1. Statistical analysis of the Virkler data on fatigue crack growth;Ditlevsen;Engineering Fracture Mechanics,1986
2. Yang JN, Manning SD, Rudd JL, Bader RM. Investigation of mechanistis-based equivelent initial flaw size approach, in: ICAF 95, International Commitee on Aeronautical Fatigue—18th symposium, Melbourne, Australia, 1995.
3. Probabilistic approach to calculation of kinetics of crack meshes;Cherniavsky;Dynamics, Strength & Wear-resistance of Machines,1997
4. Model-based Monte Carlo state estimation for condition-based component replacement;Cadini;Reliability Engineering & System Safety,2009
5. Tong YC. Review on aircraft structural risk and reliability analysis. Airframes and Engines Division, Aeronautical and Maritime Research Laboratory, 2001.