On the dynamics of the transition to vortex breakdown in axisymmetric inviscid swirling flows

被引:15
|
作者
Vanierschot, M. [1 ]
机构
[1] Katholieke Univ Leuven, Mech Engn Technol TC, Campus Grp T Leuven,Andreas Vesaliusstr 13, B-3000 Leuven, Belgium
关键词
Vortex breakdown; Stability analysis; Inviscid swirling flow; JETS; MODE; STABILITY; PIPE;
D O I
10.1016/j.euromechflu.2017.02.009
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper reports on novel features found in the dynamics of the transition to vortex breakdown in inviscid axisymmetric flows with swirl. These features are revealed by a transient simulation of an open ended pipe flow where the inlet swirl is suddenly increased from a swirl number just below the onset of vortex breakdown to a swirl number just above the onset of vortex breakdown. To eliminate the numerous parameters influencing breakdown, the axisymmetric Euler equations with swirl are used as a fluid flow model and solutions are obtained by means of numerical simulation. It is shown that as the step response has died out, the flow evolves to a quasi-static state where time derivatives of variables are negligible small. Stability analysis of this state shows that it can support standing waves in a small region of the flow domain. These standing waves are observed in the simulations as an imbalance in the axial momentum equation which slows down the flow near the central axis. The amplitude of this imbalance grows exponentially in time with a dimensionless growth rate of 0.83 scaled with the flowthrough time. Eventually, the axial velocity along the central axis becomes negative in a small part of the flow, leading to an axisymmetric recirculation zone, called vortex breakdown. To the authors knowledge, this study would be the first to reveal these features prior to breakdown and the results may help in understanding of the physical mechanisms leading to it as this is still a controversial issue in literature. (C) 2017 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:65 / 69
页数:5
相关论文
共 50 条
  • [1] A Numerical Simulation Algorithm of the Inviscid Dynamics of Axisymmetric Swirling Flows in a Pipe
    Granata, J.
    Xu, L.
    Rusak, Z.
    Wang, S.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2016, 138 (09):
  • [2] Simulations of axisymmetric, inviscid swirling flows in circular pipes with various geometries
    Zhang, Yuxin
    Rusak, Zvi
    Wang, Shixiao
    JOURNAL OF ENGINEERING MATHEMATICS, 2019, 119 (01) : 69 - 91
  • [3] Vortex breakdown control in confined swirling flows
    Saci, Rachid
    Kouadri, Amar
    MECANIQUE & INDUSTRIES, 2008, 9 (01): : 51 - 58
  • [4] Centre modes in inviscid swirling flows and their application to the stability of the Batchelor vortex
    Heaton, C. J.
    JOURNAL OF FLUID MECHANICS, 2007, 576 : 325 - 348
  • [5] How the Nozzle Geometry Impacts Vortex Breakdown in Compressible Swirling-Jet Flows
    Luginsland, T.
    AIAA JOURNAL, 2015, 53 (10) : 2936 - 2950
  • [6] A Wall Effects and Means of Controlling the Evolution of Swirling Flows with Vortex Breakdown
    Meziane, A.
    Hachemi, M.
    Kessal, M.
    Imoula, M.
    JOURNAL OF APPLIED FLUID MECHANICS, 2023, 16 (11) : 2277 - 2289
  • [7] Vortex breakdown in variable-density gaseous swirling jets
    Keeton, Benjamin W.
    Carpio, Jaime
    Nomura, Keiko K.
    Sanchez, Antonio L.
    Williams, Forman A.
    JOURNAL OF FLUID MECHANICS, 2022, 936
  • [8] Vortex breakdown of compressible subsonic swirling flows in a finite-length straight circular pipe
    Rusak, Zvi
    Choi, Jung J.
    Bourquard, Nicholas
    Wang, Shixiao
    JOURNAL OF FLUID MECHANICS, 2015, 781 : 3 - 27
  • [9] Transition in vortex breakdown modes in a coaxial isothermal unconfined swirling jet
    Santhosh, R.
    Miglani, Ankur
    Basua, Saptarshi
    PHYSICS OF FLUIDS, 2014, 26 (04)
  • [10] Vortex Breakdown Types and Global Modes in Swirling Combustor Flows with Axial Injection
    Terhaar, Steffen
    Reichel, Thoralf G.
    Schroedinger, Christina
    Rukes, Lothar
    Paschereit, Christian Oliver
    Oberleithner, Kilian
    JOURNAL OF PROPULSION AND POWER, 2015, 31 (01) : 219 - 229