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Effect of struts and central tower on aerodynamics and aeroacoustics of vertical axis wind turbines using mid-fidelity and high-fidelity methods

  • Shubham Shubham*
  • , Francesco Avallone
  • , Livia Brandetti Phd.
  • , Nigel Wright
  • , Anton Ianakiev
  • *Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This study investigates the impact of struts and a central tower on the aerodynamics and aeroacoustics of Darrieus Vertical Axis Wind Turbines (VAWTs) at chord-based Reynolds numbers of 8.12 × 104. A 2-bladed H-Darrieus VAWT is used, featuring a 1.5m diameter, a solidity of 0.1 and a blade cross-section of symmetrical NACA 0021. The turbine design is kept simple and straight-bladed which is essential for isolating and analyzing the specific effects of struts and a tower. The high-fidelity Lattice Boltzmann Method (LBM) in PowerFLOW 6-2020 and the mid-fidelity Lifting Line Free Vortex Wake (LLFVW) method in QBlade 2.0 are employed, with the mid-fidelity method providing a faster analytical tool for insights into the turbine performance. Firstly, both the LLFVW (mid-fidelity) and LBM (high-fidelity) methods effectively capture the general trends observed in VAWT power performance. However, the former predicts mean thrust values that are approximately 10% higher, and mean torque values that are approximately 19% higher, in comparison to the latter. Subsequently, the former predicts lower streamwise wake velocities relative to those predicted by the latter. These differences increase in configurations that include struts and a tower (to 30% - 31%). Secondly, the presence of struts and a tower leads to a reduction in both mean power (by 15% to 55%) and thrust (by 3% to 3.6%), with a further small decrease observed when doubling the tower diameter (power and thrust both by 0.5% to 3%). The struts predominantly affect the spanwise distribution of blade loading, while the tower impacts the azimuthal variation of blade loading. Additionally, the addition of struts and a tower reduces low-frequency noise (50-200 Hz) while increasing high-frequency noise (> 300 Hz). The observed decrease in mean blade loading results in reduced low-frequency noise, while the increase in high-frequency noise is ascribed to the increased intensity of BWI/BVI leading to higher unsteady loading fluctuations on blades.

Original languageEnglish
Title of host publicationAIAA SciTech 2024 Forum
PublisherAmerican Institute of Aeronautics and Astronautics
ISBN (Print)9781624107115
DOIs
Publication statusPublished - 4 Jan 2024
Event2024 AIAA Science and Technology Forum and Exposition - Orlando, United States
Duration: 8 Jan 202412 Jan 2024

Conference

Conference2024 AIAA Science and Technology Forum and Exposition
Abbreviated titleAIAA SciTech Forum 2024
Country/TerritoryUnited States
CityOrlando
Period8/01/2412/01/24

Bibliographical note

Publisher Copyright:
© 2024 by Shubham Shubham. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.

Keywords

  • Aerodynamic Simulation
  • Struts
  • Overall Sound Pressure Level
  • Horizontal Axis Wind Turbine
  • Lattice Boltzmann Approach
  • Vortex Structure
  • Blade Loading
  • Blade Vortex Interaction
  • NACA airfoil
  • Aerodynamic Performance

ASJC Scopus subject areas

  • Aerospace Engineering

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