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NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A LOW ORDER RADIAL TURBINE MODEL FOR ENGINE-LEVEL OPTIMISATION OF TURBOCHARGER DESIGN

机译:涡轮增压器设计发动机级优化低阶径向涡轮机模型的数值和实验研究

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This paper presents the development and validation of a meanline model by means of numerical and experimental methods, to determine it's feasibility as an optimisation tool for tur-bocharger matching. Using a parametric turbine model, numerical experiments were conducted accounting for variations of several key turbine design parameters and a wide operating range. The resulting dataset was used to test the accuracy of the mean-line model when calibrated to a baseline design and thus evaluate it's ability of extrapolating to different designs. The loss models were examined in more detail, and a set of loss models which provided the most accurate results is presented. The meanline model was further validated experimentally using dynamometer test results of 6 turbine designs from the same parametric turbine model. The result showed that for design point and high power operation, an error of less than 3.1% and 2.0% was achieved for efficiency and mass flow parameter respectively. This led to the conclusion that the model would be sufficiently accurate to represent design changes relevant to turbocharger matching.
机译:本文通过数值和实验方法提出了平均模型的开发和验证,以确定它是Tur-Bocharger匹配的优化工具的可行性。使用参数涡轮机模型,对几个关键涡轮机设计参数的变化和宽操作范围进行了数值实验。得到的数据集用于测试校准到基线设计时平均线模型的准确性,从而评估推断到不同设计的能力。更详细地检查损耗模型,并提供了一组提供最准确的结果的损耗模型。使用来自相同参数涡轮模型的6个涡轮机设计的测功机测试结果进行了实验验证的平均模型。结果表明,对于设计点和高功率操作,分别为效率和质量流量参数达到了小于3.1%和2.0%的误差。这导致了结论,该模型将足够准确地表示与涡轮增压器匹配相关的设计变化。

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