首页> 外文会议>ASME Turbine Technical Conference and Exposition >EXPERIMENTAL STUDY OF SISTER HOLE FILM COOLING PERFORMANCE IN A ROTATING FLAT PLATE MODEL
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EXPERIMENTAL STUDY OF SISTER HOLE FILM COOLING PERFORMANCE IN A ROTATING FLAT PLATE MODEL

机译:旋转平板模型中姊妹孔膜冷却性能的实验研究

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Film cooling performance of a sister hole was investigated in a flat plate model by applying Thermochromic Liquid Crystal (TLC) technique under the stationary and rotating conditions. The flat plate model is installed in the test section. The sister hole include one main hole and two additional side holes with the smaller diameter in the spanwise direction. The diameter of the main hole is 4 mm and the injection angle is 30°. The density ratio of coolant to mainstream is 1.05. The Reynolds number (Re_D) based on the velocity of mainstream and the diameter of the main hole are 2300, 3400 and 4500. Four rotational speeds of 200, 400, 600 and 800 rpm are conducted on both pressure side (trailing wall) and suction side (leading wall) with the blowing ratio varying from 0.14 to 3.5. The effects of blowing ratio, Reynolds number (Re_D) and rotation number are mainly analyzed according to film coverage and film cooling effectiveness. The results show that the film performance firstly increases then decreases with the rising of blowing ratio, the optimal blowing ratio is about M=0.5. The film cooling performance is improved with higher Reynolds number (Re_D). Under the rotation condition, the film trajectory has an obvious centrifugal deflection which can be enhanced by higher rotation number on the pressure side, and the film deflection moves a little centripetally on the suction side. The film cooling effectiveness on the suction side increases with the rising of rotation number and it is higher than that on the pressure side.
机译:通过在固定和旋转条件下施加热致变色的液晶(TLC)技术,在平板模型中研究了姐妹孔的膜冷却性能。平板模型安装在试验部分中。姐妹孔包括一个主孔和两个额外的侧孔,沿枝条方向较小。主孔的直径为4mm,注射角度为30°。冷却剂与主流的密度比为1.05。基于主流的速度和主孔的直径的雷诺数(RE_D)是2300,3400和4500.四个旋转速度为200,400,600和800rpm,在两个压力侧(尾随墙)和抽吸中进行侧面(前壁)吹出比率从0.14到3.5变化。主要根据胶片覆盖和薄膜冷却效果分析吹出比率,雷诺数(RE_D)和旋转数的影响。结果表明,薄膜性能首先增加随着吹吹比的升高而降低,最佳吹出比约为m = 0.5。较高的雷诺数(RE_D)改善了薄膜冷却性能。在旋转条件下,膜轨迹具有明显的离心偏转,这可以通过压力侧的较高旋转数来增强,并且膜偏转在吸入侧上略微厘米。吸入侧的薄膜冷却效果随着旋转数的上升而增加,并且它高于压力侧的升高。

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