Study on the fatigue crack growth behavior of 30CrMnSiA Straight Attachment Lugs
The finite element model of straight attachment lug subjected to axial or oblique loading is built by using finite element software,a cosine pin-bearing pressure distribution is applied on the pin-hole squeeze surface as a boundary condition.
attachment lug finite element method fatigue crack growth stress intensity factor the Paris law
LiMing Wu YuTing He HaiWei Zhang Teng Zhang Qing Shao
Aeronautics and Astronautics Engineering College,Air Force Engineering University,710038,China
国际会议
北京
英文
1-10
2013-06-16(万方平台首次上网日期,不代表论文的发表时间)