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Regimes of High-Speed Hydrogen Flame Propagation in Channels: Classification and Criteria of Realization

机译:通道中高速氢火焰传播的制度:分类和实现标准

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The paper discusses high-speed combustion regimes inside confined volumes on the example of hydrogen-containing gaseous mixtures. A unified description of high-speed combustion regimes is proposed on the basis of systematic analysis of flame evolution. The stage of the so-called chocked flame is shown to be the necessary step on the way to the formation of high-speed flames and detonation. Further flame evolution could proceed in different ways including quasi-steady transonic flame, deflagration-to-detonation transition or sequential auto-ignitions ahead of the primary flame front. The paper proposes a method for estimation of probability of different devastating highspeed combustion regimes, including detonation, relying only on the mixture composition and its initial thermodynamic state. Herewith, since in the process of flame acceleration inside confined volume the compression is yielded by the series of compression waves, the initial state and the state corresponded to the high-speed stage of flame propagation could be related via Hugoniot adiabat. The conducted parametric study of hydrogen flames allowed obtaining criteria according to which the possibility of one or another regime of high-speed combustion can be estimated. The obtained results correlate well with the experimental data on the different high-speed regimes taking place in hydrogen-air mixtures, stoichiometric hydrogen-oxygen, and equimolar hydrogen-oxygen mixtures. It is shown that to assess the probability of detonation onset in obstructed channels, the proposed technique is not enough and one should apply it together with the geometrical criteria. Results obtained with combined technique agree well with the available data on the criteria of deflagration-to-detonation transition in hydrogen-air mixtures of different compounds.
机译:本文以含氢气体混合物为例,讨论了密闭空间内的高速燃烧方式。在对火焰演变进行系统分析的基础上,提出了对高速燃烧状态的统一描述。事实证明,所谓的cho塞火焰阶段是形成高速火焰和爆炸的必经步骤。进一步的火焰发展可能会以不同的方式进行,包括准稳定的跨音速火焰,爆燃-爆轰过渡或在主火焰前沿之前的顺序自燃。本文提出了一种仅依赖于混合气成分及其初始热力学状态来估计包括爆轰在内的不同破坏性高速燃烧方式的可能性的方法。因此,由于在有限体积内的火焰加速过程中,压缩是通过一系列压缩波产生的,因此初始状态和对应于火焰传播的高速阶段的状态可以通过Hugoniot绝热体来关联。对氢火焰进行的参数研究允许获得标准,据此可以估计一种或另一种高速燃烧方式的可能性。获得的结果与氢气-空气混合物,化学计量氢-氧气和等摩尔氢-氧气混合物中发生的不同高速方式下的实验数据很好地相关。结果表明,要评估在阻塞通道中起爆的可能性,所提出的技术是不够的,应该将其与几何准则一起应用。组合技术获得的结果与有关不同化合物的氢-空气混合物中的由爆燃到爆轰过渡的标准的可用数据非常吻合。

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