摘要
在欧拉-拉氏体系中,在传统点源两相湍流燃烧模型(TM)中考虑液滴带火燃烧状态,提出全状态两相湍流燃烧模型(FSM),并用甲醇-空气两相湍流射流火焰实验数据对两种模型进行检验,对比结果表明:FSM模型能够给出平均温度的双峰分布,得到更合理的预报结果.
In Euler-Lagrange frame,the individual droplet burning behavior was added into the traditional point source two phase turbulent combustion model(TM),and then a full status two phase turbulent combustion model(FSM) was presented.The two kinds of two phase turbulent combustion models were tested by a set of methanol air two phase turbulent spray jet flame experimental data.The comparison results between the computational prediction results and the experimental data show that the FSM model can give two peaks in the averaged temperature profile,as well as more reasonable predictions.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2012年第10期2200-2204,共5页
Journal of Aerospace Power
基金
国家自然科学基金(51106006)
英国皇家学会基金(AL120003)
关键词
液雾燃烧
单油滴燃烧
火焰结构
湍流燃烧模型
大涡模拟
spray combustion
single droplet combustion
flame structure
turbulent combustion model
large eddy simulation