Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool

Startup capacity is always a concern to low wind speed turbines, especially the vertical axis wind turbine (VAWT). Efforts at developing low wind speed models still persist. Hence, the focus of this study is on the development of a new airfoil for VAWT, with better startup capacity, low tip loss, an...

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Autores principales: Muyiwa F. Francis, Oluseyi O. Ajayi, Joseph O. Ojo
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Lenguaje:EN
Publicado: Elsevier 2021
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spelling oai:doaj.org-article:3dbf57ae2b2a44199fc343223dcd17a72021-11-16T04:11:22ZDevelopment of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool2666-052010.1016/j.jfueco.2021.100028https://doaj.org/article/3dbf57ae2b2a44199fc343223dcd17a72021-12-01T00:00:00Zhttp://www.sciencedirect.com/science/article/pii/S2666052021000212https://doaj.org/toc/2666-0520Startup capacity is always a concern to low wind speed turbines, especially the vertical axis wind turbine (VAWT). Efforts at developing low wind speed models still persist. Hence, the focus of this study is on the development of a new airfoil for VAWT, with better startup capacity, low tip loss, and devoid of dynamic stall, from the synergistic properties of four standard airfoils. The standard airfoils are DU06-W-200-dt, NACA0012h-sa, S822, and S823. The coordinates of these airfoils were employed to generate eleven new airfoils via the interpolation of the coordinate points. The airfoils were then analysed using QBlade v0.963 64bit, to determine the coefficients of lift (CL), drag (CD), pitching moment, and minimum pressure for various angles of attack, at a specific flow characteristics such as Reynold's number, density, kinematic viscosity, and Mach number. The Reynold's and Mach numbers were modified over a range of values to generate polar of airfoil performance for every wind speed. Variations of glide ratio, CL, and CD with angle of attack at constant Reynolds number were employed to determine the optimum airfoil. High aspect ratio was used to minimise the effect of tip loss. The outcome showed that the developed airfoil exhibits better performance, good startup capacity, with potential to generate up to 1, 11 and 13 kW at speeds of 2, 11 and 16 m/s, respectively. Flow, and pressure analysis show that the turbine with the blade airfoil will not experience dynamic stall as a result of pressure differences, irrespective of the azimuth.Muyiwa F. FrancisOluseyi O. AjayiJoseph O. OjoElsevierarticleAerodynamic shapeAirfoil design analysisEnergy systemQbladeWake analysisWind turbineFuelTP315-360ENFuel Communications, Vol 9, Iss , Pp 100028- (2021)
institution DOAJ
collection DOAJ
language EN
topic Aerodynamic shape
Airfoil design analysis
Energy system
Qblade
Wake analysis
Wind turbine
Fuel
TP315-360
spellingShingle Aerodynamic shape
Airfoil design analysis
Energy system
Qblade
Wake analysis
Wind turbine
Fuel
TP315-360
Muyiwa F. Francis
Oluseyi O. Ajayi
Joseph O. Ojo
Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
description Startup capacity is always a concern to low wind speed turbines, especially the vertical axis wind turbine (VAWT). Efforts at developing low wind speed models still persist. Hence, the focus of this study is on the development of a new airfoil for VAWT, with better startup capacity, low tip loss, and devoid of dynamic stall, from the synergistic properties of four standard airfoils. The standard airfoils are DU06-W-200-dt, NACA0012h-sa, S822, and S823. The coordinates of these airfoils were employed to generate eleven new airfoils via the interpolation of the coordinate points. The airfoils were then analysed using QBlade v0.963 64bit, to determine the coefficients of lift (CL), drag (CD), pitching moment, and minimum pressure for various angles of attack, at a specific flow characteristics such as Reynold's number, density, kinematic viscosity, and Mach number. The Reynold's and Mach numbers were modified over a range of values to generate polar of airfoil performance for every wind speed. Variations of glide ratio, CL, and CD with angle of attack at constant Reynolds number were employed to determine the optimum airfoil. High aspect ratio was used to minimise the effect of tip loss. The outcome showed that the developed airfoil exhibits better performance, good startup capacity, with potential to generate up to 1, 11 and 13 kW at speeds of 2, 11 and 16 m/s, respectively. Flow, and pressure analysis show that the turbine with the blade airfoil will not experience dynamic stall as a result of pressure differences, irrespective of the azimuth.
format article
author Muyiwa F. Francis
Oluseyi O. Ajayi
Joseph O. Ojo
author_facet Muyiwa F. Francis
Oluseyi O. Ajayi
Joseph O. Ojo
author_sort Muyiwa F. Francis
title Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
title_short Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
title_full Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
title_fullStr Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
title_full_unstemmed Development of a novel airfoil for low wind speed vertical axis wind turbine using QBlade simulation tool
title_sort development of a novel airfoil for low wind speed vertical axis wind turbine using qblade simulation tool
publisher Elsevier
publishDate 2021
url https://doaj.org/article/3dbf57ae2b2a44199fc343223dcd17a7
work_keys_str_mv AT muyiwaffrancis developmentofanovelairfoilforlowwindspeedverticalaxiswindturbineusingqbladesimulationtool
AT oluseyioajayi developmentofanovelairfoilforlowwindspeedverticalaxiswindturbineusingqbladesimulationtool
AT josephoojo developmentofanovelairfoilforlowwindspeedverticalaxiswindturbineusingqbladesimulationtool
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