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非平衡流解耦方法及其计算激波诱导燃烧的应用验证
引用本文:孙明波,梁剑寒,王振国.非平衡流解耦方法及其计算激波诱导燃烧的应用验证[J].航空动力学报,2008,23(11):2055-2061.
作者姓名:孙明波  梁剑寒  王振国
作者单位:国防科技大学 航天与材料工程学院, 长沙 410073
摘    要:介绍并发展了一种改进的化学非平衡流动解耦方法.将流动控制方程与化学反应生成源项解耦处理,组分对流项的矢通量分裂基于流动方程密度对流项的分裂形式给出.对流项采用五阶WENO格式求解,化学反应源项的刚性采用简化的隐式方法进行处理.将该方法应用于预混H2/O2和H2/Air激波诱导燃烧计算,得到的定常及非定常燃烧过程与实验观测相符,振荡频率与实验测量较吻合,结果表明该方法应用于多组分多步反应流计算是可行的. 

关 键 词:激波诱导燃烧    非平衡流    解耦方法    WENO格式
收稿时间:11/1/2007 3:34:31 PM
修稿时间:2008/5/15 0:00:00

Validation of an uncoupled solver of non-equilibrium flow for shock-induced combustion
SUN Ming-bo,LIANG Jian-han and WANG Zhen-guo.Validation of an uncoupled solver of non-equilibrium flow for shock-induced combustion[J].Journal of Aerospace Power,2008,23(11):2055-2061.
Authors:SUN Ming-bo  LIANG Jian-han and WANG Zhen-guo
Institution:College of Aerospace and Materials Engineering, National University of Defense Technology, Changsha 410073, China
Abstract:An improved uncoupled solver of non-equilibrium flow was introduced and developed in this study.The splitting of convective species flux was uncoupled from the N-S equations and based on the splitting result of the convective density flux.Inviscid flux was calculated with fifth-order weighted essentially non-oscillatory scheme.Simplified implicit formulation was adopted to deal with the stiffness generated by the chemical reacting source term of every separate species equation.Shock-induced combustion pheno...
Keywords:shock-induced combustion  non-equilibrium flow  uncoupled solver  WENO(weighted essentially non-oscillatory) scheme  
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