A Reliable Update of the Ainley and Mathieson Profile and Secondary Correlations

IF 1.3 Q2 ENGINEERING, AEROSPACE
Yumin Liu, P. Hendrick, Z. Zou, F. Buysschaert
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引用次数: 2

Abstract

Empirical correlations are still fundamental in the modern design paradigm of axial turbines. Among these, the prominent Ainley and Mathieson correlation (Ainley D. and Mathieson G., 1951, “A Method of Performance Estimation for Axial-Flow Turbines,” ARC Reports and Memoranda No. 2974) and its derivatives, plays a crucial role. In this paper, the underlying assumptions of the aforementioned models are discussed by means of a descriptive review, whilst an attempt is made to enhance their reliability and, potentially, accuracy in performance estimations. Closer investigation reveals an intriguing misuse of the lift coefficient in the secondary loss. In light of this, an enhanced model that, notably, builds upon the Zweifel criterion and the vortex penetration depth concept is developed and discussed. The obtained accuracy is subsequently assessed through CFD computations, employing a database comprising 109 cascades. The results indicate a 50% probability of achieving the ±15% error interval, which is twice as good as the most recent Aungier model (Aungier R., 2006, “Turbine Aerodynamics: Axial-Flow and Radial-Inflow Turbine Design and Analysis”, ASME Press, New York). Furthermore, the reliability of the proposed model is demonstrated by a reconstruction of the Smith chart, on the one hand, and a performance analysis, on the other. The reconstruction exhibits contours that conform to the original. The results of the performance study are compared with the CFD solutions of eight cascades working in off design conditions and confirm the need of the additionally included turbine design parameters, such as the axial velocity and the meanline radius ratios.
Ainley和Mathieson剖面和次级相关性的可靠更新
在轴向涡轮机的现代设计范式中,经验关联仍然是基本的。其中,突出的Ainley和Mathieson相关性(Ainley D.和Mathieson G., 1951,“一种轴流涡轮机性能估计方法”,ARC报告和备忘录2974号)及其衍生物起着至关重要的作用。在本文中,通过描述性审查的方式讨论了上述模型的基本假设,同时试图提高它们的可靠性,并可能提高性能估计的准确性。进一步的调查揭示了二次损失中升力系数的一个有趣的误用。鉴于此,本文提出并讨论了一个基于茨威费尔准则和涡旋穿透深度概念的增强型模型。随后,采用包含109个级联的数据库,通过CFD计算评估获得的精度。结果表明,达到±15%误差区间的概率为50%,这是最新的Aungier模型的两倍(Aungier R., 2006,“涡轮空气动力学:轴向流和径向流入涡轮设计与分析”,ASME出版社,纽约)。此外,通过史密斯图的重建和性能分析,一方面证明了所提出模型的可靠性。重建的轮廓与原来的轮廓一致。将性能研究结果与8个非设计工况下叶栅的CFD计算结果进行了比较,确定了额外加入轴向速度和平均半径比等涡轮设计参数的必要性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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