| 应用PIV技术测试模型环形燃烧室流场 |
| |
| 引用本文： | 党新宪,赵坚行,张欣,徐榕,颜应文,刘勇. 应用PIV技术测试模型环形燃烧室流场[J]. 航空动力学报, 2009, 24(7): 1470-1475 |
| |
| 作者姓名： | 党新宪 赵坚行 张欣 徐榕 颜应文 刘勇 |
| |
| 作者单位： | 南京航空航天大学能源与动力学院,南京210016;中国人民解放军94580部队航理室,蚌埠233000;南京航空航天大学能源与动力学院,南京,210016 |
| |
| 摘 要： | 采用粒子图像测速仪(PIV)测量带双级旋流器模型环形燃烧室内冷态和燃烧流场,试验研究不同进口气流温度对其冷态和燃烧流场内回流区的形成以及气流速度分布的影响,试验结果表明:燃烧室燃烧流场内回流区长度要比冷态流场短,燃烧流场的脉动速度明显大于冷态流场;另外随着进口气流温度增加,燃烧室冷态和燃烧流场的回流区长度都稍有减少.
|
| 关 键 词： | 燃烧 双旋流器 火焰筒 燃烧室流场测量 粒子图像测速技术测量 |
| 收稿时间： | 2008-07-04 |
| 修稿时间： | 2008-11-05 |
Measurements of the flow fields in a model annular combustor using particle image velocimetry |
| |
| DANG Xin-xian,ZHAO Jian-xing,ZHANG Xin,XU Rong,YAN Ying-wen and LIU Yong. Measurements of the flow fields in a model annular combustor using particle image velocimetry[J]. Journal of Aerospace Power, 2009, 24(7): 1470-1475 |
| |
| Authors: | DANG Xin-xian ZHAO Jian-xing ZHANG Xin XU Rong YAN Ying-wen LIU Yong |
| |
| Affiliation: | 1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China2.Department of Flight Theory Education, The Chinese People's Liberation Army Unit 94580, Bengbu 233000, China |
| |
| Abstract: | The cold and combustion flow fields were measured by particle imaging velocimetry(PIV) in a model annular combustor with the dual-stage swirler.Influences of different inlet temperatures on generations of re-circulation zone and distributions of gas velocities were investigated experimentally in the non-reacting and reacting flow fields.Experimental data shows the lengths of re-circulation zone of combustion flows are shorter than that of cold flows,and reacting fluctuating velocities are larger than non-re... |
| |
| Keywords: | combustion two-stage swirler combustor liner combustor flow field measure particle imaging velocimetry (PIV) measurement |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
|
点击此处可从《航空动力学报》下载全文 |
|
