2012
DOI: 10.1007/s11431-012-4934-2
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Three-dimensional aerodynamic optimization design of high-speed train nose based on GA-GRNN

Abstract: With the speed upgrade of the high-speed train, the aerodynamic drag becomes one of the key factors to restrain the train speed and energy saving. In order to reduce the aerodynamic drag of train head, a new parametric approach called local shape function (LSF) was adopted based on the free form surface deformation (FFD) method and a new efficient optimization method based on the response surface method (RSM) of GA-GRNN. The optimization results show that the parametric method can control the large deformation… Show more

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Cited by 40 publications
(18 citation statements)
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References 12 publications
(11 reference statements)
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“…Thus, grid-independent validation is firstly performed in the present paper with different amounts of spatial mesh that combine prism mesh near the wall and hexahedral mesh so as to assess the influence of different spatial mesh on the calculation results. With the thickness of the first prism layer meeting the requirement of the wall function (30 ≤ y + ≤ 50) that is valid to simulation the flow around high-speed trains Yao, Guo, & Yang, 2012), three sets of mesh are obtained in this paper by changing the number of grid layers in the boundary layer, increasing the mesh size and region. As can be seen in Figure 10, the value of y + of the body surface is mainly in the range from 30 to 50.…”
Section: Mesh Independence Validationmentioning
confidence: 99%
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“…Thus, grid-independent validation is firstly performed in the present paper with different amounts of spatial mesh that combine prism mesh near the wall and hexahedral mesh so as to assess the influence of different spatial mesh on the calculation results. With the thickness of the first prism layer meeting the requirement of the wall function (30 ≤ y + ≤ 50) that is valid to simulation the flow around high-speed trains Yao, Guo, & Yang, 2012), three sets of mesh are obtained in this paper by changing the number of grid layers in the boundary layer, increasing the mesh size and region. As can be seen in Figure 10, the value of y + of the body surface is mainly in the range from 30 to 50.…”
Section: Mesh Independence Validationmentioning
confidence: 99%
“…In order to obtain a streamlined design with excellent aerodynamic performance and improve the optimization efficiency of a train head's aerodynamic shape, many scholars have done a lot of work (Kwon et al, 2001;Lee & Kim, 2008;Sun, Song, & An, 2010;Vytla, Huang, & Penmetsa, 2010;Yao, Guo, & Yang, 2012). Lee and Kim (2008) developed an optimization algorithm that combines successive quadratic programming (SQP) optimization with a support vector machine in order to reduce micro-pressure.…”
mentioning
confidence: 99%
“…In this paper, the simulation condition is open air, so we employ incompressible unsteady flow to describe the flow field and adopt standard k - turbulence model to describe the flow field, relevant control equations are defined as follows [21]:…”
Section: Air Trajectories Analysis Of the Flow Fieldmentioning
confidence: 99%
“…Ikeda et al (2006) and Suzuki et al (2008) used B-spline curve to set up a parametric model of cross-sectional panhead, and optimized the shape of the cross-sectional contour of the panhead. Yao et al (2012) adopted a new parametric approach called local shape function based on the free form surface deformation, and a new optimization method based on the response surface method of genetic algorithm-general regression neural network (GA-GRNN). After optimization, the aerodynamic drag for a three carriage train was reduced by 8.7%.…”
Section: Introductionmentioning
confidence: 99%