首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >An experimental and numerical study of flow and heat transfer in channels with pin fin-dimple and pin fin arrays
【24h】

An experimental and numerical study of flow and heat transfer in channels with pin fin-dimple and pin fin arrays

机译:针鳍-凹窝和针鳍阵列的通道内流动和传热的实验和数值研究

获取原文
获取原文并翻译 | 示例
       

摘要

An experimental and numerical study was conducted to investigate the flow friction and heat transfer performance in rectangular channels with staggered arrays of pin fin-dimple hybrid structures and pin fins in the Reynolds number range of 8200-54,000. The study aims at improving the cooling design for the gas turbine components. The friction factor, Nusselt number and the overall thermal performance parameters of the pin fin-dimple and the pin fin channels have been obtained and compared with the experimental data of a smooth rectangular channel and previously published data of the pin fin channel. The comparisons showed that, compared with the pin fin channel, the pin fin-dimple channel has further improved convective heat transfer performance by about 8.0% and whereas lowered flow friction by more than 18.0%. In addition, fully three-dimensional numerical computations have been done to investigate the physical details about the flow and heat transfer in the pin fin and pin fin-dimple channels. The computations showed that the dimples increase the near-wall turbulent mixing level by producing strong vortex flows, and therefore enhance the convective heat transfer in the channel. On the other hand, the dimples enlarge the minimum cross section area transversely between the pin fins, and therefore the pressure loss in the flow can be reduced in the pin fin-dimple channels.
机译:进行了实验和数值研究,以研究雷诺数范围为8200-54,000的针状翅片-凹窝混合结构和翅状翅片交错排列的矩形通道中的流动摩擦和传热性能。该研究旨在改善燃气轮机组件的冷却设计。已经获得了针状翅片-凹窝和针状翅片通道的摩擦系数,Nusselt数和总体热性能参数,并将其与光滑矩形通道的实验数据和先前公布的针状翅片通道的数据进行了比较。比较结果表明,与针翅通道相比,针翅凹坑通道的对流传热性能进一步提高了约8.0%,而流动摩擦降低了18.0%以上。此外,已经进行了全三维数值计算,以研究有关针鳍和针鳍凹坑通道中的流动和传热的物理细节。计算表明,凹坑通过产生强烈的涡流来增加近壁湍流混合水平,从而增强了通道中的对流换热。另一方面,凹坑在销鳍之间横向地增大最小横截面面积,因此可以减小销鳍凹道中的流动中的压力损失。

著录项

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