Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine

This paper aims to investigate aerodynamic performance of a wind turbine blade with twist modifications using computational fluid dynamics (CFD). The phenomenon of 3D stall-delay effect in relation to blade twist is the key feature to be investigated in order to improve efficiency of a wind turbine....

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Main Authors: Wiroj Beabpimai, Tawit Chitsomboon
Format: Article
Language:English
Published: Diponegoro University 2019-10-01
Series:International Journal of Renewable Energy Development
Subjects:
CFD
Online Access:https://ejournal.undip.ac.id/index.php/ijred/article/view/22603
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spelling doaj-610256c289564d9e9044c33e318120012021-01-02T13:20:41ZengDiponegoro UniversityInternational Journal of Renewable Energy Development2252-49402019-10-018328529210.14710/ijred.8.3.285-29215354Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind TurbineWiroj Beabpimai0Tawit Chitsomboon1School of mechanical engineering, Institute of engineering, Suranaree University of Technology, Nakhonratchasima 30000, ThailandSuranaree University of Technology, School of Mechanical Engineering, Nakhon Ratchasima, ThailandThis paper aims to investigate aerodynamic performance of a wind turbine blade with twist modifications using computational fluid dynamics (CFD). The phenomenon of 3D stall-delay effect in relation to blade twist is the key feature to be investigated in order to improve efficiency of a wind turbine. The NREL (National Renewable Energy Laboratory) Phase VI wind turbine rotor was used for validation and as the baseline rotor. The baseline blade geometry was modified by increasing/decreasing the twist angles in the inboard, mid-board and outboard regions of the blade in the form of a symmetrical curve with maximum twist angle of 3°. The steady incompressible Reynolds-averaged Navier-Stokes (RANS) equations with the k-ω Shear Stress Transport (SST) turbulence closure model were used for the calculations at wind speeds ranging from 5-20 m/s. The computational results for the baseline Phase VI rotor were validated against experimental data and a good agreement was found. The computational results for the modified blades were compared against those of the baseline blade. It was found that increase of annual energy production of up to 5.1% could be achieved by this modification technique.  ©2019. CBIORE-IJRED. All rights reservedhttps://ejournal.undip.ac.id/index.php/ijred/article/view/22603CFDWind turbine aerodynamicsBlade twistefficiency of wind turbine
collection DOAJ
language English
format Article
sources DOAJ
author Wiroj Beabpimai
Tawit Chitsomboon
spellingShingle Wiroj Beabpimai
Tawit Chitsomboon
Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
International Journal of Renewable Energy Development
CFD
Wind turbine aerodynamics
Blade twist
efficiency of wind turbine
author_facet Wiroj Beabpimai
Tawit Chitsomboon
author_sort Wiroj Beabpimai
title Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
title_short Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
title_full Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
title_fullStr Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
title_full_unstemmed Numerical Study of Effect of Blade Twist Modifications on the Aerodynamic Performance of Wind Turbine
title_sort numerical study of effect of blade twist modifications on the aerodynamic performance of wind turbine
publisher Diponegoro University
series International Journal of Renewable Energy Development
issn 2252-4940
publishDate 2019-10-01
description This paper aims to investigate aerodynamic performance of a wind turbine blade with twist modifications using computational fluid dynamics (CFD). The phenomenon of 3D stall-delay effect in relation to blade twist is the key feature to be investigated in order to improve efficiency of a wind turbine. The NREL (National Renewable Energy Laboratory) Phase VI wind turbine rotor was used for validation and as the baseline rotor. The baseline blade geometry was modified by increasing/decreasing the twist angles in the inboard, mid-board and outboard regions of the blade in the form of a symmetrical curve with maximum twist angle of 3°. The steady incompressible Reynolds-averaged Navier-Stokes (RANS) equations with the k-ω Shear Stress Transport (SST) turbulence closure model were used for the calculations at wind speeds ranging from 5-20 m/s. The computational results for the baseline Phase VI rotor were validated against experimental data and a good agreement was found. The computational results for the modified blades were compared against those of the baseline blade. It was found that increase of annual energy production of up to 5.1% could be achieved by this modification technique.  ©2019. CBIORE-IJRED. All rights reserved
topic CFD
Wind turbine aerodynamics
Blade twist
efficiency of wind turbine
url https://ejournal.undip.ac.id/index.php/ijred/article/view/22603
work_keys_str_mv AT wirojbeabpimai numericalstudyofeffectofbladetwistmodificationsontheaerodynamicperformanceofwindturbine
AT tawitchitsomboon numericalstudyofeffectofbladetwistmodificationsontheaerodynamicperformanceofwindturbine
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