Full Text:   <3282>

Summary:  <2364>

CLC number: TK83

On-line Access: 2024-08-27

Received: 2023-10-17

Revision Accepted: 2024-05-08

Crosschecked: 2015-06-16

Cited: 2

Clicked: 6111

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Jian-wen Wang

http://orcid.org/0000-0001-7420-5322

Kun-zan Qiu

http://orcid.org/0000-0003-0978-2697

-   Go to

Article info.
Open peer comments

Journal of Zhejiang University SCIENCE A 2015 Vol.16 No.7 P.586-595

http://doi.org/10.1631/jzus.A1400332


Time resolved particle image velocimetry experimental study of the near wake characteristics of a horizontal axis wind turbine


Author(s):  Jian-wen Wang, Ren-yu Yuan, Xue-qing Dong, San-xia Zhang, Yang Song, Zhi-ying Gao, Kun Luo, Kun-zan Qiu, Ming-jiang Ni, Ke-fa Cen

Affiliation(s):  School of Energy and Power Engineering, Inner Mongolia University of Technology, Huhhot 010051, China; more

Corresponding email(s):   qiukz@zju.edu.cn

Key Words:  Time resolved particle image velocimetry (TRPIV), Wind turbine, Tip speed ratio (TSR), Near wake, Flow characteristics



Abstract: 
Wind tunnel experiments at a model scale have been carried out to investigate the flow characteristics in the near wake of a wind turbine. time resolved particle image velocimetry (TRPIV) measurements are applied to visualize the wind turbine wake flow. The instantaneous vorticity, average velocities, turbulence kinetic energy, and Reynolds stresses in the near wake have been measured when the wind turbine is operated at tip speed ratios (TSRs) in the range of 3–5. It was found that wind turbine near the wake flow field can be divided into a velocity increased region, a velocity unchanged region, and a velocity deficit region in the radial direction, and the axial average velocities at different TSRs in the wake reach inflow velocity almost at the same radial location. The rotor wake turbulent kinetic energy appears in two peaks at approximately 0.3R and 0.9R regions in the radial direction. The Reynolds shear stress is less than the Reynolds normal stresses, the axial Reynolds normal stress is larger than the Reynolds shear stress and radial Reynolds normal stress in the blade root region, while the radial Reynolds normal stress is larger than the Reynolds shear stress and axial Reynolds normal stress in the blade tip region. The experimental data may also serve as a benchmark for validation of relevant computational fluid dynamics (CFD) models.

Open peer comments: Debate/Discuss/Question/Opinion

<1>

Please provide your name, email address and a comment





Journal of Zhejiang University-SCIENCE, 38 Zheda Road, Hangzhou 310027, China
Tel: +86-571-87952783; E-mail: cjzhang@zju.edu.cn
Copyright © 2000 - 2025 Journal of Zhejiang University-SCIENCE