首页> 外文会议>Proceedings of 3rd international symposium on jet propulsion and power engineering. >Flow and Heat Transfer Characteristics Analysis in Vane Trailing Edge Assembled Unit
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Flow and Heat Transfer Characteristics Analysis in Vane Trailing Edge Assembled Unit

机译:叶片后缘组合单元的流动和传热特性分析

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By using a certain foreign model engine vane trailing edge as the object of study, flow and heat transfer characteristics in a contracted channel with complex arrangement of pin fins has been researched. The following conclusions were obtained: As the Reynolds number increases, flow of each segment tends to average and total pressure loss coefficient decreases; total pressure losses of the two segments close to inlet are significantly larger than the other three; as the Reynolds number increases, the average convective heat transfer coefficient increases and the average temperature of wall decreases; convective heat transfer performance of blade root is poor, due to local low flow rate.
机译:以某国外某型发动机叶片后缘为研究对象,研究了翅片翅片复杂布置的收缩通道内的流动和传热特性。得到以下结论:随着雷诺数的增加,每个管段的流量趋于平均,总压力损失系数减小。靠近入口的两个部分的总压力损失明显大于其他三个部分;随着雷诺数的增加,平均对流换热系数增加,壁的平均温度降低。由于局部低流速,叶根的对流传热性能很差。

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