Retrogression and reaging of 7075 T6 aluminum alloy

Materials Science Forum

Volumn 331, Issue , 2000, Pages

  Fleck, P ^a   Calleros, D ^a   Madsen, M ^a   Trinh, T ^a   Hoang, D ^a   Foyos, J ^a   Lee, E W ^b   Es Said, O S ^a  

^a LOYOLA MARYMOUNT UNIVERSITY   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AGING OF MATERIALS; ELECTRIC CONDUCTIVITY MEASUREMENT; HARDNESS; HEAT TREATMENT; METAL FORMING; TEMPERATURE; TENSILE TESTING;

MUFFLE FURNACES; RETROGRESSION;

ALUMINUM ALLOYS;

EID: 0033877246     PISSN: 02555476     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (6)

1. Hunt, Warren H., Staley, James T. "High Strength Aluminum Alloys for Aerospace Applications." The Minerals, Metals & Materials Society, 1989. pp. 111-120.
2. Rajan, K., Wallace, W., Beddoes, J.C. "Microstructure study of a high-strength stress-corrosion resistant 7075 aluminum," Journal of Materials Science, 1982. pp. 2817-2824.
3. Park, J. K., Ardell, A. J. "Effect of Retrogression and Reaging Treatments on the Microstructure of A1-7075-T651." Metallurgical Transaction A, Vol. 15A, August 1984. pp. 1531-1543.
4. Park, J. K. "Influence of Retrogression and Reaging Treatments on the Strength and Stress Corrosion Resistance of Aluminum Alloy 7075-T6," Materials Science and Engineering, 1988. pp. 223-231.
5. Islam, M.U. and Wallace, W. "Retrogression and reaging response of 7475 aluminum alloy,." Metals Technology, October 1983. Vol 10. pp.386-392.
6. Cina, B. M. and Ranish, B. "New technique for reducing susceptibility to stress corrosion cracking of high strength aluminum alloys." Aluminum Industry Products, American Society for Metal, 1974.