Experimental and numerical impact behavior of fully carbon fiber sandwiches for different core types
The aim of this study is to experimentally and numerically examine the impact strength and damage mechanisms of sandwich composites consisting entirely of fiber-reinforced composites for different core geometries. For this purpose, firstly, composite sandwich plates with egg box, lattice and square...
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Published in: | Journal of the Brazilian Society of Mechanical Sciences and Engineering Vol. 46; no. 5 |
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Main Authors: | , , |
Format: | Journal Article |
Language: | English |
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01-05-2024
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Abstract | The aim of this study is to experimentally and numerically examine the impact strength and damage mechanisms of sandwich composites consisting entirely of fiber-reinforced composites for different core geometries. For this purpose, firstly, composite sandwich plates with egg box, lattice and square plate core structures were produced. Low-velocity impact tests were carried out by dropping impactors with hemispherical geometry onto the resulting sandwich structure with three different core geometries, and the effect of the core shape on impact strength was determined. For comparison, the cell width and height of these three different types of core were chosen to be similar. In addition, progressive damage analysis with the finite element method was applied. For this purpose, the MAT-162 material model, which provides three-dimensional progressive damage analysis in composite materials and applies the Hashin damage criterion, was preferred to be used in the LS-DYNA
®
program. When specific loads are compared using a square core specimen under the same conditions, it can be said that the contact force of the egg box structure is higher. While the striker rebounded from the square core at the same impact energy, it perforated the sandwich structure in the egg box and completely damaged the lattice core structure. |
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AbstractList | The aim of this study is to experimentally and numerically examine the impact strength and damage mechanisms of sandwich composites consisting entirely of fiber-reinforced composites for different core geometries. For this purpose, firstly, composite sandwich plates with egg box, lattice and square plate core structures were produced. Low-velocity impact tests were carried out by dropping impactors with hemispherical geometry onto the resulting sandwich structure with three different core geometries, and the effect of the core shape on impact strength was determined. For comparison, the cell width and height of these three different types of core were chosen to be similar. In addition, progressive damage analysis with the finite element method was applied. For this purpose, the MAT-162 material model, which provides three-dimensional progressive damage analysis in composite materials and applies the Hashin damage criterion, was preferred to be used in the LS-DYNA
®
program. When specific loads are compared using a square core specimen under the same conditions, it can be said that the contact force of the egg box structure is higher. While the striker rebounded from the square core at the same impact energy, it perforated the sandwich structure in the egg box and completely damaged the lattice core structure. The aim of this study is to experimentally and numerically examine the impact strength and damage mechanisms of sandwich composites consisting entirely of fiber-reinforced composites for different core geometries. For this purpose, firstly, composite sandwich plates with egg box, lattice and square plate core structures were produced. Low-velocity impact tests were carried out by dropping impactors with hemispherical geometry onto the resulting sandwich structure with three different core geometries, and the effect of the core shape on impact strength was determined. For comparison, the cell width and height of these three different types of core were chosen to be similar. In addition, progressive damage analysis with the finite element method was applied. For this purpose, the MAT-162 material model, which provides three-dimensional progressive damage analysis in composite materials and applies the Hashin damage criterion, was preferred to be used in the LS-DYNA® program. When specific loads are compared using a square core specimen under the same conditions, it can be said that the contact force of the egg box structure is higher. While the striker rebounded from the square core at the same impact energy, it perforated the sandwich structure in the egg box and completely damaged the lattice core structure. |
ArticleNumber | 318 |
Author | Kaman, Mete Onur Albayrak, Mustafa Bozkurt, Ilyas |
Author_xml | – sequence: 1 givenname: Ilyas surname: Bozkurt fullname: Bozkurt, Ilyas organization: Department of Mechanical Engineering, Architecture and Engineering Faculty, Mus Alparslan University – sequence: 2 givenname: Mete Onur orcidid: 0000-0003-0178-6079 surname: Kaman fullname: Kaman, Mete Onur email: mkaman@firat.edu.tr organization: Department of Mechanical Engineering, Engineering Faculty, Firat University – sequence: 3 givenname: Mustafa surname: Albayrak fullname: Albayrak, Mustafa organization: Department of Machine and Metal Technologies, Malatya Organized Industrial Zone Vocational School, Inonu University |
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Copyright_xml | – notice: The Author(s), under exclusive licence to The Brazilian Society of Mechanical Sciences and Engineering 2024. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law. |
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SubjectTerms | Carbon fibers Composite materials Contact force Damage assessment Engineering Fiber composites Finite element method Impact strength Impact tests Impactors Mechanical Engineering Sandwich structures Shape effects Square plates Technical Paper Three dimensional analysis Three dimensional models |
Title | Experimental and numerical impact behavior of fully carbon fiber sandwiches for different core types |
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