On the progressive failure simulation and experimental validation of fiber metal laminate bolted joints

Research output: Contribution to journalArticleResearchpeer review

Authors

Research Organisations

External Research Organisations

  • German Aerospace Center (DLR) (e.V.) Location Braunschweig
View graph of relations

Details

Original languageEnglish
Article number111368
JournalComposite structures
Volume229
Early online date12 Sept 2019
Publication statusPublished - 1 Dec 2019

Abstract

The joint efficiency of mechanical joints in fiber-reinforced composite materials can be increased significantly by embedding metal plies in the composite layup, as in the case of fiber metal laminates. In this work, a novel finite element-based framework is presented for predicting the static progressive failure behavior of fiber metal laminate bolted joints. Motivated from experimental observations, the proposed framework accounts not only for damage in the fiber-reinforced composite plies, but also for different types of damage of the metallic inlays. For this purpose, user-defined continuum-damage constitutive models are formulated and employed in the general-purpose FE software Abaqus/Implicit for the fiber-reinforced polymer plies and the embedded metallic inlays. Accordingly, the interaction between different failure modes and the influence of the bolt's washer on the damage evolution is considered to increase the predictive quality. To demonstrate the applicability and validity of the developments, predictive simulations are carried out and compared to conducted experimental measurements on different fiber metal laminate grades (GFRP/stainless steel and CFRP/titanium) with a wide range of metal volume content, reaching from 0% (pure composite material) to 50%.

Keywords

    Bolted joints, Continuum damage modeling, Experimental validation, Fiber metal laminates, Static progressive failure prediction

ASJC Scopus subject areas

Cite this

On the progressive failure simulation and experimental validation of fiber metal laminate bolted joints. / Gerendt, Christian; Dean, Aamir; Mahrholz, Thorsten et al.
In: Composite structures, Vol. 229, 111368, 01.12.2019.

Research output: Contribution to journalArticleResearchpeer review

Gerendt C, Dean A, Mahrholz T, Rolfes R. On the progressive failure simulation and experimental validation of fiber metal laminate bolted joints. Composite structures. 2019 Dec 1;229:111368. Epub 2019 Sept 12. doi: 10.1016/j.compstruct.2019.111368
Download
@article{fd2b04b1db5b4d55a32dbbc125dc8395,
title = "On the progressive failure simulation and experimental validation of fiber metal laminate bolted joints",
abstract = "The joint efficiency of mechanical joints in fiber-reinforced composite materials can be increased significantly by embedding metal plies in the composite layup, as in the case of fiber metal laminates. In this work, a novel finite element-based framework is presented for predicting the static progressive failure behavior of fiber metal laminate bolted joints. Motivated from experimental observations, the proposed framework accounts not only for damage in the fiber-reinforced composite plies, but also for different types of damage of the metallic inlays. For this purpose, user-defined continuum-damage constitutive models are formulated and employed in the general-purpose FE software Abaqus/Implicit for the fiber-reinforced polymer plies and the embedded metallic inlays. Accordingly, the interaction between different failure modes and the influence of the bolt's washer on the damage evolution is considered to increase the predictive quality. To demonstrate the applicability and validity of the developments, predictive simulations are carried out and compared to conducted experimental measurements on different fiber metal laminate grades (GFRP/stainless steel and CFRP/titanium) with a wide range of metal volume content, reaching from 0% (pure composite material) to 50%.",
keywords = "Bolted joints, Continuum damage modeling, Experimental validation, Fiber metal laminates, Static progressive failure prediction",
author = "Christian Gerendt and Aamir Dean and Thorsten Mahrholz and Raimund Rolfes",
note = "Funding Information: The work presented in this paper was funded by the Federal Ministry of Education and Research of the Federal Republic of Germany under the project LENAH – Hybrid laminates and nanoparticle reinforced materials for improved rotor blade structures (Grant No. 03SF0529A). More explicitly the author would like to thank the project partners from the German Aerospace Center (DLR), namely the Institute of Composite Structures and Adaptive Systems, as well as the partners from the Fraunhofer Society, namely the Institute for Wind Energy Systems (IWES). They laid the foundation for this work by supporting us with material data, manufacturing the FML plates and corresponding test samples for performing the static bolt bearing tests according to up-to-date test standards (see [31]) used for model validation.",
year = "2019",
month = dec,
day = "1",
doi = "10.1016/j.compstruct.2019.111368",
language = "English",
volume = "229",
journal = "Composite structures",
issn = "0263-8223",
publisher = "Elsevier BV",

