不同涡脱落模式下垂直轴风力机叶片的气动响应

郑小波; 王红亮; 徐文浩; 郜志腾; 冷峻; 李晔

doi:10.7638/kqdlxxb-2022.0040

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

不同涡脱落模式下垂直轴风力机叶片的气动响应

研究论文 | 更新时间：2026-05-28

- 不同涡脱落模式下垂直轴风力机叶片的气动响应
- Aerodynamic responses of vertical-axis wind turbine foil to different vortex shedding patterns
- 空气动力学学报 2023年41卷第6期页码：26-34
- 作者机构：
  
  1. 兰州理工大学能源与动力工程学院,兰州,730050
  2. 上海交通大学船舶海洋与建筑工程学院,上海,200240
  3. 上海交通大学多功能拖曳水池实验室,上海,200240
- 作者简介：
  
  郑小波（1991-），男，山西五台人，博士后，助理研究员，研究方向：流体力学、新能源. E-mail：xzwtzxb@lut.edu.cn
  李晔*，教授，研究方向：流体力学，海洋工程，新能源. E-mail：ye.li@sjtu.edu.cn
- 基金信息：
  
  国家重点研究发展计划（2017YFE0132000）;国家自然科学基金面上项目（11872248）;甘肃省科技计划青年项目（22JR5RA304）;水下测控技术重点实验室基金（61424070603）
- DOI：10.7638/kqdlxxb-2022.0040
  中图分类号： TK14;O355;TK81;TK83
- 纸质出版：2023
- 稿件说明：
移动端阅览
郑小波, 王红亮, 徐文浩, 等. 不同涡脱落模式下垂直轴风力机叶片的气动响应[J]. 空气动力学学报, 2023, 41(6): 26−34.

ZHENG Xiaobo, WANG Hongliang, XU Wenhao, et al. Aerodynamic responses of vertical-axis wind turbine foil to different vortex shedding patterns[J]. 2023, 41(6): 26-34.
郑小波, 王红亮, 徐文浩, 等. 不同涡脱落模式下垂直轴风力机叶片的气动响应[J]. 空气动力学学报, 2023, 41(6): 26−34. DOI： 10.7638/kqdlxxb-2022.0040

ZHENG Xiaobo, WANG Hongliang, XU Wenhao, et al. Aerodynamic responses of vertical-axis wind turbine foil to different vortex shedding patterns[J]. 2023, 41(6): 26-34. DOI： 10.7638/kqdlxxb-2022.0040.

摘要

为研究尾流中不同涡脱落模式下垂直轴风力机（vertical-axis wind turbine

VAWT）叶片的气动响应，基于攻角变化相似性，进行了叶片正弦俯仰振动的比拟实验。研究发现：在弦长雷诺数

$(10^5)$

img text_id='M1' class='formula-img' style='display:none;' src='2022-040_M1.jpg'>

范围内，尾流存在3种涡型结构：前缘离散涡（leading-edge vortex

LEV）、蜿蜒尾流（undulating wake

UW）和反卡门涡街（reverse von Kármán vortex street

RvKVS）；随着叶尖速比

$ \lambda $

img text_id='M2' class='formula-img' style='display:none;' src='2022-040_M2.jpg'>

增大，VAWT叶片缩减频率

$ k $

img text_id='M3' class='formula-img' style='display:none;' src='2022-040_M3.jpg'>

增大，攻角幅值

$ {\alpha }_{\mathrm{m}} $

img text_id='M4' class='formula-img' style='display:none;' src='2022-040_M4.jpg'>

减小；叶轮叶片几何尺度比

较小时，在低

$ \lambda $

img text_id='M2' class='formula-img' style='display:none;' src='2022-040_M2.jpg'>

产生LEV涡型的可能性较小，在高

$ \lambda $

img text_id='M2' class='formula-img' style='display:none;' src='2022-040_M2.jpg'>

产生RvKVS涡型的可能性较大；

较大时，在低

$ \lambda $

img text_id='M2' class='formula-img' style='display:none;' src='2022-040_M2.jpg'>

