In this paper, the numerical results of burning gas flow in the vertical launch system of a rocket are reported. A second-order accurate MUSCL scheme is employed. 本文报导了火箭垂直发射系统(VLS)燃气流场的数值计算结果,在计算中采用二阶精度的MUSCL格式。
Calculation of burning gas flow in the vertical launch system of a rocket 火箭垂直发射系统(VLS)燃气流场的计算
It introduces the merits of inner guide simplicity of structure, high space utilization ratio, high efficiency in common usage, high-security fitting for proper exhaust of combustible airflow of vertical launch system. 认为燃气流内排导由于具备结构简单、空间利用率高、通用性强、安全性高等优点,适合于垂直发射燃气流的合理排导;
Exhaust of Combustible Airflow of Box-Shaped Structure Vertical Launch System(VLS) 箱式垂直发射系统(VLS)燃气流的排导
Vertical launch missile system 利剑直刺苍穹&全球垂直发射导弹系统扫描