Napredna pretraga

Pregled bibliografske jedinice broj: 204511

ANALYSIS OF THE LAMINATED COMPOSITE PLATE UNDER COMBINED LOADS


Vnučec, Zdravko
ANALYSIS OF THE LAMINATED COMPOSITE PLATE UNDER COMBINED LOADS // "RIM 2005 – ; Development and Modernization of Production", ISBN 99589262-0-2 / Isak Karabegović, Milan Jurković, Vlatko Doleček (ur.).
Bihać, Bosna i Hercegovina: Društvo za robotiku BiH, 2005. str. 143-148 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)


Naslov
ANALYSIS OF THE LAMINATED COMPOSITE PLATE UNDER COMBINED LOADS

Autori
Vnučec, Zdravko

Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni

Izvornik
"RIM 2005 &#8211 ; Development and Modernization of Production", ISBN 99589262-0-2 / Isak Karabegović, Milan Jurković, Vlatko Doleček - Bihać, Bosna i Hercegovina : Društvo za robotiku BiH, 2005, 143-148

Skup
RIM 2005: 5th International Scientific Conference on Production Engineering

Mjesto i datum
Bihać, Bosna i Hercegovina, 14.-17.09.2005

Vrsta sudjelovanja
Predavanje

Vrsta recenzije
Međunarodna recenzija

Ključne riječi
Laminated composite material; elastic properties; plate; stress; strain

Sažetak
In paper, the numerical analysis performed to predict the engineering properties of the multilayered plate and the stress-strain distributions for various lamination angles of continuous fiber composite laminate is described. The computations of the stress and strain values for the angle-ply four-layered symmetric laminated plate with various lamination angles (+- alfa)s of laminas under combined loads are carried out. The analyzed laminate plates have been composed with unidirectional layers that were made from composite materials: the reinforcement fibers were E-glass, and as matrix material the epoxy resin were used. The engineering properties values of multilayered plate and several of the numerous results of the stress-strain distributions in the layers of the analyzed laminated plate subjected to known the force resultant Nx and bending moment resultant Mx graphically in diagrams are presented. The numerical results in this work were calculated by use of own made PC software that is prepared to analyzing of multilayered plate made from composite material.

Izvorni jezik
Engleski

Znanstvena područja
Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika

Napomena
COBIS.BH-ID 14365190



POVEZANOST RADA


Projekt / tema
0152015

Ustanove
Strojarski fakultet, Slavonski Brod