|Table of Contents|

Discussion on some problems in combined engine research(PDF)

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

Issue:
2022年06期
Page:
1-8
Research Field:
目次
Publishing date:

Info

Title:
Discussion on some problems in combined engine research
Author(s):
LI Bin1;  ZHANG Mengzheng2;  HUANG Daoqiong2;  NAN Xiangjun2;  ZHANG Mei2
(1.Academy of Aerospace Propulsion Technology, Xian 710100, China 2.Xian Aerospace Propulsion Institute, Xian 710100, China)
Keywords:
combined engine RBCC gas dynamics combustion structure reliability simulation test
PACS:
V439
DOI:
-
Abstract:
The combined engine is a necessary power device for the development of hypersonic aircraft, near space aircraft, and the first stage of the TSTO space transportation system, and it is a popular technology in the current aerospace industry.The combined engine is in the integration stage of key techniques, and the research means of inner flow characteristics, multi-mode combustion, system structure matching and reliability are not perfect.In order to solve the problems such as flow-tube matching of large-scale engine, similarity law of large/small scale combustion structure, mechanical environment experiment, simulation test facility and so on, the continuous innovation is required in research ideas and approaches of key techniques.

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Last Update: 1900-01-01