenvalues with<br />
squared imaginary part ci 2 overcoming a fixed threshold equals to std(ci 2). The<br />
algorithm for CS identification via wavelet analysis is based on the LIM indicator<br />
(Farge 4, Camussi and Guj 5); here only the velocity component normal to the wall has<br />
been used. The CS has been identified as the point where the maximum value of LIM<br />
over all wavelet scales shows a relative peak. Statistics of CS identified by means of the<br />
two methods revealed no substantial differences for negative-vorticity structure, and a<br />
relationship between wavelet wavelength and vortex size has been carried out (Fig. 1a).<br />
For positive-vorticity structures the analysis of results shown striking differences<br />
arising from the fact that the LIM based algorithm tends to identify negative-vorticity<br />
vortex packets (Fig. 1-b circled), which form a zone of local positive vorticity (Fig. 1-b<br />
red) along with positive-vorticity structures. Similarities and differences between high<br />
and low Re flows are also shown.<br />
a Mechanical and Industrial Engineering Department, University “ROMA TRE”, Rome, Italy.<br />
1 Adrian, R. J.,Meinhart C. D., Tomkins C., J. Fluid Mech. 422, 1–53 (2000).<br />
2 Camussi R., Exps. Fluids, 32, 76-86 (2002).<br />
3 Zhou, J., Adrian, R.J., Balachandar S., Kendall T.M., J. Fluid Mech. 387, 353-396 (1999).<br />
4 Farge M., Annual Review of Fluid <strong>Mechanics</strong>, 24, 395-457 (1992).<br />
5 Camussi R., Guj G., J. Fluid Mech. 348, 177-199 (1997).<br />
(a)<br />
y (mm)<br />
45<br />
40<br />
35<br />
30<br />
25<br />
20<br />
15<br />
10<br />
5<br />
10 20 30 40<br />
x(mm)<br />
Fig. 1: (a) r0 vs. wavelength. (b) Mean velocity field vorticity (wavelength = 26.6 mm)<br />
(b)<br />
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