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Numerical study of turbulence in a rotating pipe using Large<br />
Eddy Simulation<br />
J. Revstedt ∗ , C. Duwig ∗ ,L.Fuchs ∗<br />
Today, many industrial devices are making use of swirling flows. The main advantages<br />
of adding swirl to, for example, a jet is to increase turbulence and mixing.<br />
Modeling and understanding the swirling flows is then a key issue. However, despite<br />
of more than 40 years of research, the mechanisms of vortex break down are only<br />
partially understood. The main difficulty of the problem is the unsteady behavior of<br />
this type of flow 1 : Large structures resulting from vortex breakdown and the swirling<br />
shear-layers, affect directly the flow.<br />
In the present work, we consider an infinitely long rotating pipe. The rotation adds<br />
some swirl to the turbulent jet flow. Additional tangential shear is also added. It<br />
modifies the mean velocity profiles as well as the characteristic of turbulence. The<br />
present study aims to capture the large structures in a rotating pipe flow and understand<br />
how they are affected by swirl and Reynolds number.We use performed at<br />
three Reynolds numbers (Re =12000, 24000, 36000) and at three rotational speeds<br />
(S= 0.2, 0.5, 1.0). The influence of these parameters on the mean velocity and mean<br />
turbulent stress fields is investigated. In addition vortex tubes visualization will be<br />
presented and turbulent energy spectra will be analyzed. Mean velocities and stresses<br />
are compared also to the experimental data 2 . LES captures well the shear-layers and<br />
the ‘smoothing’ effect of turbulence. Strong vortex tubes are visualized using the λ2<br />
technique. Figure 1 shows the instantaneous vortex stuctures using this technique.<br />
∗Energy Sciences/Fluid <strong>Mechanics</strong>, Faculty of Engineering, Lund University, P.O. Box 118, SE-<br />
221 00 Lund, Sweden<br />
1Lucca-Negro and O’Doherty, Progress in Energy and Combustion Science 27, 431 (2001).<br />
2Facciolo, TRITA-MEK Tech. Rep. 2003:15 <strong>KTH</strong>, Stockholm (2003).<br />
Figure 1: Visualization of the vortex tubes using the λ2 technique. Re = 36000,<br />
S =1.0<br />
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