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预燃室低频不稳定燃烧仿真研究
引用本文:汪洪波,王振国,孙明波.预燃室低频不稳定燃烧仿真研究[J].火箭推进,2007,33(5):22-26.
作者姓名:汪洪波  王振国  孙明波
作者单位:国防科技大学,航天与材料工程学院,长沙,410073
摘    要:为弄清燃烧不稳定性激励机制,建立了氢氧预燃室低频燃烧稳定性分析数学模型,利用MATLAB/SIMULINK集成软件包搭建仿真平台,研究了与供应系统耦合的低频不稳定燃烧。结果表明:在各种不稳定激励因素中,氧的喷注压降对稳定性影响最为显著,当其值低于某一稳定边界时,出现极限环振荡,提高氧的喷注压降可以非常有效地抑制低频不稳定燃烧;当氧的喷注压降位于稳定边界附近时,混合比将对稳定性产生一定影响,降低混合比可以较好地抑制低频不稳定;氢的喷注压降对低频燃烧稳定性影响很小。

关 键 词:预燃室  低频不稳定燃烧  仿真
文章编号:(2007)05-0022-05
修稿时间:2006-07-04

Simulation investigations of low frequency combustion instability of precombustion chamber
Wang Hongbo,Wang Zhenguo,Sun Mingbo.Simulation investigations of low frequency combustion instability of precombustion chamber[J].Journal of Rocket Propulsion,2007,33(5):22-26.
Authors:Wang Hongbo  Wang Zhenguo  Sun Mingbo
Institution:Inst. of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:To reveal the mechanism of combustion instability,mathematic models for low frequency combustion stability analysis are developed.Then the low frequency combustion instability coupled with feed system is simulated by using MATLAB/SIMULINK software.The results show that the reduction of oxygen injection pressure is the most remarkable factor that prompts the instability.Once it is below a certain stable boundary,pressure oscillation increases to a limit cycle.So increasing the reduction of oxygen injection pressure can restrain the instability very effectively.If the reduction of oxygen injection pressure is close to the stable boundary,the oxidizer-fuel ratio will affect the stability in a certain extent and reducing the mixture ratio can restrain the instability.Reduction of hydrogen injection pressure has little effect on combustion stability.
Keywords:precombustion chamber  low frequency combustion instability  simulation
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