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首页> 外文期刊>International Journal of Turbo and Jet Engines >Investigation on the Film Cooling Performance of Diffuser Shaped Holes with Different Inclination Angles
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Investigation on the Film Cooling Performance of Diffuser Shaped Holes with Different Inclination Angles

机译:不同倾角的扩散孔膜冷却性能研究

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摘要

Film cooling performances of laidback hole and laidback fan-shaped hole have been investigated using transient liquid crystal measurement technique. For film cooling of laidback hole, the increase of inclination angle reduces the film cooling effectiveness under small blowing ratio, while produces better film coverage and higher film cooling effectiveness under larger blowing ratios. Heat transfer coefficient is higher in the upstream region of laidback hole film cooling with large inclination angle, while laidback hole with small inclination angle has relatively higher heat transfer coefficient in the downstream region. The increase of inclination angle reduces the film cooling effectiveness and heat transfer coefficient of laidback fan-shaped hole film cooling, especially in the upstream region. Increase of inclination angle is beneficial to the thermal protection of laidback hole film cooling under large blowing ratio. Film hole with large inclination angle has larger discharge coefficient due to smaller aerodynamic loss in the hole.
机译:已经使用瞬态液晶测量技术研究了戏隙孔和歌唱扇形孔的薄膜冷却性能。对于智慧孔的薄膜冷却,倾斜角的增加降低了小吹吹比下的薄膜冷却效果,而在较大的吹气比下产生更好的薄膜覆盖和更高的膜冷却效果。具有大倾斜角度的智乐孔膜冷却的上游区域的传热系数较高,而具有小的倾斜角的悠闲孔在下游区域中具有相对较高的传热系数。倾斜角度的增加降低了歌唱扇形孔膜冷却的薄膜冷却效果和传热系数,尤其是在上游区域。倾斜角度的增加有利于大吹吹比下的悠闲孔膜冷却的热保护。由于孔中的空气动力学损失小,倾角大的薄膜孔具有较大的放电系数。

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