| 脉冲／变燃面法测定含铝推进剂的响应函数和微粒直径 |
| |
| 引用本文： | 周金仙,谢蔚民.脉冲／变燃面法测定含铝推进剂的响应函数和微粒直径[J].固体火箭技术,1993(2):41-45. |
| |
| 作者姓名： | 周金仙 谢蔚民 |
| |
| 作者单位： | 西北工业大学 西安710072 |
| |
| 摘 要： | 介绍了在T形燃烧器中用脉冲/变燃面法测定含铝推进剂的响应函数和Al_2O_3微粒平均直径的试验方法和试验原理.并介绍了试验测试系统和试验结果.该试验可为固体火箭发动机燃烧不稳定性预估提供原始数据.
|
| 关 键 词： | 火箭发动机 固体推进剂 振荡燃烧 |
Measurement of Response Functions and Particle Diameters of Aluminuzed Propellants Using a Pulsed-Variable Area Method |
| |
| Zhou Jinxian Xie Weimin.Measurement of Response Functions and Particle Diameters of Aluminuzed Propellants Using a Pulsed-Variable Area Method[J].Journal of Solid Rocket Technology,1993(2):41-45. |
| |
| Authors: | Zhou Jinxian Xie Weimin |
| |
| Abstract: | The test method and principle for measurement of response functions and average Al_2O_3 Particle diameters of aluminized propellants using a pulsed-variable area T-burner method are described. Also the measurement system for testing and test results are presented This test can provide original data for estimation of combustion instability in solid rocket motors. |
| |
| Keywords: | Solid rocked engine Solid rocket propellant Oscillatory combustion Burner |
| 本文献已被 CNKI 维普 等数据库收录！ |
