摘要
本文在网络生成、边界条件、收敛准则等方面对KIVA程序进行了改进,以便模拟三分支管内气体流动;利用3维粒子动态分析仪(3D-PDA)测量了矩形截面三分支管试验件的3维速度场,以验证改进后的程序软件的可靠性;最后,以某一型号发动机的MPC排气系统为例,在只有支管进气和支管总管都进气两种情况下,模拟了MPC模件三分支管的3维定常湍流流动。由此揭示了MPC模件三分支管3维湍流的流动特性,并分析了引起其排气能量传递损失的主要因素。
The modification to KIVA program in grid generation,boundary conditions and convergence criterion has been made to simulate turbulent flow in manifold junctions.The three dimensional velocities of the manifold junction with a rectangular section were measured by use of three dimensional particle dynamic analyzer (3D PDA) to verify the modified KIVA program.In the last,taking a MPC exhaust manifold junction of a model engine for example, the authors simulate numerically its three dimensional steady turbulent flowfield, With that gas enters only at the entrance of the side duct, or gas enters simultaneously at the entrances of the side duct and the main duct.From the simulation results of the flowfields, the properities of three dimensional steady turbulent flow in MPC exhaust manifold junctions are revealed, and the factors which may causing its flow loss are analyed.
出处
《内燃机学报》
EI
CAS
CSCD
北大核心
1998年第4期460-468,共9页
Transactions of Csice
基金
船舶工业总公司国防预研基金
中国博士后科学基金
关键词
三分支管
湍流
数值模拟
发动机
排气系统
Manifold junction,Turbulent flow, Three dimensional numerical simulation, Experimental research