燃气蒸汽式发射系统工作过程仿真

Working Process Simulation of Gas and Steam Launching System

摘要:

建立了燃气蒸汽式导弹发射动力系统的数学模型,在此基础上进行数值模拟。在特定初始条件下计算发射筒内的温度、压力,以及导弹运动的速度、加速度和位移随时间的变化规律。研究结果可供相关研究工作参考。

Abstract:

The mathematical model of the gas and steam launching system was established. Based on the analytical result, a set of systematic program was developed to indict the change laws of pressure, temperature,acceleration, velocity and displacement of missile with time. The solution can be used as relation work reference.