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Numerical simulation of unsteady flows through a radial turbine

机译:不稳定流过径向汽轮机的数值模拟

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The article deals with the numerical simulation of unsteady flows through the turbine part of the turbocharger. The main focus of the article is the extension of the in-house CFD finite volume solver for the case of unsteady flows in radial turbines and the coupling to an external zero-dimensional model of the inlet and outlet parts. In the second part, brief description of a simplified one-dimensional model of the turbine is given. The final part presents a comparison of the results of numerical simulations using both the 3D CFD method and the 1D simplified model with the experimental data. The comparison shows that the properly calibrated 1D model gives accurate predictions of mass flow rate and turbine performance at much less computational time than the full 3D CFD method. On the other hand, the more expensive 3D CFD method does not need any specific calibration and allows detailed inspections of the flow fields.
机译:该物品涉及不稳定流过涡轮增压器的涡轮机的数值模拟。 该物品的主要焦点是延伸内部CFD有限音量求解器,用于径向涡轮机中不稳定流动的情况,以及与入口和出口部分的外部零尺寸模型的耦合。 在第二部分中,给出了涡轮机的简化一维模型的简要描述。 最后一部分呈现了使用3D CFD方法和具有实验数据的1D简化模型的数值模拟结果的比较。 比较表明,适当校准的1D模型可以精确地预测质量流量和涡轮机性能,而不是完整的3D CFD方法。 另一方面,较贵的3D CFD方法不需要任何特定的校准,并允许流场的详细检查。

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