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Constitutive modeling and experimental characterization of the non-linear stress-strain behavior of unidirectional carbon-epoxy under high strain rates

Publikation: KonferenzbeitragPaperForschungPeer-Review

Autorschaft

  • Matthias Vogler
  • Hannes Koerber
  • Peter Kuhn
  • Raimund Rolfes

Organisationseinheiten

Externe Organisationen

  • Consulting Engineer
  • Technische Universität München (TUM)
  • Universidade do Porto

Details

OriginalspracheEnglisch
PublikationsstatusVeröffentlicht - 2015
Veranstaltung20th International Conference on Composite Materials, ICCM 2015 - Copenhagen, Dänemark
Dauer: 19 Juli 201524 Juli 2015

Konferenz

Konferenz20th International Conference on Composite Materials, ICCM 2015
Land/GebietDänemark
OrtCopenhagen
Zeitraum19 Juli 201524 Juli 2015

Abstract

The mechanical response of IM7-8552 carbon epoxy was investigated for transverse tension and transverse tension / in-plane shear loadings at static and dynamic strain rates using transverse tension and off-axis tension specimens. The dynamic tests were carried out on a split-Hopkinson tension bar at axial strain rates from 113s-1 to 300s-1. With the already available off-axis and transverse compression test data for IM7-8552 presented in [1], a comprehensive data set is available now, which can be used for validation and calibration of numerical models. The measured axial stress-strain response was simulated using a fully 3D transversely isotropic elastic-viscoplastic constitutive model. The constitutive model represents a viscoplastic extension of the transversely-isotropic plasticity model presented in [2]. A generally quite good correlation between the measured and numerically predicted stress-strain response was achieved for all specimen types and both strain rate regimes. However, the results show the necessity to regard viscous effects in the elastic regime as well.

ASJC Scopus Sachgebiete

Zitieren

Constitutive modeling and experimental characterization of the non-linear stress-strain behavior of unidirectional carbon-epoxy under high strain rates. / Vogler, Matthias; Koerber, Hannes; Kuhn, Peter et al.
2015. Beitrag in 20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Dänemark.

Publikation: KonferenzbeitragPaperForschungPeer-Review

Vogler, M, Koerber, H, Kuhn, P, Rolfes, R & Camanho, P 2015, 'Constitutive modeling and experimental characterization of the non-linear stress-strain behavior of unidirectional carbon-epoxy under high strain rates', Beitrag in 20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Dänemark, 19 Juli 2015 - 24 Juli 2015. <http://www.iccm-central.org/Proceedings/ICCM20proceedings/papers/paper-3210-1.pdf>
Vogler M, Koerber H, Kuhn P, Rolfes R, Camanho P. Constitutive modeling and experimental characterization of the non-linear stress-strain behavior of unidirectional carbon-epoxy under high strain rates. 2015. Beitrag in 20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Dänemark.
Vogler, Matthias ; Koerber, Hannes ; Kuhn, Peter et al. / Constitutive modeling and experimental characterization of the non-linear stress-strain behavior of unidirectional carbon-epoxy under high strain rates. Beitrag in 20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Dänemark.
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author = "Matthias Vogler and Hannes Koerber and Peter Kuhn and Raimund Rolfes and Pedro Camanho",
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AU - Vogler, Matthias

AU - Koerber, Hannes

AU - Kuhn, Peter

AU - Rolfes, Raimund

AU - Camanho, Pedro

N1 - Publisher Copyright: © 2015 International Committee on Composite Materials. All rights reserved. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.

PY - 2015

Y1 - 2015

N2 - The mechanical response of IM7-8552 carbon epoxy was investigated for transverse tension and transverse tension / in-plane shear loadings at static and dynamic strain rates using transverse tension and off-axis tension specimens. The dynamic tests were carried out on a split-Hopkinson tension bar at axial strain rates from 113s-1 to 300s-1. With the already available off-axis and transverse compression test data for IM7-8552 presented in [1], a comprehensive data set is available now, which can be used for validation and calibration of numerical models. The measured axial stress-strain response was simulated using a fully 3D transversely isotropic elastic-viscoplastic constitutive model. The constitutive model represents a viscoplastic extension of the transversely-isotropic plasticity model presented in [2]. A generally quite good correlation between the measured and numerically predicted stress-strain response was achieved for all specimen types and both strain rate regimes. However, the results show the necessity to regard viscous effects in the elastic regime as well.

AB - The mechanical response of IM7-8552 carbon epoxy was investigated for transverse tension and transverse tension / in-plane shear loadings at static and dynamic strain rates using transverse tension and off-axis tension specimens. The dynamic tests were carried out on a split-Hopkinson tension bar at axial strain rates from 113s-1 to 300s-1. With the already available off-axis and transverse compression test data for IM7-8552 presented in [1], a comprehensive data set is available now, which can be used for validation and calibration of numerical models. The measured axial stress-strain response was simulated using a fully 3D transversely isotropic elastic-viscoplastic constitutive model. The constitutive model represents a viscoplastic extension of the transversely-isotropic plasticity model presented in [2]. A generally quite good correlation between the measured and numerically predicted stress-strain response was achieved for all specimen types and both strain rate regimes. However, the results show the necessity to regard viscous effects in the elastic regime as well.

KW - Carbon-epoxy

KW - Composites

KW - Constitutive modeling

KW - Strain rate effects

KW - Viscoplasticity

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T2 - 20th International Conference on Composite Materials, ICCM 2015

Y2 - 19 July 2015 through 24 July 2015

ER -

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