Influence of Errors of Determination of Stresses Near a Crack Tip on the Accuracy of Computation of the Coefficients of the Williams Series Under Mode II Loading

2013 ◽  
Vol 48 (4) ◽  
pp. 438-443 ◽  
Author(s):  
I. S. Holyns’kyi
Keyword(s):  
Mode Ii ◽  
2002 ◽  
Vol 2002.2 (0) ◽  
pp. 59-60
Author(s):  
Mototsugu TANAKA ◽  
Akinori KONO ◽  
Masaki HOJO ◽  
Shojiro OCHIAI

2017 ◽  
Vol 7 ◽  
pp. 254-261
Author(s):  
Stanislav Žák ◽  
Jana Horníková ◽  
Pavel Šandera ◽  
Tomáš Vojtek ◽  
Jaroslav Pokluda

2014 ◽  
Vol 51 ◽  
pp. 54-61 ◽  
Author(s):  
F.G.A. Silva ◽  
J.J.L. Morais ◽  
N. Dourado ◽  
J. Xavier ◽  
F.A.M. Pereira ◽  
...  

Author(s):  
H. L. Li ◽  
X. Wang ◽  
R. Bell

For cracks under mode-I loading, it has been demonstrated that a general weight function expression with three unknown parameters can be used to approximate a variety of crack configurations under mode-I loading. For a given crack geometry, the unknown parameters can be determined from reference stress intensity factors (SIFs) together with characteristic properties of the weight functions. It is demonstrated in this paper that a general weight function expression also exists for cracks under mode II loading. The determination of weight functions for cracks in mode II can then also be conducted using reference stress intensity factors (SIFs) together with characteristic properties of the weight functions. This method is used to obtain the mode II weight functions for test specimens including single edge cracked plate, internal center cracked plate and double edge cracked plate. These derived weight functions were further used to calculate the SIFs for the above cracks subjected to several linear and non-linear shear loads and were compared to available SIF solutions.


2019 ◽  
Vol 9 (10) ◽  
pp. 2006 ◽  
Author(s):  
Makoto Akama

Fatigue tests were performed to estimate the coplanar and branch crack growth rates on rail and wheel steel under non-proportional mixed mode I/II loading cycles simulating the load on rolling contact fatigue cracks; sequential and overlapping mode I and II loadings were applied to single cracks in the specimens. Long coplanar cracks were produced under certain loading conditions. The fracture surfaces observed by scanning electron microscopy and the finite element analysis results suggested that the growth was driven mainly by in-plane shear mode (i.e., mode II) loading. Crack branching likely occurred when the degree of overlap between these mode cycles increased, indicating that such degree enhancement leads to a relative increase of the maximum tangential stress range, based on an elasto–plastic stress field along the branch direction, compared to the maximum shear stress. Moreover, the crack growth rate decreased when the material strength increased because this made the crack tip displacements smaller. The branch crack growth rates could not be represented by a single crack growth law since the plastic zone size ahead of the crack tip increased with the shear part of the loading due to the T-stress, resulting in higher growth rates.


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