针对某车型排气尾管低频噪声大问题,利用GT-Power软件建立发动机工作过程与排气消声器耦合仿真分析模型,对排气消声器声学性能和空气动力学性能进行数值计算,分析排气尾管低频噪声大的原因。依据分析结果提出消声器结构优化方案,制作优...针对某车型排气尾管低频噪声大问题,利用GT-Power软件建立发动机工作过程与排气消声器耦合仿真分析模型,对排气消声器声学性能和空气动力学性能进行数值计算,分析排气尾管低频噪声大的原因。依据分析结果提出消声器结构优化方案,制作优化样件进行整车排气尾管噪声试验。试验结果表明,低转速时消声器插入损失提高5d B^7 d B(A),2阶次噪声整体降低,低频噪声问题明显改善。展开更多
The effects of the different landforms of the cutting leeward on the aerodynamic performance of high-speed trains were analyzed based on the three-dimensional, steady, and incompressible Navier-Stokes equation and k-e...The effects of the different landforms of the cutting leeward on the aerodynamic performance of high-speed trains were analyzed based on the three-dimensional, steady, and incompressible Navier-Stokes equation and k-e double-equation turbulent model. Results show that aerodynamic forces increase with the cutting leeward slope decreasing. The maximum adding value of lateral force, lift force, and overturning moment are 147%, 44.3%, and 107%, respectively, when the slope varies from 0.67 to -0.67, and the changes in the cutting leeward landform have more effects on the aerodynamic performance when the train is running in the line No. 2 than in the line No. 1. The aerodynamic forces, except the resistance force, sharply increase with the slope depth decreasing. By comparing the circumstance of the cutting depth H=-8 m with that of H=8 m, the resistance force, lateral force, lift force, and overturning moment increase by 26.0%, 251%, 67.3% and 177%, respectively. With the wind angle increasing, the resistance force is nonmonotonic, whereas other forces continuously rise. Under three special landforms, the changes in the law of aerodynamic forces with the wind angle are almost similar to one another.展开更多
The basic head shape of high-speed train is determined by its longitudinal type-line(LTL),so it is crucial to optimize its aerodynamic performance.Based on the parametric modeling of LTL constructed by non-uniform rel...The basic head shape of high-speed train is determined by its longitudinal type-line(LTL),so it is crucial to optimize its aerodynamic performance.Based on the parametric modeling of LTL constructed by non-uniform relational B-spline(NURBS)and the fluctuation pressure obtained by large eddy simulation(LES),the Kriging surrogate model(KSM)of LTL was constructed for low aerodynamic noise,and the accuracy of the KSM was improved gradually by adding the sample point with maximum expected improvement(EI)and the optimal point from optimization.The optimal objective was searched with genetic algorithm(GA).The results show that the total fluctuation pressure level(FPL)of the optimal LTL can be 8.7 dB less than that of original one,and the shape optimization method is feasible for low aerodynamic noise design.展开更多
文摘建立了接触网和受电弓子系统的有限元模型和空气动力学模型,采用MSC-Marc及STAR-CD软件,研究受电弓动态受流性能和空气动力学性能.通过接触实现2个子系统耦合,对弓网进行动态仿真;通过高速受电弓三维模型,对受电弓高速空气动力学性能进行仿真.仿真结果表明:简单链型悬挂比弹性链型悬挂接触线动态抬升量和平均接触压力均小,在速度250 km/h时,气流对受电弓产生的抬升力约为12 N,空气阻力为550 N.
文摘针对某车型排气尾管低频噪声大问题,利用GT-Power软件建立发动机工作过程与排气消声器耦合仿真分析模型,对排气消声器声学性能和空气动力学性能进行数值计算,分析排气尾管低频噪声大的原因。依据分析结果提出消声器结构优化方案,制作优化样件进行整车排气尾管噪声试验。试验结果表明,低转速时消声器插入损失提高5d B^7 d B(A),2阶次噪声整体降低,低频噪声问题明显改善。
基金Project(U1134203) supported by the National Natural Science Foundation of ChinaProject(132014) supported by Fok Ying Tong Education Foundation,ChinaProject(2011G006) supported by the Technological Research and Development Program of the Ministry of Railways,China
文摘The effects of the different landforms of the cutting leeward on the aerodynamic performance of high-speed trains were analyzed based on the three-dimensional, steady, and incompressible Navier-Stokes equation and k-e double-equation turbulent model. Results show that aerodynamic forces increase with the cutting leeward slope decreasing. The maximum adding value of lateral force, lift force, and overturning moment are 147%, 44.3%, and 107%, respectively, when the slope varies from 0.67 to -0.67, and the changes in the cutting leeward landform have more effects on the aerodynamic performance when the train is running in the line No. 2 than in the line No. 1. The aerodynamic forces, except the resistance force, sharply increase with the slope depth decreasing. By comparing the circumstance of the cutting depth H=-8 m with that of H=8 m, the resistance force, lateral force, lift force, and overturning moment increase by 26.0%, 251%, 67.3% and 177%, respectively. With the wind angle increasing, the resistance force is nonmonotonic, whereas other forces continuously rise. Under three special landforms, the changes in the law of aerodynamic forces with the wind angle are almost similar to one another.
基金Projects(50975289,51275531)supported by the National Natural Science Foundation of ChinaProject(201104514)supported by the Special China Postdoctoral Science Foundation,ChinaProject(20100471229)supported by China Postdoctoral Science Foundation
文摘The basic head shape of high-speed train is determined by its longitudinal type-line(LTL),so it is crucial to optimize its aerodynamic performance.Based on the parametric modeling of LTL constructed by non-uniform relational B-spline(NURBS)and the fluctuation pressure obtained by large eddy simulation(LES),the Kriging surrogate model(KSM)of LTL was constructed for low aerodynamic noise,and the accuracy of the KSM was improved gradually by adding the sample point with maximum expected improvement(EI)and the optimal point from optimization.The optimal objective was searched with genetic algorithm(GA).The results show that the total fluctuation pressure level(FPL)of the optimal LTL can be 8.7 dB less than that of original one,and the shape optimization method is feasible for low aerodynamic noise design.
