CLC number: U271.91; O355
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2017-10-12
Cited: 0
Clicked: 5814
Liang Zhang, Ji-ye Zhang, Tian Li, Ya-dong Zhang. Multi-objective aerodynamic optimization design of high-speed train head shape[J]. Journal of Zhejiang University Science A, 2017, 18(11): 841-854.
@article{title="Multi-objective aerodynamic optimization design of high-speed train head shape",
author="Liang Zhang, Ji-ye Zhang, Tian Li, Ya-dong Zhang",
journal="Journal of Zhejiang University Science A",
volume="18",
number="11",
pages="841-854",
year="2017",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A1600764"
}
%0 Journal Article
%T Multi-objective aerodynamic optimization design of high-speed train head shape
%A Liang Zhang
%A Ji-ye Zhang
%A Tian Li
%A Ya-dong Zhang
%J Journal of Zhejiang University SCIENCE A
%V 18
%N 11
%P 841-854
%@ 1673-565X
%D 2017
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A1600764
TY - JOUR
T1 - Multi-objective aerodynamic optimization design of high-speed train head shape
A1 - Liang Zhang
A1 - Ji-ye Zhang
A1 - Tian Li
A1 - Ya-dong Zhang
J0 - Journal of Zhejiang University Science A
VL - 18
IS - 11
SP - 841
EP - 854
%@ 1673-565X
Y1 - 2017
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A1600764
Abstract: To improve the aerodynamic performance of high-speed trains (HSTs) running in the open air, a multi-objective aerodynamic optimization design method for the head shape of a HST is proposed in this paper. A parametric model of the HST was established and seven design variables of the head shape were extracted. Sample points and their exact values of optimization objectives were obtained by an optimal Latin hypercube sampling (opt. LHS) plan and computational fluid dynamic (CFD) simulations, respectively. A Kriging surrogate model was constructed based on the sample points and their optimization objectives. Taking the total aerodynamic drag force and the aerodynamic lift force of the tail coach as the optimization objectives, the multi-objective aerodynamic optimization design was performed based on a non-dominated sorting genetic algorithm-II (NSGA-II) and the kriging model. After optimization, a series of Pareto-optimal head shapes were obtained. An optimal head shape was selected from the Pareto-optimal head shapes, and the aerodynamic performance of the HST with the optimal head shape was compared with that of the original train in conditions with and without crosswinds. Compared with the original train, the total aerodynamic drag force is reduced by 2.61% and the lift force of the tail coach is reduced by 9.90% in conditions without crosswind. Moreover, the optimal train benefits from lower fluctuations in aerodynamic loads in crosswind conditions.
This paper used CFD simulations,Kriging surrogate model and NSGA- II to optimize the aerodynamic drag and lift force of a high-speed train. Aerodynamic performance of the original train and optimal train in conditions within and without crosswinds were compared to confirm the improvements.
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