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

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

Keywords

Aerodynamic characteristic
Airfoil
Estimate
Full range section
Wind turbine

UN SDGs

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

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.",

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AU - Song, Wenping

AU - Hou, Yinzhu

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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

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ER -

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

Abstract

Keywords

UN SDGs

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