首页 | 本学科首页   官方微博 | 高级检索  
     检索      

某蒸发式稳定器燃烧特性及供油匹配数值研究
引用本文:丁兆波,金捷.某蒸发式稳定器燃烧特性及供油匹配数值研究[J].火箭推进,2012,38(4):43-48.
作者姓名:丁兆波  金捷
作者单位:1. 北京航天动力研究所,北京,100076
2. 北京航空航天大学航空发动机数值仿真中心,北京,100191
基金项目:中国航天科技集团公司支撑项目(2009JY06)
摘    要:为了研究一种适用于亚燃冲压发动机燃烧室的蒸发式火焰稳定器方案,采用PDF燃烧模型对其燃烧特性及供油匹配进行了流动及两相燃烧数值模拟与分析,重点研究了不同主燃区/局部供油匹配以及不同主燃区供油浓度分布等对燃烧性能的影响,获得了燃气温度峰值与均匀性相对优化的供油方案。

关 键 词:冲压燃烧室  蒸发式稳定器  燃烧特性  供油匹配  数值研究

Numerical investigation on combustion characteristics and fuel supply matching for an evaporative flame-holder
DING Zhao-bo,JIN Jie.Numerical investigation on combustion characteristics and fuel supply matching for an evaporative flame-holder[J].Journal of Rocket Propulsion,2012,38(4):43-48.
Authors:DING Zhao-bo  JIN Jie
Institution:1. Beijing Aerospace Propulsion Institute, Beijing 100076, China; 2. Aero-engine Numerical Simulation Research Center, BUAA, Beijing 100191, China)
Abstract:To study an evaporative flame-holder suitable for the ramjet combustor, the numerical simulation and analysis of two-phase combustion flow field for combustion characteristics and the fuel supply matching was carried out based on PDF combustion model. The influence of different main combustion zone / local fuel-feeding matching and fuel-feeding density distribution in different main combustion zone on the combustion performance were studied emphatically. An optimization fu- el-feeding scheme for peak value and uniformity of gas temperature were obtained. The calculation result of the scheme is rational. It has an important significance for the optimization design for the fuel-feeding scheme of the evaporative flame-holder.
Keywords:ramjet combustor  evaporative stabilizer  combustion characteristic  fuel supply matching  numerical investigation
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号