|Table of Contents|

Comparison of extlnguishing process in dump combustor at the assumption of quasi-steady state(PDF)

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

Issue:
2009年02期
Page:
25-29
Research Field:
研究与设计
Publishing date:

Info

Title:
Comparison of extlnguishing process in dump combustor at the assumption of quasi-steady state
Author(s):
Xi WenxiongWang Zhenguo
College of Aerospace and Material Ensineering,National University of Defense Technology,Changsha 410073,China
Keywords:
flame—residentlimits of pressureleardrich fuellimitsblowout
PACS:
V434
DOI:
-
Abstract:
The process of flame-out in two kinds of flame-resident ramjet combustor,centerdump and side-dump combustor,were analyzed numerically at the assumption of quasi-steady state. The difference of flow field and the change of flame were discussed when the combustor works closely to the limits of pressure and kerosene concentration.It is found that flame front of center— dump combustor shrinking during the extinguish process.The side-dump combustor has a difference in the temperature of backflow region,which leads to the lose of flameholding.

References:

[1]张均勇,张宝诚.航空发动机燃烧室工作稳定性研究忉.航空发动机.2001(1):33-4l·
[2]Sturges GJ’Sloan D G·Flame Stability and Lean Blowout-A Research Program Progress Report in Proceedings of Tenth C ISABEP[R].1991,372384.
[3]郑殿峰,张会强,林文漪,等。蒸发式稳定器常压和低压燃烧性试验研究[J].哈尔滨工业大学学报,2004,(12):1724-1728.
[4]袁怡祥.林宇震.刘高恩.旋流杯燃烧室头部流场与喷雾 大的温度梯度,易出现大量的局部火焰淬熄,导对贫油熄火的影响[J].航空动力学报,2004,(3):45-50.
[5]刘百麟,林宇震,袁怡祥,等.高温升燃烧室贫油熄火稳 定性研究[J].推进技术,2003,(5):73-76.
[6]张宝诚,纪友哲,王平.航空发动机燃烧室熄火特性的研 究[J].沈阳航空工业学院学报,2004,(3):3-5.
[7]张永芝,李卓,李海龙·超声速进气道流场三维数值模拟[J].火箭推进,2008.34(3):27-30.
[8]杨世民,唐豪,黄玥。凹腔超声速燃烧室氢气燃烧流场数值模拟[J].火箭推进,2008,34(1):12-16.

Memo

Memo:
-
Last Update: 1900-01-01