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fact this low stress regime is associated with similar characteristics as the
climb-controlled creep with distinct subgrain formation and relatively large
primary creep region. On the other hand, dislocations may break away from
the solute atmospheres at high stresses, thus entering a climb-controlled
regime again as noted at higher stresses with higher
n
value. Following
Murty's work, this breakaway stress can be calculated from the equation
74
2
Wc
m
mo
[3.44 ]
σ
=
b
β
3
,
2
kTb
T
where
W
m
is the binding energy between solute atom and the dislocation,
c
o
is the solute concentration, and
typically ranges between 2 and 4 depend-
ing on the shape of the solute atmosphere. Later, Langdon and co-workers
75
showed that this relation is valid for a number of solid solution alloys.
Assuming 0.23 eV as a reasonable value for
W
m
, the critical stress for break-
away is estimated to be ~7.5 × 10
−4
E, which is in agreement with the experi-
mental results obtained from various class-A alloys.
65
At even higher stresses,
another regime may appear involving low temperature climb-controlled
creep with a stress exponent value of
n
+ 2 (i.e. 7). This mechanism is asso-
ciated with the climb processes involving dominance of dislocation core dif-
fusion (Fig. 3.16b). However, this is often masked because the PLB regime
starts in the near vicinity.
As lower stresses are approached, one expects to note viscous creep with
n
= 1 (Fig. 3.16b) either due to N-H or Coble creep mechanisms. Depending
on the test temperature, one of the regions such as with
n
= 3 for viscous
glide may completely disappear as noted in Fig. 3.16b. This could get further
complicated if an intervening GBS regime with
n
= 2 appears between vis-
cous creep and dislocation creep regimes.
β
3.5.2 Deformation mechanism maps
The concept of deformation mechanism maps was proposed by Ashby.
76
Since different creep mechanisms operate or dominate in different stress,
temperature and grain size regimes, Ashby envisioned that a deformation
mechanism map would be an ideal representation of the materials consti-
tutive behavior. Over the years, this concept has been extended to describe
a variety of other physical phenomena such as sintering,
77
wear
78
and frac-
ture.
79
Figure 3.17 is a deformation mechanism map fi rst reported by Ashby
in 1972. The map was plotted as normalized stress (
/G
) against homologous
temperature (
T/T
m
) for a constant grain size. The map was then constructed
by determining the stress or temperature boundaries where one mechanism
would dominate others. To this end, the creep constitutive relations of dif-
ferent mechanisms were compared and stress and temperature values where
σ
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