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An Experimental Study of Mist/Air Film Cooling With Fan-Shaped Holes on an Extended Flat Plate-Part II: Two-Phase Flow Measurements and Droplet Dynamics

机译:扩展平板上带有扇形孔的薄雾/气膜冷却的实验研究-第二部分:两相流量测量和液滴动力学

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摘要

A phase Doppler particle analyzer (PDFA) system is employed to measure the two-phase mist flow behavior including flow velocity field, droplet size distribution, droplet dynamics, and turbulence characteristics. Based on the droplet measurements made through PDPA, a projected profile describing how the air-mist coolant jet flow spreads and eventually blends into the hot main flow is prescribed for both cylindrical and fan-shaped holes. The mist film layer consists of two layers: a typical coolant film layer (cooling air containing the majority of the droplets) and a wider droplet layer containing droplets outside the film layer. Thanks to the higher inertia possessed by larger droplets (>20 μm in diameter) at the injection hole, the larger droplets tend to shoot across the coolant film layer, resulting in a wider droplet layer than the coolant film layer. The wider droplet layer boundaries are detected by measuring the droplet data rate (droplet number per second) distribution, and it is identified by a wedge-shaped enclosure prescribed by the data rate distribution curve. The coolant film layer is prescribed by its core and its upper boundary. The apex of the data rate curve, depicted by the maximum data rate, roughly indicates the core region of the coolant film layer. The upper boundary of the coolant film layer, characterized by active mixing with the main flow, is found to be close to relatively high values of local Reynolds shear stresses. With the results of PDPA measurements and the prescribed coolant film and droplet layer profiles, the heat transfer results on the wall presented in Part I are re-examined, and the fundamental mist-flow physics are analyzed. The three-dimensional (3D) droplet measurements show that the droplets injected from the fan-shaped holes tend to spread wider in lateral direction than cylinder holes and accumulate at the location where the neighboring coolant film layers meet. This flow and droplet behavior explain the higher cooling performance as well as mist-enhancement occurs between the fan-shaped cooling holes, rather than along the hole's centerline as demonstrated in the case using the cylindrical holes.
机译:使用相位多普勒粒子分析仪(PDFA)系统来测量两相雾流行为,包括流速场,液滴尺寸分布,液滴动力学和湍流特性。根据通过PDPA进行的液滴测量,规定了圆柱孔和扇形孔的投影轮廓,该轮廓描述了气雾冷却剂喷射流如何扩散并最终掺入热主流中。薄雾膜层由两层组成:典型的冷却液膜层(包含大部分液滴的冷却空气)和较宽的液滴层,其在膜层外部包含液滴。由于在喷射孔处较大的液滴(直径大于20μm)具有较高的惯性,因此较大的液滴倾向于在冷却剂膜层上喷射,从而导致液滴层比冷却剂膜层更宽。通过测量墨滴数据速率(每秒的墨滴数)分布可以检测到较宽的墨滴层边界,并通过数据速率分布曲线规定的楔形外壳来识别。冷却剂薄膜层由其芯和其上边界规定。以最大数据速率表示的数据速率曲线的顶点大致表示冷却液薄膜层的核心区域。发现冷却剂薄膜层的上边界以与主流的主动混合为特征,接近于局部雷诺剪切应力的较高值。利用PDPA测量的结果以及规定的冷却液膜和液滴层轮廓,重新检查了第一部分中介绍的壁上的传热结果,并分析了基本的雾流物理性质。三维(3D)液滴测量结果表明,从扇形孔注入的液滴在横向方向上的分布比汽缸孔更宽,并在相邻的冷却剂薄膜层相遇的位置积聚。这种流动和液滴行为说明了较高的冷却性能以及在扇形冷却孔之间而不是沿着孔的中心线出现雾增强,如使用圆柱形孔的情况所示。

著录项

  • 来源
    《Journal of Heat Transfer》 |2018年第4期|042202.1-042202.11|共11页
  • 作者

    Reda Ragab; Ting Wang;

  • 作者单位

    Energy Conversion and Conservation Center, University of New Orleans, New Orleans 70148, LA;

    Energy Conversion and Conservation Center, University of New Orleans, New Orleans 70148, LA;

  • 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

    film cooling; mist cooling; droplet dynamics; gas turbine airfoil cooling;

    机译:薄膜冷却;雾冷却液滴动力学燃气轮机翼型冷却;

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