Abstract
The recent development of an unsteady, three-dimensional aerodynamic model has provided the opportunity to determine the influence of detailed blade geometry on the performance of straight-bladed vertical axis wind turbines. In particular, the present paper examines the effect of blade pitch, twist, taper and aerofoil section by comparison with a simplistic baseline configuration. The study concentrates on the low tip-speed ratio regime where the blade aerodynamics are inherently unsteady and the most severe loadings are experienced. In general, the effects of pitch and twist are similar, with both presenting only limited scope for enhanced design. Moderate taper is shown to improve the overall aerodynamic performance while having the structural benefit of reducing the bending moment at the cross-arm. The potential of a blade with varying cross-section to produce passive stall regulation is also demonstrated. Finally, the influence of unsteady blade stall is considered in more detail for each of the configurations.
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