Effect of wing height layout on the aerodynamic performance ofhigh-speed train

Purpose This paper aims to investigate the effect of different wing height layouts on the aerodynamic performance and flow structure of high-speed train, in a train-wing coupling method with multiple tandem wings installed on the train roof. Design/methodology/approach The improved delayed detached eddy simulation method based on shear stress transport k-ω turbulence model has been used to conduct computational fluid dynamics simulation on the train with three different wing height layouts, at a Reynolds number of 2.8 × 106. The accuracy of the numerical method has been validated by wind tunnel experiments. Findings The wing height layout has a significant effect on the lift, while its influence on the drag is weak. There are three distinctive vortex structures in the flow field: wingtip vortex, train body vortex and pillar vortex, which are influenced by the variation in wing height layout. The incremental wing layout reduces the mixing and merging between vortexes in the flow field, weakening the vorticity and turbulence intensity. This enhances the pressure difference between the upper and lower surfaces of both the train and wings, thereby increasing the overall lift. Simultaneously, it reduces the slipstream velocity at platform and trackside heights. Originality/value This paper contributes to understanding the aerodynamic characteristics and flow structure of a high-speed train coupled with wings. It provides a reference for the design aiming to achieve equivalent weight reduction through aerodynamic lift synergy in trains.

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Publication Details

Journal
International Journal of Numerical Methods for Heat &amp Fluid Flow
Published
2024-08-12
DOI
https://doi.org/10.1108/hff-02-2024-0136
Citations
5
Primary Topic
Aerodynamics and Fluid Dynamics Research
Type
article
Field-Weighted Citation Impact
6.49
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article

Effect of wing height layout on the aerodynamic performance ofhigh-speed train

Xiaohui Xiong, Xinran Wang, Kaiwen Wang, Jiaxu Geng
5 citations
International Journal of Numerical Methods for Heat &amp Fluid Flow
Aerodynamics and Fluid Dynamics Research
6.49
article

Effect of wing height layout on the aerodynamic performance ofhigh-speed train

Xiaohui Xiong, Xinran Wang, Kaiwen Wang, Jiaxu Geng
article en
5 citations

Abstract

Purpose This paper aims to investigate the effect of different wing height layouts on the aerodynamic performance and flow structure of high-speed train, in a train-wing coupling method with multiple tandem wings installed on the train roof. Design/methodology/approach The improved delayed detached eddy simulation method based on shear stress transport k-ω turbulence model has been used to conduct computational fluid dynamics simulation on the train with three different wing height layouts, at a Reynolds number of 2.8 × 106. The accuracy of the numerical method has been validated by wind tunnel experiments. Findings The wing height layout has a significant effect on the lift, while its influence on the drag is weak. There are three distinctive vortex structures in the flow field: wingtip vortex, train body vortex and pillar vortex, which are influenced by the variation in wing height layout. The incremental wing layout reduces the mixing and merging between vortexes in the flow field, weakening the vorticity and turbulence intensity. This enhances the pressure difference between the upper and lower surfaces of both the train and wings, thereby increasing the overall lift. Simultaneously, it reduces the slipstream velocity at platform and trackside heights. Originality/value This paper contributes to understanding the aerodynamic characteristics and flow structure of a high-speed train coupled with wings. It provides a reference for the design aiming to achieve equivalent weight reduction through aerodynamic lift synergy in trains.

International Journal of Numerical Methods for Heat &amp Fluid FlowVol. 34(10)
Central South University (CN), State Key Laboratory of Vehicle NVH and Safety Technology (CN), Ministry of Education and Child Care (CA), Changsha University of Science and Technology (CN)
Affordable and clean energy
Openalex Percentile: Top 4%
Aerodynamics and Fluid Dynamics Research
6.49
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