2020
DOI: 10.1016/j.enconman.2019.112333
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High-resolution numerical investigation into the effects of winglet on the aerodynamic performance for a three-dimensional vertical axis wind turbine

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Cited by 45 publications
(14 citation statements)
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References 37 publications
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“…The length of the bars and the density of the bowl should be considered [19] . Comparative analysis reveals that under three distinct end speed ratio scenarios, VAWTs with winglets can achieve a noteworthy improvement in power coefficients of 16 to 19 percentage points while maintaining the same coverage area [13] .…”
Section: Power Coefficient and Torquementioning
confidence: 99%
See 1 more Smart Citation
“…The length of the bars and the density of the bowl should be considered [19] . Comparative analysis reveals that under three distinct end speed ratio scenarios, VAWTs with winglets can achieve a noteworthy improvement in power coefficients of 16 to 19 percentage points while maintaining the same coverage area [13] .…”
Section: Power Coefficient and Torquementioning
confidence: 99%
“…The classical drawing line theory, on the other hand, states that a drop in the vortex tip usually leads to a decrease in the beam's load, which may reverse with an increase in the style coefficient. In order to build and arrange winglets that are optimal for practical engineering applications, it is necessary to better clarify the winglet effect from a fluid mechanics perspective [13] .…”
Section: Introductionmentioning
confidence: 99%
“…They concluded that LSB moved near to leading edge of the aerofoil as the Reynolds number was enhanced from 2.5×10 4 to 7.5×10 4 and smaller laminar separation bubbles (LSB) generated at lower angle of attack. Xu et al [7] performed numerical simulations on the aerodynamic performance of vertical-axis wind turbine blade sections. They used winglets to improve the performance of the performance of the wind turbine.…”
Section: Introductionmentioning
confidence: 99%
“…A large number of studies have been conducted to increase power production while neglecting the self-starting problem [18][19][20][21][22][23][24][25]. An important inherent parameter of any VAWT is airfoil geometry.…”
Section: Introductionmentioning
confidence: 99%