Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets
文献类型：期刊论文
| 作者 | Guo TB(郭同彪)2,3; Fang, Jian1; Zhong, Shan3; Moulinec, Charles1 |
| 刊名 | PHYSICS OF FLUIDS
 |
| 出版日期 | 2022-02-01 |
| 卷号 | 34期号:2页码:16 |
| ISSN号 | 1070-6631 |
| DOI | 10.1063/5.0080867 |
| 通讯作者 | Guo, Tongbiao(guotongbiao@imech.ac.cn) |
| 英文摘要 | Direct numerical simulations of a turbulent channel flow developing over convergent-divergent (C-D) riblets are performed at a Reynolds number of Re-b = 2800, based on the half channel height delta and the bulk velocity. To gain an in-depth understanding of the origin of the drag generated by C-D riblets, a drag decomposition method is derived from kinetic energy principle for a turbulent channel flow with wall roughness. C-D riblets with a wavelength, lambda, ranging from 0.25 delta to 1.5 delta, are examined to understand the influence of secondary flow motions on the drag. It is found that as lambda increases, the intensity of the secondary flow motion increases first and then decreases, peaking at lambda / delta = 1. At lambda / delta & GE; 1, some heterogeneity appears in the spanwise direction for the turbulent kinetic energy (TKE) and vortical structures, with the strongest enhancement occurring around regions of upwelling. All the riblet cases examined here exhibit an increased drag compared to the smooth wall case. From the energy dissipation/production point of view, such a drag increase is dominated by the TKE production and the viscous dissipation wake component. While the drag contribution from the TKE production shear component decreases as lambda increases, the drag contribution from the wake component of both the TKE production and viscous dissipation follows the same trend as the intensity of the secondary flow motion. From the work point of view, the drag increase in the riblet case at lambda / delta = 0.25 comes mainly from the work of the Reynolds shear stresses, whereas at lambda / delta & GE; 1, the drag augmentation is dominated by the work of the dispersive stresses. At lambda / delta = 0.5, both components play an important role in the increase in the drag, which also exhibits a peak. |
| WOS关键词 | DIRECT NUMERICAL-SIMULATION ; BOUNDARY-LAYER ; SKIN-FRICTION ; SEPARATION ; VORTICES |
| 资助项目 | China Scholarship Council ; University of Manchester ; Newton Fund[ST/R006733/1] ; UK Engineering and Physical Sciences Research Council (EPSRC) through the Computational Science Centre for Research Communities ; UK Turbulence Consortium[EP/R029326/1] ; PRACE |
| WOS研究方向 | Mechanics ; Physics |
| 语种 | 英语 |
| WOS记录号 | WOS:000761017900001 |
| 资助机构 | China Scholarship Council ; University of Manchester ; Newton Fund ; UK Engineering and Physical Sciences Research Council (EPSRC) through the Computational Science Centre for Research Communities ; UK Turbulence Consortium ; PRACE |
| 其他责任者 | Guo, Tongbiao |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/88638]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 作者单位 | 1.STFC Daresbury Lab, Dept Comp Sci, Warrington WA4 4AD, Cheshire, England 2.Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China; 3.Univ Manchester, Sch Engn, Manchester M13 9PL, Lancs, England; |
| 推荐引用方式 GB/T 7714 | Guo TB,Fang, Jian,Zhong, Shan,et al. Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets[J]. PHYSICS OF FLUIDS,2022,34(2):16. |
| APA | 郭同彪,Fang, Jian,Zhong, Shan,&Moulinec, Charles.(2022).Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets.PHYSICS OF FLUIDS,34(2),16. |
| MLA | 郭同彪,et al."Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets".PHYSICS OF FLUIDS 34.2(2022):16. |
入库方式： OAI收割
来源：力学研究所
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