产生LEV涡型的可能性较大，在高

$ \lambda $

img text_id='M2' class='formula-img' style='display:none;' src='2022-040_M2.jpg'>

产生RvKVS涡型的可能性较小。LEV涡型导致轻动态失速，造成VAWT叶片发生高频俯仰振动，但对叶轮转矩和VAWT功率影响不大。RvKVS涡型的出现，伴随叶片升力和转矩幅值增大以及平均推力的产生，会使VAWT叶片扭矩载荷增大，也会使叶轮转矩和输出功率提升。据此提出基于VAWT的新式风墙构型，在继承Nes浮式风墙构型优点的基础上，进一步提升了功率系数和风能输出密度。

Abstract

In order to study the aerodynamic response of the vertical axis wind turbine (VAWT) foil to different wake vortex shedding patterns

an analog experiment of the sinusoidally pitching foil was carried out based on the similarity of the variation of angle of attack. In the chord-based Reynolds number range of ~

$(10^5)$

img text_id='M9901' class='formula-img' style='display:none;' src='2022-040_M9901.jpg'>

three vortex patterns are identified in the wake: leading-edge vortex (LEV) pattern

undulating wake (UW) pattern

and reverse von Kármán vortex street (RvKVS) pattern. For VAWT

the reduced frequency

$ k $

img text_id='M12' class='formula-img' style='display:none;' src='2022-040_M12.jpg'>

increases while the amplitude of angle of attack

$ {\alpha }_{\mathrm{m}} $

img text_id='M13' class='formula-img' style='display:none;' src='2022-040_M13.jpg'>

decreases as the tip-speed ratio

$ \lambda $

img text_id='M14' class='formula-img' style='display:none;' src='2022-040_M14.jpg'>

increases. With a small ratio of the rotor radius over the foil chord

the LEV pattern is less likely to appear at low

$ \lambda $

img text_id='M14' class='formula-img' style='display:none;' src='2022-040_M14.jpg'>

while the RvKVS pattern is more likely to appear at high

$ \lambda $

img text_id='M14' class='formula-img' style='display:none;' src='2022-040_M14.jpg'>

. With large

the LEV pattern is more likely to appear at low

$ \lambda $

img text_id='M14' class='formula-img' style='display:none;' src='2022-040_M14.jpg'>

while the RvKVS pattern is less likely to appear at high

$ \lambda $

img text_id='M14' class='formula-img' style='display:none;' src='2022-040_M14.jpg'>

. The light dynamic stall caused by the LEV pattern makes VAWT foil pitch at a high frequency

but the rotor moment and the VAWT power are not affected significantly. The appearance of the RvKVS pattern causes the increase of amplitudes of lift and moment coefficients as well as the production of mean thrust on the foil

which increases the torque load on the foil

the r

otor moment

and the output power. Based on the results and discussions of the analogue experiment

a new configuration of the wind-catching wall with two-straight-foil small-scale VAWT units is proposed

which further improves the power coefficient for a given area of land

compared to the Nes configuration of the floating wind-catching wall with horizontal-axis wind turbine units.

关键词

Keywords

references

Global Wind Energy Council. GWEC global wind report 2021[R ] . Brussels: Global Wind Energy Council, 2021. https://gwec.net/global-wind-report-2021/

Global Wind Energy Council. GWEC global offshore wind report 2021[R ] . Brussels: Global Wind Energy Council, 2021. https://gwec.net/global-offshore-wind-report-2021/

Global Energy Interconnection Development and Cooperation Organization. Research on China’s 14th five-year plan for electric power development[R ] . Beijing: Global Energy Interconnection Development and Cooperation Organization, 2020. (in Chinese) https://upload.geidco.org.cn/2020/0801/1596270079592.pdf

LI Y. Status of large scale wind turbine technology development abroad[J]. Applied Mathematics and Mechanics, 2013, 34(10): 1003-1011. (in Chinese)[知网中文][知网英文]DOI: 10.3879 /j.issn.1000-0887.2013.10.001.

