摘要
本文在大尺度(D=50.3mm,63.5mm)光滑管道内对四种预混气(2H_(2)+O_(2)+50%Ar,C_(2)H_(2)+2.5O_(2)+70%Ar,C_(2)H_(2)+2.5O_(2)+85%Ar,CH_(4)+2O_(2))进行了爆轰实验研究;获得了爆轰极限Pc和胞格尺寸λ,分析了四种气体的不稳定性,计算了边界层位移厚度δ^(*)和诱导长度Δ_(i),深入研究了管径和气体性质对爆轰极限的影响。实验结果表明:随着初始压力和管径的减小,边界层位移厚度增大,边界效应加强,热损失增多,爆轰临界压力变大;大尺度管道内,不稳定性对极限的影响占据主导,因此极限情况下不稳定气(CH_(4)+2O_(2))符合判据λ=πD,稳定气(2H_(2)+O_(2)+50%Ar,C_(2)H_(2)+2.5O_(2)+70%Ar,C_(2)H_(2)+2.5O_(2)+85%Ar)则不符合;四种预混气的诱导长度均随初始压力增大而减小,2H_(2)+O_(2)+50%Ar和其余三种碳氢燃料混合气的胞格尺寸可分别用λ=52.07Δ_(i)、λ=19.6Δ_(i)预测;边界效应对诱导长度有影响,边界层位移厚度与诱导长度呈正比关系。
In this paper,an experimental study on the detonation of four premixed mixtures(2H_(2)+O_(2)+50%Ar,C_(2)H_(2)+2.5O_(2)+70%Ar,C_(2)H_(2)+2.5O_(2)+85%Ar,CH_(4)+2O_(2))is carried out respectively in large-scale(D=50.3 mm,63.5 mm)smooth tubes.The detonation limits and cell sizes A are obtained,and the instability of four mixtures is analyzed.Moreover,the boundary layer displacement thickness*and induction length;are calculated.Based on these,the effects of tube diameter and gas properties on detonation limit is studied deeply.The experimental results unfold that with the decrease of initial pressure and tube diameter,the boundary layer displacement thickness increases,so the boundary effect and the heat loss increase,ultimately leading the detonation critical pressure increases.In large-scale tubes,the influence of instability on the limit dominates,so in the limit case,the unstable mixture(CH_(4)+2O_(2))meets the criterion λ=πD,the stable mixtures(2H_(2)+O_(2)+50%Ar,C_(2)H_(2)+2.5O_(2)+70%Ar,C_(2)H_(2)+2.5O_(2)+85%Ar)do not.The induction lengths of four mixtures all decrease with the increase of the initial pressure.The cell sizes of 2H_(2)+O_(2)+50%Ar and the other three hydrocarbon fuel mixtures can be predicted throughλ=52.07Δ_(i);andλ=19.62Δ_(i),respectively.Finally,the boundary effect has an influence on the induction length,and the displacement thickness of the boundary layer is proportional to the induction length.
作者
赵焕娟
刘克庆
张英华
刘婧
林伟
杨连枝
高娜
ZHAO Huanjuan;LIU Keqing;ZHANG Yinghua;LIU Jing;LIN Wei;YANG Lianzhi;GAO Na(College of Civil and Resource Engineering,University of Science and Technology Beijing,Beijing 100083,China;Department of Aerospace Science and Technology,Spacing Engineering University,Beijing 101416,China)
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
2023年第7期2020-2029,共10页
Journal of Engineering Thermophysics
基金
国家重点研发计划重点专项(No.2018YFC0810606-02)
中央高校基本科研专项资金(No.FRF-MP-20-20,No.FRF-TP-19-020A3)
河南省瓦斯地质与瓦斯治理重点实验室开放基金(No.WS2020A03)。
关键词
爆轰极限
管径
胞格尺寸
不稳定性
诱导长度
detonation limits
tube scale
cell size
instability
induction length