The role of multistep aging on the stress corrosion cracking (SCC) behavior of aluminum alloy 7010 has been investigated. The material in the form of 5-mm-thick sheets was heat-treated to two different tempers. The heat treatments are peak-aged, obtained by a two-step aging (i.e., solution treated at 465°C, water quenched at room temperature, and aged at 100°C/8 h and 120°C/8 h) and over-aged, obtained by a three-step aging (i.e., solution treated at 465°C, water quenched at room temperature, and aged at 100°C/8 h followed by 120°C/8 h and 170°C/8 h). SCC behavior was investigated using slow strain rate testing (SSRT) in air and 3.5% sodium chloride (NaCl) solution (environment). U-bend testing was carried out as a qualitative test. SSRT results show a remarkable improvement in the SCC resistance in three-step aged samples. For example, the percent reduction in area dropped from 28.1% (in air) to just 24.4% (in environment), and there was no drop in the percent elongation (~10%) when tested at a strain rate of 10–6/s. Two-step aged samples were found to be inferior compared with the three-step aged sample—the percent reduction in area of two-step aged samples dropped from 9.9% (in air) to 3.3% (in environment) and percent of elongation dropped from 10% (in air) to 3% (in environment). U-bend test results are also in conformity with the SSRT results, showing high resistance to SCC in the three-step aged alloy, though no direct correlation can be made. Anodic dissolution along the grain boundaries leading to intergranular cracking was evident in the SSRT and U-bend fractured specimens of the two-step aged alloy, whereas, such an attack was less prominent in the three-step aged alloy leading to a relatively more ductile fracture. The breaking of grain boundary precipitate network in the three-step aged condition could be a possible reason for better SCC resistance of the three-step aged alloy.
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1 October 2003
Research Article|
October 01 2003
Influence of Multistep Aging on the Stress Corrosion Cracking Behavior of Aluminum Alloy 7010 Available to Purchase
M. Bobby-Kannan;
M. Bobby-Kannan
*Corrosion Science and Engineering, Indian Institute of Technology Bombay, Mumbai 400 076,
India
.
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V.S. Raja;
V.S. Raja
‡
*Corrosion Science and Engineering, Indian Institute of Technology Bombay, Mumbai 400 076,
India
.‡Corresponding author.
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R. Raman;
R. Raman
**Department of Metallurgical Engineering and Materials Science, Indian Institute of Technology Bombay, Mumbai 400 076,
India
.
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A.K. Mukhopadhyay
A.K. Mukhopadhyay
***Defence Metallurgical Research Laboratory, Hyderabad 500 058,
India
.
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‡Corresponding author.
Online ISSN: 1938-159X
Print ISSN: 0010-9312
NACE International
2003
CORROSION (2003) 59 (10): 881–889.
Citation
M. Bobby-Kannan, V.S. Raja, R. Raman, A.K. Mukhopadhyay; Influence of Multistep Aging on the Stress Corrosion Cracking Behavior of Aluminum Alloy 7010. CORROSION 1 October 2003; 59 (10): 881–889. https://doi.org/10.5006/1.3287709
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