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Experimental Investigation of Convecting Vortex/Boundary-Layer Interactions

机译:对流涡旋/边界层相互作用的实验研究

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摘要

The interaction between propagating spnnwise vortices and a turbulent boundary layer was studied experimentally. The results focus on the relationship between the passage of vortex structures and the response of the boundary Inyer In terms of ensemble-averaged unsteady mean velocity, wall shear, and turbulent stresses. Both positive and negative circulation vortices were studied at different heights above the test surface. The results indicate Hint the sign of the vortex has an effect on the wall shear response as well as the height of the vortex above the surface. The negative circulation vortices were found to interact more closely with and penetrate deeper into the boundary luyer than the positive sense vortices. A phase lag between the freestream disturbance caused by the vortex and the wnll shear stress response is demonstrated. The relationship of the measured wall-shear stress to the pressure gradient and to a scaling velocity determined from the standard log-law fit for the overlap layer are discussed. The response of the boundnry-iayer turbulence is examined at key phases during the interaction.
机译:实验研究了传播的涡旋涡旋和湍流边界层之间的相互作用。结果集中在涡旋结构的通过与边界Inyer响应之间的关系上。根据整体平均非稳态平均速度,壁面剪切力和湍流应力。研究了在测试表面上方不同高度的正向和负向循环涡流。结果表明,旋涡的符号对壁的剪切响应以及表面上方旋涡的高度有影响。发现负循环旋涡比正向旋涡更紧密地与边界鲁伊尔相互作用,并且更深入地渗透到边界鲁伊尔中。涡流引起的自由流扰动与wnll剪切应力响应之间存在相位滞后。讨论了测得的壁切应力与压力梯度以及由重叠层的标准对数律拟合确定的缩放速度的关系。在相互作用过程中的关键阶段检查边界层湍流的响应。

著录项

  • 来源
    《AIAA Journal》 |1995年第8期|p. 1383-1390|共8页
  • 作者单位

    Pennsylvania Stale University, University Park, Pennsylvania 16802;

    Pennsylvania Stale University, University Park, Pennsylvania 16802;

  • 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;
  • 关键词

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