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Predictions of the Performance of a Radial Turbine With Different Modeling Approaches: Comparison of the Results From 1-D and 3-D CFD

机译:具有不同建模方法的径向涡轮机性能的预测:1-D和3-D CFD的结果比较

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In this paper, the performance of a radial turbine working under pulsatile flow conditions is computed with two different modeling approaches, time-resolved 1-dimensional (1-D) and 3-dimensional (3-D) CFD. The 1-D modeling approach is based on measured turbine maps which are used to compute the mass flow rate and work output from the turbine for a given expansion ratio and temperature at the inlet. The map is measured under non-pulsatile flow conditions, and in the 1-D method the turbine is treated as being a quasi-stationary flow device. In the 3-D CFD approach, a Large Eddy Simulation (LES) turbulence approach is used. The objective of LES is to explicitly compute the large scales of the turbulence while modeling the effects of the unresolved scales. Three different cases are considered, where the simplest case only consist of the turbine and the most complex case consist of an exhaust manifold and the turbine. Both time-resolved data, such as pressure ratio, temperature and shaft torque and time mean data from the two different modeling approaches are compared. The results show that the computed time mean shaft power differs between the two different modeling approaches with as much as 100%. Since the considered operation point for the engine in this study is 1500 rpm with wide open throttle, the turbine operates in an area where the turbine map is extrapolated. Only by using a few operation points from CFD to extend the map, an improvement is achieved for the 1-D results, but still the deviation is large. Also, the pressure ratio and temperature drop over the turbine differs for the used modeling approaches. The causes for the deviations are assessed and discussed to get a better understanding of eventually limitations of the 1-D modeling approach.
机译:在本文中,用两种不同的建模方法,时间分辨的1维(1-D)和三维(3-D)CFD计算在脉冲流动条件下工作的径向涡轮机的性能。 1-D建模方法基于测量的涡轮机映射,用于计算在入口处的给定的膨胀比和温度的涡轮机的质量流量和工作。在非脉动流动条件下测量地图,并且在1-D方法中,涡轮机被处理为准固定流量装置。在3-D CFD方法中,使用大涡流仿真(LES)湍流方法。 LES的目标是明确地计算湍流的大尺度,同时建模未解决的尺度的效果。考虑了三种不同的案例,其中最简单的情况仅由涡轮机和最复杂的情​​况组成,包括排气歧管和涡轮机。比较两次分辨的数据,例如压力比,温度和轴扭矩和两种不同建模方法的均值数据。结果表明,计算的时间平均轴功率在两种不同的建模方法之间不同,具有多达100%。由于本研究中的发动机的考虑操作点是具有宽开放式节流阀的1500转,涡轮机在涡轮机地图推断的区域中操作。只有通过使用来自CFD的一些操作点才能扩展地图,仅对1-D结果实现改进,但仍然偏差大。而且,涡轮机上的压力比和温度下降对于使用的造型方法而异。评估和讨论偏差的原因以更好地了解最终限制1-D模型方法。

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