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摘要:
These experimental investigations are designed to study shock wave characteristics and spray structure. Supersonic liq- uid jets injected into ambient fields are empirically studied using projectile impacts in a two-stage light gas gun. This study looks primarily at the design of the nozzle assembly, the tip velocity of the high speed jet, the structure of the spray jet and the shock wave generation process. The supersonic liquid jets were visualized using an ultra high-speed camera and the schlieren system for visualization to quantitatively analyze the shock wave angle. The experimental re- sults with straight cone nozzle types and various non-Newtonian fluid viscosities are presented in this paper. The effects of nozzle geometry on the jet behavior are described. The characteristics of the shock wave generation and spray jet structure were found to be significantly related to the nozzle geometry. The expansion gases accelerated the projectile, which had a mass of 6 grams, from 250 m/s. As a result, it was found that the maximum jet velocity appeared in the liquid jet with high viscosity properties. Supersonic liquid jets, which occurred at the leading edge the shock waves and the compression waves in front of the jets, were observed. Also, the shock waves significantly affected the atomization process for each spray droplet.
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篇名 Spray Atomization and Structure of Supersonic Liquid Jet with Various Viscosities of Non-Newtonian Fluids
来源期刊 流体动力学(英文) 学科 医学
关键词 TWO-STAGE Light Gas GUN Projectile Impact Non-Newtonian Fluid SUPERSONIC Liquid Jet Shock Wave SMD
年,卷(期) 2012,(4) 所属期刊栏目
研究方向 页码范围 297-304
页数 8页 分类号 R73
字数 语种
DOI
五维指标
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研究主题发展历程
节点文献
TWO-STAGE
Light
Gas
GUN
Projectile
Impact
Non-Newtonian
Fluid
SUPERSONIC
Liquid
Jet
Shock
Wave
SMD
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
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0
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