2018
DOI: 10.1016/j.renene.2017.09.076
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Experimental and theoretical investigation of micro wind turbine for low wind speed regions

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Cited by 66 publications
(32 citation statements)
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“…Another experimental study aimed at optimizing the blade geometry for average wind speed 5 m/s based on operational Reynolds number and utilized the blade geometry. The result of this study shows that the design achieved in the research is more cost-effective and more wind energy is harnessed using equivalent swept area [Akour et al 2018].…”
Section: Introductionmentioning
confidence: 77%
“…Another experimental study aimed at optimizing the blade geometry for average wind speed 5 m/s based on operational Reynolds number and utilized the blade geometry. The result of this study shows that the design achieved in the research is more cost-effective and more wind energy is harnessed using equivalent swept area [Akour et al 2018].…”
Section: Introductionmentioning
confidence: 77%
“…'Power3' which is tested during transit period of rainy season and winter noted as a substantially stable power output. We used wind rose [13,14] analysis for proposed study.…”
Section: Resultsmentioning
confidence: 99%
“…Under this low Re condition, improperly designed blade airfoils encounter deterioration in aerodynamic performance which adversely affects the operating efficiency of the wind turbine [18][19][20][21]. As such, airfoils designed for large-scale wind turbines are not necessarily suitable for small-scale wind turbines [19,20,22,23]. The airfoil aerodynamic parameters of interest in low wind speed airfoils are the lift-to-drag ratio (L/D), lift coefficient, stall angle, stall performance, and drag bucket performance [22,[24][25][26][27].…”
Section: Introductionmentioning
confidence: 99%
“…As such, airfoils designed for large-scale wind turbines are not necessarily suitable for small-scale wind turbines [19,20,22,23]. The airfoil aerodynamic parameters of interest in low wind speed airfoils are the lift-to-drag ratio (L/D), lift coefficient, stall angle, stall performance, and drag bucket performance [22,[24][25][26][27].…”
Section: Introductionmentioning
confidence: 99%