液体火箭推进系统性能分析计算的通用模型  

A GENERALIZED MODEL FOR PERFORMANCE ANALYSIS AND CALCULATION OF LIQUID ROCKET PROPULSION SYSTEM

作　　者：王克昌[1] 

机构地区：[1]国防科技大学

出　　处：《推进技术》1992年第2期18-25,共8页Journal of Propulsion Technology

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。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.

关 键 词：液体推进剂 火箭发动机 计算机网络 

分 类 号：V434[航空宇航科学与技术—航空宇航推进理论与工程]