AbstractAn Al-Zn-Mg-Cu alloy is aged at 120°C for varying time and the peak hardness (T6) is found at 24h. A multi-step ageing was adapted to produce interrupted aged (T6I6) temper. Stress corrosion cracking behaviour of T6 and T6I6 tempers has been studied by slow strain rate test at free corrosion potential (FCP) and at applied anodic potentials in 3.5wt.% NaCl solution. T6I6 temper exhibited higher SCC resistance than T6 temper at FCP, but both tempers are damaging at applied potentials. TEM microstructures, SEM fractographs and crack morphology are used to analyze SCC behaviour of the alloy tempers
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
The 7000 series, high-strength aluminum alloys are used in aircraft structures because of their high...
The role of multistep aging on the stress corrosion cracking (SCC) behavior of aluminum alloy 7010 h...
In this work, the effect of recrystallization inhibition in Al-Zn-Mg-Cu (7010) alloy towards the str...
This article reports an attempt to develop high-strength aluminum alloys of 7xxx series resistant to...
The high strength Al-Zn-Mg alloy used in the aerospace industry is strengthened by coherent G.P. zon...
potentials, environmental induced cracking (EIC). Stress corrosion cracking (SCC) behaviour of 8090 ...
To investigate the effect of split-aging on Weibull distribution of failure times in stress corrosio...
The effect of one step-and a new (short) two-step aging on the resistance to stress corrosion cra...
To investigate the influence of corrosion potential on stress corrosion cracking (SCC) of A1-6.13wt....
The age hardening, stress corrosion cracking (SCC) and hydrogen embrittlement (HE) of an Al-Zn-Mg-Cu...
The stress corrosion behaviour of precipitation hardened Al-9Mg, Al-22Zn and Al-3Mg-6Zn alloys has b...
The effects of different Zn/Mg ratios on the microstructure, mechanical properties and resistance of...
The effect of one-step and a new (short) two-step aging process on the resistance to stress corrosio...
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
The 7000 series, high-strength aluminum alloys are used in aircraft structures because of their high...
The role of multistep aging on the stress corrosion cracking (SCC) behavior of aluminum alloy 7010 h...
In this work, the effect of recrystallization inhibition in Al-Zn-Mg-Cu (7010) alloy towards the str...
This article reports an attempt to develop high-strength aluminum alloys of 7xxx series resistant to...
The high strength Al-Zn-Mg alloy used in the aerospace industry is strengthened by coherent G.P. zon...
potentials, environmental induced cracking (EIC). Stress corrosion cracking (SCC) behaviour of 8090 ...
To investigate the effect of split-aging on Weibull distribution of failure times in stress corrosio...
The effect of one step-and a new (short) two-step aging on the resistance to stress corrosion cra...
To investigate the influence of corrosion potential on stress corrosion cracking (SCC) of A1-6.13wt....
The age hardening, stress corrosion cracking (SCC) and hydrogen embrittlement (HE) of an Al-Zn-Mg-Cu...
The stress corrosion behaviour of precipitation hardened Al-9Mg, Al-22Zn and Al-3Mg-6Zn alloys has b...
The effects of different Zn/Mg ratios on the microstructure, mechanical properties and resistance of...
The effect of one-step and a new (short) two-step aging process on the resistance to stress corrosio...
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
Stress corrosion cracking (SCC) in Cu-free Al-Zn-Mg (7xxx) aluminium alloys limits its use in many a...
The 7000 series, high-strength aluminum alloys are used in aircraft structures because of their high...