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

Title:

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

Creator:

Obdržálek, Vít and Vrbka, Jan

Identifier:

https://cdk.lib.cas.cz/client/handle/uuid:168b2019-5e43-4aef-abe7-f014b6d8b22e
uuid:168b2019-5e43-4aef-abe7-f014b6d8b22e

Subject:

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

Type:

model:article and TEXT

Format:

bez média and svazek

Description:

Buckling and postbuckling behaviour of a delaminated 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 delamintions of various diameteers 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 assess the practical applicability of numerous studies which focused on the buckling behaviour of substantially smaller plates. and Obsahuje seznam literatury

Language:

English

Rights:

http://creativecommons.org/licenses/by-nc-sa/4.0/
policy:public

Coverage:

297-312

Source:

Engineering mechanics: international journal for theoretical and applied mechanics | 2009 Volume:16 | Number:4

Harvested from:

CDK

Metadata only:

false