scholarly journals Evaluation of different techniques in estimating orientation of crack initiation planes and fatigue lifetime under complex multiaxial loading paths

2017 ◽  
Vol 100 ◽  
pp. 521-529 ◽  
Author(s):  
Yingyu Wang ◽  
N. Zuhair Faruq ◽  
Luca Susmel
2011 ◽  
Author(s):  
Christopher J. Szczepanski ◽  
S. L. Semiatin ◽  
James M. Larsen

2021 ◽  
pp. 114024
Author(s):  
Jiayun Chen ◽  
Lei Wan ◽  
Yaser Ismail ◽  
Pengfei Hou ◽  
Jianqiao Ye ◽  
...  

1996 ◽  
Vol 118 (2) ◽  
pp. 41-44 ◽  
Author(s):  
Z. Zhang ◽  
Daping Yao ◽  
J. K. Shang

A backface strain technique is introduced to examine fatigue crack initiation in solder lap joints. The technique detects the fatigue crack initiation by monitoring the backface strain at the end of the overlap. Variation of the backface strain with the development of a crack was simulated by finite element method. The simulation indicated that the backface strain at the end of the overlap reached a peak value when a fatigue crack initiated. Experimental verification was carried out in 63Sn-37Pb solder joints. The backface strain was recorded as a function of stress cycle to demonstrate the applicability of this technique. Experimental results showed that fatigue crack initiation took about half of the fatigue lifetime of the solder joints.


2012 ◽  
Vol 533 ◽  
pp. 43-49 ◽  
Author(s):  
Benoît Ter-Ovanessian ◽  
Dominique Poquillon ◽  
Jean-Marc Cloué ◽  
Eric Andrieu

1997 ◽  
Vol 119 (1) ◽  
pp. 104-112 ◽  
Author(s):  
Ming-Chuen Yip ◽  
Yi-Ming Jen

This paper discusses the mean strain effect on the crack initiation lives for notched specimens under biaxial nonproportional loading paths. Elastic-plastic finite element method was used to evaluate the local stresses and strains. Several prediction models related to the mean stress/strain effect were employed to correlate the experimental results with reference fatigue data for smooth specimens. It is found that Fatemi-Socie model gives good prediction for the present research with the assistance of finite element method. The stress behavior in this deflection-controlled tests is discussed in this study, and the failure surfaces are also examined after tests.


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