Detail publikace

Properties of laminate consisting of carbon prepregs and aluminium sheets

KLEMENT, J.

Anglický název

Properties of laminate consisting of carbon prepregs and aluminium sheets

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

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.

Klíčová slova anglicky

fibre metal laminate, mechanical properties, fatigue, forming limits

Vydáno

2003-01-01

Nakladatel

VGTU

Místo

Vilnius

ISSN

1648-7788

Časopis

Aviation

Ročník

2003

Číslo

1

Strany od–do

16–

Počet stran

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"
}