Experimental and numerical investigation on the impact response of CFRP under 3-point-bending

The strain rate-dependent material characteristic of carbon fiber reinforced plastics (CFRP) is widely known and has been investigated in detail at coupon level. In this study, for the first time the strain rate dependent characteristic of a three-dimensional CFRP structure was investigated. The evo...

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Main Authors: M. Nebe, T. Schmack, T. Schaefer, F. Walther
Format: Article
Language:English
Published: Elsevier 2021-03-01
Series:Composites Part C: Open Access
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2666682020300797
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spelling doaj-431221e8a37c431bb3bf8f5198530ab12021-05-04T07:33:54ZengElsevierComposites Part C: Open Access2666-68202021-03-014100079Experimental and numerical investigation on the impact response of CFRP under 3-point-bendingM. Nebe0T. Schmack1T. Schaefer2F. Walther3Department of Materials Test Engineering (WPT), TU Dortmund University, Baroper Str. 303, 44227 Dortmund, Germany; Corresponding author.Department of Materials Test Engineering (WPT), TU Dortmund University, Baroper Str. 303, 44227 Dortmund, Germany; Lightweight Center, Audi AG, NSU-Straße 1, 74148 Neckarsulm, GermanyDepartment of Lightweight Technology (LBT), Karlsruhe Institute of Technology (KIT), Rintheimer-Querallee 2, 76131 Karlsruhe, GermanyDepartment of Materials Test Engineering (WPT), TU Dortmund University, Baroper Str. 303, 44227 Dortmund, GermanyThe strain rate-dependent material characteristic of carbon fiber reinforced plastics (CFRP) is widely known and has been investigated in detail at coupon level. In this study, for the first time the strain rate dependent characteristic of a three-dimensional CFRP structure was investigated. The evolution of the determined strain rate dependency was correlated with the results at coupon level. For this purpose two special 3-point-bending fixtures were developed to obtain the flexural impact response of the investigated T700S DT120 prepreg system at coupon and component (hat profile) level. The rectangular coupon specimens were loaded with quasi-static to intermediate impact velocities from 3.3×10−5 to 10m s−1, while the structural sub components were tested using impact velocities from 3.3×10−5 to 1m s−1. With increasing impact velocities, the experimental tests showed a significant increase in force at first failure and maximum deflection at coupon level. The increases in force were of 52% and 120%, respectively. However, the increase for structural hat profile components was just 12.4% due to a different failure mode. The observed initial failure modes were compressive failure provoked by fiber kinking for the coupon and interlaminar shear failure for the structural component. Regardless of the different failure modes this work proves the necessity of considering the strain rate dependency of a composite material to accurately predict the maximum load capacity of a CFRP structure during a dynamic load event. Additionally, the comparison of the experimental results restults to numerical results revealed weaknesses in the prediction accuracy of the currently used models.http://www.sciencedirect.com/science/article/pii/S2666682020300797Carbon fiberEpoxyPrepregStrain rateComponent testing3-Point-bending
collection DOAJ
language English
format Article
sources DOAJ
author M. Nebe
T. Schmack
T. Schaefer
F. Walther
spellingShingle M. Nebe
T. Schmack
T. Schaefer
F. Walther
Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
Composites Part C: Open Access
Carbon fiber
Epoxy
Prepreg
Strain rate
Component testing
3-Point-bending
author_facet M. Nebe
T. Schmack
T. Schaefer
F. Walther
author_sort M. Nebe
title Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
title_short Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
title_full Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
title_fullStr Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
title_full_unstemmed Experimental and numerical investigation on the impact response of CFRP under 3-point-bending
title_sort experimental and numerical investigation on the impact response of cfrp under 3-point-bending
publisher Elsevier
series Composites Part C: Open Access
issn 2666-6820
publishDate 2021-03-01
description The strain rate-dependent material characteristic of carbon fiber reinforced plastics (CFRP) is widely known and has been investigated in detail at coupon level. In this study, for the first time the strain rate dependent characteristic of a three-dimensional CFRP structure was investigated. The evolution of the determined strain rate dependency was correlated with the results at coupon level. For this purpose two special 3-point-bending fixtures were developed to obtain the flexural impact response of the investigated T700S DT120 prepreg system at coupon and component (hat profile) level. The rectangular coupon specimens were loaded with quasi-static to intermediate impact velocities from 3.3×10−5 to 10m s−1, while the structural sub components were tested using impact velocities from 3.3×10−5 to 1m s−1. With increasing impact velocities, the experimental tests showed a significant increase in force at first failure and maximum deflection at coupon level. The increases in force were of 52% and 120%, respectively. However, the increase for structural hat profile components was just 12.4% due to a different failure mode. The observed initial failure modes were compressive failure provoked by fiber kinking for the coupon and interlaminar shear failure for the structural component. Regardless of the different failure modes this work proves the necessity of considering the strain rate dependency of a composite material to accurately predict the maximum load capacity of a CFRP structure during a dynamic load event. Additionally, the comparison of the experimental results restults to numerical results revealed weaknesses in the prediction accuracy of the currently used models.
topic Carbon fiber
Epoxy
Prepreg
Strain rate
Component testing
3-Point-bending
url http://www.sciencedirect.com/science/article/pii/S2666682020300797
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AT tschmack experimentalandnumericalinvestigationontheimpactresponseofcfrpunder3pointbending
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