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An experimental study of turbulent boundary layers approaching separation

机译:湍流边界层接近分离的实验研究

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The present paper deals with the experimental analysis of a strong decelerated turbulent boundary layer developed on a flat plate. The aim of the study was to examine the effects of pressure gradient on a non-equilibrium boundary layer while indicating local areas of equilibrium flow. The effect of the Reynolds number on a turbulent boundary layer developed with matching the external pressure gradient conditions was also analysed. The emphasis was on the analysis of mean flow statistics i.e. mean velocity profiles, streamwise Reynolds stress and the effect of large- and small-scale interactions by analysing the skewness factor and energy isocontours maps. The comparative analysis of the external data indicated that the structure of the turbulent boundary layer depends not only on local effects of pressure gradient but also on the upstream history of the flow. For the same condition of pressure gradient, the increased momentum is observed near the wall with the increase of the Reynolds number at the Incipient Detachment, where increased turbulence production is also observed, leading to the failure of the outer scaling methods. Surprisingly, the effect of the Reynolds number decays at the intermittent transitory detachment where similar profiles were observed. The upper inflection point in the mean profile corresponded well with the outer maximum of the Reynolds stress and zero crossing of skewness factor. Position of this point occurs at different locations, depending on the flow history effects. The last observation demonstrates that the inflection points results from large- and small-scale interactions, which led to the increased convection velocity of small scales near the wall.
机译:本文研究了在平板上形成的强减速湍流边界层的实验分析。该研究的目的是检查压力梯度对非平衡边界层的影响,同时指出平衡流的局部区域。还分析了雷诺数对匹配外部压力梯度条件形成的湍流边界层的影响。重点是通过分析偏度因子和能量等值线图来分析平均流量统计数据,即平均速度剖面,沿流方向的雷诺应力以及大小尺度相互作用的影响。对外部数据的比较分析表明,湍流边界层的结构不仅取决于压力梯度的局部影响,还取决于流动的上游历史。对于相同的压力梯度条件,随着初始分离处雷诺数的增加,在壁附近观察到动量增加,在该处也观察到湍流产生增加,导致外部结垢方法失败。出人意料的是,雷诺数的影响在观察到相似轮廓的间歇性短暂脱离处衰减。平均轮廓中的上拐点与雷诺应力的外部最大值和偏度因子的零交叉点非常吻合。该点的位置发生在不同的位置,具体取决于流动历史记录的影响。最后的观察表明,拐点是由大尺度和小尺度的相互作用引起的,这导致壁附近小尺度的对流速度增加。

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