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An Experimental and Numerical Study of Flow and Heat Transfer in Channels With Pin Fin-Dimple Combined Arrays of Different Configurations

机译:带有不同配置的Pin Fin-Dimple组合阵列的通道内流动和传热的实验和数值研究

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摘要

An experimental and numerical study was conducted to investigate the flow and heat transfer characteristics in channels with pin fin-dimple combined arrays of different configurations, where dimples are located transversely or both transversely and streamwisely between the pin fins. The flow structure, friction factor, and heat transfer characteristics of the pin fin-dimple channels of different configurations have been obtained and compared with each other for the Reynolds number range of 8200-50,500. The experimental study showed that, compared to the pin fin channel, depending on the configurations of the pin fin-dimple combined arrays the pin fin-dimple channel can have distinctively further improved convective heat transfer performance by 8.0%-20.0%, whereas lower or slightly higher friction factors over the studied Reynolds number range. Furthermore, three-dimensional and steady-state conjugate computations have been carried out for similar experimental conditions. The numerical computations showed detailed characteristics of the distribution of the velocity and turbulence level in the flow, which revealed the underlying mechanisms for the pressure loss and heat transfer characteristics in the pin fin-dimple channels of different configurations.
机译:进行了实验和数值研究,以研究具有不同构型的针状翅片-凹坑组合阵列的通道中的流动和传热特性,其中,凹坑横向或横向和横向地在针状翅片之间定位。对于8200-50,500的雷诺数范围,已获得了不同构造的针状翅片-凹坑通道的流动结构,摩擦系数和传热特性,并将它们进行了比较。实验研究表明,与针翅通道相比,根据针翅-凹窝组合阵列的配置,针翅-凹窝通道可以显着进一步提高对流传热性能8.0%-20.0%,而降低或降低在研究的雷诺数范围内,摩擦系数略高。此外,已经针对相似的实验条件进行了三维和稳态共轭计算。数值计算显示了流中速度和湍流水平分布的详细特征,这揭示了不同构型的翅片-凹窝通道中压力损失和传热特性的潜在机理。

著录项

  • 来源
    《Journal of Heat Transfer》 |2012年第12期|121901.1-121901.11|共11页
  • 作者单位

    Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;

    Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;

    Institute of Turbomachinery, Department Mechanical and Power Engineering, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    gas turbine cooling; pin fin; dimple; flow; heat transfer enhancement;

    机译:燃气轮机冷却针鳍酒窝;流;传热增强;

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