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Experimental and numerical investigation of film cooling effectiveness for rectangular injection holes

机译:矩形喷孔冷却效果的实验与数值研究

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Purpose - To investigate the film cooling effectiveness in a flat plate with a single row of rectangular injection holes. Design/methodology/approach - Three injection holes in model are in a single row. The holes are rectangular cross section and they are 9 × 6.5 mm. The injection holes are inclined at 30° along the mainstream direction. The blowing ratios are from 0.5 to 2.0. The experiments and their computational models are established to investigate its effects at the 330 and 335 and 340 K injection temperatures and the different blowing ratios. Findings - Results show that the blowing ratio and injection temperature and momentum flux ratio affect the film cooling effectiveness and to provide a good film cooling performance in both mainstream and lateral direction a suitable blowing ratio should be selected. In this study, the highest effectiveness is determined at a blowing ratio of 0.5. Further increasing this ratio results in reverse effect on the film cooling effectiveness. Originality/value - It is the fist time the film cooling effectiveness is compared at the rectangular injection holes as experimental and numerical.
机译:目的-研究具有单排矩形注射孔的平板中的薄膜冷却效果。设计/方法/方法-模型中的三个注入孔位于同一行中。孔为矩形横截面,为9×6.5 mm。注入孔沿主方向倾斜30°。吹塑比为0.5至2.0。建立了实验及其计算模型,以研究其在330 K和335 K和340 K注入温度以及不同吹炼比下的影响。研究结果-结果表明,吹塑比,注入温度和动量通量比会影响薄膜的冷却效果,并且要在主流和横向方向上提供良好的薄膜冷却性能,应选择合适的吹塑比。在这项研究中,最高效率是在吹塑比为0.5时确定的。进一步增加该比例将对薄膜冷却效果产生反作用。原创性/价值-这是第一次在矩形注入孔处比较薄膜冷却效率的实验和数值。

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