Study of aerodynamic characteristics of a high-speed train with wings moving through a tunnel

被引:1
|
作者
Wang, Tian-tian [1 ,2 ]
Huang, Da-fei [1 ]
Wang, Jun-yan [2 ]
Shi, Fang-cheng [1 ]
Zhu, Yan [3 ]
Zhang, Lei [2 ]
Gao, Guang-jun [2 ]
机构
[1] Hunan Univ, Coll Mech & Vehicle Engn, Changsha 410082, Peoples R China
[2] Cent South Univ, Sch Traff & Transportat Engn, Key Lab Traff Safety Track, Minist Educ, Changsha 410075, Peoples R China
[3] CRRC Changchun Railway Vehicles Co Ltd, Changchun 130062, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
high-speed train with wings; wing attack angle; lift; pressure; tunnel; PRESSURE WAVES; SIZE;
D O I
10.1007/s11771-024-5597-4
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
A high-speed train with wings (HSTW) is a new type of train that enhances aerodynamic lift by adding wings, effectively reducing gravity, to reduce the wear and tear of wheels and rails. This study, based on the RNG k-epsilon turbulence model and employing a sliding grid method, investigates the aerodynamic effects of HSTWs with different angles of attack when passing through tunnels. The precision of numerical simulation method is validated by data obtained through a moving model test. The results show that the lift of the HSTW increases upon entering the tunnel, with an average lift in the tunnel of 33.3% greater than that in the open air. The angle of attack is reduced from 12.5 degrees to 7.5 degrees when the train enters the tunnel, which can better reduce the lift fluctuations and concurrently also reduce the peak-to-peak pressure on the surface of the train and the tunnel, which is conducive to the train passing through the tunnel smoothly; hence, the angle of attack for the HSTW when passing through a tunnel is adjusted 7.5 degrees. Furthermore, a comparison between the high-speed trains with and without wings demonstrates that the frontal pressure of the trains increases due to the blockage effect caused by the wings, while the rear of the trains experiences decreased pressure, which is primarily influenced by the wing wake. The outcomes of this study provide technical support for HSTWs passing smoothly through tunnels.
引用
收藏
页码:1003 / 1016
页数:14
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