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MPC模块三分支联接湍流流场的数值模拟
引用本文:胡欲立,刘伯棠,徐海涛,帅石金.MPC模块三分支联接湍流流场的数值模拟[J].华中科技大学学报(自然科学版),1997(6).
作者姓名:胡欲立  刘伯棠  徐海涛  帅石金
作者单位:华中理工大学船舶和海洋工程系
基金项目:中船总国防预研基金,中国博士后科学基金
摘    要:用任意拉格朗日-欧拉(ALE)法模拟了MPC模块的二维定常可压缩湍流流场.以某一型号发动机的MPC排气系统为例,对仅支管进气及支管总管都进气两种情况获得了速度场和压力场,揭示了MPC模块三分支联接湍流流动特性,也为用ALE法模拟MPC模块三维流场奠定了基础.

关 键 词:MPC增压系统  数值模拟  流场

Numerical Simulation of the Turbulent Flow Field in MPC Exhaust Manifold Junctions
Hu Yuli Dept. of Naval Arch. & Ocean Eng.,HUST,Wuhan ,China. Liu Botang Xu Haitao Shuai Shijin.Numerical Simulation of the Turbulent Flow Field in MPC Exhaust Manifold Junctions[J].JOURNAL OF HUAZHONG UNIVERSITY OF SCIENCE AND TECHNOLOGY.NATURE SCIENCE,1997(6).
Authors:Hu Yuli Dept of Naval Arch & Ocean Eng  HUST  Wuhan  China Liu Botang Xu Haitao Shuai Shijin
Institution:Hu Yuli Dept. of Naval Arch. & Ocean Eng.,HUST,Wuhan 430074,China. Liu Botang Xu Haitao Shuai Shijin
Abstract:A two dimensional stationary compressible turbulent flow field in MPC exhaust manifold junctions is numerically simulated using the ALE method. With the MPC exhaust manifold junction of a given engine type as an example, the velocity fields and the contours of static pressure showing the turbulent flow features have been obtained for the case when gas enters only at the entrance of the ejecting nozzle or when gas enters simultaneously at the entrance of the ejecting nozzle and the main pipe.
Keywords:MPC    turbocharging system  numerical simulation  flow field
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