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Simulation Investigation of the Temperature Field of High Temperature Heading Face Under Two-pipe Mix Ventilation System

机译:两管混合通风系统下高温掘进面温度场的模拟研究

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A multicomponent single-phase model was set for hightemperature heading face in this study,based on the mass conservation law,the momentum conservation law and the energy conservation law.The standard wall function was used to correlate the physical quantities near the wall and in the turbulence kern zone.Parellel calculation method was used to simulate the distribution of the temperature field and the flow field.The calculation results show that,the temperature of the airflow goes up nonlinearly along the channel from the heading and the distribution of the temperature field depends on the characteristic of the flow field.Then the temperature curves of heading face with air injection.whose temperatures are diflerent,were analyzed.The section which is 7m far from the heading is the inflection point for all of the curves.The temperature gradient along the vertical direction increases quickly,but the largest temperature difference is less than 3K.So the comfort of human is satisfied under each temperature of the injection air.
机译:基于质量守恒定律,动量守恒定律和能量守恒定律,建立了高温掘进面多分量单相模型。标准壁函数用于关联壁附近和壁面的物理量。用并行计算方法模拟了温度场和流场的分布。计算结果表明,气流温度从航向沿通道呈非线性上升,温度场的分布取决于然后分析了不同温度下的注气航向面的温度曲线。距离航向7m的截面是所有曲线的拐点。垂直方向迅速增加,但最大温差小于3K。在注入空气的每个温度下均满足。

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