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Effects of varying Reynolds number, blowing ratio, and internal geometry on trailing edge cutback film cooling

机译:雷诺数,吹塑比和内部几何形状的变化对后缘切边薄膜冷却的影响

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Three-dimensional mean velocity and concentration fields have been measured for a water flow in a pressure side cutback trailing edge film cooling geometry consisting of rectangular film cooling slots separated by tapered lands. Three-component mean velocities were measured with conventional magnetic resonance velocimetry, while time-averaged concentration distributions were measured with a magnetic resonance concentration technique for flow at two Reynolds numbers (Re) differing by a factor of 2, three blowing ratios, and with and without an internal pin fin array in the coolant feed channel. The results show that the flows are essentially independent of Re for the regime tested in terms of the film cooling surface effectiveness, normalized velocity profiles, and normalized mean streamwise vorticity. Blowing ratio changes had a larger effect, with higher blowing ratios resulting in surface effectiveness improvements at downstream locations. The addition of a pin fin array within the slot feed channel made the spanwise distribution of coolant at the surface more uniform. Results are compared with transonic experiments in air at realistic density ratios described by Holloway et al. (2002a).
机译:已经测量了水的三维平均速度场和浓度场,该水流在压力侧切开后缘薄膜冷却几何形状中,该几何形状由由锥形凸台隔开的矩形薄膜冷却槽组成。使用常规磁共振测速仪测量三组分平均速度,同时使用磁共振浓缩技术测量两个雷诺数(Re)相差2倍,三个吹气比的流量的时间平均浓度分布,以及冷却液进料通道中没有内部销翅片阵列。结果表明,就膜冷却表面效率,归一化速度分布和归一化平均流向涡度而言,对于所测试的方案,流量基本上与Re无关。鼓风比的变化具有更大的影响,更高的鼓风比导致下游位置表面效率的提高。在缝隙进料通道内增加了一个针翅阵列,使冷却剂在表面的跨度分布更加均匀。将结果与Holloway等人在实际密度比下在空气中进行的跨音速实验进行比较。 (2002a)。

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