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首页> 外文期刊>Journal of Minerals and Materials Characterization and Engineering >Fatigue Behaviour of Silicon Carbide and Fly Ash Dispersion Strengthened High Performance Hybrid Al 5083 Metal Matrix Composites
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Fatigue Behaviour of Silicon Carbide and Fly Ash Dispersion Strengthened High Performance Hybrid Al 5083 Metal Matrix Composites

机译:碳化硅疲劳行为和粉煤灰色散强化高性能杂交Al 5083金属基复合材料

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摘要

Fatigue is a major issue concerning the use of aluminium composites in structural applications. Fatigue leads to weakening of material majorly due to the strain bands formed in the material when it is subjected to repeated loading; the damage that occurs due to fatigue is a progressive and localized one. The fatigue may occur at a stress limit much lesser than the ultimate stress limit of the composite specimen. Henceforth in the current work, fatigue behaviour of silicon carbide and fly ash dispersion strengthened high performance hybrid Al 5083 metal matrix composites are evaluated. The main purpose of fatigue characterisation is to distinctly evaluate the life cycle of components that are fabricated from metal matrix composites and eventually develop a framework model for the significant study of fatigue strength of the structure with persistent striations all along the interstitials of aluminium- silicon carbide-fly ash interfaces. Fatigue is a stochastic process rather than a deterministic one that gives a considerable scatter, even among samples of similar composition with the tests carried out in some of the critically controlled environments. Hence there is a need for statistical validation of the results to authenticate the data collected. Thus in the current work, analysis of variance is carried out to establish the authenticity of the results and validate them. The results and plots are presented with suitable rationale and inferences.
机译:疲劳是在结构应用中使用铝复合材料的主要问题。由于在对其进行重复负载时,主要是由于材料中形成的应变带,疲劳主要导致材料的弱化。由于疲劳而发生的损害是渐进和局部化的损害。疲劳可能发生在压力下限比复合样品的最终应力极限大得多。从此以后,在当前的工作中,评估高性能杂交A1083金属基复合材料的碳化硅和飞灰分散的疲劳行为。疲劳表征的主要目的是清楚地评估由金属基质复合材料制造的部件的生命周期,最终开发框架模型,用于贯穿铝碳化硅间隙的持续条件持续存在的疲劳强度的疲劳强度-fly灰界面。疲劳是一种随机过程,而不是确定性的过程,即使在与在一些批判性环境中的测试中的测试中的类似组合物的样本中,也可以提供相当大的散射。因此,需要对结果进行统计验证以验证收集的数据。因此,在当前的工作中,执行方差分析以建立结果的真实性并验证它们。结果和地块具有合适的基本原理和推论。

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