“…The relative velocity U rel is defined from the velocity triangle, as sketched in Figure 3, that is a function of the axial velocity Ux, the rotational velocity U θ , the angular rotational speed Ω in radians per second and the radial coordinate r. ϕ is the angle between U rel and the rotor plane that, together with the local pitch angle γ (sum of the blade pitch angle and local twist), defines the local angle of attack α. To account for a finite number of the blades, the tip correction of Shen et al [21,22] used, in which λ is the tip speed ratio, R is the blade radius and ci are empirical constants. Shen et al determined the constants ci from a calibration with two small experimental wind turbine rotors that have a relatively blunt tip, leading to c2 = 21.…”