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Laser Doppler Anemometer Measurements of Turbulent Boundary Layer over a Riblet Surface

机译:激光多普勒风速计测量Riblet表面上的湍流边界层

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Laser Doppler anemometer measurements in a turbulent boundary layer downstream of a change from a smooth wall to a V. grooved riblet surface provide some insight into the way the near-wall turbulence structure adjusts to the new boundary condition. Depending on the riblet dimensions, this adjustment results either in drag reduction or drag increase. In the former case (s~+<≤25, where s is the distance between neighboring riblet tips and + denotes normalization by wall variables), the turbulence structure is essentially similar to that on a smooth wall. There are major structural differences in the latter case (s~+≥25). Although near-wall secondary motions occur in both cases, the motions are much weaker when the riblets act to reduce the drag.
机译:激光多普勒风速计在从光滑壁到V形沟槽的肋状表面变化的下游的湍流边界层中进行的测量,为近壁湍流结构适应新边界条件的方式提供了一些见识。根据肋条的尺寸,此调整会导致阻力减小或阻力增大。在前一种情况下(s〜+ <≤25,其中s是相邻的肋尖之间的距离,而+表示通过壁变量进行归一化),湍流结构与光滑壁上的湍流结构基本相似。在后一种情况下(s〜+≥25)存在主要的结构差异。尽管在两种情况下都发生近壁二次运动,但是当肋条起到减小阻力的作用时,运动会弱得多。

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