The effect of retrogression and reaging on the properties of the 7249 aluminum alloy

[1]  Maria E. Iskandar,et al.  On identifying the most critical step in the sequence of heat treating operations in a 7249 aluminum alloy , 2003 .

[2]  H. Garmestani,et al.  The Effect of Varying the Solution Treatment Temperature, Natural Aging Treatment and Artificial Aging Treatment on the Mechanical Strength of 7249 Aluminum Alloy , 2002 .

[3]  O. Es-Said,et al.  Retrogression and Reaging of 7075 T6 Aluminum Alloy , 2000 .

[4]  R. L. Cudd,et al.  Retrogression and re-aging of 7010 open die forgings , 1999 .

[5]  M. Talianker,et al.  Retrogression and reaging and the role of dislocations in the stress corrosion of 7000-type aluminum alloys , 1989 .

[6]  Joong-Keun Park,et al.  Influence of retrogression and reaging treatments on the strength and stress corrosion resistance of aluminium alloy 7075-T6 , 1988 .

[7]  W. Wallace,et al.  Discussion of “Effect of retrogression and reaging treatments on the microstructure of Al-7075-T651” , 1985 .

[8]  J. Hatch,et al.  Aluminum: Properties and Physical Metallurgy , 1984 .

[9]  A. Ardell,et al.  Effect of retrogression and reaging treatments on the microstructure of Ai-7075-T651 , 1984 .

[10]  A. Ardell,et al.  Microstructures of the commercial 7075 Al alloy in the T651 and T7 tempers , 1983 .

[11]  M. O. Speidel,et al.  Stress corrosion cracking of aluminum alloys , 1975 .

[12]  David A. Tanner,et al.  Retrogression, reaging and residual stresses in 7010 forgings , 1999 .

[13]  C. J. Peel,et al.  Analysis of failures in aircraft structures , 1990 .

[14]  W. Wallace,et al.  Stresscorrosion-rack grovvth behaviour of 7475 T6 retrogressed and reaged aluminium alloy , 1984 .