Results 1 to 10 of about 6,843 (265)
In the fatigue design of metallic components using the safe-life approach, fatigue crack initiation as a development of slip systems at the nanoscale, followed by microstructurally short crack growth, is critical for the onset of structural failure.
Peter I. Christodoulou +1 more
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Effect of low temperature on fatigue and crack propagation behavior of aeronautic aluminium alloy
Fatigue and crack growth tests were performed on two categories of the common aeronautic aluminum- alloys 2524-T3 and 7050-T7451 at ambient temperature of 25 ℃ and cryogenic temperature of –70 ℃, in order to investigate the fatigue and crack propagation ...
LIU Mudong
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Crack path in aeronautical titanium alloy under ultrasonic torsion loading [PDF]
This paper discusses features of fatigue crack initiation and growth in aeronautical VT3-1 titanium alloy under pure torsion loading in gigacycle regime. Two materials: extruded and forged VT3-1 titanium alloys were studied.
A. Nikitin +3 more
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Crack initiation characteristics and fatigue property of a high-strength steel in VHCF regime under different stress ratios [PDF]
Crack initiation characteristics and fatigue property of a high-strength steel in very-high-cycle fatigue (VHCF) regime under different stress ratios were investigated in this paper.
Xiaolong Liu, Chengqi Sun, Youshi Hong
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Stress-state dependent cohesive model for fatigue crack growth [PDF]
In the cohesive framework, a stress-state dependent cohesive model, combined with an irreversible damage parameter has been used in simulation of fatigue crack growth initiation and continued growth.
R. Shravan Kumar +4 more
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Working service of structural materials at elevated temperatures generally leads to a significant decrease in their fatigue performance, thereby threatening the safety and reliability of engineering structures.
Xue Li +8 more
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Forecast of the fatigue crack initiation site of commercially pure Titanium miniature specimens with local surface topography data [PDF]
Surfaces of technical components rarely appear in perfectly smooth condition. During fatigue loading, stress concentrations at surface asperities cause localized plastic deformation that can lead to crack initiation.
Böhme L. +4 more
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To meet the design requirements, different types of defects are often machined on the surface of fatigue components. Local stress concentration formed at the notch accelerates the initiation of fatigue crack, therefore greatly shortens the service lives ...
Zhi-qiang Wang +2 more
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Early slip activity and fatigue crack initiation of a near alpha titanium alloy [PDF]
For titanium alloys, crack initiation as a result of plastic strain accumulation has been shown to govern fatigue life under the high cycle fatigue regime.
Liu Conghui +3 more
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The fatigue crack initiation of the fuselage structure skin under the uniform supercharged cyclic load of 0 ~ 7. 8 Psi was experimentally studied by the self-made aircraft fuselage skin uniform supercharged fatigue simulation device.
LIU LiPing +5 more
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