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THE EFFECT OF WAKE PASSING ON A FLOW SEPARATION IN A LOW PRESSURE TURBINE CASCADE

机译:唤醒通过对低压涡轮机级联流动分离的影响

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This paper describes an investigation into the effect that passing wakes have on a separation bubble that exists on the pressure surface and near the leading edge of a low pressure turbine blade. Previous experimental studies have shown that the behaviour of this separation is strongly incidence dependent and that it responds to its disturbance environment. The results presented in this paper examine the effect of wake passing in greater detail. Two dimensional, Reynolds averaged, numerical predictions are first used to examine qualitatively the unsteady interaction between the wakes and the separation bubble. The separation is predicted to consist of spanwise vortices whose development is in phase with the wake passing. However, comparison with experiments shows that the numerical predictions exaggerate the coherence of these vortices and also overpredict the time-averaged length of the separation. Nonetheless, experiments strongly suggest that the predicted phase locking of the vortices in the separation onto the wake passing is physical.
机译:本文描述了对在压力表面上存在的分离气泡的效果和低压涡轮叶片的前缘附近的效果的研究。以前的实验研究表明,这种分离的行为依赖性强烈发生,并且它响应其扰动环境。本文提出的结果介绍了更详细的唤醒过程的效果。二维,雷诺平均,首先使用数值预测来检查唤醒和分离气泡之间的定性相互作用。预测分离是由尾动通过的血管涡旋组成,其开发与唤醒传递相位。然而,与实验的比较表明,数值预测夸大了这些涡流的相干性,并且还超越了分离的时间平均长度。尽管如此,实验强烈建议,预测阶段锁定在分离到唤醒过程中的分离是物理的。

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