Publication detail

Properties of laminate consisting of carbon prepregs and aluminium sheets

KLEMENT, J.

Original Title

Properties of laminate consisting of carbon prepregs and aluminium sheets

Type

journal article - other

Language

English

Original Abstract

The paper describes research results of the material consisting of C/epoxy prepreg and AlCu4Mg1 aluminium alloy layers. This combination reaches tensile strength up to 900 MPa, tensile modulus 87 GPa and interlaminar shear strength 80 MPa. Fatigue properties are excellent. The material formability enables in limited grade to use forming techniques for parts manufacture. Future investigation is indicated.

Keywords

fibre metal laminate, mechanical properties, fatigue, forming limits

Authors

KLEMENT, J.

RIV year

2004

Released

1. 1. 2003

Publisher

VGTU

Location

Vilnius

ISBN

1648-7788

Periodical

AVIATION

Year of study

2003

Number

1

State

Republic of Lithuania

Pages from

16

Pages to

21

Pages count

6

BibTex

@article{BUT41488,
  author="Josef {Klement}",
  title="Properties of laminate consisting of carbon prepregs and aluminium sheets",
  journal="AVIATION",
  year="2003",
  volume="2003",
  number="1",
  pages="6",
  issn="1648-7788"
}