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Startup dynamics of drag-based multibladed vertical axis wind turbine.

Asim, Taimoor; Osame, Peter

Authors



Abstract

A multibladed drag-based Vertical Axis Wind Turbine (VAWT) was developed and its startup dynamics evaluated using wind tunnel tests. The experimental data obtained for the time-based angular position of the rotor shaft at Aberdeen's average wind speed of 6 m/s show an initial rapid acceleration of the VAWT due to the drag force being exerted on the rotor blades. This acceleration becomes more gradual until the VAWT reaches its peak rotational speed of 85 rpm in 30 s, which corresponds to an operating tip speed ratio (TSR) of 0.42. The operating TSR of the VAWT was found to be 27% higher than previously reported in numerical studies.

Citation

ASIM, T. and OSAME, P. 2024. Startup dynamics of drag-based mulibladed vertical axis wind turbine. Engineering proceedings [online], 71(1): proceedings of the 4th Annual solar and wind power conference 2024 (ASWEC 2024): next generation of energy solution, 5 June 2024, [virtual conference], article number 5. Available from: https://doi.org/10.3390/engproc2024071005

Presentation Conference Type Conference Paper (published)
Conference Name 4th Annual solar and wind power conference 2024 (ASWEC 2024): next generation of energy solution
Start Date Jun 5, 2024
Acceptance Date Apr 9, 2024
Online Publication Date Jul 29, 2024
Publication Date Dec 31, 2024
Deposit Date Oct 10, 2024
Publicly Available Date Oct 10, 2024
Journal Engineering proceedings
Electronic ISSN 2673-4591
Publisher MDPI
Peer Reviewed Peer Reviewed
Volume 71
Issue 1
Article Number 5
DOI https://doi.org/10.3390/engproc2024071005
Keywords Vertical axis wind turbine; Startup dynamics; Multibladed rotor; Tip speed ratio; Wind tunnel test
Public URL https://rgu-repository.worktribe.com/output/2423388

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Licence
https://creativecommons.org/licenses/by/4.0/

Copyright Statement
© 2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).




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