Effect of Trailing-Edge Thickening on Aerodynamic and Flow-Field Characteristics of Wind Turbine Airfoil

The trailing-edge design of a wind turbine airfoil is critical for balancing the aerodynamic performance and structural robustness of a wind turbine blade. In this paper, the S809 airfoil and its blunt trailing-edge variant, the S809-100 airfoil, are taken as the research objects. The aerodynamic and flow-field characteristics of both airfoils are analyzed by computational fluid dynamics, which is validated by U.S. National Renewable Energy Laboratory experiments and wind tunnel particle image velocimetry. The results show that the S809-100 airfoil achieves a higher lift coefficient across the entire angle of attack (α) range 0–18°, with a superior lift-to-drag ratio within 8–12°. Three distinct states of aerodynamic response are identified for both airfoils, based on time series and spectral features of lift and drag coefficients, and flow-field structures: steady convergence state, periodic fluctuation state, and irregular fluctuation state. The two airfoils differ significantly in aerodynamic response transition with respect to α: for the S809 airfoil, the aerodynamic response remains in a steady convergence state up to α=16° before shifting to a periodic fluctuation state, while for the S809-100 airfoil, it exhibits a periodic fluctuation state from α=0° and transitions to an irregular fluctuation state beyond α=14.2°. This difference stems from trailing-edge thickening, which induces flow unsteadiness in the S809-100 airfoil. This shift in the aerodynamic response from the periodic fluctuation state to the irregular fluctuation state is attributed to the transition from single-frequency large-scale vortex shedding to a multi-scale vortex interaction, confirmed via spectral and flow-field analyses. This study focuses on the correlated flow structures of wind turbine airfoils and deepens the understanding of unsteady aerodynamic responses; the combined analysis of enhanced aerodynamic performance and induced unsteady fluctuation due to trailing-edge thickening offers a valuable reference for wind turbine blade design.

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Publication Details

Journal
Journal of Marine Science and Engineering
Published
2026-03-16
DOI
https://doi.org/10.3390/jmse14060555
Primary Topic
Wind Energy Research and Development
Type
article
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article

Effect of Trailing-Edge Thickening on Aerodynamic and Flow-Field Characteristics of Wind Turbine Airfoil

Sheng Xu, Xiaobo Zheng, Peng Qin
Journal of Marine Science and Engineering
Wind Energy Research and Development
article

Effect of Trailing-Edge Thickening on Aerodynamic and Flow-Field Characteristics of Wind Turbine Airfoil

Sheng Xu, Xiaobo Zheng, Peng Qin
article en

Abstract

The trailing-edge design of a wind turbine airfoil is critical for balancing the aerodynamic performance and structural robustness of a wind turbine blade. In this paper, the S809 airfoil and its blunt trailing-edge variant, the S809-100 airfoil, are taken as the research objects. The aerodynamic and flow-field characteristics of both airfoils are analyzed by computational fluid dynamics, which is validated by U.S. National Renewable Energy Laboratory experiments and wind tunnel particle image velocimetry. The results show that the S809-100 airfoil achieves a higher lift coefficient across the entire angle of attack (α) range 0–18°, with a superior lift-to-drag ratio within 8–12°. Three distinct states of aerodynamic response are identified for both airfoils, based on time series and spectral features of lift and drag coefficients, and flow-field structures: steady convergence state, periodic fluctuation state, and irregular fluctuation state. The two airfoils differ significantly in aerodynamic response transition with respect to α: for the S809 airfoil, the aerodynamic response remains in a steady convergence state up to α=16° before shifting to a periodic fluctuation state, while for the S809-100 airfoil, it exhibits a periodic fluctuation state from α=0° and transitions to an irregular fluctuation state beyond α=14.2°. This difference stems from trailing-edge thickening, which induces flow unsteadiness in the S809-100 airfoil. This shift in the aerodynamic response from the periodic fluctuation state to the irregular fluctuation state is attributed to the transition from single-frequency large-scale vortex shedding to a multi-scale vortex interaction, confirmed via spectral and flow-field analyses. This study focuses on the correlated flow structures of wind turbine airfoils and deepens the understanding of unsteady aerodynamic responses; the combined analysis of enhanced aerodynamic performance and induced unsteady fluctuation due to trailing-edge thickening offers a valuable reference for wind turbine blade design.

Journal of Marine Science and EngineeringVol. 14(6)
Lanzhou University of Technology (CN)
Affordable and clean energy
Openalex Percentile: Top 18%
Wind Energy Research and Development
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