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Descriptive analysis of a mode transition of the flow over an open cavity

机译:描述性分析开放腔上的流动模式转变

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Incompressible flow computations have been performed on a cavity with a length to depth ratio of 2. Depending on the Reynolds number, three qualitatively different unsteady flow regimes have been identified. In the first (regular) regime the second Rossiter mode dominates the spectrum, in the second (transitional) regime two incommensurable frequencies compete with each other via mode switching, and finally, in the third (suppressed) regime a lower frequency dominates. The various forms of appearance of these regimes in the flow field are identified and discussed. Among others, the relative importance of the upstream and downstream vortices, the spatial concentration of certain frequency components, and the amplitude of the instability waves all change radically with the change of regime. In search of the hydrodynamic causes for the qualitative changes in the flow field it has become necessary to identify vortices more precisely than usual. We critically evaluate the conditions of applicability of the Truesdell-Okubo-Weiss vortex detection criterion. We propose a new vortex identification scheme by including terms describing both the local and the convective acceleration. This scheme is more accurate than that of Hua and Klein by being truly first order. The results justify the additional effort; vortical structures are more clearly identifiable with the new criterion.
机译:已经对长度与深度之比为2的腔体执行了不可压缩的流动计算。根据雷诺数,已经确定了三个定性不同的非稳态流动形式。在第一个(常规)方案中,第二个Rossiter模式占主导地位的频谱,在第二个(过渡)方案中,两个不可估量的频率通过模式切换相互竞争,最后,在第三个(受抑制的)方案中,较低的频率占主导地位。识别并讨论了这些状态在流场中的各种形式。其中,上游涡旋和下游涡旋的相对重要性,某些频率分量的空间集中以及不稳定波的幅度都随状态的变化而发生根本性的变化。在寻找导致流场质变的流体动力学原因时,有必要比平常更精确地识别涡旋。我们严格评估Truesdell-Okubo-Weiss涡流检测标准的适用条件。我们提出了一种新的涡旋识别方案,其中包括描述局部和对流加速度的术语。通过真正地是一阶,该方案比Hua和Klein的方案更准确。结果证明了额外的努力;新标准可以更清楚地识别出涡旋结构。

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