疲劳微缺陷的累积-熵解释

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2018-12-01 DOI:10.2478/fas-2018-0010
K. Szafran, N. Delas
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引用次数: 2

摘要

摘要本文介绍了几种描述微裂纹发展过程的模型。在本研究中,对选定的微裂纹模型的过程进行了分析。在该模型中,假定对材料的损伤具有某些“热力学性质”,或者更确切地说,具有大多数复杂系统固有的普遍性质。为了计算结构的长期疲劳强度特性,了解不同尺寸缺陷数量的分布参数是很重要的。利用熵原理建立了一个模型,该模型可以有效地用于测试难以形式化的复杂系统。大量的试验研究发现,疲劳损伤的发展与材料在局部缺陷接触点的塑性变形过程密切相关。计算机计算和模拟的结果得出了本文最后一部分的结论。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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Accumulation of Fatigue Microdefects– Entropy Interpretation
Abstract The authors of the paper presented some of the models describing the process of micro-cracks’ development. In this study, the process of a selected model of micro-cracking was analyzed. In the model it was assumed that the damage to the material has some “thermodynamic properties” or rather universal properties inherent in most complex systems. In order to calculate the long-term fatigue strength properties of a structure, it is important to have a good understanding of the distribution parameters of the number of defects of different sizes. A model was built using the entropy principle, which is effectively used to test complex systems that are difficult to formalize. As a result of many experimental studies it was found that the development of fatigue damage is closely related to the process of plastic deformation of the material at the contact point of local defects. The results of computer calculations and simulations led to the conclusions presented in the final part of this paper.
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
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0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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