Naila Hfaiedh

@article{khadimallah_2380,

title = {Characterization of fatigue behavior of AA2024-T351 aluminum alloy},

author = {Aymen Khadimallah and Johann Petit and Naila Hfaiedh and Amna Znaidi},

url = {https://onlinelibrary.wiley.com/share/author/5HS4PJKGQVKNQNGDT9QT?target=10.1111/ffe.14102},

year  = {2023},

date = {2023-10-01},

journal = {Fatigue & Fracture Of Engineering Materials & Structures},

volume = {46},

number = {10},

pages = {3543-4072},

abstract = {The paper aims to investigate the fatigue behavior of the widely used

AA2024-T351 aluminum alloy in the aircraft industry. An experimental program

was conducted to study the fatigue life and damage behavior under symmetrical

tensile-compressive loading. Cyclic tests in the low cycle fatigue

regime were performed under fully reversed total strain amplitudes from 0.6%

to 1.2%. The AA2024-T351 alloy exhibited cyclic hardening until failure. Symmetric

high cycle fatigue tests were also performed and the parameters for

fatigue life estimation using the Manson-Coffin-Basquin model were identified.

Elasto-plastic behavior was analyzed through stress-strain hysteresis

loops, evaluating kinematic and isotropic hardenings. Kinematic hardening

was found to be strain amplitude dependent, unlike the isotropic hardening.

The evolution of the isotropic variable with the percentage of fatigue life could

be described by an exponential law. Fractography investigations showed crack

initiation at the specimen border with quasi-cleavage and then crack propagating

by striation before ductile fracture.},

keywords = {},

pubstate = {published},

tppubtype = {article}

}

@article{zhang_1406,

title = {Failure prediction of magnesium alloys based on improved CDM model},

author = {Kai Zhang and Houssem Badreddine and Naila Hfaiedh and Khemais Saanouni and Jianlin Liu},

url = {https://www.sciencedirect.com/science/article/abs/pii/S0020768321000214?via%3Dihub},

year  = {2021},

date = {2021-01-01},

journal = {International Journal Of Solids And Structures},

volume = {217-218},

pages = {155-177},

abstract = {The aim of this contribution is to improve the behavior and failure prediction accuracy for magnesium alloy sheet forming simulation by using advanced fully coupled Continuum Damage Mechanics (CDM) model. Starting from known fully coupled constitutive equations at large inelastic (plastic or viscoplastic) strains, three aspects are enhanced on the CDM model developed by Saanouni (2012). The first one concerns the accurate description of tension-compression asymmetry in yielding and hardening of magnesium alloys induced by combined slip and twinning deformations. The second concerns introducing the stress state dependence in damage evolution to improve the fracture prediction under various loading paths. The third deals with temperature and strain rate (viscosity) effects for metal forming processes at elevated temperatures. The improved fully coupled constitutive equations were implemented into finite element code ABAQUS/Explicit via user subroutine VUMAT including the specific local integration scheme to compute the state variables at each quadrature point. Various kinds of tensile tests at different temperatures and strain rates are used to determine the material parameters, and the complete identification procedure is given in details. As validation, the improved model is applied to simulate the three-point bending and circular cup deep drawing tests, the predicted results show good agreements with the experimental observations.},

keywords = {},

pubstate = {published},

tppubtype = {article}

}

@article{badreddine_2810,

title = {A fully coupled damage model with stress triaxiality and Lode dependence},

author = {Houssem Badreddine and Naila Hfaiedh and Khemais Saanouni},

url = {https://iopscience.iop.org/article/10.1088/1757-899X/967/1/012051},

year  = {2020},

date = {2020-10-01},

volume = {967},

number = {1},

pages = {012051},

abstract = {In the present work, an advanced CDM model considering stress triaxiality and Lode

angle effect is proposed. The framework of thermodynamics of irreversible processes with

state variables is used to build the constitutive equations accounting for strong and full

coupling between all the dissipative phenomena. The proposed model is implemented into

