摘要
采用SIMPLE算法,结合分散颗粒轨道(PSIC)模型,在同位网格上实现了喷管中跨声速两相湍流流场的数值模拟。根据Rhie,Chow提出的动量插值概念,以协变物理速度分量作为求解变量,完成跨声速气相流场的数值计算。湍流模式采用k-ε双方程模型,计算结果与提供的实验数据相符合。
Based on a colocated grid arrangement,combined with PSIC
model,SIMPLE algorithm was presented for the solution of two dimensional unsteady transonic
two phase turbulent flows in nozzles.The principle of momentum interpolation was applied
to the covariant physical velocity components, which were chosen as the dependent variables
in the simulation of the fluid field. The k ε model was utilized to describe the turbulent flow
process
出处
《推进技术》
EI
CAS
CSCD
北大核心
1999年第2期37-41,共5页
Journal of Propulsion Technology
关键词
喷管
二维流
跨音速
固体发动机
数值仿真
湍流
Nozzle flow, Two dimensional flow,Transonic flow,Numerical simulation