| 摘要: |
| 论述了液体火箭推进系统的通用模型。这个模型能广泛地用于各种构型的发动机系统,而且已用于推进系统的稳态与非稳态分析。该模型是线性图论在火箭发动机中的应用,与传统方法相比,它更为有效、方便。 |
| 关键词: 液体推进剂火箭发动机 系统分析 计算机网络 |
| DOI： |
| 分类号: |
| 基金项目: |
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| A GENERALIZED MODEL FOR PERFORMANCE ANALYSIS AND CALCULATION OF LIQUID ROCKET PROPULSION SYSTEM |
|
Wang Kechang
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|
National University of Defence Technology
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| Abstract: |
| This paper describes a generalized model for characterizing liquid propulsion system.The model can be generally applied to various configurations of engine system and has been used for steady and unsteady analysis of propulsion system.It is an application of linear graph theory in the rocket engine. By comparison with conventional method,this modlling method is more efficient and convenient for practical. |
| Key words: Liquid rocket engine System analysis Computer network |
