Demonstration of pseudo-ductility in quasi-isotropic laminates comprising thin-ply UD carbon/epoxy hybrid sub-laminates

G. Czél; T. Rév; M. Jalalvand; M. Fotouhi; M. R. Wisnom

Demonstration of pseudo-ductility in quasi-isotropic laminates comprising thin-ply UD carbon/epoxy hybrid sub-laminates

G. Czél, T. Rév, M. Jalalvand, M. Fotouhi, M. R. Wisnom

Mechanical And Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

4 Citations (Scopus)

Abstract

Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates were studied. It was confirmed that ply fragmentation demonstrated previously as a successful ductility mechanism can be transferred to multi-directional laminates. Furthermore, notch-insensitivity was demonstrated by locally active fragmentation in notched quasi-isotropic specimens.

Original language	English
Title of host publication	ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials
ISBN (Electronic)	9783000533877
Publication status	Published - 2016
Event	17th European Conference on Composite Materials, ECCM 2016 - Munich, Germany Duration: 26 Jun 2016 → 30 Jun 2016

Conference

Conference	17th European Conference on Composite Materials, ECCM 2016
Country	Germany
City	Munich
Period	26/06/16 → 30/06/16

Keywords

carbon/epoxy
pseudo-ductility
quasi-isotropic

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abstract = "Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates were studied. It was confirmed that ply fragmentation demonstrated previously as a successful ductility mechanism can be transferred to multi-directional laminates. Furthermore, notch-insensitivity was demonstrated by locally active fragmentation in notched quasi-isotropic specimens.",

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AU - Rév, T.

AU - Jalalvand, M.

AU - Fotouhi, M.

AU - Wisnom, M. R.

PY - 2016

Y1 - 2016

N2 - Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates were studied. It was confirmed that ply fragmentation demonstrated previously as a successful ductility mechanism can be transferred to multi-directional laminates. Furthermore, notch-insensitivity was demonstrated by locally active fragmentation in notched quasi-isotropic specimens.

AB - Un-notched and notched tensile response and damage accumulation of quasi-isotropic carbon/epoxy hybrid laminates were studied. It was confirmed that ply fragmentation demonstrated previously as a successful ductility mechanism can be transferred to multi-directional laminates. Furthermore, notch-insensitivity was demonstrated by locally active fragmentation in notched quasi-isotropic specimens.

KW - carbon/epoxy

KW - pseudo-ductility

KW - quasi-isotropic

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AN - SCOPUS:85018193966

BT - ECCM 2016 - Proceeding of the 17th European Conference on Composite Materials

T2 - 17th European Conference on Composite Materials, ECCM 2016

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