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Origin of Surface-Shear-Stress Pulses in Turbulent Boundary Layers

机译:湍流边界层中表面剪切应力脉冲的起源

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摘要

Information related to the large magnitude pulses of surface shear stress that are present in all turbulent boundary layers [1] is sketchy. It has been demonstrated [2] that the pulses are related to the coherent events that make up the turbulent boundary layer. Recent computer simulations [3] related to "vortical" induced transition of laminar-to-turbulent boundary layers predict the occurrence of turbulent "spots" in the outer region of the layer, which in turn produce large pulses in the underlying surface shear stress. Although the transition turbulent spots differ from the coherent structures within the turbulent boundary layer, the process that produces the high-velocity pulses near the surface is expected to be similar. Flow visualization studies [4] for laminar-turbulent transition starting from Tollmien-Schlichting wave instability demonstrate a spectrum of "sweep" pulses first associated with a A vortex and progressing to much stronger sweeps (stage 3) in the final stage of transition. The present experimental study examines the development of the time-dependent surface-shear-stress pulses and/or the near-surface velocities for transition flows with moderate, 1.2-2.7% freestream turbulence levels. A bypass laminar-to-turbulent transition occurs, which is similar to the computer simulation flows.
机译:与所有湍流边界层[1]中都存在的大的表面剪切应力脉冲有关的信息是粗略的。已经证明[2],脉冲与构成湍流边界层的相干事件有关。与层流到湍流边界层的“涡旋”诱导转变有关的最新计算机模拟[3]预测,在层的外部区域中会出现湍流的“斑点”,从而在下层表面剪切应力中产生大的脉冲。尽管过渡湍流点与湍流边界层内的相干结构不同,但预计在表面附近产生高速脉冲的过程是相似的。从Tollmien-Schlichting波不稳定性开始的层流湍流转换的流动可视化研究[4]表明,一系列“扫掠”脉冲首先与A涡旋相关,并在转换的最后阶段逐渐发展为更强的扫掠(第3阶段)。目前的实验研究检查了随时间变化的表面剪切应力脉冲和/或近表面速度的变化,这些流动具有中等的,1.2-2.7%的自由流湍流水平。发生了从层流到湍流的过渡,这与计算机模拟流程相似。

著录项

  • 来源
    《AIAA Journal》 |2008年第10期|p.2646-2649|共4页
  • 作者

    V. A. Sandborn;

  • 作者单位

    Colorado State University, Fort Collins, Colorado 80523;

  • 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 航空、航天;航空;
  • 关键词

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