Drag reduction of lift-type vertical axis wind turbine with slit modified gurney flap

Syawitri, Taurista P.; Yao, Yufeng; Yao, Jun; Chandra, Budi

Abstract

This study examines aerodynamic performance enhancement of Vertical Axis Wind Turbine (VAWT) blades with Gurney flap (GF) modified by slits. A quasi-3D computational fluid dynamics solution based on Reynolds-averaged Navier-Stokes model is employed to evaluate the effectiveness of slit GF blades, in particular the lift-to-drag ratio. The computational domain includes three pairs of GFs and slits combination along the blade span-wise direction to allow quasi-3D flow development while applying translational periodic boundary condition on the two end-wall boundaries. The inlet velocity is 9 m/s for a VAWT configuration with Tip Speed Ratios (TSRs) of 1.44, 2.64, and 3.3, respectively and each of these TSRs represents low, medium, and high regimes of TSRs. Simulation results have shown a significant 8% drag reduction for blades with slit GFs at medium range of TSRs, albeit with a 2% decrease in lift compared to blades with clean GFs. This improves the lift-to-drag ratio and enhances moment production. The power generation also shows increases of 1.5%, 6.5%, and 11.3% at low, medium, and high TSR regimes, respectively, for the analysed slit GF blades. The drag reduction is primarily attributed to the generation of small-scale vortices by the slit, dissipating large coherent flow structures more rapidly in the near wake-field.

• Journal Article Type: Article
• Acceptance Date: Aug 2, 2024
• Online Publication Date: Aug 9, 2024
• Publication Date: Oct 1, 2024
• Deposit Date: Aug 28, 2024
• Publicly Available Date: Aug 10, 2025
• Journal: Journal of Wind Engineering and Industrial Aerodynamics
• Print ISSN: 0167-6105
• Publisher: Elsevier
• Peer Reviewed: Peer Reviewed
• Volume: 253
• Article Number: 105853
• DOI: https://doi.org/10.1016/j.jweia.2024.105853
• Public URL: https://uwe-repository.worktribe.com/output/12791997