Abstract The internal stress, σ i , and the effective-stress exponent of dislocation velocity, m*, have been studied during steady-state creep tests on aluminium and Al–Mg alloys containing 0·5–7 at.-% Mg at temperatures between 523 and 723K under an applied stress of 3·9–98 N/mm2. Stress-transient dip-tests showed that σ i had an appreciable value almost independent of composition and thus cannot be neglected in discussing creep processes in these materials. Values of m* determined from analyses of relaxation curves immediately after creep were close to unity in alloys containing 2 at.-% or more of magnesium. The same result was obtained from stress-increment tests on an Al–5·5 at.-% Mg alloy. It is concluded that high-temperature creep of Al–Mg alloys under the conditions of this work is controlled by solute-atmosphere dragging. An explanation has also been given for the fact that the applied-stress exponent of steady-state creep rate, n, is nearly 3 when m* = 1 and σ i is at a significant level.
[1]
H. Oikawa,et al.
Discontinuous flow in AlMg alloys at high temperatures
,
1973
.
[2]
S. Karashima,et al.
High-temperature creep rate and dislocation structure in a dilute copper-aluminium alloy
,
1973
.
[3]
H. Oikawa,et al.
Discontinuous Flow in Steady-State Creep of Al–Mg Alloys at High Temperatures
,
1973
.
[4]
H. Oikawa,et al.
Steady-State Creep Characteristics of Fe-3.5 at% Mo Alloy
,
1973
.
[5]
H. Oikawa,et al.
Activation Parameters of High-Temperature Creep in Nickel, and in Ni-9.5at% Cr and Ni-10.3at% W Alloys
,
1973
.
[6]
S. Karashima,et al.
Internal Stress and Dislocation Structure during Sigmoidal Transient Creep of a Copper–16 at.-% Aluminium Alloy
,
1972
.
[7]
M. Hansen,et al.
Constitution of Binary Alloys
,
1958
.