Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda 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, H., M. F., Abdul Hamid, Abdul Aziz, Jaafar, Shah Nor, Basri, F. I., Romli, F., Mustapha, A. S., Mohd Rafie, D. L. A., Abdul Majid
Format: Article
Language:English
Published: Hindawi Publishing Corporation 2013
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Online Access:http://umpir.ump.edu.my/id/eprint/6655/
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http://umpir.ump.edu.my/id/eprint/6655/
http://umpir.ump.edu.my/id/eprint/6655/1/fkp-2013-aajaafar-Computational%20Study%20on%20the%20Aerodynamic.pdf
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spelling ump-66552018-05-02T07:21:56Z http://umpir.ump.edu.my/id/eprint/6655/ Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet Djojodihardjo, H. M. F., Abdul Hamid Abdul Aziz, Jaafar Shah Nor, Basri F. I., Romli F., Mustapha A. S., Mohd Rafie D. L. A., Abdul Majid TS Manufactures 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 Coanda-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 Coanda-jet S809 airfoil can only be effective in certain range of trailing edge rounding-off radius, Coanda-jet thickness, and momentum jet size. The location of the Coanda-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 Coanda configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design. Hindawi Publishing Corporation 2013 Article PeerReviewed application/pdf en cc_by http://umpir.ump.edu.my/id/eprint/6655/1/fkp-2013-aajaafar-Computational%20Study%20on%20the%20Aerodynamic.pdf Djojodihardjo, H. and M. F., Abdul Hamid and Abdul Aziz, Jaafar and Shah Nor, Basri and F. I., Romli and F., Mustapha and A. S., Mohd Rafie and D. L. A., Abdul Majid (2013) Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet. Journal of Renewable Energy, 2013. pp. 1-17. http://dx.doi.org/10.1155/2013/839319 DOI: 10.1155/2013/839319
repository_type Digital Repository
institution_category Local University
institution Universiti Malaysia Pahang
building UMP Institutional Repository
collection Online Access
language English
topic TS Manufactures
spellingShingle TS Manufactures
Djojodihardjo, H.
M. F., Abdul Hamid
Abdul Aziz, Jaafar
Shah Nor, Basri
F. I., Romli
F., Mustapha
A. S., Mohd Rafie
D. L. A., Abdul Majid
Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
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 Coanda-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 Coanda-jet S809 airfoil can only be effective in certain range of trailing edge rounding-off radius, Coanda-jet thickness, and momentum jet size. The location of the Coanda-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 Coanda configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design.
format Article
author Djojodihardjo, H.
M. F., Abdul Hamid
Abdul Aziz, Jaafar
Shah Nor, Basri
F. I., Romli
F., Mustapha
A. S., Mohd Rafie
D. L. A., Abdul Majid
author_facet Djojodihardjo, H.
M. F., Abdul Hamid
Abdul Aziz, Jaafar
Shah Nor, Basri
F. I., Romli
F., Mustapha
A. S., Mohd Rafie
D. L. A., Abdul Majid
author_sort Djojodihardjo, H.
title Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
title_short Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
title_full Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
title_fullStr Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
title_full_unstemmed Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
title_sort computational study on the aerodynamic performance of wind turbine airfoil fitted with coanda jet
publisher Hindawi Publishing Corporation
publishDate 2013
url http://umpir.ump.edu.my/id/eprint/6655/
http://umpir.ump.edu.my/id/eprint/6655/
http://umpir.ump.edu.my/id/eprint/6655/
http://umpir.ump.edu.my/id/eprint/6655/1/fkp-2013-aajaafar-Computational%20Study%20on%20the%20Aerodynamic.pdf
first_indexed 2023-09-18T22:02:38Z
last_indexed 2023-09-18T22:02:38Z
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