Open Access

ARTICLE

Influence of Flap Parameters on the Aerodynamic Performance of a Wind-Turbine Airfoil

Yuanjun Dai^1,2, Jingan Cui¹, Baohua Li^1,*, Cong Wang¹, Kunju Shi¹

1 Mechanical College, Shanghai DianJi University, Shanghai, 201306, China
2 College of Energy Engineering, Xinjiang Institute of Technology, Urumqi, 830091, China

* Corresponding Author: Baohua Li. Email:

Fluid Dynamics & Materials Processing 2024, 20(4), 771-786. https://doi.org/10.32604/fdmp.2023.029584

Received 27 February 2023; Accepted 13 June 2023; Issue published 28 March 2024

Abstract

A numerical method has been used to analyze the flow field related to a NACA 0015 airfoil with and without a flap and assess the influence of the flap height and angle on the surface pressure coefficient, lift coefficient, and drag coefficient. The numerical results demonstrate that the flap can effectively improve the lift coefficient of the airfoil; however, at small attack angles, its influence is significantly reduced. When the angle of attack exceeds the critical stall angle and the flap height is 1.5% of the chord length, the influence of the flap becomes very evident. As the flap height increases, the starting point of the separation vortex gradually moves forward and generates a larger wake vortex. Optimal aerodynamic characteristics are obtained for 1.5% (of the chord length) flap height and a 45° flap angle; in this case, the separation vortex is effectively reduced.

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Keywords

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