Vortex-induced vibration of symmetric airfoils used in Vertical-Axis Wind Turbines
Vortex-induced vibration of symmetric airfoils used in Vertical-Axis Wind Turbines
We present an experimental study on a flexibly-mounted NACA 0021 airfoil, allowed to oscillate in the crossflow direction to investigate its Vortex-Induced Vibration (VIV)response at varying angles of attack, α, in the range of 0◦≤α≤180◦. This airfoil is considered since it is one of the airfoils used in Vertical-Axis Wind Turbine (VAWT) designs. Based on the experimental results of the current work, oscillations are observed for angles of attack in the range of 60◦≤α≤130◦. The peak amplitude, A∗ = 1.93, and the largest lock-in range,1.7 < U∗ < 12, are observed at α = 90◦. For angles of attack for which oscillations are observed, the frequency ratio remains close to unity, implying that lock-in has occurred. The wake and crossflow force magnitudes and frequency contents for the airfoil at angles of attack symmetric about α = 90◦are compared and differences in terms of the airfoil displacement, width of the wake, force coefficient magnitudes and frequencies are shown when the leading edge of the airfoil is facing the incoming flow (0◦≤α≤85◦) or the trailing edge is facing the incoming flow (95◦≤α≤180◦). It is also shown that the observed VIVoccurs within the range of reduced velocities that are expected for the full-scale VAWTs.
Benner, Bridget M.
9b11d1f5-62bc-4815-becf-52122fcd620e
Carlson, Daniel W.
c0f88797-732c-46ef-8e74-a5186d4733bf
Seyed-Aghazadeh, Banafsheh
518b7862-48c8-4a20-988d-04f72579d402
Modarres-Sadeghi, Yahya
ef096f40-2b74-4287-a2a9-e1ecf76ea792
27 November 2019
Benner, Bridget M.
9b11d1f5-62bc-4815-becf-52122fcd620e
Carlson, Daniel W.
c0f88797-732c-46ef-8e74-a5186d4733bf
Seyed-Aghazadeh, Banafsheh
518b7862-48c8-4a20-988d-04f72579d402
Modarres-Sadeghi, Yahya
ef096f40-2b74-4287-a2a9-e1ecf76ea792
Benner, Bridget M., Carlson, Daniel W., Seyed-Aghazadeh, Banafsheh and Modarres-Sadeghi, Yahya
(2019)
Vortex-induced vibration of symmetric airfoils used in Vertical-Axis Wind Turbines.
Journal of Fluids and Structures, 91, [102577].
(doi:10.1016/j.jfluidstructs.2019.01.018).
Abstract
We present an experimental study on a flexibly-mounted NACA 0021 airfoil, allowed to oscillate in the crossflow direction to investigate its Vortex-Induced Vibration (VIV)response at varying angles of attack, α, in the range of 0◦≤α≤180◦. This airfoil is considered since it is one of the airfoils used in Vertical-Axis Wind Turbine (VAWT) designs. Based on the experimental results of the current work, oscillations are observed for angles of attack in the range of 60◦≤α≤130◦. The peak amplitude, A∗ = 1.93, and the largest lock-in range,1.7 < U∗ < 12, are observed at α = 90◦. For angles of attack for which oscillations are observed, the frequency ratio remains close to unity, implying that lock-in has occurred. The wake and crossflow force magnitudes and frequency contents for the airfoil at angles of attack symmetric about α = 90◦are compared and differences in terms of the airfoil displacement, width of the wake, force coefficient magnitudes and frequencies are shown when the leading edge of the airfoil is facing the incoming flow (0◦≤α≤85◦) or the trailing edge is facing the incoming flow (95◦≤α≤180◦). It is also shown that the observed VIVoccurs within the range of reduced velocities that are expected for the full-scale VAWTs.
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Accepted/In Press date: 16 January 2019
e-pub ahead of print date: 1 April 2019
Published date: 27 November 2019
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Local EPrints ID: 507205
URI: http://eprints.soton.ac.uk/id/eprint/507205
ISSN: 0889-9746
PURE UUID: 1258d8da-cfa6-4093-9054-bf4a0811f329
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Date deposited: 01 Dec 2025 17:43
Last modified: 03 Dec 2025 03:06
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Author:
Bridget M. Benner
Author:
Daniel W. Carlson
Author:
Banafsheh Seyed-Aghazadeh
Author:
Yahya Modarres-Sadeghi
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