首页|气液同轴双离心式喷嘴喷雾特性

气液同轴双离心式喷嘴喷雾特性

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采用流体体积方法分析涡流器离心式喷嘴内部流动过程,采用单反相机和相位多普勒测速仪测量离心式喷嘴、气液同轴双离心式喷嘴的喷雾特性。发现涡流器离心式喷嘴内部流动的总压损失主要发生在涡流器槽道入口、收敛段和等直段。等直段使液膜厚度减小,喷雾锥角减小。离心式喷嘴喷雾粒径分布范围沿径向逐渐增加,轴向速度分布范围沿径向先减小后逐渐增加。气液同轴双离心式喷嘴喷雾特性受气液比影响很大,气液比小时旋流空气使喷雾锥角增加,粒径分布范围减小;气液比大时,气体膨胀压缩喷雾,使大液滴能够到达喷雾中心,喷雾外侧为二次雾化成的细小液滴。
Spray characteristic of gas-liquid double swirl coaxial injector
The volume of fluid method was used to analyze the flow process in pressure swirl injector.SLR camera and phase doppler anemometry were used to measure the spray characteristics of swirl injector and gas-liquid double swirl coaxial injector.Results show that the total pressure loss occurs mainly in inlet section,convergent section,and columned section of swirler trough.The longer the columned section is,the thicker the liquid film and the smaller the spray cone angle is.The range of spay particle distribution increases gradually along the radial direction while the axial velocity distribution decreases firstly and then increases along radial direction.Spray characteristic of gas-liquid double swirl coaxial injector is greatly influenced by gas-liquid ratio (GLR).While GLR is small enough,swirling air increases the spray cone angle and decreases the range of particle distribution;while GLR is large enough,the expansion of air compresses the spray,pushing large droplets to the center of the spray.And at the edge of spray locates small droplets from second atomization.

gas-liquid coaxial injectordouble swirlspray characteristic

康忠涛、李清廉、张新桥、成鹏

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国防科技大学高超声速冲压发动机技术重点实验室,湖南长沙 410073

国防科技大学航天科学与工程学院,湖南长沙 410073

气液同轴式喷嘴 双离心 喷雾特性

国家自然科学基金资助项目新世纪优秀人才支持计划

11472303,11402298NCET-13-0156

2014

国防科技大学学报
国防科学技术大学

国防科技大学学报

CSTPCDCSCD北大核心EI
影响因子:0.517
ISSN:1001-2486
年,卷(期):2014.(5)
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