Towards accurate performance prediction of a vertical axis wind turbine operating at different tip speed ratios

A. Rezaeiha, I. Kalkman, B.J.E. Blocken

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

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Abstract

Accurate prediction of the performance of a vertical-axis wind turbine (VAWT) using CFD simulation requires the employment of a sufficiently fine azimuthal increment (dθ) combined with a mesh size at which essential flow characteristics can be accurately resolved. Furthermore, the domain size needs to be large enough to minimize the effects of blockage and uncertainties in the boundary conditions on the results. The current study systematically investigates the effect of these parameters on the performance of a 2-bladed vertical axis wind turbine (VAWT) using unsteady Reynolds-averaged Navier-Stokes (URANS) simulations. The turbine operates at a constant tip speed ratio (λ) of 4.5. Refining dθ from 10.0° to 0.5° results in a significant change in the power coefficient (CP) while the effect is negligible with further refinement from 0.5° to 0.1° at the given λ. Furthermore, a distance from the turbine center of rotation to the outlet of 10D and a domain width of 20D are found to be safe choices to minimize the effects of blockage and uncertainty in the outlet boundary condition on the results.
Original languageEnglish
Title of host publication7th European and African Conference on Wind Engineering (EACWE 2017), 4-7 July 2017, Liege, Belgium
Publication statusPublished - 4 Jul 2017
Event7th European and African Conference on Wind Engineering (EACWE 2017) - Liege Convention Centre, Liège, Belgium
Duration: 4 Jul 20177 Jul 2017
Conference number: 7
http://aimontefiore.org/EACWE2017/

Conference

Conference7th European and African Conference on Wind Engineering (EACWE 2017)
Abbreviated titleEACWE 2017
Country/TerritoryBelgium
CityLiège
Period4/07/177/07/17
Internet address

Keywords

  • Wind energy
  • Vertical axis wind turbine
  • VAWT
  • CFD
  • URANS
  • guideline
  • Aerodynamics

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