Zobrazeno 1 - 10
of 119
pro vyhledávání: '"CAO ZengQiang"'
Publikováno v:
Jixie qiangdu, Vol 42, Pp 947-953 (2020)
In order to improve the fatigue performance of the aviation lug structure,a finite element（FE） model of composite strengthening process which contains cold expansion and interference fit has been established. The influence of technological parame
Externí odkaz:
https://doaj.org/article/6cfbdac80a6a4bafb19ede4c15d8f066
Publikováno v:
Jixie qiangdu, Vol 39, Pp 1432-1437 (2017)
To solve the optimization problem of edge distance in titanium alloy sheet during a new aircraft development stage,a three dimensional FE model was built on ABAQUS platfom. The effect of edge distance on residual stress distribution was analysised wi
Externí odkaz:
https://doaj.org/article/bc4badb476d84dec93370897877d410c
Publikováno v:
Jixie qiangdu, Vol 38, Pp 1093-1098 (2016)
Strengthening problem of short-edge hole of titanium lug is an important task during a new aircraft development stage,Force Mate steel bushing process has been carried out to study the fatigue life of short-edge hole. Research the interference of 0.
Externí odkaz:
https://doaj.org/article/767bafcedf5441e299abce16f0ead2d7
Publikováno v:
In Engineering Fracture Mechanics 25 November 2024 311
Publikováno v:
In International Journal of Fatigue September 2024 186
Publikováno v:
In Engineering Failure Analysis December 2024 166
Publikováno v:
In Finite Elements in Analysis & Design March 2024 230
Publikováno v:
In Composite Structures 1 February 2024 329
Autor:
Wang, Xiaohe, Cao, Zengqiang
Publikováno v:
In Engineering Failure Analysis February 2024 156
Publikováno v:
In Chinese Journal of Aeronautics February 2024 37(2):482-500