Direct numerical simulations of turbulent flow over the converging and diverging riblets

被引:2
|
作者
Wang, Hao [1 ]
Fan, Yitong [1 ,2 ]
Yan, Zhenguo [3 ]
Li, Weipeng [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
[2] Univ Melbourne, Dept Mech Engn, Parkville, Vic 3010, Australia
[3] State Key Lab Aerodynam, Mianyang 621000, Peoples R China
基金
中国国家自然科学基金;
关键词
BOUNDARY-LAYER; DRAG REDUCTION; SKIN-FRICTION; CHANNEL; STATISTICS; SURFACES; STRESS; GROWTH; FIELD;
D O I
10.1063/5.0154866
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Different from conventional streamwise-aligned riblets, converging and diverging (C-D) riblets are arranged obliquely along the main-flow direction, intending to induce a large-scale secondary flow that modulates or controls the existing large-scale vortical structures in wall turbulence. In this study, we perform direct numerical simulations of turbulent flow over the C-D riblets at a low Reynolds number and investigate the impacts of the C-D riblets on aerodynamic forces, turbulence statistics, and coherent structures. The results show that the C-D riblets can reduce the skin-friction drag, but at the expense of a significantly increased pressure drag in the diverging region, which leads to an increase in the total drag. We present detailed mean and statistical flow-fields to assess the flow characteristics in the presence of the C-D riblets, including modifications on the distributions of velocities, pressure, Reynolds stresses, and turbulence kinetic energy. Moreover, the re-arrangement of turbulence structures over the C-D riblets is examined in terms of instantaneous flow-fields and two-point correlations. The findings provide more insight into the physics of flow over C-D riblets and may contribute to the further development of this flow control strategy.
引用
收藏
页数:18
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