Selective Roughness in the Boundary Layer to Suppress Flow-Induced Motions of Circular Cylinder at 30,000<Re<120,000Source: Journal of Offshore Mechanics and Arctic Engineering:;2012:;volume( 134 ):;issue: 004::page 41801DOI: 10.1115/1.4006235Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A passive control means to suppress flow-induced motions (FIM) of a rigid circular cylinder in the TrSL3, high-lift, flow regime is formulated and tested experimentally. The developed method uses passive turbulence control (PTC) consisting of selectively located roughness on the cylinder surface with thickness about equal to the boundary layer thickness. The map of “PTC-to-FIM,” developed in previous work, revealed robust zones of weak suppression, strong suppression, hard galloping, and soft galloping. PTC has been used successfully to enhance FIM for hydrokinetic energy harnessing using the VIVACE Converter. PTC also revealed the potential to suppress FIM to various levels. The map is flow-direction dependent. In this paper, the “PTC-to-FIM” map is used to guide development of FIM suppression devices that are flow-direction independent and hardly affect cylinder geometry. Experiments are conducted in the Low Turbulence Free Surface Water Channel of the University of Michigan on a rigid, horizontal, circular cylinder, suspended on springs. Amplitude and frequency measurements and broad field-of-view visualization reveal complex flow structures and their relation to suppression. Several PTC designs are tested to understand the effect of PTC roughness, location, coverage, and configuration. Gradual modification of PTC parameters, leads to improved suppression and evolution of a design reducing the VIV synchronization range. Over a wide range of high reduced velocities, VIV is fully suppressed. The maximum amplitude occurring near the system’s natural frequency is reduced by about 63% compared to the maximum amplitude of the smooth cylinder.
keyword(s): Flow (Dynamics) , Motion , Surface roughness , Boundary layers , Circular cylinders , Cylinders , Strips , Water , Turbulence , Visualization AND Vortex-induced vibration ,
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| contributor author | Hongrae Park | |
| contributor author | Michael M. Bernitsas | |
| contributor author | R. Ajith Kumar | |
| date accessioned | 2017-05-09T00:53:42Z | |
| date available | 2017-05-09T00:53:42Z | |
| date copyright | November, 2012 | |
| date issued | 2012 | |
| identifier issn | 0892-7219 | |
| identifier other | JMOEEX-926072#041801_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/149979 | |
| description abstract | A passive control means to suppress flow-induced motions (FIM) of a rigid circular cylinder in the TrSL3, high-lift, flow regime is formulated and tested experimentally. The developed method uses passive turbulence control (PTC) consisting of selectively located roughness on the cylinder surface with thickness about equal to the boundary layer thickness. The map of “PTC-to-FIM,” developed in previous work, revealed robust zones of weak suppression, strong suppression, hard galloping, and soft galloping. PTC has been used successfully to enhance FIM for hydrokinetic energy harnessing using the VIVACE Converter. PTC also revealed the potential to suppress FIM to various levels. The map is flow-direction dependent. In this paper, the “PTC-to-FIM” map is used to guide development of FIM suppression devices that are flow-direction independent and hardly affect cylinder geometry. Experiments are conducted in the Low Turbulence Free Surface Water Channel of the University of Michigan on a rigid, horizontal, circular cylinder, suspended on springs. Amplitude and frequency measurements and broad field-of-view visualization reveal complex flow structures and their relation to suppression. Several PTC designs are tested to understand the effect of PTC roughness, location, coverage, and configuration. Gradual modification of PTC parameters, leads to improved suppression and evolution of a design reducing the VIV synchronization range. Over a wide range of high reduced velocities, VIV is fully suppressed. The maximum amplitude occurring near the system’s natural frequency is reduced by about 63% compared to the maximum amplitude of the smooth cylinder. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Selective Roughness in the Boundary Layer to Suppress Flow-Induced Motions of Circular Cylinder at 30,000<Re<120,000 | |
| type | Journal Paper | |
| journal volume | 134 | |
| journal issue | 4 | |
| journal title | Journal of Offshore Mechanics and Arctic Engineering | |
| identifier doi | 10.1115/1.4006235 | |
| journal fristpage | 41801 | |
| identifier eissn | 1528-896X | |
| keywords | Flow (Dynamics) | |
| keywords | Motion | |
| keywords | Surface roughness | |
| keywords | Boundary layers | |
| keywords | Circular cylinders | |
| keywords | Cylinders | |
| keywords | Strips | |
| keywords | Water | |
| keywords | Turbulence | |
| keywords | Visualization AND Vortex-induced vibration | |
| tree | Journal of Offshore Mechanics and Arctic Engineering:;2012:;volume( 134 ):;issue: 004 | |
| contenttype | Fulltext |