飞航导弹运输过程中的动力学计算  

CALCULATION ON DYNAMIC CHARACTERISTICS OF THE FUSELAGE OF WINGED MISSILES DURING THEIR TRANSPORTATION

作　　者：许诚[1] 侯志强[1] 李善高[1] 宋贵宝[1] 戴宇进[1] 

机构地区：[1]海军航空工程学院

出　　处：《兵工学报》2002年第2期219-223,共5页Acta Armamentarii

摘　　要：用动力学方法对飞航导弹弹体在运输过程中受到冲击的问题进行了研究。介绍了有限元方法在大型壳体动力学计算中的应用 ,对某型飞航导弹运输过程中弹体强度进行了数值计算和结果分析 。The problem of impact on the fuselage of winged missiles during their transportation was discussed. The dynamic strength of the fuselage of one type of winged missile was computed with the dynamic finite element and numerical methods. Some proposals were given.

关 键 词：飞航导弹 运输过程 动力学 有限元 数值解法 

分 类 号：TJ761.5[兵器科学与技术—武器系统与运用工程]