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富氢/富氧燃气同轴气-气喷嘴燃烧性能仿真与分析
引用本文:李茂,杜正刚,金平,蔡国飙.富氢/富氧燃气同轴气-气喷嘴燃烧性能仿真与分析[J].航空动力学报,2010,25(4):835-840.
作者姓名:李茂  杜正刚  金平  蔡国飙
作者单位:北京航空航天大学,宇航学院,北京,100191
摘    要:为研究全流量补燃循环发动机富氢/富氧燃气气-气喷嘴性能,以758 K的富氢燃气为燃料、676 K的富氧燃气为氧化剂,对采用同轴直流喷嘴、氧喷嘴扩张同轴喷嘴、氢喷嘴收缩同轴喷嘴、氧喷嘴中心具有实心圆柱同轴喷嘴、双同轴直流喷嘴的燃烧室的燃烧流场进行了数值模拟,并考察了流量对燃烧性能的影响.仿真结果表明双同轴直流喷嘴具有最好的燃烧性能.数值模拟结果对富氢/富氧燃气气-气喷注器设计有参考价值.

关 键 词:全流量补燃循环  燃烧性能  富氢/富氧燃气  气-气喷嘴  仿真
收稿时间:2009/4/18 0:00:00
修稿时间:10/9/2009 8:49:20 AM

Simulation and analysis on combustion performance of hydrogen-rich/oxygen-rich gas-gas coaxial injectors
LI Mao,DU Zheng-gang,JIN Ping and CAI Guo-biao.Simulation and analysis on combustion performance of hydrogen-rich/oxygen-rich gas-gas coaxial injectors[J].Journal of Aerospace Power,2010,25(4):835-840.
Authors:LI Mao  DU Zheng-gang  JIN Ping and CAI Guo-biao
Institution:Beihang University
Abstract:In order to investigate the performance of the hydrogen-rich/oxygen-rich gas-gas injector in the full flow staged combustion (FFSC) engine, the combustion flow field of a shear coaxial injector, a coaxial injector of the oxidizer injector with expansion angle, a coaxial injector of the fuel injector with contraction angle, a coaxial injector of the oxidizer injector with a column in the center and a shear tri-coaxial injector were simulated. The propellant of the injectors was hydrogen-rich gas in temperature of 758K and oxygen-rich gas in temperature of 676K. The results of the numerical simulation show that the shear tri-coaxial injector has the best combustion performance. The results can provide the reliable criterion for the design and experiment of hydrogen-rich/oxygen-rich gas-gas injector.
Keywords:full flow staged combustion  combustion performance  hydrogen-rich/oxygen-rich gas  gas-gas injector  simulation
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