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摘要:
The purpose of this study is to investigate experimentally the effects of orbital motion on the velocity field of boundary layer flow over a rotating disk. The characteristics of velocity field at a fixed orbital angular section measured by a hot-wire anemometer show that the structure of the 3-dimensional boundary layer flow is deformed elliptically and displaced in a certain direction that is not in the orbital radial direction, but the direction of deformation depends on the combination of orbital and rotational directions. For coincide orbital and rotational directions, there are regions where the intensity of low-frequency disturbances increases rapidly in a certain central region (laminar region under pure rotation). The transient vortices, which form streaks on the coating film, are considered to be destroyed by low-frequency disturbances. However, for opposite orbital and rotational directions, the low-frequency disturbances are not observed in any section. As the adding orbital speed increases, the intensity of velocity fluctuations in the turbulence region becomes larger in the expected except in a certain region. This location of the region also depends on the direction of deformation or the combination of orbital and rotational directions.
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篇名 Effects of Orbital Motion on the Velocity Field of Boundary Layer Flow over a Rotating Disk
来源期刊 流体动力学(英文) 学科 数学
关键词 Boundary Layer Flow ROTATING DISK Transition VORTICES HOT-WIRE ANEMOMETER
年,卷(期) 2017,(2) 所属期刊栏目
研究方向 页码范围 169-177
页数 9页 分类号 O1
字数 语种
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研究主题发展历程
节点文献
Boundary
Layer
Flow
ROTATING
DISK
Transition
VORTICES
HOT-WIRE
ANEMOMETER
研究起点
研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
流体动力学(英文)
季刊
2165-3852
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
302
总下载数(次)
0
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0
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