Uncertainty quantification in low cycle fatigue life model based on Bayesian theory

被引：0
|
作者：
Wang R. [1 ,2 ,3 ]
Liu F. [1 ]
Hu D. [1 ,2 ,3 ]
Li D. [1 ]
机构：
[1] School of Energy and Power Engineering, Beihang University, Beijing
[2] Collaborative Innovation Center of Advanced Aero-Engine, Beijing
[3] Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing
来源：
Hu, Dianyin (hdy@buaa.edu.cn) | 2017年 / Chinese Society of Astronautics卷 / 38期
基金：
中国国家自然科学基金;
关键词：
Bayesian theory; Global sensitivity; Low cycle fatigue; Probabilistic model; Uncertainty quantification;
D O I：
10.7527/S1000-6893.2017.220832
中图分类号：
学科分类号：
摘要：
To quantify the uncertainties in the model for low cycle fatigue life prediction, the classic model calibration method is applied using Bayesian theory, and the error term was verified by the normality test. Posterior distribution of the model parameter samples is obtained by Markov Chain-Monte Carlo (MCMC) simulation. An application is presented where a 95% interval of fatigue life prediction well describes the dispersity in real tests with small data samples. Correlation analysis of the samples of parameters is conducted to establish the heteroscedastic regression model. Comparison of the two models shows that the heteroscedastic regression model is questionable in uncertainty quantification performance. Morris global sensitivity analysis method is applied to quantify the sensitivity of the parameters in Manson-Coffin model, indicating that the non-informative prior is reasonable if posterior distribution is sensitive to the prior. © 2017, Press of Chinese Journal of Aeronautics. All right reserved.
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