喷管一维流场化学非平衡通用计算软件研制

推进技术 ›› 2001, Vol. 22 ›› Issue (4): 282-285.

喷管一维流场化学非平衡通用计算软件研制

王大鹏,蔡国飙

北京航空航天大学宇航学院!北京100083;北京航空航天大学宇航学院!北京100083

发布日期:2021-08-15

Chemical nonequilibrium general computational software design of nozzle one dimensional flow field

School of Astronautics, Beijing Univ. of Aeronautics and Astronautics,Beijing 100083, China;School of Astronautics, Beijing Univ. of Aeronautics and Astronautics,Beijing 100083, China

Published:2021-08-15

摘要/Abstract

摘要： 研制的火箭发动机一维喷管非平衡流通用计算软件 ,建立在一个统一的化学反应库之上。该通用计算软件可对推进剂元素为碳、氢、氧、氮、氟、氯的火箭发动机喷管进行一维化学非平衡流数值模拟。通过计算推进剂元素为氢、氧和碳、氢、氧、氮的喷管一维化学非平衡流 ,得到了喷管流场的速度、温度、密度、压力及各组分的质量百分比等参数 ,为工程设计提供了依据。

关键词: 反应动力学;喷管气流;非平衡流;数值仿真;仿真软件

Abstract: The general computational software of rocket engine one dimensional nozzle nonequilibrium flow , which is based on one unite chemical library, can simulate the flow field of rocket engine nozzle with the propellants consisted of carbon, hydrogen, oxygen, nitrogen, fluorine, and chlorine elements. By computing the nozzle flow field with the propellant elements of hydrogen, oxygen and carbon, hydrogen, oxygen, nitrogen, the fields of velocity, temperature, pressure and all species mass fraction were gotten. They can be referenced by designer.

Key words: Reaction kinetics;Nozzle flow;Nonequilibrium flow;Numerical simulation;Simulation software

王大鹏,蔡国飙. 喷管一维流场化学非平衡通用计算软件研制[J]. 推进技术, 2001, 22(4): 282-285.