2015
DOI: 10.1016/j.energy.2015.07.115
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Effect of number of blades on aerodynamic forces on a straight-bladed Vertical Axis Wind Turbine

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Cited by 175 publications
(48 citation statements)
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References 22 publications
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“…The principle of tip vortex is the airflow on the positive pressure surface of blade around the tip of blade to the negative pressure surface of blade. Similar conclusion of generation mechanism of vorticities including tip vortex can be found in the studies of Ferreira et al [19] in 2009 with PIV experiments and Li et al [41] in 2016 with pressure measurements. Moreover, from Figures 6c, 7c and 8c which include local enlarged views, it is clearly observed that vortex B around the rotor shaft can affect the vortex C around the blade.…”
Section: Resultssupporting
confidence: 74%
“…The principle of tip vortex is the airflow on the positive pressure surface of blade around the tip of blade to the negative pressure surface of blade. Similar conclusion of generation mechanism of vorticities including tip vortex can be found in the studies of Ferreira et al [19] in 2009 with PIV experiments and Li et al [41] in 2016 with pressure measurements. Moreover, from Figures 6c, 7c and 8c which include local enlarged views, it is clearly observed that vortex B around the rotor shaft can affect the vortex C around the blade.…”
Section: Resultssupporting
confidence: 74%
“…This experiment revealed that the tip speed ratio increased with the increase of the pressure difference on the blade surface. Based on this experiment, Li et al [19] in 2015 further investigated the influence of the number of blades on the aerodynamic characteristics of the Sb-VAWT via a torque meter. The results of this experiment showed that the peak value of the power coefficient of the Sb-VAWT decreased with the increase of the number of blades.…”
Section: Introductionmentioning
confidence: 99%
“…Further, the lift coefficient CL and the drag coefficient CD are obtained by the non-dimensional lift force FL and drag force FD per unit blade as determined by equations (1) and (2) from the dynamic pressure and chord length c. They are given by the following equations: Maeda et al, 2012) and Li (Li et al, 2015(Li et al, , 2016b(Li et al, , 2016c(Li et al, , 2016d.…”
Section: Non-dimensional Lift and Dragmentioning
confidence: 99%