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.
Highlights
Introduction and objectives of the studyApplied research on Darrieus-type Vertical-Axis Wind Turbines (VAWTs) has been receiving a renewed attention for the last few years [1]
Simulation methods ensuring a level of fidelity higher than that of the ubiquitous Blade Element Momentum theory are increasingly applied to VAWTs, ranging from LiftingLine methods, to Actuator Line or Computational Fluid Dynamics (CFD)
Good agreement is apparent at both tip-speed ratios (TSRs), especially in the upwind region (0°≤θ≤180°), while in the downwind region (0°≤θ≤360°), probably due to the disturbances associated to the blade shed vorticity and the presence of the shaft, the CFD curve tends to slightly deviate from experimental points
Summary
Introduction and objectives of the studyApplied research on Darrieus-type Vertical-Axis Wind Turbines (VAWTs) has been receiving a renewed attention for the last few years [1]. Due to the lack of studies in the last thirty years of the 20th century, both the knowledge of involved physics and the state of development of existing simulation tools have fallen behind those for horizontal-axis machines. To this end, computational tools with a level of fidelity higher than that of the ubiquitous Blade Element Momentum (BEM) theory are increasingly applied to VAWTs, ranging from Lifting-Line methods, to Actuator Line ones or Computational Fluid.
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