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Experimental and Numerical Study of Heat Transfer and Turbulent Flow Characteristics in Three-Short-Pass Serpentine ooling Channels With Miniature W-Ribs

机译:微型W肋三次短路蛇形煤气通道传热和湍流特性的实验性和数值研究

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摘要

Detailed experimental and numerical studies have been conducted on the heat transfer, pressure loss, and turbulent flow structure of a three-short-pass serpentine cooling channel with miniature W-shaped ribs on the wall under the Reynolds numbers from 8500 to 60,000. Steady-state heat transfer experiments were done to obtain the globally averaged and total heat transfer performance of each ribbed pass of the serpentine channel, and the streamwise pressure loss characteristics of the serpentine-channel flow were also obtained by multipoint pressure measurements. Additionally, the transient liquid crystal thermography technique was also used to obtain the local heat transfer distributions on the miniature W-ribbed surface of each pass. Furthermore, numerical simulations were done by using the AKN k-ε turbulence model to reveal the detailed turbulent flow and heat transfer characteristics in the serpentine channel. The experiments indicate that the miniature W-ribbed short pass has significantly enhanced total heat transfer by a factor of up to 4.0. The total heat transfer enhancement shows appreciably different values in different passes of the serpentine channel, and the second pass shows about 15% higher heat transfer enhancement than the first pass, and the third pass shows the highest heat transfer enhancement, which is about 15% higher than the second pass. The pressure loss measurements indicate that the two flow turnings contribute more than 90% of the total pressure loss in the serpentine channel with one ribbed pass with the miniature W ribs. The numerical simulations indicate that the flow turnings significantly increase the turbulent mixing in the flow of the downstream pass, and the miniature W-ribs on the wall appreciably improve the near-wall vortex mixing, which contributes the heat transfer enhancement.
机译:在雷诺数8500至60,000的雷诺数下,在三次短路的蛇形冷却通道的传热,压力损失和湍流结构上进行了详细的实验和数值研究。进行稳态传热实验以获得蛇形通道的每个肋状通道的全局平均和总传热性能,并且还通过多点压测量获得蛇形通道流的流动压力损失特性。另外,瞬态液晶热成像技术还用于获得每次通过的微型W形肋表面上的局部传热分布。此外,通过使用AKN K-ε湍流模型来揭示蛇形通道中的详细湍流和传热特性来完成数值模拟。实验表明,微型W重肋短通通道显着提高了总热传递量高达4.0。总传热增强在蛇形通道的不同通越野中显示出不同的值,第二通道显示出比第一阶段更高的传热增强增加约15%,第三通道显示出最高的传热增强,这约为15%高于第二次通过。压力损失测量表明,两个流动的流量有超过90%的蛇形通道中的总压力损失,其中一个带有微型W肋骨的罗纹通道。数值模拟表明,流动转弯显着增加了下游通道的流动中的湍流混合,并且壁上的微型W形肋明显改善了近壁涡流混合,这有助于传热增强。

著录项

  • 来源
    《Journal of Heat Transfer》 |2020年第12期|121901.1-121901.10|共10页
  • 作者单位

    School of Mechanical Engineering Institute of Turbomachinery Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;

    School of Mechanical Engineering Institute of Turbomachinery Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 China;

    School of Mechanical Engineering Institute of Turbomachinery Shanghai Jiao Tong University Dongchuan Road 800 Shanghai 200240 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; multipass serpentine channel; W-shaped ribs; heat transfer; Pressure loss;

    机译:燃气轮机冷却;多元蛇形通道;W形肋骨;传播热量;压力损失;

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