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多孔式喷嘴加湿旋流扩散燃烧流场的实验研究
引用本文:葛冰,臧述升,郭培卿.多孔式喷嘴加湿旋流扩散燃烧流场的实验研究[J].上海交通大学学报,2012,46(5):661-665.
作者姓名:葛冰  臧述升  郭培卿
作者单位:(上海交通大学 机械与动力工程学院, 叶轮机械研究所, 上海 200240)
基金项目:上海市重大科技专项课题资助(09DZ1200705)
摘    要:利用激光粒子图像速度场测量技术对环型多孔式喷嘴的加湿与不加湿旋流扩散燃烧流场进行了实验研究,分析了湿度对旋流扩散燃烧流场的影响.结果表明,随着燃烧流场湿度增大,火焰明显变暗,火焰宽度和高度增大,回流区漩涡与燃烧器出口和喷嘴轴线间的距离减小,轴线上最大回流速度降低,轴线最大回流速度点与喷嘴的距离增加,逆流区宽度和喷嘴旋转射流扩展角减小,流场轴向出口的不均匀系数增大.

关 键 词:   旋流燃烧    湿空气燃烧    激光粒子图像速度场测量技术  
收稿时间:2011-06-30

Experimental Investigation on Humid Air Diffustion Combustion in a Multihole Nozzle Swirl Burner
GE Bing,ZANG Shu-sheng,GUO Pei-qing.Experimental Investigation on Humid Air Diffustion Combustion in a Multihole Nozzle Swirl Burner[J].Journal of Shanghai Jiaotong University,2012,46(5):661-665.
Authors:GE Bing  ZANG Shu-sheng  GUO Pei-qing
Institution:(Turbo Machinery Institute, School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200240, China)
Abstract:Experiments were performed to investigate the flow structures of humid air combustion flame in a multihole nozzle swirl burner. The experiments show that with steam addition, the flame becomes dark, and the flame dimensions grow; the distances between vortexes of recirculation zone and nozzle reduce; the peaks of radial mean velocity, radial rms velocity and Reynolds shear stress decrease; the maximum mean turbulent kinetic energy decreases, and the biggest reversing velocity on nozzle centerline reduces; the width of recirculation zone and the distance between centerline biggest reversing velocity and nozzle is lower; the expansion angle of swirling jet reduces;the axial non uniform coefficient of outlet increases.
Keywords:swirling combustion  humid air combustion  PIV measurement  
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