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带凹腔的支板火焰稳定器三维大涡模拟
引用本文:邹咪,金捷,王旭东.带凹腔的支板火焰稳定器三维大涡模拟[J].航空动力学报,2017,32(3):607-613.
作者姓名:邹咪  金捷  王旭东
作者单位:北京航空航天大学 能源与动力工程学院,北京 100191
摘    要:为研究支板冷态流场,应用LES(大涡模拟)的方法对带凹腔的支板火焰稳定器在Ma=0.06和 Ma=0.09两种工况下分别进行三维数值模拟.对比试验和仿真结果表明:三维大涡模拟结果具有与试验相似的流场结构,定量对比试验和LES结果的尾涡脱落频率的最大相对误差为9.4%;支板尾部截面流向时均速度的最大相对误差为7.7%.表明数值模拟方法和边界条件设置的正确性和可信度.又对支板的三维流场进行分析:速度越大,支板尾涡的尺寸和强度越大;支板流场存在明显的三维效应,并且随着速度变大,三维效应越明显. 

关 键 词:加力燃烧室    支板    凹腔    大涡模拟    尾涡    三维效应
收稿时间:2015/7/2 0:00:00

Three-dimensional large eddy simulation of strut flame-holder with cavity
ZOU Mi,JIN Jie,WANG Xu-dong.Three-dimensional large eddy simulation of strut flame-holder with cavity[J].Journal of Aerospace Power,2017,32(3):607-613.
Authors:ZOU Mi  JIN Jie  WANG Xu-dong
Abstract:In order to study the cold flow field of strut,three-dimensional LES (large eddy simulation) of strut flame-holder with cavity at Ma =0.06 and Ma =0.09 was carried out respectively.The simulation results were compared with experiment data.It showed that the flow field structure of three-dimensional LES was similar with that of experiment.What's more,two quantitative comparisons in the frequency of wake vortex and time-averaged stream-wise velocity on strut rear section were made.And the maximum relative errors were 9.4% and 7.7% respectively,proving that the model of numerical calculation at boundary conditions was correct and believable.Then by analyzing the three-dimensional flow field of strut,a conclusion that the faster velocity means the bigger size and intensity of wake vortex.Besides,the result of three-dimensional LES shows an obvious phenomenon of three-dimensional effect which gets stronger when the velocity gets faster.
Keywords:after-burner  strut  cavity  large eddy simulation  wake vortex  three-dimensional effect
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