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A theoretical study of spontaneous ignition of fuel jets in an oxidizing ambient with emphasis on hydrogen jets

机译:氧化环境中燃料喷射器自燃的理论研究,重点是氢喷射

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An analysis was performed for the spontaneous ignition of a hydrogen (or other gaseous fuel) jet emanating from a slot into an oxidizing ambient (e.g., air). A similarity solution of the flow field was obtained. This was combined with the species and energy conservation equations, which were solved using activation energy asymptotics. Limits of spontaneous ignition were identified as functions of slot width, flow rate, and temperatures of the hydrogen jet and ambient gas. Two scenarios are examined: a cool jet flowing into a hot ambient and a hot jet flowing into a cool ambient. For both scenarios, ignition is favored with an increase of either the ambient temperature or the hydrogen supply temperature. Moreover, for the hot ambient scenario, a decrease in fuel Lewis number also promotes ignition. The Lewis number of the oxidizer only has a weak effect on ignition. Because spontaneous ignition is very sensitive to temperature, ignition is expected to occur near the edge of the jet if the hydrogen is cooler than the ambient gas and near the centerline if the hydrogen is hotter than the ambient gas.
机译:对从狭缝排放到氧化性环境(例如空气)中的氢气(或其他气态燃料)射流的自燃进行了分析。获得了流场的相似解。结合了物种和能量守恒方程,使用活化能渐近法对其进行了求解。确定了自发点火的极限是缝隙宽度,流速,氢射流和环境气体温度的函数。检查了两种情况:流入热环境的冷射流和流入冷环境的热射流。对于这两种情况,点火都有利于环境温度或氢气供应温度的升高。此外,在炎热的环境中,燃料路易斯数的减少也会促进点火。氧化剂的路易斯数对点火的影响很小。由于自燃对温度非常敏感,因此,如果氢气比周围环境的气体温度低,预计会在喷嘴边缘附近发生点燃,而如果氢气比周围环境的气体温度更高,则会在中心线附近发生点燃。

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