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MPC模块三分支联接湍流流场的数值模拟
Numerical Simulation of the Turbulent Flow Field in MPC Exhaust Manifold Junctions
【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.
【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.
【基金】 中船总国防预研基金,中国博士后科学基金
- 【文献出处】 华中理工大学学报 ,JOURNAL OF HUAZHONG UNIVERSITY OF SCIENCE AND TECHNOLOGY , 编辑部邮箱 ,1997年06期
- 【分类号】TK413.52
- 【被引频次】7
- 【下载频次】44