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An asymptotic analysis of spontaneous ignition of hydrogen jets

机译:氢射流自燃的渐近分析

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Analytical work is presented for the spontaneous ignition of a hydrogen jet emanating from a slot into 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 air. 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 predicted to occur near the edge of the jet if the hydrogen is cooler than the air and on the centerline if the hydrogen is hotter than the air.
机译:提出了用于自燃从狭缝排放到空气中的氢射流的自发分析工作。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。自燃极限被确定为缝隙宽度,流速,氢射流和周围空气温度的函数。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,环境温度或氢气供应温度的升高都有利于点火。此外,在炎热的环境中,燃料路易斯数的减少也会促进点火。氧化剂的路易斯数仅对点火有弱的影响。由于自燃对温度非常敏感,因此,如果氢比空气冷,则预计会在喷嘴边缘附近着火,而如果氢比空气更热,则会在中心线上点燃。

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