| 固体火箭发动机热流测量方法及试验研究 |
| |
| 引用本文： | 张翔宇,刘佩进,李鹏飞,李江.固体火箭发动机热流测量方法及试验研究[J].固体火箭技术,2011,34(1):131-134. |
| |
| 作者姓名： | 张翔宇 刘佩进 李鹏飞 李江 |
| |
| 作者单位： | 西北工业大学,燃烧、热结构与内流场重点实验室,西安,710072 |
| |
| 摘 要： | 将一套创新设计的热流测量装置嵌入到可改变条件参数的固体火箭试验发动机中,进行了含铝复合推进剂试验.通过改变推进剂含铝量、燃烧产物冲刷速度和冲刷角度,测量了不同工况下两相燃烧产物的总传热热流密度.总传热规律与理论分析结果相吻合.试验证明,该装置能经受发动机内的高温强冲刷的苛刻务件.试验得到的总热流密度可为绝热层烧蚀研究中...
|
| 关 键 词： | 固体推进剂火箭发动机 热流测量 两相流冲刷 |
Heat flux measurement method and experimental research in SRM |
| |
| ZHANG Xiang-yu,LIU Pei-jin,LI Peng-fei,LI Jiang.Heat flux measurement method and experimental research in SRM[J].Journal of Solid Rocket Technology,2011,34(1):131-134. |
| |
| Authors: | ZHANG Xiang-yu LIU Pei-jin LI Peng-fei LI Jiang |
| |
| Institution: | ZHANG Xiang-yu,LIU Pei-jin,LI Peng-fei,LI Jiang(Science and Technology on Combustion Internal Flow and Thermal-Structure Laboratory,Northwestern Poly Technical University,Xi'an 710072,China) |
| |
| Abstract: | A series of aluminized solid propellant combustion tests were carried out by using an innovativly designed instrument for heat flux measurement.The total heat flux of two-phase flow has been obtained under condition of changing the content of aluminum,altering eroding velocity and incidence angle of the combustion products.Experiments proved that the device was able to endure the harsh condition inside the engine and the test results coincided with theoretical analysis fairly.Heat-flux through the experimen... |
| |
| Keywords: | solid propellant rocket motor heat flux measurement two-phase flow impingement |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
