scholarly journals Fatigue crack growth of TiAl6V4 parts produced by SLM under biaxial mode I/mode II loading

2021 ◽  
Vol 34 ◽  
pp. 129-134
Author(s):  
L.P. Borrego ◽  
J.S. Jesus ◽  
J.A.M. Ferreira ◽  
J.D. Costa ◽  
C. Capela
2013 ◽  
Vol 750 ◽  
pp. 264-267 ◽  
Author(s):  
Masahiko Makizaki ◽  
Hisao Matsunaga ◽  
Keiji Yanase ◽  
Masahiro Endo

Effect of occasional mode II loading on subsequent mode I fatigue crack growth behavior was investigated by using a thin-walled tube made of 7075-T6511 aluminum alloy. Careful observation of crack growth behavior revealed that the occasional mode II loading has two contradictory effects for crack growth behavior. The first is a retardation effect that is associated with the plastic deformation near crack tip. However, this effect is negligibly small for the crack growth life as a whole. The second is an acceleration effect caused by mode II fatigue crack growth itself. It was found that under relatively high ΔK level, the mode II crack growth was about an order magnitude faster than mode I crack growth. Therefore, to properly evaluate the effect of occasional shear loading in the 7075 alloy, the mode II crack growth should be taken into account.


2014 ◽  
Vol 123 ◽  
pp. 126-136 ◽  
Author(s):  
H. Matsunaga ◽  
M. Makizaki ◽  
D.F. Socie ◽  
K. Yanase ◽  
M. Endo

2000 ◽  
Author(s):  
H. Nayeb-Hashemi ◽  
Pinghu Yang

Abstract Solder joints are extensively used in electronic packaging. They provide critical electrical and mechanical connections. Single edge notched sandwich specimens, which were made of two blocks of brass joined with a 63Sn-37Pb solder layer, were prepared for fatigue and fracture study of the joint under mixed mode loading. Mode I and mixed mode I/II fracture toughness, fatigue crack thresholds, and fatigue crack growth rates (FCGR) were measured at room temperature using a four point bending test setup. It was found that the fracture toughness of the joint increased and FCGR decreased upon the introduction of mode II component. The interface fracture toughness was higher than that of reported for pure solder. The data of FCGR correlated well with the power law relation of da / dN = C* (ΔG)m. It was also observed that both fracture toughness and FCGR were a function of thickness of solder layer. When the solder layer thickness increased from 0.1mm to 1.0mm, the fracture toughness decreased substantially and FCGR increased slightly. For mode I loading, fatigue crack propagated inside the solder layer. However, for mixed mode loading, once a crack initiated, it changed its direction toward the interface and then propagated along the interface. These observations were related to local mode I and mode II stress fields. Fracture surface showed sign of rubbing under mixed mode loading with elongated cavities at the crack tip. However, under mode I loading, fracture surface was covered with equi-ax voids.


Sign in / Sign up

Export Citation Format

Share Document