摘要
采用一种改进的化学非平衡流解耦方法对Euler反应流方程进行解耦处理,对流项采用五阶WENO格式进行离散,化学反应源项分别采用梯形公式和α-QSS拟稳态逼近两种方法处理,时间步进采用二阶精度的Runge-Kutta方法,对H2/O2/Ar预混气的胞格爆轰进行了二维数值模拟。两种处理方法都得到了合理的三波点结构,计算结果接近,但α-QSS拟稳态逼近处理方法的化学反应较完全,爆轰波传播速度较高;揭示了爆轰波结构的发展变化过程,横波与横波、横波与壁面碰撞引起的二次起爆对爆轰波的稳定发展至关重要;分析了数值胞格结构,胞格长宽比与参考文献基本一致,验证了本计算方法的有效性。
An improved de-coupled solver of non-equilibrium flow was used to split the Euler equations for a reacting flow.Inviscid flux was calculated with fifth-order WENO scheme.Trapezoid formula and α-QSS methods were applied to deal with the stiffness generated by the chemical reacting source term of species equations separately.Time integration was performed with two-order TVD Runge-Kutta scheme.Cellular detonation of H2/O2/Ar in a straight tube was numerically studied.Calculated results by different methods were similar,and triple point structures were analyzed.The releasing heat of chemical reaction dealt with by α-QSS method is higher than that by trapezoid formula,so the detonation wave propagating speed of α-QSS method is higher than that of trapezoid formula too.Development of cellular structure was elaborated.Due to interactions between transverse waves and between transverse wave and tube wall,re-initiation was ignited,which plays a crucial role in the propagating of detonation wave.Ratio of numerical cellular structure length to width is consistent with reference value,which indicates the feasibility of the numerical method.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2010年第5期1-6,共6页
Journal of National University of Defense Technology
基金
国家自然科学基金资助项目(90816016)