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低排放驻涡燃烧室冷态流场特性试验

蒋波 何小民 金义 吴泽俊 丁国玉

蒋波, 何小民, 金义, 吴泽俊, 丁国玉. 低排放驻涡燃烧室冷态流场特性试验[J]. 航空动力学报, 2013, 28(8): 1719-1726.
引用本文: 蒋波, 何小民, 金义, 吴泽俊, 丁国玉. 低排放驻涡燃烧室冷态流场特性试验[J]. 航空动力学报, 2013, 28(8): 1719-1726.
JIANG Bo, HE Xiao-min, JIN Yi, WU Ze-jun, DING Guo-yu. Experimental investigation on cold flow field characteristics of low emission trapped-vortex combustor[J]. Journal of Aerospace Power, 2013, 28(8): 1719-1726.
Citation: JIANG Bo, HE Xiao-min, JIN Yi, WU Ze-jun, DING Guo-yu. Experimental investigation on cold flow field characteristics of low emission trapped-vortex combustor[J]. Journal of Aerospace Power, 2013, 28(8): 1719-1726.

低排放驻涡燃烧室冷态流场特性试验

基金项目: 工业和信息化部民用航空发动机燃烧室基础预研项目

Experimental investigation on cold flow field characteristics of low emission trapped-vortex combustor

  • 摘要: 利用粒子图像测速仪(PIV)对低排放驻涡燃烧室模型进行冷态流场测量,获得该燃烧室流场的变化规律和压力损失的变化情况.试验结果表明:低排放驻涡燃烧室涡系结构稳定,在主流后方的驻涡区存在主副双涡结构,联焰板后方的驻涡区存在单涡结构,两者之间特征截面呈现出双涡涡系逐渐向单涡涡系过渡,涡心位置也随截面的变换而变化.随着进口马赫数(0.15~0.30)的增大,主涡面积随之增加,副涡面积在进口马赫数为0.2时最大,而各特征截面上主副双涡及单涡的涡心位置基本不变.驻涡区涡系强度及其边缘的气流速度,以及主燃区的气流速度均随进口马赫数增大而提高.总压损失随进口马赫数(0.15~0.30)的增大而增加.

     

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出版历程
  • 收稿日期:  2012-08-18
  • 刊出日期:  2013-08-28

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