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。
This paper simplifies the vertical launch vehicle as a cylindrical cantilever beam and builds the response to wind with any direction for the vehicle using random vibration theory.
本文将垂直发射飞行器简化为圆柱形悬臂梁，利用随机振动理论，建立了飞行器任意风向的响应。
This paper simplifies the vertical launch vehicle as a cylindrical cantilever beam and builds the response to wind with any direction for the vehicle using random vibration theory.
本文将垂直发射飞行器简化为圆柱形悬臂梁，利用随机振动理论，建立了飞行器任意风向的响应。
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