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THE HIGH CYCLE FATIGUE AND FRACTURE BEHAVIOR OF A SILICON CARBIDE PARTICULATE REINFORCED 2009 ALUMINUM ALLOY METAL MATRIX COMPOSITE

机译:碳化硅颗粒增强2009铝合金金属基质复合材料的高循环疲劳和断裂行为

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In this paper, the cyclic stress amplitude controlled fatigue response and fracture behavior of aluminum alloy 2009 discontinuously reinforced with silicon carbide (SiC) particulates is presented and discussed. Test specimens of the composite, in the T42 aging condition, were cyclically deformed under stress-amplitude-control at both ambient and elevated temperatures. The elevated temperature corresponded to the aging temperature of the alloy. The cyclic fatigue tests were conducted at two different stress ratios with the objective of documenting the conjoint influence of intrinsic composite microstructural effects, nature of loading, and magnitude of maximum stress on cyclic fatigue life and fracture characteristics The final fracture behavior of the composite is discussed in light of the concurrent and mutually interactive influences of composite microstructural effects, deformation characteristics of the composite constituents, nature of loading, the nature and role of microscopic cracks and resultant fatigue life.
机译:本文提出并讨论了用碳化硅(SiC)颗粒不连续增强铝合金2009的循环应力幅度控制疲劳反应和断裂行为。在T42老化条件下,复合材料的试样在周围环境和升高的温度下在应力幅控制下循环地变形。升高的温度对应于合金的老化温度。循环疲劳试验以两种不同的应力比进行,目的是记录内在复合微观结构效应,载荷性质的结合影响,并且循环疲劳寿命和裂缝特征的最大应力的大小讨论了复合材料的最终断裂行为鉴于复合微观结构效应的同时和相互交互的影响,复合成分的变形特征,负载性质,微观裂缝的性质和作用以及所得疲劳寿命。

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