摘要
利用功能强大的大型有限元分析软件对某导弹尾翼进行了实体建模和强度分析,具有很高的存贮和计算效率,与实验结果进行比较,说明所用方法是切实可行和有效的。
Applying powerful and large scale finite-element analysis software performs entity modelling and strength analysis for missile empenage,which has high efficiency for storage and calculation.By comparison with experiment result shows that this method is feasible and effective.
出处
《机械管理开发》
2006年第3期88-88,90,共2页
Mechanical Management and Development
