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Criterion for Detonation Transition in Liquid-Fuel Pulse Detonation Engines

机译:液体燃料脉冲爆震发动机中爆震过渡的判据

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One of the most crucial parameters for detonation transition of two-phase fuel/air mixtures is the amount of pre-vaporized fuel prior to ignition. Phase equilibrium states and droplet equilibration lifetime to achieve the phase equilibrium are calculated in an attempt to assess whether the fraction of vaporized fuel is sufficient and to establish a criterion for detonation transition of two-phase mixtures on the basis of the ratio between PDE filling time and the droplet equilibration lifetime t_f/t_e. The results show that the most important parameters which determine the critical conditions for liquid-fuel detonation are the mixture temperature and the spray droplet size. Based on the critical conditions found from experiments, a simple criterion for detonation transition of Jet A-l/air mixtures has been established. Because the DDT run-up distance of Jet A-l/ air mixture is around 40 times of the cellular width, a semiempirical equation for the criterion function of cellular width, initial droplet diameter, evaporation coefficient, and fraction of vaporized fuel at phase equilibrium state is found (see Eq. (2)).
机译:两相燃料/空气混合物的爆轰过渡的最关键参数之一是点火前的预蒸发燃料量。计算相平衡状态和达到相平衡的液滴平衡寿命,以试图评估汽化燃料的分数是否足够,并根据PDE填充时间之间的比率为两相混合物的爆轰转变建立标准液滴平衡寿命t_f / t_e。结果表明,决定液体燃料爆燃关键条件的最重要参数是混合物温度和喷雾液滴尺寸。基于从实验中发现的临界条件,已经建立了用于喷射A-1 /空气混合物的爆轰转变的简单标准。由于喷射Al /空气混合物的DDT上升距离约为泡孔宽度的40倍,因此在相平衡状态下,泡孔宽度,初始液滴直径,蒸发系数和汽化燃料分数的标准函数的半经验方程为找到(参见式(2))。

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