000012699 001__ 12699
000012699 005__ 20160920162638.0
000012699 04107 $$aeng
000012699 046__ $$k2016-09-05
000012699 100__ $$aKahya, V.
000012699 24500 $$aVibration and buckling of laminated composite and sandwich beams with a shear-deformable layered finite element

000012699 24630 $$n6.$$pInsights and Innovations in Structural Engineering, Mechanics and Computation
000012699 260__ $$bTaylor and Francis Group, London, UK
000012699 506__ $$arestricted
000012699 520__ $$2eng$$aThis study presents a shear-deformable layered finite element for free vibration and buckling analyses of laminated composite and sandwich beams. The presented multilayered beam element consists of N-thin layers, and has five nodes including three axial, four vertical, and 3N rotational Degrees Of Freedom (DOFs). Number of total DOFs of this element is, thus, 3N  +  7. Delamination and slip between the layers are not allowed. Effect of shear deformation is considered according to the First-order Shear Theory (FSDT). Numerical results for natural frequencies and buckling loads of laminated beams with different boundary conditions and lamina stacking are presented. Comparisons show the results obtained agree well with those of previous works available in the literature.

000012699 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000012699 653__ $$a

000012699 7112_ $$aSixth International Conference on Structural Engineering, Mechanics and Computation$$cCape Town, South Africa$$d2016-09-05 / 2016-09-07$$gSEMC2016
000012699 720__ $$aKahya, V.
000012699 8560_ $$ffischerc@itam.cas.cz
000012699 8564_ $$s362246$$uhttp://invenio.itam.cas.cz/record/12699/files/147.pdf$$yOriginal version of the author's contribution as presented on CD, 147.pdf.
000012699 962__ $$r12552
000012699 980__ $$aPAPER