Issue 31

J.A.F.O. Correia et alii, Frattura ed Integrità Strutturale, 31 (2015) 80-96; DOI: 10.3221/IGF-ESIS.31.07 96 [26] Kajawski, D., A new (ΔK+Kmax)0.5 driving force parameter for crack growth in aluminum alloys, International Journal of Fatigue, 23(8) (2001) 733-740. [27] Castillo, E., Galambos, J., Lifetime Regression Models Based on a Functional Equation of Physical Nature”, Journal of Applied Probability, 24 (1987) 160-169. [28] Castillo, E., Fernández-Canteli, A., Hadi, A.S., López-Anelle, M., A Fatigue Model with Local Sensitivity Analysis, Fatigue and Fracture of Engineering Material and Structure, 30 (2006) 149–168. [29] ASTM E606: Standard Practice for Strain-Controlled Fatigue Testing, Annual Book of ASTM Standards, ASTM, West Conshohocken, PA, USA, 03.01 (1998) [30] ASTM E647: Standard Test Method for Measurement of Fatigue Crack Growth Rates, Annual Book of ASTM Standards, ASTM, West Conshohocken, PA, USA, 03.01 (2000). [31] SAS, ANSYS, Swanson Analysis Systems, Inc., Houston, Version 12.0, (2011). [32] Ramberg, W., Osgood, W.R., Description of the stress-strain curves by the three parameters, NACA TN-902, National Advisory Committee for Aeronautics, (1943).