封闭式发射管内燃气流场数值模拟

推进技术 ›› 2002, Vol. 23 ›› Issue (1): 45-48.

封闭式发射管内燃气流场数值模拟

徐强,李军,廖光煊

中国科技大学火灾科学国家重点实验室安徽合肥230026;南京理工大学机械学院;江苏南京210094;中国科技大学火灾科学国家重点实验室安徽合肥230026

发布日期:2021-08-15

Numerical simulation of exhausted flow field in closed launch tube

State Key Lab. of Fire Science, China Univ. of Science and Technology, Hefei 230026, China;Coll.of Mechanics, Nanjing Univ. of Science and Technology, Nanjing 210094, China;State Key Lab. of Fire Science, China Univ. of Science and Technology, Hefei 230026, China

Published:2021-08-15

摘要/Abstract

摘要： 针对密封盖未及时开启造成发射装置损坏的问题进行了数值模拟。数值模拟采用多组分含有限速率非平衡化学反应流动模型 ,利用有限体积TVD数值格式求解方程组的对流项 ,对于化学反应造成的源项则采用四阶龙格库塔求解。研究表明密封盖不及时开启会在弹管间隙中形成破坏性的流动结构 ,在弹管间隙内存在着包含起始冲击波的激波振荡 ,这是导致发射装置损坏的重要因素

关键词: 导弹发射管;喷管气流;数值仿真

Abstract: Numerical simulation was conducted to study launching equipment damage caused by open delay of air proof cover. The flow model of multiple constituents finite rate unsteady state chemical reaction was used in numerical simulation, and finite volume TVD scheme used in solving convection term of the equation group. The source term generated by chemical reaction was solved by four order Runge Kutta algorithm. Study result shows shock oscillation with initial shock wave would be caused by open delay of the cover, and this harmful flow structure would lead to serious damage to launch equipment.

Key words: Missile launch tube;Nozzle flow;Numerical simulation

徐强,李军,廖光煊. 封闭式发射管内燃气流场数值模拟[J]. 推进技术, 2002, 23(1): 45-48.