Numerical investigation of airfoils for small wind turbine applications

A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid321a, Mid321b, Mid321c, Mid321d, and Mid321e were carried out at Reynolds numbers ranging from 0.5×105 to 2.5×105. The airfoils used for small wind turbines are designed for Reynolds number rang...

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Main Authors: Natarajan Karthikeyan, Thomas Suthakar, Ramachadran Bhagavathi Ammal Anand
Format: Article
Language:English
Published: VINCA Institute of Nuclear Sciences 2016-01-01
Series:Thermal Science
Subjects:
Online Access:http://www.doiserbia.nb.rs/img/doi/0354-9836/2016/0354-983616091N .pdf
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spelling doaj-532a490f5683467b9440f063bde4c0e72021-01-02T01:55:41ZengVINCA Institute of Nuclear SciencesThermal Science0354-98362334-71632016-01-0120suppl. 41091109810.2298/TSCI16S4091N0354-983616091NNumerical investigation of airfoils for small wind turbine applicationsNatarajan Karthikeyan0Thomas Suthakar1Ramachadran Bhagavathi Ammal Anand2National Institute of Technology Trichy, Department of Mechanical Engineering, Tiruchirappalli, Tamil Nadu, IndiaNational Institute of Technology Trichy, Department of Mechanical Engineering, Tiruchirappalli, Tamil Nadu, IndiaNational Institute of Technology Trichy, Department of Mechanical Engineering, Tiruchirappalli, Tamil Nadu, IndiaA detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid321a, Mid321b, Mid321c, Mid321d, and Mid321e were carried out at Reynolds numbers ranging from 0.5×105 to 2.5×105. The airfoils used for small wind turbines are designed for Reynolds number ranges between 3×105 and 5×105 and the blades are tend to work on off-design conditions. The blade element moment method was applied to predict the aerodynamic loads, power coefficient, and blade parameters for the airfoils. Based on the evaluate data, it was found that Mid321c airfoil has better lift to drag ratio over the range of Reynolds numbers and attained maximum power coefficient of 0.4487 at Re = 2×105.http://www.doiserbia.nb.rs/img/doi/0354-9836/2016/0354-983616091N .pdfsmall wind turbineblade element momentlow Reynolds numberairfoils
collection DOAJ
language English
format Article
sources DOAJ
author Natarajan Karthikeyan
Thomas Suthakar
Ramachadran Bhagavathi Ammal Anand
spellingShingle Natarajan Karthikeyan
Thomas Suthakar
Ramachadran Bhagavathi Ammal Anand
Numerical investigation of airfoils for small wind turbine applications
Thermal Science
small wind turbine
blade element moment
low Reynolds number
airfoils
author_facet Natarajan Karthikeyan
Thomas Suthakar
Ramachadran Bhagavathi Ammal Anand
author_sort Natarajan Karthikeyan
title Numerical investigation of airfoils for small wind turbine applications
title_short Numerical investigation of airfoils for small wind turbine applications
title_full Numerical investigation of airfoils for small wind turbine applications
title_fullStr Numerical investigation of airfoils for small wind turbine applications
title_full_unstemmed Numerical investigation of airfoils for small wind turbine applications
title_sort numerical investigation of airfoils for small wind turbine applications
publisher VINCA Institute of Nuclear Sciences
series Thermal Science
issn 0354-9836
2334-7163
publishDate 2016-01-01
description A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid321a, Mid321b, Mid321c, Mid321d, and Mid321e were carried out at Reynolds numbers ranging from 0.5×105 to 2.5×105. The airfoils used for small wind turbines are designed for Reynolds number ranges between 3×105 and 5×105 and the blades are tend to work on off-design conditions. The blade element moment method was applied to predict the aerodynamic loads, power coefficient, and blade parameters for the airfoils. Based on the evaluate data, it was found that Mid321c airfoil has better lift to drag ratio over the range of Reynolds numbers and attained maximum power coefficient of 0.4487 at Re = 2×105.
topic small wind turbine
blade element moment
low Reynolds number
airfoils
url http://www.doiserbia.nb.rs/img/doi/0354-9836/2016/0354-983616091N .pdf
work_keys_str_mv AT natarajankarthikeyan numericalinvestigationofairfoilsforsmallwindturbineapplications
AT thomassuthakar numericalinvestigationofairfoilsforsmallwindturbineapplications
AT ramachadranbhagavathiammalanand numericalinvestigationofairfoilsforsmallwindturbineapplications
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