Investigation of Afterburning Effects on the Thermal Environment of Flame Deflectors

2021 7th International Conference on Mechanical Engineering and Automation Science (ICMEAS)(2021)

引用 0|浏览2
暂无评分
摘要
In this paper, a four-nozzle liquid oxygen (LOX)/kerosene rocket is used to analyse the afterburning effects on the thermal environment of flame deflectors. Based on the three-dimensional compressible Reynolds-Averaged Navier-Stokes (RANS) equations and the realizable k-ε turbulence model, the rocket plume model is established. A 9-species,10-steps chemistry scheme is used for the simulation of af...
更多
查看译文
关键词
Heating systems,Rockets,Solid modeling,Liquids,Chemistry,Computational fluid dynamics,Fires
AI 理解论文
溯源树
样例
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要