Survey on the mode transition technique in combined cycle propulsion systems

被引：171

作者：

Huang, Wei ^{[1
]}

Yan, Li ^{[1
]}

Tan, Jian-guo ^{[1
]}

机构：

[1] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2014年 / 39卷

基金：

中国国家自然科学基金;

关键词：

Combined cycle propulsion system; Mode transition; Ramjet mode; Scramjet mode; Ejector mode; Turbojet mode; COMBUSTION CHARACTERISTICS; SCRAMJET; OPTIMIZATION; PERFORMANCE; CATASTROPHE; HYSTERESIS; ENGINES;

D O I：

10.1016/j.ast.2014.07.006

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

With the maturation of the scramjet technologies, the urgent development of the combined cycle propulsion system has been put forward, and it can help the vehicle to launch and land horizontally. In the current survey, the research status on the mode transition of the combined cycle engines has been reviewed in detail, and three typical mode transition processes have been summarized, namely the ejector/ramjet mode transition for the rocket-based combined cycle engine, the turbojet/ramjet mode transition for the turbine-based combined cycle engine and the ramjet/scramjet mode transition for the combined cycle engines. Lastly, some suggestions on the development of the combined cycle propulsion systems have been put forward. (C) 2014 Elsevier Masson SAS. All rights reserved.

引用

页码：685 / 691

页数：7

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