}

Download

TY - JOUR

T1 - On the progressive failure simulation and experimental validation of fiber metal laminate bolted joints

AU - Gerendt, Christian

AU - Dean, Aamir

AU - Mahrholz, Thorsten

AU - Rolfes, Raimund

N1 - Funding Information: The work presented in this paper was funded by the Federal Ministry of Education and Research of the Federal Republic of Germany under the project LENAH – Hybrid laminates and nanoparticle reinforced materials for improved rotor blade structures (Grant No. 03SF0529A). More explicitly the author would like to thank the project partners from the German Aerospace Center (DLR), namely the Institute of Composite Structures and Adaptive Systems, as well as the partners from the Fraunhofer Society, namely the Institute for Wind Energy Systems (IWES). They laid the foundation for this work by supporting us with material data, manufacturing the FML plates and corresponding test samples for performing the static bolt bearing tests according to up-to-date test standards (see [31]) used for model validation.

PY - 2019/12/1

Y1 - 2019/12/1

N2 - The joint efficiency of mechanical joints in fiber-reinforced composite materials can be increased significantly by embedding metal plies in the composite layup, as in the case of fiber metal laminates. In this work, a novel finite element-based framework is presented for predicting the static progressive failure behavior of fiber metal laminate bolted joints. Motivated from experimental observations, the proposed framework accounts not only for damage in the fiber-reinforced composite plies, but also for different types of damage of the metallic inlays. For this purpose, user-defined continuum-damage constitutive models are formulated and employed in the general-purpose FE software Abaqus/Implicit for the fiber-reinforced polymer plies and the embedded metallic inlays. Accordingly, the interaction between different failure modes and the influence of the bolt's washer on the damage evolution is considered to increase the predictive quality. To demonstrate the applicability and validity of the developments, predictive simulations are carried out and compared to conducted experimental measurements on different fiber metal laminate grades (GFRP/stainless steel and CFRP/titanium) with a wide range of metal volume content, reaching from 0% (pure composite material) to 50%.

AB - The joint efficiency of mechanical joints in fiber-reinforced composite materials can be increased significantly by embedding metal plies in the composite layup, as in the case of fiber metal laminates. In this work, a novel finite element-based framework is presented for predicting the static progressive failure behavior of fiber metal laminate bolted joints. Motivated from experimental observations, the proposed framework accounts not only for damage in the fiber-reinforced composite plies, but also for different types of damage of the metallic inlays. For this purpose, user-defined continuum-damage constitutive models are formulated and employed in the general-purpose FE software Abaqus/Implicit for the fiber-reinforced polymer plies and the embedded metallic inlays. Accordingly, the interaction between different failure modes and the influence of the bolt's washer on the damage evolution is considered to increase the predictive quality. To demonstrate the applicability and validity of the developments, predictive simulations are carried out and compared to conducted experimental measurements on different fiber metal laminate grades (GFRP/stainless steel and CFRP/titanium) with a wide range of metal volume content, reaching from 0% (pure composite material) to 50%.

KW - Bolted joints

KW - Continuum damage modeling

KW - Experimental validation

KW - Fiber metal laminates

KW - Static progressive failure prediction

UR - http://www.scopus.com/inward/record.url?scp=85072557538&partnerID=8YFLogxK

U2 - 10.1016/j.compstruct.2019.111368

DO - 10.1016/j.compstruct.2019.111368

M3 - Article

AN - SCOPUS:85072557538

VL - 229

JO - Composite structures

JF - Composite structures

SN - 0263-8223

M1 - 111368

ER -

By the same author(s)