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Improved Correlations for Curvature Effects in Cooling Channels of Rocket Engines

机译:火箭发动机冷却通道曲率效应的改进相关性

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New improved correlations for developing and diminishing coolant flow heat transfer coefficient as the coolant flow enters and leaves curved section of cooling channels are developed. The correlations are based on rectangular cooling channels and it is demonstrated that the heat transfer coefficients variation behave differently for the three surfaces of cooling channels. The three variables that are incorporated in the heat transfer coefficient correlations include, dimensionless distance from entrance or exit of the curved section, the dimensionless radius of curvature and cooling channel aspect ratio.
机译:随着冷却剂流进入和离开冷却通道的弯曲部分,开发了用于改善和减小冷却剂流传热系数的新的改进的相关性。相关性基于矩形冷却通道,并且证明了冷却通道的三个表面的传热系数变化行为不同。包含在传热系数相关性中的三个变量包括到弯曲部分入口或出口的无量纲距离,无量纲的曲率半径和冷却通道的长宽比。

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