首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >EXPERIMENTAL INVESTIGATION ON THE FLAT-PLATE FILM COOLING ENHANCEMENT USING THE VORTEX GENERATOR DOWNSTREAM FOR THE CYLINDRICAL HOLE AND FAN-SHAPED HOLE CONFIGURATIONS
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EXPERIMENTAL INVESTIGATION ON THE FLAT-PLATE FILM COOLING ENHANCEMENT USING THE VORTEX GENERATOR DOWNSTREAM FOR THE CYLINDRICAL HOLE AND FAN-SHAPED HOLE CONFIGURATIONS

机译:圆柱形孔和扇形孔配置中涡流发生器的平板膜冷却增强试验研究

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In our experiments, the film cooling performance of the configurations combined the different hole with the vortex generator was investigated experimentally, measured by the infrared camera. Four different configurations were studied at the blowing ratio varying at M=0.5, 1.0, 1.5, 2.0, 2.5 and 3.0. In all cases, the Reynold number of the mainstream based on the hole diameter remained at Re=8000, and the density ratio kept at DR=1.7. Experimental results show that for the two models combining the cylindrical hole and fan-shaped hole with the vortex generator respectively, the film cooling performance becomes better when the blowing ratio increases from M=0.5 to M=2.0, and then decreases when the blowing ratio increases from M=2.0 to M=3.0. The model combining the fan-shaped hole with the vortex generator performs the best among the four models at each blowing ratio. Its film attachment holds the most extensive lateral distribution and its overall film cooling effectiveness could keep at a high level at a wide range of blowing ratios from M=1.0 to M=3.0. The combined model of the fan-shaped hole could improve the area-averaged film effectiveness at most 25.5% than that of the single hole model at M=2.0. Moreover, the combined model of the cylindrical hole could improve the area-averaged film cooling effectiveness at most 431% than that of the single cylindrical hole model at M=3.0.
机译:在我们的实验中,通过实验研究了配置与涡流发生器的不同孔的薄膜冷却性能,由红外相机测量。在M = 0.5,1.0,1.5,2.0,2.5和3.0的吹气比下研究了四种不同的配置。在所有情况下,基于孔径的主流的雷诺数保持在RE = 8000处,密度比在DR = 1.7处保持。实验结果表明,对于两种模型分别将圆柱形孔和扇形孔组合,分别与涡流发生器相结合,当吹出比从m​​ = 0.5增加到m = 2.0时,薄膜冷却性能变得更好,然后在吹出比率下降从m = 2.0到m = 3.0增加。将扇形孔与涡流发生器组合的模型在每个吹风比中的四个模型中执行最佳。其薄膜附件保持最广泛的横向分布,其总薄膜冷却效果可以在宽范围的吹气比中从M = 1.0到m = 3.0保持高水平。扇形孔的组合模型可以在M = 2.0的单孔模型的最多25.5%上提高面积平均膜效果。此外,圆柱孔的组合模型可以在M = 3.0处的单圆柱孔模型的最多431%提高面积平均薄膜冷却效果。

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