Publication detail

Properties of laminate consisting of carbon prepregs and aluminium sheets

KLEMENT, J.

English title

Properties of laminate consisting of carbon prepregs and aluminium sheets

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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 in English

fibre metal laminate, mechanical properties, fatigue, forming limits

Released

2003-01-01

Publisher

VGTU

Location

Vilnius

ISSN

1648-7788

Journal

Aviation

Volume

2003

Number

1

Pages from–to

16–

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"
}