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Shock wave and flame front induced detonation in a rapid compression machine

机译:快速压缩机中的冲击波和火焰前诱导爆轰

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摘要

The present study focuses on one mode of detonation initiation observed in a rapid compression machine (RCM). This mode is referred to as shock wave and flame front-induced detonation (SWFID). Experimental high-speed imaging and two-dimensional numerical simulations with skeletal chemistry are combined to unravel the dominant steps of detonation initiation under SWFID conditions. It is shown that the interaction between the shock wave generated by the end-gas auto-ignition and the spherical flame creates a region of high pressure and temperature which enables the acceleration of the flame front and the detonation onset. The experimental observation lacks adequate spatial and temporal resolution despite good reproducibility of the detonation onset. Based on the numerical results, phenomenological interpretation of the event within the framework of shock wave refraction indicates that the formation of a free-precursor shock wave at the transition between regular and irregular refraction may be responsible for detonation onset. The present results along with previous findings on shock wave reflection-induced detonation in the RCM indicate that super-knock occurs after the interaction of the shock wave generated by end-gas auto-ignition with the RCM walls, preignition flame, or another shock wave.
机译:本研究重点介绍在快速压缩机(RCM)中观察到的一种爆轰起始。该模式被称为冲击波和火焰前诱导的爆炸(SWFID)。实验高速成像和具有骨骼化学的二维数值模拟,组合以在SWFID条件下解开爆轰起始的主要步骤。结果表明,由最终气体自动点火和球形火焰产生的冲击波之间的相互作用产生高压和温度的区域,这使得火焰前部和爆炸发作的加速度。尽管爆炸发作的良好再现性,但实验观察缺乏足够的空间和时间分辨率。基于数值结果,冲击波折射框架内的事件的现象学解释表明,在常规和不规则折射之间的过渡处形成自由前体冲击波可能是负责爆炸发作的负责。本结果以及在RCM中的冲击波反射诱导的引起的先前发现表明,在通过RCM壁的最终气体自动点火的冲击波相互作用之后发生超爆发,与RCM墙壁,通信火焰或另一个冲击波相互作用。

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