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摘要:
In this study, flow characteristics are experimentally and numerically discussed, especially concerning shock-cell structure and oscillatory phenomena of supersonic jet. The jet becomes underexpanded when the nozzle pressure ratio of convergent nozzle exceeds the critical value. The underexpanded jet is not uniform because of the presence of the expansion wave, the compression wave and the shock wave formed in it. Many vortices are induced in jet boundary region by shearing stress generated between supersonic jet flow and atmospheric air. They interact with shock waves composing cell node of jet, which is closely related to a noise radiating from the jet. In experiment, flow field is visualized and the shape of cell structure is examined. Furthermore, frequency of vortex generation is measured. The jet is simulated using TVD scheme and the results are compared with the experimental ones. Distortion of cell structure caused by three dimensional oscillation of jet and behavior of vortices are discussed.
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篇名 Structure and Oscillation of Underexpanded Jet
来源期刊 流体动力学(英文) 学科 数学
关键词 Underexpanded JET PLATE Shock INCIDENT Shock VISUALIZATION TVD Scheme
年,卷(期) ltdlxyw,(2) 所属期刊栏目
研究方向 页码范围 85-91
页数 7页 分类号 O1
字数 语种
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Underexpanded
JET
PLATE
Shock
INCIDENT
Shock
VISUALIZATION
TVD
Scheme
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研究分支
研究去脉
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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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