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A Turbulent Boundary Layer Flow Over an Open Shallow Cavity

机译:开口浅腔上的湍流边界层流

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Particle Image Velocimetry (PIV) was used to study the flow structure and turbulence, upstream, over, and downstream a shallow open cavity. Three sets of PIV measurements, corresponding to a turbulent incoming boundary layer and a cavity length-to-depth ratio of four, are reported. The cavity depth based Reynolds numbers were 21,000; 42,000; and 54,000. The selected flow configuration and well characterized inflow conditions allow for straightforward assessment of turbulence models and numerical schemes. All mean flow field measurements display a large flow recirculation region, spanning most of the cavity and a smaller, counter-rotating, secondary vortex, immediately downstream of the cavity leading edge. The Galilean decomposed instantaneous velocity vector fields, clearly demonstrate two distinct modes of interaction between the free shear and the cavity trailing edge. The first corresponds to a cascade of vortical structures emanating from the tip of the leading edge of the cavity that grow in size as they travel downstream and directly interact with the trailing edge, i.e., impinging vortices. The second represents vortices that travel above the trailing edge of the cavity, i.e., non-impinging vortices. In the case of impinging vortices, a strong, large scale region of recirculation forms inside the cavity and carries the flow disturbances, arising from the impingement of vortices on the trailing edge of the cavity, upstream in a manner that interacts with and influences the flow as it separates from the cavity leading edge.
机译:粒子图像测速(PIV)用于研究浅开腔上游,上游和下游的流动结构和湍流。报告了三组PIV测量值,分别对应于湍流进入边界层和腔长深比为四的情况。基于腔深度的雷诺数为21,000; 42,000;和54,000。选定的流量配置和特征明确的流入条件允许直接评估湍流模型和数值方案。所有的平均流场测量结果都显示出大的流动再循环区域,跨越了大部分腔体,并在腔体前缘的下游立即形成了一个较小的,反向旋转的次级涡流。伽利略分解的瞬时速度矢量场清楚地显示了自由剪切力与型腔后缘之间相互作用的两种不同模式。第一个对应于从腔体前缘尖端发出的一系列涡旋结构,当它们向下游移动并与后缘直接相互作用(即撞击涡流)时,其尺寸逐渐增大。第二个代表在空腔后缘上方传播的旋涡,即非撞击旋涡。在撞击涡流的情况下,在腔体内形成一个强大的大规模再循环区域,并在上游以与流体相互作用并影响流量的方式携带涡流撞击腔体后缘而引起的流动扰动。因为它与型腔前缘分开。

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