摘要
对用激光－莫尔偏折法测出的真实火箭燃气射流流场进行了数值仿真，在计算中采用了二阶精度的ＭＵＳＣＬ格式，将三维问题转化为二维问题，结果表明，理论计算与实验测量结果符合较好。
In this paper,the flow field for real rocket exhausted plume has been measured by use of Laser Moire deflectometry.In the meantime,a second order accurate MUSCL scheme is employed to compute the flow field.In the calculation,three dimeasional flow is converted into two dimensional case.The result fairly agrees with the theory of exhausted plume.
出处
《流体力学实验与测量》
CSCD
1998年第3期82-86,共5页
Experiments and Measurements in Fluid Mechanics
