AN APPROACH TO FATIGUE LIFE MODELING IN TITANIUM-MATRIX COMPOSITES

被引:23
作者
NICHOLAS, T
机构
[1] Wright Laboratory Materials Directorate, Wright-Patterson Air Force Base
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 1995年 / 200卷 / 1-2期
关键词
FATIGUE; MODELING; ELEVATED TEMPERATURES;
D O I
10.1016/0921-5093(95)07002-8
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
A review of the procedures developed by the author and his colleagues over the last several years for predicting elevated-temperature fatigue life of metal-matrix composites is presented. Modeling approaches involve concepts of both linear and non-linear summation of damage from cycle-dependent as well as time-dependent mechanisms. The analyses, further, treat the micromechanical stresses in the constituents as parameters in the life prediction models. The material characterized is SCS-6/Timetal(R)21S, a metastable beta titanium alloy reinforced with continuous SIC fibers. Modeling is applied to isothermal fatigue at different frequencies and temperatures, and thermomechanical fatigue (TMF) under both in-phase and out-of-phase loading conditions at different temperature ranges and maximum temperatures. Experimental data are used as the basis for determining the parameters embedded in the models. The numerical results, in turn, provide insight into the dominant mechanisms controlling fatigue life under a given condition. The capability to correlate experimental data from a wide variety of test conditions for several versions of a damage summation model is demonstrated.
引用
收藏
页码:29 / 37
页数:9
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