Direct numerical simulation of turbulent channel flow with spanwise rotation

被引:39
|
作者
Xia, Zhenhua [1 ,2 ]
Shi, Yipeng [1 ,2 ]
Chen, Shiyi [1 ,2 ,3 ,4 ]
机构
[1] Peking Univ, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China
[2] Peking Univ, Coll Engn, Dept Aeronaut & Astronaut, Beijing 100871, Peoples R China
[3] Collab Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
[4] South Univ Sci & Technol China, Dept Mech & Aerosp Engn, Shenzhen 518055, Guangdong, Peoples R China
基金
中国国家自然科学基金;
关键词
rotating turbulence; turbulence simulation; turbulent flows; LOW-REYNOLDS-NUMBER; LARGE-EDDY SIMULATION; WALL TURBULENCE; SYSTEM ROTATION; LOGARITHMIC LAW; ORDER MOMENTS; MODELS;
D O I
10.1017/jfm.2015.717
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A series of direct numerical simulations of turbulent channel flow with spanwise rotation at fixed global friction Reynolds number is performed to investigate the rotation effects on the mean velocity, streamwise velocity fluctuations, Reynolds shear stress and turbulent kinetic energy. The global friction Reynolds number is chosen to be Re-&TAU=u*(&TAU)h*/v* = 180(u(&TAU)*h* is the global friction velocity, h* is the channel half-width and v* is the kinematic viscosity), while the global-friction-velocity-based rotation number Ro(&TAU) = 2&UOMEGA*h*/u(&TAU) (&UOMEGA* is the dimensional angular velocity) varies from 0 to 130. In the previously reported 2&UOMEGA* -slope region for the mean velocity, a linear behaviour for the streamwise velocity fluctuations, a unit-slope linear profile for the Reynolds shear stress and a -2Ro(&TAU)-2Rot-slope linear profile for the production term of & have been identified for the first time. The critical rotation number, which corresponds to the laminar limit, is predicted to be equal to Re-&TAU according to the unit-slope linear profile of the Reynolds shear stress. Our results also show that a parabolic profile of the mean velocity can be identified around the 'second plateau' region of the Reynolds shear stress for Ro(&TAU) &GE 22. The parabolas at different rotation numbers have the same shape of 1/Re-&TAU, the radius of curvature at the vertex. Furthermore, the system rotation increases the volume-averaged turbulent kinetic energy at lower rotation rates, and then decreases it when Ro tau t?16Ro(&TAU)&GSIM 16.
引用
收藏
页码:42 / 56
页数:15
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