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不同环境压力下幂律流体撞击射流破碎特性

Breakup Characteristics of Power Law Fluid from Symmetric Impinging Jet Injector Under Different Ambient Pressures

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【作者】 郑勒白富强杨子明郭瑾朋杜青

【Author】 Zheng Le;Bai Fuqiang;Yang Ziming;Guo Jinpeng;Du Qing;State Key Laboratory of Engines,Tianjin University;Internal Combustion Engine Research Institute,Tianjin University;

【通讯作者】 杜青;

【机构】 天津大学内燃机燃烧学国家重点实验室天津大学内燃机研究所

【摘要】 基于自行搭建的射流系统和定容弹系统,采用高速摄影技术,获得了高环境压力下幂律流体对称撞击式射流的喷雾形貌,提取了射流特征参数破碎长度L与表面波长λ,研究了环境参数(环境压力)、射流参数(韦伯数We)、结构参数(喷孔直径)与物性参数(流体黏度)对射流破碎的影响.结果表明:幂律流体对称撞击式射流共有封闭边界模式、开边界模式、无边界模式、弓形液线模式和完全发展模式共5种破碎模式;在大气环境压力下,L随着We的增加呈"双峰"模式变化;而在有环境压力的情况下,L与We则呈"单峰"模式变化;与大气环境压力相比,高环境压力更有利于幂律流体对称撞击式射流破碎;而喷孔直径与流体黏度的增大均不利于撞击式射流破碎.提出了预测幂律流体对称撞击射流破碎表面波长的破碎模型.

【Abstract】 Experimental observations and analysis on the fluid sheet formed by symmetric impinging jet injectors of power law fluid under high ambient pressure were presented.Constant volume chamber system and high-speed photography technology were used to obtain breakup regimes and spray characteristics.The characteristic parameters such as breakup length L and wave length λ were extracted from the photograph.This paper investigated the environmental parameter(ambient pressure),jet parameter(Weber number),geometry parameter(orifice diameter)and physical parameter(fluid viscosity)on the atomization behaviors of liquid sheets.It is found that the spray regimes could be qualitatively categorized into five types:closed-rim,open-rim,rimless,bow-shaped ligaments and fully developed regimes.In the open space,the L increases with the We in ‘double peak’ mode.While in the case of situation with ambient pressure,the L and the We are in ‘single peak’ mode.Compared with the open space conditions,the high ambient pressure conditions are more favorable to the power law fluid symmetric impact jet breakup.And the increase of orifice diameter and fluid viscosity all inhibit the impingement jet from breakup.An empirical relation for predicting the surface wave length is proposed.

【基金】 国家自然科学基金资助项目(51176136);天津市应用基础与前沿技术研究计划重点资助项目(15JCZDJC39600)
  • 【文献出处】 内燃机学报 ,Transactions of CSICE , 编辑部邮箱 ,2019年01期
  • 【分类号】O358
  • 【被引频次】7
  • 【下载频次】158
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