| 引用本文: | 张育林.变推力液体火箭发动机动态特性的状态空间分析.[J].国防科技大学学报,1983,(3):23-37.[点击复制] |
| Zhang YuLin.State-Space Analysis of the Dynamic Characteristics of a Variable Thrust Liquid Propellant Rocket Engine[J].Journal of National University of Defense Technology,1983,(3):23-37[点击复制] |
|
| |
|
|
| 本文已被：浏览 5253次 下载 5471次 |
| 变推力液体火箭发动机动态特性的状态空间分析 |
| 张育林 |
|
()
|
| 摘要: |
| 本文将状态空间分析方法运用于变推力液体火箭发动机系统的动态特性分析，导出了一组描述所述变推力液体火箭发动机动态过程的状态方程。文中提出了求解该系统方程的一种有效的数值方法，理论解与实验数据得到了满意的符合。做为变推力液体火箭发动机系统分析的初步结果，在文中分析了几个重要的工作参数对所述发动机系统动态特性的影响。 |
| 关键词: |
| DOI： |
| 投稿日期：1982-11-16 |
| 基金项目: |
|
| State-Space Analysis of the Dynamic Characteristics of a Variable Thrust Liquid Propellant Rocket Engine |
| Zhang YuLin |
| Abstract: |
| This paper states the app1icalion of stale-space method to the analysis of the dynamic characteristics of a variable thrust liquid propellant rocket engine and presents a set of state equations for describing the dynamic process of the engine. An efficient numerical method for solving these system equations is developed. The theoretical solutions agree well with the experimental data. The analysis leads to the following conc1usion: the set coefficient of the impulse width，the working frequency of the solenoid valves and the deviation of the critical working points of these valves are important parameters for determining the dynamic response time and the control precision of this engine. The methods developed in this paper may be used effectively in the analysis of dynamic characteristics of variable thrust liquid propellant rocket engines. |
| Keywords: |
|
|
