Publication result detail

Damage tolerance behaviour of fibre metal laminate CARE

KLEMENT, J.; AUGUSTIN, P.; URÍK, T.

Original Title

Damage tolerance behaviour of fibre metal laminate CARE

English Title

Damage tolerance behaviour of fibre metal laminate CARE

Type

Peer-reviewed article not indexed in WoS or Scopus

Original Abstract

"Damage tolerance properties of hybrid laminate CARE consisting of 2024 alloy sheet and UD carbon/epoxy prepreg layers. Results of fatigue bending tests with constant deflection, including of hot/wet conditions, comparison with the monolithic metal alloy testing. Results of fatigue crack growth tests on CCT coupons under the flight spectrum loading, comparison with results of 2024 alloy testing.

English abstract

"Damage tolerance properties of hybrid laminate CARE consisting of 2024 alloy sheet and UD carbon/epoxy prepreg layers. Results of fatigue bending tests with constant deflection, including of hot/wet conditions, comparison with the monolithic metal alloy testing. Results of fatigue crack growth tests on CCT coupons under the flight spectrum loading, comparison with results of 2024 alloy testing.

Keywords

Fibrew metal laminate, fatigue, crack growth, hot/wet influence

Key words in English

Fibrew metal laminate, fatigue, crack growth, hot/wet influence

Authors

KLEMENT, J.; AUGUSTIN, P.; URÍK, T.

RIV year

2012

Released

19.03.2010

Publisher

Asociace leteckých výrobců

Location

Praha

ISBN

1211-877X

Periodical

Letecký zpravodaj

Volume

2010

Number

1

State

Czech Republic

Pages from

56

Pages to

59

Pages count

4

BibTex

@article{BUT74922,
  author="KLEMENT, J. and AUGUSTIN, P. and URÍK, T.",
  title="Damage tolerance behaviour of fibre metal laminate CARE",
  journal="Letecký zpravodaj",
  year="2010",
  volume="2010",
  number="1",
  pages="56--59",
  issn="1211-877X"
}