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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

dc.contributor.authorShubham, Shubham
dc.contributor.authorAvallone, Francesco
dc.contributor.authorBrandetti, Livia
dc.contributor.authorWright, Nigel
dc.contributor.authorIanakiev, Anton
dc.date.accessioned2024-06-06T10:37:17Z
dc.date.available2024-06-06T10:37:17Z
dc.date.freetoread2024-06-06
dc.date.issued2024-01-04
dc.date.pubOnline2024-01-04
dc.description.abstractThis 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 8.12e4. 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.en_UK
dc.description.journalNameAIAA SCITECH 2024 Forum
dc.description.sponsorshipThis project has received funding from the European Union’s Horizon 2020 Marie Curie zEPHYR research and innovation programme under grant agreement No EC grant 860101 (https://www.h2020-zephyr.eu/).en_UK
dc.identifier.citationShubham S, Avallone F, Brandetti L, et al., (2024) Effect of struts and central tower on aerodynamics and aeroacoustics of vertical axis wind turbines using mid-fidelity and high-fidelity methods. In: AIAA SCITECH 2024 Forum, 8-12 January 2024, Orlando, USA, Paper number AIAA 2024-1485en_UK
dc.identifier.isbn978-1-62410-711-5
dc.identifier.paperNoAIAA 2024-1485
dc.identifier.urihttps://doi.org/10.2514/6.2024-1485
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/21983
dc.language.isoen_UKen_UK
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_UK
dc.rightsAttribution 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectAerodynamic Simulationen_UK
dc.subjectStrutsen_UK
dc.subjectOverall Sound Pressure Levelen_UK
dc.subjectHorizontal Axis Wind Turbineen_UK
dc.subjectLattice Boltzmann Approachen_UK
dc.subjectVortex Structureen_UK
dc.subjectBlade Loadingen_UK
dc.subjectBlade Vortex Interactionen_UK
dc.subjectNACA airfoilen_UK
dc.subjectAerodynamic Performanceen_UK
dc.titleEffect of struts and central tower on aerodynamics and aeroacoustics of vertical axis wind turbines using mid-fidelity and high-fidelity methodsen_UK
dc.typeConference paperen_UK
dcterms.coverageOrlando, USA
dcterms.temporal.endDate2024-01-12
dcterms.temporal.startDate2024-01-08

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