Publication result detail

On buckling of a plate with multiple delaminations

OBDRŽÁLEK, V.; VRBKA, J.

Original Title

On buckling of a plate with multiple delaminations

English Title

On buckling of a plate with multiple delaminations

Type

Peer-reviewed article not indexed in WoS or Scopus

Original Abstract

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.

English abstract

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.

Keywords

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

Key words in English

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

Authors

OBDRŽÁLEK, V.; VRBKA, J.

RIV year

2011

Released

31.05.2010

Publisher

Association for Engineering Mechanics

ISBN

1802-1484

Periodical

Engineering Mechanics

Volume

17

Number

1

State

Czech Republic

Pages from

37

Pages to

47

Pages count

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"
}