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 火箭垂直发射系统燃气流场的计算