首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >EXPERIMENTAL STUDY ON ANALOGY PRINCIPLE OF OVERALL COOLING EFFECTIVENESS FOR COMPOSITE COOLING STRUCTURES WITH BOTH INTERNAL COOLING AND FILM COOLING
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EXPERIMENTAL STUDY ON ANALOGY PRINCIPLE OF OVERALL COOLING EFFECTIVENESS FOR COMPOSITE COOLING STRUCTURES WITH BOTH INTERNAL COOLING AND FILM COOLING

机译:复合型冷却结构总冷却效能类比原理的实验研究,包括内部冷却和薄膜冷却

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The previous theoretical work showed the matching principles of analogy parameters for effusion-impingement cooling model. The mismatch of temperature ratios T_g/T_c may result in different matching performance in laboratory condition. Thus, the analogy principles of overall cooling effectiveness were evaluated by experiments in different laboratory conditions for effusion-impingement cooling model. The film plate had 8 rows of cylinder film holes with staggered arrangement and the impingement holes was also employed staggered pattern. Four kinds of cases with different temperature ratios, varied from 1.1 to 2, were tested under three momentum flux ratios and corresponding blowing ratios. The 2D contours of overall cooling effectiveness were measured by using IR thermography. The results for cases with the same mainstream side Biot number and momentum flux ratio show similar contours and values of overall cooling effectiveness, although temperature ratios of these cases are different. And the maximum deviation of overall cooling effectiveness is within 0.02 for these cases. However, there were 0.04~0.08 difference in the overall cooling effectiveness when the blowing ratios were matched. The overall cooling effectiveness significantly decreases under each blowing ratios with the increase of temperature ratios.
机译:以前的理论工作表明,用于振动冲击模型的类比参数的匹配原理。温度比T_G / T_C的不匹配可能导致实验室条件下的不同匹配性能。因此,通过实验室条件下的实验室条件进行了对整体冷却效果的类比原理进行了评估,用于锻炼冲击模型。薄膜板具有8排圆柱膜孔,具有交错的布置,撞击孔也采用了交错的图案。在三次动量通量比和相应的吹风比率下测试四种具有不同温度比的不同温度比的病例。通过使用IR热成像测量总冷却效果的2D轮廓。患者具有相同主流侧生物数和动量助熔率的情况表现出类似的轮廓和总冷却效果的值,尽管这些情况的温度比不同。这些情况的总冷却效果的最大偏差在0.02内。然而,当吹出比率匹配时,整体冷却效果的差异为0.04〜0.08差异。随着温度比率的增加,每种吹气比在每个吹气比下显着降低。

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