机翼高度布局对高速列车气动性能的影响

IF 4 3区 工程技术 Q1 MATHEMATICS, INTERDISCIPLINARY APPLICATIONS
Xiaohui Xiong, Jiaxu Geng, Kaiwen Wang, Xinran Wang
{"title":"机翼高度布局对高速列车气动性能的影响","authors":"Xiaohui Xiong, Jiaxu Geng, Kaiwen Wang, Xinran Wang","doi":"10.1108/hff-02-2024-0136","DOIUrl":null,"url":null,"abstract":"<h3>Purpose</h3>\n<p>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.</p><!--/ Abstract__block -->\n<h3>Design/methodology/approach</h3>\n<p>The improved delayed detached eddy simulation method based on shear stress transport <em>k</em>-<span>\n<mml:math display=\"inline\" xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"><mml:mtext>ω</mml:mtext></mml:math></span> 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 × 10<sup>6</sup>. The accuracy of the numerical method has been validated by wind tunnel experiments.</p><!--/ Abstract__block -->\n<h3>Findings</h3>\n<p>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.</p><!--/ Abstract__block -->\n<h3>Originality/value</h3>\n<p>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.</p><!--/ Abstract__block -->","PeriodicalId":14263,"journal":{"name":"International Journal of Numerical Methods for Heat & Fluid Flow","volume":"7 1","pages":""},"PeriodicalIF":4.0000,"publicationDate":"2024-08-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Effect of wing height layout on the aerodynamic performance ofhigh-speed train\",\"authors\":\"Xiaohui Xiong, Jiaxu Geng, Kaiwen Wang, Xinran Wang\",\"doi\":\"10.1108/hff-02-2024-0136\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<h3>Purpose</h3>\\n<p>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.</p><!--/ Abstract__block -->\\n<h3>Design/methodology/approach</h3>\\n<p>The improved delayed detached eddy simulation method based on shear stress transport <em>k</em>-<span>\\n<mml:math display=\\\"inline\\\" xmlns:mml=\\\"http://www.w3.org/1998/Math/MathML\\\"><mml:mtext>ω</mml:mtext></mml:math></span> 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 × 10<sup>6</sup>. The accuracy of the numerical method has been validated by wind tunnel experiments.</p><!--/ Abstract__block -->\\n<h3>Findings</h3>\\n<p>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.</p><!--/ Abstract__block -->\\n<h3>Originality/value</h3>\\n<p>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.</p><!--/ Abstract__block -->\",\"PeriodicalId\":14263,\"journal\":{\"name\":\"International Journal of Numerical Methods for Heat & Fluid Flow\",\"volume\":\"7 1\",\"pages\":\"\"},\"PeriodicalIF\":4.0000,\"publicationDate\":\"2024-08-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Numerical Methods for Heat & Fluid Flow\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.1108/hff-02-2024-0136\",\"RegionNum\":3,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"MATHEMATICS, INTERDISCIPLINARY APPLICATIONS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Numerical Methods for Heat & Fluid Flow","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1108/hff-02-2024-0136","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MATHEMATICS, INTERDISCIPLINARY APPLICATIONS","Score":null,"Total":0}
引用次数: 0

摘要

设计/方法/途径 在雷诺数为 2.8 × 106 的条件下,采用基于剪应力传输 k-ω 湍流模型的改进型延迟分离涡模拟方法,对具有三种不同翼高布局的列车进行了计算流体动力学模拟。研究结果机翼高度布局对升力有显著影响,而对阻力的影响较弱。流场中有三种不同的涡旋结构:翼尖涡旋、裙体涡旋和支柱涡旋,它们都受到翼高布局变化的影响。增量式机翼布局减少了流场中涡旋之间的混合和融合,削弱了涡度和湍流强度。这增强了列车和机翼上下表面之间的压力差,从而提高了整体升力。本文有助于理解高速列车与机翼耦合的气动特性和流动结构。它为旨在通过空气动力升力协同作用实现列车等效减重的设计提供了参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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.

求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
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
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信