Design of advanced airfoil families for wind turbines

Zuo Wu Li; Jiang Chen; Bao Chen; Da Bin Chen

Design of advanced airfoil families for wind turbines

Zuo Wu Li^*
, Jiang Chen
, Bao Chen
, Da Bin Chen

^*Corresponding author for this work

School of Energy and Power Engineering

China Aerodynamics Research and Development Center
China Aviation Industry Corporation
China Aerodynamic Technique Institute for Astronautic Industry

Research output: Contribution to journal › Article › peer-review

12 Scopus citations

Abstract

Due to the tough condition in which the wind turbine is running, the airfoils used to design blade need to be specially designed. We should pay more attention to the aerodynamic properties as high lift, low drag and insensitive to surface roughness. Soupported under the "863" project (2007AA05Z449), two airfoil families have been designed specially for large-scale wind turbine blades through analysis, numerical simulation and wind tunnel test in BeiHang University. Experimental results show the design is successful.

Original language	English
Pages (from-to)	130-136
Number of pages	7
Journal	Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
Volume	30
Issue number	1
State	Published - Feb 2012

Keywords

Airfoil
Lift to drag ratio
Roughness
Wind tunnel experiment
Wind turbine

Cite this

@article{23f153fd15ec4e7bab463043a800139b,

title = "Design of advanced airfoil families for wind turbines",

abstract = "Due to the tough condition in which the wind turbine is running, the airfoils used to design blade need to be specially designed. We should pay more attention to the aerodynamic properties as high lift, low drag and insensitive to surface roughness. Soupported under the {"}863{"} project (2007AA05Z449), two airfoil families have been designed specially for large-scale wind turbine blades through analysis, numerical simulation and wind tunnel test in BeiHang University. Experimental results show the design is successful.",

keywords = "Airfoil, Lift to drag ratio, Roughness, Wind tunnel experiment, Wind turbine",

author = "Li, \{Zuo Wu\} and Jiang Chen and Bao Chen and Chen, \{Da Bin\}",

year = "2012",

month = feb,

language = "英语",

volume = "30",

pages = "130--136",

journal = "Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica",

issn = "0258-1825",

publisher = "Zhongguo Kongqi Dongli Yanjiu yu Fazhan Zhongxin",

number = "1",

}

TY - JOUR

T1 - Design of advanced airfoil families for wind turbines

AU - Li, Zuo Wu

AU - Chen, Jiang

AU - Chen, Bao

AU - Chen, Da Bin

PY - 2012/2

Y1 - 2012/2

N2 - Due to the tough condition in which the wind turbine is running, the airfoils used to design blade need to be specially designed. We should pay more attention to the aerodynamic properties as high lift, low drag and insensitive to surface roughness. Soupported under the "863" project (2007AA05Z449), two airfoil families have been designed specially for large-scale wind turbine blades through analysis, numerical simulation and wind tunnel test in BeiHang University. Experimental results show the design is successful.

AB - Due to the tough condition in which the wind turbine is running, the airfoils used to design blade need to be specially designed. We should pay more attention to the aerodynamic properties as high lift, low drag and insensitive to surface roughness. Soupported under the "863" project (2007AA05Z449), two airfoil families have been designed specially for large-scale wind turbine blades through analysis, numerical simulation and wind tunnel test in BeiHang University. Experimental results show the design is successful.

KW - Airfoil

KW - Lift to drag ratio

KW - Roughness

KW - Wind tunnel experiment

KW - Wind turbine

UR - https://www.scopus.com/pages/publications/84863379821

M3 - 文章

AN - SCOPUS:84863379821

SN - 0258-1825

VL - 30

SP - 130

EP - 136

JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

IS - 1

ER -

Design of advanced airfoil families for wind turbines

Abstract

Keywords

Other files and links

Fingerprint

Cite this