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结构参数对离心喷嘴出口液膜厚度的影响 被引量:12

Effect of structural parameters on film thickness at centrifugal nozzle outlet
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摘要 应用基于VOF的界面跟踪方法和realizable k-ε湍流模型分析了喷嘴出口结构参数对出口液膜厚度的影响规律,并将数值结果和试验数据进行对比,证实了模型的可靠性.结果表明:在喷嘴出口处液膜以环状形式分布,中间有一空心气锥,空心气锥半径越大,液膜越薄,并且随着流量的增大,液膜的破碎长度减小;喷嘴出口扩散角越大,喷嘴出口处液膜越薄,液膜破碎长度越短;喷嘴出口直径越大,液膜破碎长度越长,但液膜厚度不稳定;喷嘴出口直管段越长,液膜破碎长度越短,但对液膜在喷嘴出口后期发展的影响不是很大. VOF method was employed with realizable k-ε turbulence model to predict the influence of structure parameters on liquid film thickness at the outlet of centrifugal nozzle. The numerical result was compared with experimental data to verify the model reliability. The numerical simulation results show that the film is formed into a ring with an air cone in central axis. The liquid membrane is decreased with the increasing of air cone radius,and the length of film broken is shortened by improving flow rate. The bigger the diffusion angle is,the thinner the liquid film is with the shorter of the length of film broken.The bigger the nozzle diameter is,the longer the length of film broken is with unsteady film thickness,and the size of film thickness is floating. The longer the straight of nozzle exit is,the shorter the length of film broken is,while the effect of exit straight length is slight.
出处 《江苏大学学报(自然科学版)》 EI CAS CSCD 北大核心 2015年第3期271-275,共5页 Journal of Jiangsu University:Natural Science Edition
基金 国家自然科学基金资助项目(51336001)
关键词 离心式喷嘴 VOF 结构参数 液膜厚度 数值模拟 centrifugal nozzle volume of fluid structural parameter film thickness numerical simulation
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参考文献12

  • 1马昕霞,袁益超,黄鸣,刘聿拯.多喷嘴汽-液两相喷射性能的实验研究[J].动力工程学报,2010,30(10):777-781. 被引量:8
  • 2刘联胜,杨华,吴晋湘,闫运忠.环状出口气泡雾化喷嘴液膜破碎过程与喷雾特性[J].燃烧科学与技术,2005,11(2):121-125. 被引量:23
  • 3王晓英,罗惕乾,沙毅,王正,高正平.双流体喷嘴荷电雾化特性[J].江苏大学学报(自然科学版),2007,28(4):328-331. 被引量:22
  • 4Thompson J C, Rothstein J P. The atonmization of visco- elastic fluids in flat-fan and hollow-cone spray nozzles [ J 1. Journal of Non-Newtonian Fluid Mechanics, 2007, 147:11-22.
  • 5Hart Zhiyu, Perrish S, Farrell P V, et al. Modeling atomization processes of pressure-swirl hollow-cone fuel sprays[ J 1. Atomization and Sprays, 1997,7 : 663 - 684.
  • 6Hirt C W,Nichols B D. Volume of fluid (VOF) method for the dynamics of free boundaries [ J ]. Journal of Com- putational Physics, 1981, 39 ( 1 ) :201 - 225.
  • 7Torrey M D,Cloutman L D, Mjolsness R C, et al. NASA- VOF 2D: a computer program for incompressible flows with free surface [ R ]. USA:Los Alamos Scientific Labo- ratory, 1985.
  • 8郑群,李义进,孙兰昕.利用开源CFD程序计算可压缩流场[J].哈尔滨工程大学学报,2011,32(6):748-753. 被引量:5
  • 9邱庆刚,刘丽娜.喷嘴结构对流场性能影响的研究[J].石油化工高等学校学报,2011,24(1):68-72. 被引量:6
  • 10Biswas G, Sore S K. Coefficient of dischrage and spray cone angle of a pressure nozzle with combined axial and tangential entry of power-law fluids [ J ]. Applied Scienti- fic Research, 1986,43 : 3 - 22.

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