Double helix vortex breakdown in a turbulent swirling annular jet flow

被引:15
作者
Vanierschot, M. [1 ]
Percin, M. [2 ,3 ]
van Oudheusden, B. W. [4 ]
机构
[1] Univ Leuven, Mech Engn Technol Cluster TC, Campus Grp T Leuven,A Vesaliusstr 13, B-3000 Leuven, Belgium
[2] Delft Univ Technol, Dept Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[3] Middle East Tech Univ, Dept Aerosp Engn, Ankara, Turkey
[4] Delft Univ Technol, Dept Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands
关键词
STABILIZED COMBUSTOR; PIPE; DYNAMICS; RECIRCULATION; SENSITIVITY; SIMULATION; MODE;
D O I
10.1103/PhysRevFluids.3.034703
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
In this paper, we report on the structure and dynamics of double helix vortex breakdown in a turbulent annular swirling jet. Double helix breakdownhas been reported previously for the laminar flow regime, but this structure has rarely been observed in turbulent flow. The flow field is investigated experimentally by means of time-resolved tomographic particle image velocimetry. Notwithstanding the axisymmetric nature of the time-averaged flow, analysis of the instantaneous three-dimensional (3D) vortical structures shows the existence of a vortex core along the central axis which breaks up into a double helix downstream. The winding sense of this double helix is opposite to the swirl direction (m = -2) and it is wrapped around a central vortex breakdown bubble. This structure is quite different from double helix breakdown found in laminar flows where the helix is formed in the wake of the bubble and not upstream. The double helix precesses around the central axis of the jet with a precessing frequency corresponding to a Strouhal number of 0.27.
引用
收藏
页数:7
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