Open Access

ARTICLE

Fatigue Crack Growth Reliability Analysis by Stochastic Boundary Element Method

Xiyong Huang¹, M. H. Aliabadi², Z. Sharif Khodaei³

1 Department of Aeronautics, Imperial College London, South Kensington, London SW7 2AZ, U.K.
2 Department of Aeronautics, Imperial College London, South Kensington, London SW7 2AZ, U.K.E-mail: m.h.aliabadi@imperial.ac.uk
3 Department of Aeronautics, Imperial College London, South Kensington, London SW7 2AZ, U.K.E-mail: z.sharif-khodaei@imperial.ac.uk