幂律型燃料/空气气液两相爆轰的数值计算
首发时间:2012-12-20
摘要:为研究幂律型非牛顿流体燃料/空气混合物两相燃烧转爆轰过程,建立了幂律燃料和空气混合物气液两相爆轰控制方程,并运用守恒元与求解元数值计算方法编程求解了流动指数分别为0.75,1和1.25时爆轰管内的燃烧转爆轰过程。计算结果表明,幂律型非牛顿流体燃料/空气爆轰过程中,液滴半径依次经历了激波诱导反应,液滴反应加速和液滴完全反应三个变化过程。流动指数对液滴半径经历的三个变化过程均有影响,对液滴反应加速过程的影响最为明显。随着流动指数增大,燃烧转爆轰时间缩短,燃烧转爆轰距离变短,爆轰压力减小,爆轰波速度减小。计算结果对幂律流体类燃料的应用有一定参考意义。
关键词: 爆炸力学 燃烧转爆轰 幂律流体 CE/SE方法 数值模拟
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Numerical Simulation of Two Phase Detonation with Power-Law Model Fuel and Air
Abstract:In order to investigate the impact of fluid component on process of two phase deflagration to detonation transition about energetic liquids obey to power-law non-newtonian fluid and air mixture. The control equations of two phase detonation were established considering the influence of shear rate on viscosity, and solved by CE/SE method. Numerical simulation was done based on the equations for the deflagration to detonation process of gas and liquids mixture with fluid component equal to 0.75, 1 and 1.25 separately. The results show that radius of liquid experiences shock induced stage, the accelerate stage and the react completely stage in turn. Each stage is affected by fluid component, especial for the accelerate stage. With the fluid component increases, the time and distance of deflagration to detonation transition become shorter, the pressure and velocity of detonation wave become smaller. The calculation results have some significance references for application of power-law type fuels.
Keywords: explosion mechanics deflagration to detonation transition power-law fluids ce/se method numerical simulation
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