Detail publikačního výsledku

On buckling of a plate with multiple delaminations

OBDRŽÁLEK, V.; VRBKA, J.

Originální název

On buckling of a plate with multiple delaminations

Anglický název

On buckling of a plate with multiple delaminations

Druh

Článek recenzovaný mimo WoS a Scopus

Originální abstrakt

Buckling behaviour of a small delaminated plate subjected to compression loading has been studied by means of the finite element analysis. The study shows several trends in the effect of number, orientation and through-the-thickness position of delaminations upon the buckling response. These findings could be used for evaluation of reliability of laminate structures which might be subjected to impact loading, such as aircraft structures.

Anglický abstrakt

Buckling behaviour of a small delaminated plate subjected to compression loading has been studied by means of the finite element analysis. The study shows several trends in the effect of number, orientation and through-the-thickness position of delaminations upon the buckling response. These findings could be used for evaluation of reliability of laminate structures which might be subjected to impact loading, such as aircraft structures.

Klíčová slova

fibre-metal laminate, plates, buckling, delamination, finite element analysis

Klíčová slova v angličtině

fibre-metal laminate, plates, buckling, delamination, finite element analysis

Autoři

OBDRŽÁLEK, V.; VRBKA, J.

Rok RIV

2011

Vydáno

31.05.2010

Nakladatel

Association for Engineering Mechanics

ISSN

1802-1484

Periodikum

Engineering Mechanics

Svazek

17

Číslo

1

Stát

Česká republika

Strany od

37

Strany do

47

Strany počet

11

BibTex

@article{BUT48610,
  author="Vít {Obdržálek} and Jan {Vrbka}",
  title="On buckling of a plate with multiple delaminations",
  journal="Engineering Mechanics",
  year="2010",
  volume="17",
  number="1",
  pages="37--47",
  issn="1802-1484"
}