A Meta-Model for Aerodynamic Properties of a Reversible Profile in Cascade With Variable Stagger and Solidity

Gino Angelini, T. Bonanni, A. Corsini, G. Delibra, L. Tieghi, D. Volponi
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引用次数: 3

Abstract

In this paper, a systematic CFD work is carried out with the aim to inspect the influence of different cascade parameters on the aerodynamic performance of a reversible fan blade profile. From the obtained results, we derive a meta-model for the aerodynamic properties of this profile. Through RANS simulations of different arrangements in cascades, the aerodynamic performance of airfoils are analyzed as Reynolds number, solidity, pitch angle and angle of attack are varied. The definition of a trial matrix allows the reduction of the minimum number of simulations required. The computed CFD values of lift and drag coefficients, stall margin and the zero-lift angle strongly depend on cascade configuration and differ significantly from standard panel method software predictions. In this work, X-Foil has been used as a benchmark. Particularly, the high influence of pitch angle and solidity is here highlighted, while a less marked dependence from the Reynolds number has been found. Meta-models for lift and drag coefficients have been later derived, and an analysis of variance has improved the models by reducing the number of significant factors. The application of the meta-models to a quasi-3D in-house software for fan performance prediction is also shown. The effectiveness of the derived meta-models is proven through a spanwise comparison of a reversible fan with the X-Foil based and meta-model based versions of the software and 3D fields from a standard CFD simulation. The meta-model improves the software prediction capability, leading to a very low global overestimation of the specific work of the fan.
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可变交错和固体度叶栅可逆叶型气动特性的元模型
本文进行了系统的CFD工作,考察了不同叶栅参数对可逆叶片型面气动性能的影响。根据得到的结果,我们推导了该型线气动特性的元模型。通过对叶栅不同布置方式的RANS仿真,分析了不同雷诺数、固体度、俯仰角和迎角对翼型气动性能的影响。试验矩阵的定义允许减少所需的最少模拟次数。升力和阻力系数、失速裕度和零升力角的CFD计算值在很大程度上取决于叶栅的配置,与标准面板方法软件预测的结果有很大不同。在这项工作中,X-Foil已被用作基准。特别地,这里强调了俯仰角和固体度的高影响,而发现了与雷诺数的不太明显的依赖性。升力和阻力系数的元模型后来被推导出来,方差分析通过减少显著因素的数量来改进模型。本文还展示了元模型在拟三维内部风机性能预测软件中的应用。通过对基于X-Foil和基于元模型的软件版本的可逆风扇的展向比较,以及标准CFD模拟的3D场,验证了推导出的元模型的有效性。该元模型提高了软件预测能力,导致风机具体工作的整体高估非常低。
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