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) 12 blades with Gurney flap (GF) modified by slits. A quasi-3D computational fluid dynamics solution based on 13 Reynolds-averaged Navier-Stokes model is employed to evaluate the effectiveness of slit GF blades, in 14 particular the lift-to-drag ratio. The computational domain includes three pairs of GFs and slits combination 15 along the blade span-wise direction to allow quasi-3D flow development while applying translational periodic 16 boundary condition on the two end-wall boundaries. The inlet velocity is 9 m/s for a VAWT configuration 17 with Tip Speed Ratios (TSRs) of 1.44, 2.64, and 3.3, respectively and each of these TSRs represents low, 18 medium, and high regimes of TSRs. Simulation results have shown a significant 8% drag reduction for blades 19 with slit GFs at medium range of TSRs, albeit with a 2% decrease in lift compared to blades with clean GFs. 20 This improves the lift-to-drag ratio and enhances moment production. The power generation also shows 21 increases of 1.5%, 6.5%, and 11.3% at low, medium, and high TSR regimes, respectively, for the analysed slit 22 GF blades. The drag reduction is primarily attributed to the generation of small-scale vortices by the slit, 23 dissipating large coherent flow structures more rapidly in the near wake-field.