PSI - Issue 18
Ivica Čamagić et al. / Procedia Structural Integrity 18 (2019) 385 – 390 Author name / Structural Integrity Procedia 00 (2018) 000–000
388
4
Table 5. Remaining exploitation period-crack in the PM
Initial crack length a 0 , mm
Critical crack length, a c , mm
Assumed crack length, a , m
Number of cycles, N
Geometry term, Y
Stress range, , MPa
Load case
5.58 6.01 6.45 6.91 5.58 6.01 6.45 6.91
0.01 0.02 0.03 0.01 0.02 0.03 0.041 0.041
160641
46618 20868 10767
I
211
5
41
14149448 4106189 1838105
II
46
5
41
948389
* Applies in the case of initial crack length of 5 mm. In the case of a crack in the PM: C = 1.52 10-10. m = 2.94
Table 6. Remaining exploitation period-crack in the PM
Critical crack length, a c , mm
Assumed crack length, a , m
Initial crack length a 0 , mm
Number of cycles, N
Geometry term, Y
Stress range, , MPa
Load case
I
5.58 6.01 6.21 6.41 5.58 6.01 6.21 6.41
0.01 0.02
20521
9622 7421 6329
211
5
29
0.025 0.029
II
0.01 0.02
318383 149276 115128
46
5
29
0.025 0.029
98199
* Applies in the case of initial crack length of 5 mm. In the case of a crack in the PM: C = 1.48 10-8. m = 1.80
Table 7. Remaining exploitation period-crack in the WM
Critical crack length, ac, mm
Initial crack length a0, mm
Assumed crack length, a, m
Number of cycles, N
Geometry term, Y
Stress range, , MPa
Load case
I
6.01 6.45 6.88 7.21 7.65 7.81 6.01 6.45 6.88 7.21 7.65 7.81
0.02 0.03 0.04 0.05 0.06 0.02 0.03 0.04 0.05 0.06
196096
98731 58520 39320 26957 23834
211
5
63.5
0.0635
II
8972132 4517323 2677509 1799030 1233369 1090506
46
5
63.5
0.0635
* Applies in the case of initial crack length of 5 mm. In the case of a crack in the WM: C = 1.26 10-9. m = 2.51
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