会议专题

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

第13届国际断裂大会(ICF2013)

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)