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Extended blade element momentum theory for the design of small-scale wind turbines.

Blade element momentum theory (BEMT) has been widely used in the design of the small scale wind turbine (SSWT). However, the original BEMT has weaknesses in providing the final design values of the wind turbine blade partly due to inaccurate assumptions of infinite number of blades made in deriving...

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Main Authors: Roslan, Siti Amni Husna, Rasid, Zainudin A., Ariffin, Ahmad Kamal
Format: Article
Language:English
Published: Semarak Ilmu Publishing 2023
Subjects:
T Technology (General)
TA Engineering (General). Civil engineering (General)
Online Access:http://eprints.utm.my/106015/1/SitiAmniHusnaRoslan2023_ExtendedBladeElementMomentumTheoryfortheDesign.pdf
http://eprints.utm.my/106015/
http://dx.doi.org/10.37934/aram.101.1.6275
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spelling my.utm.1060152024-05-29T06:33:02Z http://eprints.utm.my/106015/ Extended blade element momentum theory for the design of small-scale wind turbines. Roslan, Siti Amni Husna Rasid, Zainudin A. Ariffin, Ahmad Kamal T Technology (General) TA Engineering (General). Civil engineering (General) Blade element momentum theory (BEMT) has been widely used in the design of the small scale wind turbine (SSWT). However, the original BEMT has weaknesses in providing the final design values of the wind turbine blade partly due to inaccurate assumptions of infinite number of blades made in deriving the theory. As such, the theory has to be amended in certain areas to form the so called the extended BEMT. In this study, a SSWT blade is designed using the extended BEMT method considering 3 factors: tip loss, low thrust at high axial induction factor, a and high angle of attack in post-stall region where 5 a correction models applying also the tip loss correction factor have been compared to the original BEMT model. The SSWT rotor has a diameter of 3m. An airfoil, SG6043 known for its suitability for SSWTs is used in this study. Furthermore, the blade geometry prior to the conduct of the shape optimization process are calculated using polynomial obtained from experimental procedures. The effect of infinite number of blades can be seen here to change the axial induction factor, a especially at the tip of the blade and as a result increases the lift coefficient, CL and overpredicts the overall power coefficient and power of the wind turbine. With the Prandtl’s tip loss factor along with the a correction model, the corrected final values of aerodynamic performances have been determined. Semarak Ilmu Publishing 2023-01 Article PeerReviewed application/pdf en http://eprints.utm.my/106015/1/SitiAmniHusnaRoslan2023_ExtendedBladeElementMomentumTheoryfortheDesign.pdf Roslan, Siti Amni Husna and Rasid, Zainudin A. and Ariffin, Ahmad Kamal (2023) Extended blade element momentum theory for the design of small-scale wind turbines. Journal of Advanced Research in Applied Mechanics, 101 (1). pp. 62-75. ISSN 2289-7895 http://dx.doi.org/10.37934/aram.101.1.6275 DOI: 10.37934/aram.101.1.6275
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic T Technology (General)
TA Engineering (General). Civil engineering (General)
spellingShingle T Technology (General)
TA Engineering (General). Civil engineering (General)
Roslan, Siti Amni Husna
Rasid, Zainudin A.
Ariffin, Ahmad Kamal
Extended blade element momentum theory for the design of small-scale wind turbines.
description Blade element momentum theory (BEMT) has been widely used in the design of the small scale wind turbine (SSWT). However, the original BEMT has weaknesses in providing the final design values of the wind turbine blade partly due to inaccurate assumptions of infinite number of blades made in deriving the theory. As such, the theory has to be amended in certain areas to form the so called the extended BEMT. In this study, a SSWT blade is designed using the extended BEMT method considering 3 factors: tip loss, low thrust at high axial induction factor, a and high angle of attack in post-stall region where 5 a correction models applying also the tip loss correction factor have been compared to the original BEMT model. The SSWT rotor has a diameter of 3m. An airfoil, SG6043 known for its suitability for SSWTs is used in this study. Furthermore, the blade geometry prior to the conduct of the shape optimization process are calculated using polynomial obtained from experimental procedures. The effect of infinite number of blades can be seen here to change the axial induction factor, a especially at the tip of the blade and as a result increases the lift coefficient, CL and overpredicts the overall power coefficient and power of the wind turbine. With the Prandtl’s tip loss factor along with the a correction model, the corrected final values of aerodynamic performances have been determined.
format Article
author Roslan, Siti Amni Husna
Rasid, Zainudin A.
Ariffin, Ahmad Kamal
author_facet Roslan, Siti Amni Husna
Rasid, Zainudin A.
Ariffin, Ahmad Kamal
author_sort Roslan, Siti Amni Husna
title Extended blade element momentum theory for the design of small-scale wind turbines.
title_short Extended blade element momentum theory for the design of small-scale wind turbines.
title_full Extended blade element momentum theory for the design of small-scale wind turbines.
title_fullStr Extended blade element momentum theory for the design of small-scale wind turbines.
title_full_unstemmed Extended blade element momentum theory for the design of small-scale wind turbines.
title_sort extended blade element momentum theory for the design of small-scale wind turbines.
publisher Semarak Ilmu Publishing
publishDate 2023
url http://eprints.utm.my/106015/1/SitiAmniHusnaRoslan2023_ExtendedBladeElementMomentumTheoryfortheDesign.pdf
http://eprints.utm.my/106015/
http://dx.doi.org/10.37934/aram.101.1.6275
_version_ 1800714786662514688
score 13.211869

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