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

Kód výsledku v 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>
Výsledek na webu
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DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
Buckling and postbuckling of a large delaminated plate subjected to shear loading.
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Buckling and postbuckling of a large delaminated plate subjected to shear loading.
Popis výsledku anglicky
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.

Druh
J<sub>x</sub> - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
CEP obor
JI - Kompositní materiály
OECD FORD obor
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Rok uplatnění
2009
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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