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Analytical and numerical study of near-field ignition of H_2/air by injection of hot gas

机译:热气注入H_2 /空气近场点火的分析与数值研究

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Ignition initiation by a turbulent hot jet involves complex transport and chemical processes with disparate and sensitive time scales. Its understanding is important for improved ignition in advanced and novel combustion engines and in ignition avoidance for explosion safety measures. This study is aimed at the modeling of turbulent hot jet ignition of stoichiometric hydrogen-air mixture with fast chemistry and short chemical time scales relative to the large-scale mixing time scales. The evolution of jet mixture fraction in the near-field shear layer of a suddenly-starting turbulent jet is analytically modeled and calibrated by large-eddy simulation of the reacting fluid. When integrated with a correlation for instantaneous chemical induction time, the model estimates the radial location and the timing of ignition as the jet travels in the streamwise direction. The estimation includes accounting for the role of the scalar dissipation rate in the suppression of ignition. The radial location of ignition migrates towards the jet centerline with time, migrating faster for higher injection temperatures and much slower for leaner ambient fuel-air ratios. The limitations of the present model are investigated by assessing the regions of mixing layer where strong diffusive transport collocates with the high production rate of active radicals. To complete the perspective into analytic modeling of transient jet ignition, other limitations associated with turbulent fluctuations and jet composition are discussed, as well as the role of near-field ignition relative to ignition at the jet tip or head vortex ring. (C) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:湍流热喷射的点火开始涉及复杂的运输和化学过程,具有不同和敏感的时间尺度。其理解对于改善先进和新型燃烧发动机的点火和爆炸安全措施的点火避免,这是一个重要的。该研究旨在采用快速化学和短化学时间尺度的快速化学和短化学时间尺度的湍流热喷射点火的建模。通过对反应流体的大涡流模拟进行分析建模和校准突出开始的湍流射流的近场剪切层中的喷射混合物级分的演变。当与瞬时化学诱导时间的相关性集成时,模型估计当射流在流动方向上行进时,径向位置和点火的定时。估计包括核对标量耗散率在抑制点火方面的作用。点火的径向位置随时间迁移到喷射中心线,迁移更快的注射温度,更慢的环境燃料空气比率较慢。通过评估混合层的区域,以强大的扩散运输与活性自由基的高生产率脱离的汇编,研究了本模型的局限性。为了完成瞬态喷射点火的分析建模的视角,讨论了与湍流波动和喷射组合物相关的其他限制,以及近场点火相对于喷射尖端或头涡环的点火的作用。 (c)2020燃烧研究所。由elsevier Inc.出版的所有权利保留。

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