| 固体火箭冲压发动机燃烧性能评价方法 |
| |
| 引用本文： | 王玉清,李立翰,刘鸣雳,何勇攀.固体火箭冲压发动机燃烧性能评价方法[J].推进技术,2011,32(4):520-524. |
| |
| 作者姓名： | 王玉清 李立翰 刘鸣雳 何勇攀 |
| |
| 作者单位： | 1. 中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室,北京100074／中国航天科工集团三十一研究所,北京100074
2. 中国航天科工集团三十一研究所,北京,100074 |
| |
| 摘 要： | 通过对固体火箭冲压发动机的工作特点分析,提出了适用于评价固体火箭冲压发动机燃烧性能的方法。对气动法、燃气分析法、台架推力法等燃烧性能评价方法进行了分析,并对其优缺点进行了说明。
|
| 关 键 词： | 固体火箭冲压发动机 燃烧室 燃烧效率 |
| 收稿时间： | 2011/1/25 0:00:00 |
| 修稿时间： | 6/7/2011 12:00:00 AM |
Analysis of combustion efficiency for ducted rocket |
| |
| WANG Yu-qing,LI Li-han,LIU Ming-li and HE Yong-pan.Analysis of combustion efficiency for ducted rocket[J].Journal of Propulsion Technology,2011,32(4):520-524. |
| |
| Authors: | WANG Yu-qing LI Li-han LIU Ming-li and HE Yong-pan |
| |
| Institution: | WANG Yu-qing1,2,LI Li-han1,LIU Ming-li 2,HE Yong-pan2(1.Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China,2.The 31st Research Inst.of CASIC,Beijing 100074) |
| |
| Abstract: | Based on analysis working characteristics of ducted rocket,an method was put forward which used to assess the combustion performance of ducted rocket.The research analyzed the combustion performance assessment methods which concluding gas dynamical method,gas analysis,rig thrust method and so on.At the same time,the advantage and disadvantage of different combustion performance assessment methods in the research. |
| |
| Keywords: | Ducted rocket Combustion chamber Combustion efficiency |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《推进技术》浏览原始摘要信息 |
| 点击此处可从《推进技术》下载免费的PDF全文 |
|
