摘要
本文对目前国内外主要的耳片强度计算方法进行了简单的分析,在理论和试验基础上,提出了一套可以计算任意角度受载的耳片强度的方法,这些方法比较符合实际,又比较适合于工程计算,并已广泛应用于飞机设计。
This paper makes a brief analysis on the calculation method of strength for the main lugs adopted both at home and alroad. Based on the theory and experiment, a comprehensive method of strength analysis of lugs in any angle loading is put forword. This method tallies with the actual state of affairs and is more suitable for engineering calculation. It has been widely used in aircraft design.
出处
《机械设计》
CSCD
北大核心
1992年第1期22-25,共4页
Journal of Machine Design
