Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.13091/5232
Title: Experimental study on cylinder wake control using forced rotation
Authors: Aksoy, M.H.
Yagmur, S.
Dogan, S.
Goktepeli, I.
Ispir, M.
Keywords: Active flow control
Circular cylinder
Drag coefficient
PIV
Rotation
Strouhal number
Boundary layers
Circular cylinders
Drag coefficient
Flow control
Flow separation
Strouhal number
Velocity measurement
Vortex flow
Wakes
Active flow control
Cylinder wake
Flow characteristic
Image velocimetry
Particle images
PIV
Rotating circular cylinders
Rotation rate
Vortex formation
Wake control
Rotation
Publisher: Elsevier B.V.
Abstract: The study focused on the flow over a rotating circular cylinder in the context of flow control. Particle Image Velocimetry was employed to examine flow characteristics at 2.5 × 103 ≤ Re ≤ 10 × 103. The rotation rates (α) were considered up to 1.57. The mean drag coefficients (CD‾) and Strouhal numbers (St) were examined. The vortex formation length was obtained as approximately 2.1 times the cylinder diameter for α = 1.57. For the stationary cylinder, the length was 1.2 times the diameter from Re = 2.5 × 103 to Re = 10 × 103. Forced rotation enhanced the momentum for the boundary layer and postponed the flow separation on the upper side of the body, leading to flow attachment at α = 1.57. The values decreased from CD‾ = 1.029 to CD‾ = 0.907 as α increased from 0 to 0.39 due to the shrinkage of the wake at Re = 10 × 103. Drag reduction was 3.5 % for α = 0.13, 5.7 % for α = 0.26, and 11.8 % for α = 0.39 thanks to active flow control. The St was attained as 0.17 ≤ St ≤ 0.21 for Re varied, while it remained relatively stable for different α values at the same Re. © 2024 Elsevier Ltd
URI: https://doi.org/10.1016/j.jweia.2024.105662
https://hdl.handle.net/20.500.13091/5232
ISSN: 0167-6105
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collections
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collections

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