Detail publikace

Properties of laminate consisting of carbon prepregs and aluminium sheets

KLEMENT, J.

Originální název

Properties of laminate consisting of carbon prepregs and aluminium sheets

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

fibre metal laminate, mechanical properties, fatigue, forming limits

Autoři

KLEMENT, J.

Rok RIV

2004

Vydáno

1. 1. 2003

Nakladatel

VGTU

Místo

Vilnius

ISSN

1648-7788

Periodikum

AVIATION

Ročník

2003

Číslo

1

Stát

Litevská republika

Strany od

16

Strany do

21

Strany počet

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"
}