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

Table 5

Estimation value of model parameters.

Specimen	Parameter estimate value
	θ1	θ2
Number 1	2.4312	−0.2598
Number 2	3.7303	−0.5435
Number 3	3.2953	−0.4592
Number 4	3.0991	−0.7331