中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Interactive Effects of Wind Tunnel Sidewalls on Flow Structures around 2D Airfoil Model

文献类型:期刊论文

作者Bai, Jingyan1,2,3,4; Zhang, Lei1,3; Yang, Ke3; Zhao, Daiqing2; Xu, Jianzhong1,3
刊名JOURNAL OF THERMAL SCIENCE
出版日期2023-01-16
页码10
关键词airfoil experiment sidewall corner vortex stall cell airfoil-wall junction
ISSN号1003-2169
DOI10.1007/s11630-023-1753-7
通讯作者Zhang, Lei(zhanglei@iet.cn)
英文摘要This paper presents the effect of wind tunnel sidewalls on the wind turbine airfoils with experimental and numerical methods. The test is carried out in a low-speed wind tunnel at Re=2.62x10(5). Pressures acting on the airfoil surface are measured by a multiport pressure device. And, the oil flow visualization technique is used to investigate the flow field characteristics of the airfoil surface. Then, a numerical simulation was conducted with the measurement results. As a result, it is clarified the flow structures on the airfoil surface depend strongly on the angles of attack and the sidewalls. At small angles of attack, the three-dimensional separation caused by the interaction between the sidewall boundary layer and the airfoil boundary layer is very small, and only appears near the junction of the airfoil model and the sidewall. This corner separation becomes large with the increase of the angle of attack. At the middle part of the testing model, the boundary layer flow evolves into three-dimensional separation, i.e., stall cell, when the separation develops to an appreciate extent. The stall phenomenon will further spread from the center line to sidewalls with the increase of the angle of attack; and then, its development will be limited by the sidewall boundary layer separation. Comparably, the simulation shows that the sidewall make the pressure coefficient C-p decrease, and proper boundary condition can maintain two-dimensional flow at large angles of attack by eliminating the influence of corner vortices.
WOS关键词BOUNDARY-LAYER ; LOCAL VARIABLES ; EDDY SIMULATION ; TURBINE
资助项目National Natural Science Foundation of China[51776204]
WOS研究方向Thermodynamics ; Engineering
语种英语
WOS记录号WOS:000913634300001
出版者SPRINGER
资助机构National Natural Science Foundation of China
源URL[http://ir.giec.ac.cn/handle/344007/38355]  
专题中国科学院广州能源研究所
通讯作者Zhang, Lei
作者单位1.Chinese Acad Sci, Key Lab CAS Wind Util, Beijing 100190, Peoples R China
2.Chinese Acad Sci, Guangzhou Inst Energy Convers, Guangzhou 510650, Peoples R China
3.Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
4.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
推荐引用方式
GB/T 7714
Bai, Jingyan,Zhang, Lei,Yang, Ke,et al. Interactive Effects of Wind Tunnel Sidewalls on Flow Structures around 2D Airfoil Model[J]. JOURNAL OF THERMAL SCIENCE,2023:10.
APA Bai, Jingyan,Zhang, Lei,Yang, Ke,Zhao, Daiqing,&Xu, Jianzhong.(2023).Interactive Effects of Wind Tunnel Sidewalls on Flow Structures around 2D Airfoil Model.JOURNAL OF THERMAL SCIENCE,10.
MLA Bai, Jingyan,et al."Interactive Effects of Wind Tunnel Sidewalls on Flow Structures around 2D Airfoil Model".JOURNAL OF THERMAL SCIENCE (2023):10.

入库方式: OAI收割

来源:广州能源研究所

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