首页> 外文会议>Proceedings of 3rd international symposium on jet propulsion and power engineering. >Three-Dimensional Numerical Study of Supercritical Heat Transfer of Cryogenic Methane in an Engine Cooling Channel
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Three-Dimensional Numerical Study of Supercritical Heat Transfer of Cryogenic Methane in an Engine Cooling Channel

机译:发动机冷却通道中低温甲烷超临界传热的三维数值研究

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A three-dimensional numerical study of the turbulent convective heat transfer of the cryogenic methane flowing inside a square engine cooling channel under supercritical pressures has been systematically conducted. Numerical results indicate that increasing the fluid pressure would result in enhanced heat transfer of the cryogenic methane under supercritical pressures; At the pseudo-critical temperature under a corresponding supercritical pressure, drastic property variations could cause heat transfer deterioration and sharp wall temperature increase at a high wall heat flux of 7 MW/m2; A modified Jackson and Hall heat transfer equation, which can be used for supercritical heat transfer calculations of the cryogenic methane, has been successfully established in this paper.
机译:在超临界压力下,对在方形发动机冷却通道内流动的低温甲烷的湍流对流换热进行了三维数值研究。数值结果表明,增加流体压力将导致超临界压力下低温甲烷的传热增加。在相应的超临界压力下的准临界温度下,剧烈的性能变化可能会导致传热恶化,并且在7 MW / m2的高壁热通量下壁温会急剧上升;本文成功建立了一种改进的杰克逊和霍尔传热方程,该方程可用于超低温甲烷的超临界传热计算。

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