A Study on the parameter estimation for crack growth prediction under variable amplitude loading

##plugins.themes.bootstrap3.article.main##

##plugins.themes.bootstrap3.article.sidebar##

Published Sep 25, 2011
Sang Hyuck Leem Dawn An Sangho Ko Joo-Ho Choi

Abstract

Bayesian formulation is presented to address the parameters estimation under uncertainty in the crack growth prediction subjected to variable amplitude loading. Huang's model is employed to describe the retardation and acceleration of the crack growth during the loadings. Model parameters are estimated in probabilistic way and updated conditional on the measured data by Bayesian inference. Markov Chain Monte Carlo (MCMC) method is employed for efficient sampling of the parameter distributions. As the model under variable amplitude loading is more complex, the conventional MCMC often fails to converge to the equilibrium distribution due to the increased number of parameters and correlations. An improved MCMC is introduced to overcome this failure, in which marginal PDF is employed as a proposal density function. A center- cracked panel under a mode I loading is considered for the feasibility study. Parameters are estimated based on the data from specimen tests. Prediction is carried out afterwards under variable amplitude loading for the same specimen, and validated by the ground truth data.

How to Cite

Hyuck Leem, S. ., An, D. ., Ko, S. ., & Choi, J.-H. . (2011). A Study on the parameter estimation for crack growth prediction under variable amplitude loading. Annual Conference of the PHM Society, 3(1). https://doi.org/10.36001/phmconf.2011.v3i1.2017
Abstract 173 | PDF Downloads 89

##plugins.themes.bootstrap3.article.details##

Keywords

Crack Growth, prognostics and health management (PHM), Markov Chain Monte Carlo (MCMC), Variable amplitude loading

References
Andrieu, C., Freitas, N. D,, Doucet, A. & Jordan, M. (2003). An introduction to MCMC for Machine Learning.Machine Learning, vol. 50(1), pp. 5-43.

Bayes, T. (1763). An Essay towards solving a Problem in the Doctrine of Chances, Philosophical Transactions of the Royal Society of London, vol. 53, pp. 370418.

Coppe, A., Haftka, R. T. & Kim, N. H. (2009). Reducing Uncertainty in Damage Growth Properties by Structural Health Monitoring. Annual Conference of the Prognostics and Health Management Society 2009 September 27 – October 1, San Diego CA

Coppe, A., Haftka, R. T., & Kim, N. H. (2010). Identification of Equivalent Damage Growth Parameters for General Crack Geometry. Annual Conference of the Prognostics and Health Management Society 2010, October 10-16, Portland, Oregon

Cross. R. J., Makeev, A. & Armainios, E. (2007). A comparison of prediction from probabilistic crack growth models inferred from Virkler’s data. Journal of ASTM International, Vol. 3(10)

An, D., Choi, C. H. & Kim. N. H. (2011). Statistical Characterization of Damage Growth Parameters and Remaining Useful Life Prediction Using Bayesian Inference, 13th AIAA Non-Deterministic Approaches Conference, April 4-7, Denver, CO.

Eiber, W. (1971). The significance of fatigue crack closure in fatigue. ASTM STP, Vol.486, pp. 230-242.

Huang, X., Torgeir, M. and Cui, W. (2007). An engineering model of fatigue crack growth under variable amplitude loading. A International Journal of Fatigue. Vol. 30. pp. 1-10.

Orchard, M., & Vachtsevanos, G. (2007). A Particle Filtering Approach for On-Line Failure Prognosis in a Planetary Carrier Plate. International Journal of Fuzzy Logic and Intelligent Systems, vol. 7(4), pp. 221-227.

Patrick, R. & Orchard, M. (2007). An integrated approach to helicopter planetary gear fault diagnosis and failure prognosis. Autotestcon 2007 IEEE , pp. 547-552.

Voorwald HJC, Torres MAS. (1991). Modeling of fatigue crack growth following overloads. International Journal of Fatigue 1991, Vol.13(5), pp.423-427.

Wheeler, OE. (1972). Spectrum loading and crack growth. Journal of Basic Engineering, Vol. 94. pp. 181-186

Willenborg, J., Engle, R.M. & Wood, H. A. (1971). A crack growth retardation model using effective stress concept. AFDL-TM-71-I-FBR Air Force Flight Dynamics Laboratory.
Section
Technical Research Papers

Most read articles by the same author(s)