Nonlinear Fatigue Damage Accumulation

Q4 Engineering
Daniel Krzysztof Dębski
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引用次数: 0

Abstract

Abstract One important element of any computational fatigue analysis is the adoption of a hypothesis of fatigue damage accumulation. The most commonly used is the hypothesis of linear accumulation of fatigue damage called the Palmgren-Miner hypothesis. This linear hypothesis does not take into account a factor of great importance: the mutual influence of consecutive fatigue load sequences on each other. In the presented paper, only two consecutive load sequences linked by mutual relations have been analyzed and the results of the analysis have been shown. A more complex form which takes into account the full load history would create complex formula difficult to use. Perhaps, we should go in this direction, especially that today we have enormous computing power at our disposal.
非线性疲劳损伤累积
任何计算疲劳分析的一个重要因素是采用疲劳损伤累积假设。最常用的是疲劳损伤线性累积假说,称为Palmgren-Miner假说。这种线性假设没有考虑到一个非常重要的因素:连续疲劳载荷序列之间的相互影响。本文只分析了两个相互联系的连续负荷序列,并给出了分析结果。考虑到全负荷历史的更复杂的形式将创建难以使用的复杂公式。也许,我们应该朝着这个方向前进,尤其是今天我们拥有巨大的计算能力。
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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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%
发文量
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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