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A fracture mechanics analysis on the fatigue behaviour of cruciform joints of duplex stainless steel
Author(s) -
INFANTE V.,
BRANCO C. M.,
MARTINS R.
Publication year - 2003
Publication title -
fatigue and fracture of engineering materials and structures
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.887
H-Index - 84
eISSN - 1460-2695
pISSN - 8756-758X
DOI - 10.1046/j.1460-2695.2003.00681.x
Subject(s) - cruciform , materials science , fracture mechanics , welding , structural engineering , cracking , paris' law , fracture (geology) , carbon steel , composite material , duplex (building) , mixed mode , metallurgy , crack closure , corrosion , engineering , dna , biology , genetics
ABSTRACT The paper presents the results of an experimental and numerical study on the fatigue behaviour of cruciform load carrying joints made from the duplex stainless steel and failing from the weld root through the weld metal. Fatigue crack growth (FCG) data, obtained in specimens of the weld metal, are presented, as well as threshold data, both obtained for R = 0 and 0.5. The influence of stress ratio is discussed, and the FCGR results are compared with data for low carbon structural steels. S–N data were obtained in the joints, both for R = 0.05 and 0.5, and the fatigue cracking mechanisms were analysed in detail with the SEM. It was found that the cracks propagated very early in the lifetime of the joints, under mixed mode conditions (I + II), but the mode I component was found to be predominant over mode II. The geometries of the cracks were defined in detail from measurements taken in the fracture surfaces. A 2D FE analysis was carried out for the mixed mode inclined cracks obtained at the weld root, and the J ‐integral formulations were obtained as a function of crack length and crack propagation angle. The values of the crack propagation angle, θ i , were obtained for the J max conditions, and it was found that, in the fatigue tests, the cracks propagated in directions very close to the predicted directions of maximum J . K I and K II formulations were obtained, and the K I data were compared with the formulations given in the PD6493 (BS7910) document, and some differences were found. A more general formulation for K under mixed mode conditions was derived. The derived K solutions were applied to predict the fatigue lives of the joints under crack propagation, and an extremely good agreement was found with the experimental results obtained in the fatigue tests.