期刊文献+

基于最优拉丁超立方设计的高速列车流线型头型减阻优化研究 被引量:4

Resistance Reduction of High Speed Train Streamline Head Based on Optimal Latin Hypercube Design
下载PDF
导出
摘要 为研究流线型头型对高速列车气动阻力性能的影响特性,利用B-Spline曲面建立高速列车流线型头型三维参数化模型,并提取5个头型设计变量。在此基础上,结合最优拉丁超立方设计和计算流体力学方法,研究高速列车流线型头型控制型线对高速列车气动阻力的影响特性,确定出关键控制型线。计算结果表明:随着流线型头型控制型线的变化,高速列车气动阻力发生明显改变,变化范围为3183~3509 N,相对变化量约为10.2%。最优设计点头型下的气动阻力较原始头型降低3.5%。对高速列车气动阻力影响最为显著的控制型线为纵向对称线,其次是车底最大轮廓线和水平最大轮廓线,而鼻尖高度控制线和中部辅助控制线对高速列车气动阻力的影响相对较小。 In order to study the influence of streamline head on aerodynamic resistance performance of high speed train,a three-dimensional parametric model of streamline head of high speed train is established with Bspline surface,and five design variables are extracted.On this basis,combined with the optimal Latin hypercube design and computational fluid dynamics method,the influence characteristics of the streamline head control profile of high speed train on the aerodynamic resistance of high speed train are studied,and the key control profile is determined.The results show that the aerodynamic resistance of high speed train varies obviously with the change of streamline head control profile with range of variation of 3183~3509 N,and the relative variation is about 10.2%.The aerodynamic resistance of the optimal design head type is 3.5%lower than that of the original head type.The most significant control line influencing high speed train aerodynamic resistance is the longitudinal symmetry line,followed by the bottom maximum contour line and the horizontal maximum contour line,while the nose height control line and the middle auxiliary control line have relatively small impact on train aerodynamic resistance.
作者 刘加利 LIU Jiali(CRRC Qingdao Sifang Co Ltd,Qingdao Shandong 266111,China)
出处 《中国铁路》 2020年第2期81-86,共6页 China Railway
基金 国家重点研发计划项目(2016YFB1200504-F) 中国铁路总公司科技研究开发计划项目(2015J009-D)
关键词 高速列车 流线型头型 最优拉丁超立方设计 气动阻力 鼻尖高度 high speed train streamline head optimal Latin hypercube design aerodynamic resistance nose height
  • 相关文献

参考文献8

二级参考文献125

共引文献163

同被引文献41

引证文献4

二级引证文献6

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部