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Physical and mathematical model of detonation in aluminum gas suspensions with regard for transition processes of nanosized particle flow, heat transfer and combustion

机译:关于纳米颗粒流动,热转印和燃烧的过渡过程的铝气悬浮液中爆炸的物理和数学模型

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A physical and mathematical model of detonation of aluminum particle gas suspensions of in a wide range of particle sizes from several micrometers to tens of nanometers is presented. In the description of transport properties of particles in the flow and interphase heat transfer, the transition from the continuum regime to the free-molecular regime is considered. The description of aluminum particle combustion is based on the reduced Arrhenius-type kinetics. We take into account the transition from the diffusion type of combustion of large particles to the kinetic type for particles smaller than 1 micrometer. The reaction constants were obtained from the data of experiments on the dependence of the burning time of nano-sized particles on the temperature and pressure of the surrounding gas and the particle diameter. Examples of Chapman-Jouguet detonation structures are given. The boundaries of the applicability of the continual description of thermal dynamics in the detonation of particle suspensions in gas are determined.
机译:提出了一种从几微米到数十纳米的宽范围粒度的铝颗粒气体悬浮液的物理和数学模型。在流动和间传热中颗粒的传输性质的描述中,考虑了从连续体制度到自由分子制度的过渡。铝颗粒燃烧的描述基于降低的Arhenius型动力学。我们考虑到从大颗粒的扩散类型的燃烧到小于1微米的颗粒的动力学类型的过渡。反应常数是从实验数据中获得的关于纳米尺寸颗粒燃烧时间对周围气体的温度和压力的依赖性的数据和粒径的数据。给出了Chapman-Jouguet爆炸结构的例子。确定了在气体中颗粒悬浮液中爆炸中的热动力学不连续描述的适用性的界限。

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