A multi-variable regression analysis is made of crack propagation data under flight simulation loading for the 2024-T3 and 7075-T6 alloys. The study is made using an equivalent effective stress range concept based on crack closure considerations. A two-variable regression model of the equivalent str
A mathematical model of fatigue crack propagation under variable amplitude loading
โ Scribed by R. Sunder
- Publisher
- Elsevier Science
- Year
- 1979
- Tongue
- English
- Weight
- 612 KB
- Volume
- 12
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
A mathematical model of fatigue crack propagation based on the crack closure concept is proposed. It allows prediction of fatigue crack growth under complex loading sequences on the basis of data obtained under constant amplitude and simple High-Low, Low-High loading sequences. The model explains the influence of single and multiple positive overloads and the interaction of positive and negative overloads. An algorithm for cycle-by-cycle calculation of crack growth is proposed.
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