An experimental and numerical analysis of the dynamic variation of the angle of attack in a vertical-axis wind turbine

Abstract

Simulation methods ensuring a level of fidelity higher than that of the ubiquitous Blade Element Momentum theory are increasingly applied to VAWTs, ranging from Lifting-Line methods, to Actuator Line or Computational Fluid Dynamics (CFD). The inherent complexity of these machines, characterised by a continuous variation of the angle of attack during the cycloidal motion of the airfoils and the onset of many related unsteady phenomena, makes nonetheless a correct estimation of the actual aerodynamics extremely difficult. In particular, a better understanding of the actual angle of attack during the motion of a VAWT is pivotal to select the correct airfoil and functioning design conditions. Moving from this background, a high-fidelity unsteady CFD model of a 2-blade H-Darrieus rotor was developed and validated against unique experimental data collected using Particle Image Velocimetry (PIV). In order to reconstruct the AoA variation during one rotor revolution, three different methods-detailed in the study-were then applied to the computed CFD flow fields. The resulting AoA trends were combined with available blade forces data to assess the corresponding lift and drag coefficients over one rotor revolution and correlate them with the most evident flow macro-structures and with the onset of dynamic stall.

Numerical Simulation Approaches for Vertical-Axis Wind Turbines: Investigating Airfoil Design and Predictive Techniques

“…At the same time, VAWTs exhibit superior wind energy utilisation, lower operational wind speeds, and reduced environmental footprint (Arredondo-Galeana & Brennan, 2021). Advances in numerical simulation have significantly mitigated the structural limitations of VAWTs, optimising their impeller blade design and thus broadening their commercial applicability (Bianchini et al, 2019;Melani et al, 2020).…”

Comparative analysis of the performance of small H-Darrieus for different pitch control strategies

“…This behavior occurred mainly at low wind speeds, where the angle of attack (AoA) reached high magnitudes, and the flow failed to stick to the surfaces of the blade and created the necessary driving lift, resulting in self-starting failure and low efficiency. 5,6 It should be noted that the unsteady behavior of the boundary layer imparted the blades a vibratory state resulting in early fatigue failure. [7][8][9] VAWTs reliability and lifetime were thus strongly affected.…”