Pregled bibliografske jedinice broj: 204511
ANALYSIS OF THE LAMINATED COMPOSITE PLATE UNDER COMBINED LOADS
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: Društvo za robotiku Bosne i Hercegovine, 2005. str. 143-148 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
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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 – ; Development and Modernization of Production", ISBN 99589262-0-2
/ Isak Karabegović, Milan Jurković, Vlatko Doleček - Bihać : Društvo za robotiku Bosne i Hercegovine, 2005, 143-148
Skup
RIM 2005: 5th International Scientific Conference on Production Engineering
Mjesto i datum
Bihać, Bosna i Hercegovina, 14.09.2005. - 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