scholarly journals Mode I and mixed-mode propagation of delamination fatigue cracks in CFRP laminates.

1987 ◽  
Vol 36 (402) ◽  
pp. 222-228 ◽  
Author(s):  
Masaki HOJO ◽  
Claes-Göran GUSTAFSON ◽  
Keisuke TANAKA ◽  
Ryuichi HAYASHI



1999 ◽  
Vol 65 (636) ◽  
pp. 1676-1683 ◽  
Author(s):  
Hiroshi TANAKA ◽  
Keisuke TANAKA ◽  
Tatsuya TSUJI ◽  
Hidetaka KATOH
Keyword(s):  


2005 ◽  
Vol 127 (1) ◽  
pp. 2-7 ◽  
Author(s):  
K. S. Chan ◽  
J. Feiger ◽  
Y.-D. Lee ◽  
R. John ◽  
S. J. Hudak,

The fatigue crack growth (FCG) behavior of PWA1484 single crystals was characterized in air under mixed-mode loading at 593°C as a function of crystallographic orientation using an asymmetric four-point bend test technique. Most mixed-mode fatigue cracks deflected from the symmetry plane and propagated as transprecipitate, noncrystallographic cracks, while self-similar fatigue crack growth occurred on the (111) planes in (111)/[011] and 111/[112]¯ oriented crystals. The local stress intensity factors and the crack paths of the deflected mixed-mode cracks were analyzed using the finite-element fracture mechanics code, FRANC2D/L. The results indicated that the deflected crack path was close to being normal to the maximum tensile stress direction where the Mode II component diminishes. Crystallographic analysis of the deflected crack paths revealed that the Mode I and the deflected mixed-mode cracks were usually of different crystallographic orientations and could exhibit different Mode I FCG thresholds when the crystallography of the crack paths differed substantially. These results were used to identify the driving force and conditions for cracking mode transition.



1999 ◽  
Vol 48 (12) ◽  
pp. 1408-1415
Author(s):  
Hiroshi TANAKA ◽  
Keisuke TANAKA ◽  
Hidetaka KATOH ◽  
Tatsuya TSUJI


2019 ◽  
Vol 9 (14) ◽  
pp. 2866 ◽  
Author(s):  
Makoto Akama ◽  
Akira Kiuchi

Rolling contact fatigue cracks in rail and wheel undergo non-proportional mixed mode I/II/III loading. Fatigue tests were performed to determine the coplanar and branch crack growth rates on these materials. Sequential and overlapping mode I and III loading cycles were applied to single cracks in round bar specimens. Experiments in which this is done have been rarely performed. The fracture surface observations and the finite element analysis results suggested that the growth of long (does not branch but grown stably and straight) coplanar cracks was driven mainly by mode III loading. The cracks tended to branch when increasing the material strength and/or the degree of overlap between the mode I and III loading cycles. The equivalent stress intensity factor range that can consider the crack face contact and successfully regressed the crack growth rate data is proposed for the branch crack. Based on the results obtained in this study, the mechanism of long coplanar shear-mode crack growth turned out to be the same regardless of whether the main driving force is in-plane shear or out-of-plane shear.



Author(s):  
P J Gregson ◽  
I Sinclair

The unusual susceptibility of the Al-Li alloy AA8090 to sustained macroscopic deviation of fatigue cracks from a nominal mode I path during conventional fatigue testing is discussed. It is demonstrated that the mixed mode crack growth associated with macroscopic deviation may be characterized in terms of elastic strain energy release rates for a range of mixed mode loading conditions. It is specifically shown that this form of mixed mode crack growth may lead to non-conservative crack growth predictions when these materials are subjected to conventional, mode I based structure lifing techniques.



2010 ◽  
Vol 3 (2) ◽  
pp. 131-139
Author(s):  
Arash Karpour ◽  
Khosrow Zarrabi
Keyword(s):  


2009 ◽  
Vol 76 (18) ◽  
pp. 2821-2833 ◽  
Author(s):  
P. Naghipour ◽  
J. Schneider ◽  
M. Bartsch ◽  
J. Hausmann ◽  
H. Voggenreiter


2021 ◽  
Vol 246 ◽  
pp. 107611
Author(s):  
Jianfeng Yang ◽  
Haojie Lian ◽  
Vinh Phu Nguyen




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