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有限空间轴对称射流流场的数值模拟
引用本文:郭金基 刘绍球. 有限空间轴对称射流流场的数值模拟[J]. 宇航学报, 1993, 14(4): 16-23
作者姓名:郭金基 刘绍球
作者单位:中山大学力学系(郭金基,陈彤),国家航天局二院(刘绍球)
摘    要:
本文在к-ε紊流模型下,采用罚有限元法对有限空间轴对称射流流场进行数值模拟。引用罚函数优化迎风格式和退化积分,建立有限元解法的数值矩阵,在不同截面上求得工,压力和紊流参数分布,计算结果与实验数据十分接近。本文研究结果可应用于火箭发动机的喷射设计和射流量论的研究。

关 键 词:有限空间射流 有限元法 火箭发动机

NUMERICAL SIMULATION OF FLUIDIC FIELD OF THE AXISYMMETRIC CONFINED SPACE JET
Guo Jinje Cben Tong Liu Shaogiu. NUMERICAL SIMULATION OF FLUIDIC FIELD OF THE AXISYMMETRIC CONFINED SPACE JET[J]. Journal of Astronautics, 1993, 14(4): 16-23
Authors:Guo Jinje Cben Tong Liu Shaogiu
Abstract:
In this paper, numerical simulation of fhlidic field of the axisymmetric confined space jet with k-e turbulent model are performed by the penalty finite element method. Author introduces the penalty function, optimal upwind and vduced integration et, the numerical matrixs of finite element of the solution are estabished. The colculated results concerning distbioution of velocity , pressure, turbulent parameters at different cross sections ane obtained , and good agreetmentwith the pervious experiment data. At the end of this paper,the research,results are used to design for ejector of rocket motor and theory study of jet.
Keywords:Confined space jet  k-e Turbulent model  penalty finite element method   Ejector   Jet motor
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