Three-Dimensional Aerodynamic Analysis of a Darrieus Wind Turbine Blade Using Computational Fluid Dynamics and Lifting Line Theory

Author:

Balduzzi Francesco1,Marten David2,Bianchini Alessandro1,Drofelnik Jernej3,Ferrari Lorenzo4,Campobasso Michele Sergio5,Pechlivanoglou Georgios2,Nayeri Christian Navid2,Ferrara Giovanni1,Paschereit Christian Oliver2

Affiliation:

1. Department of Industrial Engineering, University of Florence, Via di Santa Marta 3, Firenze 50139, Italy e-mail:

2. Hermann-Föttinger-Institut, Technische Universität Berlin, Müller-Breslau-Straße 8, Berlin 10623, Germany e-mail:

3. School of Engineering, University of Glasgow, James Watt Building South, University Avenue, Glasgow G12 8QQ, UK e-mail:

4. Department of Energy, Systems, Territory and Construction Engineering, University of Pisa, Largo Lucio Lazzarino, Pisa 56122, Italy e-mail:

5. Department of Engineering, Lancaster University, Gillow Avenue, Lancaster LA1 4YW, UK e-mail:

Abstract

Due to the rapid progress in high-performance computing and the availability of increasingly large computational resources, Navier–Stokes (NS) computational fluid dynamics (CFD) now offers a cost-effective, versatile, and accurate means to improve the understanding of the unsteady aerodynamics of Darrieus wind turbines and deliver more efficient designs. In particular, the possibility of determining a fully resolved flow field past the blades by means of CFD offers the opportunity to both further understand the physics underlying the turbine fluid dynamics and to use this knowledge to validate lower-order models, which can have a wider diffusion in the wind energy sector, particularly for industrial use, in the light of their lower computational burden. In this context, highly spatially and temporally refined time-dependent three-dimensional (3D) NS simulations were carried out using more than 16,000 processor cores per simulation on an IBM BG/Q cluster in order to investigate thoroughly the 3D unsteady aerodynamics of a single blade in Darrieus-like motion. Particular attention was paid to tip losses, dynamic stall, and blade/wake interaction. CFD results are compared with those obtained with an open-source code based on the lifting line free vortex wake model (LLFVW). At present, this approach is the most refined method among the “lower-fidelity” models, and as the wake is explicitly resolved in contrast to blade element momentum (BEM)-based methods, LLFVW analyses provide 3D flow solutions. Extended comparisons between the two approaches are presented and a critical analysis is carried out to identify the benefits and drawbacks of the two approaches.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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