Research Article

MCMC-Based Fatigue Crack Growth Prediction on 2024-T6 Aluminum Alloy

Table 6

Parameter Estimate of fatigue crack propagation curve.

SpecimenError (%)
9000180002700036000450005400063000720008100090000

Number 13.91%2.15%0.22%−0.53%−1.04%−1.16%−2.60%−0.57%3.14%−0.04%
Number 2−3.95%−1.94%−0.79%−1.72%−3.16%−1.49%−1.84%−1.46%−0.65%−3.72%
Number 3−5.53%−4.95%−8.91%−8.15%−8.90%−7.99%−8.16%−6.25%−3.19%−10.18%
Number 4−2.20%1.13%4.04%7.22%5.76%8.39%7.08%4.78%4.68%−2.43%