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

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. X represents the axial distance downstream of the cooling hole of diameter D. The second modification was to incorporate fan-shaped (diffusion) holes which are proven to have a higher film cooling efficiency, than cylindrical holes. The objective is 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 the droplet size, velocity, and turbulence information. An infrared camera and thermocouples are both used for temperature measurements. Part I is focused on the heat transfer result on the wall. 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 the water droplets to extend the cooling effects 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. Part II of this study is focused on analyzing the two-phase droplet multiphase flow behavior to explain the fundamental physics involved in the mist film cooling.
机译:由于需要在冷却效率和冷却剂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/空气薄膜冷却方案。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,以覆盖进样孔下游更长的距离,最高X / D = 100,目的是研究是否可以在薄层单相膜冷却的下游进一步利用雾气冷却没有效果。 X代表直径D的冷却孔下游的轴向距离。第二个修改是合并了扇形(扩散)孔,这些孔被证明比薄膜孔具有更高的薄膜冷却效率。目的是研究薄雾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。相位多普勒粒子分析仪(PDPA)系统用于测量液滴大小,速度和湍流信息。红外摄像机和热电偶均用于温度测量。第一部分着眼于墙体的传热结果。结果表明,当薄膜附着在表面上时,在低吹气比下,与仅使用空气的情况相比,在孔的中心线处,雾膜的冷却效率有所提高,而在近孔区域中,雾膜的冷却效率为40%在X / D = 100时达到170%以上。由于扇形孔的扩散特性,横向平均增强与中心线的增强相等。从X / D = 40-100到下游延伸距离的显着增加归因于蒸发所有液滴所需的蒸发时间。每个液滴充当冷却槽,并在完全蒸发之前飞过一段距离。这种“分布式冷却”特性使水滴能够将冷却效果扩展到注入位置下游。在较高的吹塑比下,当将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的增强比使用圆柱形孔实现的增强低约20%,但使用扇形孔的雾状绝热膜冷却效率的幅度仍远高于圆柱形孔。本研究的第二部分着重于分析两相液滴多相流动行为,以解释雾膜冷却所涉及的基本物理学。

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