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首页> 外文期刊>High temperature: English translation of teplofizika vysokikh temperatur >Numerical Simulation of Self-Excited Oscillation of a Turbulent Jet Flowing into a Rectangular Cavity
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Numerical Simulation of Self-Excited Oscillation of a Turbulent Jet Flowing into a Rectangular Cavity

机译:湍流射流进入矩形腔的自激振荡的数值模拟

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The example of a plane jet flow into a rectangular cavity ("dead end") is used in comparing the capabilities of different approaches to numerical simulation of self-oscillatory turbulent flows characterized by global quasi-periodic oscillation of all flow parameters. The calculations are performed for two flow modes, of which the first one is statistically steady according to the available experimental data, and the second one is self-oscillatory. In both cases, three approaches are used to describe the turbulence, namely, the method of large eddy simulation (LES) in combination with the subgrid model of Smagorinsky, and steady and unsteady Reynolds averaged Navier-Stokes equations (SRANS and URANS) with two well-known differential models of turbulence. In the case of the first flow mode, all three approaches produce qualitatively similar and quantitatively close results. In the case of the second (self-oscillatory) mode, a steady-state solution of Reynolds equations may only be obtained in half the domain using the symmetry boundary conditions; within the framework of the other two approaches, the solutions turn out to be unsteady-state. In so doing, their characteristics calculated using the LES and URANS methods differ significantly from each other; in the case of URANS, they further depend on the model of turbulence employed. The best results as regards the accuracy of prediction of the amplitude-frequency characteristics of self-oscillation are produced by the use of the LES and three-dimensional URANS methods. A similar inference may be made with respect to the mean flow parameters. From this standpoint, the worst results are those obtained from calculations involving the use of the symmetry boundary conditions on the geometric symmetry plane of the flow.
机译:以平面射流流入矩形腔(“死角”)为例,用于比较以所有流量参数的整体准周期振荡为特征的自激湍流数值模拟的不同方法的能力。针对两种流动模式进行计算,其中第一种根据可用的实验数据在统计上是稳定的,第二种是自振荡的。在这两种情况下,都使用三种方法来描述湍流,即大涡模拟(LES)与Smagorinsky子网格模型相结合的方法,以及具有两个的稳态和非稳态雷诺平均Navier-Stokes方程(SRANS和URANS)。众所周知的湍流微分模型。在第一种流动模式的情况下,所有这三种方法都在质量上相似且在数量上接近结果。在第二种(自激振荡)模式下,只能使用对称边界条件在一半域中获得雷诺方程的稳态解;在其他两种方法的框架内,解决方案证明是不稳定的。这样做时,使用LES和URANS方法计算出的它们的特性彼此之间存在显着差异。就URANS而言,它们还取决于所采用的湍流模型。通过使用LES和三维URANS方法,可以得到关于自振荡幅度-频率特性的预测准确性的最佳结果。关于平均流量参数可以做出类似的推断。从这个角度来看,最糟糕的结果是从涉及在几何对称平面上使用对称边界条件的计算得出的结果。

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