Experimental observation and finite element method modeling on scratch‐induced delamination of multilayer polymeric structures

Scratches that result in delamination are common in multilayer polymeric laminates and coatings. In this study, the adhesive failure among a set of model double‐layer epoxy coatings was experimentally investigated and numerically analyzed using the finite element method modeling based on the maximum...

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Published inPolymer engineering and science Vol. 61; no. 6; pp. 1742 - 1754
Main Authors Du, Shuoran, Zhu, Zewen, Liu, Cong, Zhang, Tan, Hossain, Mohammad Motaher, Sue, Hung‐Jue
Format Journal Article
LanguageEnglish
Published Hoboken, USA John Wiley & Sons, Inc 01.06.2021
Society of Plastics Engineers, Inc
Blackwell Publishing Ltd
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Online AccessGet full text
ISSN0032-3888
1548-2634
DOI10.1002/pen.25697

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Abstract Scratches that result in delamination are common in multilayer polymeric laminates and coatings. In this study, the adhesive failure among a set of model double‐layer epoxy coatings was experimentally investigated and numerically analyzed using the finite element method modeling based on the maximum principal stress criterion. The adhesive failure on the model epoxy coatings was generated using an ASTM‐standard linearly increasing normal load scratch test. The parametric study reveals that delamination may initiate at locations underneath both scratch shoulder and behind scratch tip during scratching. It is also found that the magnitude and direction of peak tensile maximum principal stress developed at the interface are affected by both the laminate thickness and the material parameters of each layer. The parametric analysis shows that the onset of delamination can be delayed by possessing a softer base layer, a top or base layer with a higher yield stress, a base layer with a lower strain‐hardening slope, and a lower surface coefficient of friction. The Mode I delamination at the interface will become dominant in a multilayer system when the base layer has a higher modulus and a lower strain hardening slope. The usefulness of the present study for determining the delamination resistance of multilayer polymeric laminates and coatings is discussed.
AbstractList Scratches that result in delamination are common in multilayer polymeric laminates and coatings. In this study, the adhesive failure among a set of model double-layer epoxy coatings was experimentally investigated and numerically analyzed using the finite element method modeling based on the maximum principal stress criterion. The adhesive failure on the model epoxy coatings was generated using an ASTM-standard linearly increasing normal load scratch test. The parametric study reveals that delamination may initiate at locations underneath both scratch shoulder and behind scratch tip during scratching. It is also found that the magnitude and direction of peak tensile maximum principal stress developed at the interface are affected by both the laminate thickness and the material parameters of each layer. The parametric analysis shows that the onset of delamination can be delayed by possessing a softer base layer, a top or base layer with a higher yield stress, a base layer with a lower strain-hardening slope, and a lower surface coefficient of friction. The Mode I delamination at the interface will become dominant in a multilayer system when the base layer has a higher modulus and a lower strain hardening slope. The usefulness of the present study for determining the delamination resistance of multilayer polymeric laminates and coatings is discussed.
Scratches that result in delamination are common in multilayer polymeric laminates and coatings. In this study, the adhesive failure among a set of model double-layer epoxy coatings was experimentally investigated and numerically analyzed using the finite element method modeling based on the maximum principal stress criterion. The adhesive failure on the model epoxy coatings was generated using an ASTM-standard linearly increasing normal load scratch test. The parametric study reveals that delamination may initiate at locations underneath both scratch shoulder and behind scratch tip during scratching. It is also found that the magnitude and direction of peak tensile maximum principal stress developed at the interface are affected by both the laminate thickness and the material parameters of each layer. The parametric analysis shows that the onset of delamination can be delayed by possessing a softer base layer, a top or base layer with a higher yield stress, a base layer with a lower strain-hardening slope, and a lower surface coefficient of friction. The Mode I delamination at the interface will become dominant in a multilayer system when the base layer has a higher modulus and a lower strain hardening slope. The usefulness of the present study for determining the delamination resistance of multilayer polymeric laminates and coatings is discussed. KEYWORDS coatings, delamination, finite element method, multilayer polymeric systems, scratch behavior
Audience Academic
Author Du, Shuoran
Sue, Hung‐Jue
Zhu, Zewen
Hossain, Mohammad Motaher
Liu, Cong
Zhang, Tan
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Snippet Scratches that result in delamination are common in multilayer polymeric laminates and coatings. In this study, the adhesive failure among a set of model...
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SubjectTerms Coatings
Coefficient of friction
Delamination
Epoxy resins
Finite element analysis
Finite element method
Laminated materials
Laminates
Mechanical properties
Modelling
multilayer polymeric systems
Multilayers
Parametric analysis
Polymers
scratch behavior
Scratch tests
Scratching
Strain hardening
Structure
Yield stress
Title Experimental observation and finite element method modeling on scratch‐induced delamination of multilayer polymeric structures
URI https://onlinelibrary.wiley.com/doi/abs/10.1002%2Fpen.25697
https://www.proquest.com/docview/2537144284
Volume 61
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