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Aerodynamic design and analysis of a small-scale vertical axis wind turbine

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Abstract

Small-scale vertical axis wind turbines are regarded today as an attractive source of green energy, still insufficiently implemented and tested. This paper presents a fast design methodology of such a VAWT, in terms of choosing its main parameters: airfoil, rotor diameter and solidity. For obtaining generated power of each considered geometrical model at different undisturbed wind velocities and rotor angular velocities two models were used — momentum and vortex-wake model, combined with experimentally measured airfoil data (airfoil lift and drag coefficients). Even though the former model is simpler, it is the most utilized model, known to provide good results in stationary working regimes. Both models still present fairly accurate and fast tools for computation and optimization, particularly useful in the phase of conceptual design. In this research, the use of the momentum model resulted in determination of the maximal power coefficient, optimal- and minimal freestream velocity for every considered VAWT model. From these output parameters, a selection of the optimal geometric model was done, and a more detailed transient analysis and flow representation around the selected solution was obtained by the vortex-wake model. The results obtained by the two used computational models coincide satisfactorily.

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Correspondence to Jelena Svorcan.

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Recommended by Associate Editor Donghyun You

Jelena Svorcan received her M.Sc. degree at the University of Belgrade, Faculty of Mechanical Engineering, Department of Aeronautics in 2010. Ms. Svorcan is in the pursuit of her Ph.D. at the same university. Her main research interests include analytical analyses and numerical simulations of various flow phenomena.

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Svorcan, J., Stupar, S., Komarov, D. et al. Aerodynamic design and analysis of a small-scale vertical axis wind turbine. J Mech Sci Technol 27, 2367–2373 (2013). https://doi.org/10.1007/s12206-013-0621-x

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  • DOI: https://doi.org/10.1007/s12206-013-0621-x

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