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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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 |
work_keys_str_mv |
AT mnebe experimentalandnumericalinvestigationontheimpactresponseofcfrpunder3pointbending AT tschmack experimentalandnumericalinvestigationontheimpactresponseofcfrpunder3pointbending AT tschaefer experimentalandnumericalinvestigationontheimpactresponseofcfrpunder3pointbending AT fwalther experimentalandnumericalinvestigationontheimpactresponseofcfrpunder3pointbending |
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1721479719566704640 |