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Numerical Investigation of Pre-detonators for Pulse Detonation Engines

机译:脉冲爆炸发动机前雷管预雷管的数值研究

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A parametric study was performed to determine optimal geometries to allow the successful transition of a detonation from a pre-detonator into the main detonation tube of a pulse detonation engine. The study was performed using a two-dimensional Euler solver with progress variables to model the chemistry. The geometrical configuration for the simulations included a pre-detonator that expanded into the main tube as well as a flat plate to divert the flow. A study of plate height and distance from the expansion was done to determine which flat plate geometries transitioned the detonation from the pre-detonator to the main tube. Both successful and unsuccessful geometries were discovered, but further examination showed that the success of a transition was dependent upon where the expansion occured with respect to the structure of the detonation wave. The consequences of this is that the probability of success given a particular geometry is the desired goal of any simulation to develop successful pre-detonators.
机译:进行参数学研究以确定最佳几何形状,以允许从预雷管中的爆炸转变到脉冲爆震发动机的主爆震管中。使用二维欧拉求解器进行该研究,其中具有进展变量来模拟化学。用于模拟的几何配置包括将延伸到主管的预雷管以及平板以转移流量。对板高度和距离膨胀的距离进行了研究,以确定哪个平板几何形状从预抛管器转移到主管的爆炸。发现了成功和不成功的几何形状,但进一步检查表明,过渡的成功取决于相对于爆炸波的结构发生的膨胀。这样做的结果是,给定特定几何形状的成功概率是开发成功预防器的任何模拟的所需目标。

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