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(1986), and add modelling equations for the recovery process. Bourdiliau
et al . (2010) go a step further and show that there is a direct relation between
recovery of hardness and recovery of ultimate tensile stress (UTS) for both
SRA Zircaloy-4 and Zr1Nb. However the recovery for Zr1Nb is more slug-
gish than for Zircaloy-4, as shown in Fig. 4.19. Zr1Nb does not fully recover
the irradiation-induced hardening, primarily due the effects of the thermally
stable, irradiation-induced phase which forms in that alloy.
Post-irradiation annealing also has effects on irradiation-affected
SPPs. The observed phenomena give important insights into, for instance,
(a)
320
After creep tests at 420°C
Annealing at 350°C
310
300
290
280
270
260
250
240
230
220
Recovery law at 350°C
Annealing at 400°C
Recovery law 400°C
Annealing at 420°C
Recovery law 420°C
Nonirradiated (no annealing)
0
1000
2000
3000
Time (h)
4000
5000
(b)
250
After creep tests at 400°C
Annealing at 350°C
230
Recovery law at 350°C
Annealing at 400°C
Recovery law at 400°C
￿ ￿ ￿ ￿ ￿ ￿
Annealing law at 450°C
210
Recovery law at 450°C
190
170
Nonirradiated (no annealing)
150
0
500
1000
1500
2000
2500
3000
3500
Time (h)
4.19 Comparison of the hardness recovery of (a) SRA Zircaloy-4 and
(b) RXA Zr1Nb. (Source: Reprinted, with permission, from Bourdiliau
et al. (2010), copyright ASTM International, 100 Barr Harbor Drive, West
Conshohocken, PA 19428.)
 
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