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.
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 fields of the combustors with a shear coaxial injector,a coaxial injector for the oxidizer injector with expansion angle,a coaxial injector for the fuel injector with contraction angle,a coaxial injector for the oxidizer injector with a column in the center and a shear dual-coaxial injector were simulated.The propellant of the injectors was hydrogen-rich gas in temperature of 758 K and oxygen-rich gas in temperature of 676 K.The results of the numerical simulation show that,the shear dual-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.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2010年第4期835-840,共6页
Journal of Aerospace Power
基金
国家863基金
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
full flow staged combustion
combustion performance
hydrogen-rich/oxygen-rich gas
gas-gas injector
simulation