Effect of reversion treatment on the fatigue strength of age hardened Al-12mass% Zn alloy was studied by measurements of Vickers micro-hardness and number of cycles to failure under repeated tensile loading. The results obtained are summarized as follows. 1) Rate of reversion was faster in the surface layer than in the interior when the age hardened specimen annealed at 353K. That is, soft surface layer was formed, again. 2) In this case, the presence of soft surface layer strengthens fatigue resistance of the age hardened Al-12mass%Zn alloy
The higher strength 7xxx aluminum alloys exhibited low resistance to stress corrosion cracking (SCC...
Aluminum alloys are widely used in aircraft structural components where light weight, high strength ...
International audienceFine-scale precipitation of the η′ phase and its precursors are essential for ...
P(論文)Effect of reversion treatment on the fatigue strength of age hardened Al-12mass% Zn alloy was s...
P(論文)The age hardening process, formation of soft surface layer and fatigue strength of Al-12mass%Zn...
P(論文)The fatigue strength under repetitive tensile stress and the age-hardening process were examine...
Effect of the soft surface layer that was formed on low temperature aging of Al-Zn alloy on fatigue ...
In this paper, the fatigue strength to repetitive tensile loading in an Al-11 mass%Zn alloy aged at ...
AbstractFatigue strength of Al-Cu alloy was examined by a repeated tensile mode when the specimens w...
Repeated tensile fatigue strength of the low temperature age-hardened Al-Zn alloys is investigated v...
P(論文)The surface layer of an Al-3mass%Mg alloy annealed at high temperature and its effect on the fa...
Fatigue strength of Al-Cu alloy was examined by a repeated tensile mode when the specimens were aged...
Reversion of the age-hardened Al-15mass % Zn alloy, in which ellipsoidal GP zones were formed, was i...
Effect of addition of a small amount of copper to Al- 12mass % Zn binary alloy on the process of low...
Aircraft grade 7010 aluminum alloy was heat treated to two different conditions: (1) standard peak a...
The higher strength 7xxx aluminum alloys exhibited low resistance to stress corrosion cracking (SCC...
Aluminum alloys are widely used in aircraft structural components where light weight, high strength ...
International audienceFine-scale precipitation of the η′ phase and its precursors are essential for ...
P(論文)Effect of reversion treatment on the fatigue strength of age hardened Al-12mass% Zn alloy was s...
P(論文)The age hardening process, formation of soft surface layer and fatigue strength of Al-12mass%Zn...
P(論文)The fatigue strength under repetitive tensile stress and the age-hardening process were examine...
Effect of the soft surface layer that was formed on low temperature aging of Al-Zn alloy on fatigue ...
In this paper, the fatigue strength to repetitive tensile loading in an Al-11 mass%Zn alloy aged at ...
AbstractFatigue strength of Al-Cu alloy was examined by a repeated tensile mode when the specimens w...
Repeated tensile fatigue strength of the low temperature age-hardened Al-Zn alloys is investigated v...
P(論文)The surface layer of an Al-3mass%Mg alloy annealed at high temperature and its effect on the fa...
Fatigue strength of Al-Cu alloy was examined by a repeated tensile mode when the specimens were aged...
Reversion of the age-hardened Al-15mass % Zn alloy, in which ellipsoidal GP zones were formed, was i...
Effect of addition of a small amount of copper to Al- 12mass % Zn binary alloy on the process of low...
Aircraft grade 7010 aluminum alloy was heat treated to two different conditions: (1) standard peak a...
The higher strength 7xxx aluminum alloys exhibited low resistance to stress corrosion cracking (SCC...
Aluminum alloys are widely used in aircraft structural components where light weight, high strength ...
International audienceFine-scale precipitation of the η′ phase and its precursors are essential for ...