Estimations of fatigue life and variability under random loading in aluminum Al-2024T351 using strip yield models from NASGRO-Reference-Cited by-同舟云学术

Estimations of fatigue life and variability under random loading in aluminum Al-2024T351 using strip yield models from NASGRO

Published:2016-10 Issue: Volume:91 Page:414-422
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

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

Funder

Spanish Ministerio de Economía y Competitividad

Junta de Andalucía

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference17 articles.

1. The significance of fatigue crack closure;Elber;ASTM STP,1971

2. FASTRAN II—a fatigue crack growth structural analysis program;Newman;NASA TM,1992

3. NASGRO 6.0, Reference Manual (version 6.02, September 2010), Fracture mechanics and fatigue crack growth analysis software, NASA Johnson Space Center and Southwest Research Institute; 2010.

4. Effect of load histories on scatter of fatigue crack growth in aluminum alloy 2024-T351;Zapatero;Eng Fract Mech,1997

5. Yielding of steel sheets containing slits;Dugdale;J Mech Phys Solids,1960

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