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摘要:
A compression wave is generated ahead of a high-speed train, while entering a tunnel. This compression wave propa- gates to the tunnel exit and spouts out as a micro pressure wave, causing an exploding sound. In order to estimate the magnitude correctly, the mechanism of the attenuation and distortion of a compression wave propagating along a tunnel must be understood and experimental information on these phenomena is required. An experimental and numerical in- vestigation is carried out to clarify the mechanism of the propagating compression wave in a tube. The final objective of our study is to understand the mechanism of the attenuation and distortion of propagating compression waves in a tun- nel. In the present paper, experimental investigations are carried out on the transition of the unsteady boundary layer induced by a propagating compression wave in a model tunnel by means of a developed laser differential interferometry technique.
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篇名 Characteristics of Unsteady Boundary Layer Induced by the Compression Wave Propagating in a Tunnel
来源期刊 流体动力学(英文) 学科 医学
关键词 Transition UNSTEADY BOUNDARY Layer Compression Wave Laser Differential INTERFEROMETRY
年,卷(期) 2012,(4) 所属期刊栏目
研究方向 页码范围 257-263
页数 7页 分类号 R73
字数 语种
DOI
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节点文献
Transition
UNSTEADY
BOUNDARY
Layer
Compression
Wave
Laser
Differential
INTERFEROMETRY
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研究去脉
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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
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