Research Article

Multi-State Reliability Analysis Based on General Wiener Degradation Process and Random Shock

Table 1

Fatigue crack growth data from test samples.

Test sampleCycle/104
0123456789101112

10.900.920.971.011.051.091.151.211.281.361.441.551.72
20.900.920.961.001.041.081.131.191.261.341.421.521.67
30.900.930.961.001.041.081.131.181.241.311.391.491.65
40.900.930.971.001.031.071.101.161.221.291.371.481.64
50.900.920.970.991.031.061.101.141.201.261.311.401.52
60.900.930.961.001.031.071.121.161.211.271.331.401.49
70.900.920.960.991.031.061.101.161.211.271.331.401.49
80.900.920.950.971.001.031.071.111.161.221.261.331.40
90.900.930.960.971.001.051.081.111.161.201.241.321.38
100.900.920.940.971.011.041.071.091.141.191.231.281.35
110.900.920.940.970.991.021.051.081.121.161.201.251.31
120.900.920.940.970.991.021.051.081.121.161.191.241.29