Prediction of the aerodynamic characteristic of wind turbine airfoils through ±180° angle of attack

Wangliu Guo; Wenping Song; Yinzhu Hou

Prediction of the aerodynamic characteristic of wind turbine airfoils through ±180° angle of attack

Wangliu Guo
, Wenping Song
, Yinzhu Hou

School of Aeronautics

Northwestern Polytechnical University Xian
The First Aircraft Institute of AVIC-1

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

1 Scopus citations

Abstract

A estimation model was built to predict the aerodynamic characteristics of airfoils through ±180° angle of attack. The lift coefficients, drag coefficients, moment coefficients of full range section were estimated for NACA0012 airfoil, NACA0015 airfoil and DU96-W-180 airfoil. Comparisons between the model predictions and experiment data showed that the estimation model is reasonable.

Original language	English
Pages (from-to)	717-722
Number of pages	6
Journal	Taiyangneng Xuebao/Acta Energiae Solaris Sinica
Volume	33
Issue number	5
State	Published - May 2012

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

Aerodynamic characteristic
Airfoil
Estimate
Full range section
Wind turbine

Cite this

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title = "Prediction of the aerodynamic characteristic of wind turbine airfoils through ±180° angle of attack",

abstract = "A estimation model was built to predict the aerodynamic characteristics of airfoils through ±180° angle of attack. The lift coefficients, drag coefficients, moment coefficients of full range section were estimated for NACA0012 airfoil, NACA0015 airfoil and DU96-W-180 airfoil. Comparisons between the model predictions and experiment data showed that the estimation model is reasonable.",

keywords = "Aerodynamic characteristic, Airfoil, Estimate, Full range section, Wind turbine",

author = "Wangliu Guo and Wenping Song and Yinzhu Hou",

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AU - Guo, Wangliu

AU - Song, Wenping

AU - Hou, Yinzhu

PY - 2012/5

Y1 - 2012/5

N2 - A estimation model was built to predict the aerodynamic characteristics of airfoils through ±180° angle of attack. The lift coefficients, drag coefficients, moment coefficients of full range section were estimated for NACA0012 airfoil, NACA0015 airfoil and DU96-W-180 airfoil. Comparisons between the model predictions and experiment data showed that the estimation model is reasonable.

AB - A estimation model was built to predict the aerodynamic characteristics of airfoils through ±180° angle of attack. The lift coefficients, drag coefficients, moment coefficients of full range section were estimated for NACA0012 airfoil, NACA0015 airfoil and DU96-W-180 airfoil. Comparisons between the model predictions and experiment data showed that the estimation model is reasonable.

KW - Aerodynamic characteristic

KW - Airfoil

KW - Estimate

KW - Full range section

KW - Wind turbine

UR - https://www.scopus.com/pages/publications/84863586141

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AN - SCOPUS:84863586141

SN - 0254-0096

VL - 33

SP - 717

EP - 722

JO - Taiyangneng Xuebao/Acta Energiae Solaris Sinica

JF - Taiyangneng Xuebao/Acta Energiae Solaris Sinica

IS - 5

ER -

Prediction of the aerodynamic characteristic of wind turbine airfoils through ±180° angle of attack

Abstract

UN SDGs

Keywords

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