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Compact Differencing and Filtering Schemes for Large-Eddy Simulation of Compressible Transitional Boundary Layer

机译:压缩过渡边界层大涡模拟的紧凑型差异和过滤方案

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Compressible large-eddy simulation is applied to a transitional compressible boundary layer using a compact differencing scheme with spatial filtering. Simulated properties of the transitional boundary layer show reasonable agreement with experiment. The nature of the unsteady nowfleld reasonably demonstrates that the interactions between the relatively large-scale coherent structures, such as low-speed streaks, pairs of longitudinal vortices, and hairpin vortices, observed in the transitional region play an important role in determining the behavior of transition. Therefore, these key coherent structures need to be directly resolved with adequate grid resolution and appropriate numerical scheme to properly simulate the physics of transition. Once the hairpin vortices appear, transition is promoted and the coherent structures break down to finer scales. Computational results show that the under-resolution of the finer scale structures has little influence on the overall results if the key coherent structures are adequately resolved. The filtering parameter sensitively delays transition when the key coherent structures are influenced by the filtering even a little. Once the flow develops into a fully turbulent state, spatial filtering has little influence on the flowfield. The present results reasonably illustrate the guidelines regarding how to properly simulate compressible transitional boundary layers using compact spatial differencing and filtering schemes.
机译:使用具有空间滤波的紧凑型差异方案,可压缩大涡模拟应用于过渡可压缩边界层。过渡边界层的模拟特性显示了与实验合理的协议。不稳定的本质的性质合理地证明了相对大规模的相干结构之间的相互作用,例如低速条纹,在过渡区域中观察到的纵向涡旋对和发夹涡流,在确定行为方面发挥着重要作用过渡。因此,这些关键相干结构需要通过足够的网格分辨率和适当的数值方案直接解决,以适当地模拟过渡的物理学。一旦出现发夹涡流,促进过渡,并且相干结构分解为更精细的尺度。计算结果表明,如果关键相干结构充分解决,则粮食尺度结构的下层对整体结果的影响几乎没有影响。当密钥相干结构受到过滤的影响时,过滤参数敏感地延迟过渡。一旦流动发展成完全湍流状态,空间滤波对流动场几乎没有影响。本结果合理地说明了关于如何使用紧凑空间差异和过滤方案正确模拟可压缩过渡边界层的指导。

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