Debonding behavior of non-welded wrapped composite X-joints subjected to monotonic tensile load – Numerical study and validation

The dominant failure mode in the non-welded wrapped composite joints made with GFRP composite material wrapped around steel circular hollow sections (CHS) is characterized as interface debonding. However, in the ultimate load joint experiments, debonding process was merely inferred from the surface strain distribution obtained by the digital image correlation (DIC). A thorough understanding and explicit illustration of debonding mechanism in wrapped composite X-joints is needed with help of finite element modeling (FEM), in order to provide prediction models for design of wrapped composite joints in engineering structures. In this paper, two FE models were developed to simulate the debonding behavior of small-scale and medium-scale wrapped composite 45° X-joints in monotonic tensile tests previously conducted by the authors. A new strategy of modeling complex composite geometry using 4-node tetrahedral elements (C3D4) without defining composite lay-up was proposed. The cohesive zone modeling (CZM) approach was utilized to simulate the debonding behavior of composite-steel interface with introduction of a new four-linear traction-separation law. The generated FE models were validated by good agreement between numerical and experimental results in terms of load-displacement response and surface strain distribution throughout the failure process at two joint scales. The validated models gained good insight into the joint debonding mechanism and determined the surface strain threshold for quantifying the debonding length. Development and validation of the FE models with unique set of parameters aligned well with the experiment results at two different scales is an important step for prediction and design of wrapped composite joints. • Cohesive zone model to simulate debonding of the complex interface. • Anisotropic plasticity model to equivalently simulate the softening behavior of composites. • Finte element model with the unique set of parameters matches well to the tests at two-scales. • Design recommendations for joint resistance based on simple mechanical-based formula.

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Publication Details

Journal
Engineering Structures
Published
2024-09-16
DOI
https://doi.org/10.1016/j.engstruct.2024.118969
Citations
3
Primary Topic
Structural Load-Bearing Analysis
Type
article
Field-Weighted Citation Impact
0.78

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article

Debonding behavior of non-welded wrapped composite X-joints subjected to monotonic tensile load – Numerical study and validation

Marko Pavlović, Pei He, Clement Waltener, Mees Wolters
3 citations
Engineering Structures
Structural Load-Bearing Analysis
0.78
article

Debonding behavior of non-welded wrapped composite X-joints subjected to monotonic tensile load – Numerical study and validation

Marko Pavlović, Pei He, Clement Waltener, Mees Wolters
article en
3 citations

Abstract

The dominant failure mode in the non-welded wrapped composite joints made with GFRP composite material wrapped around steel circular hollow sections (CHS) is characterized as interface debonding. However, in the ultimate load joint experiments, debonding process was merely inferred from the surface strain distribution obtained by the digital image correlation (DIC). A thorough understanding and explicit illustration of debonding mechanism in wrapped composite X-joints is needed with help of finite element modeling (FEM), in order to provide prediction models for design of wrapped composite joints in engineering structures. In this paper, two FE models were developed to simulate the debonding behavior of small-scale and medium-scale wrapped composite 45° X-joints in monotonic tensile tests previously conducted by the authors. A new strategy of modeling complex composite geometry using 4-node tetrahedral elements (C3D4) without defining composite lay-up was proposed. The cohesive zone modeling (CZM) approach was utilized to simulate the debonding behavior of composite-steel interface with introduction of a new four-linear traction-separation law. The generated FE models were validated by good agreement between numerical and experimental results in terms of load-displacement response and surface strain distribution throughout the failure process at two joint scales. The validated models gained good insight into the joint debonding mechanism and determined the surface strain threshold for quantifying the debonding length. Development and validation of the FE models with unique set of parameters aligned well with the experiment results at two different scales is an important step for prediction and design of wrapped composite joints. • Cohesive zone model to simulate debonding of the complex interface. • Anisotropic plasticity model to equivalently simulate the softening behavior of composites. • Finte element model with the unique set of parameters matches well to the tests at two-scales. • Design recommendations for joint resistance based on simple mechanical-based formula.

Engineering StructuresVol. 321
Eco Composites (United States) (US), Delft University of Technology (NL)
Nederlandse Organisatie voor Wetenschappelijk Onderzoek, China Scholarship Council
Openalex Percentile: Top 30%
Structural Load-Bearing Analysis
0.78
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