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Formation of Turbulent Vortex Breakdown: Intermittency,Criticality, and Global Instability

机译:湍流涡破裂的形成:间歇性,临界性和整体不稳定性

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摘要

This study provides quantitative insight into the formation of vortex breakdown and the onset of global instability in a turbulent swirling jet. A water jet is guided through a rotating honeycomb that imparts the rotational motion, passed through a contraction, and discharged into a large water tank. The flow states evolving at increasing swirl are mapped out via time-resolved particle image velocimetry. The experimental results scale properly with the swirl number based on the axial momentum flux when the commonly used boundary-layer approximations are omitted. The instantaneous velocity field reveals that vortex breakdown occurs intermittently at a wide range of swirl numbers before it appears in the mean flow. At this intermittent state, the evolving breakdown bubble oscillates heavily between two streamwise locations where the vortex core is subcritical. Upon further increasing the swirl, the breakdown oscillations decay and a region of reversed flow appears in the mean flowfield. The formation of this so-called axisymmetric breakdown state is accompanied by a supercritical-to-subcritical transition of the inflowing vortex core. The reversed flow region is found to grow linearly with increasing swirl until the flow undergoes a supercritical Hopf bifurcation to a global single-helical mode, and vortex breakdown adopts a spiral shape. The global mode shape is extracted from the particle image velocimetry snapshots by means of proper orthogonal decomposition and Fourier analysis. The present experiment reveals that, at gradually increasing swirl, the jet first transitions to an axisymmetric breakdown state that remains globally stable until a critical swirl number is exceeded. This sequence of flow states agrees well with the transient formation of vortex breakdown observed in laminar flows.
机译:这项研究提供了对湍流旋流中涡旋破坏的形成和整体不稳定性的开始的定量认识。水射流通过旋转的蜂窝引导,该蜂窝施加旋转运动,经过收缩,然后排入大水箱。通过时间分辨粒子图像测速仪可以绘制出旋流增加时的流动状态。当省略常用的边界层近似值时,实验结果可以根据轴向动量通量与旋流数适当地缩放。瞬时速度场表明,涡旋破坏在平均流中出现之前就在很宽的旋流数范围内间歇地发生。在这种间歇状态下,不断发展的破裂气泡在涡流亚临界的两个流向位置之间剧烈振荡。随着旋涡的进一步增加,击穿振荡减弱,在平均流场中出现逆流区域。所谓的轴对称击穿状态的形成伴随着流入的涡流核的超临界到亚临界转变。发现反向流动区域随着涡旋的增加而线性增长,直到该流动经历超临界霍普夫分支为整体单螺旋模式,并且涡旋分解呈螺旋形。通过适当的正交分解和傅立叶分析,从粒子图像测速快照中提取全局模式形状。本实验表明,在逐渐增加旋流的情况下,射流首先过渡到轴对称击穿状态,该状态始终保持整体稳定,直到超过临界旋流数为止。这种流动状态序列与在层流中观察到的涡旋破坏的瞬时形成非常吻合。

著录项

  • 来源
    《AIAA Journal》 |2012年第7期|p.1437-1452|共16页
  • 作者单位

    Technical University of Berlin, 10623 Berlin, Germany;

    Technical University of Berlin, 10623 Berlin, Germany;

    California Institute of Technology, Pasadena, California 91125;

    University of Arizona, Tucson, Arizona 85721;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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