The role of separation on the forces acting on a circular cylinder with a control rod

The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been known that this is an effective way to attenuate regular vortex shedding leading to reductions in its adverse effects on bluff-body flow. The a...

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Published inJournal of fluid mechanics Vol. 915
Main Authors Cicolin, M.M., Buxton, O.R.H., Assi, G.R.S., Bearman, P.W.
Format Journal Article
LanguageEnglish
Published Cambridge, UK Cambridge University Press 11.03.2021
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ISSN0022-1120
1469-7645
DOI10.1017/jfm.2021.64

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Abstract The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been known that this is an effective way to attenuate regular vortex shedding leading to reductions in its adverse effects on bluff-body flow. The aim of this study is to improve understanding of the ways the control rod affects the near-wake flow including how it influences the positions of boundary layer separation. Experiments were carried out in a water channel to measure lift and drag forces and particle image velocimetry (PIV) was employed to obtain detailed information on flow structure. The values of important properties were fixed as follows: Reynolds number, 20 000; ratio of cylinder and control rod diameters, 10 : 1; centre-to-centre distance between main cylinder and control rod, 0.7$D$ (where $D$ is the main cylinder diameter). The adjustable parameter was the angular position of the rod, $\theta$, which was varied between $90^{\circ }$ and $180^{\circ }$ from the front stagnation line. Lift and drag forces were measured separately for the main cylinder and the control rod. A new method for identifying flow states is introduced using PIV to interrogate the instantaneous flow velocity in the gap between the main cylinder and the control rod. Similarly to previous studies, three stable flow states were observed together with a bistable state. The bistable state is very sensitive to the control rod angle with a small change of ${\pm }1^{\circ }$ being sufficient to change the flow state.
AbstractList The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been known that this is an effective way to attenuate regular vortex shedding leading to reductions in its adverse effects on bluff-body flow. The aim of this study is to improve understanding of the ways the control rod affects the near-wake flow including how it influences the positions of boundary layer separation. Experiments were carried out in a water channel to measure lift and drag forces and particle image velocimetry (PIV) was employed to obtain detailed information on flow structure. The values of important properties were fixed as follows: Reynolds number, 20 000; ratio of cylinder and control rod diameters, 10 : 1; centre-to-centre distance between main cylinder and control rod, 0.7 $D$ (where $D$ is the main cylinder diameter). The adjustable parameter was the angular position of the rod, $\theta$ , which was varied between $90^{\circ }$ and $180^{\circ }$ from the front stagnation line. Lift and drag forces were measured separately for the main cylinder and the control rod. A new method for identifying flow states is introduced using PIV to interrogate the instantaneous flow velocity in the gap between the main cylinder and the control rod. Similarly to previous studies, three stable flow states were observed together with a bistable state. The bistable state is very sensitive to the control rod angle with a small change of ${\pm }1^{\circ }$ being sufficient to change the flow state.
The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been known that this is an effective way to attenuate regular vortex shedding leading to reductions in its adverse effects on bluff-body flow. The aim of this study is to improve understanding of the ways the control rod affects the near-wake flow including how it influences the positions of boundary layer separation. Experiments were carried out in a water channel to measure lift and drag forces and particle image velocimetry (PIV) was employed to obtain detailed information on flow structure. The values of important properties were fixed as follows: Reynolds number, 20 000; ratio of cylinder and control rod diameters, 10 : 1; centre-to-centre distance between main cylinder and control rod, 0.7$D$ (where $D$ is the main cylinder diameter). The adjustable parameter was the angular position of the rod, $\theta$, which was varied between $90^{\circ }$ and $180^{\circ }$ from the front stagnation line. Lift and drag forces were measured separately for the main cylinder and the control rod. A new method for identifying flow states is introduced using PIV to interrogate the instantaneous flow velocity in the gap between the main cylinder and the control rod. Similarly to previous studies, three stable flow states were observed together with a bistable state. The bistable state is very sensitive to the control rod angle with a small change of ${\pm }1^{\circ }$ being sufficient to change the flow state.
The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been known that this is an effective way to attenuate regular vortex shedding leading to reductions in its adverse effects on bluff-body flow. The aim of this study is to improve understanding of the ways the control rod affects the near-wake flow including how it influences the positions of boundary layer separation. Experiments were carried out in a water channel to measure lift and drag forces and particle image velocimetry (PIV) was employed to obtain detailed information on flow structure. The values of important properties were fixed as follows: Reynolds number, 20 000; ratio of cylinder and control rod diameters, 10 : 1; centre-to-centre distance between main cylinder and control rod, 0.7\(D\) (where \(D\) is the main cylinder diameter). The adjustable parameter was the angular position of the rod, \(\theta\), which was varied between \(90^{\circ }\) and \(180^{\circ }\) from the front stagnation line. Lift and drag forces were measured separately for the main cylinder and the control rod. A new method for identifying flow states is introduced using PIV to interrogate the instantaneous flow velocity in the gap between the main cylinder and the control rod. Similarly to previous studies, three stable flow states were observed together with a bistable state. The bistable state is very sensitive to the control rod angle with a small change of \({\pm }1^{\circ }\) being sufficient to change the flow state.
ArticleNumber A33
Author Cicolin, M.M.
Assi, G.R.S.
Bearman, P.W.
Buxton, O.R.H.
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  surname: Bearman
  fullname: Bearman, P.W.
  organization: 1Department of Aeronautics, Imperial College London, London SW7 2AZ, UK
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Snippet The development of the flow around a circular cylinder with a smaller diameter control rod in close proximity is the subject of this paper. It has long been...
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SubjectTerms Angular position
Boundary layers
Circular cylinders
Control
Control rods
Cylinders
Diameters
Drag
Flow separation
Flow structures
Flow velocity
Fluid dynamics
Fluid flow
Fluid mechanics
Forces
JFM Papers
Lift
Particle image velocimetry
Reynolds number
Separation
Vortex shedding
Vortices
Title The role of separation on the forces acting on a circular cylinder with a control rod
URI https://www.cambridge.org/core/product/identifier/S0022112021000641/type/journal_article
https://www.proquest.com/docview/2499863046
Volume 915
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