[1]
|
Yang M C,Nie I-I. Analysis approach to durability based on ma-terial initial fatigue quality and S-N curve[J].Chinese Journal of Aeronautics,2007,(01):518-523.
|
[2]
|
李重河,朱明,王宁. 钛合金在飞机上的应用[J].稀有金属,2009,(01):84-91.
|
[3]
|
Liu J,Shao X J,Liu Y S. Effect of cold expansion on fatigue performance of open holes[J].Materials Science and Engineering A:Structural Materials Properties Microstructure and Processing,2008,(01):271-276.
|
[4]
|
Nigrelli V,Pasta S. Finite-element simulation of residual stress induced by split-sleeve cold-expansion process of holes[J].Journal of Materials Processing Technology,2008,(01):290-296.
|
[5]
|
de Matos P F P,Moreira P M G P,Camanho P P. Numer-ical simulation of cold working of rivet holes[J].Finite Ele-ments in Analysis and Design,2005,(01):989-1007.
|
[6]
|
Mahendra Babu N C. A simplified 3-D finite element simu-lation of cold expansion of a circular hole to capture through thickness variation of residual stresses[J].Engineering Failure Analysis,2008.339-348.
|
[7]
|
王洪达,苏宏华. TCA开缝衬套冷挤压残余应力分布有限元仿真[J].机械制造与自动化,2010,(03):98-100.
|
[8]
|
杨洪源,刘文瑛. 孔挤压强化疲劳增寿效益的试验研究[J].机械强度,2010,(03):446-450.
|
[9]
|
张有宏,李仲,常新龙. 飞行器钛合金紧固孔结构件耐久性研究[J].稀有金属材料与工程,2010,(08):1451-1453.
|
[10]
|
刘文埏. 概率断裂力学与概率损伤容限/耐久性[M].北京:北京航空航天大学出版社,1998.
|
[11]
|
王志智,王普选,聂学洲. 一种紧固孔细节原始疲劳质量评定方法[J].航空学报,1998,(04):471-475.
|