Numerical research on two typical flow structures and aerodynamic drag characteristics of blunt-nosed trains

IF 4 3区 工程技术 Q1 MATHEMATICS, INTERDISCIPLINARY APPLICATIONS
Sha Zhong, Mingzhi Yang, Bosen Qian, Lei Zhang, Dongqing He, Tongtong Lin, Fue-Sang Lien
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引用次数: 0

Abstract

Purpose

This study aims to provide new insights into aerodynamic drag reduction for increasingly faster blunt-nosed trains, such as urban and freight trains. Specifically, this work investigates two distinctly different wake structures and associated aerodynamic drag of blunt-nosed trains.

Design/methodology/approach

Three typical cases of blunt-nosed trains with 1-, 2- and 3-m nose lengths are selected. The time-averaged and unsteady flow structures around the trains are analyzed using the improved delayed detached eddy simulation model and proper orthogonal decomposition method.

Findings

The simulation results indicate that for 2- and 3-m nose lengths, the flow separates at first and then reattaches to the slanted surface of the tail, with a pair of longitudinal vortices dominating the wake. In contrast, for the 1-m nose length case, the wake structure is characterized by complete separation, attributed to the larger curvature of the slanted tail surface. Consequently, the total time-averaged drag coefficient is reduced by 27.2% and 19.2% for the 1-m nose length case compared to the 2- and 3-m cases, respectively. Moreover, the predominant unsteady structures with Strouhal numbers St = 0.30 and St = 0.28 are detected in the near-wake of the 2- and 3-m nose length cases, respectively. These structures result from periodic vortex shedding at the lower slanted tail surface. In contrast, for the 1-m nose length case, the predominant unsteady structure with St = 0.19 is induced by the nearly periodic expansion and contraction of the upper bubbles.

Originality/value

Two distinctly different wake structures in blunt-nosed trains are identified. Unlike high-speed trains with longer, streamlined noses, for blunt-nosed trains, shorter nose lengths result in lower aerodynamic drag. Insights for reducing energy consumption in blunt-nosed trains are provided.

钝头列车两种典型流动结构及气动阻力特性的数值研究
本研究旨在为越来越快的钝头列车(如城市列车和货运列车)提供气动阻力减少的新见解。具体来说,这项工作研究了两种截然不同的尾流结构和相关的钝鼻列车气动阻力。设计/方法/方法选择了三个典型的钝鼻列车,鼻长分别为1米、2米和3米。采用改进的延迟分离涡模拟模型和适当的正交分解方法,对列车周围的时均流和非定常流结构进行了分析。结果表明,当机头长度为2 m和3 m时,气流先分离,然后重新附着在机尾的倾斜表面上,尾迹由一对纵向涡主导。相比之下,在机头长度为1m的情况下,尾迹结构的特点是完全分离,这是由于倾斜尾翼表面的曲率较大。因此,与机头长度为2米和3米的情况相比,机头长度为1米的情况下,总时间平均阻力系数分别降低了27.2%和19.2%。此外,在2 m和3 m机头长度的近尾迹中,分别检测到Strouhal数St = 0.30和St = 0.28的优势非定常结构。这些结构是由低倾斜尾翼表面周期性涡脱落造成的。而在1 m机头长度的情况下,St = 0.19的非定常结构主要是由上部气泡几乎周期性的膨胀和收缩引起的。原创性/价值在钝鼻列车中发现了两种截然不同的尾流结构。与高速列车的长流线型机头不同,对于钝头列车来说,较短的机头长度导致较低的空气动力阻力。提供了降低钝鼻列车能耗的见解。
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
9.50
自引率
11.90%
发文量
100
审稿时长
6-12 weeks
期刊介绍: The main objective of this international journal is to provide applied mathematicians, engineers and scientists engaged in computer-aided design and research in computational heat transfer and fluid dynamics, whether in academic institutions of industry, with timely and accessible information on the development, refinement and application of computer-based numerical techniques for solving problems in heat and fluid flow. - See more at: http://emeraldgrouppublishing.com/products/journals/journals.htm?id=hff#sthash.Kf80GRt8.dpuf
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