Detail publikace

Buckling and postbuckling of a large delaminated plate subjected to shear loading.

OBDRŽÁLEK, V. VRBKA, J.

Anglický název

Buckling and postbuckling of a large delaminated plate subjected to shear loading.

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

Buckling and postbuckling behaviour of a laminated plate subjected to shear loading has been studied by means of the finite element analysis. The plate was assumed to contain either one or two circular delaminations of various diameters and of various out-of-plane and in-plane positions. The size of the plate corresponded to the size of laminate panels used in aircraft structures. It was therefore possible to asses the practical applicability of numerous studies which focused on the buckling behaviour of substantially smaller plates.

Klíčová slova anglicky

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

Vydáno

2009-10-30

Nakladatel

Engineering Academy of the Czech Republic, Národní 3, 117 20 Praha 1 on behalf of the Association for Engineering Mechanics.

Místo

Brno

ISSN

1210-2717

Časopis

Inženýrská mechanika – Engineering Mechanics

Ročník

2009 (16)

Číslo

4

Strany od–do

297–312

Počet stran

16

BIBTEX


@article{BUT49147,
  author="Vít {Obdržálek} and Jan {Vrbka}",
  title="Buckling and postbuckling of a large delaminated plate subjected to shear loading.",
  journal="Inženýrská mechanika - Engineering Mechanics",
  year="2009",
  volume="2009 (16)",
  number="4",
  pages="297--312",
  issn="1210-2717"
}