Abstract

A computational damage model, which is driven by material, mechanical behavior, and nondestructive evaluation (NDE) data, is presented in this study. To collect material and mechanical behavior damage data, an aerospace grade precipitate-hardened aluminum alloy was mechanically loaded under monotonic conditions inside a scanning electron microscope, while acoustic and optical methods were used to track the damage accumulation process. In addition, to obtain experimental information about damage accumulation at the laboratory scale, a set of cyclic loading experiments was completed using three-point bending specimens made out of the same aluminum alloy and by employing the same nondestructive methods. The ensemble of recorded data for both cases was then used in a postprocessing scheme based on outlier analysis to form damage progression curves, which were subsequently used as custom damage laws in finite element (FE) simulations. Specifically, a plasticity model coupled with stiffness degradation triggered by the experimentally defined damage curves was used in custom subroutines. The results highlight the effect of the data-driven damage model on the simulated mechanical response of the geometries considered and provide an information workflow that is capable of coupling experiments with simulations that can be used for remaining useful life (RUL) estimations.

Highlights

  • Damage is a multiscale, spatially distributed, stochastic process bridging nucleation and growth that varies significantly among different material types

  • 3.1 Coupon-level analysis under monotonic and cyclic loading The data-driven damage model was first tested on a dogbone specimen subjected to monotonic loading to explore the effect of damage on the bulk mechanical response

  • Concluding remarks A data-driven continuum level local damage model based on multiphysics experimental information was proposed in this work

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Summary

Introduction

Spatially distributed, stochastic process bridging nucleation and growth that varies significantly among different material types. It has been reported that the incubation, nucleation and microstructurally-small growth regions consume most of the material’s life in high cycle fatigue loading schemes [1]. During this significant portion of material life, local microstructural features, which for example in metals include grain size and orientations, inclusions, voids etc. The damage parameter has a value of zero in the undamaged state and a value of one when final material failure has occurred [11] In this context, Kuna and Wippler [12] used a unified Chaboche model derived from a free energy potential which was enhanced to account for void growth. For an overview of microstructure-sensitive computational models with an application to fatigue crack growth, the authors refer to McDowell and Dunne [1] and references therein

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