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Lifted Flames On Fuel Jets In Co-flowing Air

机译:气流中的喷气燃料上的火焰升起

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The three principal theories for the stabilization of lifted flames on turbulent jets of fuel are reviewed in the light of the most recent flame imaging experiments in the literature. Most of these experiments have been conducted with a small co-flow of air, but the observations are relevant to lift-off with higher ratios of co-flowing air to fuel jet velocity. The similarity solutions for jets in co-flow are developed, and data from a variety of fluid dynamic sources are assessed to yield the governing parameters for mean flow, turbulence and mixture fraction. New data for lifted flames on a methane jet in diffusing streams of co-flowing air are then presented. These data provide essential information on the intermittency, and on the properties of the jet conditioned on the presence of turbulent fluid. However, the co-flow lifts the flame to stabilize in better-mixed regions than in its absence. The 'premixture' model is confirmed for this situation, in which the lift-off heights were more than 20 jet diameters and where there is little intermittency at the stabilization radius. Nevertheless, mixing data for this geometry in the absence of a flame show that, with lift-off heights less than 20 jet diameters, the base of the flame would have been in the outer regions of the jet where the mixture of fuel in air only reaches stoichiometric proportions intermittently, with the passage of large eddies. Trading on many papers from the recent literature where this was the case, both experimental and computational insights as to the processes in this region are reviewed. A question remains about how ignition is maintained in these experiments with low turbulent lift-off. It is hypothesized that the mechanism is the diffusive heating of the slowly moving surrounding air which then provides an energy store for the incoming eddies. Further time-resolved observations of reaction zone and high temperature gas structure are required to test this model.
机译:根据文献中最新的火焰成像实验,对稳定湍流燃料喷射火焰的三种主要理论进行了综述。这些实验大多数是在少量的气流共同进行的情况下进行的,但这些观察结果与较高的气流与燃料喷射速度之比的升空有关。开发了并流射流的相似性解决方案,并评估了来自各种流体动力源的数据,以得出平均流量,湍流和混合比的控制参数。然后提供了在甲烷射流中扩散的并流空气流中燃烧的火焰的新数据。这些数据提供了有关间歇性以及在湍流存在下调节的射流特性的基本信息。但是,与没有火焰时相比,同流使火焰在混合效果更好的区域稳定下来。在这种情况下可以确认“预混料”模型,在该模型中,升空高度大于20个喷嘴直径,并且稳定半径的间歇性很小。但是,在没有火焰的情况下,这种几何形状的混合数据表明,在升空高度小于20个喷嘴直径的情况下,火焰的基础将位于喷嘴的外部区域,在该区域中仅燃料与空气的混合物随着大涡流的通过,间歇地达到化学计量比。在这种情况下,利用近期文献中的许多文章进行交易,对有关该区域过程的实验和计算见解进行了回顾。在这些实验中如何以低湍流升力保持点火仍然存在问题。假设该机理是缓慢移动的周围空气的扩散加热,然后为传入的涡流提供能量存储。需要更多时间分辨的反应区和高温气体结构观察来测试该模型。

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