首页> 外文会议>AIAA aerospace sciences meeting;AIAA SciTech forum >FLOW FEATURES OF THE NEAR WAKE OF A FLAT PLATE WITH TURBULENT SEPARATING BOUNDARY LAYERS
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FLOW FEATURES OF THE NEAR WAKE OF A FLAT PLATE WITH TURBULENT SEPARATING BOUNDARY LAYERS

机译:湍流分离边界层平板尾流的流动特征。

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The near and very near wake of a flat plate with a circular trailing edge, with vigorous vortex shedding is investigated with data from direct numerical simulations. Computations were performed for four different combinations of the Reynolds numbers based on plate thickness (D) and momentum thickness near the trailing edge (θ). Unlike the case of the cylinder, these two Reynolds numbers are independent parameters for the flat plate. The objectives of the study are twofold, to investigate the entrainment process when the separating boundary layers are turbulent and to obtain a better understanding of the instability of the detached shear layers. A visualization of the entrainment process, the effect of changing the ratio θ/D on entrainment and wake-velocity statistics, and a way of understanding entrainment in a phase-averaged sense via phase-averaged distributions of the turbulent transport rate are provided here. The discussion on shear-layer instability focuses on the role of log-layer eddies in the destabilization process, the effect of high-speed streaks in the turbulent boundary layer in the vicinity of the trailing edge on shear-layer vortex generation rates, and a relationship between shear-layer vortex generation and shedding phase that is a result of an interaction between the shedding process and the shear layer instability mechanism. A power-law relationship between the ratio of shear-layer and shedding frequencies and the Reynolds numbers mentioned above is obtained. A discussion of the relative magnitudes of the exponents is provided.
机译:用直接数值模拟的数据研究了具有圆形后缘,剧烈涡旋脱落的平板的近和近尾流。根据板厚(D)和后缘附近的动量厚度(θ),对雷诺数的四种不同组合进行了计算。与圆柱体不同,这两个雷诺数是平板的独立参数。该研究的目的是双重的,以研究分离的边界层是湍流时的夹带过程,并更好地理解分离的剪切层的不稳定性。这里提供了夹带过程的可视化,改变比率θ/ D对夹带和尾流速度统计的影响,以及通过湍流传输速率的相位平均分布在相位平均意义上理解夹带的方式。关于剪切层不稳定性的讨论主要集中在对数层涡流在失稳过程中的作用,后缘附近湍流边界层中的高速条纹对剪切层涡旋产生速率的影响,以及剪切层涡旋的产生与剪切相之间的关系,这是剪切过程与剪切层失稳机制之间相互作用的结果。得到了剪切层与脱落频率之比与上述雷诺数之间的幂律关系。提供了指数的相对大小的讨论。

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