Detail publikačního výsledku

Damage tolerance behaviour of fibre metal laminate CARE

KLEMENT, J.; AUGUSTIN, P.; URÍK, T.

Originální název

Damage tolerance behaviour of fibre metal laminate CARE

Anglický název

Damage tolerance behaviour of fibre metal laminate CARE

Druh

Článek recenzovaný mimo WoS a Scopus

Originální abstrakt

"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.

Anglický abstrakt

"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.

Klíčová slova

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

Klíčová slova v angličtině

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

Autoři

KLEMENT, J.; AUGUSTIN, P.; URÍK, T.

Rok RIV

2012

Vydáno

19.03.2010

Nakladatel

Asociace leteckých výrobců

Místo

Praha

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Svazek

2010

Číslo

1

Stát

Česká republika

Strany od

56

Strany do

59

Strany počet

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"
}