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[1]李 强,聂 嵩,刘业奎,等.过氧化氢/煤油发动机推力室气液燃烧数值模拟[J].火箭推进,2011,37(04):35-39.
　LI Qiang,NIE Song,LIU Ye-kui,et al.Numerical simulation of combustion characteristicsfor thrust chamber in hydrogen peroxide/kerosene engine[J].Journal of Rocket Propulsion,2011,37(04):35-39.
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过氧化氢/煤油发动机推力室气液燃烧数值模拟

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年04期 页码: 35-39 栏目: 研究与设计 出版日期: 2011-08-15
Title:
Numerical simulation of combustion characteristics for thrust chamber in hydrogen peroxide/kerosene engine
文章编号:
1672-9374(2011)04-0035-05
作者:
李 强; 聂 嵩; 刘业奎; 潘 亮; 马梦颖
北京航天动力研究所，北京 100076
Author(s):
LI Qiang;  NIE Song;  LIU Ye-kui;  PAN Liang;  MA Meng-ying
Beijing Aerospace Propulsion Institute, Beijing 100076, China
关键词:
过氧化氢发动机; 推力室; 燃烧; 数值模拟
分类号:
V434-34
文献标志码:
A
摘要:
采用离散相模拟颗粒随机轨道方法处理两相流动，采用SST k-ω湍流模型，利用燃料的单步总反应模型模拟煤油蒸汽燃烧，针对过氧化氢/煤油发动机推力室，进行三维两相燃烧数值模拟。对推力室的总体流场特征及性能进行了初步研究，为开展进一步的数值研究奠定基础。
Abstract:
The gas-liquid combustion and flow field in HTP/kerosene engine thrust chamber were numerically simulated in the paper. Discrete phase modeling (DPM) and SST k-ω turbulence model were used to simulate the kerosene gas-liquid flow and turbulence respectively. A one-step general reaction model of fuel was employed to simulate the kerosene vapour combustion. The combustion flow field and performance parameters of the combustion chamber were numerically investigated. A foundation for the further numerical research was established in this paper.

参考文献/References:

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备注/Memo

收稿日期：2010-11-24；修回日期：2011-04-20
基金项目：中国航天科技集团公司支撑项目
作者简介： 李强（1981—），男，工程师，博士，研究领域为液体火箭发动

更新日期/Last Update: 1900-01-01