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An Experimental Study of Mist/Air Film Cooling with Fan-shaped Holes on an Extended Flat Plate - Part 2: 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2部分:两相流测量和液滴动力学

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A Phase Doppler Particle Analyzer (PDPA) 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 a typical coolant film layer and a wider droplet layer. The droplet layer is identified by a wedge-shaped enclosure prescribed by the data rate (droplet number per second) distribution. The apex of the enclosure, depicting by the maximum data rate, roughly indicating the core region of the coolant film. The upper boundary of the film layer, characterized by active mixing with the main flow, is found to be close to relatively high values of local Reynolds shear stresses. Thanks to higher inertia possessed by larger droplets (>20 μm in diameter) at the injection hole, the larger droplets tend to shoot across the coolant layer, resulting in a wider droplet layer than the cooling film layer. With the prescribed coolant film and droplet layer profiles, the heat transfer results on the wall presented in Part 1 are re-examined. The 3-D 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 explains 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(PDPA)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,为圆柱孔和扇形孔规定了一个投影轮廓,该轮廓描述了气雾冷却剂喷射流如何扩散并最终混入热主流中。薄雾层由典型的冷却液层和较宽的液滴层组成。液滴层由数据速率(每秒的液滴数)分布规定的楔形外壳标识。外壳的顶点,以最大数据速率表示,大致指示了冷却剂薄膜的核心区域。发现膜层的上边界的特征在于与主流的主动混合,其接近于局部雷诺剪切应力的相对较高的值。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层上喷射,从而导致液滴层比冷却膜层更宽。使用规定的冷却液膜和液滴层轮廓,将重新检查第1部分中显示的壁上的传热结果。 3-D液滴的测量表明,从扇形孔注入的液滴在横向方向上比汽缸孔分布得更宽,并聚集在相邻的冷却剂薄膜层相遇的位置。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在使用圆柱孔的情况下沿孔的中心线增强了雾气。

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