BORG M, SHIRES A, COLLU M. Offshore floating vertical axis wind turbines, dynamics modelling state of the art. part I: Aerodynamics[J]. Renewable and Sustainable Energy Reviews, 2014, 39: 1214-1225. DOI:10.1016/j.rser.2014.07.096[LinkOut]

TJIU W, MARNOTO T, MAT S, et al. Darrieus vertical axis wind turbine for power generation II: challenges in HAWT and the opportunity of multi-megawatt Darrieus VAWT development[J]. Renewable Energy, 2015, 75: 560-571. DOI:10.1016/j.renene.2014.10.039[LinkOut]

ZHAO Z Z, WANG D D, WANG T G, et al. A review: approaches for aerodynamic performance improvement of lift-type vertical axis wind turbine[J]. Sustainable Energy Technologies and Assessments, 2022, 49: 101789. DOI:10.1016/j.seta.2021.101789[LinkOut]

SØRENSEN B. Renewable energy: physics, engineering, environmental impacts, economics and planning[M]. New York: Academic Press, 2017.

IVANELL S, SØRENSEN J N, HENNINGSON D. Numerical computations of wind turbine wakes[M]// PEINKE J, SCHAUMANN P, BARTH S, ed. Wind Energy. Heidelberg: Springer Berlin, 2007: 259-263. doi: 10.1007/978-3-540-33866-6_48

RAJAGOPALAN R G, RICKERL T L, KLIMAS P C. Aerodynamic interference of vertical axis wind turbines[J]. Journal of Propulsion and Power, 1990, 6(5): 645-653. DOI:10.2514/3.23266[LinkOut]

THOMAS R N. Coupled vortex vertical axis wind turbine: US Patent 6784566[P ] . 2004-8-31. https://www.freepatentsonline.com/6784566.pdf

WHITTLESEY R W, LISKA S, DABIRI J O. Fish schooling as a basis for vertical axis wind turbine farm design[J]. Bioinspiration Biomimetics, 2010, 5(3): 035005. DOI:10.1088/1748-3182/5/3/035005[PubMed]

HAU E. Wind Turbines: fundamentals, technologies, application, economics[M]. Heidelberg: Springer Berlin, 2013. doi: 10.1007/978-3-642-27151-9

PARASCHIVOIU I. Wind turbine design: with emphasis on Darrieus concept[M]. Montreal, Canada: Polytechnic International Press, 2002.

ZHENG X B, PRÖBSTING S, WANG H L, et al. Characteristics of vortex shedding from a sinusoidally pitching hydrofoil at high Reynolds number[J]. Physical Review Fluids, 2021, 6(8): 084702. DOI:10.1103/physrevfluids.6.084702[LinkOut]

SCHNIPPER T, ANDERSEN A, BOHR T. Vortex wakes of a flapping foil[J]. Journal of Fluid Mechanics, 2009, 633: 411-423. DOI:10.1017/s0022112009007964[LinkOut]

CORKE T C, THOMAS F O. Dynamic stall in pitching airfoils: aerodynamic damping and compressibility effects[J]. Annual Review of Fluid Mechanics, 2015, 47: 479-505. DOI:10.1146/annurev-fluid-010814-013632[LinkOut]

MCCROSKEY W J. Unsteady airfoils[J]. Annual Review of Fluid Mechanics, 1982, 14: 285-311. DOI:10.1146/annurev.fl.14.010182.001441[LinkOut]

GARRICK I E. Propulsion of a flapping and oscillating airfoil[R]. NACA, Technical Report No. 567, 1936.

FERNANDEZ-FERIA R. Erratum: Linearized propulsion theory of flapping airfoils revisited[Phys. Rev. Fluids 1 , 084502 (2016) ] [J ] . Physical Review Fluids, 2017, 2(11): 119901.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

类HyTRV升力体阻尼/交叉动导数特性分析

基于Ac-准则的最优输入设计方法

基于LBM方法的LAGOON起落架噪声预测与降噪方法研究

大展弦比飞行器突风响应数值计算

水滴撞击运动超疏水表面特性及其调控