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Interaction of a Backward-Facing Step and Crossflow Instabilities in Boundary-Layer Transition

机译:边界层过渡中向后步的相互作用和错流不稳定性

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摘要

A swept flat plate model with an imposed pressure gradient was experimentally investigated in a low-speed flow to determine the effect of a backward-facing step on transition in a stationary crossflow-dominated flow. Detailed hotwire measurements of boundary-layer flow were performed to investigate the upstream shift in transition due to a step height of 49% of the local unperturbed boundary-layer thickness. Increasing the initial stationary crossflow amplitude caused an upstream movement of the transition front for the backward-facing step case. The step caused a local increase in the growth of the stationary crossflow instabilities, but the stationary crossflow amplitude at transition was sufficiently low (<0.04U(e)) so that stationary crossflow was not solely responsible for transition. The unsteady velocity spectra downstream of the step were rich with unsteady disturbances in the 80- to 1500-Hz range. Three distinct families of disturbances were identified based on phase speed and wave angle, namely, a highly oblique disturbance (possibly traveling-crossflow-like), a Tollmien-Schlichting-wave-like disturbance, and a shear-layer instability. The stationary crossflow disturbances caused a modulation of the unsteady disturbances, resulting in spatially concentrated peaks in unsteady disturbance amplitude. This modulation of the unsteady disturbances is believed to be the reason for the upstream movement of the transition front with increasing stationary crossflow amplitude.
机译:在低速流中对带有施加压力梯度的后掠平板模型进行了实验研究,以确定向后步骤对平稳的以横流为主的流中过渡的影响。进行了边界层流动的详细热线测量,以研究由于局部不受扰动的边界层厚度的49%的台阶高度而导致的上游过渡转变。初始静态横流幅值的增加导致面向后向阶梯情况的过渡前沿向上游运动。该台阶导致固定横流不稳定性的增长局部增加,但是过渡时的固定横流幅度足够低(<0.04U(e)),因此固定横流不仅是过渡的原因。台阶下游的非稳态速度谱充满了80-1500Hz范围内的非稳态干扰。根据相速度和波角确定了三个不同的扰动家族,即高度倾斜扰动(可能像行进横流一样),Tollmien-Schlichting波状扰动和剪切层不稳定性。平稳的横流扰动引起非稳态扰动的调制,从而在空间上集中了非稳态扰动幅度的峰值。非稳态扰动的这种调制被认为是过渡前沿随着固定横流幅度增加而向上游运动的原因。

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  • 来源
    《AIAA Journal》 |2018年第2期|497-509|共13页
  • 作者单位

    NASA, Langley Res Ctr, Flow Phys & Control Branch, MS 170, Hampton, VA 23681 USA;

    Iowa State Univ, 2271 Howe Hall,Room 1200A, Ames, IA 50011 USA|Iowa State Univ, Aerosp Engn, 2271 Howe Hall,Room 1200A, Ames, IA 50011 USA;

    NASA, Langley Res Ctr, Flow Phys & Control Branch, MS 170, Hampton, VA 23681 USA;

    NASA, Langley Res Ctr, Computat Aerosci Branch, MS 128, Hampton, VA 23681 USA;

  • 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
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