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Experimental investigation of the stochastic nature of end-gas autoignition with detonation development in confined combustion chamber

机译:密闭燃烧室中具有爆轰发展的终端气体自燃随机性的实验研究

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In the present work, end-gas autoignition formation, and the effects of oxygen concentration on the flame/shock waves propagation and pressure oscillation, are investigated in a self-designed constant-volume chamber equipped with a perforated plate. A hydrogen-oxygen-nitrogen mixture with adjustable oxygen to nitrogen ratio is chosen as the test fuel. In an oxygen-enriched condition, the probability of an end-gas autoignition occurrence increases significantly. End-gas autoignition with detonation development is further investigated, with a special emphasis on the stochasticity of the detonation development. In a low-oxygen condition, detonation occurs randomly owing to its stochastic physical behavior. However, when the oxygen concentration increases to 28%, the stochastic factors have a lower impact, and the detonation occurrence is certain. Nevertheless, the pressure and pressure oscillation in the autoignition exhibit random behaviors and are unrelated to the oxygen concentration. The variation tendency of the flame tip velocity remains constant under different oxygen concentrations. However, an increase in the oxygen concentration improves the flame tip velocity, thereby inducing stronger shock waves and promoting autoignition. Based on the start time of the autoignition, two types of autoignition modes were identified: Mode 1 and Mode 2. 1n Mode 2, the unburnt mixture experiences merely one compression by the shock wave before autoignition and only occurs under high oxygen concentrations of 27-28%. Under equal oxygen concentrations, the pressure and pressure oscillation of Mode 2 are higher than those of Mode 1 owing to the larger amount of unburnt mixture. Finally, the exhaust gas was introduced into the initial unburnt mixture to investigate the effect of an inert gas on the combustion. (C) 2019 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:在目前的工作中,在配有多孔板的自行设计的恒容室中研究了最终气体的自燃形成以及氧气浓度对火焰/冲击波传播和压力振荡的影响。选择氧氮比可调的氢-氧-氮混合物作为测试燃料。在富氧条件下,发生末端气体自燃的可能性大大增加。进一步研究了具有爆炸发展的终端气体自燃,特别着重于爆炸发展的随机性。在低氧条件下,由于其随机的物理行为,爆炸会随机发生。但是,当氧气浓度增加到28%时,随机因素的影响较小,并且一定会发生爆炸。然而,自燃中的压力和压力振荡表现出随机行为,并且与氧浓度无关。在不同的氧气浓度下,火焰尖端速度的变化趋势保持恒定。但是,氧浓度的增加会改善火焰尖端的速度,从而引起更强的冲击波并促进自燃。根据自燃开始时间,确定了两种类型的自燃模式:模式1和模式2。1n模式2,未燃烧的混合物在自燃之前仅受到冲击波的一次压缩,并且仅在高氧浓度27- 28%。在相同的氧气浓度下,由于大量未燃烧的混合物,模式2的压力和压力振荡高于模式1。最后,将废气引入初始未燃烧混合物中,以研究惰性气体对燃烧的影响。 (C)2019燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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