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一种微结构在脊状表面上的湍流减阻机理研究。

Investigation of the Turbulent Drag Reduction Mechanism of a Kind of Microstructure on Riblet Surface.

作者信息

Ao Mingrui, Wang Miaocao, Zhu Fulong

机构信息

School of Materials Science and Engineering, Huazhong University of Science and Technology, 1037 Luoyu Road, Wuhan 430074, China.

Institute of Microsystems, School of Mechanical Science and Engineering, Huazhong University of Science and Technology, 1037 Luoyu Road, Wuhan 430074, China.

出版信息

Micromachines (Basel). 2021 Jan 6;12(1):59. doi: 10.3390/mi12010059.

Abstract

With the k-ε renormalization group turbulence model, the drag reduction mechanism of three- dimensional spherical crown microstructure of different protruding heights distributing on the groove surface was studied in this paper. These spherical crown microstructures were divided into two categories according to the positive and negative of protruding height. The positive spherical crown micro-structures can destroy a large number of vortexes on the groove surface, which increases relative friction between water flow and the groove surface. With decreasing the vertical height of the spherical crown microstructure, the number of rupture vortexes gradually decreases. Due to the still water area causes by the blocking effect of the spherical crown microstructure, it was found that the shear stress on the groove surface can be reduced, which can form the entire drag reduction state. In another case, the spherical crown microstructures protrude in the negative direction, vortexes can be generated inside the spherical crown, it was found that these vortexes can effectively reduce the resistance in terms of pressure and friction. In a small volume, it was shown that the surface drag reduction rate of spherical crown microstructures protrudes in negative directions can be the same as high as 24.8%.

摘要

本文采用k-ε重整化群湍流模型,研究了分布在槽面上不同突出高度的三维球形冠微结构的减阻机理。这些球形冠微结构根据突出高度的正负分为两类。正球形冠微结构会破坏槽面上大量的涡旋,增加水流与槽面之间的相对摩擦力。随着球形冠微结构垂直高度的减小,破裂涡旋的数量逐渐减少。由于球形冠微结构的阻挡作用形成了静水区域,发现槽面上的剪应力可以降低,从而形成整体减阻状态。在另一种情况下,球形冠微结构向负方向突出,在球形冠内部会产生涡旋,发现这些涡旋在压力和摩擦方面都能有效降低阻力。在小体积范围内,结果表明向负方向突出的球形冠微结构的表面减阻率可高达24.8%。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/48c6/7825431/c038f79df693/micromachines-12-00059-g001.jpg

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