2015
DOI: 10.1016/j.engfracmech.2014.11.009
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Effect of water vapor pressure on fatigue crack growth in Al–Zn–Cu–Mg over wide-range stress intensity factor loading

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Cited by 30 publications
(14 citation statements)
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“…One of the characteristics of heat treatment of aluminum [21] is rapid formation of a thin layer of passive oxide of Al2O3 [22][23][24]. The hydrogen bubbles formed in the aluminum microstructure during heat treatment depend on many aspects, such as water vapor pressure [25], solubility [26,27], permeability, diffusivity [28] and activity [28,29]. Some of these aspects can be verified by mass spectrometric analyzer [11] or a thermal desorption spectroscopy system [30].…”
Section: Hydrogen In High Temperature Solid Aluminum Alloysmentioning
confidence: 99%
“…One of the characteristics of heat treatment of aluminum [21] is rapid formation of a thin layer of passive oxide of Al2O3 [22][23][24]. The hydrogen bubbles formed in the aluminum microstructure during heat treatment depend on many aspects, such as water vapor pressure [25], solubility [26,27], permeability, diffusivity [28] and activity [28,29]. Some of these aspects can be verified by mass spectrometric analyzer [11] or a thermal desorption spectroscopy system [30].…”
Section: Hydrogen In High Temperature Solid Aluminum Alloysmentioning
confidence: 99%
“…There is an extensive data based on fatigue crack growth rates (FCGRs; d a /d N ) versus stress intensity range relationships for alloys used in airframe structures; such data are typically generated in ambient laboratory conditions. However, aluminum alloys (and other structural alloys) 10–12 have drastically slower FCGR behavior at low temperature and low water vapor pressure environments 13–23 . Such environments are pertinent to high‐altitude operation, where a significant portion of loading can occur for airframe structural components 13,17 .…”
Section: Introductionmentioning
confidence: 99%
“…Such environments are pertinent to high‐altitude operation, where a significant portion of loading can occur for airframe structural components 13,17 . The phenomenological and mechanistic underpinnings of the low moisture environment effect on aerospace aluminum alloys fatigue cracking behavior have been extensively studied 13,14,18,21,24–39 . It is understood that in moist air, the environmental cracking contribution is governed by hydrogen environment embrittlement 20,27,40–42 .…”
Section: Introductionmentioning
confidence: 99%
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