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.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2002年第2期219-223,共5页
Acta Armamentarii
关键词
飞航导弹
运输过程
动力学
有限元
数值解法
winged missile, transportation, dynamics, finite element, numerical method
