Drawing behaviour of metal-composite sandwich structures

J. Gresham; W. Cantwell; M. J. Cardew-Hall; P. Compston; S. Kalyanasundaram

doi:10.1016/j.compstruct.2006.04.010

Drawing behaviour of metal-composite sandwich structures

J. Gresham
, W. Cantwell
, M. J. Cardew-Hall
, P. Compston
, S. Kalyanasundaram

Aerospace Engineering

Australian National University

Research output: Contribution to journal › Article › peer-review

127 Scopus citations

Abstract

The drawing behaviour of metal-composite sandwich structures is investigated as a function of the constituent material properties and the process variables of blank preheat temperature and blank-holder force. Materials include three grades of aluminium alloy as the skin layer material and two types of reinforced polypropylene composite as the core layer material. Blank-holder force has a significant effect on the failure mode of the metal-composite system with lower forces resulting in wrinkling as the dominate mode and higher forces resulting in splitting and fracture. Increasing preheat temperature decreases the failure in the composite core however it will increase the severity of wrinkling in the outer flange and sidewall.

Original language	British English
Pages (from-to)	305-312
Number of pages	8
Journal	Composite Structures
Volume	75
Issue number	1-4
DOIs	https://doi.org/10.1016/j.compstruct.2006.04.010
State	Published - Sep 2006

Keywords

Drawing
Fibre-metal laminate
Metal-composite
Stamp forming
Wrinkling

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10.1016/j.compstruct.2006.04.010

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title = "Drawing behaviour of metal-composite sandwich structures",

abstract = "The drawing behaviour of metal-composite sandwich structures is investigated as a function of the constituent material properties and the process variables of blank preheat temperature and blank-holder force. Materials include three grades of aluminium alloy as the skin layer material and two types of reinforced polypropylene composite as the core layer material. Blank-holder force has a significant effect on the failure mode of the metal-composite system with lower forces resulting in wrinkling as the dominate mode and higher forces resulting in splitting and fracture. Increasing preheat temperature decreases the failure in the composite core however it will increase the severity of wrinkling in the outer flange and sidewall.",

keywords = "Drawing, Fibre-metal laminate, Metal-composite, Stamp forming, Wrinkling",

author = "J. Gresham and W. Cantwell and Cardew-Hall, \{M. J.\} and P. Compston and S. Kalyanasundaram",

year = "2006",

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doi = "10.1016/j.compstruct.2006.04.010",

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AU - Gresham, J.

AU - Cantwell, W.

AU - Cardew-Hall, M. J.

AU - Compston, P.

AU - Kalyanasundaram, S.

PY - 2006/9

Y1 - 2006/9

N2 - The drawing behaviour of metal-composite sandwich structures is investigated as a function of the constituent material properties and the process variables of blank preheat temperature and blank-holder force. Materials include three grades of aluminium alloy as the skin layer material and two types of reinforced polypropylene composite as the core layer material. Blank-holder force has a significant effect on the failure mode of the metal-composite system with lower forces resulting in wrinkling as the dominate mode and higher forces resulting in splitting and fracture. Increasing preheat temperature decreases the failure in the composite core however it will increase the severity of wrinkling in the outer flange and sidewall.

AB - The drawing behaviour of metal-composite sandwich structures is investigated as a function of the constituent material properties and the process variables of blank preheat temperature and blank-holder force. Materials include three grades of aluminium alloy as the skin layer material and two types of reinforced polypropylene composite as the core layer material. Blank-holder force has a significant effect on the failure mode of the metal-composite system with lower forces resulting in wrinkling as the dominate mode and higher forces resulting in splitting and fracture. Increasing preheat temperature decreases the failure in the composite core however it will increase the severity of wrinkling in the outer flange and sidewall.

KW - Drawing

KW - Fibre-metal laminate

KW - Metal-composite

KW - Stamp forming

KW - Wrinkling

UR - https://www.scopus.com/pages/publications/33745740656

U2 - 10.1016/j.compstruct.2006.04.010

DO - 10.1016/j.compstruct.2006.04.010

M3 - Article

AN - SCOPUS:33745740656

SN - 0263-8223

VL - 75

SP - 305

EP - 312

JO - Composite Structures

JF - Composite Structures

IS - 1-4

ER -

Drawing behaviour of metal-composite sandwich structures

Abstract

Keywords

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