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EFFECT OF GEOMETRY VARIATIONS ON THE COOLING PERFORMANCE OF FAN-SHAPED COOLING HOLES

机译:几何形状变化对扇形冷却孔冷却性能的影响

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The flow conditions at both, the cooling hole exit as well as the cooling hole entrance affect in a very different way the cooling performance downstream of cylindrical and fan-shaped holes. The consequences of a change in a flow parameter very obviously depend on the respective hole geometry. To gain an as complete as possible view of the specific effects of varying operating conditions and hence an enhanced understanding of the dominating mechanisms, a variation of the hole geometry is imperative. The expansion angle of the diffuser, the inclination angle of the hole, and the length of the cylindrical part at the hole entrance are considered to be the most important geometric parameters of diffuser holes.The effect of a change of exactly these parameters on the film cooling performance will be analyzed. For a better assessment of the characteristic effects associated with contouring of the hole, every diffuser hole is compared to an adequate cylindrical hole. The comparison will be performed by means of discharge coefficients and local and laterally averaged adiabatic film cooling effectiveness and heat transfer coefficients derived from experiments.
机译:冷却孔出口和冷却孔入口处的流动条件以非常不同的方式影响圆柱孔和扇形孔下游的冷却性能。流量参数变化的后果非常明显地取决于相应的孔几何形状。为了尽可能全面地了解变化的工作条件的特定效果,从而更好地理解主导机构,必须改变孔的几何形状。扩散器的膨胀角,孔的倾斜角和孔入口处的圆柱部分的长度被认为是扩散器孔的最重要的几何参数。 将分析恰好这些参数的变化对薄膜冷却性能的影响。为了更好地评估与孔轮廓相关的特征效应,将每个扩散孔与适当的圆柱孔进行比较。比较将通过排放系数以及从实验得出的局部和横向平均绝热膜冷却效率以及传热系数来进行。

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