| 变几何喉道对超燃冲压发动机点火与燃烧性能的影响 |
| |
| 引用本文： | 潘余,李大鹏,刘卫东,梁剑寒,王振国. 变几何喉道对超燃冲压发动机点火与燃烧性能的影响[J]. 推进技术, 2006, 27(3): 225-229 |
| |
| 作者姓名： | 潘余 李大鹏 刘卫东 梁剑寒 王振国 |
| |
| 作者单位： | 国防科技大学,航天与材料工程学院,湖南,长沙,410073 |
| |
| 基金项目： | 国家高技术研究发展计划(863计划) |
| |
| 摘 要： | 1引言超燃冲压发动机能高速飞行且能利用空气中的氧气作氧化剂,增加了有效载荷,因而备受重视,但它需要在较高的飞行马赫数下才能工作,因此受到较大的限制。由于双模态超燃冲压发动机可以将工作飞行马赫数下限降低至Ma=3,发动机在飞行马赫数Ma=3~6时以亚燃冲压模态工作,在马赫数
|
| 关 键 词： | 超音速冲压喷气发动机 模态转换 变几何喉道 点火 燃烧性能 |
| 文章编号： | 1001-4055（2006）03-0225-05 |
| 收稿时间： | 2005-05-18 |
| 修稿时间： | 2005-09-10 |
Variable geometry effects on the scramjet ignition and combustion |
| |
| PAN Yu,Li Da-peng,LIU Wei-dong,LIANG Jian-han and WANG Zhen-guo. Variable geometry effects on the scramjet ignition and combustion[J]. Journal of Propulsion Technology, 2006, 27(3): 225-229 |
| |
| Authors: | PAN Yu Li Da-peng LIU Wei-dong LIANG Jian-han WANG Zhen-guo |
| |
| Affiliation: | Inst. of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073, China |
| |
| Abstract: | To study the variable geometry effects on the dual mode scramjet operation,the mode translation with different ER(equivalence ratio) and the influence on the ignition ability and combustion efficiency of variable geometry dual mode scramjet were investigated by experimental method.The results revealed that the variable geometry can improve the ignition ability,flame holding ability and combustion efficiency and make the mode translation procedure quickly.However,it can also influence the ignition and flame holding process. |
| |
| Keywords: | Supersonic combustion ramjet engine Mode translation~+ Variable geometry~+ Ignition Combustion performance |
| 本文献已被 CNKI 维普 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 |
|
