应用马尔可夫矩阵极值序列的裂纹扩展模型研究裂纹扩展速率的变异性

IF 0.4 Q4 ENGINEERING, MECHANICAL
I. V. Gadolina
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引用次数: 0

摘要

飞机结构在疲劳作用下的裂纹扩展阶段引起了人们极大的兴趣。考虑了疲劳裂纹扩展时间的变化问题。在不规则载荷下,耐久性会有很大的变化。在本研究中,采用马尔可夫地址矩阵方法对装载过程进行建模,得到了初始过程的多个副本。使用Willenborg裂纹扩展延迟模型计算每个副本的疲劳寿命。采用随机过程模型TWIST序列作为仿真基础,该模型在航空数值实验中广泛用于研究载荷信息不确定性导致的耐久性可能散射。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Study of Variability of the Crack Growth Rate by Applying a Crack Growth Model to Sequences of Extrema Modeled by Markov Matrices

Study of Variability of the Crack Growth Rate by Applying a Crack Growth Model to Sequences of Extrema Modeled by Markov Matrices

The stage of crack propagation in aircraft structures under fatigue is of great interest. The problem of variation in the duration of fatigue crack growth is considered. Under irregular loading, durability can vary significantly. For this study, loading processes are modeled using the Markov address matrix method and several replicas of the initial process are obtained. The fatigue life of each replica is calculated using the Willenborg crack growth retardation model. A model for random processes, the TWIST sequence, which is widely used in aviation to investigate the likely scatter of durability due to the uncertainty of load information in a numerical experiment, is used as the basis for the simulation.

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来源期刊
CiteScore
0.80
自引率
33.30%
发文量
61
期刊介绍: Journal of Machinery Manufacture and Reliability  is devoted to advances in machine design; CAD/CAM; experimental mechanics of machines, machine life expectancy, and reliability studies; machine dynamics and kinematics; vibration, acoustics, and stress/strain; wear resistance engineering; real-time machine operation diagnostics; robotic systems; new materials and manufacturing processes, and other topics.
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