Aerodynamic model comparison for an X-shaped vertical-axis wind turbine

Journal Article (2024)
Author(s)

A. Giri Ajay (TU Delft - Wind Energy)

Laurence Morgan (University of Strathclyde)

Y. Wu (TU Delft - Wind Energy)

David Bretos (Centro Nacional de Energías Renovables)

Aurelio Cascales (Centro Nacional de Energías Renovables)

Oscar Pires (Centro Nacional de Energías Renovables)

Carlos Ferreira (TU Delft - Wind Energy)

Research Group
Wind Energy
DOI related publication
https://doi.org/10.5194/wes-9-453-2024
More Info
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Publication Year
2024
Language
English
Research Group
Wind Energy
Issue number
2
Volume number
9
Pages (from-to)
453-470
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Abstract

This article presents a comparison study of different aerodynamic models for an X-shaped vertical-axis wind turbine and offers insight into the 3D aerodynamics of this rotor at fixed pitch offsets. The study compares six different numerical models: a double-multiple streamtube (DMS) model, a 2D actuator cylinder (2DAC) model, an inviscid free vortex wake model (from CACTUS), a free vortex wake model with turbulent vorticity (from QBlade), a blade-resolved unsteady Reynolds-averaged Navier–Stokes (URANS) model, and a lattice Boltzmann method (from PowerFLOW). All models, except URANS and PowerFLOW use the same blade element characteristics other than the number of blade elements. This comparison covers the present rotor configuration for several tip-speed ratios and fixed blade pitch offsets without unsteady corrections, except for the URANS and PowerFLOW which cover a single case. The results show that DMS and 2DAC models are inaccurate – especially at highly loaded conditions, are unable to predict the downwind blade vortex interaction, and do not capture the vertical/axial induction this rotor exhibits. The vortex models are consistent with each other, and the differences when compared against the URANS and PowerFLOW mostly arise due to the unsteady and flow curvature effects. Furthermore, the influence of vertical induction is very prominent for this rotor, and this effect becomes more significant with fixed pitch offsets where the flow at the blade root is considerably altered.

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