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液体火箭推进系统性能分析计算的通用模型
引用本文:王克昌.液体火箭推进系统性能分析计算的通用模型[J].推进技术,1992,13(2):18-25.
作者姓名:王克昌
作者单位:国防科技大学
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  计算机网络

A GENERALIZED MODEL FOR PERFORMANCE ANALYSIS AND CALCULATION OF LIQUID ROCKET PROPULSION SYSTEM
Wang Kechang.A GENERALIZED MODEL FOR PERFORMANCE ANALYSIS AND CALCULATION OF LIQUID ROCKET PROPULSION SYSTEM[J].Journal of Propulsion Technology,1992,13(2):18-25.
Authors:Wang Kechang
Institution:National University of Defence Technology
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.
Keywords:Liquid rocket engine  System analysis  Computer network  
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