Finite Element (FE) code ABAQUS/Explicit via a user material subroutine (VUMAT). A

detailed parametric study with various values of the new material parameters is conducted in

order to show the predictive capability of the proposed model. Applications to sheet metal

forming simulation have been performed to validate the damage prediction capability of the

proposed model, and the numerical simulation results are analysed and discussed},

keywords = {},

pubstate = {published},

tppubtype = {article}

}

@article{zhang_1270,

title = {Enhanced CDM model accounting of stress triaxiality and Lode angle for ductile damage prediction in metal forming},

author = {Kai Zhang and Houssem Badreddine and Naila Hfaiedh and Khemais Saanouni and Jianlin Liu},

url = {https://journals.sagepub.com/doi/full/10.1177/1056789520958045},

year  = {2020},

date = {2020-09-01},

journal = {International Journal Of Damage Mechanics},

volume = {30},

number = {2},

pages = {260-282},

abstract = {This paper deals with the prediction of ductile damage based on CDM approach fully coupled with advanced elastoplastic constitutive equations. This fully coupled damage model is developed based on the total energy equivalence assumption under the thermodynamics of irreversible processes framework with state variables. In this model, the damage evolution is enhanced by accounting for both stress triaxiality and Lode angle. The proposed constitutive equations are implemented into Finite Element (FE) code ABAQUS/Explicit through a user material subroutine (VUMAT). The material parameters are determined by the hybrid experimental-numerical method using various tensile and shear tests. Validation of the proposed model has been done using different tests of two aluminum alloys (Al6061-T6 and Al6014-T4). Through comparisons of numerical simulations with experimental results for different loading paths, the predictive capabilities of the proposed model have been shown. The model is found to be able to capture the initiation as well as propagation of macro-crack in sheet and bulk metals during their forming processes},

keywords = {},

pubstate = {published},

tppubtype = {article}

}

@article{hfaiedh_505,

title = {Interaction between ductile damage and texture evolution in finite polycrystalline elastoplasticity},

author = {Naila Hfaiedh and A. Roos and Houssem Badreddine and Khemais Saanouni},

url = {https://journals.sagepub.com/doi/10.1177/1056789518775179},

year  = {2019},

date = {2019-04-01},

journal = {International Journal Of Damage Mechanics},

volume = {28},

number = {4},

pages = {481-501},

abstract = {In this paper, a multiscale model of ductile damage and its effects on the inelastic behavior of face centered cubic polycrystalline metallic materials, such as the evolution of their crystallographic textures, are investigated. The constitutive equations are written in the framework of rate-dependent polycrystalline plasticity at the microscopic scale. Plasticity and damage are coupled through a ductile damage variable introduced at the scale of the crystallographic slip systems of each grain. When homogenized to the macro-scale, this becomes an approximate phenomenological measure of the macroscopic ductile damage which can describe the material degradation by initiation, growth, and coalescence of micro-defects. In this paper, thermally activated intergranular (or creep) damage is not taken into account. Both theoretical and numerical aspects of the model are presented. The model is implemented into a generalpurpose finite element code in order to analyze the effects of texture evolution and ductile damage initiation in the grains with favorably oriented slip systems. The capability of the proposed model to predict the plastic strain localization and the induced textural evolution, as well as the effects of the ductile damage and its evolution up to the final macroscopic failure are studied for a classical tensile loading path, applied to a representative volume element and to a 3D tensile specimen on which a parametric study has been carried out.},

keywords = {},

pubstate = {published},

tppubtype = {article}

}

@article{hfaiedh_2812,

title = {Finite element analysis of laser shock peening of 2050-T8 aluminum alloy},

author = {Naila Hfaiedh and Patrice Peyre and Song Hongbin and Ioana Popa and Vincent Ji and Vincent Vignal},

url = {https://www.sciencedirect.com/science/article/pii/S0142112314001686},

year  = {2015},

date = {2015-01-01},

journal = {International Journal Of Fatigue},

volume = {70},

pages = {480-489},

abstract = {Laser shock processing is a recently developed surface treatment designed to improve the mechanical

properties and fatigue performance of materials, by inducing a deep compressive residual stress field.

The purpose of this work is to investigate the residual stress distribution induced by laser shock process-

ing in a 2050-T8 aeronautical aluminium alloy with both X-ray diffraction measurements and 3D finite

element simulation. The method of X-ray diffraction is extensively used to characterize the crystallo-

graphic texture and the residual stress crystalline materials at different scales (macroscopic, mesoscopic

and microscopic).

Shock loading and materials' dynamic response are experimentally analysed using Doppler velocimetry

in order to use adequate data for the simulation. Then systematic experience versus simulation compar-

isons are addressed, considering first a single impact loading, and in a second step the laser shock

processing treatment of an extended area, with a specific focus on impact overlap. Experimental and

numerical results indicate a residual stress anisotropy, and a better surface stress homogeneity with

an increase of impact overlap.

A correct agreement is globally shown between experimental and simulated residual stress values,

even if simulations provide us with local stress values whereas X-ray diffraction determinations give

averaged residual stresses.},

keywords = {},

pubstate = {published},

tppubtype = {article}

}