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Simulation-based investigation of unsteady flow in near-hub region of a Kaplan Turbine with experimental comparison

机译:基于仿真的Kaplan涡轮近轮毂区域非定常流动研究与实验比较

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This paper presents a detailed comparison of steady and unsteady turbulent flow simulation results in the U9 Kaplan turbine draft tube with experimental velocity and pressure measurements. The computational flow domain includes the guide vanes, the runner and the draft tube. A number of turbulence models were studied, including the standard , RNG , SST and SST-SAS models. Prediction of the flow behavior in the conical section of the draft tube directly below the runner cone is very sensitive to the prediction of the separation point on the runner cone. The results demonstrate a significant increase in precision of the flow modeling in the runner cone region by using unsteady flow simulations compare to stage simulation. The prediction of the flow in the runner cone region, however, remains delicate, and no turbulence model could accurately predict the complex phenomena observed experimentally.
机译:本文通过实验速度和压力测量结果,对U9 Kaplan涡轮引流管中稳态和非稳态湍流模拟结果进行了详细的比较。计算流量域包括导向叶片,流道和引流管。研究了许多湍流模型,包括标准,RNG,SST和SST-SAS模型。在流道锥正下方的引流管圆锥形部分中的流动行为的预测对流道锥上分离点的预测非常敏感。结果表明,与阶段模拟相比,使用非稳态流动模拟可以显着提高流道锥区域流动模型的精度。然而,对流道锥区域中的流动的预测仍然是微妙的,并且没有湍流模型可以准确地预测实验观察到的复杂现象。

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