摘要
在研究混合气体燃烧中产生的爆震波传播机理的基础上,应用特征线法对爆震波在爆震燃烧室内的传播过程进行了数值模拟,为分析脉冲爆震发动机的工作原理、性能计算与分析及实验研究提供理论依据。
On the basis of investigating the propagation mechanism of detonation wave produced in combustion of mixing gas,the numerical simulation on propagation process of detonation wave in detonation combustion chamber was made by applying characteristic method.This can provide theoretical base for analyses of operating principle and calculation of performance as well as experimental investigation of pulsed detonation engine.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1998年第6期70-73,共4页
Journal of Propulsion Technology
基金
国家自然科学基金
"八六三"资助研究项目
关键词
爆震波
燃烧室
传播速度
特征曲线
航空发动机
Detonation wave +,Combustion chamber,Propagation velocity,Characteristic curve,Numerical simulation