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CFD Analysis for an Overpressure Buildup Phenomenon of SRI Hydrogen Explosion Test at Fuel Lean and Fuel Rich Conditions in an Open Space

机译:燃料瘦燃料益氢爆炸试验超压累积现象的CFD分析,燃料富裕条件

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A computational fluid dynamics (CFD) calculation for a hydrogen explosion test with a complicated obstacle tube geometry of pitch 21.3 mm and diameter 99.1 mm at fuel lean and fuel rich conditions was performed to establish a CFD analysis methodology for a hypothetical hydrogen explosion accident between a very high temperature reactor (VHTR) and a hydrogen production facility. We firstly developed the CFD analysis methodology with an error range of about ±34% at the hydrogen stoichiometric condition on the basis of SRI's hydrogen explosion test results. The proposed CFD analysis methodology consisted of the standard k-ε turbulent model for a turbulent flow, eddy dissipation model (EDM) constants of A=10 and B=0.8 for a combustion flow, a time step size of 0.01 ms with backward Euler 2nd order for a transient flow and a cell length of 10 mm around the obstacle tube approximately equaled to a large length scale of eddy. A spark ignition model was developed to simulate a high ignition energy of 40 J induced by an electric device for 2 ms in the hydrogen explosion test based on an energy conservation law. However, the EDM model constants of A=10 and B=0.8 was modified to A=7 and B=0.8 for the fuel lean and fuel rich conditions because the main idea of the turbulence mixing rate in the EDM cannot cover the variation of combustion energy due to the hydrogen concentration difference from the stoichiometric condition to the fuel lean or fuel rich conditions. The calculated error range of the CFD analysis methodology was about ±7% from the simulation results of SRI's hydrogen explosion test at the fuel lean and fuel rich conditions. Therefore, it is known that a CFD analysis with the EDM may be used as an accurate evaluation tool to predict overpressure buildup if the EDM constants may be properly chosen according to the hydrogen concentration.
机译:进行计算流体动力学(CFD)计算氢气爆炸试验的耐螺距21.3mm和直径为99.1mm,富含燃料浓度的耐燃料和富含条件,以建立一个CFD分析方法,用于A之间的假设氢爆炸事故非常高的温度反应器(VHTR)和氢气生产设施。我们首先在SRI的氢爆炸试验结果的基础上开发了CFD分析方法,误差范围为氢化学计量条件约为±34%。所提出的CFD分析方法包括标准K-ε湍流模型,用于湍流,燃烧流动的涡流耗散模型(EDM)常数,用于燃烧流量的时间步长0.01ms的时间步长瞬态流动的顺序和围绕障碍物围绕障碍物10mm的电池长度大致等于大长度涡流。开发了一种火花点火模型,用于在基于节能法的氢爆炸测试中模拟由电气设备引起的40 j诱导的高点火能量。然而,对于燃料稀释和燃料富裕的燃料稀释和燃料的燃料浓度,EDM模型常数被修改为A = 7和B = 0.8,因为EDM中的湍流混合速率的主要思想不能覆盖燃烧的变化由于氢浓度与燃料稀燃料的氢浓度差异导致的能量。 CFD分析方法的计算误差范围是SRI氢气爆炸试验在燃料瘦和燃料富裕的条件下的仿真结果的约±7%。因此,已知利用EDM的CFD分析可以用作准确的评估工具,以预测超压累积,如果可以根据氢浓度正确选择EDM常数。

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