摘要
通过对机翼接头结构的有限元分析计算 ,得到接头各部分的应力数值 .将有限元计算和光弹性模型实验相结合 ,成功地把机翼接头各部分的应力场直观地展现出来 。
In this paper, technical data have been obtained precisely by computing and analyzing the structure of wing joint with finite element method. The stress distribution of wing joint is successfully exhibited by photoelastic experiment, and the design method of wing joint is improved.
出处
《扬州大学学报（自然科学版）》
CAS
CSCD
2002年第1期75-78,共4页
Journal of Yangzhou University：Natural Science Edition
