• It is shown that the forced convection over micro pin fin heat sinks is a very effective heat transfer mode.

    本文以去离子水为冷却工质,流体横向冲刷方形肋阵列传热特性进行了实验研究。

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  • The numerical study was carried out on the trailing edge cooling of turbine blade using the circular pin fin that was arranged in cross type.

    一个有交叉排列圆形扰流柱涡轮叶片冷却方案进行数值研究

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  • The 3-D numerical prediction proved that the copper pin fin structures have 24%-34% higher convection heat transfer coefficients with 10%-16% pressure drop increase.

    三维空间上对流换热模拟表明铜制结构的换系数高出百叶窗翅片24%-34%,而流阻仅高出10%-16%。

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  • An experimental research was conducted to simulate the effect of trailing edge ejection of turbine blades on heat transfer of the inner cooling passage with staggered pin fin array.

    本文实验方法模拟研究涡轮叶片缘出流对带叉排扰流柱阵列通道对流换特性的影响

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  • The effect of each parameter on distribution of static pressure and pressure loss coefficient are found out. Experiments have been carried out in trapezoidal duct with staggered pin fin arrays.

    为了解不同雷诺数流比情况下各种因素压力损失系数影响,对流梯形扰流柱通道端壁的静压和压力损失系数进行实验测量。

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  • In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically.

    本文应用湍流模型涡轮叶片缘针通道的换流动进行了二维数值模拟研究。

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  • This paper studies the pin-fin tube, smooth tube and finned tube on the same wind channel test apparatus through experimental method.

    采用实验研究方法,分别对针,平直翅片管和光管同一风洞实验台上进行了实验。

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  • Heat transfer in channel for trailing edge of turbine blade with pin-fin arrays is studied numerically.

    涡轮叶片缘针通道的换进行了数值模拟研究。

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  • The design of fin-line PIN switches is presented.

    本文介绍集成化PIN开关设计过程。

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  • The heat transfer and characteristics of the fluid flow in the duct with waist-shaped pin - fin arrays for the trailing edge of the turbine blade were experimentally investigated.

    本文涡轮叶片缘中具有结构扰冷却通道传热流动阻力特性进行了实验研究,重点研究了雷诺数、扰流柱的束腰比以及不同组合的影响。

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  • The heat transfer and characteristics of the fluid flow in the duct of the trailing edge of the turbine blade with parted pin-fin arrays were experimentally investigated.

    本文对具有断裂结构扰涡轮叶片尾缘楔型通道流动过程进行了实验研究。

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  • The result shows that the flow inside the lamilloy varied when the structure is different from one to another, and the changes are mainly close-by the area of pin-fin.

    实验结果表明,层板内部流动情况结构变化而变化,这种变化主要集中在扰流柱附近区域

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  • The first tube was winded pin-fin tube which was improved and self-designed.

    第一自行改进设计的绕针翅

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  • The first tube was winded pin-fin tube which was improved and self-designed.

    第一自行改进设计的绕针翅

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