摘要
为对液体火箭发动机羽流光谱实验数据进行定量分析 ,通过建立高温气体下辐射传递模型 ,对1 Cr1 8Ni9Ti的理论光谱进行了仿真计算。结果表明 ,在路径一定的情况下 ,羽流中原子浓度较低时 ,可采用光学薄模型 ,原子浓度较高时 。
Based on the quantitative analysis of exhaust plume spectral experimental data,a radiative transport theory for high temperature gas was developed. The result of simulation for 1Cr18Ni9Ti in the plume was represented. The results indicate that while the length is equal, optically thin model is fit for lower concentration and optically thick model for upper situations.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2000年第2期15-18,共4页
Journal of Propulsion Technology
关键词
羽流
光谱测量
数值仿真
液体火箭发动机
Liquid propellant rocket engine
Plume
Spectral measurement
Optical thickress
Atomic spec-troscopy
Numerical simulation