首页 | 本学科首页   官方微博 | 高级检索  
     检索      

液体火箭发动机初始雾化液滴分布预测
引用本文:黄兵,张楠.液体火箭发动机初始雾化液滴分布预测[J].火箭推进,2007,33(2):31-39.
作者姓名:黄兵  张楠
作者单位:1. 中国运载火箭技术研究院总体设计部
2. 北京航天动力研究所
摘    要:在简要描述使用最大熵原理预测初始雾化液滴分布的基础上,发展了较传统方法具有更大收敛域的数值计算方法,建立了离心式喷嘴雾化特性研究实验台,使用激光相位粒子分析仪进行了雾化粒径分布研究,结果显示实验数据同使用最大熵原理预测的分布吻合性较好,在此基础上最后提出了在液体火箭发动机雾化粒径分布预测应用中的策略。

关 键 词:初始雾化  液滴分布  液体火箭发动机  最大熵原理  激光相位多普勒粒子分析仪
修稿时间:2006-10-25

Prediction of droplet size distributions of primary atomization in liquid rocket engine
Huang Bing,Zhang Nan.Prediction of droplet size distributions of primary atomization in liquid rocket engine[J].Journal of Rocket Propulsion,2007,33(2):31-39.
Authors:Huang Bing  Zhang Nan
Institution:1. China Academy of Launch Vehicle Technology Systems Engineering Division, Beijing 100076, China; 2 .Beijing Aerospace Propulsion Institute, Beijing 100076, China
Abstract:The method based Maximum Entropy Principle for prediction of droplet size distributions of primary atomization in liquid rocket engine is described and a developed numerical method is introduced. A study of swirl atomization characteristics is accomplished by using PDPA after an centrifigual type experimental system of atomization characteristics was built. The results show that the prediction value and the experimental data are in good accordance when compared with experimental data, therefore the strategy of applying the method for liquid rocket engine is presented.
Keywords:primary atomization  droplet size distribution  liquid rocket engine  maximum entropy principle  laser phase doppler particle analyzer
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号