| 基于主动轮廓方法提取雾化锥角 |
| |
| 引用本文： | 曾青华,范慧杰,王岳,孔文俊.基于主动轮廓方法提取雾化锥角[J].航空动力学报,2014,29(2):284-289. |
| |
| 作者姓名： | 曾青华 范慧杰 王岳 孔文俊 |
| |
| 作者单位： | 1.中国科学院 工程热物理研究所 中国科学院轻型动力重点实验室, 北京 100190 |
| |
| 基金项目： | 国家自然科学基金（50936005，50876110）；国家高技术研究发展计划（2007AA050501，2007AA050502） |
| |
| 摘 要： | 基于主动轮廓方法（ACM）原理，将ACM延伸开发应用到雾化锥角的测量领域.经过调试，ACM成功捕捉到了雾锥边界以及喷雾矩在喷口后一定位置处出现的收缩特征，准确地获得了雾化锥角.验证结果显示:ACM获得的雾化锥角数值与阴影法测量值之间的相对误差小于1.5%.基于ACM提取雾化锥角方法的应用可以在保证实验结果准确度的同时降低工程应用成本.
|
| 关 键 词： | 雾化锥角 主动轮廓 燃烧室 喷嘴 喷雾测量 |
| 收稿时间： | 2012/12/11 0:00:00 |
Spray angle tracking based on active contour method |
| |
| ZENG Qing-hu,FAN Hui-jie,WANG Yue and KONG Wen-jun.Spray angle tracking based on active contour method[J].Journal of Aerospace Power,2014,29(2):284-289. |
| |
| Authors: | ZENG Qing-hu FAN Hui-jie WANG Yue and KONG Wen-jun |
| |
| Institution: | 1.Key Laboratory of Light-duty Gas-turbine Chinese Academy of Sciences, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China2.University of Chinese Academy of Sciences, Beijing 100039, China3.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China |
| |
| Abstract: | Active contour model (ACM) was developed to track spray angle of atomizer. Through debugging and testing, ACM successfully captured the boundary of atomizer spray. The feature of spray contraction at downstream part of spray was also obtained, and spray angle was got exactly. The verification results show that, the relative errors between the spray angle values measured by the ACM tracking and the shadowgraph measurement are less than 1.5%. The ACM tracking spray angle can reduce cost of engineering applications with an identical measuring accuracy. |
| |
| Keywords: | spray angle active contour combustor atomizer measurement of spray |
| 本文献已被 CNKI 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》下载免费的PDF全文 |
|
