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Large-Eddy Simulations of Longitudinal Vortices Embedded in a Turbulent Boundary Layer

机译:湍流边界层中埋置的纵向涡旋的大涡模拟

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Large-eddy simulations of pairs of artificially generated longitudinal vortices embedded in a two-dimensional turbulent boundary layer are performed to study the dynamics of the vortical structures and to provide the unsteady inflow data for use in a future turbomachinery simulation. An immersed boundary method is employed to represent the wall-mounted half-delta wings that generate the counter-rotating vortex pairs. Two vortex pair configurations, with "common flow" between the vortices toward the end wall (common flow down) and away from the end wall (common flow up), respectively, are investigated. Mean velocities and Reynolds stresses compare well with experimental data, demonstrating the accuracy of the numerical approach and, in particular, the efficacy of immersed boundary treatment of the vortex generators. The large coherent vortices are characterized by stream wise velocity defect and negative mean pressure. The boundary layer in the common flow region is thinned by the vortices in the common-flow-down case and thickened by them in the common-flow-up case.
机译:对嵌入二维湍流边界层中的人工生成的纵向涡流对进行大涡模拟,以研究涡结构的动力学并提供不稳定的入流数据,以供将来的涡轮机械仿真使用。采用浸没边界法来表示壁挂式半三角翼,该半三角翼产生反向旋转的涡流对。研究了两个涡流对结构,分别在涡流之间朝向端壁(向下流动)和远离端壁(向上流动)之间具有“公共流”。平均速度和雷诺应力与实验数据很好地比较,证明了数值方法的准确性,特别是涡流发生器的浸没边界处理的功效。大的相干涡以流向速度缺陷和平均负压力为特征。在共同流动区域中的边界层在共同流动向下的情况下被涡流变薄,而在共同流动向上的情况下被涡流变厚。

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