scholarly journals Cyclic bending deformation and residual stress change due to bending fatigue in laminated inhomogeneous metals.

1985 ◽  
Vol 34 (380) ◽  
pp. 542-548
Author(s):  
Tashiyuki TORII ◽  
Kazuo HONDA ◽  
Hiromi NAKANO
2022 ◽  
Vol 50 (3) ◽  
pp. 20210457
Author(s):  
Wanhua Liang ◽  
James Pineault ◽  
F. Albrecht Conle ◽  
Timothy H. Topper

2009 ◽  
Vol 31 (8-9) ◽  
pp. 1225-1236 ◽  
Author(s):  
M. Benedetti ◽  
V. Fontanari ◽  
P. Scardi ◽  
C.L.A. Ricardo ◽  
M. Bandini

2017 ◽  
Vol 2017.55 (0) ◽  
pp. K0303
Author(s):  
Nuwan KARUNATHILAKA ◽  
Naoya TADA ◽  
Takeshi UEMORI ◽  
Toshiya NAKATA ◽  
Masahiro KAWANO

Author(s):  
Kouitsu MIYACHIKA ◽  
Wei-Dong XUE ◽  
Kengo NOJIMA ◽  
Tomoya YOSHIKAWA ◽  
Hidefumi MADA ◽  
...  

2012 ◽  
Vol 433-440 ◽  
pp. 6558-6564
Author(s):  
You Li Ma

For a slant pre-crack under mixed-mode conditions, a method is proposed in which mode Ⅰ and mode Ⅱ stress intensity factors ‹KI›mes and ‹KII›mes can be directly evaluated from the discontinuous displacement along it. The effect on fatigue pre-crack deformation behavior was discussed by comparing fatigue and annealed cracks. In general, using the biggest tangential stress criterion the direction propagating from the pre-cracks can be predicted by ‹KI›mes and ‹KII›mes calculated above. So testing for bending fatigue crack propagation under mixed-mode conditions was carried out using fatigue and annealed slant pre-cracks with slant angle β=450 defined as the angle between loading and pre-crack direction in a rectangular plate. As a result, for annealed pre-crack, the estimated fracture angle θestcorresponded to the measured oneθmes ; On the other hand, for fatigue pre-crack,θmes is bigger than θest because of the compressive residual stress around the pre-crack .


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