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Modelling dynamic pantograph loads with combined numerical analysis
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作者 F.F.Jackson r.mishra +6 位作者 J.M.Rebelo J.Santos P.Antunes J.Pombo H.Magalhaes L.Wills M.Askill 《Railway Engineering Science》 EI 2024年第1期81-94,共14页
Appropriate interaction between pantograph and catenary is imperative for smooth operation of electric trains.Changing heights of overhead lines to accommodate level crossings,overbridges,and tunnels pose significant ... Appropriate interaction between pantograph and catenary is imperative for smooth operation of electric trains.Changing heights of overhead lines to accommodate level crossings,overbridges,and tunnels pose significant challenges in maintaining consistent current collection performance as the pantograph aerodynamic profile,and thus aerodynamic load changes significantly with operational height.This research aims to analyse the global flow characteristics and aerodynamic forces acting on individual components of an HSX pantograph operating in different configurations and orientations,such that the results can be combined with multibody simulations to obtain accurate dynamic insight into contact forces.Specifically,computational fluid dynamics simulations are used to investigate the pantograph component loads in a representative setting,such as that of the recessed cavity on a Class 800 train.From an aerodynamic perspective,this study indicates that the total drag force acting on non-fixed components of the pantograph is larger for the knuckle-leading orientation rather than the knuckle-trailing,although the difference between the two is found to reduce with increasing pantograph extension.Combining the aerodynamic loads acting on individual components with multibody tools allows for realistic dynamic insight into the pantograph behaviour.The results obtained show how considering aerodynamic forces enhance the realism of the models,leading to behaviour of the pantograph-catenary contact forces closely matching that seen in experimental tests. 展开更多
关键词 Pantograph-catenary interaction Pantograph aerodynamics Computational fluid dynamics Pantograph loads Current collection performance
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Computational Analysis of the Compressible Flow Driven by a Piston in a Ballistic Range
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作者 G.Rajesh r.mishra +1 位作者 H.G.Kang H.D.Kim 《Journal of Thermal Science》 SCIE EI CAS CSCD 2007年第4期360-369,共10页
弹道的范围长在象高速度的影响工程,射弹气体动力学和航空弹道学那样的许多设计领域里被采用了,自从它能在很短的时间创造一个极其高压的状态。因为弹道的范围的操作包括许多复杂现象,每个过程应该为设备的表演改进详细被理解。在设... 弹道的范围长在象高速度的影响工程,射弹气体动力学和航空弹道学那样的许多设计领域里被采用了,自从它能在很短的时间创造一个极其高压的状态。因为弹道的范围的操作包括许多复杂现象,每个过程应该为设备的表演改进详细被理解。在设备性能上有重要影响的主要进程之一是驱动程序气体的压缩进程。大多数在这个领域里可得到的研究几乎不详细讨论这现象并且因此在整个系统表演上缺乏它的效果的合适的理解。在现在的学习,计算分析被做了调查压缩的动态方面在一个弹道的范围的泵试管处理的液体并且估计它怎么影响弹道的范围的性能。获得的结果与可得到的试验性的数据被验证。以便评估系统性能,几个性能参数被定义。在泵试管之间增加的一个吃惊试管和弹道的范围的表演上的发射试管的效果是也学习的经分解。弹道的范围的性能能被泵试管和高压的试管参数和吃惊试管的增加的合适的选择显著地改进。 展开更多
关键词 导弹射程 可压缩流理论 活塞 震激管
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