Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet

Various methods of flow control for enhanced aerodynamic performance have been developed and applied to enhance and control the behavior of aerodynamic components. The use of Coandă effect for the enhancement of circulation and lift has gained renewed interest, in particular with the progress of CFD...

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Main Authors: Djojodihardjo, Harijono, Abdul Hamid, Mohd Faisal, Jaafar, Abdul Aziz, Basri, Shahnor, Romli, Fairuz Izzudin, Mustapha, Faizal, Mohd Rafie, Azmin Shakrine, Abang Abdul Majid, Dayang Laila
Format: Article
Language:English
Published: Hindawi Publishing Corporation 2013
Online Access:http://psasir.upm.edu.my/id/eprint/28845/1/839319.pdf
http://psasir.upm.edu.my/id/eprint/28845/
http://www.hindawi.com/journals/jre/2013/839319/
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Institution: Universiti Putra Malaysia
Language: English
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spelling my.upm.eprints.288452019-12-17T06:35:42Z http://psasir.upm.edu.my/id/eprint/28845/ Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet Djojodihardjo, Harijono Abdul Hamid, Mohd Faisal Jaafar, Abdul Aziz Basri, Shahnor Romli, Fairuz Izzudin Mustapha, Faizal Mohd Rafie, Azmin Shakrine Abang Abdul Majid, Dayang Laila Various methods of flow control for enhanced aerodynamic performance have been developed and applied to enhance and control the behavior of aerodynamic components. The use of Coandă effect for the enhancement of circulation and lift has gained renewed interest, in particular with the progress of CFD. The present work addresses the influence, effectiveness, and configuration of Coandă-jet fitted aerodynamic surface for improving lift and , specifically for S809 airfoil, with a view on its incorporation in the wind turbine. A simple two-dimensional CFD modeling using - turbulence model is utilized to reveal the key elements that could exhibit the desired performance for a series of S809 airfoil configurations. Parametric study performed indicates that the use of Coandă-jet S809 airfoil can only be effective in certain range of trailing edge rounding-off radius, Coandă-jet thickness, and momentum jet size. The location of the Coandă-jet was found to be effective when it is placed close to the trailing edge. The results are compared with experimental data for benchmarking. Three-dimensional configurations are synthesized using certain acceptable assumptions. A trade-off study on the S809 Coandă configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design. Hindawi Publishing Corporation 2013 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/28845/1/839319.pdf Djojodihardjo, Harijono and Abdul Hamid, Mohd Faisal and Jaafar, Abdul Aziz and Basri, Shahnor and Romli, Fairuz Izzudin and Mustapha, Faizal and Mohd Rafie, Azmin Shakrine and Abang Abdul Majid, Dayang Laila (2013) Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet. Journal of Renewable Energy, 2013. art. no. 839319. pp. 1-17. ISSN 2314-4386; ESSN: 2314-4394 http://www.hindawi.com/journals/jre/2013/839319/ 10.1155/2013/839319
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
description Various methods of flow control for enhanced aerodynamic performance have been developed and applied to enhance and control the behavior of aerodynamic components. The use of Coandă effect for the enhancement of circulation and lift has gained renewed interest, in particular with the progress of CFD. The present work addresses the influence, effectiveness, and configuration of Coandă-jet fitted aerodynamic surface for improving lift and , specifically for S809 airfoil, with a view on its incorporation in the wind turbine. A simple two-dimensional CFD modeling using - turbulence model is utilized to reveal the key elements that could exhibit the desired performance for a series of S809 airfoil configurations. Parametric study performed indicates that the use of Coandă-jet S809 airfoil can only be effective in certain range of trailing edge rounding-off radius, Coandă-jet thickness, and momentum jet size. The location of the Coandă-jet was found to be effective when it is placed close to the trailing edge. The results are compared with experimental data for benchmarking. Three-dimensional configurations are synthesized using certain acceptable assumptions. A trade-off study on the S809 Coandă configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design.
format Article
author Djojodihardjo, Harijono
Abdul Hamid, Mohd Faisal
Jaafar, Abdul Aziz
Basri, Shahnor
Romli, Fairuz Izzudin
Mustapha, Faizal
Mohd Rafie, Azmin Shakrine
Abang Abdul Majid, Dayang Laila
spellingShingle Djojodihardjo, Harijono
Abdul Hamid, Mohd Faisal
Jaafar, Abdul Aziz
Basri, Shahnor
Romli, Fairuz Izzudin
Mustapha, Faizal
Mohd Rafie, Azmin Shakrine
Abang Abdul Majid, Dayang Laila
Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
author_facet Djojodihardjo, Harijono
Abdul Hamid, Mohd Faisal
Jaafar, Abdul Aziz
Basri, Shahnor
Romli, Fairuz Izzudin
Mustapha, Faizal
Mohd Rafie, Azmin Shakrine
Abang Abdul Majid, Dayang Laila
author_sort Djojodihardjo, Harijono
title Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
title_short Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
title_full Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
title_fullStr Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
title_full_unstemmed Computational study on the aerodynamic performance of wind turbine airfoil fitted with Coandă jet
title_sort computational study on the aerodynamic performance of wind turbine airfoil fitted with coandă jet
publisher Hindawi Publishing Corporation
publishDate 2013
url http://psasir.upm.edu.my/id/eprint/28845/1/839319.pdf
http://psasir.upm.edu.my/id/eprint/28845/
http://www.hindawi.com/journals/jre/2013/839319/
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