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首页> 外文期刊>Flow, turbulence and combustion >Simulation of a Large-Eddy-Break-up Device (LEBU) in a Moderate Reynolds Number Turbulent Boundary Layer
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Simulation of a Large-Eddy-Break-up Device (LEBU) in a Moderate Reynolds Number Turbulent Boundary Layer

机译:在适度雷诺数湍流边界层中的大涡流装置(LEBU)的仿真

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摘要

A well-resolved large eddy simulation (LES) of a large-eddy break-up (LEBU) device in a spatially evolving turbulent boundary layer is performed with, Reynolds number, based on free-stream velocity and momentum-loss thickness, of R e (theta) ae 4300. The implementation of the LEBU is via an immersed boundary method. The LEBU is positioned at a wall-normal distance of 0.8 delta (delta denoting the local boundary layer thickness at the location of the LEBU) from the wall. The LEBU acts to delay the growth of the turbulent boundary layer and produces global skin friction reduction beyond 180 delta downstream of the LEBU, with a peak local skin friction reduction of approximately 12 %. However, no net drag reduction is found when accounting for the device drag of the LEBU in accordance with the towing tank experiments by Sahlin et al. (Phys. Fluids 31, 2814, 1988). Further investigation is performed on the interactions of high and low momentum bulges with the LEBU and the corresponding output is analysed, showing a 'break-up' of these large momentum bulges downstream of the LEBU. In addition, results from the spanwise energy spectra show consistent reduction in energy at spanwise length scales for independent of streamwise and wall-normal location when compared to the corresponding turbulent boundary layer without LEBU.
机译:在空间不断发展的湍流边界层中进行良好的大型涡流(LEBU)装置的良好的大涡流模拟(LES),基于R的自由流速度和动量损耗厚度进行雷诺数进行E(θ)4300. LEBU的实施是通过浸没的边界方法。 LEBU位于壁正常距离为0.8Δ的壁正常距离(Delta)从墙壁中表示局部边界层厚度的局部边界层厚度)。 LEBU采取促使湍流边界层的生长,并在LEBU下游的180倍三角洲产生全球肌肤摩擦减少,局部皮肤摩擦力减少约12%。但是,在萨赫林等人的牵引箱实验中占LEBU的设备拖动时,没有发现净减阻。 (物理。流体31,2814,1988)。对具有LEBU的高和低动量凸起的相互作用进行进一步研究,并分析相应的输出,显示出在LEBU下游的这些大型动量凸起的“分解”。另外,与没有LEBU的相应湍流边界层相比,翼展能量光谱的结果显示在翼展长度尺度上以翼展长度尺度的能量的一致减小。

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