|Table of Contents|

Research on effects of methane injection temperature on combustion stability(PDF)

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

Issue:
2013年04期
Page:
36-40
Research Field:
研究与设计
Publishing date:

Info

Title:
Research on effects of methane injection temperature on combustion stability
Author(s):
REN Zheng-da1;  NIE Wan-sheng2;  CHEN Xin-hua2
1. Department of Postgraduate, the Academy of Equipment, Beijing 101416, China;
Keywords:
LOX/methane rocket engine;  methane injection temperature;  combustion stability
PACS:
V434+.13-34
DOI:
-
Abstract:
A numerical simulation research on combustion stability of LOX/methane rocket engine was made. The effects of methane injection temperature on the combustion stability are analyzed and compared in this paper. The results show that the combustion stability of the engine is better at 222 K, 224 K, 226 K, 228 K, 230 K and 234 K.

References:

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