On the Use of NASGRO Software to Estimate Fatigue Crack Growth under Variable Amplitude Loading in Aluminium Alloy 2024-T351

Author:

Moreno B.,Martin A.,Lopez-Crespo P.,Zapatero J.,Dominguez J.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference16 articles.

1. Newman Jr JC. FASTRAN II—a fatigue crack growth structural analysis program. N ASA TM 104159, 1992.

2. NASGRO, Fracture mechanics and fatigue crack growth analysis software (version 6.0), reference manual, NASA Johnson Space Center and Southwest Research Institute; 2010.

3. On the use of the strip-yield model to predict fatigue crack growth under irregular loading;Zapatero;Fatigue Fract Engng Mater Struct,1997

4. Numerical and experimental analysis of the fatigue crack growth under random loading;Zapatero;International Journal of Fatigue.,2005

5. Application of the strip-yield model from the NASGRO software to predict fatigue crack growth in aluminium alloys under constant and variable amplitude loading;Skorupa;Engineering Fracture Mechanics.,2007

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