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An Experimental Study of Mist Film Cooling with Fan-Shaped Holes on an Extended Flat Plate - Part 1: Heat Transfer

机译:扩展平板上带扇形孔的薄雾冷却实验研究-第1部分:传热

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Motivated by the need to further improve film cooling in terms of both cooling effectiveness and coolant coverage area, the mist/air film cooling scheme is investigated through experiments using fan-shaped holes over an extended downstream length in this study. Both an existing wind tunnel and test facility, used in previous work, have been retrofitted. The first modification was extending the length of the flat plate test section to cover longer distances downstream of the injection holes, up to X/D=100, in order to investigate whether mist cooling can be harnessed farther downstream where single-phase film cooling is not effective. The second modification was to incorporate a fan-shaped diffusion hole geometry in order to investigate whether mist can further enhance the film cooling performance of the already highly effective fan-shaped holes. A Phase Doppler Particle Analyzer (PDPA) system is employed to measure droplet size, velocity, and turbulence information. An infrared camera and thermocouples are both used for temperature measurements. Part 1 is focused on the heat transfer result on the wall, and Part 2 is focused on the two-phase droplet multiphase flow behavior. Three blowing ratios are investigated. The results show that, at low blowing ratios when the film is attached to the surface, the enhancement of the mist film cooling effectiveness, compared to the air-only case, on the centerline of the hole ranges from 40% in the near hole region to over 170% at X/D = 100. Due to the diffusive nature of the fan-shaped hole, the laterally-averaged enhancement is on par with that on the centerline. The significant enhancement over the extended downstream distance from X/D=40-100 is attributed to the evaporation time needed to evaporate all of the droplets. Each droplet acts as a cooling sink and flies over a distance before it completely vaporizes. This "distributed cooling" characteristic allows controlled cooling by manipulating the size distribution of the water droplets to extend the cooling effects of the droplets farther downstream from the injection location. At higher blowing ratios, when the cooling film is lifted off from the surface, the cooling enhancement drops below 40%. Although the enhancement in the near hole region X/D < 40 is about 20% lower than that achieved by using the cylindrical holes, the magnitudes of the mist adiabatic film cooling effectiveness using fan-shaped holes are still much higher than those of the cylindrical holes.
机译:由于需要在冷却效率和冷却液覆盖面积方面进一步改善薄膜冷却的动机,因此在本研究中,通过使用扇形孔进行了实验,研究了雾气/空气薄膜的冷却方案。先前工作中使用的现有风洞和测试设施均已进行了改造。第一个修改是延长平板测试部分的长度,以覆盖喷孔下游更长的距离,最高可达X / D = 100,以便研究是否可以将雾气冷却带到更下游的单相薄膜冷却。没有效果。第二个修改是合并一个扇形扩散孔几何形状,以研究雾气是否可以进一步增强已经非常有效的扇形孔的薄膜冷却性能。使用相位多普勒粒子分析仪(PDPA)系统来测量液滴尺寸,速度和湍流信息。红外摄像机和热电偶均用于温度测量。第1部分关注于壁上的传热结果,第2部分关注于两相液滴多相流动行为。研究了三种吹气比。结果表明,当薄膜附着在表面上时,在低鼓风比下,与仅空气情况相比,在孔的中心线上,与仅使用空气的情况相比,雾膜的冷却效率得到了增强,在近孔区域的范围为40%。在X / D = 100时达到170%以上。由于扇形孔的扩散特性,横向平均增强效果与中心线的增强效果相当。在从X / D = 40-100开始的延长下游距离上的显着增强归因于蒸发所有液滴所需的蒸发时间。每个液滴都充当冷却槽,并在完全蒸发之前飞过一段距离。这种“分布式冷却”特性允许通过控制水滴的大小分布来控制冷却,以将水滴的冷却效果扩展到更远离注入位置的下游。在较高的吹塑比下,当冷却膜从表面剥离时,冷却增强会降至40%以下。尽管近孔区域X / D <40的增强效果比使用圆柱形孔实现的效果低约20%,但使用扇形孔实现的雾绝热膜冷却效率的幅度仍远高于圆柱形效果孔。

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