Drag Reduction of Lift-Type Vertical Axis Wind Turbine with Slit Modified Gurney Flap

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) TSR s) of 1.44, 2.64, and 3.3, respectively and each of these TSRs s represents low, medium, and high regimes of TSR s. Simulation results have shown a significant 8% drag reduction for blades with slit GFs at medium range of TSR s, 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.