首页> 外文期刊>Journal of Heat Transfer >A Numerical Study of the Flow and Heat Transfer in the Pin Fin-Dimple Channels With Various Dimple Depths
【24h】

A Numerical Study of the Flow and Heat Transfer in the Pin Fin-Dimple Channels With Various Dimple Depths

机译:不同凹坑深度的销鳍-凹坑通道内流动和传热的数值研究

获取原文
获取原文并翻译 | 示例
           

摘要

A numerical study was conducted to investigate the effects of dimple depth on the flow and heat transfer characteristics in a pin fin-dimple channel, where dimples are located spanwisely between the pin fins. The study aimed at promoting the understanding of the underlying convective heat transfer mechanisms in the pin fin-dimple channels and improving the cooling design for the gas turbine components. The flow structure, friction factor, and heat transfer performance of the pin fin-dimple channels with various dimple depths have been obtained and compared with each other for the Reynolds number range of 8200-80,800. The study showed that, compared to the pin fin channel, the pin fin-dimple channels have further improved convective heat transfer performance, and the pin fin-dimple channel with deeper dimples shows relatively higher Nusselt number values. The study still showed a dimple depth-dependent flow friction performance for the pin fin-dimple channels compared to the pin fin channel, and the pin fin-dimple channel with shallower dimples shows relatively lower friction factors over the studied Reynolds number range. Furthermore, the computations showed the detailed characteristics in the distribution of the velocity and turbulence level in the flow, which revealed the underlying mechanisms for the heat transfer enhancement and flow friction reduction phenomenon in the pin fin-dimple channels.
机译:进行了数值研究,以研究凹痕深度对针状翅片-凹痕通道中流动和传热特性的影响,其中,凹痕沿翼展方向分布在针状翅片之间。该研究旨在增进对销翅片-凹窝通道中潜在对流传热机理的了解,并改善燃气轮机组件的冷却设计。对于8200-80,800的雷诺数范围,已获得了具有不同凹坑深度的针状翅片-凹坑通道的流动结构,摩擦系数和传热性能,并将它们进行了比较。研究表明,与针翅式通道相比,针翅式微凹通道具有更好的对流换热性能,而凹痕较深的针翅式微凹通道显示出相对较高的努塞尔数值。这项研究仍然显示出,与翅片翅片通道相比,翅片翅片-凹坑通道的凹坑深度依赖于流动摩擦性能,凹坑较浅的翅片-翅片凹坑通道在研究的雷诺数范围内显示出相对较低的摩擦系数。此外,计算结果显示出流中速度和湍流水平分布的详细特征,揭示了针状翅片-凹痕通道中传热增强和流摩擦减小现象的潜在机理。

著录项

  • 来源
    《Journal of Heat Transfer》 |2012年第7期|p.071902.1-071902.9|共9页
  • 作者

    Yu Rao; Yamin Xu; Chaoyi Wan;

  • 作者单位

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

    School of Aeronautics and Astronautics, Shanghai Jiaotong University, Dongchuan Road 800, Shanghai 200240, P.R. China;

    Department Mechanical and Power Engineering, Institute of Turbomachinery, 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

    pin fin; dimple; numerical computation; friction factor; heat transfer; enhancement;

    机译:针鳍酒窝;数值计算摩擦系数传播热量;增强;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号