摘要
讨论两种应用于导弹翼面结构的随机有限元法及其计算程序。试算表明，本方法与程序可适用于常用导弹翼面结构的可靠性预测与可靠性设计。
This paper discusses two random finite element methods and calculating program used for missile airfoil surface. The pilot calculation shows that the methods and programs are suitable for reliability forecast and design of ordinary missile airfoil surface construction.
出处
《上海航天》
1998年第6期8-12,共5页
Aerospace Shanghai
关键词
导弹翼面
可靠性设计
有限元法
程序
Missile airfoil surface Reliability design Finite element method Program
