Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Haitong Wang, Yan’gang Wang, Si Wang, Fang Zhou, Hanru Liu
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引用次数: 0

Abstract

The image vortex model is widely used in lifting line method to predict the fl ow induced by the shroud and hub surface in ducted fan, but it does not perform well in lift fan design due to the zero far fi eld in fl ow. In this paper the theoretical defects and numerical error propagation characteristic of the image vortex model in simulating duct surface are studied. Then the vortex rings correction based on image vortex model is veri fi ed and applied in lifting line method. In order to test the improved method, a 150 mm diameter lift fan is designed by the modi fi ed lifting line method, after that, analyzed by the modi fi ed lifting line itself and RANS solver respectively. The results show that the contribution of the vortex rings at the rotor accounts for 50% of the total induced velocity, and it accounts for 35% at the stator, which veri fi es the necessity of the vortex rings correction. The performance of the rotor and stator geometry is consistent with the design expectation, the e ffi ciency is up to 90.97% by numerical simulation and 88.32% by experimental measurement, which con fi rms the reli-ability of the modi fi ed lifting line method developed in this paper especially on lift fan design.
基于涡环的改进提升线法及其在提升风机设计中的应用
升力线法中广泛采用像涡模型来预测导管式风机叶冠和轮毂表面诱导的气流,但由于气流中的远场为零,在升力风机设计中表现不佳。本文研究了像涡模型在模拟管道表面时的理论缺陷和数值误差传播特性。然后验证了基于图像涡模型的涡环校正方法,并将其应用于提升线法。为了验证改进后的方法,采用定矩提升线法设计了一个直径150mm的提升风机,然后分别用定矩提升线本身和RANS求解器进行了分析。结果表明,转子处涡流环的贡献占总感应速度的50%,定子处涡流环的贡献占总感应速度的35%,验证了涡流环校正的必要性。转子和定子几何形状的性能符合设计预期,数值模拟效率达90.97%,实验测量效率达88.32%,证实了本文提出的固定升力线方法特别是升力风机设计的可靠性。
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
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
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