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TURBULENT HEAT TRANSFER ENHANCEMENT IN RECTANGULAR CHANNELS WITH TWO OPPOSITE RIB-ROUGHENED WALLS

机译:带有两个相对的肋筋加强壁的矩形通道中湍流传热的增强

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摘要

This work presents the results of an experimental investigation into the effects of variations in the channel aspect ratio and rib angle-of-attack, on the friction factor and local heat transfer in rectangular channels with two opposite ribbed rough walls. Rectangular tubes with three different aspect ratios were tested. Using a thin stainless steel foil, the local heat transfer coefficients were measured both on the ribbed side wall and on the smooth side wall, in the hydrodynamic and thermal entrance region and in the fully developed region. Similarity laws for the friction factor and heat transfer coefficient were used to correlate the experimental results for cases where the rib height-to-equivalent diameter ratio, e/D, was 0.047, 0.078, rib pitch-to-height ratio, p/e, was 10, 20, rib angle-of-attack, (alpha), was 90(DEGREES), 60(DEGREES), 45(DEGREES), 30(DEGREES), for value of the Reynolds number between 10,000 and 60,000 and channel aspect ratio, b/a, between 1 and 4.;The results were compared with previously existing theoretical and experimental results. The results obtained in this study provide an excellent reference for designing advanced turbine blade cooling passages and efficient heat exchangers.
机译:这项工作提出了一个实验研究的结果,该实验研究了通道纵横比和肋的攻角变化对具有两个相对的肋状粗糙壁的矩形通道中的摩擦系数和局部传热的影响。测试了具有三种不同长宽比的矩形管。使用薄的不锈钢箔,在带肋的侧壁和光滑的侧壁上,在流体动力和热力进入区域以及充分展开的区域中,都测量了局部传热系数。对于肋高与等效直径之比e / D为0.047、0.078,肋距与高之比p / e的情况,使用摩擦因数和热传递系数的相似律来关联实验结果对于10,000和60,000之间的雷诺数和通道,分别为10、20,肋骨攻角α(α),90(DEGREES),60(DEGREES),45(DEGREES),30(DEGREES)长宽比,b / a,介于1-4之间;将结果与先前存在的理论和实验结果进行比较。这项研究中获得的结果为设计先进的涡轮叶片冷却通道和高效的热交换器提供了极好的参考。

著录项

  • 作者

    PARK, JONGSOO.;

  • 作者单位

    Texas A&M University.;

  • 授予单位 Texas A&M University.;
  • 学科 Mechanical engineering.
  • 学位 Ph.D.
  • 年度 1986
  • 页码 138 p.
  • 总页数 138
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:51:00

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