Publication detail

Damage tolerance behaviour of fibre metal laminate CARE

KLEMENT, J. AUGUSTIN, P. URÍK, T.

English title

Damage tolerance behaviour of fibre metal laminate CARE

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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.

Keywords in English

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

Released

2010-03-19

Publisher

Asociace leteckých výrobců

Location

Praha

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2010

Number

1

Pages from–to

56–59

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"
}