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DIRECT NUMERICAL SIMULATION OF THE HYDRODYNAMICAL PERTURBATIONS EVOLUTION

机译:流体动力学扰动演化的直接数值模拟

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Nowadays contemporary experimental and numerical methods allow us to study a large-scale flows with high degree of accuracy. Meanwhile the dynamics of small scales against the background of the primary flow remains less studied. In turn, the small-scale perturbations of the flow may play a significant role in the whole process evolution (e.g. it may influence on the burning kinetics and contaminants formation in the combustors). The main numerical approach for hydrodynamical modeling is based on utilizing of the sub-grid models for the evolution of the flows on the unresolved scales. In this case the small-scale flows are forced to evolve according to the laws of isotropic turbulence. Thus such an approach may cause confusing results when the small-scale flows evolution differs from the one predicted by isotropic laws. The paper discusses a problem of the evolution of hydrodynamical perturbations in closed volume with non-slip walls using the results of 2D and 3D direct numerical simulations. It is shown that initially random flow field evolves into regular structure with integral length-scale comparable with the dimensions of the volume. In 3D case the randomness of the initial velocity field causes anisotropy of the generated structure along one of the directions (the direction is random). One can observe a cone vortex belted with a transverse toroidal flow. Here it is advisable to treat such a flow as an axisymmetric one described e.g. in [1]. In [2] the flows within combustor were analyzed utilizing the approach of so-called "axisymmetric turbulence". The numerical simulation of the experiment from [2] was performed using axisymmetric setup. Correlation analysis was implemented for the numerical results averaged over the set of computations and gave a good agreement with data for correlations growth during the compression stroke obtained in [2]. The formation of the stable microstructures against the background of the primary flow was according to the cascade scenario: small vortices were born out from the random perturbations and evolve into vortices with scales comparable with combustors dimensions. The results show that correlation characteristics of the velocity deviations can be reproduced by the basic transport model for viscous compressible gas without additional turbulent model. The perturbations evolve according to the axisymmetric scenario.
机译:如今当代实验和数值方法允许我们研究了大规模的高精确度的流动。同时对主流量保持的背景小尺度的动态研究较少。反过来,该流的小规模的扰动可能在整个过程中进化一个显著作用(例如其可以在燃烧器燃烧动力学和污染物形成的影响)。用于流体动力学模型的主要数值方法是基于子网格模型的利用上尚未解决的尺度流动的演变。在这种情况下,小规模的流动被迫按照各向同性的湍流的法律发展。当小规模来自一个通过各向同性法预测的流的不同进化因此这种方法可能会导致混乱的结果。本文讨论流体动力学扰动的在封闭容积使用2D和3D直接数值模拟的结果防滑壁的演变的问题。结果表明,最初随机流场演变成具有整体长度尺度与该卷的尺寸可比常规结构。在3D情况下的初始速度场的随机性引起各向异性沿着一个方向(方向是随机的)所产生的结构的。一个可以观察锥涡束带与横向流环。这里最好是作为一个轴对称一个例如描述来治疗这样的流在[1]中。在[2]进行分析燃烧器内的流动利用所谓的“轴对称湍流”的方法。使用轴对称设置进行实验的从[2]的数值模拟。相关性分析实施了数值结果平均在组计算的和在[2]获得的压缩冲程期间给出了与数据相关性生长的良好吻合。对一次流的背景中的微结构稳定的形成根据级联情形:小旋涡分别从随机扰动和发展成鳞片与燃烧器的尺寸可比旋涡诞生出来。该结果表明,该速度偏差的相关特性可以通过基本传输模型用于粘性可压缩气体没有附加湍流模型被再现。扰动根据轴对称的情况下发展。

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