2019
DOI: 10.1016/j.ijfatigue.2019.01.021
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Cyclic deformation response of ultra-fine grained titanium at elevated temperatures

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Cited by 16 publications
(6 citation statements)
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“…The area of a hysteresis loop is an indicator for the energy dissipation per cycle. Thus, this characteristic can be linked to the dislocation activity and cyclic plastic deformation [32,33]. By comparing stress amplitudes of both conditions based on the half-life hysteresis loops, it can be deduced that the cast-cast joints generally experienced slightly lower stress amplitudes than AM-cast specimens, which again is an indication of lower deformation resistance being rationalized by the inferior base material strength.…”
Section: Low-cycle Fatigue (Lcf) Behavior and Fracture Analysismentioning
confidence: 92%
“…The area of a hysteresis loop is an indicator for the energy dissipation per cycle. Thus, this characteristic can be linked to the dislocation activity and cyclic plastic deformation [32,33]. By comparing stress amplitudes of both conditions based on the half-life hysteresis loops, it can be deduced that the cast-cast joints generally experienced slightly lower stress amplitudes than AM-cast specimens, which again is an indication of lower deformation resistance being rationalized by the inferior base material strength.…”
Section: Low-cycle Fatigue (Lcf) Behavior and Fracture Analysismentioning
confidence: 92%
“…Concomitantly, fatigue lives of both alloys reduced with the increase of the total strain amplitude. At higher total strain amplitudes, specimens suffer more rapid fatigue crack initiation and propagation [48][49]. It should also be noted that at higher Δε t /2, stress levels of AA7075 alloy are always higher than those of AA6082 alloy.…”
Section: Mechanical Properties Under Cyclic Loadingmentioning
confidence: 97%
“…As-received (T6) specimens also show a saturation stage similar to the conditions formed in the cold tool. A lack of softening/hardening is an indication of predominant elastic deformation (at the global scale) and/or simultaneous generation and cancellation of dislocations [48,55]. Furthermore it can be directly deduced that neither cutting of precipitates and strain localization nor evolution of dislocation cell structures take place [52,56].…”
Section: Mechanical Properties Under Cyclic Loadingmentioning
confidence: 99%
“…Due to an increasing total strain amplitude, fatigue crack nucleation and propagation can be promoted. [36,45,46] At total strain amplitudes of Δε t /2 = AE0.4% and Δε t /2 = AE0.6%, cyclic stability with no traces of cyclic hardening and softening is evident. However, an interesting cyclic hardening can be observed for the specimens being conventionally and stress-aged for a short time (2 h) during fatigue at a total strain amplitude of Δε t /2 = AE0.8%.…”
Section: Mechanical Properties Under Cyclic Loadingmentioning
confidence: 99%