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M. Kikuchi et alii, Frattura ed Integrità Strutturale, 34 (2015) 318-325; DOI: 10.3221/IGF-ESIS.34.34 324 half of the plate thickness. Fig. 14 shows change of crack depth and crack length along inner sursface with time (year). In the first several years, crack grows very rapidly, but growth rate decreases in low residual stress area. After 27 years, crack depth increases again very fast. If the crack depth exceeds 75% of plate thickness, this crack is treated to be fixed immediately. This crack reaches to this limit depth after 27 years, as shown in Fig.13. It is enoughly long time for the usual operation of nuclear power plant. By using this method, similar estimation of SCC process is possible. It enables to evaluate correctly the integrity of nuclear components. Figure 10 : Residual stress distribution in Hot Leg. Figure 11 : Cross section of hot leg and materials. Table 3 : Material constants of hot leg materials. (a) Initial crack (0 year ). (b) 1.95 years. (c) 15.4 years. (d) 22.8 years. (e) 30.2 years. Figure 12 : SCC growing process in the hot leg. Material E [GPa] ν α β Low Carbon Steel 176.0 0.3 0.0 1.00 Stainless Steel 174.5 0.3 0.0 1.00 Ni-based Alloy 198.3 0.3 6.73×10 -14 2.42