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MEAN LINE FLOW MODEL OF STEADY AND PULSATING FLOW OF A MIXED-FLOW TURBINE TURBOCHARGER

机译:混流涡轮增压器的稳态和脉动流平均线模型

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A one-dimensional investigation for a mixed-flow turbine turbocharger turbine is described in this paper. The main outcome of the research is to develop a validated procedure for turbine performance maps in both steady and pulsating flow. The approach is limited to a simple procedure that can be integrated in wave action codes and thus not requiring 2D or 3D calculations. The mass flow parameter map is used as an input for the investigation, thus requiring some knowledge of either from experiments or from mean line methods calculations. In this paper, the mass flow parameter is experimentally measured at the turbocharger facility in Imperial College. A realistic yet reduced-order model for turbine losses allows the prediction of the steady flow performance; the calibration of the model is performed at peak efficiency of the turbine for a given rotational speed. The loss model for steady flow is then extended for pulsating conditions and for presumed quasi-steady operation. Finally, the predicted turbine performance is compared with experimental data. The comparison between one-dimensional modeling and experimental data for steady flow condition has shown Relative Standard Deviation (RSD) range from 1.62 % to 11.62 %. Meanwhile, a good trend agreement has been achieved for pulsating flow condition.
机译:本文描述了混合流涡轮增压器涡轮的一维研究。该研究的主要成果是为稳态和脉动流中的涡轮机性能图开发经过验证的程序。该方法限于可以集成在波动函数代码中的简单过程,因此不需要2D或3D计算。质量流量参数图用作调查的输入,因此需要从实验或平均线方法计算中获得一些知识。在本文中,质量流量参数是在帝国理工学院的涡轮增压器设施中通过实验测量的。涡轮损耗的现实的但降阶的模型可以预测稳定的流量性能。对于给定的转速,模型的校准以涡轮机的峰值效率执行。然后,针对脉动条件和假定的准稳态运行,扩展了稳态流量的损失模型。最后,将预测的涡轮机性能与实验数据进行比较。一维建模和稳态流量实验数据的比较表明,相对标准偏差(RSD)的范围为1.62%至11.62%。同时,对于脉动流动条件已经达成了良好的趋势协议。

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