An exponential equation of fatigue crack growth in titanium

被引:23
作者
Adib, A. M. L.
Baptista, C. A. R. P.
机构
[1] Univ Sao Paulo, EEL, Dept Mat Engn, BR-12602810 Lorena, SP, Brazil
[2] Empresa Brasileira Aeronaut SA, BR-12227901 Sao Jose Dos Campos, Brazil
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2007年 / 452卷
关键词
fatigue crack growth; cycle asymmetry; titanium;
D O I
10.1016/j.msea.2006.10.124
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Titanium and its alloys are known for not showing a high degree of linearity of the fatigue crack growth (FCG) data. In the present work, the FCG curves of commercially pure titanium are evaluated using the conventional Paris approach and a new exponential equation named alpha beta model, which allows for considering non-linear da/dN-Delta K relationships. The following load ratios (min/max) were adopted for the fatigue tests: R = 0.05, 0.1, 0.15, 0.30, 0.50 and 0.60. The alpha beta model is more effective than Paris-based equations in describing the FCG behavior of titanium and can be easily generalized to take in account a range of stress ratios. This new model also qualifies as a promising tool to assess the FCG curves of other structural materials. (c) 2006 Elsevier B. V. All rights reserved.
引用
收藏
页码:321 / 325
页数:5
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