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

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F09%3APU85381" target="_blank" >RIV/00216305:26210/09:PU85381 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

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

Original language description

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.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JI - Composite materials

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2009

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Inženýrská mechanika - Engineering Mechanics

ISSN

1210-2717

e-ISSN

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Volume of the periodical

2009 (16)

Issue of the periodical within the volume

4

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

16

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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