Fatigue Damage Evolution in a Short Fiber Reinforced Metal Matrix Composite

S. Canumalla, Robert N. Pangborn
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Abstract

The micromechanisms of fatigue failure of a short, alumina-silicate fiber reinforced cast aluminum alloy (A356) are investigated in this study. The nature of damage evolution is studied by three complementary perspectives — i) monitoring of the mechanical response, ii) microscopy on the gage length and fracture surface, and iii) probing of the microstructural changes in the bulk nondestructively using acoustic emission. The damage evolution in the composite is driven by strain or fatigue cycles imposed on the specimen and is manifested as three distinct mechanisms: a) cracking at hollow shot particles early in the life, b) microcracking in the form of fracture of fibers oriented in the direction of the loading and splitting or decohesion at fiber/matrix interface of transversely oriented fibers, and c) void formation at fiber ends and other stress concentrations. The interaction among the different modes, which defines the evolution of microstructural damage, is described. A flow chart for the progression of damage is presented and the most important steps in the damage evolution are identified. Suggestions are made for improving fatigue performance by tailoring the microstructure of the composite.
短纤维增强金属基复合材料疲劳损伤演化研究
研究了一种短型硅酸铝纤维增强铸造铝合金(A356)疲劳失效的微观机制。损伤演化的本质是通过三个互补的角度来研究的:1)机械响应的监测,2)测量长度和断口表面的显微观察,3)利用声发射无损探测体中的微观结构变化。复合材料的损伤演化是由施加在试样上的应变或疲劳循环驱动的,表现为三种不同的机制:a)在寿命早期的空心弹丸颗粒处开裂;b)在加载方向取向的纤维断裂和横向取向纤维/基体界面处的分裂或脱黏;c)纤维端部形成空洞和其他应力集中。描述了不同模态之间的相互作用,定义了微观结构损伤的演化过程。给出了损伤发展的流程图,并确定了损伤发展过程中最重要的步骤。提出了通过调整复合材料的微观组织来改善其疲劳性能的建议。
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