Conceptual design model of rocket base combined cycle propulsion system

Sheng Hong Huang, Hong Qing He, Guo Qiang He, Pei Jin Liu, Fei Qin, Guo Hui Wang

科研成果: 期刊稿件文章同行评审

10 引用 (Scopus)

摘要

The Rocket-Based-Combined-Cyele Propulsion system and the development of it's conceptual design model were briefly described. Based on the analysis of current model's shortcomings, an one-dimensional performance computation model was established by applying quasi-one-dimensional flow model and chemistry model. In this model, multiple elements, such as variable cross section area, ejecting, fuel injecting, mixing, combustion and so on were considered. The model was solved by implicit RK algorithm, the results agree with the literature.

源语言英语
页(从-至)1-5
页数5
期刊Tuijin Jishu/Journal of Propulsion Technology
24
1
出版状态已出版 - 2月 2003

指纹

探究 'Conceptual design model of rocket base combined cycle propulsion system' 的科研主题。它们共同构成独一无二的指纹。

引用此