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Large-Eddy simulations of circular synthetic jets in quiescent surroundings and in turbulent cross-flow

机译:静态环境和湍流中圆形合成射流的大涡模拟

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摘要

Large-Eddy simulation (LES) is used to investigate the physical processes involved in the injection of a synthetic (zero-net-mass-flux) jet in quiescent surroundings and into a zero-pressure-gradient, turbulent boundary layer over a flat plate at conditions corresponding to experimental data obtained by others. The former case is studied because it constitutes a key ingredient of the latter. Specifically, it allows the computational framework to be verified, basic properties of synthetic jets to be studied, and the sensitivity of the jet structure to the details of the computational representation of the jet orifice to be investigated. In particular, the validity of representing the circular orifice, within a multi-block H-topology mesh, alternatively, by an equivalent square orifice, or by means of a solid-cell-blocking technique or via local mesh distortion, is examined. The boundary layer ahead of the jet is generated by a separate precursor simulation at a momentum-thickness Reynolds number Re_0 = 2380, providing the main simulation with a full and accurate description of the unsteady conditions at the computational inflow boundary. Time- and phase-averaged results are presented and compared against experimental data.
机译:大涡模拟(LES)用于研究在静态环境中将合成(零净质量通量)射流注入到平板上的零压力梯度湍流边界层中所涉及的物理过程在与他人获得的实验数据相对应的条件下。对前一种情况进行研究是因为它构成了后者的关键要素。特别地,它允许验证计算框架,研究合成射流的基本特性以及射流结构对要研究的射流孔的计算表示细节的敏感性。特别地,检查了在多块H形拓扑网格内或者通过等效的正方形孔口,或者通过固体单元阻塞技术或者通过局部网格变形来表示圆形孔口的有效性。射流之前的边界层是通过动量厚度雷诺数Re_0 = 2380进行的单独前驱体模拟生成的,为主要模拟提供了对计算流入边界处非稳态条件的完整而准确的描述。给出了时间和相位平均结果,并与实验数据进行了比较。

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