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首页> 外文期刊>Journal of turbomachinery >Effect of Reynolds number, hole patterns, and target plate thickness on the cooling performance of an impinging jet array-part II: Conjugate heat transfer results and optimization
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Effect of Reynolds number, hole patterns, and target plate thickness on the cooling performance of an impinging jet array-part II: Conjugate heat transfer results and optimization

机译:雷诺数,孔型和靶板厚度对射流阵列冷却性能的影响-第二部分:共轭传热结果和优化

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摘要

This study comprehensively illustrates the effect of Reynolds number, hole spacing, nozzle-to-target distance, and target plate thickness on the conjugate heat transfer (CHT) performance of an impinging jet array. Test models are composed of a specific thermalconductivity material which exerts a matched model Biot number to that of engine condition. High-resolution temperature measurements are conducted on the impinging-target plate utilizing steady liquid crystal (SLC) with Reynolds numbers ranging from 5000 to 27,500. Different streamwise and spanwise jet-to-jet spacing (i.e., X/D and Y/D: 4-8), nozzle-to-target plate distance (Z/D: 0.75-3), and target plate thickness (t/D: 0.75-2.75) are employed to compose a total of 108 different geometries. Experimental measured temperature is utilized as boundary conditions to conduct finite element simulation. Local and averaged nondimensional temperature and averaged temperature uniformity of target plate "hot side" are obtained. Optimum hole spacing arrangements, impingement distance, and target plate thickness are pointed out to minimize hot side temperature, amount of cooling air and to maximize temperature uniformity. Also included are 2D predictions with different convective boundary conditions, i.e., local 2D distribution and row-averaged heat transfer coefficients (HTCs), to estimate the accuracy of temperature prediction in comparison with the conjugate results.
机译:这项研究全面地说明了雷诺数,孔距,喷嘴到目标的距离以及目标板的厚度对射流阵列的共轭传热(CHT)性能的影响。测试模型由特定的导热材料组成,该材料具有与发动机工况匹配的比奥特数模型。使用雷诺数范围为5000至27,500的稳定液晶(SLC)在撞击目标板上进行高分辨率温度测量。沿流向和跨向的射流间距(即X / D和Y / D:4-8),喷嘴到目标板的距离(Z / D:0.75-3)和目标板厚度(t / D:0.75-2.75)用于构成总共108个不同的几何形状。利用实验测得的温度作为边界条件进行有限元模拟。获得目标板“热侧”的局部和平均无量纲温度以及平均温度均匀性。指出了最佳的孔间距布置,冲击距离和目标板厚度,以最大程度地降低热侧温度,冷却空气量并最大程度地提高温度均匀性。还包括具有不同对流边界条件的2D预测,即局部2D分布和行平均传热系数(HTC),以便与共轭结果相比估算温度预测的准确性。

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  • 来源
    《Journal of turbomachinery》 |2017年第10期|101001.1-101001.13|共13页
  • 作者单位

    Department of Thermal Engineering, Gas Turbine Institute, Tsinghua University, Beijing, China;

    Department of Mechanical Engineering and Material Science, University of Pittsburgh, Pittsburgh, PA, United States;

    Department of Thermal Engineering, Gas Turbine Institute, Tsinghua University, Beijing, China;

    Department of Thermal Engineering, Gas Turbine Institute, Tsinghua University, Beijing, China;

    Department of Thermal Engineering, Gas Turbine Institute, Tsinghua University, Beijing, China;

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