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NUMERICAL SIMULATION OF COMPRESSIBLE MIXING LAYERS

机译:可压缩混合层的数值模拟

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摘要

Three-dimensional spatially developing compressible planar mixing layers are studied numerically for convective Mach number Mc = 0.4, 0.8 and 1.2. The present results for the flow-field structure, the mean velocity profiles, the mixing-layer growth rate, and Reynolds stresses agree well with those of experiments and other numerical studies. The normalized growth rate decreases with increasing Mc. Shocklets are found to exist in the mixing layer at Mc = 1.2 and their formation mechanism shows good agreement with the model of flow around a bluff body. The effect of compressibility on the large-scale structures is stronger than that on the small-scale ones. The budget of the Reynolds-stress transport equations agree well with that from the temporal developing results. The magnitudes of most of the contributing terms in the budget reduce with increased compressibility effect except the pressure-dilatation term although it is still very small.
机译:对流马赫数Mc = 0.4、0.8和1.2进行了三维空间发展的可压缩平面混合层的数值研究。目前关于流场结构,平均速度分布,混合层生长速率和雷诺应力的结果与实验和其他数值研究的结果非常吻合。归一化增长率随着Mc的增加而降低。发现在Mc = 1.2的混合层中存在冲击波,并且冲击波的形成机理与阻流体周围的流动模型吻合良好。可压缩性对大型结构的影响要强于对小规模结构的影响。雷诺应力输运方程的预算与时间发展结果吻合良好。预算中大多数贡献项的大小都随着压缩效应的增加而减小,除了压力-膨胀项,尽管它仍然很小。

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