Darrieus Vertical Axis Wind Turbine (VAWT) Performance Enhancement by Means of Gurney Flap

This study investigates the aerodynamic effect of Gurney flaps (GFs) of different heights on the performance of a Darrieus vertical axis wind turbine (VAWT). Through numerical simulations, the performance of a baseline airfoil is compared against configurations with GFs of 0.5%c, 1%c, and 1.5%c chord lengths across a range of tip-speed ratios (TSRs). Results identify the 0.5%c GF as the optimal configuration, providing consistent power enhancement across all tested conditions, unlike the taller flaps which showed inconsistent or negative effects. This optimal configuration achieved a peak power coefficient (Cp) of 0.366 at TSR = 2.0, a 3.73% improvement over the baseline, and critically, enhanced the low-speed power by 6.30% at TSR = 0.5, improving the turbine’s self-starting capability. Flow field analysis reveals a dual-benefit mechanism for this superior performance: at low TSRs, the GF delays flow separation during the upwind pass to increase lift, while at higher TSRs, it effectively manages the wake during the downwind pass to reduce drag and mitigate negative torque. The study concludes that the 0.5%c GF strikes an optimal balance between lift augmentation and drag.

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Publication Details

Journal
Machines
Published
2025-10-31
DOI
https://doi.org/10.3390/machines13111004
Primary Topic
Wind Energy Research and Development
Type
article
Field-Weighted Citation Impact
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article

Darrieus Vertical Axis Wind Turbine (VAWT) Performance Enhancement by Means of Gurney Flap

Antonio Pantano, Vincenzo Gulizzi, Qing Xiao, Hanif Ullah et al.
Machines
Wind Energy Research and Development
article

Darrieus Vertical Axis Wind Turbine (VAWT) Performance Enhancement by Means of Gurney Flap

Antonio Pantano, Vincenzo Gulizzi, Qing Xiao, Hanif Ullah, Zhongsheng Deng
article en

Abstract

This study investigates the aerodynamic effect of Gurney flaps (GFs) of different heights on the performance of a Darrieus vertical axis wind turbine (VAWT). Through numerical simulations, the performance of a baseline airfoil is compared against configurations with GFs of 0.5%c, 1%c, and 1.5%c chord lengths across a range of tip-speed ratios (TSRs). Results identify the 0.5%c GF as the optimal configuration, providing consistent power enhancement across all tested conditions, unlike the taller flaps which showed inconsistent or negative effects. This optimal configuration achieved a peak power coefficient (Cp) of 0.366 at TSR = 2.0, a 3.73% improvement over the baseline, and critically, enhanced the low-speed power by 6.30% at TSR = 0.5, improving the turbine’s self-starting capability. Flow field analysis reveals a dual-benefit mechanism for this superior performance: at low TSRs, the GF delays flow separation during the upwind pass to increase lift, while at higher TSRs, it effectively manages the wake during the downwind pass to reduce drag and mitigate negative torque. The study concludes that the 0.5%c GF strikes an optimal balance between lift augmentation and drag.

MachinesVol. 13(11)
University of Strathclyde (GB), University of Palermo (IT)
Openalex Percentile: Top 56%
Wind Energy Research and Development
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Darrieus Vertical Axis Wind Turbine (VAWT) Performance Enhancement by Means of Gurney Flap — Antonio Pantano, Vincenzo Gulizzi, et al. · Machines (2025) | TGRS Research Map | TGRS