|Table of Contents|

Research progress about rocket based combined cycle combustion organization(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2015年04期
Page:
1-7
Research Field:
专论与综述
Publishing date:

Info

Title:
Research progress about rocket based combined cycle combustion organization
Author(s):
CUI Peng;  XU Wanwu;  CHEN Jian;  SONG Changqing
Key Laboratory on Scramjet Technology, National University of Defense Technology, Changsha 410073, China
Keywords:
rocket based combined cycle;  combustion organization;  fuel injection scheme;  secondary combustion;  adjustment of thermal throat
PACS:
V439-34
DOI:
-
Abstract:
With the increased demand for efficiency and economy on aerospace propulsion, people are looking forward to developing an engine with high thrust-to-weight ratio and high specific impulse. Rocket based combined cycle (RBCC) engine becomes an important direction of development in the fields of aeronautics and astronautics, in which the advantages of rocket engine and ramjet engine are fused. Precise and highly efficient combustion organization is important for the wide range reliable operation and thrust increase of RBCC engine. In this paper, the fundamental concepts and principles of RBCC are introduced, and the research progress of combustion organization on RBCC is reviewed in the aspects of fuel injection scheme, combustion mode and thermal throat adjustment. The fuel injection schemes and thermal throat adjustment in different modes are discussed. The investigation situation of each combustion mode is elaborated. The difficulties and experience during the development of RBCC combustion organization are analyzed. Some suggestions for the study on RBCC in the future are given.

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