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PREDICTION OF THE PRESSURE PULSATION IN A DRAFT TUBE FOR A PART LOAD CONDITION USING THE LES APPROACH

机译:利用LES方法预测部分负载条件下的管内压力脉动。

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The present paper focuses on the vortex rope that arises when operating a model Francis turbine at a part load condition: 65% of the Best Efficiency Point (BEP). The investigation is performed numerically using the Large Eddy Simulation (LES) approach with the Dynamic Smagorinsky Model (DSM). Such approach and turbulence model are implemented in the overset finite element open source code, FrontFlow/blue (FFB). Furthermore, a cavitation model is implemented allowing computations for non-cavitating and cavitating conditions. Thanks to the use of the K supercomputer, located at Kobe in Japan, and to the use of large computational mesh (123 million elements), it is shown that the frequency of the precession of the vortex rope as well as the head can be accurately computed. However, the predicted amplitude of the fluctuation did not fully agree with the experiment. Differences in a particular region near the back side of the elbow are about 35%. A comparison between the variation of the size of the vortex rope and the swirl number has been investigated and showed a clear relation. The location of the vortex rope and the minimum of the pressure were also investigated and showed that they do not fully share the same location. Furthermore, in a preliminary study to the computation of the cavitating vortex rope, computations of the flow around a Clark-11.7% hydrofoil under cavitation condition and for angles of attack of 2° and 8° are carried out. The results showed the common issue for this computation, i.e. the sharp change of the lift and drag coefficients could not be accurately predicted. Currently underway are the computation of the cavitating vortex rope. The effect of the cavitation on the vortex rope will be studied and reported at a later stage.
机译:本文着重研究在部分负荷条件下运行模型弗朗西斯涡轮机时产生的涡流绳:最​​佳效率点(BEP)的65%。使用大涡模拟(LES)方法和动态Smagorinsky模型(DSM)进行数值研究。这种方法和湍流模型是在有限有限元开放源代码FrontFlow / blue(FFB)中实现的。此外,实现了空化模型,允许计算非空化和空化条件。由于使用了位于日本神户的K超级计算机,并且使用了较大的计算网格(1.23亿个元素),因此可以证明旋涡进动和头部的进动频率可以准确地进行。计算的。但是,波动的预测幅度与实验不完全一致。在肘部后侧附近的特定区域中的差异约为35%。已经研究了涡流绳的尺寸变化与旋流数之间的比较,并显示出明确的关系。还对涡流绳的位置和最小压力进行了调查,结果表明它们没有完全共享相同的位置。此外,在对空化涡流绳的计算的初步研究中,进行了在空化条件下以及迎角为2°和8°的Clark-11.7%水翼周围流动的计算。结果表明了该计算的共同问题,即不能准确地预测升力和阻力系数的急剧变化。目前正在进行的是空化涡流绳的计算。空化对涡流绳的影响将在以后的阶段进行研究和报告。

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