INTERPRETATION OF FATIGUE CRACK GROWTH IN ALUMINIUM ALLOYS UNDER PROGRAMMED BLOCK LOADING
Author:
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.1984.tb00197.x/fullpdf
Reference14 articles.
1. 1. A. Y. Koning (1981 ) A simple crack closure model for prediction of fatigue, crack growth rate under variable amplitude loading. ASTM STP 743, pp.63 -85 .
2. 2. J. Schijve (1976 ) Observations of the prediction of fatigue crack growth propagation under variable amplitude loading. ASTM STP 595, pp.3 -23 .
3. 3. J. Schijve (1972 ) The accumulation of fatigue damage in Aircraft materials and structure. AGARD Monograph No. 157.
4. Four lectures on fatigue crack growth
5. 5. W. Elber (1976 ) Equivalent constant amplitude concept for crack growth under spectrum loading. ASTM STP 595, pp.236 -250 .
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