Fatigue-life prediction methodology using small-crack theory

被引:251
作者
Newman, JC [1 ]
Phillips, EP
Swain, MH
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23665 USA
[2] Lockheed Martin Engn & Sci, Hampton, VA 23665 USA
关键词
crack closure; fatigue; fracture; large cracks; plasticity; small cracks; spectrum loading;
D O I
10.1016/S0142-1123(98)00058-9
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper reviews the capabilities of a plasticity induced crack-closure model to predict fatigue lives of metallic materials using 'small-crack theory' for various materials and loading conditions. Crack-tip constraint factors, to account for three-dimensional State-of-stress effects, were selected to correlate large-crack growth rare data as a function of the effective-stress-intensity factor range (Delta K-eff) under constant-amplitude loading. Some modifications to the Delta K-eff rate relations were needed in the near-threshold regime to fit measured small-crack growth rate behavior and fatigue endurance limits. The model was then used to calculate small- and large-crack growth rates, and to predict total fatigue lives, for notched and un-notched specimens made of two aluminum alloys and a steel under constant-amplitude and spectrum loading. Fatigue lives were calculated using the crack-growth relations and microstructural features like those that initiated cracks for the aluminum alloys and steel for edge-notched specimens. An equivalent-initial-flaw-size concept was used to calculate fatigue lives in other cases. Results from the tests and analyses agreed well. (C) 1999 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:109 / 119
页数:11
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